11 PHY discussion need in 24 hours
Cutnell & Johnson Physics
Eleventh Edition
DAVID YOUNG SHANE STADLER
Louisiana State University
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iii
About the Authors
DAVID YOUNG received his Ph.D. in experimental condensed matter physics from Florida State University in 1998. He then held a
post-doc position in the Department of Chemistry and the Princeton
Materials Institute at Princeton University before joining the fac-
ulty in the Department of Physics and Astronomy at Louisiana State
University in 2000. His research focuses on the synthesis and char-
acterization of high-quality single crystals of novel electronic and
magnetic materials. The goal of his research group is to understand
the physics of electrons in materials under extreme conditions, i.e.,
at temperatures close to absolute zero, in high magnetic fi elds, and
under high pressure. He is the coauthor of over 200 research publica-
tions that have appeared in peer-reviewed journals, such as Physical Review B, Physical Review Letters, and Nature. Professor Young has taught introductory physics with the Cutnell & Johnson text since he
was a senior undergraduate over 20 years ago. He routinely lectures
to large sections, often in excess of 300 students. To engage such a
large number of students, he uses WileyPLUS, electronic response systems, tutorial-style recitation sessions, and in-class demonstra-
tions. Professor Young has received multiple awards for outstanding
teaching of undergraduates. David enjoys spending his free time with
his family, playing basketball, and working on his house.
I would like to thank my family for their continuous love and support.
—David Young
SH ANE STADLER Shane Stadler earned a Ph.D. in experi- mental condensed matter physics from Tulane University in 1998.
Afterwards, he accepted a National Research Council Postdoctoral
Fellowship with the Naval Research Laboratory in Washington, DC,
where he conducted research on artifi cially structured magnetic ma-
terials. Three years later, he joined the faculty in the Department of
Physics at Southern Illinois University (the home institution of John
Cutnell and Ken Johnson, the original authors of this textbook), be-
fore joining the Department of Physics and Astronomy at Louisiana
State University in 2008. His research group studies novel magnetic
materials for applications in the areas of spintronics and magnetic
cooling.
Over the past fi fteen years, Professor Stadler has taught the full
spectrum of physics courses, from physics for students outside the
sciences, to graduate-level physics courses, such as classical electro-
dynamics. He teaches classes that range from fewer than ten students
to those with enrollments of over 300. His educational interests are
focused on developing teaching tools and methods that apply to both
small and large classes, and which are applicable to emerging teach-
ing strategies, such as “fl ipping the classroom.”
In his spare time, Shane writes science fi ction/thriller novels.
I would like to thank my parents, George and Elissa, for their constant
support and encouragement. —Shane Stadler
C o u rt
es y D
av id
Y o u n g
C o u rt
es y S
h an
e S
ta d le
r
Dear Students and Inst ructors:
Welcome to college ph ysics! To the students:
We know there is a ne gative stigma associate
d with physics, and yo u yourself may har-
bor some trepidation a s you begin this course
. But fear not! We’re h ere to help. Whether y
ou’re worried about yo ur math profi ciency,
understanding the con cepts, or developing yo
ur problem-solving ski lls, the resources avail
able to you are designe d to address all of
these areas and more. Research has shown th
at learning styles vary greatly among student
s. Maybe some of you have a more visual
preference, or auditory preference, or some o
ther preferred learning modality. In any case,
the resources availabl e to you in this course
will satisfy all of these preferences and impro
ve your chance of succ ess. Take a moment to
explore below what th e textbook and
online course have to o ff er. We suspect that, a
s you continue to impr ove throughout the cou
rse, some of that initia l trepidation will be
replaced with exciteme nt.
To start, we have creat ed a new learning med
ium specifi c to this boo k in the form of a comp
rehensive set of LECTURE VIDE OS – one
for every section (259 in all). These animated
lectures (created and n arrated by the authors)
are 2–10 minutes in le ngth, and explain the
basic concepts and lear ning objectives of each
section. They are assig nable within WileyPLU
S and can be paired wi th follow-up ques-
tions that are gradable. In addition to supplem
enting traditional lectu ring, the videos can be
used in a variety of wa ys, including fl ipping
the classroom, a comp lete set of lectures for o
nline courses, and revi ewing for exams. Next
, we have enhanced “T he Physics of …”
examples by increasing the bio-inspired exam
ples by 40%. Although they are of general ins
tructional value, they a re also similar to what
premed students will e ncounter in the Chemical and Ph
ysical Foundations of Biological Systems Passages section of the
MCAT. Finally,
we have introduced new “team problems” in th
e end-of-chapter proble ms that are designed fo
r group problem-solvin g exercises. These
are context-rich proble ms of medium diffi cult
y designed for group c ooperation, but may al
so be tackled by the in dividual student.
One of the great streng ths of this text is the sy
nergistic relationship i t develops between pro
blem solving and conc eptual understand-
ing. For instance, avail able in WileyPLUS are animated
Chalkboard Videos, which cons ist of short (2–3 min) v
ideos demonstrat-
ing step-by-step practi cal solutions to typical
homework problems. Also available are num
erous Guided Online (GO) Tuto rials that
implement a step-by-s tep pedagogical approa
ch, which provides stu dents a low-stakes env
ironment for refi ning t heir problem solving
skills. One of the most important techniques
developed in the text f or solving problems in
volving multiple force s is the free-body
diagram (FBD). Many problems in the force-intensive
chapters, such as chap ters 4 and 18, take adv
antage of the new FBD capabilities
now available online in WileyPLUS, where students can
construct the FBD’s f or a select number of p
roblems and be graded on them.
Finally, ORION, an online adapt ive learning environme
nt, is seamlessly integr ated into WileyPLUS for Cutnell
& Johnson.
The content and functi onality of WileyPLUS, and the a
daptive learning enviro nment of ORION (see below), w
ill provide students wi th
all the resources they n eed to be successful in
the course.
• The Lecture Videos created b y the authors for each
section include questio ns with intelligent feed
back when a student en ters the
wrong answer.
• The multi-step GO Tutorial p roblems created in WileyPLUS a
re designed to provide targeted, intelligent fe
edback.
• The Free-body Diagram vecto r drawing tools provid
e students an easy way to enter answers requi
ring vector drawing, an d also
provide enhanced feed back.
• Chalkboard Video Solutions t ake the students step-b
y-step through the solu tion and the thought pr
ocess of the authors. P roblem-
solving strategies are d iscussed, and common
misconceptions and p otential pitfalls are add
ressed. The students ca n then apply these
techniques to solve sim ilar, but diff erent probl
ems.
All of these features ar e designed to encourag
e students to remain w ithin the WileyPLUS environme
nt, as opposed to pursu ing the
“pay-for solutions” we bsites that short circui
t the learning process. To the students – We s
trongly recommend th at you take this honest
approach to the course . Take full advantage o
f the many features an d learning resources th
at accompany the text and the online con-
tent. Be engaged with the material and push
yourself to work throu gh the exercises. Physi
cs may not be the easie st subject to under-
stand, but with the Wi ley resources at your d
isposal and your hard w ork, you CAN be succ
essful.
We are immensely gra teful to all of you who
have provided feedbac k as we’ve worked on
this new edition, and t o our students who
have taught us how to teach. Thank you for y
our guidance, and keep the feedback coming.
Best wishes for succes s in this course and
wherever your major m ay take you!
Sincerely,
David Young and Shan e Stadler, Louisiana St
ate University
email: dyoun14@gma il.com or stadler.ls
iv
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v
Brief Contents
1 Introduction and Mathematical Concepts 1
2 Kinematics in One Dimension 27
3 Kinematics in Two Dimensions 55
4 Forces and Newton’s Laws of Motion 80
5 Dynamics of Uniform Circular Motion 121
6 Work and Energy 144
7 Impulse and Momentum 175
8 Rotational Kinematics 200
9 Rotational Dynamics 223
10 Simple Harmonic Motion and Elasticity 257
11 Fluids 289
12 Temperature and Heat 326
13 The Transfer of Heat 360
14 The Ideal Gas Law and Kinetic Theory 380
15 Thermodynamics 401
16 Waves and Sound 433
17 The Principle of Linear Superposition and Interference Phenomena 465
18 Electric Forces and Electric Fields 489
19 Electric Potential Energy and the Electric Potential 523
20 Electric Circuits 551
21 Magnetic Forces and Magnetic Fields 590
22 Electromagnetic Induction 625
23 Alternating Current Circuits 661
24 Electromagnetic Waves 684
25 The Reflection of Light: Mirrors 711
26 The Refraction of Light: Lenses and Optical Instruments 733
27 Interference and the Wave Nature of Light 777
28 Special Relativity 808
29 Particles and Waves 832
30 The Nature of the Atom 853
31 Nuclear Physics and Radioactivity 885
32 Ionizing Radiation, Nuclear Energy, and Elementary Particles 911
Contents
1 Introduction and Mathematical Concepts 1
1.1 The Nature of Physics 1 1.2 Units 2 1.3 The Role of Units in Problem Solving 3 1.4 Trigonometry 6 1.5 Scalars and Vectors 8 1.6 Vector Addition and Subtraction 10 1.7 The Components of a Vector 12 1.8 Addition of Vectors by Means of Components 15 Concept Summary 19 Focus on Concepts 19 Problems 21 Additional Problems 24 Concepts and Calculations Problems 25 Team Problems 26
2 Kinematics in One Dimension 27 2.1 Displacement 27 2.2 Speed and Velocity 28 2.3 Acceleration 31 2.4 Equations of Kinematics for Constant
Acceleration 34 2.5 Applications of the Equations of Kinematics 37 2.6 Freely Falling Bodies 41 2.7 Graphical Analysis of Velocity and
Acceleration 45 Concept Summary 47 Focus on Concepts 48 Problems 49 Additional Problems 53 Concepts and Calculations Problems 54 Team Problems 54
3 Kinematics in Two Dimensions 55 3.1 Displacement, Velocity, and Acceleration 55 3.2 Equations of Kinematics in Two Dimensions 56 3.3 Projectile Motion 60 3.4 Relative Velocity 68 Concept Summary 72 Focus on Concepts 73 Problems 74 Additional Problems 77 Concepts and Calculations Problems 78 Team Problems 79
4 Forces and Newton’s Laws of Motion 80 4.1 The Concepts of Force and Mass 80 4.2 Newton’s First Law of Motion 81 4.3 Newton’s Second Law of Motion 83 4.4 The Vector Nature of Newton’s Second Law of Motion 85 4.5 Newton’s Third Law of Motion 86 4.6 Types of Forces: An Overview 88 4.7 The Gravitational Force 88 4.8 The Normal Force 92 4.9 Static and Kinetic Frictional Forces 95 4.10 The Tension Force 101 4.11 Equilibrium Applications of Newton’s Laws
of Motion 102 4.12 Nonequilibrium Applications of Newton’s Laws
of Motion 106 Concept Summary 111 Focus on Concepts 112 Problems 114 Additional Problems 118 Concepts and Calculations Problems 119 Team Problems 120
5 Dynamics of Uniform Circular Motion 121
5.1 Uniform Circular Motion 121 5.2 Centripetal Acceleration 122 5.3 Centripetal Force 125 5.4 Banked Curves 129 5.5 Satellites in Circular Orbits 130 5.6 Apparent Weightlessness and Artificial Gravity 133 5.7 *Vertical Circular Motion 136 Concept Summary 137 Focus on Concepts 138 Problems 139 Additional Problems 141 Concepts and Calculations Problems 142 Team Problems 143
6 Work and Energy 144 6.1 Work Done by a Constant Force 144 6.2 The Work–Energy Theorem and Kinetic Energy 147 6.3 Gravitational Potential Energy 153 6.4 Conservative Versus Nonconservative Forces 155 6.5 The Conservation of Mechanical Energy 157 6.6 Nonconservative Forces and the Work–Energy
Theorem 161
Contents vii
6.7 Power 162 6.8 Other Forms of Energy and the Conservation
of Energy 164 6.9 Work Done by a Variable Force 164 Concept Summary 166 Focus on Concepts 167 Problems 168 Additional Problems 172 Concepts and Calculations Problems 173 Team Problems 174
7 Impulse and Momentum 175 7.1 The Impulse–Momentum Theorem 175 7.2 The Principle of Conservation of Linear
Momentum 179 7.3 Collisions in One Dimension 184 7.4 Collisions in Two Dimensions 189 7.5 Center of Mass 189 Concept Summary 192 Focus on Concepts 193 Problems 194 Additional Problems 197 Concepts and Calculations Problems 198 Team Problems 199
8 Rotational Kinematics 200 8.1 Rotational Motion and Angular Displacement 200 8.2 Angular Velocity and Angular Acceleration 203 8.3 The Equations of Rotational Kinematics 205 8.4 Angular Variables and Tangential Variables 208 8.5 Centripetal Acceleration and Tangential
Acceleration 210 8.6 Rolling Motion 213 8.7 *The Vector Nature of Angular Variables 214 Concept Summary 215 Focus on Concepts 216 Problems 216 Additional Problems 220 Concepts and Calculations Problems 221 Team Problems 222
9 Rotational Dynamics 223 9.1 The Action of Forces and Torques on Rigid
Objects 223 9.2 Rigid Objects in Equilibrium 226 9.3 Center of Gravity 231 9.4 Newton’s Second Law for Rotational Motion About a
Fixed Axis 236 9.5 Rotational Work and Energy 241 9.6 Angular Momentum 244
Concept Summary 246 Focus on Concepts 247 Problems 248 Additional Problems 254 Concepts and Calculations Problems 255 Team Problems 256
10 Simple Harmonic Motion and Elasticity 257
10.1 The Ideal Spring and Simple Harmonic Motion 257 10.2 Simple Harmonic Motion and the Reference Circle 261 10.3 Energy and Simple Harmonic Motion 267 10.4 The Pendulum 270 10.5 Damped Harmonic Motion 273 10.6 Driven Harmonic Motion and Resonance 274 10.7 Elastic Deformation 275 10.8 Stress, Strain, and Hooke’s Law 279 Concept Summary 280 Focus on Concepts 281 Problems 282 Additional Problems 287 Concepts and Calculations Problems 288 Team Problems 288
11 Fluids 289 11.1 Mass Density 289 11.2 Pressure 291 11.3 Pressure and Depth in a Static Fluid 293 11.4 Pressure Gauges 297 11.5 Pascal’s Principle 298 11.6 Archimedes’ Principle 300 11.7 Fluids in Motion 305 11.8 The Equation of Continuity 307 11.9 Bernoulli’s Equation 309 11.10 Applications of Bernoulli’s Equation 311 11.11 *Viscous Flow 314 Concept Summary 317 Focus on Concepts 318 Problems 319 Additional Problems 323 Concepts and Calculations Problems 324 Team Problems 325
12 Temperature and Heat 326 12.1 Common Temperature Scales 326 12.2 The Kelvin Temperature Scale 328 12.3 Thermometers 329 12.4 Linear Thermal Expansion 330 12.5 Volume Thermal Expansion 337 12.6 Heat and Internal Energy 339
12.7 Heat and Temperature Change: Specific Heat Capacity 340
12.8 Heat and Phase Change: Latent Heat 343 12.9 *Equilibrium Between Phases of Matter 347 12.10 *Humidity 350 Concept Summary 352 Focus on Concepts 352 Problems 353 Additional Problems 358 Concepts and Calculations Problems 358 Team Problems 359
13 The Transfer of Heat 360 13.1 Convection 360 13.2 Conduction 363 13.3 Radiation 370 13.4 Applications 373 Concept Summary 375 Focus on Concepts 375 Problems 376 Additional Problems 378 Concepts and Calculations Problems 379 Team Problems 379
14 The Ideal Gas Law and Kinetic Theory 380
14.1 Molecular Mass, the Mole, and Avogadro’s Number 380 14.2 The Ideal Gas Law 383 14.3 Kinetic Theory of Gases 388 14.4 *Diff usion 392 Concept Summary 395 Focus on Concepts 396 Problems 397 Additional Problems 399 Concepts and Calculations Problems 400 Team Problems 400
15 Thermodynamics 401 15.1 Thermodynamic Systems and Their Surroundings 401 15.2 The Zeroth Law of Thermodynamics 402 15.3 The First Law of Thermodynamics 402 15.4 Thermal Processes 404 15.5 Thermal Processes Using an Ideal Gas 408 15.6 Specific Heat Capacities 411 15.7 The Second Law of Thermodynamics 412 15.8 Heat Engines 413 15.9 Carnot’s Principle and the Carnot Engine 414 15.10 Refrigerators, Air Conditioners, and Heat Pumps 417 15.11 Entropy 420 15.12 The Third Law of Thermodynamics 425
Concept Summary 425 Focus on Concepts 426 Problems 427 Additional Problems 431 Concepts and Calculations Problems 432 Team Problems 432
16 Waves and Sound 433 16.1 The Nature of Waves 433 16.2 Periodic Waves 435 16.3 The Speed of a Wave on a String 436 16.4 *The Mathematical Description of a Wave 439 16.5 The Nature of Sound 439 16.6 The Speed of Sound 442 16.7 Sound Intensity 446 16.8 Decibels 448 16.9 The Doppler Eff ect 450 16.10 Applications of Sound in Medicine 454 16.11 *The Sensitivity of the Human Ear 455 Concept Summary 456 Focus on Concepts 457 Problems 458 Additional Problems 463 Concepts and Calculations Problems 464 Team Problems 464
17 The Principle of Linear Superposition and Interference Phenomena 465
17.1 The Principle of Linear Superposition 465 17.2 Constructive and Destructive Interference of
Sound Waves 466 17.3 Diff raction 470 17.4 Beats 473 17.5 Transverse Standing Waves 474 17.6 Longitudinal Standing Waves 478 17.7 *Complex Sound Waves 481 Concept Summary 482 Focus on Concepts 483 Problems 484 Additional Problems 487 Concepts and Calculations Problems 488 Team Problems 488
18 Electric Forces and Electric Fields 489 18.1 The Origin of Electricity 489 18.2 Charged Objects and the Electric Force 490 18.3 Conductors and Insulators 493 18.4 Charging by Contact and by Induction 493 18.5 Coulomb’s Law 495 18.6 The Electric Field 500
viii Contents
Contents ix
18.7 Electric Field Lines 505 18.8 The Electric Field Inside a Conductor: Shielding 508 18.9 Gauss’ Law 510 18.10 *Copiers and Computer Printers 513 Concept Summary 516 Focus on Concepts 516 Problems 517 Additional Problems 521 Concepts and Calculations Problems 521 Team Problems 522
19 Electric Potential Energy and the Electric Potential 523
19.1 Potential Energy 523 19.2 The Electric Potential Diff erence 524 19.3 The Electric Potential Diff erence Created by Point
Charges 530 19.4 Equipotential Surfaces and Their Relation to the
Electric Field 534 19.5 Capacitors and Dielectrics 537 19.6 *Biomedical Applications of Electric Potential
Diff erences 541 Concept Summary 544 Focus on Concepts 544 Problems 546 Additional Problems 548 Concepts and Calculations Problems 549 Team Problems 550
20 Electric Circuits 551 20.1 Electromotive Force and Current 551 20.2 Ohm’s Law 553 20.3 Resistance and Resistivity 554 20.4 Electric Power 557 20.5 Alternating Current 559 20.6 Series Wiring 562 20.7 Parallel Wiring 565 20.8 Circuits Wired Partially in Series and Partially in
Parallel 569 20.9 Internal Resistance 570 20.10 Kirchhoff ’s Rules 571 20.11 The Measurement of Current and Voltage 574 20.12 Capacitors in Series and in Parallel 575 20.13 RC Circuits 577 20.14 Safety and the Physiological Eff ects of Current 579 Concept Summary 580 Focus on Concepts 581 Problems 582 Additional Problems 588 Concepts and Calculations Problems 589 Team Problems 589
21 Magnetic Forces and Magnetic Fields 590
21.1 Magnetic Fields 590 21.2 The Force That a Magnetic Field Exerts on a Moving
Charge 592 21.3 The Motion of a Charged Particle in a Magnetic Field 595 21.4 The Mass Spectrometer 599 21.5 The Force on a Current in a Magnetic Field 600 21.6 The Torque on a Current-Carrying Coil 602 21.7 Magnetic Fields Produced by Currents 605 21.8 Ampère’s Law 612 21.9 Magnetic Materials 613 Concept Summary 616 Focus on Concepts 617 Problems 618 Additional Problems 623 Concepts and Calculations Problems 624 Team Problems 624
22 Electromagnetic Induction 625 22.1 Induced Emf and Induced Current 625 22.2 Motional Emf 627 22.3 Magnetic Flux 631 22.4 Faraday’s Law of Electromagnetic Induction 634 22.5 Lenz’s Law 637 22.6 *Applications of Electromagnetic Induction to the
Reproduction of Sound 640 22.7 The Electric Generator 641 22.8 Mutual Inductance and Self-Inductance 646 22.9 Transformers 649 Concept Summary 652 Focus on Concepts 653 Problems 654 Additional Problems 659 Concepts and Calculations Problems 659 Team Problems 660
23 Alternating Current Circuits 661 23.1 Capacitors and Capacitive Reactance 661 23.2 Inductors and Inductive Reactance 664 23.3 Circuits Containing Resistance, Capacitance, and
Inductance 665 23.4 Resonance in Electric Circuits 670 23.5 Semiconductor Devices 672 Concept Summary 678 Focus on Concepts 679 Problems 680 Additional Problems 681 Concepts and Calculations Problems 682 Team Problems 683
24 Electromagnetic Waves 684 24.1 The Nature of Electromagnetic Waves 684 24.2 The Electromagnetic Spectrum 688 24.3 The Speed of Light 690 24.4 The Energy Carried by Electromagnetic Waves 692 24.5 The Doppler Eff ect and Electromagnetic Waves 695 24.6 Polarization 697 Concept Summary 704 Focus on Concepts 704 Problems 705 Additional Problems 708 Concepts and Calculations Problems 709 Team Problems 710
25 The Reflection of Light: Mirrors 711 25.1 Wave Fronts and Rays 711 25.2 The Reflection of Light 712 25.3 The Formation of Images by a Plane Mirror 713 25.4 Spherical Mirrors 716 25.5 The Formation of Images by Spherical Mirrors 718 25.6 The Mirror Equation and the Magnification
Equation 722 Concept Summary 728 Focus on Concepts 728 Problems 729 Additional Problems 731 Concepts and Calculations Problems 731 Team Problems 732
26 The Refraction of Light: Lenses and Optical Instruments 733
26.1 The Index of Refraction 733 26.2 Snell’s Law and the Refraction of Light 734 26.3 Total Internal Reflection 739 26.4 Polarization and the Reflection and Refraction of
Light 745 26.5 The Dispersion of Light: Prisms and Rainbows 746 26.6 Lenses 748 26.7 The Formation of Images by Lenses 749 26.8 The Thin-Lens Equation and the Magnification
Equation 752 26.9 Lenses in Combination 755 26.10 The Human Eye 756 26.11 Angular Magnification and the Magnifying Glass 761 26.12 The Compound Microscope 763 26.13 The Telescope 764 26.14 Lens Aberrations 765 Concept Summary 767 Focus on Concepts 768 Problems 769
Additional Problems 775 Concepts and Calculations Problems 775 Team Problems 776
27 Interference and the Wave Nature of Light 777
27.1 The Principle of Linear Superposition 777 27.2 Young’s Double-Slit Experiment 779 27.3 Thin-Film Interference 782 27.4 The Michelson Interferometer 786 27.5 Diff raction 787 27.6 Resolving Power 791 27.7 The Diff raction Grating 796 27.8 *Compact Discs, Digital Video Discs, and the Use of
Interference 798 27.9 X-Ray Diff raction 799 Concept Summary 801 Focus on Concepts 802 Problems 803 Additional Problems 805 Concepts and Calculations Problems 806 Team Problems 807
28 Special Relativity 808 28.1 Events and Inertial Reference Frames 808 28.2 The Postulates of Special Relativity 809 28.3 The Relativity of Time: Time Dilation 811 28.4 The Relativity of Length: Length Contraction 815 28.5 Relativistic Momentum 817 28.6 The Equivalence of Mass and Energy 819 28.7 The Relativistic Addition of Velocities 824 Concept Summary 827 Focus on Concepts 827 Problems 828 Additional Problems 830 Concepts and Calculations Problems 831 Team Problems 831
29 Particles and Waves 832 29.1 The Wave–Particle Duality 832 29.2 Blackbody Radiation and Planck’s Constant 833 29.3 Photons and the Photoelectric Eff ect 834 29.4 The Momentum of a Photon and the Compton
Eff ect 840 29.5 The De Broglie Wavelength and the Wave Nature
of Matter 843 29.6 The Heisenberg Uncertainty Principle 845 Concept Summary 849 Focus on Concepts 849 Problems 850
x Contents
Contents xi
Additional Problems 852 Concepts and Calculations Problems 852 Team Problems 852
30 The Nature of the Atom 853 30.1 Rutherford Scattering and the Nuclear Atom 853 30.2 Line Spectra 855 30.3 The Bohr Model of the Hydrogen Atom 857 30.4 De Broglie’s Explanation of Bohr’s Assumption About
Angular Momentum 861 30.5 The Quantum Mechanical Picture of the Hydrogen
Atom 862 30.6 The Pauli Exclusion Principle and the Periodic Table of
the Elements 866 30.7 X-Rays 868 30.8 The Laser 872 30.9 *Medical Applications of the Laser 874 30.10 *Holography 876 Concept Summary 878 Focus on Concepts 879 Problems 880 Additional Problems 883 Concepts and Calculations Problems 883 Team Problems 883
31 Nuclear Physics and Radioactivity 885 31.1 Nuclear Structure 885 31.2 The Strong Nuclear Force and the Stability of the
Nucleus 887 31.3 The Mass Defect of the Nucleus and Nuclear Binding
Energy 888 31.4 Radioactivity 890 31.5 The Neutrino 896 31.6 Radioactive Decay and Activity 897 31.7 Radioactive Dating 900 31.8 Radioactive Decay Series 903 31.9 Radiation Detectors 904
Concept Summary 906 Focus on Concepts 907 Problems 908 Additional Problems 910 Concepts and Calculations Problems 910 Team Problems 910
32 Ionizing Radiation, Nuclear Energy, and Elementary Particles 911
32.1 Biological Eff ects of Ionizing Radiation 911 32.2 Induced Nuclear Reactions 915 32.3 Nuclear Fission 916 32.4 Nuclear Reactors 919 32.5 Nuclear Fusion 920 32.6 Elementary Particles 922 32.7 Cosmology 928 Concept Summary 931 Focus on Concepts 932 Problems 932 Additional Problems 934 Concepts and Calculations Problems 935 Team Problems 935
Appendixes A-1
APPENDIX A Powers of Ten and Scientific Notation A-1 APPENDIX B Significant Figures A-1 APPENDIX C Algebra A-2 APPENDIX D Exponents and Logarithms A-3 APPENDIX E Geometry and Trigonometry A-4 APPENDIX F Selected Isotopes A-5
ANSWERS TO CHECK YOUR UNDERSTANDING A-10
ANSWERS TO ODD-NUMBERED PROBLEMS A-18
INDEX I -1
Note: Chapter sections marked with an asterisk (*) can be omitted with little impact to the overall development of the material.
Our Vision Our goal is to provide students with the skills they need to succeed in this course, and instructors with the tools they need to develop those skills.
Skills Development One of the great strengths of this text is the synergistic relationship
between conceptual understanding, problem solving, and establish-
ing relevance. We identify here some of the core features of the text
that support these synergies.
Conceptual Understanding Students often regard physics as a collection of equations that can be used blindly to solve problems. How-
ever, a good problem-solving technique does not begin with equations. It
starts with a fi rm grasp of physics concepts and how they fi t together to
provide a coherent description of natural phenomena. Helping students
develop a conceptual understanding of physics principles is a primary
goal of this text. The features in the text that work toward this goal are:
• Lecture Videos (one for each section of the text) • Conceptual Examples • Concepts & Calculations problems (now with video solutions) • Focus on Concepts homework material • Check Your Understanding questions • Concept Simulations (an online feature)
Problem Solving The ability to reason in an organized and mathematically correct manner is essential to solving problems, and
helping students to improve their reasoning skills is also one of our
primary goals. To this end, we have included the following features:
• Math Skills boxes for just-in-time delivery of math support • Explicit reasoning steps in all examples • Reasoning Strategies for solving certain classes of problems • Analyzing Multiple-Concept Problems • Video Support and Tutorials (in WileyPLUS)
Physics Demonstration Videos
Video Help
Concept Simulations
• Problem Solving Insights
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we take for granted in our lives (for example, household plumbing). To
call attention to the applications we have used the label The Physics of.
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Chemical and Physical Foundations of Biological Systems Passages section of the MCAT. All biomedical examples and end-of-chapter
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EXAMPLE 7 BIO The Physics of Hearing Loss— Standing Waves in the Ear
Inner ear
Semicircular canals
Anvil
Hammer
Cochlea
Auditory nerve
Eustachian tubeOval
window Stirrup
Middle ear
Tympanic membrane
Outer ear
Auditory canal
Pinna
2.3 cm
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xvi Our V is ion and the Wi leyPLUS with ORION Advantage
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About the cover: The cover image shows an artist’s rendition of a synaptic gap between an axon and a dendrite of a human nerve cell. Just like
the wires in the electrical system of your home, the nerve cells make connec-
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In spite of our best eff orts to produce an error-free book, errors no doubt remain. They are solely our responsibility, and we would appreciate hearing of any that
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at [email protected] or [email protected].
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
1.1 Describe the fundamental nature of physics.
1.2 Describe diff erent systems of units.
1.3 Solve unit conversion problems.
1.4 Solve trigonometry problems.
1.5 Distinguish between vectors and scalars.
1.6 Solve vector addition and subtraction problems by graphical methods.
1.7 Calculate vector components.
1.8 Solve vector addition and subtraction problems using components.
P h o to
1 2 /A
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P h o to
CHAPTER 1
Introduction and Mathematical Concepts
The animation techniques and special eff ects used in the fi lm The Avengers rely on computers and mathematical concepts such as trigonometry and vectors. Such mathematical concepts will be very useful
throughout this book in our discussion of physics.
1.1 The Nature of Physics Physics is the most basic of the sciences, and it is at the very root of subjects like chem-
istry, engineering, astronomy, and even biology. The discipline of physics has developed
over many centuries, and it continues to evolve. It is a mature science, and its laws en-
compass a wide scope of phenomena that range from the formation of galaxies to the in-
teractions of particles in the nuclei of atoms. Perhaps the most visible evidence of physics
in everyday life is the eruption of new applications that have improved our quality of life,
such as new medical devices, and advances in computers and high-tech communications.
The exciting feature of physics is its capacity for predicting how nature will be-
have in one situation on the basis of experimental data obtained in another situation.
Such predictions place physics at the heart of modern technology and, therefore, can
have a tremendous impact on our lives. Rocketry and the development of space travel
have their roots fi rmly planted in the physical laws of Galileo Galilei (1564–1642) and
Isaac Newton (1642–1727). The transportation industry relies heavily on physics in
the development of engines and the design of aerodynamic vehicles. Entire electronics
and computer industries owe their existence to the invention of the transistor, which
grew directly out of the laws of physics that describe the electrical behavior of solids.
The telecommunications industry depends extensively on electromagnetic waves, 1
2 CHAPTER 1 Introduction and Mathematical Concepts
whose existence was predicted by James Clerk Maxwell (1831–1879) in his theory of electricity and magnetism. The medical profession uses X-ray, ultrasonic, and magnetic resonance methods for obtaining images of the interior of the human body, and physics lies at the core of all these. Perhaps the most widespread impact in modern technology is that due to the laser. Fields ranging from space exploration to medicine benefi t from this incredible device, which is a direct applica- tion of the principles of atomic physics.
Because physics is so fundamental, it is a required course for students in a wide range of major areas. We welcome you to the study of this fascinating topic. You will learn how to see the world through the “eyes” of physics and to reason as a physicist does. In the process, you will learn how to apply physics principles to a wide range of problems. We hope that you will come to recognize that physics has important things to say about your environment.
1.2 Units Physics experiments involve the measurement of a variety of quantities, and a great deal of eff ort goes into making these measurements as accurate and reproducible as possible. The fi rst step toward ensuring accuracy and reproducibility is defi ning the units in which the measurements are made.
In this text, we emphasize the system of units known as SI units, which stands for the French phrase “Le Système International d’Unités.” By international agreement, this system employs the meter (m) as the unit of length, the kilogram (kg) as the unit of mass, and the second (s) as the unit of time. Two other systems of units are also in use, however. The CGS system utilizes the centimeter (cm), the gram (g), and the second for length, mass, and time, respectively, and the BE or British Engineering system (the gravitational version) uses the foot (ft), the slug (sl), and the second. Table 1.1 summarizes the units used for length, mass, and time in the three systems.
Originally, the meter was defi ned in terms of the distance measured along the earth’s surface between the north pole and the equator. Eventually, a more accurate measurement standard was needed, and by international agreement the meter became the distance between two marks on a bar of platinum–iridium alloy (see Figure 1.1) kept at a temperature of 0 °C. Today, to meet further demands for increased accuracy, the meter is defi ned as the distance that light travels in a vacuum in a time of 1/299 792 458 second. This defi nition arises because the speed of light is a universal constant that is defi ned to be 299 792 458 m/s.
The defi nition of a kilogram as a unit of mass has also undergone changes over the years. As Chapter 4 discusses, the mass of an object indicates the tendency of the object to continue in motion with a constant velocity. Originally, the kilogram was expressed in terms of a specifi c amount of water. Today, one kilogram is defi ned to be the mass of a standard cylinder of platinum– iridium alloy, like the one in Figure 1.2.
As with the units for length and mass, the present defi nition of the second as a unit of time is diff erent from the original defi nition. Originally, the second was defi ned according to the average time for the earth to rotate once about its axis, one day being set equal to 86 400 seconds. The earth’s rotational motion was chosen because it is naturally repetitive, occurring over and over again. Today, we still use a naturally occurring repetitive phenomenon to defi ne the second, but of a very diff erent kind. We use the electromagnetic waves emitted by cesium-133 atoms in an atomic clock like that in Figure 1.3. One second is defi ned as the time needed for 9 192 631 770 wave cycles to occur.*
The units for length, mass, and time, along with a few other units that will arise later, are regarded as base SI units. The word “base” refers to the fact that these units are used along with
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IS T
A rc
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s
FIGURE 1.1 The standard platinum–iridium meter bar.
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So ur
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FIGURE 1.2 The standard platinum–iridium kilogram is kept at the International Bureau of Weights and Measures in Sèvres, France. This copy of it was assigned to the United States in 1889 and is housed at the National Institute of Standards and Technology.
© G
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FIGURE 1.3 This atomic clock, the NIST-F1, keeps time with an uncertainty of about one second in sixty million years. *See Chapter 16 for a discussion of waves in general and Chapter 24 for a discussion of electromagnetic waves in particular.
TABLE 1.1 Units of Measurement
System SI CGS BE
Length Meter (m) Centimeter (cm) Foot (ft)
Mass Kilogram (kg) Gram (g) Slug (sl)
Time Second (s) Second (s) Second (s)
1.3 The Role of Units in Problem Solving 3
various laws to defi ne additional units for other important physical quantities, such as force and energy. The units for such other physical quantities are referred to as derived units, since they are combinations of the base units. Derived units will be introduced from time to time, as they arise naturally along with the related physical laws.
The value of a quantity in terms of base or derived units is sometimes a very large or very small number. In such cases, it is convenient to introduce larger or smaller units that are related to the normal units by multiples of ten. Table 1.2 summarizes the prefi xes that are used to denote multiples of ten. For example, 1000 or 103 meters are referred to as 1 kilometer (km), and 0.001 or 10 −3 meter is called 1 millimeter (mm). Similarly, 1000 grams and 0.001 gram are referred to as 1 kilogram (kg) and 1 milligram (mg), respectively. Appendix A contains a discussion of scientifi c notation and powers of ten, such as 103 and 10 −3.
1.3 The Role of Units in Problem Solving The Conversion of Units Since any quantity, such as length, can be measured in several diff erent units, it is important to know how to convert from one unit to another. For instance, the foot can be used to express the distance between the two marks on the standard platinum–iridium meter bar. There are 3.281 feet in one meter, and this number can be used to convert from meters to feet, as the following example demonstrates.
TABLE 1.2 Standard Prefixes Used to Denote Multiples of Ten
Prefix Symbol Factora
tera T 1012
giga G 109
mega M 106
kilo k 103
hecto h 102
deka da 101
deci d 10−1
centi c 10−2
milli m 10−3
micro μ 10−6
nano n 10−9
pico p 10−12
femto f 10−15
aAppendix A contains a discussion of powers of ten and
scientific notation.
EXAMPLE 1 The World’s Highest Waterfall
The highest waterfall in the world is Angel Falls in Venezuela, with a total drop of 979.0 m (see Figure 1.4). Express this drop in feet.
Reasoning When converting between units, we write down the units explicitly in the calculations and treat them like any algebraic quantity. In particular, we will take advantage of the following algebraic fact: Multiplying or dividing an equation by a factor of 1 does not alter an equation.
Solution Since 3.281 feet = 1 meter, it follows that (3.281 feet)/ (1 meter) = 1. Using this factor of 1 to multiply the equation “Length = 979.0 meters,” we fi nd that
Length = (979.0 m)(1) = (979.0 meters) (3.281 feet1 meter ) = 3212 feet The colored lines emphasize that the units of meters behave like any al- gebraic quantity and cancel when the multiplication is performed, leaving only the desired unit of feet to describe the answer. In this regard, note that 3.281 feet = 1 meter also implies that (1 meter)/(3.281 feet) = 1. However, we chose not to multiply by a factor of 1 in this form, because the units of meters would not have canceled.
A calculator gives the answer as 3212.099 feet. Standard proced- ures for signifi cant fi gures, however, indicate that the answer should be rounded off to four signifi cant fi gures, since the value of 979.0 meters is accurate to only four signifi cant fi gures. In this regard, the “1 meter” in the denominator does not limit the signifi cant fi gures of the answer, be- cause this number is precisely one meter by defi nition of the conversion factor. Appendix B contains a review of signifi cant fi gures. ©
A nd
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FIGURE 1.4 Angel Falls in Venezuela is the highest waterfall in the world.
Problem-Solving Insight In any conversion, if the units do not combine algebraically to give the desired result, the conversion has not been carried out properly.
4 CHAPTER 1 Introduction and Mathematical Concepts
EXAMPLE 2 Interstate Speed Limit
Express the speed limit of 65 miles/hour in terms of meters/second.
Reasoning As in Example 1, it is important to write down the units explicitly in the calculations and treat them like any algebraic quantity. Here, we take advantage of two well-known relationships—namely, 5280 feet = 1 mile and 3600 seconds = 1 hour. As a result, (5280 feet)/ (1 mile) = 1 and (3600 seconds)/(1 hour) = 1. In our solution we will use the fact that multiplying and dividing by these factors of unity does not alter an equation.
Solution Multiplying and dividing by factors of unity, we fi nd the speed limit in feet per second as shown below:
Speed = (65 mileshour ) (1)(1) =
(65 mileshour ) ( 5280 feet
1 mile ) ( 1 hour
3600 seconds) = 95 feet
second
To convert feet into meters, we use the fact that (1 meter)/(3.281 feet) = 1:
Speed = (95 feetsecond) (1) =
(95 feetsecond) ( 1 meter
3.281 feet) = 29 meters second
In addition to their role in guiding the use of conversion factors, units serve a useful purpose in solving problems. They can provide an internal check to eliminate errors, if they are carried along during each step of a calculation and treated like any algebraic factor.
Problem-Solving Insight In particular, remember that only quantities with the same units can be added or subtracted.
Thus, at one point in a calculation, if you fi nd yourself adding 12 miles to 32 kilometers, stop and reconsider. Either miles must be converted into kilometers or kilometers must be converted into miles before the addition can be carried out.
A collection of useful conversion factors is given on the page facing the inside of the front cover. The reasoning strategy that we have followed in Examples 1 and 2 for converting between units is outlined as follows:
REASONING STRATEGY Converting Between Units 1. In all calculations, write down the units explicitly. 2. Treat all units as algebraic quantities. In particular, when identical units are divided,
they are eliminated algebraically. 3. Use the conversion factors located on the page facing the inside of the front cover. Be
guided by the fact that multiplying or dividing an equation by a factor of 1 does not alter the equation. For instance, the conversion factor of 3.281 feet = 1 meter might be applied in the form (3.281 feet)/(1 meter) = 1. This factor of 1 would be used to multiply an equa- tion such as “Length = 5.00 meters” in order to convert meters to feet.
4. Check to see that your calculations are correct by verifying that the units combine algeb- raically to give the desired unit for the answer. Only quantities with the same units can be added or subtracted.
Sometimes an equation is expressed in a way that requires specifi c units to be used for the variables in the equation. In such cases it is important to understand why only certain units can be used in the equation, as the following example illustrates.
EXAMPLE 3 BIO The Physics of the Body Mass Index
The body mass index (BMI) takes into account your mass in kilograms (kg) and your height in meters (m) and is defi ned as follows:
BMI = Mass in kg
(Height in m)2
However, the BMI is often computed using the weight* of a person in pounds (lb) and his or her height in inches (in.). Thus, the expression for the BMI incorporates these quantities, rather than the mass in kilograms and the height in meters. Starting with the defi nition above, determine the expression for the BMI that uses pounds and inches.
*Weight and mass are different concepts, and the relationship between them will be discussed in Section 4.7.
With this in mind, the next example stresses the importance of writing down the units and illustrates a typical situation in which several conversions are required.
1.3 The Role of Units in Problem Solving 5
Dimensional Analysis We have seen that many quantities are denoted by specifying both a number and a unit. For
example, the distance to the nearest telephone may be 8 meters, or the speed of a car might be
25 meters/second. Each quantity, according to its physical nature, requires a certain type of unit. Distance must be measured in a length unit such as meters, feet, or miles, and a time unit will not
do. Likewise, the speed of an object must be specifi ed as a length unit divided by a time unit. In
physics, the term dimension is used to refer to the physical nature of a quantity and the type of unit used to specify it. Distance has the dimension of length, which is symbolized as [L], while
speed has the dimensions of length [L] divided by time [T], or [L/T]. Many physical quantities
can be expressed in terms of a combination of fundamental dimensions such as length [L], time
[T], and mass [M]. Later on, we will encounter certain other quantities, such as temperature,
which are also fundamental. A fundamental quantity like temperature cannot be expressed as a
combination of the dimensions of length, time, mass, or any other fundamental dimension.
Dimensional analysis is used to check mathematical relations for the consistency of their
dimensions. As an illustration, consider a car that starts from rest and accelerates to a speed υ in a time t. Suppose we wish to calculate the distance x traveled by the car but are not sure whether the correct relation is x = 12 𝜐t
2 or x = 12 𝜐t. We can decide by checking the quantities on both sides of the equals sign to see whether they have the same dimensions. If the dimensions are not the
same, the relation is incorrect. For x = 12 𝜐t 2, we use the dimensions for distance [L], time [T], and
speed [L/T] in the following way:
x = 12 𝜐t 2
Dimensions [L] ≟ [ LT ] [T]2 = [L][T] Dimensions cancel just like algebraic quantities, and pure numerical factors like
1
2 have no dimen-
sions, so they can be ignored. The dimension on the left of the equals sign does not match those
on the right, so the relation x = 12 𝜐t 2 cannot be correct. On the other hand, applying dimensional
analysis to x = 12 𝜐t, we fi nd that
x = 12 𝜐t 2
Dimensions [L] ≟ [ LT ] [T] = [L]
Reasoning We will begin with the BMI defi nition and work separately with the numerator and the denominator. We will determine the mass in
kilograms that appears in the numerator from the weight in pounds by using
the fact that 1 kg corresponds to 2.205 lb. Then, we will determine the height
in meters that appears in the denominator from the height in inches with the
aid of the facts that 1 m = 3.281 ft and 1 ft = 12 in. These conversion factors
are located on the page facing the inside of the front cover of the text.
Solution Since 1 kg corresponds to 2.205 lb, the mass in kilograms can be determined from the weight in pounds in the following way:
Mass in kg = (Weight in lb)( 1 kg
2.205 lb) Since 1 ft = 12 in. and 1 m = 3.281 ft, we have
Height in m = (Height in in.)( 1 ft12 in.)( 1 m
3.281 ft) Substituting these results into the numerator and denominator of the BMI
defi nition gives
BMI = Mass in kg
(Height in m)2 =
(Weight in lb)( 1 kg
2.205 lb) (Height in in.)2 ( 1 ft12 in.)
2
( 1 m3.281 ft) 2
= ( 1 kg
2.205 lb)( 12 in.
1 ft ) 2
(3.281 ft1 m ) 2 (Weight in lb)
(Height in in.)2
BMI = (703.0 kg · in.2
lb · m2 ) (Weight in lb)
(Height in in.)2
For example, if your weight and height are 180 lb and 71 in., your body
mass index is 25 kg/m2. The BMI can be used to assess approximately
whether your weight is normal for your height (see Table 1.3).
TABLE 1.3 The Body Mass Index
BMI (kg/m2) Evaluation Below 18.5 Underweight
18.5–24.9 Normal
25.0–29.9 Overweight
30.0–39.9 Obese
40 and above Morbidly obese
6 CHAPTER 1 Introduction and Mathematical Concepts
Problem-Solving Insight You can check for errors that may have arisen during algebraic manipulations by performing a dimensional analysis on the fi nal expression.
The dimension on the left of the equals sign matches that on the right, so this relation is dimen- sionally correct. If we know that one of our two choices is the right one, then x = 12 𝜐t is it. In the absence of such knowledge, however, dimensional analysis cannot identify the correct relation. It can only identify which choices may be correct, since it does not account for numerical factors like 12 or for the manner in which an equation was derived from physics principles.
Check Your Understanding
(The answers are given at the end of the book.) 1. (a) Is it possible for two quantities to have the same dimensions but diff erent units? (b) Is it possible for two quantities to have the same units but diff erent dimensions? 2. You can always add two numbers that have the same units (such as 6 meters + 3 meters). Can you always add
two numbers that have the same dimensions, such as two numbers that have the dimensions of length [L]?
3. The following table lists four variables, along with their units:
Variable Units x Meters (m) υ Meters per second (m/s) t Seconds (s) a Meters per second squared (m/s2)
These variables appear in the following equations, along with a few numbers that have no units. In which of the equations are the units on the left side of the equals sign consistent with the units on the right side?
(a) x = 𝜐t (d) 𝜐 = at + 12 at 3
(b) x = 𝜐t + 12 at 2 (e) 𝜐 3 = 2ax 2
(c) 𝜐 = at (f) t = √2xa 4. In the equation y = cnat2 you wish to determine the integer value (1, 2, etc.) of the exponent n. The di-
mensions of y, a, and t are known. It is also known that c has no dimensions. Can dimensional analysis be used to determine n?
1.4 Trigonometry Scientists use mathematics to help them describe how the physical universe works, and tri- gonometry is an important branch of mathematics. Three trigonometric functions are utilized throughout this text. They are the sine, the cosine, and the tangent of the angle θ (Greek theta), abbreviated as sin θ, cos θ, and tan θ, respectively. These functions are defi ned below in terms of the symbols given along with the right triangle in Interactive Figure 1.5.
DEFINITION OF SIN θ, COS θ, AND TAN θ
sin θ = ho h
(1.1)
cos θ = ha h
(1.2)
tan θ = ho ha
(1.3)
h = length of the hypotenuse of a right triangle ho = length of the side opposite the angle θ ha = length of the side adjacent to the angle θ
INTERACTIVE FIGURE 1.5 A right triangle.
90°
h = hypotenuse
θ
ho = length of side opposite the angle
ha = length of side adjacent to the angle θ
θ
1.4 Trigonometry 7
The sine, cosine, and tangent of an angle are numbers without units, because each is the ratio of the lengths of two sides of a right triangle. Example 4 illustrates a typical application of Equation 1.3.
EXAMPLE 4 Using Trigonometric Functions
On a sunny day, a tall building casts a shadow that is 67.2 m long. The angle between the sun’s rays and the ground is θ = 50.0°, as Figure 1.6 shows. Determine the height of the building.
Reasoning We want to fi nd the height of the building. Therefore, we begin with the colored right triangle in Figure 1.6 and identify the height as the length ho of the side opposite the angle θ. The length of the shadow is the length ha of the side that is adjacent to the angle θ. The ratio of the length of the opposite side to the length of the adjacent side is the tangent of the angle θ, which can be used to fi nd the height of the building.
Solution We use the tangent function in the following way, with θ = 50.0° and ha = 67.2 m:
tan θ = ho ha
(1.3)
ho = ha tan θ = (67.2 m)(tan 50.0°) = (67.2 m)(1.19) = 80.0 m
The value of tan 50.0° is found by using a calculator. FIGURE 1.6 From a value for the angle θ and the length ha of the
shadow, the height ho of the building can be found using trigonometry.
= 50.0°θ
= 67.2 mha
ho
The sine, cosine, or tangent may be used in calculations such as that in Example 4, depend- ing on which side of the triangle has a known value and which side is asked for.
Problem-Solving Insight However, the choice of which side of the triangle to label ho (opposite) and which to label ha (adjacent) can be made only after the angle θ is identifi ed.
Often the values for two sides of the right triangle in Interactive Figure 1.5 are available, and the value of the angle θ is unknown. The concept of inverse trigonometric functions plays an important role in such situations. Equations 1.4–1.6 give the inverse sine, inverse cosine, and inverse tangent in terms of the symbols used in the drawing. For instance, Equation 1.4 is read as “θ equals the angle whose sine is ho/h.”
θ = sin−1 ( ho h ) (1.4)
θ = cos−1 ( ha h ) (1.5)
θ = tan−1 ( ho ha) (1.6)
The use of −1 as an exponent in Equations 1.4–1.6 does not mean “take the reciprocal.” For instance, tan−1 (ho/ha) does not equal 1/tan (ho/ha). Another way to express the inverse trigono- metric functions is to use arc sin, arc cos, and arc tan instead of sin−1, cos−1, and tan−1. Example 5 illustrates the use of an inverse trigonometric function.
EXAMPLE 5 Using Inverse Trigonometric Functions
A lakefront drops off gradually at an angle θ, as Figure 1.7 indicates. For safety reasons, it is necessary to know how deep the lake is at vari- ous distances from the shore. To provide some information about the depth, a lifeguard rows straight out from the shore a distance of 14.0 m
and drops a weighted fi shing line. By measuring the length of the line, the lifeguard determines the depth to be 2.25 m. (a) What is the value of θ? (b) What would be the depth d of the lake at a distance of 22.0 m from the shore?
8 CHAPTER 1 Introduction and Mathematical Concepts
The right triangle in Interactive Figure 1.5 provides the basis for defi ning the various tri- gonometric functions according to Equations 1.1–1.3. These functions always involve an angle and two sides of the triangle. There is also a relationship among the lengths of the three sides of a right triangle. This relationship is known as the Pythagorean theorem and is used often in this text.
PYTHAGOREAN THEOREM The square of the length of the hypotenuse of a right triangle is equal to the sum of the squares of the lengths of the other two sides:
h2 = ho2 + ha2 (1.7)
1.5 Scalars and Vectors The volume of water in a swimming pool might be 50 cubic meters, or the winning time of a race could be 11.3 seconds. In cases like these, only the size of the numbers matters. In other words, how much volume or time is there? The 50 specifi es the amount of water in units of cubic meters, while the 11.3 specifi es the amount of time in seconds. Volume and time are examples of scalar quantities. A scalar quantity is one that can be described with a single number (including any units) giving its size or magnitude. Some other common scalars are temperature (e.g., 20 °C) and mass (e.g., 85 kg).
While many quantities in physics are scalars, there are also many that are not, and for these quantities the magnitude tells only part of the story. Consider Figure 1.8, which depicts a car that has moved 2 km along a straight line from start to fi nish. When describing the motion, it is incomplete to say that “the car moved a distance of 2 km.” This statement would indicate only that the car ends up somewhere on a circle whose center is at the starting point and whose radius
Reasoning Near the shore, the lengths of the opposite and adjacent sides of the right triangle in Figure 1.7 are ho = 2.25 m and ha = 14.0 m, relative to the angle θ. Having made this identifi cation, we can use the inverse tangent to fi nd the angle in part (a). For part (b) the opposite and adjacent sides farther from the shore become ho = d and ha = 22.0 m. With the value for θ obtained in part (a), the tangent function can be used to fi nd the unknown depth. Considering the way in which the lake bottom drops off in Figure 1.7, we expect the unknown depth to be greater than 2.25 m.
Solution (a) Using the inverse tangent given in Equation 1.6, we fi nd that
θ = tan−1 ( ho ha) = tan
−1 (2.25 m14.0 m) = 9.13° (b) With θ = 9.13°, the tangent function given in Equation 1.3 can be used to fi nd the unknown depth farther from the shore, where ho = d and ha = 22.0 m. Since tan θ = ho /ha, it follows that
ho = ha tan θ d = (22.0 m)(tan 9.13°) = 3.54 m
which is greater than 2.25 m, as expected.
FIGURE 1.7 If the distance from the shore and the depth of the water at any one point are known, the angle θ can be found with the aid of trigonometry. Knowing the value of θ is useful, because then the depth d at another point can be determined.
14.0 m
2.25 m d
22.0 m
θ
1.5 Scalars and Vectors 9
is 2 km. A complete description must include the direction along with the distance, as in the state- ment “the car moved a distance of 2 km in a direction 30° north of east.” A quantity that deals inherently with both magnitude and direction is called a vector quantity. Because direction is an important characteristic of vectors, arrows are used to represent them; the direction of the arrow gives the direction of the vector. The colored arrow in Figure 1.8, for example, is called the displacement vector, because it shows how the car is displaced from its starting point. Chapter 2 discusses this particular vector.
The length of the arrow in Figure 1.8 represents the magnitude of the displacement vector. If the car had moved 4 km instead of 2 km from the starting point, the arrow would have been drawn twice as long. By convention, the length of a vector arrow is proportional to the magnitude of the vector.
In physics there are many important kinds of vectors, and the practice of using the length of an arrow to represent the magnitude of a vector applies to each of them. All forces, for instance, are vectors. In common usage a force is a push or a pull, and the direction in which a force acts is just as important as the strength or magnitude of the force. The magnitude of a force is measured in SI units called newtons (N). An arrow representing a force of 20 newtons is drawn twice as long as one representing a force of 10 newtons.
The fundamental distinction between scalars and vectors is the characteristic of direction. Vectors have it, and scalars do not. Conceptual Example 6 helps to clarify this distinction and explains what is meant by the “direction” of a vector.
FIGURE 1.8 A vector quantity has a magnitude and a direction. The colored arrow in this drawing represents a displacement vector.
N
S
W E
30.0°
Start
Finish2 km
CONCEPTUAL EXAMPLE 6 Vectors, Scalars, and the Role of Plus and Minus Signs
There are places where the temperature is +20 °C at one time of the year and −20 °C at another time. Do the plus and minus signs that signify positive and negative temperatures imply that temperature is a vector quantity? (a) Yes (b) No
Reasoning A hallmark of a vector is that there is both a magnitude and a physical direction associated with it, such as 20 meters due east or 20 meters due west.
Answer (a) is incorrect. The plus and minus signs associated with +20 °C and −20 °C do not convey a physical direction, such as due east or due west. Therefore, temperature cannot be a vector quantity.
Answer (b) is correct. On a thermometer, the algebraic signs simply mean that the temperature is a number less than or greater than zero on the temperature scale being used and have nothing to do with east, west, or any other physical direction. Temperature, then, is not a vector. It is a scalar, and scalars can sometimes be negative.
*Vectors are also sometimes written in other texts as boldface symbols without arrows above them.
Often, for the sake of convenience, quantities such as volume, time, displacement, velo- city, and force are represented in physics by symbols. In this text, we write vectors in boldface symbols (this is boldface) with arrows above them* and write scalars in italic symbols (this is italic). Thus, a displacement vector is written as “A→ = 750 m, due east,” where the A→ is a boldface symbol. By itself, however, separated from the direction, the magnitude of this vector is a scalar quantity. Therefore, the magnitude is written as “A = 750 m,” where the A is an italic symbol without an arrow.
Check Your Understanding
(The answer is given at the end of the book.) 5. Which of the following statements, if any, involves a vector? (a) I walked 2 miles along the beach. (b) I
walked 2 miles due north along the beach. (c) I jumped off a cliff and hit the water traveling at 17 miles per hour. (d) I jumped off a cliff and hit the water traveling straight down at a speed of 17 miles per hour. (e) My bank account shows a negative balance of −25 dollars.
10 CHAPTER 1 Introduction and Mathematical Concepts
1.6 Vector Addition and Subtraction Addition Often it is necessary to add one vector to another, and the process of addition must take into ac- count both the magnitude and the direction of the vectors. The simplest situation occurs when the vectors point along the same direction—that is, when they are colinear, as in Figure 1.9. Here, a car fi rst moves along a straight line, with a displacement vector A→ of 275 m, due east. Then the car moves again in the same direction, with a displacement vector B→ of 125 m, due east. These two vectors add to give the total displacement vector R→ , which would apply if the car had moved from start to fi nish in one step. The symbol R→ is used because the total vector is often called the resultant vector. With the tail of the second arrow located at the head of the fi rst arrow, the two lengths simply add to give the length of the total displacement. This kind of vector addition is identical to the familiar addition of two scalar numbers (2 + 3 = 5) and can be carried out here only because the vectors point along the same direction. In such cases we add the individual magnitudes to get the magnitude of the total, knowing in advance what the direction must be. Formally, the addition is written as follows:
R→ = A→ + B→
R→ = 275 m, due east + 125 m, due east = 400 m, due east Perpendicular vectors are frequently encountered, and Figure 1.10 indicates how they can
be added. This fi gure applies to a car that fi rst travels with a displacement vector A→ of 275 m, due east, and then with a displacement vector B→ of 125 m, due north. The two vectors add to give a resultant displacement vector R→ . Once again, the vectors to be added are arranged in a tail-to- head fashion, and the resultant vector points from the tail of the fi rst to the head of the last vector added. The resultant displacement is given by the vector equation
R→ = A→ + B→
The addition in this equation cannot be carried out by writing R = 275 m + 125 m, because the vectors have diff erent directions. Instead, we take advantage of the fact that the triangle in Figure 1.10 is a right triangle and use the Pythagorean theorem (Equation 1.7). According to this theorem, the magnitude of R→ is
R = √(275 m)2 + (125 m)2 = 302 m
The angle θ in Figure 1.10 gives the direction of the resultant vector. Since the lengths of all three sides of the right triangle are now known, sin θ, cos θ, or tan θ can be used to determine θ. Noting that tan θ = B/A and using the inverse trigonometric function, we fi nd that:
θ = tan−1 (BA) = tan−1 ( 125 m 275 m) = 24.4°
Thus, the resultant displacement of the car has a magnitude of 302 m and points north of east at an angle of 24.4°. This displacement would bring the car from the start to the fi nish in Figure 1.10 in a single straight-line step.
When two vectors to be added are not perpendicular, the tail-to-head arrangement does not lead to a right triangle, and the Pythagorean theorem cannot be used. Figure 1.11a illustrates such a case for a car that moves with a displacement A→ of 275 m, due east, and then with a dis- placement B→ of 125 m, in a direction 55.0° north of west. As usual, the resultant displacement vector R→ is directed from the tail of the fi rst to the head of the last vector added. The vector addition is still given according to
R→ = A→ + B→
However, the magnitude of R→ is not R = A + B, because the vectors A→ and B→ do not have the same direction, and neither is it R = √A2 + B2, because the vectors are not perpendicular, so the Pythagorean theorem does not apply. Some other means must be used to fi nd the magnitude and direction of the resultant vector.
N
S
W E
Tail-to-head
Start Finish A
R
B
FIGURE 1.9 Two colinear displacement
vectors A→ and B→ add to give the resultant displacement vector R→ .
FIGURE 1.10 The addition of two perpendicular displacement vectors A→ and B→ gives the resultant vector R→ .
N
S
W E
Tail-to-head
Start
R B
Finish
90°θ
A
FIGURE 1.11 (a) The two displacement vectors A→ and B→ are neither colinear nor perpendicular, but even so they add to give the resultant vector R→. (b) In one method for adding them together, a graphical technique is used.
Finish
Start
Tail-to-head
55.0°
55.0°
( )a
( )b
22. 8 c
m
4 8
12
20
0
24 cm
16
28
N
S
W E
θ
θ
A
R B
A
R B
1.6 Vector Addition and Subtraction 11
One approach uses a graphical technique. In this method, a diagram is constructed in which the arrows are drawn tail to head. The lengths of the vector arrows are drawn to scale, and the angles are drawn accurately (with a protractor, perhaps). Then the length of the arrow representing the resultant vector is measured with a ruler. This length is converted to the mag- nitude of the resultant vector by using the scale factor with which the drawing is constructed. In Figure 1.11b, for example, a scale of one centimeter of arrow length for each 10.0 m of displacement is used, and it can be seen that the length of the arrow representing R→ is 22.8 cm. Since each centimeter corresponds to 10.0 m of displacement, the magnitude of R→ is 228 m. The angle θ, which gives the direction of R→ , can be measured with a protractor to be θ = 26.7° north of east.
Subtraction The subtraction of one vector from another is carried out in a way that depends on the follow- ing fact. When a vector is multiplied by −1, the magnitude of the vector remains the same, but the direction of the vector is reversed. Conceptual Example 7 illustrates the meaning of this statement.
Reasoning A displacement vector of −D→ is (−1) D→ . The presence of the (−1) factor reverses the direction of the vector, but does not change its magnitude. Similarly, a force vector of −F→ has the same magnitude as the vector F→ but has the opposite direction.
Answer (a) and (b) are incorrect. While scalars can sometimes be negative, magnitudes of vectors are never negative.
Answer (c) is correct. The vectors −D→ and −F→ have the same mag- nitudes as D→ and F→, but point in the opposite direction, as indicated in Figures 1.12b and 1.13b.
Related Homework: Problems 67
CONCEPTUAL EXAMPLE 7 Multiplying a Vector by −1
Consider two vectors described as follows:
1. A woman climbs 1.2 m up a ladder, so that her displacement vec- tor D→ is 1.2 m, upward along the ladder, as in Figure 1.12a.
2. A man is pushing with 450 N of force on his stalled car, trying to move it eastward. The force vector F→ that he applies to the car is 450 N, due east, as in Figure 1.13a.
What are the physical meanings of the vectors −D→ and −F→? (a) −D→ points upward along the ladder and has a magnitude of −1.2 m; −F→ points due east and has a magnitude of −450 N. (b) −D→ points downward along the ladder and has a magnitude of −1.2 m; −F→ points due west and has a magnitude of −450 N. (c) −D→ points downward along the ladder and has a magnitude of 1.2 m; −F→ points due west and has a magnitude of 450 N.
FIGURE 1.12 (a) The displacement vector for a woman climbing 1.2 m up a ladder is D→ . (b) The displacement vector for a woman climbing 1.2 m down a ladder is −D→ .
(a) (b)
–DD
FIGURE 1.13 (a) The force vector for a man pushing on a car with 450 N of force in a direction due east is F→ . (b) The force vector for a man pushing on a car with 450 N of force in a direction due west is −F→ .
(a)
(b)
F
–F
12 CHAPTER 1 Introduction and Mathematical Concepts
In practice, vector subtraction is carried out exactly like vector addition, except that one of the vectors added is multiplied by a scalar factor of −1. To see why, look at the two vectors A→ and B→ in Figure 1.14a. These vectors add together to give a third vector C→, according to C→ = A→ + B→. Therefore, we can calculate vector A→ as A→ = C→ − B→, which is an example of vector subtraction. However, we can also write this result as A→ = C→ + (−B→) and treat it as vector addi- tion. Figure 1.14b shows how to calculate vector A→ by adding the vectors C→ and −B→. Notice that vectors C→ and −B→ are arranged tail to head and that any suitable method of vector addition can be employed to determine A→.
Check Your Understanding
(The answers are given at the end of the book.) 6. Two vectors A→ and B→ are added together to give a resultant vector R→: R→ = A→ + B→. The magnitudes
of A→ and B→ are 3 m and 8 m, respectively, but the vectors can have any orientation. What are (a) the maximum possible value and (b) the minimum possible value for the magnitude of R→?
7. Can two nonzero perpendicular vectors be added together so their sum is zero? 8. Can three or more vectors with unequal magnitudes be added together so their sum is zero? 9. In preparation for this question, review Conceptual Example 7. Vectors A→ and B→ satisfy the vector
equation A→ + B→ = 0. (a) How does the magnitude of B→ compare with the magnitude of A→? (b) How does the direction of B→ compare with the direction of A→?
10. Vectors A→, B→, and C→ satisfy the vector equation A→ + B→ = C→, and their magnitudes are related by the scalar equation A2 + B2 = C2. How is vector A→ oriented with respect to vector B→?
11. Vectors A→, B→, and C→ satisfy the vector equation A→ + B→ = C→, and their magnitudes are related by the scalar equation A + B = C. How is vector A→ oriented with respect to vector B→?
1.7 The Components of a Vector Vector Components Suppose a car moves along a straight line from start to fi nish, as in Figure 1.15, the corres- ponding displacement vector being r→. The magnitude and direction of the vector r→ give the distance and direction traveled along the straight line. However, the car could also arrive at the fi nish point by fi rst moving due east, turning through 90°, and then moving due north. This alternative path is shown in the drawing and is associated with the two displacement vectors x→ and y→. The vectors x→ and y→ are called the x vector component and the y vector component of r→.
Vector components are very important in physics and have two basic features that are appar- ent in Figure 1.15. One is that the components add together to equal the original vector:
r→ = x→ + y→
The components x→ and y→, when added vectorially, convey exactly the same meaning as does the original vector r→: they indicate how the fi nish point is displaced relative to the starting point. The other feature of vector components that is apparent in Figure 1.15 is that x→ and y→ are not just any two vectors that add together to give the original vector r→: they are perpendicular vectors. This perpendicularity is a valuable characteristic, as we will soon see.
Any type of vector may be expressed in terms of its components, in a way similar to that illustrated for the displacement vector in Figure 1.15. Interactive Figure 1.16 shows an arbitrary vector A→ and its vector components A→ x and A
→ y. The components are drawn parallel
to convenient x and y axes and are perpendicular. They add vectorially to equal the original vector A→ :
A→ = A→ x + A →
y
FIGURE 1.15 The displacement vector r→ and its vector components x→ and y→.
FIGURE 1.14 (a) Vector addition according to C→ = A→ + B→ . (b) Vector subtraction accord- ing to A→ = C→ − B→ = C→ + (−B→ ).
A
B
C = A + B
( )a
B–
C
Tail-to-head
( )b
A = C – B
Start
Finish
90°
N
S
W E
x
yr
INTERACTIVE FIGURE 1.16 An arbitrary
vector A→ and its vector components A→ x and A →
y.
A
y+
y
x+ Ax
A
θ
1.7 The Components of a Vector 13
There are times when a drawing such as Interactive Figure 1.16 is not the most convenient way to represent vector components, and Figure 1.17 presents an alternative method. The disadvant- age of this alternative is that the tail-to-head arrangement of A→ x and A
→ y is missing, an arrange-
ment that is a nice reminder that A→ x and A →
y add together to equal A →
. The defi nition that follows summarizes the meaning of vector components:
DEFINITION OF VECTOR COMPONENTS In two dimensions, the vector components of a vector A→ are two perpendicular vectors A→ x and A
→ y that are parallel to the x and y axes, respectively, and add together vectorially
according to A→ = A→ x + A →
y.
Problem-Solving Insight In general, the components of any vector can be used in place of the vector itself in any calculation where it is convenient to do so.
The values calculated for vector components depend on the orientation of the vector relative to the axes used as a reference. Figure 1.18 illustrates this fact for a vector A→ by showing two sets of axes, one set being rotated clockwise relative to the other. With respect to the black axes, vector A→ has perpendicular vector components A→ x and A
→ y; with respect to the colored rotated axes,
vector A→ has diff erent vector components A→ x′ and A →
y′. The choice of which set of components to use is purely a matter of convenience.
Scalar Components It is often easier to work with the scalar components, Ax and Ay (note the italic symbols), rather than the vector components A→ x and A
→ y. Scalar components are positive or negative numbers (with
units) that are defi ned as follows: The scalar component Ax has a magnitude equal to that of A →
x and is given a positive sign if A→ x points along the +x axis and a negative sign if A
→ x points along
the −x axis. The scalar component Ay is defi ned in a similar manner. The following table shows an example of vector and scalar components:
In this text, when we use the term “component,” we will be referring to a scalar component, unless otherwise indicated.
Another method of expressing vector components is to use unit vectors. A unit vector is a vector that has a magnitude of 1, but no dimensions. We will use a caret (^) to distinguish it from other vectors. Thus,
x̂ is a dimensionless unit vector of length l that points in the positive x direction, and ŷ is a dimensionless unit vector of length l that points in the positive y direction.
These unit vectors are illustrated in Figure 1.19. With the aid of unit vectors, the vector com- ponents of an arbitrary vector A→ can be written as A→ x = Ax x̂ and A
→ y = Ay ŷ, where Ax and Ay are
its scalar components (see the drawing and the third column of the table above). The vector A→ is then written as A→ = Ax x̂ + Ay ŷ.
Resolving a Vector into Its Components If the magnitude and direction of a vector are known, it is possible to fi nd the components of the vector. The process of fi nding the components is called “resolving the vector into its components.” As Example 8 illustrates, this process can be carried out with the aid of trigo- nometry, because the two perpendicular vector components and the original vector form a right triangle.
Ay
+y
+x Ax
A
θ
FIGURE 1.17 This alternative way of
drawing the vector A→ and its vector components is completely equivalent to that shown in Interactive Figure 1.16.
+y
+x
+y´
+x´
Ax
Áy
Á x
A
Ay
FIGURE 1.18 The vector components of the vector depend on the orientation of the axes used as a reference.
x
y Axx
Ayy
+x
+y
FIGURE 1.19 The dimensionless unit vectors x̂ and ŷ have magnitudes equal to 1, and they point in the +x and +y directions, respectively. Expressed in terms of unit vectors, the vector components of the vector A→ are Ax x̂ and Ay ŷ.
Vector Components Scalar Components Unit Vectors
A→ x = 8 meters, directed along the +x axis Ax = +8 meters A →
x = (+8 meters) x̂
A→ y = 10 meters, directed along the –y axis Ay = −10 meters A →
y = (–10 meters) ŷ
14 CHAPTER 1 Introduction and Mathematical Concepts
EXAMPLE 8 Finding the Components of a Vector
A displacement vector r→ has a magnitude of r = 175 m and points at an angle of 50.0° relative to the x axis in Figure 1.20. Find the x and y com- ponents of this vector.
Reasoning We will base our solution on the fact that the triangle formed in Figure 1.20 by the vector r→ and its components x→ and y→ is a right triangle. This fact enables us to use the trigonometric sine and cosine functions, as defi ned in Equations 1.1 and 1.2.
Problem-Solving Insight You can check to see whether the components of a vector are correct by substituting them into the Pythagorean theorem in order to calculate the magnitude of the original vector.
Solution The y component can be obtained using the 50.0° angle and Equation 1.1, sin θ = y/r:
y = r sin θ = (175 m)(sin 50.0°) = 134 m
In a similar fashion, the x component can be obtained using the 50.0° angle and Equation 1.2, cos θ = x/r:
x = r cos θ = (175 m)(cos 50.0°) = 112 m
Math Skills Either acute angle of a right triangle can be used to determine the components of a vector. The choice of angle is a matter of convenience. For instance, instead of the 50.0° angle, it is also possible to use the angle α in Figure 1.20. Since α + 50.0° = 90.0°, it follows that α = 40.0°. The solution using α yields the same answers as the solution using the 50.0° angle:
cos α = y r
y = r cos α = (175 m)(cos 40.0°) = 134 m
sin α = x r
x = r sin α = (175 m)(sin 40.0°) = 112 m90.0°50.0°
x
yr
α
FIGURE 1.20 The x and y components of the displacement vector r→ can be found using trigonometry.
Since the vector components and the original vector form a right triangle, the Pythagorean theorem can be applied to check the validity of calculations such as those in Example 8. Thus, with the components obtained in Example 8, the theorem can be used to verify that the magnitude of the original vector is indeed 175 m, as given initially:
r = √(112 m) 2 + (134 m) 2 = 175 m
It is possible for one of the components of a vector to be zero. This does not mean that the vector itself is zero, however.
Problem-Solving Insight For a vector to be zero, every vector component must individually be zero.
Thus, in two dimensions, saying that A→ = 0 is equivalent to saying that A→ x = 0 and A →
y = 0. Or, stated in terms of scalar components, if A→ = 0, then Ax = 0 and Ay = 0.
Problem-Solving Insight Two vectors are equal if, and only if, they have the same magnitude and direction.
Thus, if one displacement vector points east and another points north, they are not equal, even if each has the same magnitude of 480 m. In terms of vector components, two vectors A→ and B →
are equal if, and only if, each vector component of one is equal to the corresponding vector component of the other. In two dimensions, if A→ = B
→ , then A→ x = B
→ x and A
→ y = A
→ y. Alternatively,
using scalar components, we write that Ax = Bx and Ay = By.
Check Your Understanding
(The answers are given at the end of the book.) 12. Which of the following displacement vectors
(if any) are equal?
Variable Magnitude Direction A→ 100 m 30° north of east
B→ 100 m 30° south of west
C→ 50 m 30° south of west
D→ 100 m 60° east of north
1.8 Addition of Vectors by Means of Components 15
13. Two vectors, A→ and B→, are shown in CYU Figure 1.1. (a) What are the signs (+ or −) of the scalar components, Ax and Ay, of the vector A→? (b) What are the signs of the scalar components, Bx and By, of the vector B
→ ? (c) What are the signs of the scalar
components, Rx and Ry, of the vector R →
, where R→ = A→ + B→? 14. Are two vectors with the same magnitude necessarily equal? 15. The magnitude of a vector has doubled, its direction remaining
the same. Can you conclude that the magnitude of each com- ponent of the vector has doubled?
16. The tail of a vector is fi xed to the origin of an x, y axis sys- tem. Originally the vector points along the +x axis and has a magnitude of 12 units. As time passes, the vector rotates coun- terclockwise. What are the sizes of the x and y components of the vector for the following rotational angles? (a) 90° (b) 180° (c) 270° (d) 360°
17. A vector has a component of zero along the x axis of a certain axis system. Does this vector necessarily have a component of zero along the x axis of another (rotated) axis system?
1.8 Addition of Vectors by Means of Components The components of a vector provide the most convenient and accurate way of adding (or sub- tracting) any number of vectors. For example, suppose that vector A→ is added to vector B→. The resultant vector is C→, where C→ = A→ + B→. Interactive Figure 1.21a illustrates this vector addition, along with the x and y vector components of A→ and B→. In part b of the drawing, the vectors A→ and B→ have been removed, because we can use the vector components of these vectors in place of them. The vector component B→x has been shifted downward and arranged tail to head with vector component A→ x. Similarly, the vector component A
→ y has been shifted to the right and arranged tail
to head with the vector component B→y. The x components are colinear and add together to give the x component of the resultant vector C→. In like fashion, the y components are colinear and add together to give the y component of C→. In terms of scalar components, we can write
Cx = Ax + Bx and Cy = Ay + By
The vector components C→x and C →
y of the resultant vector form the sides of the right triangle shown in Interactive Figure 1.21c. Thus, we can fi nd the magnitude of C→ by using the Pythagorean theorem:
C = √C 2x + C 2y The angle θ that C
→ makes with the x axis is given by θ = tan−1 (Cy/Cx). Example 9 illustrates how
to add several vectors using the component method.
C
A
B
Bx
By
Ax
Ay +x
+y
(a) (c)
Cy
Cx
C
C
Bx
By
Ax
Ay
(b)
A
θ
INTERACTIVE FIGURE 1.21 (a) The vectors A→ and B→ add together to give the resultant vector C→. The x and y components of A→ and B→ are also shown. (b) The drawing illustrates that C
→ x = A
→ x + B
→ x and C
→ y = A
→ y +
B→ y. (c) Vector C →
and its components form a right triangle.
+x
+y
A B
CYU FIGURE 1.1
16 CHAPTER 1 Introduction and Mathematical Concepts
Analyzing Multiple -Concept Problems
EXAMPLE 9 The Component Method of Vector Addition
A jogger runs 145 m in a direction 20.0° east of north (displacement vector A→) and then 105 m in a direction 35.0° south of east (displacement vector B→). Using components, determine the magnitude and direction of the resultant vector C→ for these two displacements.
Reasoning Figure 1.22 shows the vectors A→ and B→, assuming that the y axis corresponds to the dir- ection due north. The vectors are arranged in a tail-to-head fashion, with the resultant vector C→ drawn from the tail of A→ to the head of B→. The components of the vectors are also shown in the fi gure. Since C→ and its components form a right triangle (red in the drawing), we will use the Pythagorean theorem and trigonometry to express the magnitude and directional angle θ for C→ in terms of its components. The components of C→ will then be obtained from the components of A→ and B→ and the data given for these two vectors.
Knowns and Unknowns The data for this problem are listed in the table that follows:
Description Symbol Value Comment
Magnitude of vector A→ 145 m
Direction of vector A→ 20.0° east of north See Figure 1.22.
Magnitude of vector B→ 105 m
Direction of vector B→ 35.0° south of east See Figure 1.22.
Unknown Variable Magnitude of resultant vector C ?
Direction of resultant vector θ ?
FIGURE 1.22 The vectors A→ and B→ add together to give the resultant vector C→. The vector components of A→ and B→ are also shown. The resultant vector C→ can be obtained once its components have been found.
N
S
W E
20.0°
+x
35.0°
+y Bx
By
Ax
Ay
CyC
Cx
B A
θ
Modeling the Problem
STEP 1 Magnitude and Direction of C→ In Figure 1.22 the vector C→ and its components C→x and C→y form a right triangle, as the red arrows show. Applying the Pythagorean theorem to this right triangle shows that the magnitude of C→ is given by Equation 1a at the right. From the red triangle it also follows that the directional angle θ for the vector C→ is given by Equation 1b at the right.
STEP 2 Components of C→ Since vector C→ is the resultant of vectors A→ and B→, we have C→ = A→ + B→ and can write the scalar components of C→ as the sum of the scalar components of A→ and B→:
Cx = Ax + Bx and Cy = Ay + By
These expressions can be substituted into Equations 1a and 1b for the magnitude and direction of C→, as shown at the right.
Solution Algebraically combining the results of each step, we fi nd that
C = √C 2x + C 2y = √(Ax + Bx)2 + (Ay + By )2
θ = tan−1 ( Cy Cx) = tan−1(
Ay + By Ax + Bx)
To use these results we need values for the individual components of A→ and B→.
C = √Cx 2 + Cy 2 (1a)
θ = tan−1 ( Cy Cx) (1b)
C = √Cx 2 + Cy 2 (1a)
Cx = Ax + Bx Cy = Ay + By (2)
θ = tan−1 ( Cy Cx) (1b)
Cx = Ax + Bx Cy = Ay + By (2)
STEP 1 STEP 2
STEP 1 STEP 2
1.8 Addition of Vectors by Means of Components 17
Referring to Figure 1.22, we fi nd these values to be
Ax = (145 m) sin 20.0° = 49.6 m and Ay = (145 m) cos 20.0° = 136 m
Bx = (105 m) cos 35.0° = 86.0 m and By = −(105 m) sin 35.0° = −60.2 m
Note that the component By is negative, because B →
y points downward, in the negative y direction in the drawing. Substituting these values into the results for C and θ gives
C = √(Ax + Bx)2 + (Ay + By)2
= √(49.6 m + 86.0 m)2 + (136 m − 60.2 m)2 = 155 m
θ = tan−1( Ay + By Ax + Bx)
= tan−1( 136 m − 60.2 m49.6 m + 86.0 m) = 29°
Math Skills According to the defi nitions given in Equations 1.1 and 1.2, the sine and
cosine functions are sin ϕ = ho h
and cos ϕ = ha h
, where ho is the length of the side of a
right triangle that is opposite the angle ϕ, ha is the length of the side adjacent to the angle ϕ, and h is the length of the hypotenuse (see Figure 1.23a). Applications of the sine and cosine functions to determine the scalar components of a vector occur frequently. In such applications we begin by identifying the angle ϕ. Figure 1.23b shows the relevant portion of Figure 1.22 and indicates that ϕ = 20.0° for the vector A→. In this case we have ho = Ax, ha = Ay, and h = A = 145 m; it follows that
sin 20.0° = ho h
= Ax A
or Ax = A sin 20.0° = (145 m) sin 20.0° = 49.6 m
cos 20.0° = ha h
= Ay A
or Ay = A cos 20.0° = (145 m) cos 20.0° = 136 m
(a) (b)
Ax
+y
+x
Ay ha
ho
h
ha
ho
h A
ϕ
20.0°
90°
FIGURE 1.23 Math Skills drawing.
Related Homework: Problems 45, 47, 50, 54
18 CHAPTER 1 Introduction and Mathematical Concepts
In later chapters we will often use the component method for vector addition. For future reference, the main features of the reasoning strategy used in this technique are summarized below.
REASONING STRATEGY The Component Method of Vector Addition 1. For each vector to be added, determine the x and y components relative to a conveniently
chosen x, y coordinate system. Be sure to take into account the directions of the compon- ents by using plus and minus signs to denote whether the components point along the positive or negative axes.
2. Find the algebraic sum of the x components, which is the x component of the resultant vector. Similarly, fi nd the algebraic sum of the y components, which is the y component of the resultant vector.
3. Use the x and y components of the resultant vector and the Pythagorean theorem to de- termine the magnitude of the resultant vector.
4. Use the inverse sine, inverse cosine, or inverse tangent function to fi nd the angle that specifi es the direction of the resultant vector.
Check Your Understanding
(1) (2) (3) (4)
Ax
Ay
R
R
R
RBy Bx
(The answer is given at the end of the book.) 18. Two vectors, A→ and B→, have vector components that are shown (to the same scale) in CYU Figure 1.2.
The resultant vector is labeled R→. Which drawing shows the correct vector sum of A→ + B→? (a) 1, (b) 2, (c) 3, (d) 4
joint, and vector B→ represents the position of the ball relative to the elbow joint. Use the component method of vector addition and the angles given in the fi gure to fi nd the magnitude and direction (θ) of vector C→, which represents the position of the ball relative to the shoulder joint. The mag- nitude of vector A→ is 35.6 cm, and the magnitude of vector B→ is 31.2 cm. The angle θ is measured relative to a vertical anatomical plane known as the frontal or coronal plane.
Reasoning Similar to Example 9, the vectors A→ and B→ in Figure 1.24 are drawn tail-to-head. Thus, the resultant vector C→ = A→ + B→. The com- ponents of vector C→ will be obtained from the components of vectors A→ and B→. Once Cx and Cy are known, we can calculate the magnitude of vector C→ using the Pythagorean theorem. The directional angle θ will be determined from the components of vector C→.
Solution Applying the component method of vector addition, we know that Cx = Ax + Bx, and Cy = Ay + By. From Figure 1.24, we see that Ax = (35.6 cm) cos 45° = 25.2 cm, Bx = – (31.2) cos 80° = – 5.42 cm, Ay = (35.6 cm) sin 45° = 25.2 cm, and By = (31.2 cm) sin 80° = 30.7 cm. Therefore, Cx = 25.2 cm + (– 5.42 cm) = 19.8 cm, and Cy = 25.2 cm + 30.7 cm = 55.9 cm. The magnitude of vector C→ is now found by the Pythagorean theorem: C = √C2x + C2y = √(19.8 cm)2 + (55.9 cm)2 = 59.3 cm The directional angle θ is found by using the tangent function:
θ = tan−1( Cy Cx) = tan−1(
55.9 cm 19.8 cm) = 70.5° .
EXAMPLE 10 BIO Multi-joint Movements
Figure 1.24 shows an example of a multi-joint movement involving the shoulder and elbow joints. The view from above shows a person holding a ball in a position that involves both shoulder fl exion and elbow extension. Vector A→ represents the position of the elbow joint relative to the shoulder
FIGURE 1.24 Top view of a multi-joint movement involving the shoulder and elbow joints. The vectors A→ and B→ add together to give the resultant vector C→, which represents the position vector of the ball with respect to the shoulder joint. The resultant vector C→ can be obtained, once its components are determined.
Shoulder joint
Elbow joint
Ball
Frontal plane
45.0°
80.0°
+y
B
A
C
+x θ
CYU FIGURE 1.2
Focus on Concepts 19
Concept Summary 1.2 Units The SI system of units includes the meter (m), the kilogram (kg), and the second (s) as the base units for length, mass, and time, respectively. One meter is the distance that light travels in a vacuum in a time of 1/299 792 458 second. One kilogram is the mass of a standard cylinder of platinum–iridium alloy kept at the International Bureau of Weights and Measures. One second is the time for a certain type of electromagnetic wave emitted by cesium-133 atoms to undergo 9 192 631 770 wave cycles.
1.3 The Role of Units in Problem Solving To convert a number from one unit to another, multiply the number by the ratio of the two units. For instance, to convert 979 meters to feet, multiply 979 meters by the factor (3.281 foot/1 meter).
The dimension of a quantity represents its physical nature and the type of unit used to specify it. Three such dimensions are length [L], mass [M], time [T]. Dimensional analysis is a method for checking mathematical rela- tions for the consistency of their dimensions.
1.4 Trigonometry The sine, cosine, and tangent functions of an angle θ are defi ned in terms of a right triangle that contains θ, as in Equations 1.1–1.3, where ho and ha are, respectively, the lengths of the sides opposite and adja- cent to the angle θ, and h is the length of the hypotenuse.
sin θ = ho h
(1.1)
cos θ = ha h
(1.2)
tan θ = ho ha
(1.3)
The inverse sine, inverse cosine, and inverse tangent functions are given in Equations 1.4–1.6.
θ = sin−1 ( ho h ) (1.4)
θ = cos−1 ( ha h ) (1.5)
θ = tan−1 ( ho ha) (1.6)
The Pythagorean theorem states that the square of the length of the hypot- enuse of a right triangle is equal to the sum of the squares of the lengths of the other two sides, according to Equation 1.7.
h2 = ho2 + ha2 (1.7)
1.5 Scalars and Vectors A scalar quantity is described by its size, which is also called its magnitude. A vector quantity has both a magnitude and a direction. Vectors are often represented by arrows, the length of the arrow being proportional to the magnitude of the vector and the direction of the arrow indicating the direction of the vector.
1.6 Vector Addition and Subtraction One procedure for adding vectors utilizes a graphical technique, in which the vectors to be added are ar- ranged in a tail-to-head fashion. The resultant vector is drawn from the tail of the fi rst vector to the head of the last vector. The subtraction of a vector is treated as the addition of a vector that has been multiplied by a scalar factor of −1. Multiplying a vector by −1 reverses the direction of the vector.
1.7 The Components of a Vector In two dimensions, the vector compon- ents of a vector A→ are two perpendicular vectors A→ x and A
→ y that are parallel
to the x and y axes, respectively, and that add together vectorially so that A→ = A→ x + A
→ y. The scalar component Ax has a magnitude that is equal to that
of A→ x and is given a positive sign if A →
x points along the +x axis and a negative sign if A→ x points along the −x axis. The scalar component Ay is defi ned in a similar manner.
Two vectors are equal if, and only if, they have the same magnitude and direction. Alternatively, two vectors are equal in two dimensions if the x vector components of each are equal and the y vector components of each are equal. A vector is zero if, and only if, each of its vector components is zero.
1.8 Addition of Vectors by Means of Components If two vec- tors A→ and B→ are added to give a resultant C→ such that C→ = A→ + B→, then Cx = Ax + Bx and Cy = Ay + By, where Cx, Ax, and Bx are the scalar compon- ents of the vectors along the x direction, and Cy, Ay, and By are the scalar components of the vectors along the y direction.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 1.6 Vector Addition and Subtraction 1. During a relay race, runner A runs a certain distance due north and then hands off the baton to runner B, who runs for the same distance in a direction south of east. The two displacement vectors A→ and B→ can be added together to give a resultant vector R→. Which drawing correctly shows the resultant vector? (a) 1 (b) 2 (c) 3 (d) 4
North
East (1)
North
East (2)
North
East (3)
North
East (4)
A A A
A
BBBB
RRRR
QUESTION 1
2. How is the magnitude R of the resultant vector R→ in the drawing related to the magnitudes A and B of the vectors A→ and B→? (a) The magnitude of the resultant vector R→ is equal to the sum of the magnitudes of A→ and B→, or R = A + B. (b) The magnitude of the resultant vector R→ is greater than the
Focus on Concepts
20 CHAPTER 1 Introduction and Mathematical Concepts
sum of the magnitudes of A→ and B→, or R > A + B. (c) The magnitude of the resultant vector R→ is less than the sum of the magnitudes of A→ and B→, or R < A + B. 5. The fi rst drawing shows three displacement vectors, A→, B→, and C→, which are added in a tail-to-head fashion. The resultant vector is labeled R→. Which of the following drawings shows the correct resultant vector for A→ + B→ − C→? (a) 1 (b) 2 (c) 3
(1) (2) (3)
A
A A
A B
C
R R R
R
QUESTION 5
6. The fi rst drawing shows the sum of three displacement vectors, A→, B→, and C→. The resultant vector is labeled R→. Which of the following drawings shows the correct resultant vector for A→ − B→ − C→? (a) 1 (b) 2 (c) 3
(1) (2) (3)
A
A A
A B
C
R R R
R
QUESTION 6
Section 1.7 The Components of a Vector 8. A person is jogging along a straight line, and her displacement is denoted by the vector A→ in the drawings. Which drawing represents the correct vector components, A→ x and A
→ y, for the vector A
→ ? (a) 1 (b) 2 (c) 3 (d) 4
+y
+x
+x
+x
+x
+y
+y +y
(1)
Ax
Ay Ay
Ay Ay
Ax
Ax Ax
A
(2)
A
(3)
A
(4)
A
QUESTION 8
11. A person drives a car for a distance of 450.0 m. The displacement A→ of the car is illustrated in the drawing. What are the scalar components of this displacement vector?
(a) Ax = 0 m and Ay = +450.0 m (b) Ax = 0 m and Ay = −450.0 m (c) Ax = +450.0 m and Ay = +450.0 m (d) Ax = −450.0 m and Ay = 0 m (e) Ax = −450.0 m and Ay = +450.0 m
12. Drawing a shows a displacement vector A→ (450.0 m along the −y axis). In this x, y coordinate system the scalar components are Ax = 0 m and Ay = −450.0 m. Suppose that the coordinate system is rotated counterclockwise by 35.0°, but the magnitude (450.0 m) and direction of vector A→ remain unchanged, as in drawing b. What are the scalar components, Ax′ and Ay′, of the vector A
→ in the rotated x′, y′ coordinate system?
(a) Ax′ = −369 m and Ay′ = −258 m (b) Ax′ = +369 m and Ay′ = −258 m (c) Ax′ = +258 m and Ay′ = +369 m (d) Ax′ = +258 m and Ay′ = −369 m (e) Ax′ = −258 m and Ay′ = −369 m
QUESTION 12
+y
+x
A
(a)
A
+y´
+x´
35.0°
(b)
15. Suppose the vectors A→ and B→ in the drawing have magnitudes of 6.0 m and are directed as shown. What are Ax and Bx, the scalar components of A
→
and B→ along the x axis?
Ax Bx (a) +(6.0 m) cos 35° = +4.9 m −(6.0 m) cos 35° = −4.9 m
(b) +(6.0 m) sin 35° = +3.4 m −(6.0 m) cos 35° = −4.9 m
(c) −(6.0 m) cos 35° = −4.9 m +(6.0 m) sin 35° = +3.4 m
(d) −(6.0 m) cos 35° = −4.9 m +(6.0 m) cos 35° = +4.9 m
(e) −(6.0 m) sin 35° = −3.4 m +(6.0 m) sin 35° = +3.4 m
QUESTION 15
A B
35° 35°
6.0 m 6.0 m
+y
+x
Section 1.8 Addition of Vectors by Means of Components 17. Drawing a shows two vectors A→ and B→, and drawing b shows their com- ponents. The scalar components of these vectors are as follows:
Ax = −4.9 m Ay = +3.4 m Bx = +4.9 m By = +3.4 m
When the vectors A→ and B→ are added, the resultant vector is R→, so that R→ = A→ + B→. What are the values of Rx and Ry, the x and y components of R
→ ?
QUESTION 17
+y
+x
+x
+y
A B
35° 35°
6.0 m 6.0 m
A Ay By
BxAx
B
(a)
(b)
θ θ
A
B
R
QUESTION 2
QUESTION 11
+y
+x
A
Problems 21
18. The displacement vectors A→ and B→, when added together, give the res- ultant vector R→, so that R→ = A→ + B→. Use the data in the drawing to fi nd the magnitude R of the resultant vector and the angle θ that it makes with the +x axis.
QUESTION 18
A B
R
+y
6.0 m 8.0 m
23°
+xθ
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual MMH Problem-solving help GO Guided Online Tutorial V-HINT Video Hints CHALK Chalkboard Videos
BIO Biomedical application E Easy M Medium H Hard
Section 1.2 Units
Section 1.3 The Role of Units in Problem Solving 1. E GO A student sees a newspaper ad for an apartment that has 1330 square feet (ft2) of fl oor space. How many square meters of area are there?
2. E Bicyclists in the Tour de France reach speeds of 34.0 miles per hour (mi/h) on fl at sections of the road. What is this speed in (a) kilometers per hour (km/h) and (b) meters per second (m/s)? 3. E SSM Vesna Vulovic survived the longest fall on record without a para- chute when her plane exploded and she fell 6 miles, 551 yards. What is this distance in meters?
4. E Suppose a man’s scalp hair grows at a rate of 0.35 mm per day. What is this growth rate in feet per century?
5. E Given the quantities a = 9.7 m, b = 4.2 s, c = 69 m/s, what is the value of the quantity d = a3/(cb2)?
6. E Consider the equation 𝜐 = 13 zxt 2. The dimensions of the variables υ, x, and t are [L]/[T], [L], and [T], respectively. The numerical factor 3 is di- mensionless. What must be the dimensions of the variable z, such that both sides of the equation have the same dimensions? Show how you determined your answer.
7. E SSM A bottle of wine known as a magnum contains a volume of 1.5 liters. A bottle known as a jeroboam contains 0.792 U.S. gallons. How many magnums are there in one jeroboam?
8. E The CGS unit for measuring the viscosity of a liquid is the poise (P): 1 P = 1 g/(s · cm). The SI unit for viscosity is the kg/(s · m). The viscosity of water at 0 °C is 1.78 × 10−3 kg/(s · m). Express this viscosity in poise. 9. E BIO Azelastine hydrochloride is an antihistamine nasal spray. A standard size container holds one fl uid ounce (oz) of the liquid. You are searching for this medication in a European drugstore and are asked how many milliliters (mL) there are in one fl uid ounce. Using the following con- version factors, determine the number of milliliters in a volume of one fl uid ounce: 1 gallon (gal) = 128 oz, 3.785 × 10−3 cubic meters (m3) = 1 gal, and 1 mL = 10−6 m3.
10. M GO A partly full paint can has 0.67 U.S. gallons of paint left in it. (a) What is the volume of the paint in cubic meters? (b) If all the remaining paint is used to coat a wall evenly (wall area = 13 m2), how thick is the layer of wet paint? Give your answer in meters.
11. M SSM A spring is hanging down from the ceiling, and an object of mass m is attached to the free end. The object is pulled down, thereby stretch- ing the spring, and then released. The object oscillates up and down, and the time T required for one complete up-and-down oscillation is given by the equation T = 2π√m/k, where k is known as the spring constant. What must be the dimension of k for this equation to be dimensionally correct?
Section 1.4 Trigonometry 12. E You are driving into St. Louis, Missouri, and in the distance you see the famous Gateway to the West arch. This monument rises to a height of 192 m. You estimate your line of sight with the top of the arch to be 2.0° above the horizontal. Approximately how far (in kilometers) are you from the base of the arch?
13. E SSM A highway is to be built between two towns, one of which lies 35.0 km south and 72.0 km west of the other. What is the shortest length of highway that can be built between the two towns, and at what angle would this highway be directed with respect to due west?
14. E GO A hill that has a 12.0% grade is one that rises 12.0 m vertically for every 100.0 m of distance in the horizontal direction. At what angle is such a hill inclined above the horizontal?
15. E GO The corners of a square lie on a circle of diameter D = 0.35 m. Each side of the square has a length L. Find L.
16. E GO The drawing shows a person looking at a building on top of which an antenna is mounted. The horizontal distance between the per- son’s eyes and the building is 85.0 m. In part a the person is looking at the base of the antenna, and his line of sight makes an angle of 35.0° with the horizontal. In part b the person is looking at the top of the antenna, and his line of sight makes an angle of 38.0° with the horizontal. How tall is the antenna?
(a) (b)
35.0° 38.0°
85.0 m85.0 m
PROBLEM 16
Problems
22 CHAPTER 1 Introduction and Mathematical Concepts
Section 1.6 Vector Addition and Subtraction 23. E SSM (a) Two workers are trying to move a heavy crate. One pushes on the crate with a force A→, which has a magnitude of 445 newtons and is directed due west. The other pushes with a force B→, which has a magnitude of 325 newtons and is directed due north. What are the magnitude and direc- tion of the resultant force A→ + B→ applied to the crate? (b) Suppose that the second worker applies a force −B→ instead of B→. What then are the magnitude and direction of the resultant force A→ − B→ applied to the crate? In both cases express the direction relative to due west.
24. E A force vector F1 →
points due east and has a magnitude of 200 new- tons. A second force F2
→ is added to F1
→ . The resultant of the two vectors has
a magnitude of 400 newtons and points along the east/west line. Find the magnitude and direction of F2
→ . Note that there are two answers.
25. E SSM Consider the following four force vectors:
F1 →
= 50.0 newtons, due east
F2 →
= 10.0 newtons, due east
F3 →
= 40.0 newtons, due west
F4 →
= 30.0 newtons, due west
Which two vectors add together to give a resultant with the smallest mag- nitude, and which two vectors add to give a resultant with the largest mag- nitude? In each case specify the magnitude and direction of the resultant.
26. E GO Vector A→ has a magnitude of 63 units and points due west, while vector B→ has the same magnitude and points due south. Find the magnitude and direction of (a) A→ + B→ and (b) A→ − B→. Specify the directions relative to due west. 27. E Two bicyclists, starting at the same place, are riding toward the same campground by two diff erent routes. One cyclist rides 1080 m due east and then turns due north and travels another 1430 m before reaching the camp- ground. The second cyclist starts out by heading due north for 1950 m and then turns and heads directly toward the campground. (a) At the turning point, how far is the second cyclist from the campground? (b) In what direc- tion (measured relative to due east) must the second cyclist head during the last part of the trip?
28. E GO The drawing shows a triple jump on a checkerboard, starting at the center of square A and ending on the center of square B. Each side of a square measures 4.0 cm. What is the magnitude of the displacement of the colored checker during the triple jump?
B
A PROBLEM 28
29. E Given the vectors P→ and Q→ shown on the grid, sketch and calculate the magnitudes of the vectors (a) M
→ = P→ + Q→ and (b) K→ = 2P→ − Q→.
Use the tail-to-head method and express the mag- nitudes in centimeters with the aid of the grid scale shown in the drawing.
17. E CHALK The two hot-air balloons in the drawing are 48.2 and 61.0 m above the ground. A person in the left balloon observes that the right balloon is 13.3° above the horizontal. What is the horizontal distance x between the two balloons?
PROBLEM 17
48.2 m
13.3°
61.0 m
x
18. M Available on WileyPLUS. 19. M MMH The drawing shows sodium and chloride ions positioned at the corners of a cube that is part of the crystal structure of sodium chloride (common table salt). The edges of the cube are each 0.281 nm (1 nm = 1 nanometer = 10−9 m) in length. What is the value of the angle θ in the drawing? 20. M GO A person is standing at the edge of the water and looking out at the ocean (see the drawing). The height of the person’s eyes above the water is h = 1.6 m, and the radius of the earth is R = 6.38 × 106 m. (a) How far is it to the horizon? In other words, what is the distance d from the person’s eyes to the horizon? (Note: At the horizon the angle between the line of sight and the radius of the earth is 90°.) (b) Express this distance in miles.
PROBLEM 20
Horizon
h
R
d
R
90°
21. M SSM Three deer, A, B, and C, are grazing in a fi eld. Deer B is located 62 m from deer A at an angle of 51° north of west. Deer C is located 77° north of east relative to deer A. The distance between deer B and C is 95 m. What is the distance between deer A and C? (Hint: Consider the law of cosines given in Appendix E.) 22. H An aerialist on a high platform holds on to a trapeze attached to a support by an 8.0-m cord. (See the drawing.) Just before he jumps off the platform, the cord makes an angle of 41° with the vertical. He jumps, swings down, then back up, releasing the trapeze at the instant it is 0.75 m below its initial height. Calculate the angle θ that the trapeze cord makes with the vertical at this instant.
8.0 m
0.75 m
41°θ
PROBLEM 22
8.00 cm P
Q
PROBLEM 29
PROBLEM 19
Chloride ion Sodium ion
0.281 nanometers
θ
Problems 23
30. M MMH Vector A→ has a magnitude of 12.3 units and points due west. Vector B→ points due north. (a) What is the magnitude of B→ if A→ + B→ has a magnitude of 15.0 units? (b) What is the direction of A→ + B→ relative to due west? (c) What is the magnitude of B→ if A→ − B→ has a magnitude of 15.0 units? (d) What is the direction of A→ − B→ relative to due west? 31. M SSM A car is being pulled out of the mud by two forces that are ap- plied by the two ropes shown in the drawing. The dashed line in the drawing
bisects the 30.0° angle. The magnitude of the force applied by each rope is
2900 newtons. Arrange the force vectors tail to head and use the graphical
technique to answer the following questions. (a) How much force would a single rope need to apply to accomplish the same eff ect as the two forces
added together? (b) How would the single rope be directed relative to the dashed line?
30.0°
2900 newtons
2900 newtons
PROBLEM 31
32. M GO A jogger travels a route that has two parts. The fi rst is a displace- ment A→ of 2.50 km due south, and the second involves a displacement B→ that points due east. (a) The resultant displacement A→ + B→ has a magnitude of 3.75 km. What is the magnitude of B→, and what is the direction of A→ + B→ relative to due south? (b) Suppose that A→ − B→ had a magnitude of 3.75 km. What then would be the magnitude of B→, and what is the direction of A→ − B→ relative to due south?
33. M At a picnic, there is a contest in which hoses are used to shoot water at a beach ball from three directions. As a result, three forces act on
the ball, F1 →
, F2 →
, and F3 →
(see the drawing). The magnitudes of F1 →
and F2 → are
F1 = 50.0 newtons and F2 = 90.0 newtons. Using a scale drawing and the graphical technique, determine (a) the magnitude of F3
→ and (b) the angle θ
such that the resultant force acting on the ball is zero.
60.0°
F3
F1
F2
N
S
W E
θ
PROBLEM 33
Section 1.7 The Components of a Vector 34. E GO A force vector has a magnitude of 575 newtons and points at an angle of 36.0° below the positive x axis. What are (a) the x scalar component and (b) the y scalar component of the vector? 35. E SSM Vector A→ points along the +y axis and has a magnitude of 100.0 units. Vector B→ points at an angle of 60.0° above the +x axis and has a mag- nitude of 200.0 units. Vector C→ points along the +x axis and has a magnitude of 150.0 units. Which vector has (a) the largest x component and (b) the largest y component? 36. E Soccer player #1 is 8.6 m from the goal (see the drawing). If she kicks the ball directly into the net, the ball has a displacement labeled A→. If, on the other hand, she fi rst kicks it to player #2, who then kicks it into the net, the
ball undergoes two successive displacements, A→ y and A →
x. What are the mag-
nitudes and directions of A→ x and A →
y?
#1
Net
90°
30.0°
#2
N
S
W E
Ay A
Ax
PROBLEM 36
37. E GO The components of vector A→ are Ax and Ay (both positive), and the angle that it makes with respect to the positive x axis is θ. Find the angle θ if the components of the displacement vector A→ are (a) Ax = 12 m and Ay = 12 m, (b) Ax = 17 m and Ay = 12 m, and (c) Ax = 12 m and Ay = 17 m. 38. E During takeoff , an airplane climbs with a speed of 180 m/s at an angle of 34° above the horizontal. The speed and direction of the airplane constitute
a vector quantity known as the velocity. The sun is shining directly overhead.
How fast is the shadow of the plane moving along the ground? (That is, what
is the magnitude of the horizontal component of the plane’s velocity?)
39. E SSM The x vector component of a displacement vector r→ has a mag- nitude of 125 m and points along the negative x axis. The y vector component has a magnitude of 184 m and points along the negative y axis. Find the mag- nitude and direction of r→. Specify the direction with respect to the negative x axis. 40. E Your friend has slipped and fallen. To help her up, you pull with a force F→, as the drawing shows. The vertical component of this
force is 130 newtons, and the horizontal com-
ponent is 150 newtons. Find (a) the magnitude of F→ and (b) the angle θ. 41. E Available on WileyPLUS. 42. M GO Two racing boats set out from the same dock and speed away at the same con-
stant speed of 101 km/h for half an hour (0.500 h), the blue boat headed
25.0° south of west, and the green boat headed 37.0° south of west. During
this half hour (a) how much farther west does the blue boat travel, compared to the green boat, and (b) how much farther south does the green boat travel, compared to the blue boat? Express your answers in km.
43. M SSM MMH The magnitude of the force vector F→ is 82.3 newtons. The x component of this vector is directed along the +x axis and has a magnitude of 74.6 newtons. The y component points along the +y axis. (a) Find the direction of F→ relative to the +x axis. (b) Find the component of F→ along the +y axis. 44. H Available on WileyPLUS.
Section 1.8 Addition of Vectors by Means of Components 45. E SSM Consult Multiple-Concept Example 9 in preparation for this problem. A golfer, putting on a green, requires three strokes to “hole the ball.”
During the fi rst putt, the ball rolls 5.0 m due east. For the second putt, the
ball travels 2.1 m at an angle of 20.0° north of east. The third putt is 0.50 m
due north. What displacement (magnitude and direction relative to due east)
would have been needed to “hole the ball” on the very fi rst putt?
F
θ
PROBLEM 40
24 CHAPTER 1 Introduction and Mathematical Concepts
46. E CHALK The three displacement vectors in the drawing have mag- nitudes of A = 5.00 m, B = 5.00 m, and C = 4.00 m. Find the resultant (magnitude and directional angle) of the three vectors by means of the com- ponent method. Express the directional angle as an angle above the positive or negative x axis.
PROBLEM 46
+y
+x
A
B
60.0°20.0°
C
47. E MMH Multiple-Concept Example 9 reviews the concepts that play a role in this problem. Two forces are applied to a tree stump to pull it out of the ground. Force FA
→ has a magnitude of 2240 newtons and points 34.0°
south of east, while force FB →
has a magnitude of 3160 newtons and points due south. Using the component method, fi nd the magnitude and direction of the resultant force FA
→ + FB
→ that is applied to the stump. Specify the direction
with respect to due east.
48. E GO A baby elephant is stuck in a mud hole. To help pull it out, game keepers use a rope to apply a force FA
→ , as part a of the drawing shows. By
itself, however, force FA →
is insuffi cient. Therefore, two additional forces FB →
and FC
→ are applied, as in part b of the drawing. Each of these additional
forces has the same magnitude F. The magnitude of the resultant force acting on the elephant in part b of the drawing is k times larger than that in part a. Find the ratio F/FA when k = 2.00.
20.0° 20.0°
FB
FA FA
FC
(a) (b)
PROBLEM 48
49. E Displacement vector A→ points due east and has a magnitude of 2.00 km. Displacement vector B→ points due north and has a magnitude of 3.75 km. Displacement vector C→ points due west and has a magnitude of 2.50 km. Displacement vector D→ points due south and has a magnitude of 3.00 km. Find the magnitude and direction (relative to due west) of the resultant vector A→ + B→ + C→ + D→. 50. E Multiple-Concept Example 9 provides background pertinent to this problem. The magnitudes of the four displacement vectors shown in the drawing are A = 16.0 m, B = 11.0 m, C = 12.0 m, and D = 26.0 m. Determine the magnitude and directional angle for the resultant that occurs when these vectors are added together.
B
A
D
50.0° +x
+y
35.0° 20.0°
C
PROBLEM 50
51. E MMH Available on WileyPLUS. 52. M GO Two geological fi eld teams are working in a remote area. A global positioning system (GPS) tracker at their base camp shows the location of the fi rst team as 38 km away, 19° north of west, and the second team as 29 km away, 35° east of north. When the fi rst team uses its GPS to check the position of the second team, what does the GPS give for the second team’s (a) distance from them and (b) direction, measured from due east? 53. M SSM A sailboat race course con- sists of four legs, defi ned by the dis- placement vectors A→, B→, C→, and D→, as the drawing indicates. The mag- nitudes of the fi rst three vectors are A = 3.20 km, B = 5.10 km, and C = 4.80 km. The fi nish line of the course coincides with the starting line. Using the data in the drawing, fi nd the distance of the fourth leg and the angle θ. 54. M Multiple-Concept Example 9 deals with the concepts that are import- ant in this problem. A grasshopper makes four jumps. The displacement vec- tors are (1) 27.0 cm, due west; (2) 23.0 cm, 35.0° south of west; (3) 28.0 cm, 55.0° south of east; and (4) 35.0 cm, 63.0° north of east. Find the magnitude and direction of the resultant displacement. Express the direction with respect to due west.
55. M MMH Available on WileyPLUS. 56. M The route followed by a hiker consists of three displacement vec- tors A→, B→, and C→. Vector A→ is along a measured trail and is 1550 m in a direction 25.0° north of east. Vector B→ is not along a measured trail, but the hiker uses a compass and knows that the direction is 41.0° east of south. Similarly, the direction of vector C→ is 35.0° north of west. The hiker ends up back where she started. Therefore, it follows that the res- ultant displacement is zero, or A→ + B→ + C→ = 0. Find the magnitudes of (a) vector B→ and (b) vector C→.
57. E Available on WileyPLUS. 58. E A monkey is chained to a stake in the ground. The stake is 3.00 m from a vertical pole, and the chain is 3.40 m long. How high can the monkey climb up the pole?
59. E SSM Available on WileyPLUS. 60. E BIO The volume of liquid fl owing per second is called the volume fl ow rate Q and has the dimensions of [L]3/[T]. The fl ow rate of a liquid
through a hypodermic needle during an injection can be estimated with the following equation:
Q = πRn (P2 − P1)
8ηL
The length and radius of the needle are L and R, respectively, both of which have the dimension [L]. The pressures at opposite ends of the needle are P2
Additional Problems
23.0°
35.0°
40.0°
Finish Start
B
AD
C
θ
PROBLEM 53
Concepts and Calculations Problems 25
and P1, both of which have the dimensions of [M]/{[L][T]2}. The symbol 𝜂 represents the viscosity of the liquid and has the dimensions of [M]/{[L][T]}. The symbol 𝜋 stands for pi and, like the number 8 and the exponent n, has no dimensions. Using dimensional analysis, determine the value of n in the expression for Q. 61. E An ocean liner leaves New York City and travels 18.0° north of east for 155 km. How far east and how far north has it gone? In other words, what are the magnitudes of the components of the ship’s displacement vector in the directions (a) due east and (b) due north? 62. E GO A pilot fl ies her route in two straight-line segments. The dis- placement vector A→ for the fi rst segment has a magnitude of 244 km and a direction 30.0° north of east. The displacement vector B→ for the second segment has a magnitude of 175 km and a direction due west. The resultant displacement vector is R→ = A→ + B→ and makes an angle θ with the direction due east. Using the component method, fi nd the magnitude of R→ and the directional angle θ. 63. E SSM Available on WileyPLUS. 64. M Available on WileyPLUS. 65. M SSM Vector A→ has a magnitude of 6.00 units and points due east. Vector B→ points due north. (a) What is the magnitude of B→, if the vector A→ + B→ points 60.0° north of east? (b) Find the magnitude of A→ + B→. 66. M GO Three forces act on an object, as indicated in the drawing. Force F1
→ has a mag-
nitude of 21.0 newtons (21.0 N) and is direc- ted 30.0° to the left of the +y axis. Force F2
→
has a magnitude of 15.0 N and points along the +x axis. What must be the magnitude and direction (specifi ed by the angle θ in the drawing) of the third force F3
→ such that the
vector sum of the three forces is 0 N?
67. M Available on WileyPLUS. 68. M CHALK You live in the building on the left in the drawing, and a friend lives in the other building. The two of you are having a discussion about the heights of the buildings, and your friend claims that the height of his building is more than 1.50 times the height of yours. To resolve the issue you climb to the roof of your building and estimate that your line of sight to the top edge of the other building makes an angle of 21° above the horizontal, whereas your line of sight to the base of the other building makes an angle of 52° below the horizontal. Determine the ratio of the height of the taller building to the height of the shorter building. State whether your friend is right or wrong.
21° 52°
PROBLEM 68
69. H Available on WileyPLUS.
+x
+y
30.0°
F1
F2
F3
θ
PROBLEM 66
This chapter has presented an introduction to the mathematics of trigono- metry and vectors, which will be used throughout the text. In this section we apply some of the important features of this mathematics, and review some concepts that can help in anticipating some of the characteristics of the numerical answers.
70. M CHALK The fi gure shows two dis- placement vectors A→ and B→. Vector A→ points at an angle of 22° above the x axis and has an unknown magnitude. Vector B→ has an x component Bx = 35.0 m and has an unknown y component By. These two vectors are equal. Concepts: (i) What does the condition that vector A→ equals B→ imply about the magnitudes and dir- ections of the vectors? (ii) What does the condition that vector A→ equals B→ imply about the x and y components of the vec- tors? Calculations: Find the magnitude of A→ and the value of By.
71. M CHALK SSM The fi gure shows three displacement vectors A→, B→, and C→. These vectors are arranged in tail-to-head fashion, and they add together to give a resultant displacement R→ , which lies along the x axis. Note that the vector B→ is parallel to the x axis. Concepts: (i) How is the magnitude of A→ related to its scalar components Ax and Ay? (ii) Do any of the vectors in the fi gure have a zero value for either their x or y components? (If so, which ones?) (iii) What does the fact that A→, B→, and C→ add together to give R→ tell you about the components of these vectors? Calculations: What is the mag- nitude of the vector A→ and its directional angle θ?
+y
B
A C
R +x
10.0 m
35.0 m
50.0°
23.0 m
θ
PROBLEM 71
+y
35.0 m
Bx
22.0°
By
B
+x
+y
A
+x
(b)
(a)
θ
PROBLEM 70
Concepts and Calculations Problems
26 CHAPTER 1 Introduction and Mathematical Concepts
72. M The Waterfall. You and your team are exploring a river in South America when you come to the bottom of a tall waterfall. You estimate the
cliff over which the water fl ows to be about 100 feet tall. You have to choose
between climbing the cliff or backtracking and taking another route, but
climbing the cliff would cut two hours off of your trip. There is only one
experienced climber in the group: she would climb the cliff alone and drop a
rope over the edge to lift supplies and allow the others to climb without packs.
The climber estimates it will take her 45 minutes to get to the top. However,
you are concerned that the rope might be too short to reach the bottom of the
cliff (it is exactly 30.0 m long). If it is too short, she’ll have to climb back
down (another 45 minutes) and you will be too far behind schedule to get to
your destination before dark. As you contemplate how to determine whether
the rope is long enough, you notice that the late afternoon shadow of the
cliff grows as the sun descends over its edge. You suddenly remember your
trigonometry. You measure the length of the shadow from the base of the cliff
to the shadow’s edge (144 ft), and the angle subtended between the base and
top of the cliff measured from the shadow’s edge. The angle is 38.1°. Do you
send the climber, or start backtracking to take another route?
73. M The Weather Monitor. Your South American expedition splits into two groups: one that stays at home base, and yours that goes off to set up a
sensor that will monitor precipitation, temperature, and sunlight through the
upcoming winter. The sensor must link up to a central communications sys-
tem at base camp that simultaneously uploads the data from numerous sensors
to a satellite. In order to set up and calibrate the sensor, you will have to com-
municate with base camp to give them specifi c location information. Unfor-
tunately, the group’s communication and navigation equipment has dwindled
to walkie-talkies and a compass due to a river-raft mishap, which means your
group must not exceed the range of the walkie-talkies (3.0 miles). However,
you do have a laser rangefi nder to help you measure distances as you navigate
with the compass. After a few hours of hiking, you fi nd the perfect plateau on
which to mount the sensor. You have carefully mapped your path from base
camp around lakes and other obstacles: 550 m West (W), 275 m S, 750 m W,
900 m NE, 800 m W, and 400 m 30.0° W of S. The fi nal leg is due south,
2.20 km up a constant slope and ending at a plateau that is 320 m above the
level of base camp. (a) How far are you from base camp? Will you be able to communicate with home base using the walkie-talkies? (b) What is the geographical direction from base camp to the sensor (expressed in the form
θ° south of west, etc.)? (c) What is the angle of inclination from base camp to the detector?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
2.1 Define one-dimensional displacement.
2.2 Discriminate between speed and velocity.
2.3 Define one-dimensional acceleration.
2.4 Use one-dimensional kinematic equations to predict future or past values of variables.
2.5 Solve one-dimensional kinematic problems.
2.6 Solve one-dimensional free-fall problems.
2.7 Predict kinematic quantities using graphical analysis.
er n ie
d ec
k er
/i S
to ck
p h o to
CHAPTER 2
Kinematics in One Dimension
The pilots in the United States Navy’s Blue Angels can perform high-speed maneuvers in perfect unison.
They do so by controlling the displacement, velocity, and acceleration of their jet aircraft. These three
concepts and the relationships among them are the focus of this chapter.
2.1 Displacement There are two aspects to any motion. In a purely descriptive sense, there is the move-
ment itself. Is it rapid or slow, for instance? Then, there is the issue of what causes
the motion or what changes it, which requires that forces be considered. Kinematics deals with the concepts that are needed to describe motion, without any reference to
forces. The present chapter discusses these concepts as they apply to motion in one
dimension, and the next chapter treats two-dimensional motion. Dynamics deals with the eff ect that forces have on motion, a topic that is considered in Chapter 4. Together,
kinematics and dynamics form the branch of physics known as mechanics. We turn now to the fi rst of the kinematics concepts to be discussed, which is displacement.
To describe the motion of an object, we must be able to specify the location of
the object at all times, and Figure 2.1 shows how to do this for one-dimensional motion. In this drawing, the initial position of a car is indicated by the vector
labeled x0→ . The length of x0→ is the distance of the car from an arbitrarily chosen origin. At a later time the car has moved to a new position, which is indicated by the
vector x→. The displacement of the car ∆ x→ (read as “delta x” or “the change in x”) is a vector drawn from the initial position to the fi nal position. Displacement is a vec-
tor quantity in the sense discussed in Section 1.5, for it conveys both a magnitude 27
28 CHAPTER 2 Kinematics in One Dimension
(the distance between the initial and fi nal positions) and a direction. The displacement can be
related to x0→ and x→ by noting from the drawing that x0→ + ∆x→ = x→ or ∆x→ = x→ − x0→
Thus, the displacement ∆x→ is the diff erence between x→ and x0→ , and the Greek letter delta (∆) is used to signify this diff erence. It is important to note that the change in any variable is always the
fi nal value minus the initial value.
DEFINITION OF DISPLACEMENT The displacement is a vector that points from an object’s initial position to its fi nal position and has a magnitude that equals the shortest distance between the two positions. SI Unit of Displacement: meter (m)
The SI unit for displacement is the meter (m), but there are other units as well, such as the
centimeter and the inch. When converting between centimeters (cm) and inches (in.), remember
that 2.54 cm = 1 in.
Often, we will deal with motion along a straight line. In such a case, a displacement in one
direction along the line is assigned a positive value, and a displacement in the opposite direction is
assigned a negative value. For instance, assume that a car is moving along an east/west direction
and that a positive (+) sign is used to denote a direction due east. Then, ∆x→ = +500 m represents a displacement that points to the east and has a magnitude of 500 meters. Conversely, ∆x→ = −500 m is a displacement that has the same magnitude but points in the opposite direction, due west.
The magnitude of the displacement vector is the shortest distance between the initial and
fi nal positions of the object. However, this does not mean that displacement and distance are the
same physical quantities. In Figure 2.1, for example, the car could reach its fi nal position after going forward and backing up several times. In that case, the total distance traveled by the car
would be greater than the magnitude of the displacement vector.
Check Your Understanding
(The answer is given at the end of the book.) 1. A honeybee leaves the hive and travels a total distance of 2 km before returning to the hive. What is the
magnitude of the displacement vector of the bee?
2.2 Speed and Velocity
Average Speed One of the most obvious features of an object in motion is how fast it is moving. If a car travels
200 meters in 10 seconds, we say its average speed is 20 meters per second, the average speed being the distance traveled divided by the time required to cover the distance:
Average speed = Distance
Elapsed time (2.1)
Equation 2.1 indicates that the unit for average speed is the unit for distance divided by the unit for time,
or meters per second (m/s) in SI units. Example 1 illustrates how the idea of average speed is used.
Origin
Displacement = Δx
t0
x0
x
t
FIGURE 2.1 The displacement ∆x→ is a vector that points from the initial position x→ 0 to the fi nal position x→.
EXAMPLE 1 Distance Run by a Jogger
How far does a jogger run in 1.5 hours (5400 s) if his average speed is
2.22 m/s?
Reasoning The average speed of the jogger is the average distance per second that he travels. Thus, the distance covered by the jogger is equal
to the average distance per second (his average speed) multiplied by the
number of seconds (the elapsed time) that he runs.
Solution To fi nd the distance run, we rewrite Equation 2.1 as
Distance = (Average speed)(Elapsed time) = (2.22 m /s)(5400 s)
= 12 000 m
2.2 Speed and Velocity 29
Speed is a useful idea, because it indicates how fast an object is moving. However, speed does not
reveal anything about the direction of the motion. To describe both how fast an object moves and
the direction of its motion, we need the vector concept of velocity.
Average Velocity To defi ne the velocity of an object, we will use two concepts that we have already encountered,
displacement and time. The building of new concepts from more basic ones is a common theme
in physics. In fact the great strength of physics as a science is that it builds a coherent understand-
ing of nature through the development of interrelated concepts.
Suppose that the initial position of the car in Figure 2.1 is x→ 0 when the time is t0. A little later that car arrives at the fi nal position x→ at the time t. The diff erence between these times is the time required for the car to travel between the two positions. We denote this diff erence
by the shorthand notation ∆t (read as “delta t”), where ∆t represents the fi nal time t minus the initial time t0:
∆t = t − t0 Elapsed time
Note that ∆t is defi ned in a manner analogous to ∆x→, which is the fi nal position minus the initial position (∆x→ = x→ − x→ 0). Dividing the displacement ∆x→ of the car by the elapsed time ∆t gives the average velocity of the car. It is customary to denote the average value of a quantity by pla- cing a horizontal bar above the symbol representing the quantity. The average velocity, then, is
written as v→, as specifi ed in Equation 2.2:
DEFINITION OF AVERAGE VELOCITY
Average velocity = Displacement
Elapsed time
v→ = x→ − x→0 t − t0
= ∆ x→ ∆ t
(2.2)
SI Unit of Average Velocity: meter per second (m/s)
Equation 2.2 indicates that the unit for average velocity is the unit for length divided by the
unit for time, or meters per second (m/s) in SI units. Velocity can also be expressed in other units,
such as kilometers per hour (km/h) or miles per hour (mi/h).
Average velocity is a vector that points in the same direction as the displacement in Equa-
tion 2.2. Figure 2.2 illustrates that the velocity of an object confi ned to move along a line can point either in one direction or in the opposite direction. As with displacement, we will use
plus and minus signs to indicate the two possible directions. If the displacement points in the
positive direction, the average velocity is positive. Conversely, if the displacement points in
the negative direction, the average velocity is negative. Example 2 illustrates these features of
average velocity.
⏟
FIGURE 2.2 The boats in this photograph are traveling in opposite directions; in other
words, the velocity of one boat points in a
direction that is opposite to the velocity of
the other boat.
© Michael Dietrich/Age Fotostock
EXAMPLE 2 The World’s Fastest Jet-Engine Car
Andy Green in the car ThrustSSC set a world record of 341.1 m/s (763 mi/h) in 1997. The car was powered by two jet engines, and it was
the fi rst one offi cially to exceed the speed of sound. To establish such a
record, the driver makes two runs through the course, one in each direc-
tion, to nullify wind eff ects. Figure 2.3a shows that the car fi rst travels from left to right and covers a distance of 1609 m (1 mile) in a time of
4.740 s. Figure 2.3b shows that in the reverse direction, the car covers the same distance in 4.695 s. From these data, determine the average
velocity for each run.
Reasoning Average velocity is defi ned as the displacement divided by the elapsed time. In using this defi nition we recognize that the displace-
ment is not the same as the distance traveled. Displacement takes the dir-
ection of the motion into account, and distance does not. During both
runs, the car covers the same distance of 1609 m. However, for the fi rst
run the displacement is ∆ x→ = +1609 m, while for the second it is ∆ x→ = −1609 m. The plus and minus signs are essential, because the fi rst run is
to the right, which is the positive direction, and the second run is in the
opposite or negative direction.
30 CHAPTER 2 Kinematics in One Dimension
Instantaneous Velocity Suppose the magnitude of your average velocity for a long trip was 20 m/s. This value, being an
average, does not convey any information about how fast you were moving or the direction of
the motion at any instant during the trip. Both can change from one instant to another. Surely
there were times when your car traveled faster than 20 m/s and times when it traveled more
slowly. The instantaneous velocity v→ of the car indicates how fast the car moves and the direc- tion of the motion at each instant of time. The magnitude of the instantaneous velocity is called
the instantaneous speed, and it is the number (with units) indicated by the speedometer. The instantaneous velocity at any point during a trip can be obtained by measuring the time
interval ∆t for the car to travel a very small displacement ∆x→. We can then compute the average velocity over this interval. If the time ∆t is small enough, the instantaneous velocity does not change much during the measurement. Then, the instantaneous velocity v→ at the point of interest is approximately equal to (≈) the average velocity v→ computed over the interval, or v→ ≈ v→ = ∆x→/∆t (for suffi ciently small ∆t). In fact, in the limit that ∆t becomes infi nitesimally small, the instant- aneous velocity and the average velocity become equal, so that
v→ = lim ∆t → 0
∆x→
∆t (2.3)
The notation lim ∆ t → 0
∆x→
∆t means that the ratio ∆x→/∆t is defi ned by a limiting process in
which smaller and smaller values of ∆t are used, so small that they approach zero. As smaller values of ∆t are used, ∆x→ also becomes smaller. However, the ratio ∆x→/∆t does not become zero but, rather, approaches the value of the instantaneous velocity. For brevity, we will use the word
velocity to mean “instantaneous velocity” and speed to mean “instantaneous speed.”
Check Your Understanding
(The answers are given at the end of the book.) 2. Is the average speed of a vehicle a vector or a scalar quantity? 3. Two buses depart from Chicago, one going to New York and one to San Francisco. Each bus travels at
a speed of 30 m/s. Do they have equal velocities?
4. One of the following statements is incorrect. (a) The car traveled around the circular track at a con- stant velocity. (b) The car traveled around the circular track at a constant speed. Which statement is incorrect?
Start Finish
Δx = +1609 m
t0 = 0 s
(a)
t = 4.740 s
Finish Start
Δx = –1609 m
t0 = 0 s
(b)
t = 4.695 s
– +
FIGURE 2.3 The arrows in the box at the top of the drawing indicate the positive and negative directions for the displacements of the car, as
explained in Example 2.
Solution According to Equation 2.2, the average velocities are
Run 1 v→ = ∆x →
∆t =
+1609 m
4.740 s = +339.5 m/s
Run 2 v→ = ∆x →
∆t =
−1609 m
4.695 s = −342.7 m/s
In these answers the algebraic signs convey the directions of the velocity
vectors. In particular, for run 2 the minus sign indicates that the average
velocity, like the displacement, points to the left in Figure 2.3b. The magnitudes of the velocities are 339.5 and 342.7 m/s. The average of
these numbers is 341.1 m/s, and this is recorded in the record book.
2.3 Acceleration 31
5. A straight track is 1600 m in length. A runner begins at the starting line, runs due east for the full length of the track, turns around and runs halfway back. The time for this run is fi ve minutes. What is the
runner’s average velocity, and what is his average speed?
6. The average velocity for a trip has a positive value. Is it possible for the instantaneous velocity at a point during the trip to have a negative value?
2.3 Acceleration In a wide range of motions, the velocity changes from moment to moment, such as in the case of
the sprinter in Photo 2.1. To describe the manner in which it changes, the concept of acceleration is needed. The velocity of a moving object may change in a number of ways. For example, it may
increase, as it does when the driver of a car steps on the gas pedal to pass the car ahead. Or it may
decrease, as it does when the driver applies the brakes to stop at a red light. In either case, the
change in velocity may occur over a short or a long time interval. To describe how the velocity
of an object changes during a given time interval, we now introduce the new idea of acceleration.
This idea depends on two concepts that we have previously encountered, velocity and time. Spe-
cifi cally, the notion of acceleration emerges when the change in the velocity is combined with the time during which the change occurs.
The meaning of average acceleration can be illustrated by considering a plane during takeoff . Figure 2.4 focuses attention on how the plane’s velocity changes along the runway. Dur- ing an elapsed time interval ∆t = t − t0, the velocity changes from an initial value of v→ 0 to a fi nal velocity of v→. The change ∆v→ in the plane’s velocity is its fi nal velocity minus its initial velocity, so that ∆v→ = v→ − v→ 0. The average acceleration a→ is defi ned in the following manner, to provide a measure of how much the velocity changes per unit of elapsed time.
DEFINITION OF AVERAGE ACCELERATION
Average acceleration = Change in velocity
Elapsed time
a→ =
v→ − v0→
t − t0 =
∆ v→ ∆t (2.4)
SI Unit of Average Acceleration: meter per second squared (m/s2)
The average acceleration a→ is a vector that points in the same direction as ∆v→, the change in the velocity. Following the usual custom, plus and minus signs indicate the two possible direc-
tions for the acceleration vector when the motion is along a straight line.
We are often interested in an object’s acceleration at a particular instant of time. The
instantaneous acceleration a→ can be defi ned by analogy with the procedure used in Section 2.2 for instantaneous velocity:
a→ = lim ∆ t → 0
∆v→
∆t (2.5)
Equation 2.5 indicates that the instantaneous acceleration is a limiting case of the average
acceleration. When the time interval ∆t for measuring the acceleration becomes extremely small
t0
v0 v
t– +
a
FIGURE 2.4 During takeoff , the plane accelerates from an initial velocity v→0 to a fi nal velocity v→ during the time interval ∆t = t − t0.
PHOTO 2.1 As this sprinter explodes out of the starting block, his velocity is changing,
which means that he is accelerating.
Jim Cummins/Taxi/Getty Images
32 CHAPTER 2 Kinematics in One Dimension
(approaching zero in the limit), the average acceleration and the instantaneous acceleration be-
come equal. Moreover, in many situations the acceleration is constant, so the acceleration has
the same value at any instant of time. In the future, we will use the word acceleration to mean “instantaneous acceleration.” Example 3 deals with the acceleration of a plane during takeoff .
EXAMPLE 3 Acceleration and Increasing Velocity
Suppose the plane in Figure 2.4 starts from rest (v→0 = 0 m/s) when t0 = 0 s. The plane accelerates down the runway and at t = 29 s attains a velocity of v→ = +260 km/h, where the plus sign indicates that the velocity points to the right. Determine the average acceleration of the plane.
Reasoning The average acceleration of the plane is defi ned as the change in its velocity divided by the elapsed time. The change in the plane’s
velocity is its fi nal velocity v→ minus its initial velocity v→0, or v→ − v→0. The elapsed time is the fi nal time t minus the initial time t0, or t − t0.
Problem-Solving Insight The change in any variable is the fi nal value minus the initial value: for example, the change in velocity is ∆v→ = v→ − v0→ , and the change in time is ∆ t = t − t0.
Solution The average acceleration is expressed by Equation 2.4 as
a→ = v→ − v→0 t − t0
= 260 km/h − 0 km/h
29 s − 0 s = +9.0
km /h
s
The average acceleration calculated in Example 3 is read as “nine kilometers per hour
per second.” Assuming the acceleration of the plane is constant, a value of +9.0 km/h
s
means the velocity changes by +9.0 km/h during each second of the motion. During the fi rst
second, the velocity increases from 0 to 9.0 km/h; during the next second, the velocity increases
by another 9.0 km/h to 18 km/h, and so on. Figure 2.5 illustrates how the velocity changes dur- ing the fi rst two seconds. By the end of the 29th second, the velocity is 260 km/h.
It is customary to express the units for acceleration solely in terms of SI units. One way to
obtain SI units for the acceleration in Example 3 is to convert the velocity units from km/h to m/s:
(260 kmh )( 1000 m
1 km )( 1 h
3600 s) = 72 m
s
The average acceleration then becomes
a→ = 72 m/s − 0 m/s 29 s − 0 s
= +2.5 m/s2
where we have used 2.5 m/s
s = 2.5
m
s ·s = 2.5 m
s2 . An acceleration of 2.5
m
s2 is read as
“2.5 meters per second per second” (or “2.5 meters per second squared”) and means that the
velocity changes by 2.5 m/s during each second of the motion.
Example 4 deals with a case where the motion becomes slower as time passes.
Δt = 0 s
Δt = 1.0 s
Δt = 2.0 s
v0 = 0 m/s
v = +9.0 km/h
v = +18 km/h
a = +9.0 km/h
s
FIGURE 2.5 An acceleration of +9.0 km /h
s
means that the velocity of the plane changes
by +9.0 km/h during each second of the
motion. The “+” direction for a→ and v → is to the right.
2.3 Acceleration 33
Figure 2.7 shows how the velocity of the dragster in Example 4 changes during the braking, assuming that the acceleration is constant throughout the motion. The acceleration
calculated in Example 4 is negative, indicating that the acceleration points to the left in the
drawing. As a result, the acceleration and the velocity point in opposite directions.
Problem-Solving Insight Whenever the acceleration and velocity vectors have opposite directions, the object slows down and is said to be “decelerating.”
In contrast, the acceleration and velocity vectors in Figure 2.5 point in the same direction, and the object speeds up.
Check Your Understanding
(The answers are given at the end of the book.) 7. At one instant of time, a car and a truck are traveling side by side in adjacent lanes of a highway. The
car has a greater velocity than the truck has. Does the car necessarily have the greater acceleration?
EXAMPLE 4 Acceleration and Decreasing Velocity
A drag racer crosses the fi nish line, and the driver deploys a parachute and
applies the brakes to slow down, as Figure 2.6 illustrates. The driver be- gins slowing down when t0 = 9.0 s and the car’s velocity is v→ 0 = +28 m/s. When t = 12.0 s, the velocity has been reduced to v→ = +13 m/s. What is the average acceleration of the dragster?
Reasoning The average acceleration of an object is always specifi ed as its change in velocity, v→ − v→ 0, divided by the elapsed time, t − t0. This
is true whether the fi nal velocity is less than the initial velocity or greater
than the initial velocity.
Solution The average acceleration is, according to Equation 2.4,
a→ = v→ − v→0 t − t0
= 13 m/s − 28 m/s
12.0 s − 9.0 s = −5.0 m /s2
FIGURE 2.6 (a) To slow down, a drag racer deploys a parachute and applies the brakes. (b) The velocity of the car is decreasing, giving rise to an average acceleration a→ that points opposite to the velocity.
v0 = +28 m/s v = +13 m/s
a = –5.0 m/s2
t0 = 9.0 s t = 12 s
– +
(b)(a)
C h ri
s S
za g o la
/C al
S p o rt
M ed
ia /
N ew
sc o m
FIGURE 2.7 Here, an acceleration of −5.0 m/s2 means the velocity decreases by 5.0 m/s during each
second of elapsed time.
Δt = 0 s
Δt = 1.0 s
Δt = 2.0 s
v0 = +28 m/s
v = +23 m/s
v = +18 m/s
a = –5.0 m/s 2
Continued
34 CHAPTER 2 Kinematics in One Dimension
8. Two cars are moving in the same direction (the positive direction) on a straight road. The acceleration of each car also points in the positive direction. Car 1 has a greater acceleration than car 2 has. Which
one of the following statements is true? (a) The velocity of car 1 is always greater than the velocity of car 2. (b) The velocity of car 2 is always greater than the velocity of car 1. (c) In the same time interval, the velocity of car 1 changes by a greater amount than the velocity of car 2 does. (d) In the same time interval, the velocity of car 2 changes by a greater amount than the velocity of car 1 does.
9. An object moving with a constant acceleration slows down if the acceleration points in the direction opposite to the direction of the velocity. But can an object ever come to a permanent halt if its acceler-
ation truly remains constant?
10. A runner runs half the remaining distance to the fi nish line every ten seconds. She runs in a straight line and does not ever reverse her direction. Does her acceleration have a constant magnitude?
2.4 Equations of Kinematics for Constant Acceleration It is now possible to describe the motion of an object traveling with a constant acceleration
along a straight line. To do so, we will use a set of equations known as the equations of
kinematics for constant acceleration. These equations entail no new concepts, because they
will be obtained by combining the familiar ideas of displacement, velocity, and acceleration.
However, they will provide a very convenient way to determine certain aspects of the motion,
such as the fi nal position and velocity of a moving object.
In discussing the equations of kinematics, it will be convenient to assume that the object is
located at the origin x→0 = 0 m when t0 = 0 s. With this assumption, the displacement ∆x→ = x→ − x→0 becomes ∆x→ = x→. Furthermore, in the equations that follow, as is customary, we dispense with the use of boldface symbols overdrawn with small arrows for the displacement, velocity, and
acceleration vectors. We will, however, continue to convey the directions of these vectors with
plus or minus signs.
Consider an object that has an initial velocity of υ0 at time t0 = 0 s and moves for a time t with a constant acceleration a. For a complete description of the motion, it is also necessary to know the fi nal velocity and displacement at time t. The fi nal velocity υ can be obtained directly from Equation 2.4:
a = a = υ − υ0
t or υ = υ0 + at (constant acceleration) (2.4)
The displacement x at time t can be obtained from Equation 2.2, if a value for the average velocity υ can be obtained. Considering the assumption that x→0 = 0 m at t0 = 0 s, we have
υ = x − x0 t − t0
= x t or x = υt (2.2)
Because the acceleration is constant, the velocity increases at a constant rate. Thus, the average
velocity υ is midway between the initial and fi nal velocities:
υ = 12(υ0 + υ) (constant acceleration) (2.6)
Equation 2.6, like Equation 2.4, applies only if the acceleration is constant and cannot be used
when the acceleration is changing. The displacement at time t can now be determined as
x = υt = 12(υ0 + υ)t (constant acceleration) (2.7)
Notice in Equations 2.4 (υ = υ0 + at) and 2.7 [x = 1
2(υ0 + υ)t] that there are fi ve kinematic variables:
1. x = displacement 2. a = a = acceleration (constant) 3. υ = fi nal velocity at time t 4. υ0 = initial velocity at time t0 = 0 s 5. t = time elapsed since t0 = 0 s
2.4 Equations of Kinematics for Constant Acceleration 35
Each of the two equations contains four of these variables, so if three of them are known, the
fourth variable can always be found. Example 5 illustrates how Equations 2.4 and 2.7 are used to
describe the motion of an object.
Analyzing Multiple-Concept Problems
EXAMPLE 5 The Displacement of a Speedboat
The speedboat in Figure 2.8 has a constant acceleration of +2.0 m/s2. If the initial velocity of the boat is +6.0 m/s, fi nd the boat’s displacement
after 8.0 seconds.
Reasoning As the speedboat accelerates, its velocity is changing. The displacement of the speedboat during a given time interval is equal to
the product of its average velocity during that interval and the time. The
average velocity, on the other hand, is just one-half the sum of the boat’s
initial and fi nal velocities. To obtain the fi nal velocity, we will use the
defi nition of constant acceleration, as given in Equation 2.4.
Knowns and Unknowns The numerical values for the three known variables are listed in the table:
Description Symbol Value Comment Acceleration a +2.0 m/s2 Positive, because the boat is accelerating to the right, which is the positive
direction. See Figure 2.8b.
Initial velocity υ0 +6.0 m/s Positive, because the boat is moving to the right, which is the positive direction. See Figure 2.8b.
Time interval t 8.0 s
Unknown Variable Displacement of boat x ?
FIGURE 2.8 (a) An accelerating speedboat. (b) The boat’s displacement x can be determined if the boat’s acceleration, initial velocity, and time of travel are known.
t0 = 0 s
x
a = +2.0 m/s2
0 = +6.0 m/sυ υ
t = 8.0 s
(b)
– +
(a)
A n th
o n y B
ra d sh
aw /G
et ty
Im ag
es
Modeling the Problem
STEP 1 Displacement Since the acceleration is constant, the displacement x of the boat is given by Equation 2.7, in which υ0 and υ are the initial and fi nal velocities, respectively. In this equation, two of the variables, υ0 and t, are known (see the Knowns and Unknowns table), but the fi nal velocity υ is not. However, the fi nal velocity can be determined by employing the defi nition of acceleration, as Step 2 shows.
STEP 2 Acceleration According to Equation 2.4, which is just the defi nition of constant acceleration, the fi nal velocity υ of the boat is
𝜐 = 𝜐0 + at (2.4)
All the variables on the right side of the equals sign are known, and we can substitute this relation
for υ into Equation 2.7, as shown at the right.
?
x = 12(𝜐0 + 𝜐)t (2.7)
x = 12(𝜐0 + 𝜐)t (2.7)
𝜐 = 𝜐0 + at (2.4)
36 CHAPTER 2 Kinematics in One Dimension
In Example 5, we combined two equations [x = 12(υ0 + υ)t and υ = υ0 + at] into a single equation by algebraically eliminating the fi nal velocity υ of the speedboat (which was not known). The result was the following expression for the displacement x of the speedboat:
x = υ0t + 1
2 at 2 (constant acceleration) (2.8)
The fi rst term (υ0t) on the right side of this equation represents the displacement that would res- ult if the acceleration were zero and the velocity remained constant at its initial value of υ0. The second term (
1
2 at 2) gives the additional displacement that arises because the velocity changes (a is not zero) to values that are diff erent from its initial value.
Equation 2.8 allows us to calculate the displacement of an object undergoing constant accel-
eration, given its acceleration (a), the initial velocity (υ0), and the time (t). However, even if the time interval is not given, we can still calculate the displacement, provided we also know the fi nal
velocity (υ) of the object. We can solve Equation 2.4 for the time t, and then make this substitu- tion into Equation 2.8. The result is x = (υ2 − υ02) /2a. Solving for υ2 gives
υ2 = υ 20 + 2ax (constant acceleration) (2.9)
Equation 2.9 is often used when the time involved in the motion is unknown.
Table 2.1 presents a summary of the equations that we have been considering. These equa- tions are called the equations of kinematics. Each equation contains four of the fi ve kinematic variables, as indicated by the check marks (✓) in the table. The next section shows how to apply
the equations of kinematics.
Check Your Understanding
(The answers are given at the end of the book.) 11. The muzzle velocity of a gun is the velocity of the bullet when it leaves the barrel. The muzzle velocity
of one rifl e with a short barrel is greater than the muzzle velocity of another rifl e that has a longer bar-
rel. In which rifl e is the acceleration of the bullet larger?
12. A motorcycle starts from rest and has a constant acceleration. In a time interval t, it undergoes a dis- placement x and attains a fi nal velocity υ. Then t is increased so that the displacement is 3x. In this same increased time interval, what fi nal velocity does the motorcycle attain?
Solution Algebraically combining the results of Steps 1 and 2, we fi nd that
x = 12(υ0 + υ)t = 1
2[𝜐0 + (υ0 + at) ]t = υ0t + 1
2at 2
The displacement of the boat after 8.0 s is
x = υ0t + 1
2at 2 = (+6.0 m/s)(8.0 s) + 1
2 (+2.0 m/s 2)(8.0 s)2 = +112 m
Related Homework: Problems 39, 55
STEP 1 STEP 2
TABLE 2.1 Equations of Kinematics for Constant Acceleration
Variables Equation Number Equation x a υ υ0 t (2.4) 𝜐 = 𝜐0 + at — ✓ ✓ ✓ ✓
(2.7) x = 12(𝜐0 + 𝜐)t ✓ — ✓ ✓ ✓
(2.8) x = 𝜐0t + 1
2 at 2 ✓ ✓ — ✓ ✓
(2.9) 𝜐 2 = 𝜐0 2 + 2ax ✓ ✓ ✓ ✓ —
2.5 Applications of the Equations of Kinematics 37
2.5 Applications of the Equations of Kinematics The equations of kinematics can be applied to any moving object, as long as the acceleration of
the object is constant. However, remember that each equation contains four variables. Therefore,
numerical values for three of the four must be available if an equation is to be used to calculate the
value of the remaining variable. To avoid errors when using these equations, it helps to follow a
few sensible guidelines and to be alert for a few situations that can arise during your calculations.
Problem-Solving Insight Decide at the start which directions are to be called positive (+) and negative (−) relative to a conveniently chosen coordinate origin.
This decision is arbitrary, but important because displacement, velocity, and acceleration are vectors, and their directions must always be taken into account. In the examples that follow, the positive and negative directions will be shown in the drawings that accompany the problems. It does not matter which direction is chosen to be positive. However, once the choice is made, it should not be changed during the course of the calculation.
Problem-Solving Insight As you reason through a problem before attempting to solve it, be sure to interpret the terms “decelerating” or “deceleration” correctly, should they occur in the
problem statement.
These terms are the source of frequent confusion, and Conceptual Example 6 off ers help in understanding them.
Problem-Solving Insight Sometimes there are two possible answers to a kinematics problem, each answer corresponding to a diff erent situation.
Example 7 discusses one such case.
CONCEPTUAL EXAMPLE 6 Deceleration Versus Negative Acceleration
A car is traveling along a straight road and is decelerating. Which one of
the following statements correctly describes the car’s acceleration? (a) It must be positive. (b) It must be negative. (c) It could be positive or negative.
Reasoning The term “decelerating” means that the acceleration vector points opposite to the velocity vector and indicates that the car is slowing
down. One possibility is that the velocity vector of the car points to the
right, in the positive direction, as Figure 2.9a shows. The term “deceler- ating” implies, then, that the acceleration vector of the car points to the
left, which is the negative direction. Another possibility is that the car
is traveling to the left, as in Figure 2.9b. Now, since the velocity vector points to the left, the acceleration vector would point opposite, or to the
right, which is the positive direction.
Answers (a) and (b) are incorrect. The term “decelerating” means only that the acceleration vector points opposite to the velocity vector. It
is not specifi ed whether the velocity vector of the car points in the positive
or negative direction. Therefore, it is not possible to know whether the
acceleration is positive or negative.
Answer (c) is correct. As shown in Figure 2.9, the acceleration vector of the car could point in the positive or the negative direction, so that the
acceleration could be either positive or negative, depending on the direc-
tion in which the car is moving.
Related Homework: Problems 14, 73
FIGURE 2.9 When a car decelerates along a straight road, the acceleration
vector points opposite to the velocity
vector, as Conceptual Example 6
discusses.
(a)
a
v
(b)
a
v
– +
– +
38 CHAPTER 2 Kinematics in One Dimension
Problem-Solving Insight The motion of two objects may be interrelated, so that they share a common variable. The fact that the motions are interrelated is an important piece of inform-
ation. In such cases, data for only two variables need be specifi ed for each object.
See Interactive LearningWare 2.2 at www.wiley.com/college/cutnell for an example that illustrates this.
Problem-Solving Insight Often the motion of an object is divided into segments, each with a diff erent acceleration. When solving such problems, it is important to realize that
the fi nal velocity for one segment is the initial velocity for the next segment, as Example 8
illustrates.
EXAMPLE 7 The Physics of Spacecraft Retrorockets
The spacecraft shown in Figure 2.10a is traveling with a velocity of +3250 m/s. Suddenly the retrorockets are
fi red, and the spacecraft begins to slow down with an
acceleration whose magnitude is 10.0 m/s2. What is the
velocity of the spacecraft when the displacement of the
craft is +215 km, relative to the point where the ret-
rorockets began fi ring?
Reasoning Since the spacecraft is slowing down, the acceleration must be opposite to the velocity. The
velocity points to the right in the drawing, so the ac-
celeration points to the left, in the negative direction;
thus, a = −10.0 m/s2. The three known variables are listed as follows:
The fi nal velocity υ of the spacecraft can be calcu- lated using Equation 2.9, since it contains the four per-
tinent variables.
Solution From Equation 2.9 (υ2 = υ0 2 + 2ax), we fi nd that
υ = ±√υ 02 + 2ax
= ±√(3250 m /s)2 + 2(−10.0 m /s2)(215 000 m)
= +2500 m/s and −2500 m/s
Both of these answers correspond to the same displace- ment (x = +215 km), but each arises in a diff erent part of the motion. The answer υ = +2500 m/s corresponds to the situation in Figure 2.10a, where the spacecraft has slowed to a speed of 2500 m/s, but is still traveling
to the right. The answer υ = −2500 m/s arises because the retrorockets eventually bring the spacecraft to a
momentary halt and cause it to reverse its direction.
Then it moves to the left, and its speed increases due
to the continually fi ring rockets. After a time, the
velocity of the craft becomes υ = −2500 m/s, giving rise to the situation in Figure 2.10b. In both parts of the drawing the spacecraft has the same displacement,
but a greater travel time is required in part b compared to part a.
Spacecraft Data x a υ υ0 t
+215 000 m −10.0 m/s2 ? +3250 m/s
FIGURE 2.10 (a) Because of an acceleration of −10.0 m/s2, the spacecraft changes its velocity from υ0 to υ. (b) Continued fi ring of the retrorockets changes the direction of the craft’s motion.
0 = +3250 m/sυ
0 = +3250 m/sυ
= +2500 m/sυ
= 0 m/s υ
= 0 m/s υ
= –2500 m/sυ
(b)
(a)
υ
x = +215 km
x = +215 km
–
+
2.5 Applications of the Equations of Kinematics 39
Analyzing Multiple-Concept Problems
EXAMPLE 8 A Motorcycle Ride
A motorcycle ride consists of two segments, as shown in Interactive Figure 2.11a. During segment 1, the motorcycle starts from rest, has an acceleration of +2.6 m/s2, and has a displacement of +120 m. Immedi-
ately after segment 1, the motorcycle enters segment 2 and begins slow-
ing down with an acceleration of −1.5 m/s2 until its velocity is +12 m/s.
What is the displacement of the motorcycle during segment 2?
Reasoning We can use an equation of kinematics from Table 2.1 to fi nd the displacement x2 for segment 2. To do this, it will be necessary to have values for three of the variables that appear in the equation.
Values for the acceleration (a2 = −1.5 m/s2) and fi nal velocity (υ2 = +12 m/s) are given. A value for a third variable, the initial velocity υ02, can be obtained by noting that it is also the fi nal velocity of segment 1. The
fi nal velocity of segment 1 can be found by using an appropriate equation
of kinematics, since three variables (x1, a1, and υ01) are known for this part of the motion, as the following table reveals.
Knowns and Unknowns The data for this problem are listed in the table:
Description Symbol Value Comment Explicit Data Displacement for segment 1 x1 +120 m
Acceleration for segment 1 a1 +2.6 m/s2 Positive, because the motorcycle moves in the +x direction and speeds up.
Acceleration for segment 2 a2 −1.5 m/s2 Negative, because the motorcycle moves in the +x direction and slows down.
Final velocity for segment 2 υ2 +12 m/s
Implicit Data Initial velocity for segment 1 υ01 0 m/s The motorcycle starts from rest.
Unknown Variable Displacement for segment 2 x2 ?
x2
v2 = +12 m/s
v02 v01 = 0 m/s
v1
a1 = +2.6 m/s 2a2 = –1.5 m/s
2
(b) Segment 2
x1 = +120 m
(c) Segment 1
Segment 1
x2
x1
Segment 2
(a)
–
+
INTERACTIVE FIGURE 2.11 (a) This motorcycle ride consists of two segments, each with a diff erent acceleration. (b) The variables for segment 2. (c) The variables for segment 1.
40 CHAPTER 2 Kinematics in One Dimension
Modeling the Problem
STEP 1 Displacement During Segment 2 Interactive Figure 2.11b shows the situation during segment 2. Two of the variables—the fi nal velocity υ2 and the acceleration a2—are known, and for convenience we choose Equation 2.9 to fi nd the displacement x2 of the motorcycle:
υ 22 = υ 202 + 2a2 x2 (2.9)
Solving this relation for x2 yields Equation 1 at the right. Although the initial velocity υ02 of segment 2 is not known, we will be able to determine its value from a knowledge of the motion
during segment 1, as outlined in Steps 2 and 3.
STEP 2 Initial Velocity of Segment 2 Since the motorcycle enters segment 2 immediately after leaving segment 1, the initial velocity υ02 of segment 2 is equal to the fi nal velocity υ1 of segment 1, or υ02 = υ1. Squaring both sides of this equation gives
𝜐 202 = 𝜐
2 1
This result can be substituted into Equation 1 as shown at the right. In the next step υ1 will be determined.
STEP 3 Final Velocity of Segment 1 Interactive Figure 2.11c shows the motorcycle during segment 1. Since we know the initial velocity υ01, the acceleration a1, and the displacement x1, we can employ Equation 2.9 to fi nd the fi nal velocity υ1 at the end of segment 1:
𝜐 21 = 𝜐
2 01 + 2a1x1
This relation for υ12 can be substituted into Equation 2, as shown at the right.
Solution Algebraically combining the results of each step, we fi nd that
x2 = υ 22 − υ 202
2a2 =
υ 22 − υ 21 2a2
= υ 22 − (υ 201 + 2a1x1)
2a2 The displacement x2 of the motorcycle during segment 2 is
x2 = υ 22 − (υ 201 + 2a1x1)
2a2
= (+12 m/s)2 − [(0 m/s)2 + 2(+2.6 m/s2)(+120 m)]
2(−1.5 m/s2) = +160 m
Related Homework: Problems 59, 80
STEP 2STEP 1 STEP 3
x2 = 𝜐 22 − 𝜐
2 02
2a2 (1)
?
Math Skills Interactive Figure 2.11a shows which direction has been chosen as the positive direction, and the choice leads to a value of x2 = +160 m for the displacement of the motorcycle during segment 2. This answer means that displacement is 160 m in the
positive direction, which is upward and to the right in the drawing. The choice for the pos-
itive direction is completely arbitrary, however. The meaning of the answer to the problem
will be the same no matter what choice is made. Suppose that the choice for the positive
direction were opposite to that shown in Interactive Figure 2.11a. Then, all of the data listed in the Knowns and Unknowns table would appear with algebraic signs opposite to
those specifi ed, and the calculation of the displacement x2 would appear as follows:
x2 = (−12 m/s)2 − [(0 m/s)2 + 2(−2.6 m/s2)(−120 m)]
2(+1.5 m/s2) = −160 m
The value for x2 has the same magnitude of 160 m as before, but it is now negative. The negative sign means that the displacement of the motorcycle during segment 2 is 160 m
in the negative direction. But the negative direction is now upward and to the right in Interactive Figure 2.11a, so the meaning of the result is exactly the same as it was before.
?
x2 = 𝜐 22 − 𝜐
2 02
2a2 (1)
𝜐 202 = 𝜐 2
1 (2)
x2 = 𝜐 22 − 𝜐
2 02
2a2 (1)
𝜐 202 = 𝜐 2
1 (2)
𝜐 21 = 𝜐 2
01 + 2a1x1 (3)
2.6 Freely Falling Bodies 41
Now that we have seen how the equations of kinematics are applied to various situations,
it’s a good idea to summarize the reasoning strategy that has been used. This strategy, which
is outlined below, will also be used when we consider freely falling bodies in Section 2.6 and
two-dimensional motion in Chapter 3.
REASONING STRATEGY Applying the Equations of Kinematics 1. Make a drawing to represent the situation being studied. A drawing helps us to see what’s
happening. 2. Decide which directions are to be called positive (+) and negative (−) relative to a con-
veniently chosen coordinate origin. Do not change your decision during the course of a calculation.
3. In an organized way, write down the values (with appropriate plus and minus signs) that are given for any of the fi ve kinematic variables (x, a, υ, υ0, and t). Be on the alert for implicit data, such as the phrase “starts from rest,” which means that the value of the initial velocity is υ0 = 0 m/s. The data summary tables used in the examples in the text are a good way to keep track of this information. In addition, identify the variables that you are being asked to determine.
4. Before attempting to solve a problem, verify that the given information contains values for at least three of the fi ve kinematic variables. Once the three known variables are identifi ed along with the desired unknown variable, the appropriate relation from Table 2.1 can be selected. Remember that the motion of two objects may be interrelated, so they may share a common variable. The fact that the motions are interrelated is an important piece of information. In such cases, data for only two variables need be specifi ed for each object.
5. When the motion of an object is divided into segments, as in Example 8, remember that the fi nal velocity of one segment is the initial velocity for the next segment.
6. Keep in mind that there may be two possible answers to a kinematics problem as, for instance, in Example 7. Try to visualize the diff erent physical situations to which the answers correspond.
2.6 Freely Falling Bodies Everyone has observed the eff ect of gravity as it causes objects to fall downward. In the absence
of air resistance, it is found that all bodies at the same location above the earth fall vertically with
the same acceleration. Furthermore, if the distance of the fall is small compared to the radius of
the earth, the acceleration remains essentially constant throughout the descent. This idealized
motion, in which air resistance is neglected and the acceleration is nearly constant, is known as
free-fall. Since the acceleration is constant in free-fall, the equations of kinematics can be used. The acceleration of a freely falling body is called the acceleration due to gravity, and its
magnitude (without any algebraic sign) is denoted by the symbol g. The acceleration due to gravity is directed downward, toward the center of the earth. Near the earth’s surface, g is approximately
g = 9.80 m/s2
or 32.2 ft/s2
Unless circumstances warrant otherwise, we will use either of these values for g in subsequent cal- culations. In reality, however, g decreases with increasing altitude and varies slightly with latitude.
Figure 2.12a shows the well-known phenomenon of a rock falling faster than a sheet of paper. The eff ect of air resistance is responsible for the slower fall of the paper, for when air is removed
from the tube, as in Figure 2.12b, the rock and the paper have exactly the same acceleration due to gravity. In the absence of air, the rock and the paper both exhibit free-fall motion. Free-fall is closely
approximated for objects falling near the surface of the moon, where there is no air to retard the mo-
tion. A nice demonstration of free-fall was performed on the moon by astronaut David Scott, who
dropped a hammer and a feather simultaneously from the same height. Both experienced the same
acceleration due to lunar gravity and consequently hit the ground at the same time. The acceleration
due to gravity near the surface of the moon is approximately one-sixth as large as that on the earth.
When the equations of kinematics are applied to free-fall motion, it is natural to use the
symbol y for the displacement, since the motion occurs in the vertical or y direction. Thus, when using the equations in Table 2.1 for free-fall motion, we will simply replace x with y. There is no
Air-filled tube (a)
Evacuated tube (b)
FIGURE 2.12 (a) In the presence of air res- istance, the acceleration of the rock is greater
than that of the paper. (b) In the absence of air resistance, both the rock and the paper
have the same acceleration.
42 CHAPTER 2 Kinematics in One Dimension
signifi cance to this change. The equations have the same algebraic form for either the horizontal
or vertical direction, provided that the acceleration remains constant during the motion. We now
turn our attention to several examples that illustrate how the equations of kinematics are applied
to freely falling bodies.
EXAMPLE 9 A Falling Stone
A stone is dropped from rest from the top of a tall building, as Animated Figure 2.13 indicates. After 3.00 s of free-fall, what is the displacement y of the stone?
Reasoning The upward direction is chosen as the positive direction. The three known variables are shown in the table below. The initial ve-
locity υ0 of the stone is zero, because the stone is dropped from rest. The acceleration due to gravity is negative, since it points downward in the
negative direction.
Stone Data y a υ υ0 t
? −9.80 m/s2 0 m/s 3.00 s
Equation 2.8 contains the appropriate variables and off ers a direct solu-
tion to the problem. Since the stone moves downward, and upward is the
positive direction, we expect the displacement y to have a negative value.
Problem-Solving Insight It is only when values are avail- able for at least three of the fi ve kinematic variables (y, a, υ, υ0, and t) that the equations in Table 2.1 can be used to determine the fourth and fi fth variables.
Solution Using Equation 2.8, we fi nd that
y = υ0t + 1
2 at 2 = (0 m/s)(3.00 s) + 1
2 (−9.80 m/s 2) (3.00 s)2 = −44.1 m
The answer for y is negative, as expected.
ANIMATED FIGURE 2.13 The stone, starting with zero velocity at the top of
the building, is accelerated downward
by gravity.
+
–
υ
y
υ0 = 0 m/s
t = 3.00 s
EXAMPLE 10 The Velocity of a Falling Stone
After 3.00 s of free-fall, what is the velocity υ of the stone in Animated Figure 2.13?
Reasoning Because of the acceleration due to gravity, the magnitude of the stone’s downward velocity increases by 9.80 m/s during each second
of free-fall. The data for the stone are the same as in Example 9, and
Equation 2.4 off ers a direct solution for the fi nal velocity. Since the stone
is moving downward in the negative direction, the value determined for υ should be negative.
Solution Using Equation 2.4, we obtain
υ = υ0 + at = 0 m/s + (−9.80 m/s2)(3.00 s) = −29.4 m/s
The velocity is negative, as expected.
FIGURE 2.14 At the start of a football game, a referee tosses a
coin upward with an initial
velocity of υ0 = +5.00 m/s. The velocity of the coin is
momentarily zero when the coin
reaches its maximum height.
υ = 0 m/s
υ 0 = +5.00 m/s
y
–
+
The acceleration due to gravity is always a downward-pointing vector. It describes how the
speed increases for an object that is falling freely downward. This same acceleration also de-
scribes how the speed decreases for an object moving upward under the infl uence of gravity
alone, in which case the object eventually comes to a momentary halt and then falls back to earth.
Examples 11 and 12 show how the equations of kinematics are applied to an object that is moving
upward under the infl uence of gravity.
2.6 Freely Falling Bodies 43
EXAMPLE 11 How High Does It Go?
A football game customarily begins with a coin toss to determine who
kicks off . The referee tosses the coin up with an initial speed of 5.00 m/s.
In the absence of air resistance, how high does the coin go above its point
of release?
Reasoning The coin is given an upward initial velocity, as in Figure 2.14. But the acceleration due to gravity points downward. Since the velocity
and acceleration point in opposite directions, the coin slows down as it
moves upward. Eventually, the velocity of the coin becomes υ = 0 m/s at the highest point. Assuming that the upward direction is positive, the data
can be summarized as shown below:
Coin Data y a υ υ0 t
? −9.80 m/s2 0 m/s +5.00 m/s
With these data, we can use Equation 2.9 (υ2 = υ02 + 2ay) to fi nd the maximum height y.
Problem-Solving Insight Implicit data are important. In Example 11, for instance, the phrase “how high does the coin go” refers to the maximum height, which occurs when the fi nal velocity υ in the vertical direction is υ = 0 m/s.
Solution Rearranging Equation 2.9, we fi nd that the maximum height of the coin above its release point is
y = υ2 − υ02
2a =
(0 m/s)2 − (5.00 m/s)2
2(−9.80 m/s2) = 1.28 m
Math Skills The rearrangement of algebraic equations is a problem-solving step that occurs often. The guiding rule in such
a procedure is that whatever you do to one side of an equation,
you must also do to the other side. Here in Example 11, for
instance, we need to rearrange υ2 = υ02 + 2ay (Equation 2.9) in order to determine y. The part of the equation that contains y is 2ay, and we begin by isolating that part on one side of the equals sign. To do this we subtract υ02 from each side of the equation:
𝜐2 − 𝜐 20 = 𝜐0 2 + 2ay − 𝜐02 = 2ay
Thus, we see that 2ay = υ2 − υ02. Then, we eliminate the term 2a from the left side of the equals sign by dividing both sides of the
equation by 2a.
2ay 2a
= υ2 − υ02
2a or y =
υ2 − υ02
2a
The term 2a occurs both in the numerator and the denominator on the left side of this result and can be eliminated algebraically,
leaving the desired expression for y.
EXAMPLE 12 How Long Is It in the Air?
In Figure 2.14, what is the total time the coin is in the air before returning to its release point?
Reasoning During the time the coin travels upward, gravity causes its speed to decrease to zero. On the way down, however, gravity causes the
coin to regain the lost speed. Thus, the time for the coin to go up is equal to
the time for it to come down. In other words, the total travel time is twice
the time for the upward motion. The data for the coin during the upward trip
are the same as in Example 11. With these data, we can use Equation 2.4
(υ = υ0 + at) to fi nd the upward travel time.
Solution Rearranging Equation 2.4, we fi nd that
t = υ − υ0
a =
0 m/s − 5.00 m/s
−9.80 m/s2 = 0.510 s
The total up-and-down time is twice this value, or 1.02 s .
It is possible to determine the total time by another method. When
the coin is tossed upward and returns to its release point, the displace-
ment for the entire trip is y = 0 m. With this value for the displacement, Equation 2.8 (y = υ0t +
1
2at 2) can be used to fi nd the time for the entire trip directly.
Examples 11 and 12 illustrate that the expression “freely falling” does not necessarily mean
an object is falling down. A freely falling object is any object moving either upward or downward
under the infl uence of gravity alone. In either case, the object always experiences the same down- ward acceleration due to gravity, a fact that is the focus of the next example.
CONCEPTUAL EXAMPLE 13 Acceleration Versus Velocity
There are three parts to the motion of the coin in Figure 2.14, in which air resistance is being ignored. On the way up, the coin has an upward-
pointing velocity vector with a decreasing magnitude. At the top of its
path, the velocity vector of the coin is momentarily zero. On the way
down, the coin has a downward-pointing velocity vector with an increasing
magnitude. Compare the acceleration vector of the coin with the velocity
44 CHAPTER 2 Kinematics in One Dimension
The motion of an object that is thrown upward and eventually returns to earth has a sym-
metry that is useful to keep in mind from the point of view of problem solving. The calculations
just completed indicate that a time symmetry exists in free-fall motion, in the sense that the time
required for the object to reach maximum height equals the time for it to return to its starting
point.
A type of symmetry involving the speed also exists. Figure 2.15 shows the coin considered in Examples 11 and 12. At any displacement y above the point of release, the coin’s speed during the upward trip equals the speed at the same point during the downward trip. For instance, when
y = +1.04 m, Equation 2.9 gives two possible values for the fi nal velocity υ, assuming that the initial velocity is υ0 = +5.00 m/s:
υ2 = υ02 + 2ay = (5.00 m/s)2 + 2(−9.80 m /s2)(1.04 m) = 4.62 m2/s2
υ = ±2.15 m/s
The value υ = +2.15 m/s is the velocity of the coin on the upward trip, and υ = −2.15 m/s is the velocity on the downward trip. The speed in both cases is identical and equals 2.15 m/s.
Likewise, the speed just as the coin returns to its point of release is 5.00 m/s, which equals the
initial speed. This symmetry involving the speed arises because the coin loses 9.80 m/s in speed
each second on the way up and gains back the same amount each second on the way down. In
Conceptual Example 14, we use just this kind of symmetry to guide our reasoning as we analyze
the motion of a pellet shot from a gun.
vector. (a) Do the direction and magnitude of the acceleration vector be- have in the same fashion as the direction and magnitude of the velocity
vector or (b) does the acceleration vector have a constant direction and a constant magnitude throughout the motion?
Reasoning Since air resistance is being ignored, the coin is in free-fall motion. This means that the acceleration vector of the coin is the acceler-
ation due to gravity. Acceleration is the rate at which velocity changes and is not the same concept as velocity itself.
Answer (a) is incorrect. During the upward and downward parts of the motion, and also at the top of the path, the acceleration due to
gravity has a constant downward direction and a constant magnitude
of 9.80 m/s2. In other words, the acceleration vector of the coin does
not behave as the velocity vector does. In particular, the acceleration
vector is not zero at the top of the motional path just because the velo-
city vector is zero there. Acceleration is the rate at which the velocity
is changing, and the velocity is changing at the top even though at one
instant it is zero.
Answer (b) is correct. The acceleration due to gravity has a constant downward direction and a constant magnitude of 9.80 m/s2 at all times
during the motion.
υ
y = +1.04 m
+
υ–
FIGURE 2.15 For a given displacement along the motional path, the upward speed
of the coin is equal to its downward speed,
but the two velocities point in opposite
directions.
(a) (b) (c)
30 m/s
30 m/s
30 m/s
INTERACTIVE FIGURE 2.16 (a) From the edge of a cliff , a pellet is fi red straight
upward from a gun. The pellet’s initial speed
is 30 m/s. (b) The pellet is fi red straight downward with an initial speed of 30 m/s.
(c) In Conceptual Example 14 this drawing plays the central role in reasoning that is
based on symmetry.
CONCEPTUAL EXAMPLE 14 Taking Advantage of Symmetry
Interactive Figure 2.16a shows a pellet that has been fi red straight upward from a gun at the edge of a cliff . The initial speed of the pellet is
30 m/s. It goes up and then falls back down, eventually hitting the ground
beneath the cliff . In Interactive Figure 2.16b the pellet has been fi red straight downward at the same initial speed. In the absence of air resist-
ance, would the pellet in Interactive Figure 2.16b strike the ground with
(a) a smaller speed than, (b) the same speed as, or (c) a greater speed than the pellet in Interactive Figure 2.16a?
Reasoning In the absence of air resistance, the motion is that of free- fall, and the symmetry inherent in free-fall motion off ers an immediate
answer.
2.7 Graphical Analysis of Velocity and Acceleration 45
Check Your Understanding
(The answers are given at the end of the book.) 13. An experimental vehicle slows down and comes to a halt with an acceleration whose magnitude is
9.80 m/s2. After reversing direction in a negligible amount of time, the vehicle speeds up with an
acceleration of 9.80 m/s2. Except for being horizontal, is this motion (a) the same as or (b) diff erent from the motion of a ball that is thrown straight upward, comes to a halt, and falls back to earth? Ignore
air resistance.
14. A ball is thrown straight upward with a velocity v→0 and in a time t reaches the top of its fl ight path, which is a displacement y→ above the launch point. With a launch velocity of 2v→0, what would be the time required to reach the top of its fl ight path and what would be the displacement of the top point
above the launch point? (a) 4t and 2y→ (b) 2t and 4y→ (c) 2t and 2y→ (d) 4t and 4y→ (e) t and 2y→ . 15. Two objects are thrown vertically upward, fi rst one, and then, a bit later, the other. Is it (a) possible or
(b) impossible that both objects reach the same maximum height at the same instant of time? 16. A ball is dropped from rest from the top of a building and strikes the ground with a speed υf. From
ground level, a second ball is thrown straight upward at the same instant that the fi rst ball is dropped.
The initial speed of the second ball is υ0 = υf, the same speed with which the fi rst ball eventually strikes the ground. Ignoring air resistance, decide whether the balls cross paths (a) at half the height of the building, (b) above the halfway point, or (c) below the halfway point.
2.7 Graphical Analysis of Velocity and Acceleration Graphical techniques are helpful in understanding the concepts of velocity and acceleration. Sup-
pose a bicyclist is riding with a constant velocity of υ = +4 m/s. The position x of the bicycle can be plotted along the vertical axis of a graph, while the time t is plotted along the horizontal axis. Since the position of the bike increases by 4 m every second, the graph of x versus t is a straight line. Furthermore, if the bike is assumed to be at x = 0 m when t = 0 s, the straight line passes through the origin, as Figure 2.17 shows. Each point on this line gives the position of the bike at a particular time. For instance, at t = 1 s the position is 4 m, while at t = 3 s the position is 12 m.
In constructing the graph in Figure 2.17, we used the fact that the velocity was +4 m/s. Sup- pose, however, that we were given this graph, but did not have prior knowledge of the velocity.
The velocity could be determined by considering what happens to the bike between the times of
1 and 3 s, for instance. The change in time is ∆t = 2 s. During this time interval, the position of the bike changes from +4 to +12 m, and the change in position is ∆x = +8 m. The ratio ∆x/∆t is called the slope of the straight line.
Slope = ∆x ∆t
= +8 m
2 s = +4 m /s
Notice that the slope is equal to the velocity of the bike. This result is no accident, because ∆x/∆t is the defi nition of average velocity (see Equation 2.2). Thus, for an object moving with a con- stant velocity, the slope of the straight line in a position–time graph gives the velocity. Since the position–time graph is a straight line, any time interval ∆t can be chosen to calculate the velocity. Choosing a diff erent ∆t will yield a diff erent ∆x, but the velocity ∆x/∆t will not change. In the real world, objects rarely move with a constant velocity at all times, as the next example illustrates.
Answers (a) and (c) are incorrect. These answers are incorrect, be- cause they are inconsistent with the symmetry that is discussed next in
connection with the correct answer.
Answer (b) is correct. Interactive Figure 2.16c shows the pellet after it has been fi red upward and has fallen back down to its starting point. Sym-
metry indicates that the speed in Interactive Figure 2.16c is the same as in Interactive Figure 2.16a—namely, 30 m/s, as is also the case when the
pellet has been actually fi red downward. Consequently, whether the pellet is
fi red as in Interactive Figure 2.16a or b, it begins to move downward from the cliff edge at a speed of 30 m/s. In either case, there is the same accel-
eration due to gravity and the same displacement from the cliff edge to the
ground below. Given these conditions, when the pellet reaches the ground,
it has the same speed in both Interactive Figures 2.16a and b.
Related Homework: Problems 47, 54
0 1 2 3 4
P os
it io
n
(m )
x
t = 2 sΔ
x = + 8 m Δ
Time (s)t
+16
+12
+8
+4
0
FIGURE 2.17 Position–time graph for an object moving with a constant velocity of
υ = Δx/Δt = +4 m/s.
46 CHAPTER 2 Kinematics in One Dimension
EXAMPLE 15 A Bicycle Trip
Segment 2 υ = ∆ x ∆ t
= 1200 m − 1200 m
1000 s − 600 s =
0 m
400 s = 0 m/s
Segment 3 υ = ∆ x ∆ t
= 400 m − 800 m
1800 s − 1400 s =
−400 m
400 s = −1 m/s
In the second segment of the journey the velocity is zero, refl ecting the
fact that the bike is stationary. Since the position of the bike does not
change, segment 2 is a horizontal line that has a zero slope. In the third
part of the motion the velocity is negative, because the position of the
bike decreases from x = +800 m to x = +400 m during the 400-s interval shown in the graph. As a result, segment 3 has a negative slope, and the
velocity is negative.
A bicyclist maintains a constant velocity on the outgoing leg of a trip,
zero velocity while stopped, and another constant velocity on the way
back. Interactive Figure 2.18 shows the corresponding position–time graph. Using the time and position intervals indicated in the drawing,
obtain the velocities for each segment of the trip.
Reasoning The average velocity υ is equal to the displacement ∆x di- vided by the elapsed time ∆t, υ = ∆x /∆t. The displacement is the fi nal position minus the initial position, which is a positive number for segment 1
and a negative number for segment 3. Note for segment 2 that ∆x = 0 m, since the bicycle is at rest. The drawing shows values for ∆t and ∆x for each of the three segments.
Solution The average velocities for the three segments are
Segment 1 υ = ∆ x ∆t
= 800 m − 400 m
400 s − 200 s =
+400 m
200 s = +2 m/s
+1200
+800
+400
0 0 200 400 600 800
Time t (s)
1000 1200 1400 1600 1800
Δ t = 400 s
Δ t = 400 s Δ x = 0 m
Δ t = 200 s
Δ x = –400 mΔ x = +400 m
2
3
1
P os
it io
n x
(m )
Positive velocity
Zero velocity Negative velocity
INTERACTIVE FIGURE 2.18 This position–time graph consists of three straight-line segments, each corresponding to a diff erent constant velocity.
If the object is accelerating, its velocity is changing. When the velocity is changing, the
position–time graph is not a straight line, but is a curve, perhaps like that in Figure 2.19. This curve was drawn using Equation 2.8 (x = υ0t +
1
2at 2), assuming an acceleration of a = 0.26 m/s2 and an initial velocity of υ0 = 0 m/s. The velocity at any instant of time can be determined by measuring the slope of the curve at that instant. The slope at any point along the curve is defi ned
to be the slope of the tangent line drawn to the curve at that point. For instance, in Figure 2.19 a tangent line is drawn at t = 20.0 s. To determine the slope of the tangent line, a triangle is con- structed using an arbitrarily chosen time interval of ∆t = 5.0 s. The change in x associated with this time interval can be read from the tangent line as ∆x = +26 m. Therefore,
Slope of tangent line = ∆x ∆t
= +26 m
5.0 s = +5.2 m /s
The slope of the tangent line is the instantaneous velocity, which in this case is υ = +5.2 m/s. This graphical result can be verifi ed by using Equation 2.4 with υ0 = 0 m/s: υ = at = (+0.26 m/s2)(20.0 s) = +5.2 m/s.
Time (s)t
5.0 10.0 15.0 20.0 25.0
Δ t = 5.0 s
Δ x = +26 m
Tangent line80.0
60.0
40.0
20.0
0 0
P os
it io
n x
(m )
FIGURE 2.19 When the velocity is changing, the position–time graph is a
curved line. The slope Δx/Δt of the tangent line drawn to the curve at a given time is
the instantaneous velocity at that time.
Concept Summary 47
Insight into the meaning of acceleration can also be gained with the aid of a graphical rep-
resentation. Consider an object moving with a constant acceleration of a = +6 m/s2. If the object has an initial velocity of υ0 = +5 m/s, its velocity at any time is represented by Equation 2.4 as
υ = υ0 + at = 5 m/s + (6 m/s2)t
This relation is plotted as the velocity–time graph in Figure 2.20. The graph of υ versus t is a straight line that intercepts the vertical axis at υ0 = 5 m/s. The slope of this straight line can be calculated from the data shown in the drawing:
Slope = ∆υ ∆t
= +12 m/s
2 s = +6 m/s2
The ratio ∆υ/∆t is, by defi nition, equal to the average acceleration (Equation 2.4), so the slope of the straight line in a velocity–time graph is the average acceleration.
+36
+24
+12
0 0 1 2 3 4
Ve lo
ci ty
(m /s
) υ
5
= +5 m/s0
= 2 sΔ t
Δ
Time (s)t
= +12 m/s
υ
υ
FIGURE 2.20 A velocity–time graph that applies to an object with an acceleration of
Δυ/Δt = +6 m/s2. The initial velocity is υ0 = +5 m/s when t = 0 s.
EXAMPLE 16 BIO The Average Acceleration of a Sprinter
Figure 2.21 shows the velocity-time graph for a sprinter competing in a 100-m race. At the beginning of the race, usually initiated by the report of
a starter’s pistol, the sprinter accelerates from rest for a period of 4.00 s.
After accelerating, the sprinter runs at constant speed, before slowing
(decelerating) near the end of the race. Use the velocity and time intervals
shown in the graph to determine the sprinter’s average acceleration during
the fi rst 4.00 s of the race.
Reasoning The slope of the line during the fi rst 4-second interval of
the race will be given by ∆υ ∆t
, which is equivalent to the sprinter’s average
acceleration, a = ∆υ ∆t
.
Solution Using the fact that the average acceleration is given by
a = ∆υ ∆t
, we just need to calculate the slope of the velocity-time graph
over the period from 0 to 4.00 s.
a = ∆υ ∆t
= +12.5 m/s − 0
4.00 s − 0 = +3.13 m/s2
FIGURE 2.21 The velocity-time graph for a track and fi eld athlete running a 100-m sprint. At the start of the race, the sprinter accelerates from rest
for 4.00 s and then maintains a constant speed of 12.5 m/s for approxim-
ately four more seconds, before decelerating near the end of the race.
Time t (s)
6
4
2
0
8
10
12
0 1 2 3 4
Ve lo
ci ty
(m /s
) υ
5 6 7 8 9 10
Δt = +4.00 s
= + 12.5 m/sΔυ
Concept Summary 2.1 Displacement Displacement is a vector that points from an object’s initial position to its fi nal position. The magnitude of the displacement is the
shortest distance between the two positions.
2.2 Speed and Velocity The average speed of an object is the distance traveled by the object divided by the time required to cover the distance, as
shown in Equation 2.1.
The average velocity v→ of an object is the object’s displacement ∆x→ divided by the elapsed time ∆t, as shown in Equation 2.2. Average veloc- ity is a vector that has the same direction as the displacement. When the
elapsed time becomes infi nitesimally small, the average velocity becomes
equal to the instantaneous velocity v→, the velocity at an instant of time, as indicated in Equation 2.3.
Average speed = Distance
Elapsed time (2.1)
v→ = ∆x →
∆t (2.2)
v→ = lim ∆t → 0
∆x→
∆t (2.3)
2.3 Acceleration The average acceleration a→ is a vector. It equals the change ∆v→ in the velocity divided by the elapsed time ∆t, the change in the velocity being the fi nal minus the initial velocity; see Equation 2.4. When ∆t becomes infi nitesimally small, the average acceleration becomes equal to the
48 CHAPTER 2 Kinematics in One Dimension
instantaneous acceleration a→, as indicated in Equation 2.5. Acceleration is the rate at which the velocity is changing.
a→ = ∆v →
∆t (2.4)
a→ = lim ∆ t → 0
∆v→ ∆t (2.5)
2.4 Equations of Kinematics for Constant Acceleration/2.5 Applications of the Equations of Kinematics The equations of kinematics apply when an object moves with a constant acceleration along a straight line. These equa-
tions relate the displacement x − x0, the acceleration a, the fi nal velocity υ, the initial velocity υ0, and the elapsed time t − t0. Assuming that x0 = 0 m at t0 = 0 s, the equations of kinematics are as shown in Equations 2.4 and 2.7–2.9.
υ = υ0 + at (2.4) x = 12 (υ0 + υ)t (2.7) x = υ0t +
1
2 at 2 (2.8) υ2 = υ 20 + 2ax (2.9)
2.6 Freely Falling Bodies In free-fall motion, an object experiences neg- ligible air resistance and a constant acceleration due to gravity. All objects at
the same location above the earth have the same acceleration due to gravity.
The acceleration due to gravity is directed toward the center of the earth and
has a magnitude of approximately 9.80 m/s2 near the earth’s surface.
2.7 Graphical Analysis of Velocity and Acceleration The slope of a plot of position versus time for a moving object gives the object’s velocity. The
slope of a plot of velocity versus time gives the object’s acceleration.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 2.1 Displacement 1. What is the diff erence between distance and displacement? (a) Distance is a vector, while displacement is not a vector. (b) Displacement is a vector, while distance is not a vector. (c) There is no diff erence between the two concepts; they may be used interchangeably.
Section 2.2 Speed and Velocity 3. A jogger runs along a straight and level road for a distance of 8.0 km and then runs back to her starting point. The time for this round-trip is 2.0 h. Which one
of the following statements is true? (a) Her average speed is 8.0 km/h, but there is not enough information to determine her average velocity. (b) Her average speed is 8.0 km/h, and her average velocity is 8.0 km/h. (c) Her average speed is 8.0 km/h, and her average velocity is 0 km/h.
Section 2.3 Acceleration 6. The velocity of a train is 80.0 km/h, due west. One and a half hours later its velocity is 65.0 km/h, due west. What is the train’s average acceleration?
(a) 10.0 km/h2, due west (b) 43.3 km/h2, due west (c) 10.0 km/h2, due east (d) 43.3 km/h2, due east (e) 53.3 km/h2, due east.
Section 2.4 Equations of Kinematics for Constant Acceleration 10. In which one of the following situations can the equations of kinematics not be used? (a) When the velocity changes from moment to moment, (b) when the velocity remains constant, (c) when the acceleration changes from moment to moment, (d) when the acceleration remains constant. 13. In a race two horses, Silver Bullet and Shotgun, start from rest and each maintains a constant acceleration. In the same elapsed time Silver Bullet runs
1.20 times farther than Shotgun. According to the equations of kinematics,
which one of the following is true concerning the accelerations of the horses?
(a) aSilver Bullet = 1.44 aShotgun (b) aSilver Bullet = aShotgun (c) aSilver Bullet = 2.40 aShotgun (d) aSilver Bullet = 1.20 aShotgun (e) aSilver Bullet = 0.72 aShotgun
Section 2.6 Freely Falling Bodies 19. A rocket is sitting on the launch pad. The engines ignite, and the rocket begins to rise straight upward, picking up speed as it goes. At about 1000 m
above the ground the engines shut down, but the rocket continues straight
upward, losing speed as it goes. It reaches the top of its fl ight path and then
falls back to earth. Ignoring air resistance, decide which one of the follow-
ing statements is true. (a) All of the rocket’s motion, from the moment the engines ignite until just before the rocket lands, is free-fall. (b) Only part of the rocket’s motion, from just after the engines shut down until just before it
lands, is free-fall. (c) Only the rocket’s motion while the engines are fi ring is free-fall. (d) Only the rocket’s motion from the top of its fl ight path until just before landing is free-fall. (e) Only part of the rocket’s motion, from just after the engines shut down until it reaches the top of its fl ight path, is
free-fall.
22. The top of a cliff is located a distance H above the ground. At a distance H/2 there is a branch that juts out from the side of the cliff , and on this branch a bird’s nest is located. Two children throw stones at the nest with the same
initial speed, one stone straight downward from the top of the cliff and the
other stone straight upward from the ground. In the absence of air resistance,
which stone hits the nest in the least amount of time? (a) There is insuffi cient information for an answer. (b) Both stones hit the nest in the same amount of time. (c) The stone thrown from the ground. (d) The stone thrown from the top of the cliff .
Section 2.7 Graphical Analysis of Velocity and Acceleration 24. The graph accompanying this prob- lem shows a three-part motion. For each
of the three parts, A, B, and C, identify
the direction of the motion. A positive ve-
locity denotes motion to the right. (a) A right, B left, C right (b) A right, B right, C left (c) A right, B left, C left (d) A left, B right, C left (e) A left, B right, C right
Focus on Concepts
Time
Position
A B
C
QUESTION 24
Problems 49
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 2.1 Displacement
Section 2.2 Speed and Velocity 1. E SSM The space shuttle travels at a speed of about 7.6 × 103 m/s. The blink of an astronaut’s eye lasts about 110 ms. How many football fi elds
(length = 91.4 m) does the shuttle cover in the blink of an eye?
2. E GO For each of the three pairs of positions listed in the following table, determine the magnitude and direction (positive or negative) of the
displacement.
Initial position x0 Final position x (a) +2.0 m +6.0 m (b) +6.0 m +2.0 m (c) −3.0 m +7.0 m
3. E SSM Due to continental drift, the North American and European con- tinents are drifting apart at an average speed of about 3 cm per year. At this
speed, how long (in years) will it take for them to drift apart by another 1500 m
(a little less than a mile)?
4. E BIO You step onto a hot beach with your bare feet. A nerve impulse, generated in your foot, travels through your nervous system at an average
speed of 110 m/s. How much time does it take for the impulse, which travels
a distance of 1.8 m, to reach your brain?
5. E GO The data in the following table describe the initial and fi nal pos- itions of a moving car. The elapsed time for each of the three pairs of posi-
tions listed in the table is 0.50 s. Review the concept of average velocity in
Section 2.2 and then determine the average velocity (magnitude and direc-
tion) for each of the three pairs. Note that the algebraic sign of your answers
will convey the direction.
Initial position x0 Final position x (a) +2.0 m +6.0 m (b) +6.0 m +2.0 m (c) −3.0 m +7.0 m
6. E CHALK One afternoon, a couple walks three-fourths of the way around a circular lake, the radius of which is 1.50 km. They start at the west side
of the lake and head due south to begin with. (a) What is the distance they travel? (b) What are the magnitude and direction (relative to due east) of the couple’s displacement?
7. E The three-toed sloth is the slowest-moving land mammal. On the ground, the sloth moves at an average speed of 0.037 m/s, considerably
slower than the giant tortoise, which walks at 0.076 m/s. After 12 minutes of
walking, how much further would the tortoise have gone relative to the sloth?
8. E GO An 18-year-old runner can complete a 10.0-km course with an av- erage speed of 4.39 m/s. A 50-year-old runner can cover the same distance
with an average speed of 4.27 m/s. How much later (in seconds) should the
younger runner start in order to fi nish the course at the same time as the older runner?
9. E A tourist being chased by an angry bear is running in a straight line toward his car at a speed of 4.0 m/s. The car is a distance d away. The bear is 26 m behind the tourist and running at 6.0 m/s. The tourist reaches the car
safely. What is the maximum possible value for d? 10. M V-HINT In reaching her destination, a backpacker walks with an av- erage velocity of 1.34 m/s, due west. This average velocity results because
she hikes for 6.44 km with an average velocity of 2.68 m/s, due west, turns
around, and hikes with an average velocity of 0.447 m/s, due east. How far
east did she walk?
11. M SSM A bicyclist makes a trip that consists of three parts, each in the same direction (due north) along a straight road. During the fi rst part, she
rides for 22 minutes at an average speed of 7.2 m/s. During the second part,
she rides for 36 minutes at an average speed of 5.1 m/s. Finally, during the
third part, she rides for 8.0 minutes at an average speed of 13 m/s. (a) How far has the bicyclist traveled during the entire trip? (b) What is her average velocity for the trip?
12. M V-HINT A car makes a trip due north for three-fourths of the time and due south one-fourth of the time. The average northward velocity has
a magnitude of 27 m/s, and the average southward velocity has a mag-
nitude of 17 m/s. What is the average velocity (magnitude and direction)
for the entire trip?
13. H You are on a train that is traveling at 3.0 m/s along a level straight track. Very near and parallel to the track is a wall that slopes upward at a
12° angle with the horizontal. As you face the window (0.90 m high, 2.0 m
wide) in your compartment, the train is moving to the left, as the drawing
indicates. The top edge of the wall fi rst appears at window corner A and
eventually disappears at window corner B. How much time passes between
appearance and disappearance of the upper edge of the wall?
3.0 m/s
A
12°
BB
A
PROBLEM 13
Section 2.3 Acceleration 14. E Review Conceptual Example 6 as background for this problem. A car is traveling to the left, which is the negative direction. The direction of travel
remains the same throughout this problem. The car’s initial speed is 27.0 m/s,
and during a 5.0-s interval, it changes to a fi nal speed of (a) 29.0 m/s and (b) 23.0 m/s. In each case, fi nd the acceleration (magnitude and algebraic sign) and state whether or not the car is decelerating.
15. E GO (a) Suppose that a NASCAR race car is moving to the right with a constant velocity of +82 m/s. What is the average acceleration of the car?
Problems
50 CHAPTER 2 Kinematics in One Dimension
25. E SSM A jogger accelerates from rest to 3.0 m/s in 2.0 s. A car acceler- ates from 38.0 to 41.0 m/s also in 2.0 s. (a) Find the acceleration (magnitude only) of the jogger. (b) Determine the acceleration (magnitude only) of the car. (c) Does the car travel farther than the jogger during the 2.0 s? If so, how much farther?
26. E GO A VW Beetle goes from 0 to 60.0 mi/h with an acceleration of +2.35 m/s2. (a) How much time does it take for the Beetle to reach this speed? (b) A top-fuel dragster can go from 0 to 60.0 mi/h in 0.600 s. Find the acceleration (in m/s2) of the dragster.
27. E BIO The left ventricle of the heart accelerates blood from rest to a velocity of +26 cm/s. (a) If the displacement of the blood during the accel- eration is +2.0 cm, determine its acceleration (in cm/s2). (b) How much time does blood take to reach its fi nal velocity?
28. E (a) What is the magnitude of the average acceleration of a skier who, starting from rest, reaches a speed of 8.0 m/s when going down a slope for
5.0 s? (b) How far does the skier travel in this time? 29. E SSM A jetliner, traveling northward, is landing with a speed of 69 m/s. Once the jet touches down, it has 750 m of runway in which to reduce its
speed to 6.1 m/s. Compute the average acceleration (magnitude and direc-
tion) of the plane during landing.
30. E V-HINT MMH The Kentucky Derby is held at the Churchill Downs track in Louisville, Kentucky. The track is one and one-quarter miles in
length. One of the most famous horses to win this event was Secretariat. In
1973 he set a Derby record that would be hard to beat. His average accelera-
tion during the last four quarter-miles of the race was +0.0105 m/s2. His ve-
locity at the start of the fi nal mile (x = +1609 m) was about +16.58 m/s. The acceleration, although small, was very important to his victory. To assess its
eff ect, determine the diff erence between the time he would have taken to run
the fi nal mile at a constant velocity of +16.58 m/s and the time he actually
took. Although the track is oval in shape, assume it is straight for the purpose
of this problem.
31. E SSM MMH A cart is driven by a large propeller or fan, which can accelerate or decelerate the cart. The cart starts out at the position x = 0 m, with an initial velocity of +5.0 m/s and a constant acceleration due to the fan.
The direction to the right is positive. The cart reaches a maximum position
of x = +12.5 m, where it begins to travel in the negative direction. Find the acceleration of the cart.
32. E MMH Two rockets are fl ying in the same direction and are side by side at the instant their retrorockets fi re. Rocket A has an initial velocity
of +5800 m/s, while rocket B has an initial velocity of +8600 m/s. After a
time t both rockets are again side by side, the displacement of each being zero. The acceleration of rocket A is −15 m/s2. What is the acceleration of
rocket B?
33. M CHALK MMH A car is traveling at 20.0 m/s, and the driver sees a traffi c light turn red. After 0.530 s (the reaction time), the driver applies the brakes,
and the car decelerates at 7.00 m/s2. What is the stopping distance of the car,
as measured from the point where the driver fi rst sees the red light?
34. M GO MMH A race driver has made a pit stop to refuel. After refuel- ing, he starts from rest and leaves the pit area with an acceleration whose
magnitude is 6.0 m/s2; after 4.0 s he enters the main speedway. At the same
instant, another car on the speedway and traveling at a constant velocity of
70.0 m/s overtakes and passes the entering car. The entering car maintains
its acceleration. How much time is required for the entering car to catch the
other car?
35. M V-HINT In a historical movie, two knights on horseback start from rest 88.0 m apart and ride directly toward each other to do battle. Sir George’s
acceleration has a magnitude of 0.300 m/s2, while Sir Alfred’s has a mag-
nitude of 0.200 m/s2. Relative to Sir George’s starting point, where do the
knights collide?
(b) Twelve seconds later, the car is halfway around the track and traveling in the opposite direction with the same speed. What is the average acceleration
of the car?
16. E Over a time interval of 2.16 years, the velocity of a planet orbiting a distant star reverses direction, changing from +20.9 km/s to −18.5 km/s.
Find (a) the total change in the planet’s velocity (in m/s) and (b) its aver- age acceleration (in m/s2) during this interval. Include the correct algebraic
sign with your answers to convey the directions of the velocity and the
acceleration.
17. E SSM A motorcycle has a constant acceleration of 2.5 m/s2. Both the velocity and acceleration of the motorcycle point in the same direction. How
much time is required for the motorcycle to change its speed from (a) 21 to 31 m/s, and (b) 51 to 61 m/s? 18. E A sprinter explodes out of the starting block with an acceleration of +2.3 m/s2, which she sustains for 1.2 s. Then, her acceleration drops to zero
for the rest of the race. What is her velocity (a) at t = 1.2 s and (b) at the end of the race?
19. E GO The initial velocity and acceleration of four moving objects at a given instant in time are given in the following table. Determine the fi nal speed of each of the objects, assuming that the time elapsed since t = 0 s is 2.0 s.
Initial velocity υ0 Acceleration a (a) +12 m/s +3.0 m/s2
(b) +12 m/s −3.0 m/s2
(c) −12 m/s +3.0 m/s2
(d) −12 m/s −3.0 m/s2
20. E GO An Australian emu is running due north in a straight line at a speed of 13.0 m/s and slows down to a speed of 10.6 m/s in 4.0 s. (a) What is the direction of the bird’s acceleration? (b) Assuming that the accelera- tion remains the same, what is the bird’s velocity after an additional 2.0 s
has elapsed?
21. E SSM For a standard production car, the highest road-tested acceler- ation ever reported occurred in 1993, when a Ford RS200 Evolution went
from zero to 26.8 m/s (60 mi/h) in 3.275 s. Find the magnitude of the car’s
acceleration.
22. M MMH A car is traveling along a straight road at a velocity of +36.0 m/s when its engine cuts out. For the next twelve seconds the car slows down,
and its average acceleration is a1. For the next six seconds the car slows down further, and its average acceleration is a2. The velocity of the car at the end of the eighteen-second period is +28.0 m/s. The ratio of the average accel-
eration values is a1 / a2 = 1.50. Find the velocity of the car at the end of the initial twelve-second interval.
23. H Two motorcycles are traveling due east with diff erent velocities. However, four seconds later, they have the same velocity. During this four-
second interval, cycle A has an average acceleration of 2.0 m/s2 due east,
while cycle B has an average acceleration of 4.0 m/s2 due east. By how much
did the speeds diff er at the beginning of the four-second interval, and which motorcycle was moving faster?
Section 2.4 Equations of Kinematics for Constant Acceleration/Section 2.5 Applications of the Equations of Kinematics 24. E In getting ready to slam-dunk the ball, a basketball player starts from rest and sprints to a speed of 6.0 m/s in 1.5 s. Assuming that the player accel-
erates uniformly, determine the distance he runs.
Problems 51
46. E GO MMH A ball is thrown vertically upward, which is the posit- ive direction. A little later it returns to its point of release. The ball is in
the air for a total time of 8.0 s. What is its initial velocity? Neglect air
resistance.
47. E Review Conceptual Example 14 before attempting this problem. Two identical pellet guns are fi red simultaneously from the edge of a cliff . These
guns impart an initial speed of 30.0 m/s to each pellet. Gun A is fi red straight
upward, with the pellet going up and then falling back down, eventually hit-
ting the ground beneath the cliff . Gun B is fi red straight downward. In the
absence of air resistance, how long after pellet B hits the ground does pellet
A hit the ground?
48. E MMH An astronaut on a distant planet wants to determine its acceler- ation due to gravity. The astronaut throws a rock straight up with a velocity of
+15 m/s and measures a time of 20.0 s before the rock returns to his hand.
What is the acceleration (magnitude and direction) due to gravity on this
planet?
49. E SSM A hot-air balloon is rising upward with a constant speed of 2.50 m/s. When the balloon is 3.00 m above the ground, the balloonist
accidentally drops a compass over the side of the balloon. How much time
elapses before the compass hits the ground?
50. E GO A ball is thrown straight upward and rises to a maximum height of 16 m above its launch point. At what height above its launch point has the
speed of the ball decreased to one-half of its initial value?
51. E A diver springs upward with an initial speed of 1.8 m/s from a 3.0-m board. (a) Find the velocity with which he strikes the water. [Hint: When the diver reaches the water, his displacement is y = −3.0 m (measured from the board), assuming that the downward direction is chosen as the negative direction.] (b) What is the highest point he reaches above the water?
52. E GO A ball is thrown straight upward. At 4.00 m above its launch point, the ball’s speed is one-half its launch speed. What maximum height
above its launch point does the ball attain?
53. E SSM From her bedroom window a girl drops a water-fi lled balloon to the ground, 6.0 m below. If the balloon is released from rest, how long is
it in the air?
54. E Before working this problem, review Conceptual Example 14. A pellet gun is fi red straight downward from the edge of a cliff that is 15 m above
the ground. The pellet strikes the ground with a speed of 27 m/s. How far
above the cliff edge would the pellet have gone had the gun been fi red straight
upward?
55. E V-HINT Consult Multiple-Concept Example 5 in preparation for this problem. The velocity of a diver just before hitting the water is −10.1 m/s,
where the minus sign indicates that her motion is directly downward. What is
her displacement during the last 1.20 s of the dive?
56. M V-HINT A golf ball is dropped from rest from a height of 9.50 m. It hits the pavement, then bounces back up, rising just 5.70 m before falling back
down again. A boy then catches the ball on the way down when it is 1.20 m
above the pavement. Ignoring air resistance, calculate the total amount of
time that the ball is in the air, from drop to catch.
57. M MMH A woman on a bridge 75.0 m high sees a raft fl oating at a constant speed on the river below. Trying to hit the raft, she drops a stone
from rest when the raft has 7.00 m more to travel before passing under the
bridge. The stone hits the water 4.00 m in front of the raft. Find the speed
of the raft.
58. M GO Two stones are thrown simultaneously, one straight upward from the base of a cliff and the other straight downward from the top of the cliff .
The height of the cliff is 6.00 m. The stones are thrown with the same speed
36. M GO Two soccer players start from rest, 48 m apart. They run directly toward each other, both players accelerating. The fi rst player’s
acceleration has a magnitude of 0.50 m/s2. The second player’s accelera-
tion has a magnitude of 0.30 m/s2. (a) How much time passes before the players collide? (b) At the instant they collide, how far has the fi rst player run?
37. M MMH A car is traveling at a constant speed of 33 m/s on a highway. At the instant this car passes an entrance ramp, a second car enters the highway
from the ramp. The second car starts from rest and has a constant accelera-
tion. What acceleration must it maintain, so that the two cars meet for the fi rst
time at the next exit, which is 2.5 km away?
38. M Available on WileyPLUS. 39. M GO Refer to Multiple-Concept Example 5 to review a method by which this problem can be solved. You are driving your car, and the traffi c
light ahead turns red. You apply the brakes for 3.00 s, and the velocity of
the car decreases to +4.50 m/s. The car’s deceleration has a magnitude of
2.70 m/s2 during this time. What is the car’s displacement?
40. H A Boeing 747 “Jumbo Jet” has a length of 59.7 m. The runway on which the plane lands intersects another runway. The width of the intersec-
tion is 25.0 m. The plane decelerates through the intersection at a rate of
5.70 m/s2 and clears it with a fi nal speed of 45.0 m/s. How much time is
needed for the plane to clear the intersection?
41. H SSM A locomotive is accelerating at 1.6 m/s2. It passes through a 20.0-m-wide crossing in a time of 2.4 s. After the locomotive leaves the
crossing, how much time is required until its speed reaches 32 m/s?
42. H Available on WileyPLUS.
Section 2.6 Freely Falling Bodies 43. E SSM The greatest height reported for a jump into an airbag is 99.4 m by stuntman Dan Koko. In 1948 he jumped from rest from the top of the
Vegas World Hotel and Casino. He struck the airbag at a speed of 39 m/s
(88 mi/h). To assess the eff ects of air resistance, determine how fast he would
have been traveling on impact had air resistance been absent.
44. E A dynamite blast at a quarry launches a chunk of rock straight up- ward, and 2.0 s later it is rising at a speed of 15 m/s. Assuming air resistance
has no eff ect on the rock, calculate its speed (a) at launch and (b) 5.0 s after launch.
45. E BIO The drawing shows a device that you can make with a piece of cardboard, which can be used to measure a person’s reaction time. Hold
the card at the top and suddenly drop it. Ask a friend to try to catch the card
between his or her thumb and index fi nger. Initially, your friend’s fi ngers
must be level with the asterisks at the bottom. By noting where your friend
catches the card, you can determine his or her reaction time in milliseconds
(ms). Calculate the distances d1, d2, and d3.
PROBLEM 45
HOLD HERE
180 ms
120 ms
60.0 ms
d3
d1 d2
∗ ∗ ∗ ∗ ∗ ∗ ∗
52 CHAPTER 2 Kinematics in One Dimension
+100
+80
+60
+40
+20
0 0
Ve lo
ci ty
(m
/s )
υ
A
B
C
Time (s)t
10 20 30 40 50 60
PROBLEM 67
68. E A bus makes a trip according to the position–time graph shown in the drawing. What is the average velocity (magnitude and direction) of
the bus during each of the segments A, B, and C? Express your answers in km/h.
+50.0
+40.0
+30.0
+20.0
+10.0
0 0 0.5 1.0 1.5
Time t (h)
2.0 2.5 3.0
P os
it io
n x
(k m
)
A
B
C
PROBLEM 68
69. M GO A bus makes a trip according to the position–time graph shown in the illustration. What is the average acceleration (in km/h2) of the bus for
the entire 3.5-h period shown in the graph?
+40.0
+30.0
+20.0
+10.0
0 0
P os
it io
n
(k m
) x
0.5 1.0 1.5 2.0 2.5 3.0 3.5
A
B C
Time (h)t
PROBLEM 69
70. M A runner is at the position x = 0 m when time t = 0 s. One hundred meters away is the fi nish line. Every ten seconds, this runner runs half the re-
maining distance to the fi nish line. During each ten-second segment, the run-
ner has a constant velocity. For the fi rst forty seconds of the motion, construct
(a) the position–time graph and (b) the velocity–time graph. 71. H SSM Available on WileyPLUS.
of 9.00 m/s. Find the location (above the base of the cliff ) of the point where
the stones cross paths.
59. M SSM Available on WileyPLUS. 60. M GO Two arrows are shot vertically upward. The second arrow is shot after the fi rst one, but while the fi rst is still on its way up. The initial
speeds are such that both arrows reach their maximum heights at the same
instant, although these heights are diff erent. Suppose that the initial speed
of the fi rst arrow is 25.0 m/s and that the second arrow is fi red 1.20 s after
the fi rst. Determine the initial speed of the second arrow.
61. M CHALK SSM A cement block accidentally falls from rest from the ledge of a 53.0-m-high building. When the block is 14.0 m above the
ground, a man, 2.00 m tall, looks up and notices that the block is directly
above him. How much time, at most, does the man have to get out of the
way?
62. M V-HINT A model rocket blasts off from the ground, rising straight upward with a constant acceleration that has a magnitude of 86.0 m/s2 for
1.70 seconds, at which point its fuel abruptly runs out. Air resistance has
no eff ect on its fl ight. What maximum altitude (above the ground) will the
rocket reach?
63. H While standing on a bridge 15.0 m above the ground, you drop a stone from rest. When the stone has fallen 3.20 m, you throw a second stone
straight down. What initial velocity must you give the second stone if they
are both to reach the ground at the same instant? Take the downward direc-
tion to be the negative direction.
64. H Available on WileyPLUS.
Section 2.7 Graphical Analysis of Velocity and Acceleration 65. E SSM A person who walks for exercise produces the position–time graph given with this problem. (a) Without doing any calculations, decide which segments of the graph (A, B, C, or D) indicate positive, negative, and zero average velocities. (b) Calculate the average velocity for each segment to verify your answers to part (a).
+1.25
+1.00
+0.75
+0.50
+0.25
0 0
P os
it io
n
( km
) x
A B
C
Time (h)t 0.20 0.40 0.60 0.80 1.00
D
PROBLEM 65
66. E Starting at x = −16 m at time t = 0 s, an object takes 18 s to travel 48 m in the +x direction at a constant velocity. Make a position–time graph of the object’s motion and calculate its velocity.
67. E MMH A snowmobile moves according to the velocity–time graph shown in the drawing. What is the snowmobile’s average acceleration during
each of the segments A, B, and C?
Additional Problems 53
72. E GO The data in the following table represent the initial and fi nal ve- locities for a boat traveling along the x axis. The elapsed time for each of the four pairs of velocities in the table is 2.0 s. Review the concept of aver-
age acceleration in Section 2.3 and then determine the average acceleration
(magnitude and direction) for each of the four pairs. Note that the algebraic
sign of your answers will convey the direction.
Initial velocity υ0 Final velocity υ (a) +2.0 m/s +5.0 m/s
(b) +5.0 m/s +2.0 m/s
(c) −6.0 m/s −3.0 m/s
(d) +4.0 m/s −4.0 m/s
73. E SSM Available on WileyPLUS.
74. E In 1954 the English runner Roger Bannister broke the four-minute barrier for the mile with a time of 3:59.4 s (3 min and 59.4 s). In 1999 the
Moroccan runner Hicham el-Guerrouj set a record of 3:43.13 s for the mile.
If these two runners had run in the same race, each running the entire race at
the average speed that earned him a place in the record books, el-Guerrouj
would have won. By how many meters?
75. E SSM Available on WileyPLUS.
76. E MMH At the beginning of a basketball game, a referee tosses the ball straight up with a speed of 4.6 m/s. A player cannot touch the ball until after
it reaches its maximum height and begins to fall down. What is the minimum
time that a player must wait before touching the ball?
77. E Electrons move through a certain electric circuit at an average speed of 1.1 × 10−2 m/s. How long (in minutes) does it take an electron to traverse
1.5 m of wire in the fi lament of a light bulb?
78. E Available on WileyPLUS.
79. E V-HINT MMH A cheetah is hunting. Its prey runs for 3.0 s at a constant velocity of +9.0 m/s. Starting from rest, what constant acceleration must
the cheetah maintain in order to run the same distance as its prey runs in the
same time?
80. M Available on WileyPLUS. 81. M SSM Available on WileyPLUS. 82. M GO The leader of a bicycle race is traveling with a constant velocity of +11.10 m/s and is 10.0 m ahead of the second-place cyclist. The second-
place cyclist has a velocity of +9.50 m/s and an acceleration of +1.20 m/s2.
How much time elapses before he catches the leader?
83. M V-HINT A golfer rides in a golf cart at an average speed of 3.10 m/s for 28.0 s. She then gets out of the cart and starts walking at an average speed of
1.30 m/s. For how long (in seconds) must she walk if her average speed for
the entire trip, riding and walking, is 1.80 m/s?
84. M GO Two cars cover the same distance in a straight line. Car A covers the distance at a constant velocity. Car B starts from rest and main-
tains a constant acceleration. Both cars cover a distance of 460 m in 210 s.
Assume that they are moving in the +x direction. Determine (a) the constant velocity of car A, (b) the fi nal velocity of car B, and (c) the acceleration of car B.
85. M V-HINT MMH A police car is traveling at a velocity of 18.0 m/s due north, when a car zooms by at a constant velocity of 42.0 m/s due north. After
a reaction time of 0.800 s the policeman begins to pursue the speeder with an
acceleration of 5.00 m/s2. Including the reaction time, how long does it take
for the police car to catch up with the speeder?
86. H MMH Available on WileyPLUS. 87. H SSM Available on WileyPLUS. 88. H Available on WileyPLUS. 89. M GO SSM A jet is taking off from the deck of an aircraft carrier, as shown in the image. Starting from rest, the jet is catapulted with a constant
acceleration of +31 m/s2 along a straight line and reaches a velocity of +62 m/s.
Find the displacement of the jet.
Additional Problems
0 = 0 m/sυ = + 62 m/sυa = + 31 m/s 2
– +
(b)
x
(a) A jet is being launched from an aircraft carrier. (b) During the launch, a catapult accelerates the jet down the fl ight deck.
(a)
M ar
k u s
S ch
re ib
er /A
P /W
id e
W o rl
d
P h o to
s
PROBLEM 89
54 CHAPTER 2 Kinematics in One Dimension
92. M A Deadly Virus. On your fl ight out of South America your cargo plane emergency-lands on a deserted island somewhere in the South Pacifi c.
Because it was a beach landing, the pilot skids the plane on its belly rather
than lowering the landing gear. The landing is rough: an initial vertical drop
followed by an abrupt horizontal deceleration. When the dust settles, the pi-
lot and your scientist colleagues are all okay, but you know there might be
a big problem. Your team is transporting samples of a deadly virus from a
recent breakout in a small village. The samples were packed in a cryogen-
ically cooled container that has a special seal that may leak if it exceeds
an acceleration greater than 10 g. The container has a mechanical acceler-
ometer gauge that measures the maximum vertical deceleration in case the
container is dropped. It reads a value of a = 7.30 g. However, you are still worried: there was another component of the acceleration. You get out of
the plane and measure the length of the skid the plane made in the sand as
it landed: 154 ft. The pilot claims the plane’s horizontal speed on impact
was 160 m.p.h. Assuming the worst case scenario (i.e., that the vertical and
horizontal accelerations occurred simultaneously), and that the horizontal
deceleration was uniform, is it likely that the seal on the virus container is
compromised? Explain.
93. M The Lost Drone. You and your team are exploring the edge of an Ant- arctic mountain range and you send a drone ahead to help navigate. After takeoff
you lose sight of the drone and, a few seconds later, the controls malfunction and
the drone stops sending visual images and navigational information except for
speed and directional data. Changing speeds erratically, the drone heads west
until it makes a drastic turn at the 5-minute mark to 35.0° east of south. After
nearly ten minutes, the speed
drops to zero and the drone
stops sending data. It has
crashed. Using the speed/
directional data, the team
draws up the graph shown in
the drawing.. How far is the
drone from you, and in what
direction must you go to re-
trieve it? Express your result
as a geographical direction
(i.e., in the form 30° north of
east, etc.).
In this chapter we have studied the displacement, velocity, and acceleration
vectors. The concept questions are designed to review some of the important
concepts that can help in anticipating some of the characteristics of the nu-
merical answers.
90. M CHALK A skydiver is falling straight down, along the negative y dir- ection. (a) During the initial part of the fall, her speed increases from 16 to 28 m/s in 1.5 s, as in part a of the fi gure. (b) Later, her parachute opens, and her speed decreases from 48 to 26 m/s in 11 s, as in part b of the draw- ing. Concepts: (i) Is her average acceleration positive or negative when her speed is increasing in part a of the fi gure? (ii) Is her average acceleration positive or negative when her speed is decreasing in part b of the fi gure? Calculations: In both instances (parts a and b of the fi gure) determine the magnitude and direction of her average acceleration.
91. M CHALK SSM A top-fuel dragster starts from rest and has a constant acceleration of 40.0 m/s2. Concepts: (i) At time t the dragster has a certain velocity. Keeping in mind that the dragster starts from rest, when the time
doubles to 2t, does the velocity also double? (ii) When the time doubles to 2t, does the displacement of the dragster also double? Calculations: What are the (a) fi nal velocities and (b) displacements of the dragster at the end of 2.0 s and at the end of twice this time, or 4.0 s?
Team Problems
Concepts and Calculations Problems
(b)
0υ
υ
–
+
(a)
0υ
υ
–
+
PROBLEM 90
200
WEST
Time t (s)
15
10
5
0
20
0 100 300 400
Ve lo
ci ty
(m /s
) υ
500 600
35º East of South
PROBLEM 93
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
3.1 Define two-dimensional kinematic variables.
3.2 Use two-dimensional kinematic equations to predict future or past values of variables.
3.3 Analyze projectile motion to predict future or past values of variables.
3.4 Apply relative velocity equations.
© t
h re
es p ee
d jo
n es
/i S
to ck
p h o to
CHAPTER 3
Kinematics in Two Dimensions
The beautiful water fountain at the World War II Memorial in Washington, D.C., is illuminated at night.
The arching streams of water follow parabolic paths whose sizes depend on the launch velocity of the
water and the acceleration due to gravity, assuming that the eff ects of air resistance are negligible.
3.1 Displacement, Velocity, and Acceleration In Chapter 2 the concepts of displacement, velocity, and acceleration are used to
describe an object moving in one dimension. There are also situations in which the
motion is along a curved path that lies in a plane. Such two-dimensional motion can
be described using the same concepts. In Grand Prix racing, for example, the course
follows a curved road, and Figure 3.1 shows a race car at two diff erent positions along it. These positions are identifi ed by the vectors r→ and r→0, which are drawn from an arbitrary coordinate origin. The displacement Δr→ of the car is the vector drawn from the initial position r→0 at time t0 to the fi nal position r→ at time t. The magnitude of Δr→ is the shortest distance between the two positions. In the drawing, the vectors r→0 and Δr→ are drawn tail to head, so it is evident that r→ is the vector sum of r→0 and Δr→. (See Sections 1.5 and 1.6 for a review of vectors and vector addition.) This means that
r→ = r→0 + Δr→, or Displacement = Δr→ = r→ − r→0 The displacement here is defi ned as it is in Chapter 2. Now, however, the displacement
vector may lie anywhere in a plane, rather than just along a straight line. 55
56 CHAPTER 3 Kinematics in Two Dimensions
The average velocity v→ of the car in Figure 3.1 between the two positions is defi ned in a manner similar to that in Equation 2.2, as the displacement Δr→ = r→ − r→0 divided by the elapsed time Δt = t − t0:
v→ = r→ − r→0 t − t0
= ∆r→
∆t (3.1)
Since both sides of Equation 3.1 must agree in direction, the average velocity vector has the same
direction as the displacement Δr→. The velocity of the car at an instant of time is its instanta- neous velocity v→. The average velocity becomes equal to the instantaneous velocity v→ in the limit that Δt becomes infi nitesimally small (Δt → 0 s):
v→ = lim ∆ t → 0
∆ r→
∆ t
Figure 3.2 illustrates that the instantaneous velocity v→ is tangent to the path of the car. The draw- ing also shows the vector components v →x and v →y of the velocity, which are parallel to the x and y axes, respectively.
The average acceleration a→ is defi ned just as it is for one-dimensional motion—namely, as the change in velocity, Δv→ = v→ − v →0, divided by the elapsed time Δt:
a→ = v→ − v→0 t − t0
= ∆v→
∆ t (3.2)
The average acceleration has the same direction as the change in velocity Δv→. In the limit that the elapsed time becomes infi nitesimally small, the average acceleration becomes equal to the
instantaneous acceleration a→:
→a = lim ∆t → 0
v→
∆t
The acceleration has a vector component a→x along the x direction and a vector component a→y along the y direction.
Check Your Understanding
(The answer is given at the end of the book.) 1. Suppose you are driving due east, traveling a distance of 1500 m in 2 minutes. You then turn due north
and travel the same distance in the same time. What can be said about the average speeds and the aver-
age velocities for the two segments of the trip? (a) The average speeds are the same, and the average velocities are the same. (b) The average speeds are the same, but the average velocities are diff erent. (c) The average speeds are diff erent, but the average velocities are the same.
3.2 Equations of Kinematics in Two Dimensions To understand how displacement, velocity, and acceleration are applied to two-dimensional
motion, consider a spacecraft equipped with two engines that are mounted perpendicular to each
other. These engines produce the only forces that the craft experiences, and the spacecraft is
assumed to be at the coordinate origin when t0 = 0 s, so that r→0 = 0 m. At a later time t, the space- craft’s displacement is Δr→ = r→ − r→0 = r→. Relative to the x and y axes, the displacement r→ has vector components of x→ and y→, respectively.
In Figure 3.3 only the engine oriented along the x direction is fi ring, and the vehicle accelerates along this direction. It is assumed that the velocity in the y direction is zero, and it remains zero, since the y engine is turned off . The motion of the spacecraft along the x direction is described by the fi ve kinematic variables x, ax, υx, υ0x, and t. Here the symbol “x” reminds us
+y
+x
r0
r
Δr
t0
t
FIGURE 3.1 The displacement Δr→ of the car is a vector that points from the initial
position of the car at time t0 to the fi nal position at time t. The magnitude of Δr→ is the shortest distance between the two
positions.
+y
+x
vy
vx
θ
v
FIGURE 3.2 The instantaneous velocity v→ and its two vector components v→x and v→y.
3.2 Equations of Kinematics in Two Dimensions 57
that we are dealing with the x components of the displacement, velocity, and acceleration vectors. (See Sections 1.7 and 1.8 for a review of vector components.) The variables x, ax, υx, and υ0x are scalar components (or “components,” for short). As Section 1.7 discusses, these components are
positive or negative numbers (with units), depending on whether the associated vector compo-
nents point in the +x or the −x direction. If the spacecraft has a constant acceleration along the x direction, the motion is exactly like that described in Chapter 2, and the equations of kinematics
can be used. For convenience, these equations are written in the left column of Table 3.1. Figure 3.4 is analogous to Figure 3.3, except that now only the y engine is fi ring, and
the spacecraft accelerates along the y direction. Such a motion can be described in terms of the kinematic variables y, ay, υy, υ0y, and t. And if the acceleration along the y direction is constant, these variables are related by the equations of kinematics, as written in the right
column of Table 3.1. Like their counterparts in the x direction, the scalar components, y, ay, υy, and υ0y, may be positive (+) or negative (−) numbers (with units).
If both engines of the spacecraft are fi ring at the same time, the resulting motion takes place in part along the x axis and in part along the y axis, as Interactive Figure 3.5 illus- trates. The thrust of each engine gives the vehicle a corresponding acceleration component.
The x engine accelerates the craft in the x direction and causes a change in the x component of the velocity. Likewise, the y engine causes a change in the y component of the velocity.
Problem-Solving Insight It is important to realize that the x part of the motion occurs exactly as it would if the y part did not occur at all. Similarly, the y part of the motion occurs exactly as it would if the x part of the motion did not exist.
In other words, the x and y motions are independent of each other. The independence of the x and y motions lies at the heart of two-dimensional kinematics. It
allows us to treat two-dimensional motion as two distinct one-dimensional motions, one for the x direction and one for the y direction. Everything that we have learned in Chapter 2 about kinemat- ics in one dimension will now be applied separately to each of the two directions. In so doing, we
will be able to describe the x and y variables separately and then bring these descriptions together to understand the two-dimensional picture. Examples 1 and 2 take this approach in dealing with
a moving spacecraft.
+y
ax
+x
x
υ 0x υ x x
y
x
y FIGURE 3.3 The spacecraft is moving with a constant
acceleration ax parallel to the x axis. There is no motion in the y direction, and the y engine is turned off .
TABLE 3.1 Equations of Kinematics for Constant Acceleration in Two-Dimensional Motion
x Component Variable y Component x Displacement y
ax Acceleration ay
υx Final velocity υy
υ0x Initial velocity υ0y
t Elapsed time t
υx = υ0x + axt (3.3a) υy = υ0y + ayt (3.3b)
x = 12 (υ0x + υx) t (3.4a) y = 1
2(υ0y + υy)t (3.4b)
x = υ0 xt + 1
2 ax t2 (3.5a) y = υ0y t + 1
2 ay t 2 (3.5b)
υx 2 = υ0x2 + 2ax x (3.6a) υy 2 = υ 20y + 2ay y (3.6b)
ay
+x
y
+y
υ 0y
υ y
x
y
y
x
FIGURE 3.4 The spacecraft is moving with a constant acceleration ay parallel to the y axis. There is no motion in the x direction, and the x engine is turned off .
58 CHAPTER 3 Kinematics in Two Dimensions
+y
υ 0x +x
υ 0y
υ y
υ x
y x
y x
INTERACTIVE FIGURE 3.5 The two-dimensional motion of the spacecraft can be viewed as the combination of the
separate x and y motions.
EXAMPLE 1 The Displacement of a Spacecraft
In Interactive Figure 3.5, the directions to the right and upward are the positive directions. In the x direction, the spacecraft has an initial veloc- ity component of υ0x = +22 m/s and an acceleration component of ax = +24 m/s2. In the y direction, the analogous quantities are υ0y = +14 m/s and ay = +12 m/s2. At a time of t = 7.0 s, fi nd the x and y components of the spacecraft’s displacement.
Reasoning The motion in the x direction and the motion in the y direc- tion can be treated separately, each as a one-dimensional motion subject
to the equations of kinematics for constant acceleration (see Table 3.1). By following this procedure we will be able to determine x and y, which specify the spacecraft’s location after an elapsed time of 7.0 s.
Problem-Solving Insight When the motion is two- dimensional, the time variable t has the same value for both the x and y directions.
Solution The data for the motion in the x direction are listed in the fol- lowing table:
x-Direction Data x ax υx υ0x t ? +24 m/s2 +22 m/s 7.0 s
The x component of the craft’s displacement can be found by using Equation 3.5a:
x = υ0x t + 1
2 ax t 2 = (22 m /s)(7.0 s) + 1
2 (24 m /s 2) (7.0 s)2 = +740 m
The data for the motion in the y direction are listed in the following table:
y-Direction Data y ay υy υ0y t ? +12 m/s2 +14 m/s 7.0 s
The y component of the craft’s displacement can be found by using Equation 3.5b:
y = υ0yt + 1
2ayt 2 = (14 m/s)(7.0 s) + 1
2 (12 m/s 2)(7.0 s)2 = +390 m
After 7.0 s, the spacecraft is 740 m to the right and 390 m above the origin.
Analyzing Multiple-Concept Problems
EXAMPLE 2 The Velocity of a Spacecraft
This example also deals with the spacecraft in Interactive Fig ure 3.5. As in Example 1, the x components of the craft’s initial velocity and acceleration are υ0x = +22 m/s and ax = +24 m/s2, respectively. The corresponding y components are υ0y = +14 m/s and ay = +12 m/s2. At a time of t = 7.0 s, fi nd the spacecraft’s fi nal velocity (magnitude and direction).
Reasoning Figure 3.6 shows the fi nal velocity vector, which has com- ponents υx and υy and a magnitude υ. The fi nal velocity is directed at an angle θ above the +x axis. The vector and its components form a right triangle, the hypotenuse being the magnitude of the velocity and the
components being the other two sides. Thus, we can use the Pythagorean
theorem to determine the magnitude υ from values for the components υx and υy. We can also use trigonometry to determine the directional angle θ.
+y
υ x
υ y
+x
y
x
υ
θ
FIGURE 3.6 The velocity vector has components υx and υy and a magnitude υ. The magnitude gives the speed of the spacecraft, and the
angle θ gives the direction of travel relative to the positive x direction.
3.2 Equations of Kinematics in Two Dimensions 59
Knowns and Unknowns The data for this problem are listed in the table that follows:
Description Symbol Value Comment x component of acceleration ax +24 m/s2
x component of initial velocity υ0x +22 m/s
y component of acceleration ay +12 m/s2
y component of initial velocity υ0y +14 m/s
Time t 7.0 s Same time for x and y directions
Unknown Variables Magnitude of final velocity υ ?
Direction of final velocity θ ?
Modeling the Problem
STEP 1 Final Velocity In Figure 3.6 the fi nal velocity vector and its components υx and υy form a right triangle. Applying the Pythagorean theorem to this right triangle shows that the
magnitude υ of the fi nal velocity is given in terms of the components by Equation 1a at the right. From the right triangle in Figure 3.6 it also follows that the directional angle θ is given by Equa- tion 1b at the right.
STEP 2 The Components of the Final Velocity Values are given for the kinematic variables ax, υ0x, and t in the x direction and for the corresponding variables in the y direction (see the table of knowns and unknowns). For each direction, then, these values allow us to calculate the fi nal
velocity components υx and υy by using Equations 3.3a and 3.3b from the equations of kinematics.
υx = υ0x + axt (3.3a)
υy = υ0y + ayt (3.3b)
These expressions can be substituted into Equations 1a and 1b for the magnitude and direction of
the fi nal velocity, as shown at the right.
Solution Algebraically combining the results of each step, we fi nd that
υ = √υx2 + υy2 = √(υ0x + ax t)2 + (υ0y + ay t)2
θ = tan−1( υy υx) = tan−1(
υ0y + ay t υ0x + ax t)
With the data given for the kinematic variables in the x and y directions, we fi nd that the magnitude and direction of the fi nal velocity of the spacecraft are
υ = √(υ0x + ax t)2 + (υ0y + ay t)2
= √[(22 m /s) + (24 m /s2)(7.0 s)]2 + [(14 m/s) + (12 m/s2)(7.0 s)]2 = 210 m/s
θ = tan−1 ( υ0y + ay t υ0x + ax t) = tan−1[
(14 m/s) + (12 m/s2) (7.0 s)
(22 m/s) + (24 m/s2) (7.0 s)]= 27° After 7.0 s, the spacecraft, at the position determined in Example 1, has a velocity of 210 m/s in
a direction of 27° above the positive x axis.
Related Homework: Problem 66
STEP 1 STEP 2
STEP 1 STEP 2
υ = √υx2 + υy2 (1a)
θ = tan−1 ( υy υx) (1b)
υ = √υx2 + υy2 (1a)
υx = υ0x + axt
υy = υ0y + ayt
(3.3a,b)
θ = tan−1 ( υy υx) (1b)
υx = υ0x + axt
υy = υ0y + ayt
(3.3a,b)
60 CHAPTER 3 Kinematics in Two Dimensions
The following Reasoning Strategy gives an overview of how the equations of kinematics are
applied to describe motion in two dimensions, as in Examples 1 and 2.
REASONING STRATEGY Applying the Equations of Kinematics in Two Dimensions 1. Make a drawing to represent the situation being studied. 2. Decide which directions are to be called positive (+) and negative (−) relative to a con-
veniently chosen coordinate origin. Do not change your decision during the course of a calculation.
3. Remember that the time variable t has the same value for the part of the motion along the x axis and the part along the y axis.
4. In an organized way, write down the values (with appropriate + and − signs) that are given for any of the fi ve kinematic variables associated with the x direction and the y direction. Be on the alert for implied data, such as the phrase “starts from rest,” which means that the values of the initial velocity components are zero: υ0x = 0 m/s and υ0y = 0 m/s. The data summary tables that are used in the examples are a good way of keeping track of this information. In addition, identify the variables that you are being asked to determine.
5. Before attempting to solve a problem, verify that the given information contains values for at least three of the kinematic variables. Do this for the x and the y direction of the motion. Once the three known variables are identifi ed along with the desired unknown variable, the appropriate relations from Table 3.1 can be selected.
6. When the motion is divided into segments, remember that the fi nal velocity for one seg- ment is the initial velocity for the next segment.
7. Keep in mind that a kinematics problem may have two possible answers. Try to visualize the diff erent physical situations to which the answers correspond.
Check Your Understanding
(The answer is given at the end of the book.) 2. A power boat, starting from rest, maintains a constant acceleration. After a certain time t, its
displacement and velocity are r→ and v→. At time 2t, what would be its displacement and velocity, assuming the acceleration remains the same? (a) 2 r→ and 2 v→ (b) 2 r→ and 4 v→ (c) 4 r→ and 2 v→ (d) 4 r→ and 4 v→
3.3 Projectile Motion The biggest thrill in baseball is a home run. The motion of the ball on its curving path into
the stands is a common type of two-dimensional motion called “projectile motion.” A good
description of such motion can often be obtained with the assumption that air resistance is
absent.
Using the equations in Table 3.1, we consider the horizontal and vertical parts of the motion separately. In the horizontal or x direction, the moving object (the projectile) does not slow down in the absence of air resistance. Thus, the x component of the velocity remains con- stant at its initial value or υx = υ0x, and the x component of the acceleration is ax = 0 m/s2. In the vertical or y direction, however, the projectile experiences the eff ect of gravity. As a result, the y component of the velocity υy is not constant and changes. The y component of the accelera- tion ay is the downward acceleration due to gravity. If the path or trajectory of the projectile is near the earth’s surface, ay has a magnitude of 9.80 m/s2. In this text, then, the phrase “projec- tile motion” means that ax = 0 m/s2 and ay equals the acceleration due to gravity. Example 3 and other examples in this section illustrate how the equations of kinematics are applied to
projectile motion.
3.3 Projectile Motion 61
The freely falling package in Example 3 picks up vertical speed on the way downward. The
horizontal component of the velocity, however, retains its initial value of υ0x = +115 m/s throughout the entire descent. Since the plane also travels at a constant horizontal velocity of +115 m/s, it
remains directly above the falling package. The pilot always sees the package directly beneath the
plane, as the dashed vertical lines in Figure 3.7 show. This result is a direct consequence of the fact that the package has no acceleration in the horizontal direction. In reality, air resistance would
slow down the package, and it would not remain directly beneath the plane during the descent.
Figure 3.8 illustrates what happens to two packages that are released simultaneously from the same height, in order to emphasize that the vertical and horizontal parts of the motion in
Example 3 occur independently. Package A is dropped from a stationary balloon and falls straight
downward toward the ground, since it has no horizontal velocity component (υ0x = 0 m/s). Pack- age B, on the other hand, is given an initial velocity component of υ0x = +115 m/s in the hori- zontal direction, as in Example 3, and follows the path shown in the fi gure. Both packages hit the
ground at the same time. Not only do the packages in Figure 3.8 reach the ground at the same time, but the y components of their velocities are also equal at all points on the way down. How- ever, package B does hit the ground with a greater speed than does package A. Remember, speed
y = –1050 m
+x
+y
υ y
x = 115 m/sυ
x = 115 m/sυ
x = 115 m/sυ
υ
υ y υ
FIGURE 3.7 The package falling from the plane is an example of projectile motion,
as Examples 3 and 4 discuss.
EXAMPLE 3 A Falling Care Package
Figure 3.7 shows an airplane moving horizontally with a constant ve- locity of +115 m/s at an altitude of 1050 m. The directions to the right
and upward have been chosen as the positive directions. The plane
releases a “care package” that falls to the ground along a curved tra-
jectory. Ignoring air resistance, determine the time required for the
package to hit the ground.
Reasoning The time required for the package to hit the ground is the time it takes for the package to fall through a vertical distance of 1050 m.
In falling, it moves to the right, as well as downward, but these two
parts of the motion occur independently. Therefore, we can focus solely
on the vertical part. We note that the package is moving initially in
the horizontal or x direction, not in the y direction, so that υ0y = 0 m/s. Furthermore, when the package hits the ground, the y component of its displacement is y = −1050 m, as the drawing shows. The acceleration is that due to gravity, so ay = −9.80 m/s2. These data are summarized as follows:
y-Direction Data y ay υy υ0y t
−1050 m −9.80 m/s2 0 m/s ?
With these data, Equation 3.5b (y = υ0y t + 1
2 ay t 2) can be used to fi nd the fall time.
Problem-Solving Insight The variables y, ay, υy, and υ0y are scalar components. Therefore, an algebraic sign (+ or −) must be included with each one to denote direction.
Solution Since υ0y = 0 m/s, it follows from Equation 3.5b that y = 12ayt2 and
t = √2yay = √ 2(−1050 m)
−9.80 m/s2 = 14.6 s
62 CHAPTER 3 Kinematics in Two Dimensions
is the magnitude of the velocity vector, and the velocity of B has an x component, whereas the velocity of A does not. The magnitude and direction of the velocity vector for package B at the
instant just before the package hits the ground is computed in Example 4.
BA
x = 115 m/sυ
0x = 115 m/sυ
υ yυ y
υ yυ y
υ yυ y
υ
θ FIGURE 3.8 Package A and package B are released
simultaneously at the same height and strike the ground at
the same time because their y variables (y, ay, and 𝜐0y) are the same.
Analyzing Multiple-Concept Problems
EXAMPLE 4 The Velocity of the Care Package
Figure 3.7 shows a care package falling from a plane, and Figure 3.8 shows this package as package B. As in Example 3, the directions to the right
and upward are chosen as the positive directions, and the plane is moving
horizontally with a constant velocity of +115 m/s at an altitude of 1050 m.
Ignoring air resistance, fi nd the magnitude υ and the directional angle θ of the fi nal velocity vector that the package has just before it strikes the ground.
Reasoning Figures 3.7 and 3.8 show the fi nal velocity vector, which has components υx and υy and a magnitude υ. The vector is directed at
an angle θ below the horizontal or x direction. We note the right triangle formed by the vector and its components. The hypotenuse of the triangle
is the magnitude of the velocity, and the components are the other two
sides. As in Example 2, we can use the Pythagorean theorem to express
the magnitude or speed υ in terms of the components υx and υy, and we can use trigonometry to determine the directional angle θ.
Knowns and Unknowns The data for this problem are listed in the table that follows:
Description Symbol Value Comment Explicit Data, x Direction x component of initial velocity υ0x +115 m/s Package has plane’s horizontal velocity at instant of release
Implicit Data, x Direction x component of acceleration ax 0 m/s2 No horizontal acceleration, since air resistance is ignored
Explicit Data, y Direction y component of displacement y −1050 m Negative, since upward is positive and package falls downward
Implicit Data, y Direction y component of initial velocity υ0y 0 m/s Package traveling horizontally in x direction at instant of release,
not in y direction
y component of acceleration ay −9.80 m/s2 Acceleration vector for gravity points downward in the negative direction
Unknown Variables Magnitude of final velocity υ ?
Direction of final velocity θ ?
3.3 Projectile Motion 63
CONCEPTUAL EXAMPLE 5 Shot a Bullet Into the Air . . .
Suppose you are driving in a convertible with the top down. The car is
moving to the right at a constant velocity. As Figure 3.9 illustrates, you point a rifl e straight upward and fi re it. In the absence of air resistance,
would the bullet land (a) behind you, (b) ahead of you, or (c) in the barrel of the rifl e?
Reasoning Because there is no air resistance to slow it down, the bul- let experiences no horizontal acceleration. Thus, the bullet’s horizontal
velocity component does not change, and it stays the same as that of the
rifl e and the car.
Modeling the Problem
STEP 1 Final Velocity Using the Pythagorean theorem to express the speed υ in terms of the components υx and υy (see Figure 3.7 or 3.8), we obtain Equation 1a at the right. Furthermore, in a right triangle, the cosine of an angle is the side adjacent to the angle divided by the hypotenuse.
With this in mind, we see in Figure 3.7 or Figure 3.8 that the directional angle θ is given by Equation 1b at the right.
STEP 2 The Components of the Final Velocity Reference to the table of knowns and un- knowns shows that, in the x direction, values are available for the kinematic variables υ0x and ax. Since the acceleration ax is zero, the fi nal velocity component υx remains unchanged from its initial value of υ0x, so we have
𝜐x = 𝜐0x
In the y direction, values are available for y, υ0y, and ay, so that we can determine the fi nal velocity component υy using Equation 3.6b from the equations of kinematics:
𝜐 2y = 𝜐
2 0y + 2ayy (3.6b)
These results for υx and υy can be substituted into Equations 1a and lb, as shown at the right.
Solution Algebraically combining the results of each step, we fi nd that
υ = √υx2 + υy2 = √υ 20x + υ 20y + 2ayy
θ = cos−1 ( υx
√υ 2x + υy2 ) = cos−1 (
υ0x √υ0x2 + υ0y2 + 2ayy
)
With the data given for the kinematic variables in the x and y directions, we fi nd that the magni- tude and direction of the fi nal velocity of the package are
STEP 1 STEP 2
STEP 1 STEP 2
υ = √υ 20x + υ 20y + 2ayy = √(115 m/s)2 + (0 m/s)2 + 2 (−9.80 m/s2)(−1050 m) = 184 m/s
θ = cos−1 ( υ0x
√υ 20x + υ 20y + 2ayy) = cos−1[ 115 m/s
√(115 m/s)2 + (0 m/s)2 + 2(−9.80 m/s2)(−1050 m) ] = 51.3°
Related Homework: Problems 33, 38, 71
υ = √υx2 + υy2 (1a)
θ = cos−1( 𝜐x
𝜐) = cos−1( 𝜐x
√𝜐x2 + 𝜐y2 )
(1b)
υ = √υx2 + υy2 (1a)
𝜐x = 𝜐0x 𝜐 2y = 𝜐 2
0y + 2ayy (3.6b)
θ = cos−1( 𝜐x
√𝜐x2 + 𝜐y2 ) (1b)
𝜐x = 𝜐0x 𝜐 2y = 𝜐 2
0y + 2ayy (3.6b)
An important feature of projectile motion is that there is no acceleration in the horizontal, or
x, direction. Conceptual Example 5 discusses an interesting implication of this feature.
Problem-Solving Insight The speed of a projectile at any location along its path is the magnitude 𝜐 of its velocity at that location: 𝜐 = √𝜐x2 + 𝜐y2. Both the hori- zontal and vertical velocity components contribute to the speed.
64 CHAPTER 3 Kinematics in Two Dimensions
Often projectiles, such as footballs and baseballs, are sent into the air at an angle with respect
to the ground. From a knowledge of the projectile’s initial velocity, a wealth of information can
be obtained about the motion. For instance, Example 6 demonstrates how to calculate the maxi-
mum height reached by the projectile.
Answers (a) and (b) are incorrect. If air resistance were present, it would slow down the bullet and cause it to land behind you, toward the
rear of the car. However, air resistance is absent. If the bullet were to land
ahead of you, its horizontal velocity component would have to be greater
than that of the rifl e and the car. This cannot be, since the bullet’s horizon-
tal velocity component never changes.
Answer (c) is correct. Since the bullet’s horizontal velocity component does not change, it retains its initial value, and remains matched to that of
the rifl e and the car. As a result, the bullet remains directly above the rifl e
at all times and would fall directly back into the barrel of the rifl e. This
situation is analogous to that in Figure 3.7, where the care package, as it falls, remains directly below the plane.
Related Homework: Problem 39
FIGURE 3.9 The car is moving with a constant velocity to the right, and the rifl e is
pointed straight up. In the absence of air
resistance, a bullet fi red from the rifl e has no
acceleration in the horizontal direction.
Example 5 discusses what happens to the
bullet.
EXAMPLE 6 The Height of a Kickoff
A placekicker kicks a football at an angle of θ = 40.0° above the horizon- tal axis, as Animated Figure 3.10 shows. The initial speed of the ball is υ0 = 22 m/s. Ignore air resistance, and fi nd the maximum height H that the ball attains.
Reasoning The maximum height is a characteristic of the vertical part of the motion, which can be treated separately from the horizontal part. In
preparation for making use of this fact, we calculate the vertical compo-
nent of the initial velocity:
υ0y = υ0 sin θ = +(22 m/s) sin 40.0° = +14 m/s
The vertical component of the velocity, υy, decreases as the ball moves up- ward. Eventually, υy = 0 m/s at the maximum height H. The data below can be used in Equation 3.6b (υy2 = υ0y2 + 2ay y) to fi nd the maximum height:
y-Direction Data y ay υy υ0y t
H = ? −9.80 m/s2 0 m/s +14 m/s
Problem-Solving Insight When a projectile reaches maximum height, the vertical component of its velocity is momentarily zero (υy = 0 m/s). However, the horizontal component of its velocity is not zero.
Solution From Equation 3.6b, we fi nd that
y = H = υy 2 − υ0 y 2
2ay =
(0 m /s) 2 − (14 m /s) 2
2(−9.80 m /s2) = +10 m
The height H depends only on the y variables; the same height would have been reached had the ball been thrown straight up with an initial velocity of υ0y = +14 m/s.
ANIMATED FIGURE 3.10 A football is kicked with an initial speed of υ0 at an angle of θ above the ground. The ball attains a maximum height H and a range R.
H = Maximum height
+y
+x
R = Range
υ 0y
υ 0x
υ 0
+x
+y
θ
3.3 Projectile Motion 65
It is also possible to fi nd the total time or “hang time” during which the football in Animated Figure 3.10 is in the air. Example 7 shows how to determine this time.
EXAMPLE 7 The Physics of the “Hang Time” of a Football
For the motion illustrated in Animated Figure 3.10, ignore air resistance and use the data from Example 6 to determine the time of fl ight between
kickoff and landing.
Reasoning Given the initial velocity, it is the acceleration due to gravity that determines how long the ball stays in the air. Thus, to fi nd the time
of fl ight we deal with the vertical part of the motion. Since the ball starts
at and returns to ground level, the displacement in the y direction is zero. The initial velocity component in the y direction is the same as that in Example 6; that is, υ0y = +14 m/s. Therefore, we have
y-Direction Data y ay υy υ0y t
0 m −9.80 m/s2 +14 m/s ?
The time of fl ight can be determined from Equation 3.5b ( y = υ0y t + 1
2 ay t 2).
Solution Using Equation 3.5b and the fact that y = 0 m, we fi nd that
y = 0 = υ0y t + 1
2 ay t 2 = (υ0y + 1
2 ay t)t
There are two solutions to this equation. One is given by υ0y + 1
2 ay t = 0, with the result that
t = −2υ0y
ay =
−2(14 m/s)
−9.80 m/s2 = 2.9 s
The other is given by t = 0 s. The solution we seek is t = 2.9 s , because t = 0 s corresponds to the initial kickoff .
EXAMPLE 8 The Range of a Kickoff
For the motion shown in Animated Figure 3.10 and discussed in Examples 6 and 7, ignore air resistance and calculate the range R of the projectile.
Reasoning The range is a characteristic of the horizontal part of the motion. Thus, our starting point is to determine the horizontal component
of the initial velocity:
υ0x = υ0 cos θ = +(22 m/s)cos 40.0° = +17 m/s
Recall from Example 7 that the time of fl ight is t = 2.9 s. Since there is no acceleration in the x direction, υx remains constant, and the range is simply the product of υx = υ0x and the time.
Solution The range is
x = R = υ0x t = +(17 m/s)(2.9 s) = +49 m
Another important feature of projectile motion is called the “range.” The range, as Animated Figure 3.10 shows, is the horizontal distance traveled between launching and landing, assuming the projectile returns to the same vertical level at which it was fi red. Example 8 shows how to obtain the range.
Math Skills To show that a projectile launched from and returning to ground level has its maximum range when θ = 45°, we begin with the expression for the range R from Example 8:
R = 𝜐0x t = (𝜐0 cos θ)t
The range in the previous example depends on the angle θ at which the projectile is fi red above the horizontal. When air resistance is absent, the maximum range results when
θ = 45°.
(Continued)
66 CHAPTER 3 Kinematics in Two Dimensions
In projectile motion, the magnitude of the acceleration due to gravity aff ects the trajectory in
a signifi cant way. For example, a baseball or a golf ball would travel much farther and higher on
the moon than on the earth, when launched with the same initial velocity. The reason is that the
moon’s gravity is only about one-sixth as strong as the earth’s.
Section 2.6 points out that certain types of symmetry with respect to time and speed are
present for freely falling bodies. These symmetries are also found in projectile motion, since pro-
jectiles are falling freely in the vertical direction. In particular, the time required for a projectile
to reach its maximum height H is equal to the time spent returning to the ground. In addition, Figure 3.11 shows that the speed υ of the object at any height above the ground on the upward part of the trajectory is equal to the speed υ at the same height on the downward part. Although the two speeds are the same, the velocities are diff erent, because they point in diff erent directions.
Conceptual Example 9 shows how to use this type of symmetry in your reasoning.
Example 7 shows that the time of fl ight of the projectile is
t = −2𝜐0y
ay =
−2𝜐0y
−9.80 m/s2 =
2𝜐0y
9.80 m/s2
According to Example 6, the velocity component υ0y in this result is υ0y = υ0 sin θ, so that
t = 2𝜐0 sin θ 9.80 m/s2
Substituting this expression for t into the range expression gives
R = (𝜐0 cos θ)t = (𝜐0 cos θ) 2𝜐0 sin θ 9.80 m/s2
= 𝜐0
2 2 sin θ cos θ 9.80 m/s2
Equation 6 (Other Trigonometric Identities) in Appendix E.2 shows that 2 sin θ cos θ = sin 2θ, so the range expression becomes
R = 𝜐 20 2 sin θ cos θ
9.80 m/s2 =
𝜐 20 sin 2θ 9.80 m/s2
In this result R has its maximum value when sin 2θ has its maximum value of 1. This occurs when 2θ = 90°, or when θ = 45°.
FIGURE 3.11 The speed 𝜐 of a projectile at a given height above the ground is the
same on the upward and downward parts of
the trajectory. The velocities are diff erent,
however, since they point in diff erent
directions.
Height
υ
υ
θ θ
θ θ θ P
2
1
v0
v0 v0
FIGURE 3.12 Two stones are thrown off the cliff with identical initial speeds υ0, but at equal angles θ that are below and above the horizontal. Conceptual Example 9 compares the velocities with which the stones hit
the water below.
CONCEPTUAL EXAMPLE 9 Two Ways to Throw a Stone
From the top of a cliff overlooking a lake, a person throws two stones.
The stones have identical initial speeds υ0, but stone 1 is thrown down- ward at an angle θ below the horizontal, while stone 2 is thrown upward at the same angle above the horizontal, as Figure 3.12 shows. Neglect air resistance and decide which stone, if either, strikes the water with the
greater velocity: (a) both stones strike the water with the same velocity, (b) stone 1 strikes with the greater velocity, (c) stone 2 strikes with the greater velocity.
Reasoning Note point P in the drawing, where stone 2 returns to its initial height; here the speed of stone 2 is υ0 (the same as its initial speed), but its velocity is directed at an angle θ below the horizontal. This is exactly the type of projectile symmetry illustrated in Figure 3.11, and this symmetry will lead us to the correct answer.
3.3 Projectile Motion 67
In all the examples in this section, the projectiles follow a curved trajectory. In general, if
the only acceleration is that due to gravity, the shape of the path can be shown to be a parabola.
Check Your Understanding
(The answers are given at the end of the book.) 3. A projectile is fi red into the air, and it follows the parabolic path shown in CYU Figure 3.1, landing on
the right. There is no air resistance. At any instant, the projectile has a velocity v→ and an acceleration a→. Which one or more of the drawings could not represent the directions for v→ and a→ at any point on the trajectory?
(a) (b) (c) (d)
v
v
v
a
a a av
CYU FIGURE 3.1
4. An object is thrown upward at an angle θ above the ground, eventually returning to earth. (a) Is there any place along the trajectory where the velocity and acceleration are perpendicular? If so, where?
(b) Is there any place where the velocity and acceleration are parallel? If so, where? 5. Is the acceleration of a projectile equal to zero when the projectile reaches the top of its trajectory? 6. In baseball, the pitcher’s mound is raised to compensate for the fact that the ball falls downward as it
travels from the pitcher toward the batter. If baseball were played on the moon, would the pitcher’s
mound have to be (a) higher than, (b) lower than, or (c) the same height as it is on earth? 7. A tennis ball is hit upward into the air and moves along an arc. Neglecting air resistance, where along
the arc is the speed of the ball (a) a minimum and (b) a maximum? 8. A wrench is accidentally dropped from the top of the mast on a sailboat. Air resistance is negligible.
Will the wrench hit at the same place on the deck whether the sailboat is at rest or moving with a con-
stant velocity?
9. A rifl e, at a height H above the ground, fi res a bullet parallel to the ground. At the same instant and at the same height, a second bullet is dropped from rest. In the absence of air resistance, which bullet, if
either, strikes the ground fi rst?
10. A stone is thrown horizontally from the top of a cliff and eventually hits the ground below. A second stone is dropped from rest from the same cliff , falls through the same height, and also hits the ground
below. Ignore air resistance. Is each of the following quantities diff erent or the same in the two cases?
(a) Displacement (b) Speed just before impact with the ground (c) Time of fl ight 11. A leopard springs upward at a 45° angle and then falls back to the ground. Air resistance is negligible.
Does the leopard, at any point on its trajectory, ever have a speed that is one-half its initial value?
12. Two balls are launched upward from the same spot at diff erent angles with respect to the ground. Both balls rise to the same maximum height. Ball A, however, follows a trajectory that has a greater
range than that of ball B. Ignoring air resistance, decide which ball, if either, has the greater launch
speed.
Answers (b) and (c) are incorrect. You might guess that stone 1, being hurled downward, would strike the water with the greater velocity. Or,
you might think that stone 2, having reached a greater height than stone 1,
would hit the water with the greater velocity. To understand why neither
of these answers is correct, see the response for answer (a) below.
Answer (a) is correct. Let’s follow the path of stone 2 as it rises to its maximum height and falls back to earth. When it reaches point P in the
drawing, stone 2 has a velocity that is identical to the velocity with which
stone 1 is thrown downward from the top of the cliff (see the drawing).
From this point on, the velocity of stone 2 changes in exactly the same
way as that for stone 1, so both stones strike the water with the same
velocity.
Related Homework: Problems 23, 75
68 CHAPTER 3 Kinematics in Two Dimensions
3.4 Relative Velocity To someone hitchhiking along a highway, two cars speeding by in adjacent lanes seem like a blur.
But if the cars have the same velocity, each driver sees the other remaining in place, one lane
away. The hitchhiker observes a velocity of perhaps 30 m/s, but each driver observes the other’s
velocity to be zero. Clearly, the velocity of an object is relative to the observer who is making
the measurement.
Figure 3.13 illustrates the concept of relative velocity by showing a passenger walking toward the front of a moving train. The people sitting on the train see the passenger walking with
a velocity of +2.0 m/s, where the plus sign denotes a direction to the right. Suppose the train
is moving with a velocity of +9.0 m/s relative to an observer standing on the ground. Then the
ground-based observer would see the passenger moving with a velocity of +11 m/s, due in part
to the walking motion and in part to the train’s motion. As an aid in describing relative velocity,
let us defi ne the following symbols:
v→ PT = velocity of the Passenger relative to the Train = +2.0 m/s v→ TG = velocity of the Train relative to the Ground = +9.0 m/s v→ PG = velocity of the Passenger relative to the Ground = +11 m/s
In terms of these symbols, the situation in Figure 3.13 can be summarized as follows: v→PG = v→PT + v→TG (3.7) or
v→PG = (2.0 m/s) + (9.0 m/s) = +11 m/s According to Equation 3.7*, v→PG is the vector sum of v→PT and v→TG, and this sum is shown in the drawing. Had the passenger been walking toward the rear of the train, rather than toward the
front, the velocity relative to the ground-based observer would have been v→PG = (−2.0 m/s) + (9.0 m/s) = +7.0 m/s.
Each velocity symbol in Equation 3.7 contains a two-letter subscript. The fi rst letter in the
subscript refers to the body that is moving, while the second letter indicates the object relative
to which the velocity is measured. For example,v→TG and v→PG are the velocities of the Train and Passenger measured relative to the Ground. Similarly, v→PT is the velocity of the Passenger measured by an observer sitting on the Train.
The ordering of the subscript symbols in Equation 3.7 follows a defi nite pattern. The fi rst
subscript (P) on the left side of the equation is also the fi rst subscript on the right side of the equa-
tion. Likewise, the last subscript (G) on the left side is also the last subscript on the right side. The
third subscript (T) appears only on the right side of the equation as the two “inner” subscripts.
The colored boxes below emphasize the pattern of the symbols in the subscripts:
v→ PG = v→ P T + v →
T G
In other situations such as in the case of a helicopter landing on an aircraft carrier (Photo 3.1), the subscripts will not necessarily be P, G, and T, but will be compatible with the names of the
objects involved in the motion.
PHOTO 3.1 In landing on a moving aircraft carrier, the pilot of the helicopter must match
the helicopter’s horizontal velocity to the
carrier’s velocity, so that the relative velocity
of the helicopter and the carrier is zero.
TAL COHEN/AFP/Getty Images
FIGURE 3.13 The velocity of the passenger relative to the ground-based observer is v→PG. It is the vector sum of the velocity v→PT of the passenger relative to the train and the velocity v→TG of the train relative to the ground: v→PG = v→PT + v→TG.
vTG = +9.0 m/s
Ground-based observer
vPT = +2.0 m/s
vPG = +11.0 m/s
vTGvPT
*This equation assumes that the train and the ground move in a straight line relative to one another.
3.4 Relative Velocity 69
Equation 3.7 has been presented in connection with one-dimensional motion, but the result
is also valid for two-dimensional motion. Figure 3.14 depicts a common situation that deals with relative velocity in two dimensions. Part a of the drawing shows a boat being carried downstream by a river; the engine of the boat is turned off . In part b, the engine is turned on, and now the boat moves across the river in a diagonal fashion because of the combined motion produced by the
current and the engine. The list below gives the velocities for this type of motion and the objects
relative to which they are measured:
v→ BW = velocity of the Boat relative to the Water v→ WS = velocity of the Water relative to the Shore v→ BS = velocity of the Boat relative to the Shore The velocity v→BW of the boat relative to the water is the velocity measured by an observer who, for instance, is fl oating on an inner tube and drifting downstream with the current. When the
engine is turned off , the boat also drifts downstream with the current, and v→BW is zero. When the engine is turned on, however, the boat can move relative to the water, and v→BW is no longer zero. The velocity v→WS of the water relative to the shore is the velocity of the current measured by an observer on the shore. The velocity v→BS of the boat relative to the shore is due to the com- bined motion of the boat relative to the water and the motion of the water relative to the shore.
In symbols,
v→ BS = v→ B W + v →
W S
The ordering of the subscripts in this equation is identical to that in Equation 3.7, although the letters
have been changed to refl ect a diff erent physical situation. Example 10 illustrates the concept of
relative velocity in two dimensions.
FIGURE 3.14 (a) A boat with its engine turned off is carried along by the current.
(b) With the engine turned on, the boat moves across the river in a diagonal fashion.
Current
Current
(a)
(b)
EXAMPLE 10 Crossing a River
The engine of a boat drives it across a river that is 1800 m wide. The
velocity v→BW of the boat relative to the water is 4.0 m/s, directed perpen- dicular to the current, as in Interactive Figure 3.15. The velocity v→WS of the water relative to the shore is 2.0 m/s. (a) What is the velocity v→BS of the boat relative to the shore? (b) How long does it take for the boat to cross the river?
Reasoning (a) The velocity of the boat relative to the shore is v→BS. It is the vector sum of the velocity v→BW of the boat relative to the water and the velocity v→WS of the water relative to the shore: v→BS = v→BW + v→WS. Since v→BW and v→WS are both known, we can use this relation among the veloci- ties, with the aid of trigonometry, to fi nd the magnitude and directional
angle of v→BS. (b) The component of v→BS that is parallel to the width of the river (see Interactive Figure 3.15) determines how fast the boat crosses the river; this parallel component is υBS sin θ = υBW = 4.0 m/s. The time for the boat to cross the river is equal to the width of the river divided by
the magnitude of this velocity component.
Solution (a) Since the vectors v→BW and v→WS are perpendicular (see Interactive Figure 3.15), the magnitude of v→BS can be determined by using the Pythagorean theorem:
υBS = √(υBW)2 + (υWS)2 = √(4.0 m/s)2 + (2.0 m/s)2 = 4.5 m/s
Thus, the boat moves at a speed of 4.5 m/s with respect to an observer on
shore. The direction of the boat relative to the shore is given by the angle
θ in the drawing:
tan θ = υBW υWS
or θ = tan−1 ( υBW υWS) = tan−1 (
4.0 m/s
2.0 m/s) = 63° (b) The time t for the boat to cross the river is
t = Width
υBS sin θ =
1800 m
4.0 m/s = 450 s
INTERACTIVE FIGURE 3.15 The velocity of the boat relative to the shore
is v→BS. It is the vector sum of the velocity v→BW of the boat relative to the water and the velocity v→WS of the water relative to the shore: v→BS = v→BW + v→WS.
vBW = 4.0 m/s
vWS = 2.0 m/s
vBS +y
+x
θ
70 CHAPTER 3 Kinematics in Two Dimensions
Sometimes, situations arise when two vehicles are in relative motion, and it is useful to know
the relative velocity of one with respect to the other. Example 11 considers this type of relative
motion.
EXAMPLE 11 Approaching an Intersection
Figure 3.16a shows two cars approaching an intersection along perpen- dicular roads. The cars have the following velocities:
v→ AG = velocity of car A relative to the Ground = 25.0 m/s, eastward
v→ BG = velocity of car B relative to the Ground = 15.8 m/s, northward
Find the magnitude and direction of v→AB, where
v→ AB = velocity of car A as measured by a passenger in car B
Reasoning To fi nd v→AB, we use an equation whose subscripts follow the order outlined earlier. Thus,
v→ AB = v→ A G + v→G B
In this equation, the term v→GB is the velocity of the ground relative to a passenger in car B, rather than v→BG, which is given as 15.8 m/s, north- ward. In other words, the subscripts are reversed. However, v→GB is related to v→BG according to
v→GB = −v→BG This relationship refl ects the fact that a passenger in car B, moving north-
ward relative to the ground, looks out the car window and sees the ground
moving southward, in the opposite direction. Therefore, the equation
v→AB = v→AG + v→GB may be used to fi nd v→AB, provided we recognize v→GB as a vector that points opposite to the given velocity v→BG. With this in mind, Figure 3.16b illustrates how v→AG and v→GB are added vectorially to give v→AB.
Problem-Solving Insight In general, the velocity of object R relative to object S is always the negative of the velocity of object S relative to R: v→RS = −v→SR.
Solution From the vector triangle in Figure 3.16b, the magnitude and direction of v→AB can be calculated as
υAB = √(υAG)2 + (υGB)2 = √(25.0 m/s)2 + (−15.8 m/s)2 = 29.6 m/s
and
cos θ = υAG υAB
or θ = cos−1( υAG υAB) = cos−1(
25.0 m/s
29.6 m/s) = 32.4°
FIGURE 3.16 Two cars are approaching an intersection along perpendicular roads.
(b)
(a)
Car B
Car A
vAG = 25.0 m/s vGB = –vBG
vAG
vAB = vAG + vGB
vBG = 15.8 m/s
N
S
W E
θ
THE PHYSICS OF . . . raindrops falling on car windows. While driving a car, have you ever noticed that the rear window sometimes remains dry, even though rain is falling? This
phenomenon is a consequence of relative velocity, as Figure 3.17 helps to explain. Part a shows a car traveling horizontally with a velocity of v→CG and a raindrop falling vertically with a velocity of v→RG. Both velocities are measured relative to the ground. To determine whether the raindrop
3.4 Relative Velocity 71
hits the window, however, we need to consider the velocity of the raindrop relative to the car, not
to the ground. This velocity is v→RC, and we know that v→RC = v→RG + v→GC = v→RG − v→CG Here, we have used the fact that v→GC = −v→CG. Part b of the drawing shows the tail-to-head arrangement corresponding to this vector subtraction and indicates that the direction of v→RC is given by the angle θR. In comparison, the rear window is inclined at an angle θW with respect to the vertical (see the blowup in part a). When θR is greater than θW, the raindrop will miss the window. However, θR is determined by the speed υRG of the raindrop and the speed υCG of the car, according to θR = tan−1(υCG/υRG). At higher car speeds, the angle θR becomes too large for the drop to hit the window. At a high enough speed, then, the car simply drives out from under each
falling drop!
Check Your Understanding
(The answers are given at the end of the book.) 13. Three cars, A, B, and C, are moving along a straight section of a highway. The velocity of A relative
to B is v→AB, the velocity of A relative to C is v→AC, and the velocity of C relative to B is v→CB. Fill in the missing velocities in the table.
v→AB v→AC v→CB (a) ? +40 m/s +30 m/s
(b) ? +50 m/s −20 m/s
(c) +60 m/s +20 m/s ?
(d) −50 m/s ? +10 m/s
14. On a riverboat cruise, a plastic bottle is accidentally dropped overboard. A passenger on the boat estimates that the boat pulls ahead of the bottle by 5 meters each second. Is it possible to conclude
that the magnitude of the velocity of the boat with respect to the shore is 5 m/s?
15. A plane takes off at St. Louis, fl ies straight to Denver, and then returns the same way. The plane fl ies at the same speed with respect to the ground during the entire fl ight, and there are no head winds or
tail winds. Since the earth revolves around its axis once a day, you might expect that the times for
the outbound trip and the return trip diff er, depending on whether the plane fl ies against the earth’s
rotation or with it. Is this true, or are the two times the same?
16. A child is playing on the fl oor of a recreational vehicle (RV) as it moves along the highway at a constant velocity. He has a toy cannon, which shoots a marble at a fi xed angle and speed with respect to the fl oor.
The cannon can be aimed toward the front or the rear of the RV. Is the range toward the front the same
as, less than, or greater than the range toward the rear? Answer this question (a) from the child’s point of view and (b) from the point of view of an observer standing still on the ground.
17. Three swimmers can swim equally fast relative to the water. They have a race to see who can swim across a river in the least time. Swimmer A swims perpendicular to the current and lands on the far
shore downstream, because the current has swept him in that direction. Swimmer B swims upstream at
an angle to the current, choosing the angle so that he lands on the far shore directly opposite the starting
point. Swimmer C swims downstream at an angle to the current in an attempt to take advantage of the
current. Who crosses the river in the least time?
FIGURE 3.17 (a) With respect to the ground, a car is traveling at a velocity of v→CG and a raindrop is falling at a velocity of v→RG. The rear window of the car is inclined at an angle θW with respect to the vertical. (b) This tail-to-head arrangement of vectors corresponds to the equation v→RC = v→RG − v→CG.
w Raindrop
R
–vCG
vRC
(b)(a)
vRG vCG
vRG
θ
θ
72 CHAPTER 3 Kinematics in Two Dimensions
Finally, 𝜐CG = 𝜐BC
tan 15° =
4.6 m/s
tan 15° = 17 m/s
EXAMPLE 12 BIO The Physics of Blood Splatter
The shape of the splatter made by a falling drop of blood on a surface can
provide information on the velocity of the drop at impact. By measuring
the physical dimensions of the pattern, forensic scientists can determine
the drop’s angle of impact with the surface. If a drop of blood falls straight
downward and strikes a horizontal surface, the pattern it leaves is fairly
circular (Figure 3.18a). However, if the drop strikes the surface at some angle less than 90°, then the pattern will be elongated with a tail (Fig- ure 3.18a). Consider the following situation where a chef at a restaurant accidentally cuts her fi nger while slicing vegetables. She quickly gets in
her car to drive to the closest emergency room for stitches, but she keeps
her hand outside the window, so as to not drip blood inside the car. Based
on the elongation of the drops of blood on the roadway, the impact angle
was determined to be 15°. Assume the drops of blood behave like a pro-
jectile released from a height of 1.1 m and determine the speed of the car.
Reasoning This problem is similar to the physics of falling raindrops. We can analyze the blood splatter by using relative velocity. Here, we
assume the chef’s car is traveling horizontally with a velocity relative
to ground of v→CG, and the blood drop is falling vertically and impacts the ground with a velocity relative to the car of v→BC (Figure 3.18b). The velocity of the blood drop relative to the ground, which determines its
elongation on impact, will be given by:
v→BG = v→BC + v→CG Notice how the subscripts follow the order outlined earlier. This equation
can be solved for the velocity of the car relative to ground (v→CG). The velocity of the blood drop relative to the car (v→BC) at impact can be deter- mined using the kinematic equations for freely falling bodies.
Solution From the vector triangle in Figure 3.18c, tan 15° = 𝜐BC
𝜐CG ,
therefore, 𝜐CG = 𝜐BC
tan 15° . To calculate this we have to fi nd v→BC. This
represents the speed of the blood drop relative to the car at impact. The speed of the blood drop at impact will be equal to the speed of an object
that falls from rest through a distance of 1.1 m. Using Equation 2.9, we
have υBC2 = 𝜐 2BC0 + 2ay or υBC = √υBC02 + 2ay. Therefore,
υBC = √(0 m/s)2 + 2(−9.8 m/s2)(−1.1 m) = 4.6 m/s
Concept Summary 3.1 Displacement, Velocity, and Acceleration The position of an object is located with a vector r→ drawn from the coordinate origin to the object. The displacement Δ r→ of the object is defi ned as Δ r→ = r→ − r→0, where r→ and r→0 specify its fi nal and initial positions, respectively.
The average velocity v→ of an object moving between two positions is defi ned as its displacement Δr→ = r→ − r→0 divided by the elapsed time ∆t = t − t0, as in Equation 3.1.
v→ = r→ − r→0 t − t0
= ∆r→
∆t (3.1)
The instantaneous velocity v→ is the velocity at an instant of time. The average velocity becomes equal to the instantaneous velocity in
the limit that Δt becomes infi nitesimally small (∆t → 0 s), as shown in Equation 1.
v→ = lim ∆t → 0
∆r→
∆ t (1)
The average acceleration a→ of an object is the change in its velocity, Δv→ = v→ − v→0 divided by the elapsed time ∆t = t − t0, as in Equation 3.2.
a→ = v→ − v→0 t − t0
= ∆v→
∆ t (3.2)
The instantaneous acceleration a→ is the acceleration at an instant of time. The average acceleration becomes equal to the instantaneous acceleration in
the limit that the elapsed time Δt becomes infi nitesimally small, as shown in Equation 2.
→a = lim ∆ t → 0
∆v→
∆t (2)
vBC
(b)
1.1 m
vCG
(c)
15°
vCG
vBG vBC
FIGURE 3.18 (a) The shape of a drop of blood splatter on a horizontal surface depends on the angle of impact (θ ) of the drop. (b) The velocity of the car relative to the ground is v→CG, and the velocity of the blood drop relative to the car is v→BC. (c) This fi gure illustrates how v→BC and v→CG add vectorially to give v→BG.
Blood Drop Elongation
Elongation of droplet occurs upon impact
How Bloodstain Pattern Analysis Works
(a)
90° 80° 70° 60°
10°20° 40°
θ Blood droplet
Angle of impact
Focus on Concepts 73
3.2 Equations of Kinematics in Two Dimensions Motion in two dimen- sions can be described in terms of the time t and the x and y components of four vectors: the displacement, the acceleration, and the initial and fi nal velo-
cities. The x part of the motion occurs exactly as it would if the y part did not occur at all. Similarly, the y part of the motion occurs exactly as it would if the x part of the motion did not exist. The motion can be analyzed by treating the x and y components of the four vectors separately and realizing that the time t is the same for each component.
When the acceleration is constant, the x components of the displacement, the acceleration, and the initial and fi nal velocities are related by the equa-
tions of kinematics, and so are the y components:
x Component 𝜐x = 𝜐0x + axt (3.3a)
x = 12 (𝜐0x + 𝜐x)t (3.4a)
x = 𝜐0xt + 1
2 axt2 (3.5a)
𝜐x 2 = 𝜐0x
2 + 2ax x (3.6a)
y Component 𝜐y = 𝜐0y + ayt (3.3b)
y = 12 (𝜐0y + 𝜐y)t (3.4b)
y = 𝜐0yt + 1
2 ay t 2 (3.5b)
𝜐y 2 = 𝜐0y
2 + 2ayy (3.6b)
The directions of the components of the displacement, the acceleration,
and the initial and fi nal velocities are conveyed by assigning a plus (+) or
minus (−) sign to each one.
3.3 Projectile Motion Projectile motion is an idealized kind of motion that occurs when a moving object (the projectile) experiences only the ac-
celeration due to gravity, which acts vertically downward. If the trajectory
of the projectile is near the earth’s surface, the vertical component ay of the acceleration has a magnitude of 9.80 m/s2. The acceleration has no
horizontal component (ax = 0 m/s2), the eff ects of air resistance being negligible.
There are several symmetries in projectile motion: (1) The time to reach
maximum height from any vertical level is equal to the time spent returning
from the maximum height to that level. (2) The speed of a projectile depends
only on its height above its launch point, and not on whether it is moving
upward or downward.
3.4 Relative Velocity The velocity of object A relative to object B is v→AB, and the velocity of object B relative to object C is v→BC. The velocity of A rel- ative to C is shown in Equation 3 (note the ordering of the subscripts). While
the velocity of object A relative to object B is v→AB, the velocity of B relative to A is v→BA = −v→AB.
v→AC = v→AB + v→BC (3)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 3.3 Projectile Motion 1. The drawing shows projectile motion at three points along the trajectory. The speeds at the
points are υ1, υ2, and υ3. Assume there is no air resistance and rank the speeds, largest to smallest.
(Note that the symbol > means “greater than.”)
(a) υ1 > υ3 > υ2 (b) υ1 > υ2 > υ3 (c) υ2 > υ3 > υ1 (d) υ2 > υ1 > υ3 (e) υ3 > υ2 > υ1 3. Two balls are thrown from the top of a building, as in the drawing. Ball 1 is thrown straight down, and ball 2 is thrown with the same speed, but upward
at an angle θ with respect to the horizontal. Consider the motion of the balls after they are released. Which
one of the following statements is true? (a) The accel- eration of ball 1 becomes larger and larger as it falls,
because the ball is going faster and faster. (b) The ac- celeration of ball 2 decreases as it rises, becomes zero
at the top of the trajectory, and then increases as the
ball begins to fall toward the ground. (c) Both balls have the same acceleration at all times. (d) Ball 2 has an acceleration in both the horizontal and vertical
directions, but ball 1 has an acceleration only in the
vertical direction.
4. Each drawing shows three points along the path of a projectile, one on its way up, one at the top, and one on its way down. The launch point
is on the left in each drawing. Which drawing correctly represents the
acceleration a→ of the projectile at these three points? (a) 1 (b) 2 (c) 3 (d) 4 (e) 5
1 2 3
a = 0 m/s2 a = 0 m/s2 a = 0 m/s2
4 5
QUESTION 4 6. Ball 1 is thrown into the air and it follows the trajectory for projectile motion shown in the drawing. At the instant that ball 1 is at the top of its
trajectory, ball 2 is dropped from rest from the same height. Which ball reaches
the ground fi rst? (a) Ball 1 reaches the ground fi rst, since it is moving at the top of the trajectory, while ball 2 is dropped from rest. (b) Ball 2 reaches the ground fi rst, because it has the shorter distance to travel. (c) Both balls reach the ground at the same time. (d) There is not enough information to tell which ball reaches the ground fi rst.
QUESTION 6
Ball 1
Ball 2 xυ
Focus on Concepts
QUESTION 1
1
2
3
QUESTION 3
Ball 2
Ball 1
θ
74 CHAPTER 3 Kinematics in Two Dimensions
9. Two objects are fi red into the air, and the drawing shows the projectile mo- tions. Projectile 1 reaches the greater height, but projectile 2 has the greater
range. Which one is in the air for the greater amount of time? (a) Projectile 1, because it travels higher than projectile 2. (b) Projectile 2, because it has the greater range. (c) Both projectiles spend the same amount of time in the air. (d) Projectile 2, because it has the smaller initial speed and, therefore, travels more slowly than projectile 1.
QUESTION 9
1
2
Section 3.4 Relative Velocity 14. A slower-moving car is traveling behind a faster-moving bus. The velo- cities of the two vehicles are as follows:
v→CG = velocity of the Car relative to the Ground = +12 m/s
v→BG = velocity of the Bus relative to the Ground = +16 m/s
A passenger on the bus gets up and walks toward the front of the bus with a
velocity of v→PB, where v→PB = velocity of the Passenger relative to the Bus = +2 m/s. What is v→PC, the velocity of the Passenger relative to the Car?
(a) +2 m/s + 16 m/s + 12 m/s = +30 m/s (b) −2 m/s + 16 m/s + 12 m/s = +26 m/s (c) +2 m/s + 16 m/s − 12 m/s = +6 m/s (d) −2 m/s + 16 m/s − 12 m/s = +2 m/s
15. Your car is traveling behind a jeep. Both are moving at the same speed, so the velocity of the jeep relative to you is zero. A spare tire is strapped to
the back of the jeep. Suddenly the strap breaks, and the tire falls off the jeep.
Will your car hit the spare tire before the tire hits the road? Assume that air
resistance is absent. (a) Yes. As long as the car doesn’t slow down, it will hit the tire. (b) No. The car will not hit the tire before the tire hits the ground, no matter how close you are to the jeep. (c) If the tire falls from a great enough height, the car will hit the tire. (d) If the car is far enough behind the jeep, the car will not hit the tire.
16. The drawing shows two cars traveling in diff erent directions with diff er- ent speeds. Their velocities are:
v→AG = velocity of car A relative to the Ground = 27.0 m/s, due east
v→BG = velocity of car B relative to the Ground = 21.0 m/s, due north
The passenger of car B looks out the window and sees car A. What is the
velocity (magnitude and direction) of car A as observed by the passenger of
car B? In other words, what is the velocity v→AB of car A relative to car B? Give the directional angle of v→AB with respect to due east.
QUESTION 16
Car A
Car B
East
North
vBG
vAG
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 3.1 Displacement, Velocity, and Acceleration 1. E SSM Two trees have perfectly straight trunks and are both growing perpendicular to the fl at horizontal ground beneath them. The sides of
the trunks that face each other are separated by 1.3 m. A frisky squirrel
makes three jumps in rapid succession. First, he leaps from the foot of
one tree to a spot that is 1.0 m above the ground on the other tree. Then,
he jumps back to the fi rst tree, landing on it at a spot that is 1.7 m above
the ground. Finally, he leaps back to the other tree, now landing at a spot
that is 2.5 m above the ground. What is the magnitude of the squirrel’s
displacement?
2. E A meteoroid is traveling east through the atmosphere at 18.3 km/s while descending at a rate of 11.5 km/s. What is its speed, in km/s?
3. E GO In a football game a kicker attempts a fi eld goal. The ball remains in contact with the kicker’s foot for 0.050 s, during which time it experiences an ac-
celeration of 340 m/s2. The ball is launched at an angle of 51° above the ground.
Determine the horizontal and vertical components of the launch velocity.
4. E A baseball player hits a triple and ends up on third base. A baseball “dia- mond” is a square, each side of length 27.4 m, with home plate and the three
bases on the four corners. What is the magnitude of the player’s displacement?
5. E SSM In diving to a depth of 750 m, an elephant seal also moves 460 m due east of his starting point. What is the magnitude of the seal’s displacement?
6. E A mountain-climbing expedition establishes two intermediate camps, labeled A and B in the drawing, above the base camp. What is the magnitude Δr of the displacement between camp A and camp B?
PROBLEM 6
3200 m
4900 m
B
A
Base Camp
11 200 m
19 600 m
rΔ
Problems
Problems 75
7. E SSM A radar antenna is tracking a satellite orbiting the earth. At a cer- tain time, the radar screen shows the satellite to be 162 km away. The radar
antenna is pointing upward at an angle of 62.3° from the ground. Find the x and y components (in km) of the position vector of the satellite, relative to the antenna.
8. E GO In a mall, a shopper rides up an escalator between fl oors. At the top of the escalator, the shopper turns right and walks 9.00 m to a store. The
magnitude of the shopper’s displacement from the bottom of the escalator
to the store is 16.0 m. The vertical distance between the fl oors is 6.00 m. At
what angle is the escalator inclined above the horizontal?
9. E SSM A skateboarder, starting from rest, rolls down a 12.0-m ramp. When she arrives at the bottom of the ramp her speed is 7.70 m/s. (a) De- termine the magnitude of her acceleration, assumed to be constant. (b) If the ramp is inclined at 25.0° with respect to the ground, what is the component
of her acceleration that is parallel to the ground?
10. M V-HINT MMH E A bird watcher meanders through the woods, walking 0.50 km due east, 0.75 km due south, and 2.15 km in a direction 35.0° north
of west. The time required for this trip is 2.50 h. Determine the magnitude
and direction (relative to due west) of the bird watcher’s (a) displacement and (b) average velocity. Use kilometers and hours for distance and time, respectively.
11. M MMH The earth moves around the sun in a nearly circular orbit of radius 1.50 × 1011 m. During the three summer months (an elapsed time of
7.89 × 106 s), the earth moves one-fourth of the distance around the sun.
(a) What is the average speed of the earth? (b) What is the magnitude of the average velocity of the earth during this period?
Section 3.2 Equations of Kinematics in Two Dimensions/ Section 3.3 Projectile Motion 12. E A spacecraft is traveling with a velocity of υ0x = 5480 m/s along the +x direction. Two engines are turned on for a time of 842 s. One engine gives the spacecraft an acceleration in the +x direction of ax = 1.20 m/s2, while the other gives it an acceleration in the +y direction of ay = 8.40 m/s2. At the end of the fi ring, fi nd (a) υx and (b) υy. 13. E SSM A volleyball is spiked so that it has an initial velocity of 15 m/s dir- ected downward at an angle of 55° below the horizontal. What is the horizontal
component of the ball’s velocity when the opposing player fi elds the ball?
14. E CHALK As a tennis ball is struck, it departs from the racket horizont- ally with a speed of 28.0 m/s. The ball hits the court at a horizontal distance
of 19.6 m from the racket. How far above the court is the tennis ball when it
leaves the racket?
15. E A skateboarder shoots off a ramp with a velocity of 6.6 m/s, directed at an angle of 58° above the horizontal. The end of the ramp is 1.2 m above
the ground. Let the x axis be parallel to the ground, the +y direction be vertic- ally upward, and take as the origin the point on the ground directly below the
top of the ramp. (a) How high above the ground is the highest point that the skateboarder reaches? (b) When the skateboarder reaches the highest point, how far is this point horizontally from the end of the ramp?
16. E GO A puck is moving on an air hockey table. Relative to an x, y coordin- ate system at time t = 0 s, the x components of the puck’s initial velocity and acceleration are υ0x = +1.0 m/s and ax = +2.0 m/s2. The y components of the puck’s initial velocity and acceleration are υ0y = +2.0 m/s and ay = −2.0 m/s2. Find the magnitude and direction of the puck’s velocity at a time of t = 0.50 s. Specify the direction relative to the +x axis. 17. E SSM A spider crawling across a table leaps onto a magazine blocking its path. The initial velocity of the spider is 0.870 m/s at an angle of 35.0°
above the table, and it lands on the magazine 0.0770 s after leaving the table.
Ignore air resistance. How thick is the magazine? Express your answer in
millimeters.
18. E A horizontal rifl e is fi red at a bull’s-eye. The muzzle speed of the bullet is 670 m/s. The gun is pointed directly at the center of the bull’s-eye, but the
bullet strikes the target 0.025 m below the center. What is the horizontal dis-
tance between the end of the rifl e and the bull’s-eye?
19. E MMH A golfer imparts a speed of 30.3 m/s to a ball, and it travels the maximum possible distance before landing on the green. The tee and the
green are at the same elevation. (a) How much time does the ball spend in the air? (b) What is the longest hole in one that the golfer can make, if the ball does not roll when it hits the green?
20. E GO A golfer hits a shot to a green that is elevated 3.0 m above the point where the ball is struck. The ball leaves the club at a speed of 14.0 m/s
at an angle of 40.0° above the horizontal. It rises to its maximum height and
then falls down to the green. Ignoring air resistance, fi nd the speed of the ball
just before it lands.
21. E SSM In the aerials competition in skiing, the competitors speed down a ramp that slopes sharply upward at the end. The sharp upward slope
launches them into the air, where they perform acrobatic maneuvers. The
end of a launch ramp is directed 63° above the horizontal. With this launch
angle, a skier attains a height of 13 m above the end of the ramp. What is the
skier’s launch speed?
22. E GO A space vehicle is coasting at a constant velocity of 21.0 m/s in the +y direction relative to a space station. The pilot of the vehicle fi res a RCS (reaction control system) thruster, which causes it to accelerate at 0.320 m/s2
in the +x direction. After 45.0 s, the pilot shuts off the RCS thruster. After the RCS thruster is turned off , fi nd (a) the magnitude and (b) the direction of the vehicle’s velocity relative to the space station. Express the direction as an
angle measured from the +y direction. 23. E SSM As preparation for this prob- lem, review Conceptual Example 9. The
drawing shows two planes each about to
drop an empty fuel tank. At the moment of
release each plane has the same speed of
135 m/s, and each tank is at the same height
of 2.00 km above the ground. Although the
speeds are the same, the velocities are dif-
ferent at the instant of release, because one
plane is fl ying at an angle of 15.0° above
the horizontal and the other is fl ying at an
angle of 15.0° below the horizontal. Find
the magnitude and direction of the velocity
with which the fuel tank hits the ground if it
is from (a) plane A and (b) plane B. In each part, give the directional angles with respect
to the horizontal.
24. E GO A criminal is escaping across a rooftop and runs off the roof ho- rizontally at a speed of 5.3 m/s, hoping to land on the roof of an adjacent
building. Air resistance is negligible. The horizontal distance between the
two buildings is D, and the roof of the adjacent building is 2.0 m below the jumping-off point. Find the maximum value for D. 25. E On a spacecraft, two engines are turned on for 684 s at a moment when the velocity of the craft has x and y components of υ0x = 4370 m/s and υ0y = 6280 m/s. While the engines are fi ring, the craft undergoes a displace- ment that has components of x = 4.11 × 106 m and y = 6.07 × 106 m. Find the x and y components of the craft’s acceleration. 26. E GO In the absence of air resistance, a projectile is launched from and returns to ground level. It follows a trajectory similar to that shown in
Animated Figure 3.10 and has a range of 23 m. Suppose the launch speed is doubled, and the projectile is fi red at the same angle above the ground. What
is the new range?
27. E SSM A fi re hose ejects a stream of water at an angle of 35.0° above the horizontal. The water leaves the nozzle with a speed of 25.0 m/s. Assuming
PROBLEM 23
15°
15°
Fuel tank
Plane A
Plane B
76 CHAPTER 3 Kinematics in Two Dimensions
that the water behaves like a projectile, how far from a building should the
fi re hose be located to hit the highest possible fi re?
28. E Available on WileyPLUS. 29. E A major-league pitcher can throw a baseball in excess of 41.0 m/s. If a ball is thrown horizontally at this speed, how much will it drop by the time
it reaches a catcher who is 17.0 m away from the point of release?
30. E A quarterback claims that he can throw the football a horizontal dis- tance of 183 m (200 yd). Furthermore, he claims that he can do this by launch-
ing the ball at the relatively low angle of 30.0° above the horizontal. To evaluate
this claim, determine the speed with which this quarterback must throw the ball.
Assume that the ball is launched and caught at the same vertical level and that
air resistance can be ignored. For comparison, a baseball pitcher who can ac-
curately throw a fastball at 45 m/s (100 mph) would be considered exceptional.
31. E SSM An eagle is fl ying horizontally at 6.0 m/s with a fi sh in its claws. It accidentally drops the fi sh. (a) How much time passes before the fi sh’s speed doubles? (b) How much additional time would be required for the fi sh’s speed to double again?
32. E GO The highest barrier that a projectile can clear is 13.5 m, when the projectile is launched at an angle of 15.0° above the horizontal. What is the
projectile’s launch speed?
33. E Consult Multiple-Concept Example 4 for background before begin- ning this problem. Suppose the water at the top of Niagara Falls has a hori-
zontal speed of 2.7 m/s just before it cascades over the edge of the falls. At
what vertical distance below the edge does the velocity vector of the water
point downward at a 75° angle below the horizontal?
34. E MMH On a distant planet, golf is just as popular as it is on earth. A golfer tees off and drives the ball 3.5 times as far as he would have on earth,
given the same initial velocities on both planets. The ball is launched at a
speed of 45 m/s at an angle of 29° above the horizontal. When the ball lands,
it is at the same level as the tee. On the distant planet, what are (a) the max- imum height and (b) the range of the ball? 35. E CHALK A rocket is fi red at a speed of 75.0 m/s from ground level, at an angle of 60.0° above the horizontal. The rocket is fi red toward an
11.0-m-high wall, which is located 27.0 m away. The rocket attains its launch
speed in a negligibly short period of time, after which its engines shut down
and the rocket coasts. By how much does the rocket clear the top of the wall?
36. E A rifl e is used to shoot twice at a target, using identical cartridges. The fi rst time, the rifl e is aimed parallel to the ground and directly at the
center of the bull’s-eye. The bullet strikes the target at a distance of HA below the center, however. The second time, the rifl e is similarly aimed, but from
twice the distance from the target. This time the bullet strikes the target at a
distance of HB below the center. Find the ratio HB/HA. 37. M SSM An airplane with a speed of 97.5 m/s is climbing upward at an angle of 50.0° with respect to the horizontal. When the plane’s altitude is
732 m, the pilot releases a package. (a) Calculate the distance along the ground, measured from a point directly beneath the point of release, to where
the package hits the earth. (b) Relative to the ground, determine the angle of the velocity vector of the package just before impact.
38. M V-HINT Multiple-Concept Example 4 deals with a situation similar to that presented here. A marble is thrown horizontally with a speed of 15 m/s
from the top of a building. When it strikes the ground, the marble has a velo-
city that makes an angle of 65° with the horizontal. From what height above
the ground was the marble thrown?
39. M V-HINT MMH Review Conceptual Example 5 before beginning this problem. You are traveling in a convertible with the top down. The car is
moving at a constant velocity of 25 m/s, due east along fl at ground. You
throw a tomato straight upward at a speed of 11 m/s. How far has the car
moved when you get a chance to catch the tomato?
40. M V-HINT A diver springs upward from a diving board. At the instant she contacts the water, her speed is 8.90 m/s, and her body is extended at
an angle of 75.0° with respect to the horizontal surface of the water. At this
instant her vertical displacement is −3.00 m, where downward is the negative
direction. Determine her initial velocity, both magnitude and direction.
41. M GO MMH A soccer player kicks the ball toward a goal that is 16.8 m in front of him. The ball leaves his foot at a speed of 16.0 m/s and an angle
of 28.0° above the ground. Find the speed of the ball when the goalie catches
it in front of the net.
42. M V-HINT In the javelin throw at a track-and-fi eld event, the javelin is launched at a speed of 29 m/s at an angle of 36° above the horizontal. As the
javelin travels upward, its velocity points above the horizontal at an angle
that decreases as time passes. How much time is required for the angle to be
reduced from 36° at launch to 18°?
43. M SSM An airplane is fl ying with a velocity of 240 m/s at an angle of 30.0° with the horizontal, as the drawing shows. When the altitude of the
plane is 2.4 km, a fl are is released from the plane. The fl are hits the target on
the ground. What is the angle θ?
PROBLEM 43 Target
2.4 km
Line of sight
30.0°
Path of flare
θ
0 = 240 m/sυ
44. M V-HINT A child operating a radio-controlled model car on a dock accidentally steers it off the edge. The car’s displacement 1.1 s after leaving
the dock has a magnitude of 7.0 m. What is the car’s speed at the instant it
drives off the edge of the dock?
45. M MMH After leaving the end of a ski ramp, a ski jumper lands downhill at a point that is displaced 51.0 m horizontally from the end of the ramp. His
velocity, just before landing, is 23.0 m/s and points in a direction 43.0° below
the horizontal. Neglecting air resistance and any lift he experiences while
airborne, fi nd his initial velocity (magnitude and direction) when he left the
end of the ramp. Express the direction as an angle relative to the horizontal.
46. M GO Stones are thrown horizontally with the same velocity from the tops of two diff erent buildings. One stone lands twice as far from the base of
the building from which it was thrown as does the other stone. Find the ratio
of the height of the taller building to the height of the shorter building.
47. H SSM The drawing shows an exaggerated view of a rifl e that has been “sighted in” for a 91.4-meter target. If the muzzle speed of the bullet is
υ0 = 427 m/s, what are the two possible angles θ1 and θ2 between the rifl e barrel and the horizontal such that the bullet will hit the target? One of
these angles is so large that it is never used in target shooting. (Hint: The following trigonometric identity may be useful: 2 sin θ cos θ = sin 2θ.)
91.4 m
0
θ
υ
PROBLEM 47
48. H MMH A projectile is launched from ground level at an angle of 12.0° above the horizontal. It returns to ground level. To what value should the
launch angle be adjusted, without changing the launch speed, so that the
range doubles?
Additional Problems 77
49. H SSM From the top of a tall building, a gun is fi red. The bullet leaves the gun at a speed of 340 m/s, parallel to the ground. As the drawing shows,
the bullet puts a hole in a window of another building and hits the wall that
faces the window. Using the data in the drawing, determine the distances D and H, which locate the point where the gun was fi red. Assume that the bullet does not slow down as it passes through the window.
340 m/s
H
D
Hole in window
Bullet in wall
0.50 m
6.9 m
PROBLEM 49
50. H Available on WileyPLUS. 51. H Available on WileyPLUS.
Section 3.4 Relative Velocity 52. E In a marathon race Chad is out in front, running due north at a speed of 4.00 m/s. John is 95 m behind him, running due north at a speed of 4.50
m/s. How long does it take for John to pass Chad?
53. E SSM A swimmer, capable of swimming at a speed of 1.4 m/s in still water (i.e., the swimmer can swim with a speed of 1.4 m/s relative to the wa-
ter), starts to swim directly across a 2.8-km-wide river. However, the current
is 0.91 m/s, and it carries the swimmer downstream. (a) How long does it take the swimmer to cross the river? (b) How far downstream will the swim- mer be upon reaching the other side of the river?
54. E GO Two friends, Barbara and Neil, are out rollerblading. With re- spect to the ground, Barbara is skating due south at a speed of 4.0 m/s. Neil
is in front of her. With respect to the ground, Neil is skating due west at a
speed of 3.2 m/s. Find Neil’s velocity (magnitude and direction relative to
due west), as seen by Barbara.
55. E Available on WileyPLUS. 56. E At some airports there are speed ramps to help passengers get from one place to another. A speed ramp is a moving conveyor belt on which you
can either stand or walk. Suppose a speed ramp has a length of 105 m and is
moving at a speed of 2.0 m/s relative to the ground. In addition, suppose you
can cover this distance in 75 s when walking on the ground. If you walk at the
same rate with respect to the speed ramp that you walk on the ground, how
long does it take for you to travel the 105 m using the speed ramp?
57. E You are in a hot-air balloon that, relative to the ground, has a velocity of 6.0 m/s in a direction due east. You see a hawk moving directly away from
the balloon in a direction due north. The speed of the hawk relative to you is
2.0 m/s. What are the magnitude and direction of the hawk’s velocity relative
to the ground? Express the directional angle relative to due east.
58. E GO On a pleasure cruise a boat is traveling relative to the water at a speed of 5.0 m/s due south. Relative to the boat, a passenger walks toward
the back of the boat at a speed of 1.5 m/s. (a) What are the magnitude and direction of the passenger’s velocity relative to the water? (b) How long does it take for the passenger to walk a distance of 27 m on the boat? (c) How long does it take for the passenger to cover a distance of 27 m on the water?
59. E SSM Available on WileyPLUS. 60. E GO The captain of a plane wishes to proceed due west. The cruising speed of the plane is 245 m/s relative to the air. A weather report indicates
that a 38.0-m/s wind is blowing from the south to the north. In what direc-
tion, measured with respect to due west, should the pilot head the plane?
61. M V-HINT A person looking out the window of a stationary train notices that raindrops are falling vertically down at a speed of 5.0 m/s relative to the
ground. When the train moves at a constant velocity, the raindrops make an
angle of 25° when they move past the window, as the drawing shows. How
fast is the train moving?
25°
PROBLEM 61
62. M MMH Available on WileyPLUS. 63. M SSM Mario, a hockey player, is skating due south at a speed of 7.0 m/s relative to the ice. A teammate passes the puck to him. The puck has a speed
of 11.0 m/s and is moving in a direction of 22° west of south, relative to
the ice. What are the magnitude and direction (relative to due south) of the
puck’s velocity, as observed by Mario?
64. H A jetliner can fl y 6.00 hours on a full load of fuel. Without any wind it fl ies at a speed of 2.40 × 102 m/s. The plane is to make a round-trip by
heading due west for a certain distance, turning around, and then heading due
east for the return trip. During the entire fl ight, however, the plane encounters
a 57.8-m/s wind from the jet stream, which blows from west to east. What is
the maximum distance that the plane can travel due west and just be able to
return home?
65. H SSM Available on WileyPLUS.
66. E Useful background for this problem can be found in Multiple-Concept Example 2. On a spacecraft two engines fi re for a time of 565 s. One gives
the craft an acceleration in the x direction of ax = 5.10 m/s2, while the other produces an acceleration in the y direction of ay = 7.30 m/s2. At the end of the fi ring period, the craft has velocity components of υx = 3775 m/s and υy = 4816 m/s. Find the magnitude and direction of the initial velocity. Express the direction as an angle with respect to the +x axis.
67. E A dolphin leaps out of the water at an angle of 35° above the hori- zontal. The horizontal component of the dolphin’s velocity is 7.7 m/s. Find
the magnitude of the vertical component of the velocity.
68. E A hot-air balloon is rising straight up with a speed of 3.0 m/s. A ballast bag is released from rest relative to the balloon at 9.5 m above the
ground. How much time elapses before the ballast bag hits the ground?
Additional Problems
78 CHAPTER 3 Kinematics in Two Dimensions
69. E CHALK A golf ball rolls off a horizontal cliff with an initial speed of 11.4 m/s. The ball falls a vertical distance of 15.5 m into a lake below.
(a) How much time does the ball spend in the air? (b) What is the speed υ of the ball just before it strikes the water?
70. E GO When chasing a hare along a fl at stretch of ground, a greyhound leaps into the air at a speed of 10.0 m/s, at an angle of 31.0° above the hori-
zontal. (a) What is the range of his leap and (b) for how much time is he in the air?
71. E SSM Multiple-Concept Example 4 provides useful background for this problem. A diver runs horizontally with a speed of 1.20 m/s off a plat-
form that is 10.0 m above the water. What is his speed just before striking
the water?
72. E GO A ball is thrown upward at a speed υ0 at an angle of 52° above the horizontal. It reaches a maximum height of 7.5 m. How high would this ball
go if it were thrown straight upward at speed υ0? 73. M MMH A golfer, standing on a fairway, hits a shot to a green that is elevated 5.50 m above the point where she is standing. If the ball leaves her
club with a velocity of 46.0 m/s at an angle of 35.0° above the ground, fi nd
the time that the ball is in the air before it hits the green.
74. M V-HINT Available on WileyPLUS. 75. M SSM As preparation for this problem, review Conceptual Example 9. The two stones described there have identical initial speeds of υ0 = 13.0 m/s and are thrown at an angle θ = 30.0°, one below the horizontal and one above the horizontal. What is the distance between the points where the stones strike the ground?
76. M GO Relative to the ground, a car has a velocity of 16.0 m/s, directed due north. Relative to this car, a truck has a velocity of 24.0 m/s, directed
52.0° north of east. What is the magnitude of the truck’s velocity relative to
the ground?
77. M V-HINT The lob in tennis is an eff ective tactic when your opponent is near the net. It consists of lofting the ball over his head, forcing him to
move quickly away from the net (see the drawing). Suppose that you lob
the ball with an initial speed of 15.0 m/s, at an angle of 50.0° above the
horizontal. At this instant your opponent is 10.0 m away from the ball. He
begins moving away from you 0.30 s later, hoping to reach the ball and
hit it back at the moment that it is 2.10 m above its launch point. With
what minimum average speed must he move? (Ignore the fact that he can
stretch, so that his racket can reach the ball before he does.)
10.0 m
15.0 m/s 2.10 m
50.0°
PROBLEM 77
78. H Available on WileyPLUS. 79. H Available on WileyPLUS. 80. M GO A baseball player hits a home run, and the ball lands in the left- fi eld seats, 7.5 m above the point at which it was hit. It lands with a velocity of
36 m/s at an angle of 28° below the horizontal (see the drawing). The positive
directions are upward and to the right in the drawing. Ignoring air resistance,
fi nd the magnitude and direction of the initial velocity with which the ball
leaves the bat.
+y
+x
= 36 m/s
x
y y = 7.5 m
28° 0y
0x
0
θ
υ υ
υ
υ
υ
υ
PROBLEM 80
A primary focus of this chapter has been projectile motion. These additional
problems serve as a review of the basic features of this type of motion.
81. M CHALK SSM Three balls are launched simultaneously, as in the fi gure. The red ball is launched at an initial velocity υ→0 directed at an angle θ above the horizontal. The blue ball is launched vertically with a speed of 10.0 m/s,
and the yellow ball is launched horizontally with a speed of 4.6 m/s. The blue
and red balls reach identical maximum heights and return to the ground at the
same time, and the red ball returns to the ground to meet the yellow ball at the
same place along the horizontal. Concepts: (i) Since the blue and red balls reach the same maximum height, what can be said about the y components of their velocities? (ii) Since the red and yellow balls travel equal distances
along the x direction in the same amount of time, what can be said about the x components of their initial velocities? Calculations: Find the launch speed υ0 and launch angle θ for the red ball.
10.0 m/s
4.6 m/s
y
hmax
x
v0
θ
PROBLEM 80
Concepts and Calculations Problems
Team Problems 79
82. M CHALK A projectile is launched from and returns to ground level, as the fi gure shows. There is no air resistance. The horizontal range of the projectile
is measured to be R = 175 m, and the horizontal component of the launch ve- locity is υ0x = +25 m/s. Concepts: (i) What is the fi nal value of the horizontal component υx of the projectile’s velocity? (ii) Can the time be determined for the horizontal part of the motion? (iii) Is the time for the horizontal part
of the motion the same as that for the vertical part? (iv) For the vertical part of
the motion, what is the displacement of the projectile? Calculations: Find the vertical component υ0y of the projectile.
PROBLEM 82
v0
0y
0x = +25 m/s
R = 175 m
+x
v0
+y
υ
υ
83. M A Water Balloon Battle. You are launching water balloons at a rival team using a large slingshot. The other team is set up on the opposite side of a
fl at-topped building that is 30.0 ft tall and 50.0 ft wide. Your reconnaissance
team has reported that the opposition is set up 10.0 m from the wall of the
building. Your balloon launcher is calibrated for launch speeds that can reach
as high as 100 mph at angles between 0 and 80.0° from the horizontal. Since
a direct shot is not possible (the opposing team is on the opposite side of the
building), you plan to splash the other team by making a balloon explode on
the ground near them. If your launcher is located 55.0 m from the building
(opposite side as the opposing team), what should your launch velocity be
(magnitude and direction) to land a balloon 5.0 meters beyond the opposing
team with maximum impact (i.e., maximum vertical speed)?
84. M A Motorcycle Jump. You are planning to make a jump with your motorcycle by driving over a ramp that will launch you at an angle of 30.0°
with respect to the horizontal. The front edge of the ramp on which you
are supposed to land, however, is 25.0 ft lower than the edge of the launch
ramp (i.e., your launch height). (a) Assuming a launch speed of 65 mph, at what horizontal distance from your launch point should the landing ramp be
placed? (b) In order to land smoothly, the angle of the landing ramp should match the direction of your velocity vector when you touch down. What
should be the angle of the landing ramp?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
4.1 Discuss the concepts of force and mass.
4.2 Define Newton’s first law of motion.
4.3 Define Newton’s second law of motion.
4.4 Apply Newton’s second law of motion in two dimensions.
4.5 Apply Newton’s third law of motion.
4.6 Identify types of forces.
4.7 Define Newton’s law of universal gravitation.
4.8 Solve problems using the normal force.
4.9 Solve problems involving friction.
4.10 Solve problems involving tension.
4.11 Apply Newton’s first law to equilibrium problems.
4.12 Apply Newton’s second law to nonequilibrium problems.
© S
to ck
tr ek
I m
ag es
CHAPTER 4
Forces and Newton’s Laws of Motion
In order to successfully land the planetary rover, Curiosity, on the surface of Mars, NASA scientists and engineers had to take into account many forces, such as the thrust from the “sky crane” rocket engines, the
tension in its towing cables, air resistance, and the weight of the rover due to the gravity on Mars, just to
name a few. This chapter will discuss how forces infl uence the motion of objects.
4.1 The Concepts of Force and Mass In common usage, a force is a push or a pull, as the examples in Figure 4.1 illustrate. In football, an off ensive lineman pushes against his opponent. The tow bar attached to
a speeding boat pulls a water skier. Forces such as those that push against the football
player or pull the skier are called contact forces, because they arise from the physical contact between two objects. There are circumstances, however, in which two objects
exert forces on one another even though they are not touching. Such forces are referred to
as noncontact forces or action-at-a-distance forces. One example of such a noncontact force occurs when a diver is pulled toward the earth because of the force of gravity. The
earth exerts this force even when it is not in direct contact with the diver. In Figure 4.1, arrows are used to represent the forces. It is appropriate to use arrows, because a force is
a vector quantity and has both a magnitude and a direction. The direction of the arrow
gives the direction of the force, and the length is proportional to its strength or magnitude.
The word mass is just as familiar as the word force. A massive supertanker, for instance, is one that contains an enormous amount of mass. As we will see in the next
section, it is diffi cult to set such a massive object into motion and diffi cult to bring it
to a halt once it is moving. In comparison, a penny does not contain much mass. The
80
4.2 Newton’s First Law of Motion 81
emphasis here is on the amount of mass, and the idea of direction is of no concern. Therefore,
mass is a scalar quantity.
During the seventeenth century, Isaac Newton, building on the work of Galileo, developed
three important laws that deal with force and mass. Collectively they are called “Newton’s laws of
motion” and provide the basis for understanding the eff ect that forces have on an object. Because
of the importance of these laws, a separate section will be devoted to each one.
4.2 Newton’s First Law of Motion
The First Law To gain some insight into Newton’s fi rst law, think about the game of ice hockey (Figure 4.2). If a player does not hit a stationary puck, it will remain at rest on the ice. After the puck is struck,
however, it coasts on its own across the ice, slowing down only slightly because of friction. Since
ice is very slippery, there is only a relatively small amount of friction to slow down the puck. In
fact, if it were possible to remove all friction and wind resistance, and if the rink were infi nitely
large, the puck would coast forever in a straight line at a constant speed. Left on its own, the puck
would lose none of the velocity imparted to it at the time it was struck. This is the essence of
Newton’s fi rst law of motion:
NEWTON’S FIRST LAW OF MOTION An object continues in a state of rest or in a state of motion at a constant velocity (constant speed in a constant direction), unless compelled to change that state by a net force.
In the fi rst law the phrase “net force” is crucial. Often, several forces act simultaneously on
a body, and the net force is the vector sum of all of them. Individual forces matter only to the extent that they contribute to the total. For instance, if friction and other opposing forces were ab-
sent, a car could travel forever at 30 m/s in a straight line, without using any gas after it had come
up to speed. In reality gas is needed, but only so that the engine can produce the necessary force
to cancel opposing forces such as friction. This cancellation ensures that there is no net force to
change the state of motion of the car.
When an object moves at a constant speed in a constant direction, its velocity is constant.
Newton’s fi rst law indicates that a state of rest (zero velocity) and a state of constant velocity
are completely equivalent, in the sense that neither one requires the application of a net force to
sustain it. The purpose served when a net force acts on an object is not to sustain the object’s velocity, but, rather, to change it.
Inertia and Mass A greater net force is required to change the velocity of some objects than of others. For instance,
a net force that is just enough to cause a bicycle to pick up speed will cause only an imperceptible
change in the motion of a freight train. In comparison to the bicycle, the train has a much greater
tendency to remain at rest. Accordingly, we say that the train has more inertia than the bicycle.
FIGURE 4.1 The arrow labeled F→ represents the force that acts on (a) the football player, (b) the water skier, and (c) the cliff diver.
F
D av
id D
er m
er /D
ia m
o n d I
m ag
es /G
et ty
I m
ag es
(a)
F
ag e
fo to
st o ck
/S u p er
S to
ck
(b)
F
Ik o n I
m ag
es /S
u p er
S to
ck
(c)
S co
tt G
ar d n er
/A P
/W id
e W
o rl
d P
h o to
s
FIGURE 4.2 The game of ice hockey can give some insight into Newton’s laws of motion.
82 CHAPTER 4 Forces and Newton’s Laws of Motion
Quantitatively, the inertia of an object is measured by its mass. The following defi nition of inertia and mass indicates why Newton’s fi rst law is sometimes called the law of inertia:
DEFINITION OF INERTIA AND MASS Inertia is the natural tendency of an object to remain at rest or in motion at a constant velocity. The mass of an object is a quantitative measure of inertia. SI Unit of Inertia and Mass: kilogram (kg)
The SI unit for mass is the kilogram (kg), whereas the units in the CGS system and the BE
system are the gram (g) and the slug (sl), respectively. Conversion factors between these units are
given on the page facing the inside of the front cover. Interactive Figure 4.3 gives the typical masses of various objects, ranging from a penny to a supertanker. The larger the mass, the greater
is the inertia. Often the words “mass” and “weight” are used interchangeably, but this is incorrect.
Mass and weight are diff erent concepts, and Section 4.7 will discuss the distinction between them.
THE PHYSICS OF . . . seat belts. Figure 4.4 shows a useful application of inertia. Auto- mobile seat belts unwind freely when pulled gently, so they can be buckled. But in an accident, they
hold you safely in place. One seat-belt mechanism consists of a ratchet wheel, a locking bar, and a
pendulum. The belt is wound around a spool mounted on the ratchet wheel. While the car is at rest
or moving at a constant velocity, the pendulum hangs straight down, and the locking bar rests ho-
rizontally, as the gray part of the drawing shows. Consequently, nothing prevents the ratchet wheel
from turning, and the seat belt can be pulled out easily. When the car suddenly slows down in an ac-
cident, however, the relatively massive lower part of the pendulum keeps moving forward because
of its inertia. The pendulum swings on its pivot into the position shown in color and causes the
locking bar to block the rotation of the ratchet wheel, thus preventing the seat belt from unwinding.
An Inertial Reference Frame Newton’s fi rst law (and also the second law) can appear to be invalid to certain observers. Sup-
pose, for instance, that you are a passenger riding in a friend’s car. While the car moves at a con-
stant speed along a straight line, you do not feel the seat pushing against your back to any unusual
extent. This experience is consistent with the fi rst law, which indicates that in the absence of a net
force you should move with a constant velocity. Suddenly the driver fl oors the gas pedal. Imme-
diately you feel the seat pressing against your back as the car accelerates. Therefore, you sense
that a force is being applied to you. The fi rst law leads you to believe that your motion should
change, and, relative to the ground outside, your motion does change. But relative to the car, you can see that your motion does not change, because you remain stationary with respect to the car. Clearly, Newton’s fi rst law does not hold for observers who use the accelerating car as a frame of
reference. As a result, such a reference frame is said to be noninertial. All accelerating reference frames are noninertial. In contrast, observers for whom the law of inertia is valid are said to be
using inertial reference frames for their observations, as defi ned below:
DEFINITION OF AN INERTIAL REFERENCE FRAME An inertial reference frame is one in which Newton’s law of inertia is valid.
The acceleration of an inertial reference frame is zero, so it moves with a constant velocity. All
of Newton’s laws of motion are valid in inertial reference frames, and when we apply these laws,
we will be assuming such a reference frame. In particular, the earth itself is a good approximation
of an inertial reference frame.
Check Your Understanding
(The answer is given at the end of the book.) 1. Which of the following statements can be explained by Newton’s fi rst law? (A): When your car sud-
denly comes to a halt, you lunge forward. (B): When your car rapidly accelerates, you are pressed
backward against the seat. (a) Neither A nor B (b) Both A and B (c) A but not B (d) B but not A
INTERACTIVE FIGURE 4.3 Typical masses of various objects.
IN GOD
WE TRUST
LIBERTY 1996
Penny (0.003 kg)
Book (2 kg)
Bicycle (15 kg)
Car (2000 kg)
Jetliner (1.2 x 105 kg)
Supertanker (1.5 x 108 kg)
Seat belt
Motion of car
Ratchet wheel
Locking bar
Pivots
Pendulum
FIGURE 4.4 Inertia plays a central role in one seat-belt mechanism. The gray part of the
drawing applies when the car is at rest or
moving at a constant velocity. The colored
parts show what happens when the car
suddenly slows down, as in an accident.
4.3 Newton’s Second Law of Motion 83
4.3 Newton’s Second Law of Motion Newton’s fi rst law indicates that if no net force acts on an object, then the velocity of the object
remains unchanged. The second law deals with what happens when a net force does act. Consider
a hockey puck once again. When a player strikes a stationary puck, he causes the velocity of the
puck to change. In other words, he makes the puck accelerate. The cause of the acceleration is the
force that the hockey stick applies. As long as this force acts, the velocity increases, and the puck
accelerates. Now, suppose another player strikes the puck and applies twice as much force as the
fi rst player does. The greater force produces a greater acceleration. In fact, if the friction between
the puck and the ice is negligible, and if there is no wind resistance, the acceleration of the puck is
directly proportional to the force. Twice the force produces twice the acceleration. Moreover, the
acceleration is a vector quantity, just as the force is, and points in the same direction as the force.
Often, several forces act on an object simultaneously. Friction and wind resistance, for in-
stance, do have some eff ect on a hockey puck. In such cases, it is the net force, or the vector sum
of all the forces acting, that is important. Mathematically, the net force is written as ∑F →
, where
the Greek capital letter ∑ (sigma) denotes the vector sum. Newton’s second law states that the
acceleration is proportional to the net force acting on the object.
In Newton’s second law, the net force is only one of two factors that determine the accel-
eration. The other is the inertia or mass of the object. After all, the same net force that imparts
an appreciable acceleration to a hockey puck (small mass) will impart very little acceleration to
a semitrailer truck (large mass). Newton’s second law states that for a given net force, the mag-
nitude of the acceleration is inversely proportional to the mass. Twice the mass means one-half
the acceleration, if the same net force acts on both objects. Thus, the second law shows how the
acceleration depends on both the net force and the mass, as given in Equation 4.1.
NEWTON’S SECOND LAW OF MOTION When a net external force ∑F
→ acts on an object of mass m, the acceleration a→ that results
is directly proportional to the net force and has a magnitude that is inversely proportional to the mass. The direction of the acceleration is the same as the direction of the net force.
a→ = ΣF →
m or ΣF→ = ma→ (4.1)
SI Unit of Force: kg · m/s2 = newton (N)
Note that the net force in Equation 4.1 includes only the forces that the environment exerts on
the object of interest. Such forces are called external forces. In contrast, internal forces are forces that one part of an object exerts on another part of the object and are not included in Equation 4.1.
According to Equation 4.1, the SI unit for force is the unit for mass (kg) times the unit for
acceleration (m/s2), or
SI unit for force = (kg)(m s2) = kg · m
s2
The combination of kg · m/s2 is called a newton (N) and is a derived SI unit, not a base unit; 1 newton = 1 N = 1 kg · m/s2.
In the CGS system, the procedure for establishing the unit of force is the same as with SI
units, except that mass is expressed in grams (g) and acceleration in cm/s2. The resulting unit for
force is the dyne; 1 dyne = 1 g · cm/s2. In the BE system, the unit for force is defi ned to be the pound (lb),* and the unit for acceleration
is ft/s2. With this procedure, Newton’s second law can then be used to obtain the BE unit for mass:
BE unit for force = lb = (unit for mass)(fts2) Unit for mass =
lb · s2 ft
*We refer here to the gravitational version of the BE system, in which a force of one pound is defi ned to be the pull of
the earth on a certain standard body at a location where the acceleration due to gravity is 32.174 ft/s2.
84 CHAPTER 4 Forces and Newton’s Laws of Motion
The combination of lb · s2/ft is the unit for mass in the BE system and is called the slug (sl); 1 slug = 1 sl = 1 lb · s2/ft.
Table 4.1 summarizes the various units for mass, acceleration, and force. Conversion factors between force units from diff erent systems are provided on the page facing the inside of the front
cover.
When using the second law to calculate the acceleration, it is necessary to determine the net
force that acts on the object. In this determination a free-body diagram helps enormously. A free- body diagram is a diagram that represents the object and the forces that act on it. Only the forces
that act on the object appear in a free-body diagram. Forces that the object exerts on its environment are not included. Example 1 illustrates the use of a free-body diagram.
TABLE 4.1 Units for Mass, Acceleration, and Force
System Mass Acceleration Force SI kilogram (kg) meter/second2 (m/s2) newton (N)
CGS gram (g) centimeter/second2 (cm/s2) dyne (dyn)
BE slug (sl) foot/second2 (ft/s2) pound (lb)
Check Your Understanding
(The answers are given at the end of the book.) 2. The net external force acting on an object is zero. Which one of the following statements is true?
(a) The object can only be stationary. (b) The object can only be traveling with a constant velocity. (c) The object can be either stationary or traveling with a constant velocity. (d) The object can only be traveling with a velocity that is changing.
EXAMPLE 1 Pushing a Stalled Car
Two people are pushing a stalled car, as Animated Figure 4.5a indicates. The mass of the car is 1850 kg. One person applies a force of 275 N to the
car, while the other applies a force of 395 N. Both forces act in the same
direction. A third force of 560 N also acts on the car, but in a direction
opposite to that in which the people are pushing. This force arises because
of friction and the extent to which the pavement opposes the motion of the
tires. Find the acceleration of the car.
Reasoning According to Newton’s second law, the acceleration is the net force divided by the mass of the car. To determine the net force, we
use the free-body diagram in Animated Figure 4.5b. In this diagram, the car is represented as a dot, and its motion is along the +x axis. The dia- gram makes it clear that the forces all act along one direction. Therefore,
they can be added as colinear vectors to obtain the net force.
Problem-Solving Insight The direction of the acceleration is always the same as the direction of the net force.
Solution From Equation 4.1, the acceleration is a = (∑F)/m. The net force is
ΣF = +275 N + 395 N − 560 N = +110 N
The acceleration can now be obtained:
a = ΣF m
= +110 N
1850 kg = +0.059 m/s2 (4.1)
The plus sign indicates that the acceleration points along the +x axis, in the same direction as the net force.
ANIMATED FIGURE 4.5 (a) Two people push a stalled car. A force created by friction and the pavement opposes their eff orts. (b) A free-body diagram that shows the horizontal forces acting on the car.
+x
+y
560 N 395 N
275 N
(b) Free-body diagram of the car(a)
Opposing force = 560 N
275 N
395 N
4.4 The Vector Nature of Newton’s Second Law of Motion 85
3. In Case A an object is moving straight downward with a constant speed of 9.80 m/s, while in Case B an object is moving straight downward with a constant acceleration of magnitude 9.80 m/s2. Which one of the following is true? (a) A nonzero net external force acts on the object in both cases. (b) A nonzero net external force acts on the object in neither case. (c) A nonzero net external force acts on the object in Case A only. (d) A nonzero net external force acts on the object in Case B only.
4.4 The Vector Nature of Newton’s Second Law of Motion When a football player throws a pass, the direction of the force he applies to the ball is important.
Both the force and the resulting acceleration of the ball are vector quantities, as are all forces and
accelerations. The directions of these vectors can be taken into account in two dimensions by
using x and y components. The net force ∑F →
in Newton’s second law has components ∑Fx and ∑Fy, while the acceleration a→ has components ax and ay. Consequently, Newton’s second law, as expressed in Equation 4.1, can be written in an equivalent form as two equations, one for the x components and one for the y components:
ΣFx = max (4.2a)
ΣFy = may (4.2b)
This procedure is similar to that employed in Chapter 3 for the equations of two-
dimensional kinematics (see Table 3.1). The components in Equations 4.2a and 4.2b are scalar components and will be either positive or negative numbers, depending on whether they point
along the positive or negative x or y axis. The remainder of this section deals with examples that show how these equations are used.
EXAMPLE 2 Applying Newton’s Second Law Using Components
(a)
FIGURE 4.6 (a) A man is paddling a raft, as in Examples 2 and 3. (b) The free-body diagram shows the forces P→ and A→ that act on the raft. Forces acting on the raft in a direction perpendicular to the surface of the water play no role in the examples and are omitted for clarity. (c) The raft’s acceleration components ax and ay. (d) In 65 s, the components of the raft’s displacement are x = 48 m and y = 23 m.
A man is stranded on a raft (mass of man and raft = 1300 kg), as shown
in Figure 4.6a. By paddling, he causes an average force P →
of 17 N to be
applied to the raft in a direction due east (the +x direction). The wind also exerts a force A→ on the raft. This force has a magnitude of 15 N and points 67° north of east. Ignoring any resistance from the water, fi nd the x and y components of the raft’s acceleration.
Reasoning Since the mass of the man and the raft is known, Newton’s second law can be used to determine the acceleration components from the
given forces. According to the form of the second law in Equations 4.2a
and 4.2b, the acceleration component in a given direction is the com-
ponent of the net force in that direction divided by the mass. As an aid
in determining the components ∑Fx and ∑Fy of the net force, we use the
+x
+y
+x
+y
A sin 67°
A = 15 N
P = 17 N
A cos 67°
67°
A
Free-body diagram of the raft
N
S
EW
(b)
+x
ax
ay
+y
(c)
x = 48x m
y = 23 m
+x
+y
(d )
86 CHAPTER 4 Forces and Newton’s Laws of Motion
Check Your Understanding
(The answers are given at the end of the book.) 4. Newton’s second law indicates that when a net force acts on an object, it must accelerate. Does this mean
that when two or more forces are applied to an object simultaneously, it must accelerate?
5. All of the following, except one, cause the acceleration of an object to double. Which one is the excep- tion? (a) All forces acting on the object double. (b) The net force acting on the object doubles. (c) Both the net force acting on the object and the mass of the object double. (d) The net force acting on the object remains the same, while the mass of the object is reduced by a factor of two.
4.5 Newton’s Third Law of Motion Imagine you are in a football game. You line up facing your opponent, the ball is snapped, and
the two of you crash together. No doubt, you feel a force. But think about your opponent. He too
feels something, for while he is applying a force to you, you are applying a force to him. In other
words, there isn’t just one force on the line of scrimmage; there is a pair of forces. Newton was
the fi rst to realize that all forces occur in pairs and there is no such thing as an isolated force,
existing all by itself. His third law of motion deals with this fundamental characteristic of forces.
NEWTON’S THIRD LAW OF MOTION Whenever one object exerts a force on a second object, the second object exerts an oppositely directed force of equal magnitude on the fi rst object.
free-body diagram in Figure 4.6b. In this diagram, the directions due east and due north are the +x and +y directions, respectively.
Solution Figure 4.6b shows the force components:
Force x Component y Component
P→ +17 N 0 N
A→ +(15 N)cos 67° = +6 N +(15 N)sin 67° = +14 N
ΣFx = +17 N + 6 N = +23 N ΣFy = +14 N
The plus signs indicate that ∑Fx points in the direction of the +x axis and ∑Fy points in the direction of the +y axis. The x and y components of the acceleration point in the directions of ∑Fx and ∑Fy, respectively, and can now be calculated:
ax = ΣFx m
= +23 N
1300 kg = +0.018 m/s2 (4.2a)
ay = ΣFy
m =
+14 N
1300 kg = +0.011 m/s2 (4.2b)
These acceleration components are shown in Figure 4.6c.
EXAMPLE 3 The Displacement of a Raft
At the moment that the forces P→ and A→ begin acting on the raft in Example 2, the velocity of the raft is 0.15 m/s, in a direction due east
(the +x direction). Assuming that the forces are maintained for 65 s, fi nd the x and y components of the raft’s displacement during this time interval.
Reasoning Once the net force acting on an object and the object’s mass have been used in Newton’s second law to determine the acceleration, it
becomes possible to use the equations of kinematics to describe the res-
ulting motion. We know from Example 2 that the acceleration compon-
ents are ax = +0.018 m/s2 and ay = +0.011 m/s2, and it is given here that the initial velocity components are υ0x = +0.15 m/s and υ0y = 0 m/s. Thus,
Equation 3.5a (x = 𝜐0x t + 1
2axt2) and Equation 3.5b (y = 𝜐0y t + 1
2ay t2) can be used with t = 65 s to determine the x and y components of the raft’s displacement.
Solution According to Equations 3.5a and 3.5b, the x and y components of the displacement are
x = 𝜐0xt + 1
2 axt 2 = (0.15 m /s)(65 s) + 1
2(0.018 m /s 2)(65 s)2 = 48 m
y = 𝜐0yt + 1
2 ayt 2 = (0 m /s)(65 s) + 1
2 (0.011 m /s 2)(65 s)2 = 23 m
Figure 4.6d shows the fi nal location of the raft.
4.5 Newton’s Third Law of Motion 87
The third law is often called the “action–reaction” law, because it is sometimes quoted as follows:
“For every action (force) there is an equal, but opposite, reaction.”
Figure 4.7 illustrates how the third law applies to an astronaut who is drifting just outside a spacecraft and who pushes on the spacecraft with a force P→. According to the third law, the spacecraft pushes back on the astronaut with a force −P→ that is equal in magnitude but opposite in direction. In Example 4, we examine the accelerations produced by each of these forces.
EXAMPLE 4 The Accelerations Produced by Action and Reaction Forces
Suppose that the mass of the spacecraft in Figure 4.7 is mS = 11 000 kg and that the mass of the astronaut is mA = 92 kg. In addition, assume that the astronaut pushes with a force of P→ = +36 N on the spacecraft. Find the accelerations of the spacecraft and the astronaut.
Reasoning Consistent with Newton’s third law, when the astronaut applies the force P→ = +36 N to the spacecraft, the spacecraft applies a reaction force −P→ = −36 N to the astronaut. As a result, the spacecraft and the astronaut accelerate in opposite directions. Although the action and
reaction forces have the same magnitude, they do not create accelerations
of the same magnitude, because the spacecraft and the astronaut have
diff erent masses. According to Newton’s second law, the astronaut,
having a much smaller mass, will experience a much larger accelera-
tion. In applying the second law, we note that the net force acting on
the spacecraft is ∑F→ = P→ , while the net force acting on the astronaut is ∑F→ = −P→.
Problem-Solving Insight Even though the magnitudes of the action and reaction forces are always equal, these forces do not necessarily produce accelerations that have equal magnitudes, since each force acts on a diff erent object that may have a diff erent mass.
Solution Using the second law, we fi nd that the acceleration of the spacecraft is
a →S = P →
mS =
+36 N
11 000 kg = +0.0033 m/s2
The acceleration of the astronaut is
a →A = −P → mA
= −36 N
92 kg = −0.39 m/s2
–P +P
FIGURE 4.7 The astronaut pushes on the spacecraft with a force +P→. According to Newton’s third law, the spacecraft simultaneously pushes back on the astronaut with
a force −P→.
Mechanism for actuating trailer brakes
FIGURE 4.8 Some rental trailers include an automatic brake-actuating mechanism.
THE PHYSICS OF . . . automatic trailer brakes. There is a clever application of Newton’s third law in some rental trailers. As Figure 4.8 illustrates, the tow bar connecting the trailer to the rear bumper of a car contains a mechanism that can automatically actuate brakes on
the trailer wheels. This mechanism works without the need for electrical connections between the
car and the trailer. When the driver applies the car brakes, the car slows down. Because of inertia,
however, the trailer continues to roll forward and begins pushing against the bumper. In reaction,
the bumper pushes back on the tow bar. The reaction force is used by the mechanism in the tow
bar to “push a brake pedal” for the trailer.
88 CHAPTER 4 Forces and Newton’s Laws of Motion
Check Your Understanding
(The answer is given at the end of the book.) 6. A father and his seven-year-old daughter are facing each other on ice skates. With their hands, they
push off against one another. Which one or more of the following statements is (are) true? (a) Each experiences an acceleration that has a diff erent magnitude. (b) Each experiences an acceleration of the same magnitude. (c) Each experiences a pushing force that has a diff erent magnitude. (d) Each experi- ences a pushing force that has the same magnitude.
4.6 Types of Forces: An Overview Newton’s three laws of motion make it clear that forces play a central role in determining the
motion of an object. In the next four sections some common forces will be discussed: the grav-
itational force (Section 4.7), the normal force (Section 4.8), frictional forces (Section 4.9), and
the tension force (Section 4.10). In later chapters, we will encounter still others, such as electric
and magnetic forces. It is important to realize that Newton’s second law is always valid, regard-
less of which of these forces may act on an object. One does not have a diff erent law for every
type of common force. Thus, we need only to determine what forces are acting on an object, add
them together to form the net force, and then use Newton’s second law to determine the object’s
acceleration.
In nature there are two general types of forces, fundamental and nonfundamental. Funda-
mental forces are the ones that are truly unique, in the sense that all other forces can be explained
in terms of them. Only three fundamental forces have been discovered:
1. Gravitational force 2. Strong nuclear force 3. Electroweak force The gravitational force is discussed in the next section. The strong nuclear force plays a primary
role in the stability of the nucleus of the atom (see Section 31.2). The electroweak force is a
single force that manifests itself in two ways (see Section 32.6). One manifestation is the elec-
tromagnetic force that electrically charged particles exert on one another (see Sections 18.5,
21.2, and 21.8). The other manifestation is the so-called weak nuclear force that plays a role in
the radioactive disintegration of certain nuclei (see Section 31.5).
Except for the gravitational force, all of the forces discussed in this chapter are nonfunda-
mental, because they are related to the electromagnetic force. They arise from the interactions
between the electrically charged particles that comprise atoms and molecules. Our understanding
of which forces are fundamental, however, is continually evolving. For instance, in the 1860s and
1870s James Clerk Maxwell showed that the electric force and the magnetic force could be ex-
plained as manifestations of a single electromagnetic force. Then, in the 1970s, Sheldon Glashow
(1932– ), Abdus Salam (1926–1996), and Steven Weinberg (1933– ) presented the theory that
explains how the electromagnetic force and the weak nuclear force are related to the electroweak
force. They received a Nobel Prize in 1979 for their achievement. Today, eff orts continue that
have the goal of further reducing the number of fundamental forces.
4.7 The Gravitational Force
Newton’s Law of Universal Gravitation Objects fall downward because of gravity, and Chapters 2 and 3 discuss how to describe the
eff ects of gravity by using a value of g = 9.80 m/s2 for the downward acceleration it causes. However, nothing has been said about why g is 9.80 m/s2. The reason is fascinating, as we will see later in this section.
4.7 The Gravitational Force 89
The acceleration due to gravity is like any other acceleration, and Newton’s second law
indicates that it must be caused by a net force. In addition to his famous three laws of motion,
Newton also provided a coherent understanding of the gravitational force. His “law of universal gravitation” is stated as follows:
NEWTON’S LAW OF UNIVERSAL GRAVITATION Every particle in the universe exerts an attractive force on every other particle. A particle is a piece of matter, small enough in size to be regarded as a mathematical point. For two particles that have masses m1 and m2 and are separated by a distance r, the force that each exerts on the other is directed along the line joining the particles (see Figure 4.9) and has a magnitude given by
F = G m1m2
r2 (4.3)
The symbol G denotes the universal gravitational constant, whose value is found exper- imentally to be G = 6.674 × 10−11 N · m2/kg2
The constant G that appears in Equation 4.3 is called the universal gravitational constant, because it has the same value for all pairs of particles anywhere in the universe, no matter what
their separation. The value for G was fi rst measured in an experiment by the English scientist Henry Cavendish (1731–1810), more than a century after Newton proposed his law of universal
gravitation.
To see the main features of Newton’s law of universal gravitation, look at the two particles
in Figure 4.9. They have masses m1 and m2 and are separated by a distance r. In the picture, it is assumed that a force pointing to the right is positive. The gravitational forces point along the line
joining the particles and are
+F →
, the gravitational force exerted on particle 1 by particle 2
−F →
, the gravitational force exerted on particle 2 by particle 1
These two forces have equal magnitudes and opposite directions. They act on diff erent
bodies, causing them to be mutually attracted. In fact, these forces are an action–reaction pair, as
required by Newton’s third law. Example 5 shows that the magnitude of the gravitational force is
extremely small for ordinary values of the masses and the distance between them.
r
m1 m2–F+F
FIGURE 4.9 The two particles, whose masses are m1 and m2, are attracted by gravitational forces +F→ and −F→.
Moon
r
Earth
ME
ME
MM
MM +F –F
+F –F
FIGURE 4.10 The gravitational force that each uniform sphere of matter exerts on the
other is the same as if each sphere were a
particle with its mass concentrated at its
center. The earth (mass ME) and the moon (mass MM) approximate such uniform spheres.
EXAMPLE 5 Gravitational Attraction
What is the magnitude of the gravitational force that acts on each particle
in Figure 4.9, assuming m1 = 12 kg (approximately the mass of a bicycle), m2 = 25 kg, and r = 1.2 m?
Reasoning and Solution The magnitude of the gravitational force can be found using Equation 4.3:
F = G m1m2
r2 = (6.67 × 10 −11 N · m2 / kg2)
(12 kg)(25 kg)
(1.2 m)2 = 1.4 × 10−8 N
For comparison, you exert a force of about 1 N when pushing a doorbell,
so that the gravitational force is exceedingly small in circumstances such
as those here. This result is due to the fact that G itself is very small. However, if one of the bodies has a large mass, like that of the earth
(5.98 × 1024 kg), the gravitational force can be large.
As expressed by Equation 4.3, Newton’s law of gravitation applies only to particles. How-
ever, most familiar objects are too large to be considered particles. Nevertheless, the law of
universal gravitation can be applied to such objects with the aid of calculus. Newton was able
to prove that an object of fi nite size can be considered to be a particle for purposes of using
the gravitation law, provided the mass of the object is distributed with spherical symmetry
about its center. Thus, Equation 4.3 can be applied when each object is a sphere whose mass
is spread uniformly over its entire volume. Figure 4.10 shows this kind of application, as- suming that the earth and the moon are such uniform spheres of matter. In this case, r is the
90 CHAPTER 4 Forces and Newton’s Laws of Motion
distance between the centers of the spheres and not the distance between the outer surfaces. The gravitational forces that the spheres exert on each other are the same as if the entire mass of
each were concentrated at its center. Even if the objects are not uniform spheres, Equation 4.3
can be used to a good degree of approximation if the sizes of the objects are small relative to
the distance of separation r.
Weight The weight of an object exists because of the gravitational pull of the earth, according to the
following defi nition:
DEFINITION OF WEIGHT The weight of an object on or above the earth is the gravitational force that the earth exerts on the object. The weight always acts downward, toward the center of the earth. On or above another astronomical body, the weight is the gravitational force exerted on the object by that body. SI Unit of Weight: newton (N)
Using W for the magnitude of the weight,* m for the mass of the object, and ME for the mass of the earth, it follows from Equation 4.3 that
W = G M E m
r 2 (4.4)
Equation 4.4 and Figure 4.11 both emphasize that an object has weight whether or not it is resting on the earth’s surface, because the gravitational force is acting even when the distance r is not equal to the radius RE of the earth. However, the gravitational force becomes weaker as r increases, since r is in the denominator of Equation 4.4. Figure 4.12, for example, shows how the weight of the Hubble Space Telescope becomes smaller as the distance r from the center of the earth increases. In Example 6 the telescope’s weight is determined when it is on earth and
in orbit.
EXAMPLE 6 The Hubble Space Telescope
The mass of the Hubble Space Telescope is 11 600 kg. Determine the
weight of the telescope (a) when it was resting on the earth and (b) as it is in its orbit 598 km above the earth’s surface.
Reasoning The weight of the Hubble Space Telescope is the gravit- ational force exerted on it by the earth. According to Equation 4.4, the
weight varies inversely as the square of the radial distance r. Thus, we ex- pect the telescope’s weight on the earth’s surface (r smaller) to be greater than its weight in orbit (r larger).
Problem-Solving Insight When applying Newton’s gravit- ation law to uniform spheres of matter, remember that the distance r is between the centers of the spheres, not between the surfaces.
Solution (a) On the earth’s surface, the weight is given by Equation 4.4 with r = 6.38 × 106 m (the earth’s radius):
W = G ME m
r 2 =
(6.67 × 10−11 N · m2/kg2)(5.98 × 1024 kg)(11 600 kg) (6.38 × 106 m)2
W = 1.14 × 105 N
(b) When the telescope is 598 km above the surface, its distance from the center of the earth is
r = 6.38 × 106 m + 598 × 103 m = 6.98 × 106 m
The weight now can be calculated as in part (a), except that the new value
of r must be used: W = 0.950 × 105 N . As expected, the weight is less in orbit.
*Often, the word “weight” and the phrase “magnitude of the weight” are used interchangeably, even though weight is a
vector. Generally, the context makes it clear when the direction of the weight vector must be taken into account.
r
W
Object of mass m
RE
Mass of earth = ME
FIGURE 4.11 On or above the earth, the
weight W →
of an object is the gravitational
force exerted on the object by the earth.
5
0.2
0
0.4
0.6
0.8
1.0
10 15 20
r (× 106 m)
RE = 6.38 x 10 6 m
W (×
1 0
5 N
)
FIGURE 4.12 The weight of the Hubble Space Telescope decreases as the telescope
gets farther from the earth. The distance from
the center of the earth to the telescope is r.
4.7 The Gravitational Force 91
The space age has forced us to broaden our ideas about weight. For instance, an astronaut
weighs only about one-sixth as much on the moon as on the earth. To obtain his weight on the
moon from Equation 4.4, it is only necessary to replace ME by MM (the mass of the moon) and let r = RM (the radius of the moon).
Relation Between Mass and Weight Although massive objects weigh a lot on the earth, mass and weight are not the same quantity.
As Section 4.2 discusses, mass is a quantitative measure of inertia. As such, mass is an intrinsic
property of matter and does not change as an object is moved from one location to another. Weight,
in contrast, is the gravitational force acting on the object and can vary, depending on how far the
object is above the earth’s surface or whether it is located near another body such as the moon.
The relation between weight W and mass m can be written in two ways:
W = G ME m r2
(4.4)
W = m g (4.5)
Equation 4.4 is Newton’s law of universal gravitation, and Equation 4.5 is Newton’s second law
(net force equals mass times acceleration) incorporating the acceleration g due to gravity. These expressions make the distinction between mass and weight stand out. The weight of an object
whose mass is m depends on the values for the universal gravitational constant G, the mass ME of the earth, and the distance r. These three parameters together determine the acceleration g due to gravity. The specifi c value of g = 9.80 m/s2 applies only when r equals the radius RE of the earth. For larger values of r, as would be the case on top of a mountain, the eff ective value of g is less than 9.80 m/s2. The fact that g decreases as the distance r increases means that the weight likewise decreases. The mass of the object, however, does not depend on these eff ects and does
not change. Conceptual Example 7 further explores the diff erence between mass and weight. →
CONCEPTUAL EXAMPLE 7 Mass Versus Weight
A vehicle designed for exploring the moon’s surface (see Photo 4.1) is be- ing tested on earth, where it weighs roughly six times more than it will on
the moon. The acceleration of the vehicle along the ground is measured.
To achieve the same acceleration on the moon, will the required net force
be (a) the same as, (b) greater than, or (c) less than that on earth?
Reasoning Do not be misled by the fact that the vehicle weighs more on earth. The greater weight occurs only because the mass and radius of the
earth are diff erent from the mass and radius of the moon. In any event, in
Newton’s second law the net force is proportional to the vehicle’s mass,
not its weight.
Answers (b) and (c) are incorrect. According to Newton’s second law, for a given acceleration, the net force depends only on the mass. If the
required net force were greater or smaller on the moon than it is on
the earth, the implication would be that the vehicle’s mass is diff erent on
the moon than it is on earth, which is contrary to fact.
Answer (a) is correct. The net force ∑F →
required to accelerate the
vehicle is specifi ed by Newton’s second law as ∑F →
= ma→, where m is the vehicle’s mass and a→ is the acceleration. For a given acceleration, the net force depends only on the mass, which is the same on the moon as it is on
the earth. Therefore, the required net force is the same on the moon as it
is on the earth.
Related Homework: Problems 26, 105
PHOTO 4.1 On the moon the Lunar Roving Vehicle that astronaut Eugene Cernan is driving and the Lunar Excursion
Module (behind the Roving Vehicle) have the same masses
that they have on the earth. However, their weights are
diff erent on the moon than on the earth, as Conceptual
Example 7 discusses.
N A
S A
/J o h n so
n S
p ac
e C
en te
r
92 CHAPTER 4 Forces and Newton’s Laws of Motion
Check Your Understanding
(The answers are given at the end of the book.) 7. When a body is moved from sea level to the top of a mountain, what changes: (a) the body’s mass,
(b) its weight, or (c) both its mass and its weight? 8. Object A weighs twice as much as object B at the same spot on the earth. Would the same be true at a
given spot on Mars?
9. Three particles have identical masses. Each particle experiences only the gravitational forces due to the other two particles. How should the particles be arranged so each one experiences a net gravitational
force that has the same magnitude? (a) On the corners of an equilateral triangle (b) On three of the four corners of a square (c) On the corners of a right triangle
10. Two objects with masses m1 and m2 are separated by a distance 2d (see CYU Figure 4.1). Mass m2 is greater than mass m1. A third object has a mass m3. All three objects are located on the same straight line. The net gravitational force acting on the third object is zero. Which one of the drawings correctly
represents the locations of the objects?
m1
m1 m1
m1 m2
m2 m2
m2m3
m3 m3
m3
dd dd
dd
(a) (b)
(c) (d)
dd
CYU FIGURE 4.1
4.8 The Normal Force The Definition and Interpretation of the Normal Force In many situations, an object is in contact with a surface, such as a tabletop. Because of the con-
tact, there is a force acting on the object. The present section discusses only one component of this
force, the component that acts perpendicular to the surface. The next section discusses the com-
ponent that acts parallel to the surface. The perpendicular component is called the normal force.
DEFINITION OF THE NORMAL FORCE The normal force FN
→ is one component of the force that a surface exerts on an object with which it is in contact—namely, the component that is perpendicular to the surface.
Figure 4.13 shows a block resting on a horizontal table and identifi es the two forces that act on the block, the weight W→ and the normal force FN
→ . To understand how an inanimate object, such as a
tabletop, can exert a normal force, think about what happens when you sit on a mattress. Your weight
causes the springs in the mattress to compress. As a result, the compressed springs exert an upward
force (the normal force) on you. In a similar manner, the weight of the block causes invisible “atomic
springs” in the surface of the table to compress, thus producing a normal force on the block.
Newton’s third law plays an important role in connection with the normal force. In
Figure 4.13, for instance, the block exerts a force on the table by pressing down on it. Consistent with the third law, the table exerts an oppositely directed force of equal magnitude on the block.
This reaction force is the normal force. The magnitude of the normal force indicates how hard the
two objects press against each other.
If an object is resting on a horizontal surface and there are no vertically acting forces except the
object’s weight and the normal force, the magnitudes of these two forces are equal; that is, FN = W. This is the situation in Figure 4.13. The weight must be balanced by the normal force for the object
FN
W
FIGURE 4.13 Two forces act on the block,
its weight W →
and the normal force FN →
exerted by the surface of the table.
4.8 The Normal Force 93
to remain at rest on the table. If the magnitudes of these forces
were not equal, there would be a net force acting on the block, and
the block would accelerate either upward or downward, in accord
with Newton’s second law.
If other forces in addition to W→ and FN →
act in the vertical
direction, the magnitudes of the normal force and the weight
are no longer equal. In Figure 4.14a, for instance, a box whose weight is 15 N is being pushed downward against a table. The
pushing force has a magnitude of 11 N. Thus, the total downward
force exerted on the box is 26 N, and this must be balanced by the
upward-acting normal force if the box is to remain at rest. In this
situation, then, the normal force is 26 N, which is considerably
larger than the weight of the box.
Figure 4.14b illustrates a diff erent situation. Here, the box is being pulled upward by a rope that applies a force of 11 N. The
net force acting on the box due to its weight and the rope is only
4 N, downward. To balance this force, the normal force needs to
be only 4 N. It is not hard to imagine what would happen if the
force applied by the rope were increased to 15 N—exactly equal
to the weight of the box. In this situation, the normal force would
become zero. In fact, the table could be removed, since the block
would be supported entirely by the rope. The situations in Figure 4.14 are consistent with the idea that the magnitude of the normal force indicates how hard two objects press against each other.
Clearly, the box and the table press against each other harder in part a of the picture than in part b. Like the box and the table in Figure 4.14, various parts of the human body press against
one another and exert normal forces. Example 8 illustrates the remarkable ability of the human
skeleton to withstand a wide range of normal forces.
FIGURE 4.14 (a) The normal force FN →
is greater than the weight of the box,
because the box is being pressed downward with an 11-N force. (b) The normal force is smaller than the weight, because the rope supplies an upward force of
11 N that partially supports the box.
11 N
W = 15 N (b)
FN = 4 N
11 N
FN = 26 N
W = 15 N (a)
EXAMPLE 8 BIO The Physics of the Human Skeleton
+x
+y
+x
+y
FN
FN
FN
FN
50 N
50 N
50 N
490 N
490 N
50 N
(b)(a) (c)
Seventh cervical vertebra
Free-body diagram Free-body diagram
FIGURE 4.15 (a) A young woman keeps her balance during a performance by China’s Sichuan Acrobatic group. A free-body diagram is shown for the standing performer’s body above the shoulders (b) before the act and (c) during the act. For convenience, the scales used for the vectors in parts b and c are diff erent.
In a circus balancing act, a woman performs a headstand on top of a
standing performer’s head, as Figure 4.15a illustrates. The woman weighs 490 N, and the standing performer’s head and neck weigh 50 N. It
is primarily the seventh cervical vertebra in the spine that supports all the
weight above the shoulders. What is the normal force that this vertebra
exerts on the neck and head of the standing performer (a) before the act and (b) during the act?
S u p ri
/R E
U T
E R
S /N
ew sc
o m
94 CHAPTER 4 Forces and Newton’s Laws of Motion
In summary, the normal force does not necessarily have the same magnitude as the weight of the
object. The value of the normal force depends on what other forces are present. It also depends on
whether the objects in contact are accelerating. In one situation that involves accelerating objects, the
magnitude of the normal force can be regarded as a kind of “apparent weight,” as we will now see.
Apparent Weight Usually, the weight of an object can be determined with the aid of a scale. However, even though
a scale is working properly, there are situations in which it does not give the correct weight. In
such situations, the reading on the scale gives only the “apparent” weight, rather than the gravit-
ational force or “true” weight. The apparent weight is the force that the object exerts on the scale
with which it is in contact.
To see the discrepancies that can arise between true weight and apparent weight, consider
the scale in the elevator in Interactive Figure 4.16. The reasons for the discrepancies will be explained shortly. A person whose true weight is 700 N steps on the scale. If the elevator is at
rest or moving with a constant velocity (either upward or downward), the scale registers the true
weight, as Interactive Figure 4.16a illustrates. If the elevator is accelerating, the apparent weight and the true weight are not equal. When
the elevator accelerates upward, the apparent weight is greater than the true weight, as Interactive Figure 4.16b shows. Conversely, if the elevator accelerates downward, as in part c, the apparent weight is less than the true weight. In fact, if the elevator falls freely, so its acceleration is equal to
the acceleration due to gravity, the apparent weight becomes zero, as part d indicates. In a situation such as this, where the apparent weight is zero, the person is said to be “weightless.” The apparent
weight, then, does not equal the true weight if the scale and the person on it are accelerating.
Reasoning To begin, we draw a free-body diagram for the neck and head of the standing performer. Before the act, there are only two forces,
the weight of the standing performer’s head and neck, and the normal
force. During the act, an additional force is present due to the woman’s
weight. In both cases, the upward and downward forces must balance for
the head and neck to remain at rest. This condition of balance will lead us
to values for the normal force.
Solution (a) Figure 4.15b shows the free-body diagram for the stand- ing performer’s head and neck before the act. The only forces acting are
the normal force FN →
and the 50-N weight. These two forces must balance
for the standing performer’s head and neck to remain at rest. Therefore,
the seventh cervical vertebra exerts a normal force of FN = 50 N .
(b) Figure 4.15c shows the free-body diagram that applies during the act. Now, the total downward force exerted on the standing performer’s
head and neck is 50 N + 490 N = 540 N, which must be balanced by the
upward normal force, so that FN = 540 N .
(a) No acceleration (v = constant) (b) Upward acceleration (c) Downward acceleration (d) Free-fall
0
700
0
W = 700 N
0
400
0
W = 700 N
a a
a = g
1000
W = 700 N W = 700 N
INTERACTIVE FIGURE 4.16 (a) When the elevator is not accelerating, the scale registers the true weight (W = 700 N) of the person. (b) When the elevator accelerates upward, the apparent weight (1000 N) exceeds the true weight. (c) When the elevator accelerates downward, the apparent weight (400 N) is less than the true weight. (d) The apparent weight is zero if the elevator falls freely—that is, if it falls with the acceleration due to gravity.
4.9 Static and Kinetic Frictional Forces 95
The discrepancies between true weight and apparent weight can be understood with the aid
of Newton’s second law. Figure 4.17 shows a free-body diagram of the person in the elevator. The two forces that act on him are the true weight W→ = mg→ and the normal force FN
→ exerted by
the platform of the scale. Applying Newton’s second law in the vertical direction gives
ΣFy = +FN − mg = ma
where a is the acceleration of the elevator and person. In this result, the symbol g stands for the magnitude of the acceleration due to gravity and can never be a negative quantity. However, the
acceleration a may be either positive or negative, depending on whether the elevator is accelerat- ing upward (+) or downward (−). Solving for the normal force FN shows that
FN = mg + ma (4.6)
In Equation 4.6, FN is the magnitude of the normal force exerted on the person by the scale. But in accord with Newton’s third law, FN is also the magnitude of the downward force that the person exerts on the scale—namely, the apparent weight.
Equation 4.6 contains all the features shown in Interactive Figure 4.16. If the elevator is not accelerating, a = 0 m/s2, and the apparent weight equals the true weight. If the elevator acceler- ates upward, a is positive, and the equation shows that the apparent weight is greater than the true weight. If the elevator accelerates downward, a is negative, and the apparent weight is less than the true weight. If the elevator falls freely, a = −g, and the apparent weight is zero. The apparent weight is zero because when both the person and the scale fall freely, they cannot push against one another.
In this text, when the weight is given, it is assumed to be the true weight, unless stated otherwise.
Check Your Understanding
(The answers are given at the end of the book.) 11. A stack of books whose true weight is 165 N is placed on a scale in an elevator. The scale reads 165 N.
From this information alone, can you tell whether the elevator is moving with a constant velocity of
2 m/s upward, is moving with a constant velocity of 2 m/s downward, or is at rest?
12. A 10-kg suitcase is placed on a scale that is in an elevator. In which direction is the elevator accelerating when the scale reads 75 N and when it reads 120 N? (a) Downward when it reads 75 N and upward when it reads 120 N (b) Upward when it reads 75 N and downward when it reads 120 N (c) Downward in both cases (d) Upward in both cases
13. You are standing on a scale in an elevator that is moving upward with a constant velocity. The scale reads 600 N. The following table shows fi ve options for what the scale reads when the elevator slows
down as it comes to a stop, when it is stopped, and when it picks up speed on its way back down. Which
one of the fi ve options correctly describes the scale’s readings? Note that the symbol < means “less
than” and > means “greater than.”
Option Elevator slows down as it comes to a halt
Elevator is stopped
Elevator picks up speed on its way back down
(a) > 600 N > 600 N > 600 N
(b) < 600 N 600 N < 600 N
(c) > 600 N 600 N < 600 N
(d) < 600 N < 600 N < 600 N
(e) < 600 N 600 N > 600 N
4.9 Static and Kinetic Frictional Forces When an object is in contact with a surface, there is a force acting on the object. The previous
section discusses the component of this force that is perpendicular to the surface, which is called
the normal force. When the object moves or attempts to move along the surface, there is also a
Apparent
weight
⏟ True
weight
⏟
+x
W = mg
FN
+y
FIGURE 4.17 A free-body diagram showing the forces acting on the person riding in the
elevator of Interactive Figure 4.16. W →
is the
true weight, and FN →
is the normal force exerted
on the person by the platform of the scale.
96 CHAPTER 4 Forces and Newton’s Laws of Motion
component of the force that is parallel to the surface. This parallel force component is called the
frictional force, or simply friction. In many situations considerable engineering eff ort is expended trying to reduce friction.
For example, oil is used to reduce the friction that causes wear and tear in the pistons and
cylinder walls of an automobile engine. Sometimes, however, friction is absolutely necessary.
Without friction, car tires could not provide the traction needed to move the car. In fact, the
raised tread on a tire is designed to maintain friction. On a wet road, the spaces in the tread
pattern (see Figure 4.18) provide channels for the water to collect and be diverted away. Thus, these channels largely prevent the water from coming between the tire surface and the road
surface, where it would reduce friction and allow the tire to skid.
Surfaces that appear to be highly polished can actually look quite rough when examined
under a microscope. Such an examination reveals that two surfaces in contact touch only at re-
latively few spots, as Figure 4.19 illustrates. The microscopic area of contact for these spots is substantially less than the apparent macroscopic area of contact between the surfaces—perhaps
thousands of times less. At these contact points the molecules of the diff erent bodies are close
enough together to exert strong attractive intermolecular forces on one another, leading to what
are known as “cold welds.” Frictional forces are associated with these welded spots, but the exact
details of how frictional forces arise are not well understood. However, some empirical relations
have been developed that make it possible to account for the eff ects of friction.
Interactive Figure 4.20 helps to explain the main features of the type of friction known as static friction. The block in this drawing is initially at rest on a table, and as long as there is no attempt to move the block, there is no static frictional force. Then, a horizontal force F→ is applied to the block by means of a rope. If F→ is small, as in part a, experience tells us that the block still does not move. Why? It does not move because the static frictional force f s
→ exactly cancels the
eff ect of the applied force. The direction of f s →
is opposite to that of F,→ and the magnitude of f s →
equals the magnitude of the applied force, f s = F. Increasing the applied force in Interactive Figure 4.20 by a small amount still does not cause the block to move. There is no movement because the static frictional force also increases by an amount that cancels out the increase in the
applied force (see part b of the drawing). If the applied force continues to increase, however, there comes a point when the block fi nally “breaks away” and begins to slide. The force just before
breakaway represents the maximum static frictional force f MAXs →
that the table can exert on the
block (see part c of the drawing). Any applied force that is greater than f MAXs →
cannot be balanced
by static friction, and the resulting net force accelerates the block to the right.
Experimental evidence shows that, to a good degree of approximation, the maximum
static frictional force between a pair of dry, unlubricated surfaces has two main character-
istics. It is independent of the apparent macroscopic area of contact between the objects,
provided that the surfaces are hard or nondeformable. For instance, in Figure 4.21 the max- imum static frictional force that the surface of the table can exert on a block is the same,
whether the block is resting on its largest or its smallest side. The other main characteristic
of f MAXs →
is that its magnitude is proportional to the magnitude of the normal force FN →
. As
Section 4.8 points out, the magnitude of the normal force indicates how hard two surfaces are
being pressed together. The harder they are pressed, the larger is f s MAX, presumably because the number of “cold-welded,” microscopic contact points is increased. Equation 4.7 expresses
the proportionality between f sMAX and FN with the aid of a proportionality constant μs, which is called the coeffi cient of static friction.
STATIC FRICTIONAL FORCE The magnitude f s of the static frictional force can have any value from zero up to a max- imum value of f sMAX, depending on the applied force. In other words, f s ≤ f sMAX, where the symbol ≤ is read as “less than or equal to.” The equality holds only when f s attains its maximum value, which is f sMAX = μs FN (4.7)
In Equation 4.7, μs is the coeffi cient of static friction, and FN is the magnitude of the normal force.
It should be emphasized that Equation 4.7 relates only the magnitudes of f MAXs →
and FN →
, not the vectors themselves. This equation does not imply that the directions of the vectors are the same. In fact, f MAXs
→ is parallel to the surface, while FN
→ is perpendicular to it.
Microscopic contact points
FIGURE 4.19 Even when two highly polished surfaces are in contact, they touch
only at relatively few points.
F
No movement (a)
No movement (b)
When movement just begins (c)
F
fsMAX
F
fs
fs
INTERACTIVE FIGURE 4.20 (a) and (b) Applying a small force F→ to the block produces no movement, because the static
frictional force f s →
exactly balances the applied
force. (c) The block just begins to move when the applied force is slightly greater than the
maximum static frictional force f MAXs →
.
FIGURE 4.18 This photo, shot parallel to the road surface, shows a tire rolling under
wet conditions. The channels in the tire
collect and divert water away from the
regions where the tire contacts the surface,
thus providing better traction.
S to
ck sn
ap p
er /S
h u
tt er
st o
ck
4.9 Static and Kinetic Frictional Forces 97
The coeffi cient of static friction, being the ratio of the magnitudes of two forces
(μs = f sMAX/FN), has no units. Also, it depends on the type of material from which each surface is made (steel on wood, rubber on concrete, etc.), the condition of the surfaces (polished, rough,
etc.), and other variables such as temperature. Table 4.2 gives some typical values of μs for vari- ous surfaces. Example 9 illustrates the use of Equation 4.7 for determining the maximum static
frictional force. FIGURE 4.21 The maximum static frictional
force f MAXs →
would be the same, no matter
which side of the block is in contact with the
table.TABLE 4.2 Approximate Values of the Coefficients of Friction for Various Surfaces a
Materials Coefficient of
Static Friction, μs Coefficient of
Kinetic Friction, μk Glass on glass (dry) 0.94 0.4
Ice on ice (clean, 0 °C) 0.1 0.02
Rubber on dry concrete 1.0 0.8
Rubber on wet concrete 0.7 0.5
Steel on ice 0.1 0.05
Steel on steel (dry hard steel) 0.78 0.42
Teflon on Teflon 0.04 0.04
Wood on wood 0.35 0.3
a The last column gives the coefficients of kinetic friction, a concept that will be discussed shortly.
Analyzing Multiple -Concept Problems
EXAMPLE 9 The Force Needed to Start a Skier Moving
A skier is standing motionless on a horizontal patch of snow. She is hold-
ing onto a horizontal tow rope, which is about to pull her forward (see
Figure 4.22a). The skier’s mass is 59 kg, and the coeffi cient of static friction between the skis and snow is 0.14. What is the magnitude of the
maximum force that the tow rope can apply to the skier without causing
her to move?
Reasoning When the rope applies a relatively small force, the skier does not accelerate. The reason is that the static frictional force opposes
the applied force and the two forces have the same magnitude. We can
apply Newton’s second law in the horizontal direction to this situation.
In order for the rope to pull the skier forward, it must exert a force large
enough to overcome the maximum static frictional force acting on the skis. The magnitude of the maximum static frictional force depends on
the coeffi cient of static friction (which is known) and on the magnitude
of the normal force. We can determine the magnitude of the normal force
by using Newton’s second law, along with the fact that the skier does not
accelerate in the vertical direction.
Knowns and Unknowns The data for this problem are as follows:
Description Symbol Value Mass of skier m 59 kg
Coefficient of static friction μs 0.14
Unknown Variable Magnitude of maximum horizontal
force that tow rope can apply F ?
(a)
+y
+x
(b)
FN
mg
fs MAX
F
FIGURE 4.22 (a) Two forces act on the skier in the horizontal direction just
before she begins to move. (b) Two vertical forces act on the skier.
98 CHAPTER 4 Forces and Newton’s Laws of Motion
BIO THE PHYSICS OF . . . rock climbing. Static friction is often essential, as it is to the rock climber in Figure 4.23, for instance. She presses outward against the walls of the rock formation with her hands and feet to create suffi ciently large normal forces, so that the static
frictional forces help support her weight.
Once two surfaces begin sliding over one another, the static frictional force is no longer of any
concern. Instead, a type of friction known as kinetic* friction comes into play. The kinetic fric- tional force opposes the relative sliding motion. If you have ever pushed an object across a fl oor, you
may have noticed that it takes less force to keep the object sliding than it takes to get it going in the
fi rst place. In other words, the kinetic frictional force is usually less than the static frictional force.
*The word “kinetic” is derived from the Greek word kinetikos, meaning “pertaining to motion.”
Modeling the Problem
STEP 1 Newton’s Second Law (Horizontal Direction) Figure 4.22a shows the two hori- zontal forces that act on the skier just before she begins to move: the force F→ applied by the tow rope and the maximum static frictional force f MAXs
→ . Since the skier is standing motionless, she is
not accelerating in the horizontal or x direction, so ax = 0 m/s2. Applying Newton’s second law (Equation 4.2a) to this situation, we have
ΣFx = max = 0
Since the net force ∑Fx in the x direction is ∑Fx = +F − f sMAX, Newton’s second law can be writ- ten as +F − f sMAX = 0. Thus,
F = f sMAX
We do not know f sMAX, but its value will be determined in Steps 2 and 3.
STEP 2 The Maximum Static Frictional Force The magnitude f sMAX of the maximum static frictional force is related to the coeffi cient of static friction μs and the magnitude FN of the normal force by Equation 4.7:
f sMAX = μs FN (4.7)
We now substitute this result into Equation 1, as indicated in the right column. The coeffi cient
of static friction is known, but FN is not. An expression for FN will be obtained in the next step.
STEP 3 Newton’s Second Law (Vertical Direction) We can fi nd the magnitude FN of the normal force by noting that the skier does not accelerate in the vertical or y direction, so ay = 0 m/s2. Figure 4.22b shows the two vertical forces that act on the skier: the normal force FN
→ and
her weight mg→. Applying Newton’s second law (Equation 4.2b) in the vertical direction gives ΣFy = may = 0
The net force in the y direction is ∑Fy = +FN − mg, so Newton’s second law becomes +FN − mg = 0. Thus,
FN = mg
We now substitute this result into Equation 4.7, as shown at the right.
Solution Algebraically combining the results of the three steps, we have
F = f sMAX = μsFN = μsmg
The magnitude F of the maximum force is
F = μs mg = (0.14)(59 kg)(9.80 m /s2) = 81 N
If the force exerted by the tow rope exceeds this value, the skier will begin to accelerate forward.
Related Homework: Problems 44, 109, 118
STEP 1 STEP 2 STEP 3
?
F = f sMAX (1)
F = f sMAX (1)
f sMAX = μs FN (4.7)
FN = mg
?
F = f sMAX (1)
f sMAX = μs FN (4.7)
4.9 Static and Kinetic Frictional Forces 99
Experimental evidence indicates that the kinetic frictional force f k →
has three main charac-
teristics, to a good degree of approximation. It is independent of the apparent area of contact
between the surfaces (see Figure 4.21). It is independent of the speed of the sliding motion, if the speed is small. And last, the magnitude of the kinetic frictional force is proportional to the
magnitude of the normal force. Equation 4.8 expresses this proportionality with the aid of a pro-
portionality constant 𝜇k, which is called the coeffi cient of kinetic friction.
KINETIC FRICTIONAL FORCE The magnitude fk of the kinetic frictional force is given by
fk = μkFN (4.8)
In Equation 4.8, 𝜇k is the coeffi cient of kinetic friction, and FN is the magnitude of the normal force.
Equation 4.8, like Equation 4.7, is a relationship between only the magnitudes of the fric-
tional and normal forces. The directions of these forces are perpendicular to each other. Moreover,
like the coeffi cient of static friction, the coeffi cient of kinetic friction is a number without units
and depends on the type and condition of the two surfaces that are in contact. As indicated in
Table 4.2, values for 𝜇k are typically less than those for 𝜇s, refl ecting the fact that kinetic friction is generally less than static friction. The next example illustrates the eff ect of kinetic friction.
Analyzing Multiple-Concept Problems
EXAMPLE 10 Sled Riding
A sled and its rider are moving at a speed of 4.0 m/s along a
horizontal stretch of snow, as Figure 4.24a illustrates. The snow exerts a kinetic frictional force on the runners of the
sled, so the sled slows down and eventually comes to a s
top. The coeffi cient of kinetic friction is 0.050. What is the
displacement x of the sled?
Reasoning As the sled slows down, its velocity is decreas- ing. As our discussions in Chapters 2 and 3 indicate, the
changing velocity is described by an acceleration (which in
this case is a deceleration since the sled is slowing down).
Assuming that the acceleration is constant, we can use one
of the equations of kinematics from Chapter 3 to relate the
displacement to the initial and fi nal velocities and to the ac-
celeration. The acceleration of the sled is not given directly.
However, we can determine it by using Newton’s second
law of motion, which relates the acceleration to the net force
(which is the kinetic frictional force in this case) acting on
the sled and to the mass of the sled (plus rider).
Knowns and Unknowns The data for this problem are listed in the table:
0x = 4.0 m/sυ x = 0 m/sυ
+x
+y
FN
fk
W = mg
(b) Free-body diagram for the sled and rider
(a)
x
FIGURE 4.24 (a) The moving sled decelerates because of the kinetic frictional force. (b) Three forces act on the moving sled: the weight W
→ of the sled and its
rider, the normal force FN →
, and the kinetic frictional force fk →
. The free-body diagram
for the sled and rider shows these forces.
Description Symbol Value Comment Explicit Data Initial velocity υ0x +4.0 m/s Positive, because the velocity points in the +x direction. See the drawing.
Coefficient of kinetic friction μk 0.050
Implicit Data Final velocity υx 0 m/s The sled comes to a stop.
Unknown Variable Displacement x ?
FIGURE 4.23 In maneuvering her way up Devil’s Tower at Devil’s Tower National
Monument in Wyoming, this rock climber
uses the static frictional forces between her
hands and feet and the vertical rock walls to
help support her weight.
© René Robert/Collection Catherine Destivelle/Sygma/Getty
100 CHAPTER 4 Forces and Newton’s Laws of Motion
Modeling the Problem
STEP 1 Displacement To obtain the displacement x of the sled we will use Equation 3.6a from the equations of kinematics:
𝜐x 2 = 𝜐0x
2 + 2ax x
Solving for the displacement x gives the result shown at the right. This equation is useful because two of the variables, υ0x and υx, are known and the acceleration ax can be found by applying Newton’s second law to the accelerating sled (see Step 2).
STEP 2 Newton’s Second Law Newton’s second law, as given in Equation 4.2a, states that the acceleration ax is equal to the net force ΣFx divided by the mass m:
ax = ΣFx m
The free-body diagram in Figure 4.24b shows that the only force acting on the sled in the hori- zontal or x direction is the kinetic frictional force f k
→ . We can write this force as −fk, where f k is
the magnitude of the force and the minus sign indicates that it points in the −x direction. Since the net force is ΣFx = −f k, Equation 4.2a becomes
ax = −f k m
This result can now be substituted into Equation 1, as shown at the right.
STEP 3 Kinetic Frictional Force We do not know the magnitude f k of the kinetic frictional force, but we do know the coeffi cient of kinetic friction 𝜇k. According to Equation 4.8, the two
are related by
f k = μkFN (4.8)
where FN is the magnitude of the normal force. This relation can be substituted into Equation 2, as shown at the right. An expression for FN will be obtained in the next step.
STEP 4 Normal Force The magnitude FN of the normal force can be found by noting that the sled does not accelerate in the vertical or y direction (ay = 0 m/s2). Thus, Newton’s second law, as given in Equation 4.2b, becomes
ΣFy = may = 0 There are two forces acting on the sled in the y direction: the normal force FN
→ and its weight W
→
(see Figure 4.24b). Therefore, the net force in the y direction is
ΣFy = +FN − W
where W = mg (Equation 4.5). Thus, Newton’s second law becomes
+FN − mg = 0 or FN = mg
This result for FN can be substituted into Equation 4.8, as shown at the right.
Solution Algebraically combining the results of each step, we fi nd that
x = 𝜐x
2 − 𝜐0x 2
2ax =
𝜐x 2 − 𝜐0x
2
2( −fk m )
= 𝜐x
2 − 𝜐0x 2
2( −μkFN
m ) =
𝜐x 2 − 𝜐0x
2
2( −μk mg
m ) =
𝜐x 2 − 𝜐0x
2
2(−μkg)
Note that the mass m of the sled and rider is algebraically eliminated from the fi nal result. Thus, the displacement of the sled is
x = 𝜐x
2 − 𝜐0x 2
2(−μkg) =
(0 m/s)2 − (+4.0 m /s)2
2[−(0.050)(9.80 m/s2)] = +16 m
Related Homework: Problems 48, 112, 115
STEP 2STEP 1 STEP 3 STEP 4
x = 𝜐x
2 − 𝜐0x 2
2ax (1)
?
?
x = 𝜐x
2 − 𝜐0x 2
2ax (1)
ax = −f k m
(2)
x = 𝜐x
2 − 𝜐0x 2
2ax (1)
ax = −f k m
(2)
f k = μkFN (4.8)?
x = 𝜐x
2 − 𝜐0x 2
2ax (1)
ax = −f k m
(2)
f k = μkFN
(4.8)
FN = mg
4.10 The Tension Force 101
Static friction opposes the impending relative motion between two objects, while kinetic fric-
tion opposes the relative sliding motion that actually does occur. In either case, relative motion is opposed. However, this opposition to relative motion does not mean that friction prevents or
works against the motion of all objects. For instance, consider what happens when you walk. BIO THE PHYSICS OF . . . walking. Your foot exerts a force on the earth, and the
earth exerts a reaction force on your foot. This reaction force is a static frictional force, and it
opposes the impending backward motion of your foot, propelling you forward in the process.
Kinetic friction can also cause an object to move, all the while opposing relative motion, as it does
in Example 10. In this example the kinetic frictional force acts on the sled and opposes the relative
motion of the sled and the earth. Newton’s third law indicates, however, that since the earth exerts
the kinetic frictional force on the sled, the sled must exert a reaction force on the earth. In response,
the earth accelerates, but because of the earth’s huge mass, the motion is too slight to be noticed.
Check Your Understanding
(The answers are given at the end of the book.) 14. Suppose that the coeffi cients of static and kinetic friction have values such that μs = 1.4 μk for a crate in
contact with a cement fl oor. Which one of the following statements is true? (a) The magnitude of the static frictional force is always 1.4 times the magnitude of the kinetic frictional force. (b) The magnitude of the kinetic frictional force is always 1.4 times the magnitude of the static frictional force. (c) The mag- nitude of the maximum static frictional force is 1.4 times the magnitude of the kinetic frictional force.
15. A person has a choice of either pushing or pulling a sled at a constant velocity, as CYU Figure 4.2 illustrates. Friction is present. If the angle θ is the same in both cases, does it require less force to push or to pull the sled?
θ θ
CYU FIGURE 4.2
16. A box has a weight of 150 N and is being pulled across a horizontal fl oor by a force that has a mag- nitude of 110 N. The pulling force can point horizontally, or it can point above the horizontal at an
angle θ. When the pulling force points horizontally, the kinetic frictional force acting on the box is twice as large as when the pulling force points at the angle θ. Find θ.
17. A box rests on the fl oor of an elevator. Because of static friction, a force is required to start the box sliding across the fl oor when the elevator is (a) stationary, (b) accelerating upward, and (c) accelerating downward. Rank the forces required in these three situations in ascending order—that is, smallest fi rst.
4.10 The Tension Force Forces are often applied by means of cables or ropes that are used to pull an object. For instance,
Figure 4.25a shows a force T→ being applied to the right end of a rope attached to a box. Each particle in the rope in turn applies a force to its neighbor. As a result, the force is applied to the
box, as part b of the drawing shows. In situations such as that in Figure 4.25, we say that the force T→ is applied to the box be-
cause of the tension in the rope, meaning that the tension and the force applied to the box have
the same magnitude. However, the word “tension” is commonly used to mean the tendency of
the rope to be pulled apart. To see the relationship between these two uses of the word “tension,”
consider the left end of the rope, which applies the force T→ to the box. In accordance with Newton’s third law, the box applies a reaction force to the rope. The reaction force has the same
magnitude as T→ but is oppositely directed. In other words, a force −T→ acts on the left end of the rope. Thus, forces of equal magnitude act on opposite ends of the rope, as in Figure 4.25c, and tend to pull it apart.
In the previous discussion, we have used the concept of a “massless” rope (m = 0 kg) without saying so. In reality, a massless rope does not exist, but it is useful as an idealization when applying
T
(a)
T
(b)
T
–T
(c)
FIGURE 4.25 (a) A force T →
is being
applied to the right end of a rope. (b) The force is transmitted to the box. (c) Forces are applied to both ends of the rope. These
forces have equal magnitudes and opposite
directions.
102 CHAPTER 4 Forces and Newton’s Laws of Motion
Newton’s second law. According to the second law, a net force is required to accelerate an object
that has mass. In contrast, no net force is needed to accelerate a massless rope, since ΣF→ = ma→ and m = 0 kg. Thus, when a force T→ is applied to one end of a massless rope, none of the force is needed to accelerate the rope. As a result, the force T→ is also applied undiminished to the object attached at the other end, as we assumed in Figure 4.25.* If the rope had mass, however, some of the force T→ would have to be used to accelerate the rope. The force applied to the box would then be less than T→, and the tension would be diff erent at diff erent locations along the rope. In this text we will assume that a rope connecting one object to another is massless, unless stated otherwise.
The ability of a massless rope to transmit tension undiminished from one end to the other is not
aff ected when the rope passes around objects such as the pulley in Figure 4.26 (provided the pulley itself is massless and frictionless).
Check Your Understanding
(The answer is given at the end of the book.) 18. A rope is used in a tug-of-war between two teams of fi ve people each. Both teams are equally strong,
so neither team wins. An identical rope is tied to a tree, and the same ten people pull just as hard on the
loose end as they did in the contest. In both cases, the people pull steadily with no jerking. Which rope
sustains the greater tension, (a) the rope tied to the tree or (b) the rope in the tug-of-war, or (c) do the ropes sustain the same tension?
4.11 Equilibrium Applications of Newton’s Laws of Motion Have you ever been so upset that it took days to recover your “equilibrium”? In this context, the
word “equilibrium” refers to a balanced state of mind, one that is not changing wildly. In physics,
the word “equilibrium” also refers to a lack of change, but in the sense that the velocity of an
object isn’t changing. If its velocity doesn’t change, an object is not accelerating. Our defi nition
of equilibrium, then, is as follows:
DEFINITION OF EQUILIBRIUM†
An object is in equilibrium when it has zero acceleration.
Newton’s laws of motion apply whether or not an object is in equilibrium. For an
object in equilibrium the acceleration is zero (a→ = 0 m /s2) in Newton’s second law, and the present section presents several examples of this type. In the nonequilibrium case the acceleration
of the object is not zero (a→ ≠ 0 m /s2) in the second law, and Section 4.12 deals with these kinds of situations.
Since the acceleration is zero for an object in equilibrium, all of the acceleration components
are also zero. In two dimensions, this means that ax = 0 m/s2 and ay = 0 m/s2. Substituting these values into the second law (∑Fx = max and ∑Fy = may) shows that the x component and the y component of the net force must each be zero. In other words, the forces acting on an object in
equilibrium must balance. Thus, in two dimensions, the equilibrium condition is expressed by
two equations:
ΣFx = 0 (4.9a)
ΣFy = 0 (4.9b)
*If a rope is not accelerating, a→ is zero in the second law, and ΣF→ = ma→ = 0, regardless of the mass of the rope. Then, the rope can be ignored, no matter what mass it has.
†In this discussion of equilibrium we ignore rotational motion, which is discussed in Chapters 8 and 9. In
Section 9.2 a more complete treatment of the equilibrium of a rigid object is presented and takes into account the
concept of torque and the fact that objects can rotate.
T
–T
FIGURE 4.26 The force T→ applied at one end of a massless rope is transmitted
undiminished to the other end, even when
the rope bends around a pulley, provided the
pulley is also massless and friction is absent.
4.11 Equilibrium Applications of Newton’s Laws of Motion 103
In using Equations 4.9a and 4.9b to solve equilibrium problems, we will use the following
fi ve-step reasoning strategy:
REASONING STRATEGY Analyzing Equilibrium Situations 1. Select the object (often called the “system”) to which Equations 4.9a and 4.9b are to be
applied. It may be that two or more objects are connected by means of a rope or a cable. If so, it may be necessary to treat each object separately according to the following steps.
2. Draw a free-body diagram for each object chosen above. Be sure to include only forces that act on the object. Do not include forces that the object exerts on its environment.
3. Choose a set of x, y axes for each object and resolve all forces in the free-body diagram into components that point along these axes. Select the axes so that as many forces as possible point along one or the other of the two axes. Such a choice minimizes the calcu- lations needed to determine the force components.
4. Apply Equations 4.9a and 4.9b by setting the sum of the x components and the sum of the y components of the forces each equal to zero.
5. Solve the two equations obtained in Step 4 for the desired unknown quantities, remem- bering that two equations can yield answers for only two unknowns at most.
Example 11 illustrates how these steps are followed. It deals with a traction device in which three
forces act together to bring about the equilibrium.
Problem-Solving Insight Choose the orientation of the x, y axes for convenience. In Example 11, the axes have been ro- tated so the force F→ points along the x axis. Since F→ does not have a component along the y axis, the analysis is simplifi ed.
Solution Since the sum of the y components of the forces is zero, it follows that
ΣFy = +T1 sin 35° − T2 sin 35° = 0 (4.9b)
or T1 = T2. In other words, the magnitudes of the tension forces are equal. In addition, the sum of the x components of the forces is zero, so we have that
ΣFx = +T1 cos 35° + T2 cos 35° − F = 0 (4.9a)
Solving for F and letting T1 = T2 = T, we fi nd that F = 2T cos 35°. How- ever, the tension T in the rope is determined by the weight of the 2.2-kg object: T = mg, where m is its mass and g is the acceleration due to gravity. Therefore, the magnitude of F→ is F = 2T cos 35° = 2mg cos 35° = 2(2.2 kg)(9.80 m/s2) cos 35° = 35 N
EXAMPLE 11 BIO The Physics of Traction for the Foot
F
T1 35°
35°
2.2 kg
T2
F
T1
T1 s in 35
°
T2 s in 35
°
T2 c os 35
°
T1 c os 35
°
T1
T2
35° +x
+y
35°
T2
(a) (b) Free-body diagram for the foot pulley
FIGURE 4.27 (a) A traction device for the foot. (b) The free-body diagram for the pulley on the foot.
Figure 4.27a shows a traction device used with a foot injury. The weight of the 2.2-kg object creates a tension in the rope that passes around the
pulleys. Therefore, tension forces T1 →
and T2 →
are applied to the pulley on
the foot. (It may seem surprising that the rope applies a force to either side
of the foot pulley. A similar eff ect occurs when you place a fi nger inside
a rubber band and push downward. You can feel each side of the rubber
band pulling upward on the fi nger.) The foot pulley is kept in equilibrium
because the foot also applies a force F→ to it. This force arises in reaction (Newton’s third law) to the pulling eff ect of the forces T1
→ and T2
→ . Ignoring
the weight of the foot, fi nd the magnitude of F→.
Reasoning The forces T1 →
, T2 →
, and F→ keep the pulley on the foot at rest. The pulley, therefore, has no acceleration and is in equilibrium. As a res-
ult, the sum of the x components and the sum of the y components of the three forces must each be zero. Figure 4.27b shows the free-body diagram of the pulley on the foot. The x axis is chosen to be along the direction of force F,→ and the components of the forces T1
→ and T2
→ are indic-
ated in the drawing. (See Section 1.7 for a review of vector components.)
104 CHAPTER 4 Forces and Newton’s Laws of Motion
Example 12 presents another situation in which three forces are responsible for the equilib-
rium of an object. However, in this example all the forces have diff erent magnitudes.
The plus signs in the table denote components that point along the pos-
itive axes, and the minus signs denote components that point along the
negative axes. Setting the sum of the x components and the sum of the y components equal to zero leads to the following equations:
ΣFx = −T1 sin 10.0° + T2 sin 80.0° = 0 (4.9a)
ΣFy = +T1 cos 10.0° − T2 cos 80.0° − W = 0 (4.9b)
Solving the fi rst of these equations for T1 shows that
T1 = (sin 80.0°sin 10.0°)T2 Substituting this expression for T1 into the second equation gives
(sin 80.0°sin 10.0°) T2 cos 10.0° − T2 cos 80.0° − W = 0
T2 = W
(sin 80.0°sin 10.0°) cos 10.0° − cos 80.0° Setting W = 3150 N in this result yields T2 = 582 N .
Since T1 = (sin 80.0°sin 10.0°) T2 and T2 = 582 N, it follows that T1 = 3.30 × 103 N .
EXAMPLE 12 Replacing an Engine
An automobile engine has a weight W →
, whose magnitude is W = 3150 N. This engine is being positioned above an engine compartment, as
Figure 4.28a illustrates. To position the engine, a worker is using a rope. Find the tension T1
→ in the supporting cable and the tension T2
→ in the
positioning rope.
Reasoning Under the infl uence of the forces W →
, T1 →
, and T2 →
the ring in
Figure 4.28a is at rest and, therefore, in equilibrium. Consequently, the sum of the x components and the sum of the y components of these forces must each be zero; ∑Fx = 0 and ∑Fy = 0. By using these relations, we can fi nd T1 and T2. Figure 4.28b shows the free-body diagram of the ring and the force components for a suitable x, y axis system.
Problem-Solving Insight When an object is in equilibrium, as here in Example 12, the net force is zero, ∑F→ = 0. This does not mean that each individual force is zero. It means that the vector sum of all the forces is zero.
Solution The free-body diagram shows the components for each of the three forces, and the components are listed in the following table:
Force x Component y Component
T1 → −T1 sin 10.0° +T1 cos 10.0°
T2 → +T2 sin 80.0° −T2 cos 80.0°
W → 0 −W
10.0° 10.0°
80.0°
80.0°
(a) (b) Free-body diagram for the ring
Ring
T1 T1
T2
T2
WW
+y
+x
T1
T1 cos 10.0°
T1 sin 10.0°
T2
T2
sin 80.0°
T2 cos 80.0°
FIGURE 4.28 (a) The ring is in equilibrium because of the three forces T1
→ (the tension force in the supporting
cable), T2 →
(the tension force in the positioning rope), and W
→ (the weight of the engine). (b) The free-body
diagram for the ring.
An object can be moving and still be in equilibrium, provided there is no acceleration.
Example 13 illustrates such a case, and the solution is again obtained using the fi ve-step reason-
ing strategy summarized at the beginning of the section.
4.11 Equilibrium Applications of Newton’s Laws of Motion 105
Check Your Understanding
(The answers are given at the end of the book.) 19. In which one of the following situations could an object possibly be in equilibrium? (a) Three forces
act on the object; the forces all point along the same line but may have diff erent directions. (b) Two perpendicular forces act on the object. (c) A single force acts on the object. (d) In none of the situations described in (a), (b), and (c) could the object possibly be in equilibrium.
20. A stone is thrown from the top of a cliff . Air resistance is negligible. As the stone falls, is it (a) in equi- librium or (b) not in equilibrium?
21. During the fi nal stages of descent, a sky diver with an open parachute approaches the ground with a constant velocity. There is no wind to blow him from side to side. Which one of the following state-
ments is true? (a) The sky diver is not in equilibrium. (b) The force of gravity is the only force acting on the sky diver, so that he is in equilibrium. (c) The sky diver is in equilibrium because no forces are
Solution When determining the components of the weight, it is neces- sary to realize that the angle 𝛽 in Figure 4.29a is 30.0°. Part c of the drawing focuses attention on the geometry that is responsible for this fact.
There it can be seen that α + 𝛽 = 90° and α + 30.0° = 90°, with the result that 𝛽 = 30.0°. The following table lists the components of the forces acting on the jet.
Force x Component y Component
W → −W sin 30.0° −W cos 30.0°
L→ 0 +L
T→ +T 0
R→ −R 0
Setting the sum of the x component of the forces to zero gives
ΣFx = −W sin 30.0° + T − R = 0 (4.9a)
R = T − W sin 30.0° = 103 000 N − (86 500 N) sin 30.0° = 59 800 N
Setting the sum of the y component of the forces to zero gives
ΣFy = −W cos 30.0° + L = 0 (4.9b)
L = W cos 30.0° = (86 500 N) cos 30.0° = 74 900 N
EXAMPLE 13 Equilibrium at Constant Velocity
A jet plane is fl ying with a constant speed along a straight line, at an
angle of 30.0° above the horizontal, as Figure 4.29a indicates. The plane has a weight W
→ whose magnitude is W = 86 500 N, and its engines
provide a forward thrust T→ of magnitude T = 103 000 N. In addition, the lift force L→ (directed perpendicular to the wings) and the force R→ of air resistance (directed opposite to the motion) act on the plane. Find L→ and R→.
Reasoning Figure 4.29b shows the free-body diagram of the plane, including the forcesW
→ , L→, T→, and R→. Since the plane is fl ying with a
constant speed along a straight line, it is not accelerating, it is in equi-
librium, and the sum of the x components and the sum of the y com- ponents of these forces must be zero. The weight W
→ and the thrust T→
are known, so the lift force L→ and the force R→ of air resistance can be obtained from these equilibrium conditions. To calculate the components,
we have chosen axes in the free-body diagram that are rotated by 30.0°
from their usual horizontal–vertical positions. This has been done purely
for convenience, since the weight W →
is then the only force that does not
lie along either axis.
Problem-Solving Insight A moving object is in equilibrium if it moves with a constant velocity; then its acceleration is zero. A zero acceleration is the fundamental characteristic of an object in equilibrium.
T L
R
+y
+x +y
+x
W
(a) (c)(b) Free-body diagram
30.0° 90°
90°
β α
α β
W sin 30.0° W cos 30.0°
30.0°
30.0°
TL
R
W
FIGURE 4.29 (a) A plane moves with a constant velocity at an angle of 30.0° above the horizontal due to the action of four forces, the weight W
→ , the lift
L→, the engine thrust T→, and the air re- sistance R→ . (b) The free-body diagram for the plane. (c) This geometry occurs often in physics.
(Continued)
106 CHAPTER 4 Forces and Newton’s Laws of Motion
acting on him. (d) The sky diver is in equilibrium because two forces act on him, the downward-acting force of gravity and the upward-acting force
of the parachute.
22. A crate hangs from a ring at the middle of a rope, as CYU Figure 4.3 illustrates. A person is pulling on the right end of the rope to keep the
crate in equilibrium. Can the rope ever be made to be perfectly horizontal?
4.12 Nonequilibrium Applications of Newton’s Laws of Motion When an object is accelerating, it is not in equilibrium. The forces acting on it are not balanced,
so the net force is not zero in Newton’s second law. However, with one exception, the reasoning
strategy followed in solving nonequilibrium problems is identical to that used in equilibrium
situations. The exception occurs in Step 4 of the fi ve steps outlined at the beginning of the pre-
vious section. Since the object is now accelerating, the representation of Newton’s second law
in Equations 4.2a and 4.2b applies instead of Equations 4.9a and 4.9b:
ΣFx = max (4.2a) and ΣFy = may (4.2b)
Example 14 uses these equations in a situation where the forces are applied in directions similar
to those in Example 11, except that now an acceleration is present.
EXAMPLE 14 Towing a Supertanker
A supertanker of mass m = 1.50 × 108 kg is being towed by two tugboats, as in Figure 4.30a. The tensions in the towing cables apply the forces T1
→
and T2 →
at equal angles of 30.0° with respect to the tanker’s axis. In addi-
tion, the tanker’s engines produce a forward drive force D→, whose mag- nitude is D = 75.0 × 103 N. Moreover, the water applies an opposing force R→, whose magnitude is R = 40.0 × 103 N. The tanker moves forward with an acceleration that points along the tanker’s axis and has a magnitude of
2.00 × 10−3 m/s2. Find the magnitudes of the tensions T1 →
and T2 →
.
Reasoning The unknown forces T1 →
and T2 →
contribute to the net force
that accelerates the tanker. To determine T1 →
and T2 →
, therefore, we analyze
the net force, which we will do using components. The various force com-
ponents can be found by referring to the free-body diagram for the tanker
in Figure 4.30b, where the ship’s axis is chosen as the x axis. We will then use Newton’s second law in its component form, ∑Fx = max and ∑Fy = may, to obtain the magnitudes of T1
→ and T2
→ .
30.0° 30.0°
30.0° 30.0°
(b) Free-body diagram for the tanker(a)
T1
T2T2
T1
+y
+x R D
T2 sin 30.0°
T2 cos 30.0°
T1 cos 30.0°
T1 sin 30.0° T1
T2
D
a
R
FIGURE 4.30 (a) Four forces act on a supertanker: T1 →
and T2 →
are the tension forces due to the towing
cables, D→ is the forward drive force produced by the tanker’s engines, and R→ is the force with which the water opposes the tanker’s motion. (b) The free-body diagram for the tanker.
CYU FIGURE 4.3
4.12 Nonequilibrium Applications of Newton’s Laws of Motion 107
It often happens that two objects are connected somehow, perhaps by a drawbar like that
used when a truck pulls a trailer. If the tension in the connecting device is of no interest, the ob-
jects can be treated as a single composite object when applying Newton’s second law. However,
if it is necessary to fi nd the tension, as in the next example, then the second law must be applied
separately to at least one of the objects.
Solution The individual force components are summarized as follows:
Force x Component y Component
T1 → +T1 cos 30.0° +T1 sin 30.0°
T2 → +T2 cos 30.0° −T2 sin 30.0°
D→ +D 0
R→ −R 0
Since the acceleration points along the x axis, there is no y component of the acceleration (ay = 0 m/s2). Consequently, the sum of the y components of the forces must be zero:
ΣFy = +T1 sin 30.0° − T2 sin 30.0° = 0
This result shows that the magnitudes of the tensions in the cables are
equal, T1 = T2. Since the ship accelerates along the x direction, the sum of the x components of the forces is not zero. The second law indicates that
ΣFx = T1 cos 30.0° + T2 cos 30.0° + D − R = max
Since T1 = T2, we can replace the two separate tension symbols by a single symbol T, the magnitude of the tension. Solving for T gives
T = max + R − D 2 cos 30.0°
= (1.50 × 108 kg)(2.00 × 10−3 m /s2) + 40.0 × 103 N − 75.0 × 103 N
2 cos 30.0°
= 1.53 × 105 N
EXAMPLE 15 Hauling a Trailer
A truck is hauling a trailer along a level road, as Figure 4.32a illustrates. The mass of the truck is m1 = 8500 kg and that of the trailer is m2 = 27 000 kg. The two move along the x axis with an acceleration of ax =
0.78 m/s2. Ignoring the retarding forces of friction and air resistance,
determine (a) the tension T→ in the horizontal drawbar between the trailer and the truck and (b) the force D→ that propels the truck forward.
Trailer Truck
(b) Free-body diagrams
+x +xT D
T
Drawbar
(a)
m1 = 8500 kg m2 = 27 000 kg
a = 0.78 m/s2
DT´
DT´ FIGURE 4.32 (a) The force D →
acts on the
truck and propels it forward. The drawbar
exerts the tension force T→′ on the truck and the tension force T→ on the trailer. (b) The free-body diagrams for the trailer and the
truck, ignoring the vertical forces.
Math Skills The sine and cosine functions are defi ned in
Equations 1.1 and 1.2 as sin θ = ho h
and cos θ = ha h
, where ho is
the length of the side of a right triangle that is opposite the angle θ, ha is the length of the side adjacent to the angle θ, and h is the length of the hypotenuse (see Figure 4.31a). When using the sine and cosine functions to determine the scalar components of a vector, we begin
by identifying the angle θ. Figure 4.31b indicates that θ = 30.0° for the vector T1
→ . The components of T1
→ are T1x and T1y. Comparing the
shaded triangles in Figure 4.31, we can see that ho = T1y, ha = T1x, and h = T1. Therefore, we have
cos 30.0° = ha h
= T1x T1
or T1x = T1 cos 30.0°
sin 30.0° = ho h
= T1y T1
or T1y = T1 sin 30.0°
FIGURE 4.31 Math Skills drawing.
(b)
T1 T1y
T1x
30.0°
+y
+x
(a)
ha
h
θ
ho
108 CHAPTER 4 Forces and Newton’s Laws of Motion
Reasoning Since the truck and the trailer accelerate along the hori- zontal direction and friction is being ignored, only forces that have com-
ponents in the horizontal direction are of interest. Therefore, Figure 4.32 omits the weight and the normal force, which act vertically. To determine
the tension force T→ in the drawbar, we draw the free-body diagram for the trailer and apply Newton’s second law, ∑Fx = max. Similarly, we can determine the propulsion force D→ by drawing the free-body diagram for the truck and applying Newton’s second law.
Problem-Solving Insight A free-body diagram is very helpful when applying Newton’s second law. Always start a problem by drawing the free-body diagram.
Solution (a) The free-body diagram for the trailer is shown in Fig- ure 4.32b. There is only one horizontal force acting on the trailer, the tension force T→ due to the drawbar. Therefore, it is straightforward to
obtain the tension from ∑Fx = m2ax, since the mass of the trailer and the acceleration are known:
ΣFx = T = m2 ax = (27 000 kg)(0.78 m /s2) = 21 000 N
(b) Two horizontal forces act on the truck, as the free-body diagram in Figure 4.32b shows. One is the desired force D→. The other is the force T→′. According to Newton’s third law, T→′ is the force with which the trailer pulls back on the truck, in reaction to the truck pulling forward. If the
drawbar has negligible mass, the magnitude of T→′ is equal to the mag- nitude of T→—namely, 21 000 N. Since the magnitude of T→′, the mass of the truck, and the acceleration are known, ∑Fx = m1ax can be used to determine the drive force:
ΣFx = +D − T′ = m1ax
D = m1ax + T′ = (8500 kg)(0.78 m /s2) + 21 000 N = 28 000 N
In Section 4.11 we examined situations where the net force acting on an object is zero, and in
the present section we have considered two examples where the net force is not zero. Conceptual
Example 16 illustrates a common situation where the net force is zero at certain times but is not
zero at other times.
a. The skier is fl oating motionless in the water, so her velocity and acceleration are both zero. Therefore, the net force acting on her is
zero, and she is in equilibrium.
b. As the skier is being pulled up and out of the water, her velocity is increasing. Thus, she is accelerating, and the net force acting on her
is not zero. The skier is not in equilibrium. The direction of the net
force is shown in Figure 4.33b. c. The skier is now moving at a constant speed along a straight line
(Figure 4.33c), so her velocity is constant. Since her velocity is con- stant, her acceleration is zero. Thus, the net force acting on her is
zero, and she is again in equilibrium, even though she is moving.
d. After the skier lets go of the tow rope, her speed decreases, so she is decelerating. Thus, the net force acting on her is not zero, and she is not
in equilibrium. The direction of the net force is shown in Figure 4.33d.
Related Homework: Problem 75
CONCEPTUAL EXAMPLE 16 The Motion of a Water Skier
Figure 4.33 shows a water skier at four diff erent moments:
a. The skier is fl oating motionless in the water. b. The skier is being pulled out of the water and up onto the skis. c. The skier is moving at a constant speed along a straight line. d. The skier has let go of the tow rope and is slowing down.
For each moment, explain whether the net force acting on the skier is
zero.
Reasoning and Solution According to Newton’s second law, if an ob- ject has zero acceleration, the net force acting on it is zero. In such a case,
the object is in equilibrium. In contrast, if the object has an acceleration,
the net force acting on it is not zero. Such an object is not in equilibrium.
We will consider the acceleration in each of the four phases of the motion
to decide whether the net force is zero.
Net force Net force
(a) (c)(b) (d )
FIGURE 4.33 A water skier (a) fl oating in the water, (b) being pulled up by the boat, (c) moving at a constant velocity, and (d) slowing down.
The force of gravity is often present among the forces that aff ect the acceleration of an
object. Examples 17 and 18 deal with typical situations.
4.12 Nonequilibrium Applications of Newton’s Laws of Motion 109
assumption that block 1 moves up the incline. Now there are two equa-
tions in two unknowns, and they may be solved simultaneously (see
Appendix C) to give T and a:
T = 86.3 N and a = 5.89 m/s2
EXAMPLE 17 Accelerating Blocks
Block 1 (mass m1 = 8.00 kg) is moving on a frictionless 30.0° incline. This block is connected to block 2 (mass m2 = 22.0 kg) by a massless cord that passes over a massless and frictionless pulley (see Figure 4.34a). Find the acceleration of each block and the tension in the cord.
Reasoning Since both blocks accelerate, there must be a net force acting on each one. The key to this problem is to realize that Newton’s
second law can be used separately for each block to relate the net force
and the acceleration. Note also that both blocks have accelerations of the
same magnitude a, since they move as a unit. We assume that block 1 accelerates up the incline and choose this direction to be the +x axis. If block 1 in reality accelerates down the incline, then the value obtained for
the acceleration will be a negative number.
Problem-Solving Insight Mass and weight are dif- ferent quantities. They cannot be interchanged when solving problems.
Solution Three forces act on block 1: (1) W1 →
is its weight [W1 = m1g = (8.00 kg) (9.80 m/s2) = 78.4 N], (2) T→ is the force applied because of the tension in the cord, and (3) FN
→ is the normal force the incline exerts.
Figure 4.34b shows the free-body diagram for block 1. The weight is the only force that does not point along the x, y axes, and its x and y components are given in the diagram. Applying Newton’s second law
(∑Fx = m1ax) to block 1 shows that
ΣFx = −W1 sin 30.0° + T = m1a
where we have set ax = a. This equation cannot be solved as it stands, since both T and a are unknown quantities. To complete the solution, we next consider block 2.
Two forces act on block 2, as the free-body diagram in Figure 4.34b indicates: (1) W2
→ is its weight [W2 = m2g = (22.0 kg)(9.80 m/s2) = 216 N]
and (2) T→′ is exerted as a result of block 1 pulling back on the connecting cord. Since the cord and the frictionless pulley are massless, the mag-
nitudes of T→′ and T→ are the same: T ′ = T. Applying Newton’s second law (∑Fy = m2ay) to block 2 reveals that
ΣFy = T − W2 = m2 (−a)
The acceleration ay has been set equal to −a since block 2 moves down- ward along the −y axis in the free-body diagram, consistent with the
(a) (b) Free-body diagrams
T´ T´
m1
a
a 30.0°
30.0°
T
Block 1 Block 2
FN
FN
W1 W2
W1
W2
T
W1 cos 30.0°
30.0°
W1 sin 30.0°
+x
+x
+y
+y
m2
FIGURE 4.34 (a) Three forces act on block 1: its weight W1
→ , the normal force FN
→ , and the force T→
due to the tension in the cord. Two forces act on block 2: its weight W2
→ and the force T→′ due to the tension. The
acceleration is labeled according to its magnitude a. (b) Free-body diagrams for the two blocks.
Math Skills The two equations containing the unknown quantit- ies T and a are
−W1 sin 30.0° + T = m1a (1) and T − W2 = m2 (−a) (2)
Neither equation by itself can yield numerical values for T and a. However, the two equations can be solved simultaneously in the following manner. To begin with, we rearrange Equation (1)
to give T = m1a + W1 sin 30.0°. Next, we substitute this result into Equation (2) and obtain a result containing only the unknown
acceleration a:
m1a + W1 sin 30.0° − W2 = m2 (−a) ⏟⎵⎵⎵⏟⎵⎵⎵⏟
T
Rearranging this equation so that the terms m1a and m2a stand alone on the left of the equals sign, we have
m1a + m2a = W2 − W1 sin 30.0° or a = W2 − W1 sin 30.0°
m1 + m2
This result yields the value of a = 5.89 m /s2 . We can also substitute the expression for a into either one of the two starting equations and obtain a result containing only the unknown tension T. We choose Equation (1) and fi nd that
−W1 sin 30.0° + T = m1( W2 − W1 sin 30.0°
m1 + m2 ) ⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟
a Solving for T gives
T = W1 sin 30.0° + m1( W2 − W1 sin 30.0°
m1 + m2 ) This expression yields the value of T = 86.3 N .
110 CHAPTER 4 Forces and Newton’s Laws of Motion
EXAMPLE 18 Hoisting a Scaff old
A window washer on a scaff old is hoisting the scaff old up the side of a
building by pulling downward on a rope, as in Figure 4.35a. The mag- nitude of the pulling force is 540 N, and the combined mass of the worker
and the scaff old is 155 kg. Find the upward acceleration of the unit.
Reasoning The worker and the scaff old form a single unit, on which the rope exerts a force in three places. The left end of the rope exerts an
upward force T→ on the worker’s hands. This force arises because he pulls downward with a 540-N force, and the rope exerts an oppositely directed
force of equal magnitude on him, in accord with Newton’s third law. Thus,
the magnitude T of the upward force is T = 540 N and is the magnitude of the tension in the rope. If the masses of the rope and each pulley are
negligible and if the pulleys are friction-free, the tension is transmitted
undiminished along the rope. Then, a 540-N tension force T→ acts upward on the left side of the scaff old pulley (see part a of the drawing). A tension force is also applied to the point P, where the rope attaches to the roof. The roof pulls back on the rope in accord with the third law, and this pull
leads to the 540-N tension force T→ that acts on the right side of the scaf- fold pulley. In addition to the three upward forces, the weight of the unit
must be taken into account [W = mg = (155 kg)(9.80 m/s2) = 1520 N]. Part b of the drawing shows the free-body diagram.
Solution Newton’s second law (ΣFy = may) can be applied to calculate the acceleration ay:
ΣFy = +T + T + T − W = may
ay = 3T − W
m =
3(540 N) − 1520 N
155 kg = 0.65 m /s2
ay
P
T
T
T T
+x
+y
(a)
(b) Free-body diagram of the unit
T
T
W = mg
W = mg
FIGURE 4.35 (a) A window washer pulls down on the rope to hoist the scaff old up the side of a building. The force T
→ results from the eff ort of the
window washer and acts on him and the scaff old in three places, as discussed in Example 18. (b) The free-body diagram of the unit comprising the man and the scaff old.
Sled
Passenger
Rails
6.5°
Stop
2.3 m
(a)
a
(b) Free-body diagram
6.5°
W cos 6.5° +x
+y
W sin 6.5°
FN
W
EXAMPLE 19 BIO The Importance of Seatbelts
Police departments around the country use a device, called The Convincer, to educate the public on the safety of seatbelts (see Figure 4.36a). The device consists of a sled that is free to move on rails that are inclined at
6.5° above the horizontal. A passenger is placed in the sled and secured
with a seatbelt. The sled is released from rest and travels a distance of
2.3 m along the rails before slamming into a stop at the bottom, thereby
simulating a car collision. Assume the rails are frictionless and calculate
the speed of the sled at impact.
Reasoning The free-body diagram for the sled is shown in Figure 4.36b. The x-component of the sled’s weight is the only force acting on the sled in the x-direction. Once released, the sled will accelerate down the rails.
Thus, this is a nonequilibrium problem, and the sum of the forces acting
on the sled in the x-direction will be equal to its mass times its accelera- tion in that direction. Since the sled’s acceleration down the rails will be
constant, we can use our relationships from kinematics to calculate its
speed when it strikes the stop.
Solution Applying Newton’s second law to the sled in the x-direction, we have ΣFx = W sin 6.5° = max. We can solve this expression for the
acceleration of the sled in the x-direction: ax = W sin 6.5°
m =
mg sin 6.5° m
=
g sin 6.5° = (9.8 m/s2)(sin 6.5°) = 1.1 m/s2. Now that we have the accelera- tion of the sled, we can use Equation 3.6a to calculate its speed when it
FIGURE 4.36 (a) The passenger in the sled accel- erates down the rails and collides with a stop in order to simulate a car collision. (b) Free-body diagram showing the forces acting on the sled. The only force providing its acceleration down the rails is the x-component of its weight.
Concept Summary 111
Check Your Understanding
(The answers are given at the end of the book.) 23. A circus performer hangs stationary from a rope. She then begins to climb upward by pulling herself
up, hand over hand. When she starts climbing, is the tension in the rope (a) less than, (b) equal to, or (c) greater than it is when she hangs stationary?
24. A freight train is accelerating on a level track. Other things being equal, would the tension in the coup- ling between the engine and the fi rst car change if some of the cargo in the last car were transferred to
any one of the other cars?
25. Two boxes have masses m1 and m2, and m2 is greater than m1. The boxes are being pushed across a frictionless horizontal surface (see CYU Figure 4.4). As the drawing shows, there are two possible arrangements, and the pushing force is the same in each. In which arrangement, (a) or (b), does the force that the left box applies to the right box have a greater magnitude, or (c) is the magnitude the same in both cases?
m1 m1 m2
(a) (b)
m2
Pushing force
Pushing force
CYU FIGURE 4.4
strikes the stop: 𝜐x 2 = 𝜐0x
2 + 2axx. Solving for υx, and using the fact that the sled begins from rest (υ0x = 0), we get the following result for its speed at impact: υx = √2axx = √2(1.1 m/s2)(2.3 m) = 2.2 m/s . Consider the magnitude of this speed. This is approximately equal to 5 mi/h, which is
a relatively low speed for a car. Even so, the passenger still receives quite
a jolt when the sled strikes the stop. Without the seatbelt to decelerate the
passenger upon impact, she would continue to move in a straight line and
strike the front of the sled (Newton’s fi rst law). Since many car collisions
occur at speeds much larger than 5 mi/h, The Convincer demonstrates that seatbelt use is essential for passenger safety.
Concept Summary 4.1 The Concepts of Force and Mass A force is a push or a pull and is a vector quantity. Contact forces arise from the physical contact between
two objects. Noncontact forces are also called action-at-a-distance forces,
because they arise without physical contact between two objects.
Mass is a property of matter that determines how diffi cult it is to acceler-
ate or decelerate an object. Mass is a scalar quantity.
4.2 Newton’s First Law of Motion Newton’s fi rst law of motion, some- times called the law of inertia, states that an object continues in a state of rest
or in a state of motion at a constant velocity unless compelled to change that
state by a net force.
Inertia is the natural tendency of an object to remain at rest or in motion
at a constant velocity. The mass of a body is a quantitative measure of inertia
and is measured in an SI unit called the kilogram (kg). An inertial reference
frame is one in which Newton’s law of inertia is valid.
4.3 Newton’s Second Law of Motion/4.4 The Vector Nature of Newton’s Second Law of Motion Newton’s second law of motion states that when a net force ΣF
→ acts on an object of mass m, the acceleration a→ of the object can
be obtained from Equation 4.1. This is a vector equation and, for motion in
two dimensions, is equivalent to Equations 4.2a and 4.2b. In these equations
the x and y subscripts refer to the scalar components of the force and acceler- ation vectors. The SI unit of force is the newton (N).
Σ F →
= ma→ (4.1) ΣFx = max (4.2a) ΣFy = may (4.2b)
When determining the net force, a free-body diagram is helpful. A free-
body diagram is a diagram that represents the object and the forces acting on it.
4.5 Newton’s Third Law of Motion Newton’s third law of motion, often called the action–reaction law, states that whenever one object exerts a force
on a second object, the second object exerts an oppositely directed force of
equal magnitude on the fi rst object.
4.6 Types of Forces: An Overview Only three fundamental forces have been discovered: the gravitational force, the strong nuclear force, and the
electroweak force. The electroweak force manifests itself as either the elec-
tromagnetic force or the weak nuclear force.
4.7 The Gravitational Force Newton’s law of universal gravitation states that every particle in the universe exerts an attractive force on every other
112 CHAPTER 4 Forces and Newton’s Laws of Motion
particle. For two particles that are separated by a distance r and have masses m1 and m2, the law states that the magnitude of this attractive force is as given in Equation 4.3. The direction of this force lies along the line between the
particles. The constant G has a value of G = 6.674 × 10−11 N · m2/kg2 and is called the universal gravitational constant.
F = G m1m2
r2 (4.3)
The weight W of an object on or above the earth is the gravitational force that the earth exerts on the object and can be calculated from the mass m of the object and the magnitude g of the acceleration due to the earth’s gravity, according to Equation 4.5.
W = mg (4.5)
4.8 The Normal Force The normal force FN →
is one component of the force
that a surface exerts on an object with which it is in contact—namely, the
component that is perpendicular to the surface.
Apparent weight = mg + ma (4.6)
The apparent weight is the force that an object exerts on the platform of a
scale and may be larger or smaller than the true weight mg if the object and the scale have an acceleration a (+ if upward, − if downward). The apparent weight is given by Equation 4.6.
4.9 Static and Kinetic Frictional Forces A surface exerts a force on an object with which it is in contact. The component of the force perpendicular
to the surface is called the normal force. The component parallel to the surface
is called friction.
The force of static friction between two surfaces opposes any impending
relative motion of the surfaces. The magnitude of the static frictional force
depends on the magnitude of the applied force and can assume any value up
to the maximum specifi ed in Equation 4.7, where μs is the coeffi cient of static friction and FN is the magnitude of the normal force.
f sMAX = μs FN (4.7)
The force of kinetic friction between two surfaces sliding against one an-
other opposes the relative motion of the surfaces. This force has a magnitude
given by Equation 4.8, where mk is the coeffi cient of kinetic friction.
f k = μkFN (4.8)
4.10 The Tension Force The word “tension” is commonly used to mean the tendency of a rope to be pulled apart due to forces that are applied at each
end. Because of tension, a rope transmits a force from one end to the other.
When a rope is accelerating, the force is transmitted undiminished only if the
rope is massless.
4.11 Equilibrium Applications of Newton’s Laws of Motion An object is in equilibrium when the object has zero acceleration, or, in other words,
when it moves at a constant velocity. The constant velocity may be zero, in
which case the object is stationary. The sum of the forces that act on an object
in equilibrium is zero. Under equilibrium conditions in two dimensions, the
separate sums of the force components in the x direction and in the y direction must each be zero, as in Equations 4.9a and 4.9b.
ΣFx = 0 (4.9a) ΣFy = 0 (4.9b)
4.12 Nonequilibrium Applications of Newton’s Laws of Motion If an object is not in equilibrium, then Newton’s second law, as expressed in Equa-
tions 4.2a and 4.2b, must be used to account for the acceleration.
ΣFx = max (4.2a) ΣFy = may (4.2b)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 4.2 Newton’s First Law of Motion 1. An object is moving at a constant velocity. All but one of the following statements could be true. Which one cannot be true? (a) No forces act on the object. (b) A single force acts on the object. (c) Two forces act simultan- eously on the object. (d) Three forces act simultaneously on the object. 3. A cup of coff ee is sitting on a table in a recreational vehicle (RV). The cup slides toward the rear of the RV. According to Newton’s fi rst law, which one
or more of the following statements could describe the motion of the RV?
(A) The RV is at rest, and the driver suddenly accelerates. (B) The RV is
moving forward, and the driver suddenly accelerates. (C) The RV is moving
backward, and the driver suddenly hits the brakes. (a) A (b) B (c) C (d) A and B (e) A, B, and C
Section 4.4 The Vector Nature of Newton’s Second Law of Motion 5. Two forces act on a moving object that has a mass of 27 kg. One force has a magnitude of 12 N and points due south, while the other force has
a magnitude of 17 N and points due west. What is the acceleration of the
object? (a) 0.63 m/s2 directed 55° south of west (b) 0.44 m/s2 directed 24° south of west (c) 0.77 m/s2 directed 35° south of west (d) 0.77 m/s2 directed 55° south of west (e) 1.1 m/s2 directed 35° south of west
Section 4.5 Newton’s Third Law of Motion 7. Which one of the following is true, according to Newton’s laws of motion? Ignore friction. (a) A sports utility vehicle (SUV) hits a stationary motorcycle. Since it is stationary, the motorcycle sustains a greater force
than the SUV does. (b) A semitrailer truck crashes all the way through a wall. Since the wall collapses, the wall sustains a greater force than the
truck does. (c) Sam (18 years old) and his sister (9 years old) go ice skating. They push off against each other and fl y apart. Sam fl ies off with the greater
acceleration. (d) Two astronauts on a space walk are throwing a ball back and forth between each other. In this game of catch the distance between
them remains constant. (e) None of the above is true, according to the third law.
8. Two ice skaters, Paul and Tom, are each holding on to opposite ends of the same rope. Each pulls the other toward him. The magnitude of Paul’s
acceleration is 1.25 times greater than the magnitude of Tom’s acceleration.
What is the ratio of Paul’s mass to Tom’s mass? (a) 0.67 (b) 0.80 (c) 0.25 (d) 1.25 (e) 0.50
Focus on Concepts
Focus on Concepts 113
Section 4.7 The Gravitational Force 9. In another solar system a planet has twice the earth’s mass and three times the earth’s radius. Your weight on this planet is ________ times your earth-
weight. Assume that the masses of the earth and of the other planet are uni-
formly distributed. (a) 0.667 (b) 2.000 (c) 0.111 (d) 0.444 (e) 0.222 11. What is the mass on Mercury of an object that weighs 784 N on the earth’s surface? (a) 80.0 kg (b) 48.0 kg (c) 118 kg (d) 26.0 kg (e) There is not enough information to calculate the mass.
Section 4.8 The Normal Force 12. The apparent weight of a passenger in an elevator is greater than his true weight. Which one of the following is true? (a) The elevator is either mov- ing upward with an increasing speed or moving upward with a decreasing
speed. (b) The elevator is either moving upward with an increasing speed or moving downward with an increasing speed. (c) The elevator is either moving upward with a decreasing speed or moving downward with a de-
creasing speed. (d) The elevator is either moving upward with an increasing speed or moving downward with a decreasing speed. (e) The elevator is either moving upward with a decreasing speed or moving downward with
an increasing speed.
13. The drawings show three examples of the force with which
someone pushes against a vertical
wall. In each case the magnitude
of the pushing force is the same.
Rank the normal forces that the
wall applies to the pusher in as-
cending order (smallest fi rst). (a) C, B, A (b) B, A, C (c) A, C, B (d) B, C, A (e) C, A, B
Section 4.9 Static and Kinetic Frictional Forces 15. The drawing shows three blocks, each with the same mass, stacked one upon the other. The bottom block rests on a frictionless horizontal surface
and is being pulled by a force F→ that is parallel to this surface. The sur- faces where the blocks touch each other have identical coeffi cients of static
friction. Which one of the following correctly de-
scribes the magnitude of the net force of static friction fs that acts on each block?
(a) f s,A = f s,B = fs,C (b) f s,A = f s,B = 12 fs,C (c) fs,A = 0 and fs,B = 12 fs,C (d) fs,C = 0 and fs,A = 12 fs,B (e) fs,A = f s,C = 12 fs,B
16. Three identical blocks are being pulled or pushed across a horizontal surface by a force F→, as shown in the drawings. The force F→ in each case has the same magnitude. Rank the kinetic frictional forces that act on the blocks
in ascending order (smallest fi rst).
(a) B, C, A (b) C, A, B (c) B, A, C (d) C, B, A (e) A, C, B
A
F
FF
B C
QUESTION 16
Section 4.10 The Tension Force 18. A heavy block is suspended from a ceiling using pulleys in three diff er- ent ways, as shown in the drawings. Rank the tension in the rope that passes
over the pulleys in ascending order (smallest fi rst).
(a) B, A, C (b) C, B, A (c) A, B, C (d) C, A, B (e) B, C, A
CBA
QUESTION 18
Section 4.11 Equilibrium Applications of Newton’s Laws of Motion 20. A certain object is in equilibrium. Which one of the following state- ments is not true? (a) The object must be at rest. (b) The object has a con- stant velocity. (c) The object has no acceleration. (d) No net force acts on the object.
23. Two identical boxes are being pulled across a horizontal fl oor at a con- stant velocity by a horizontal pulling force of 176 N that is applied to one
of the boxes, as the drawing shows. There is kinetic friction between each
box and the fl oor. Find the tension in the rope between the boxes. (a) 176 N (b) 88.0 N (c) 132 N (d) 44.0 N (e) There is not enough information to calculate the tension.
Section 4.12 Nonequilibrium Applications of Newton’s Laws of Motion 25. A man is standing on a platform that is connected to a pulley arrange- ment, as the drawing shows. By pulling upward on the rope with a force P→ the man can raise the platform and himself. The total mass of the man plus
the platform is 94.0 kg. What pulling force should the man apply to create an
upward acceleration of 1.20 m/s2?
A B C
QUESTION 13
A
B
C F
QUESTION 15
176 N
QUESTION 23
P
Platform
Ceiling
QUESTION 25
114 CHAPTER 4 Forces and Newton’s Laws of Motion
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 4.3 Newton’s Second Law of Motion 1. E An airplane has a mass of 3.1 × 104 kg and takes off under the infl u- ence of a constant net force of 3.7 × 104 N. What is the net force that acts on
the plane’s 78-kg pilot?
2. E MMH A boat has a mass of 6800 kg. Its engines generate a drive force of 4100 N due west, while the wind exerts a force of 800 N due east and the
water exerts a resistive force of 1200 N due east. What are the magnitude and
direction of the boat’s acceleration?
3. E GO Two horizontal forces, F1 →
and F2 →
, are acting on a box, but only F1 →
is shown in the drawing. F2 →
can point either to the right or to the left. The
box moves only along the x axis. There is no friction between the box and the surface. Suppose that F1
→ = +9.0 N and the mass of the box is 3.0 kg.
Find the magnitude and direction of F2 →
when the acceleration of the box is (a) +5.0 m/s2, (b) −5.0 m/s2, and (c) 0 m/s2.
PROBLEM 3
+x F1
4. E In the amusement park ride known as Magic Mountain Superman, power- ful magnets accelerate a car and its riders from rest to 45 m/s (about 100 mi/h)
in a time of 7.0 s. The combined mass of the car and riders is 5.5 × 103 kg.
Find the average net force exerted on the car and riders by the magnets.
5. E SSM A person in a kayak starts paddling, and it accelerates from 0 to 0.60 m/s in a distance of 0.41 m. If the combined mass of the person and the
kayak is 73 kg, what is the magnitude of the net force acting on the kayak?
6. E Scientists are experimenting with a kind of gun that may eventually be used to fi re payloads directly into orbit. In one test, this gun accelerates a 5.0-kg
projectile from rest to a speed of 4.0 × 103 m/s. The net force accelerating
the projectile is 4.9 × 105 N. How much time is required for the projectile to
come up to speed?
7. E SSM MMH A 1580-kg car is traveling with a speed of 15.0 m/s. What is the magnitude of the horizontal net force that is required to bring the car to
a halt in a distance of 50.0 m?
8. E GO The space probe Deep Space 1 was launched on October 24, 1998. Its mass was 474 kg. The goal of the mission was to test a new kind of engine
called an ion propulsion drive. This engine generated only a weak thrust, but
it could do so over long periods of time with the consumption of only small
amounts of fuel. The mission was spectacularly successful. At a thrust of
56 mN how many days were required for the probe to attain a velocity of
805 m/s (1800 mi/h), assuming that the probe started from rest and that the
mass remained nearly constant?
9. M SSM Two forces FA →
and FB →
are applied to an object whose mass is
8.0 kg. The larger force is FA →
. When both forces point due east, the object’s
acceleration has a magnitude of 0.50 m/s2. However, when FA →
points due east
and FB →
points due west, the acceleration is 0.40 m/s2, due east. Find (a) the magnitude of FA
→ and (b) the magnitude of FB
→ .
10. M V-HINT An electron is a subatomic particle (m = 9.11 × 10−31 kg) that is subject to electric forces. An electron moving in the +x direction accelerates from an initial velocity of +5.40 × 105 m/s to a fi nal velocity of +2.10 × 106 m/s
while traveling a distance of 0.038 m. The electron’s acceleration is due
to two electric forces parallel to the x axis: F1 →
= +7.50 × 10−17 N, and F2 →
,
which points in the −x direction. Find the magnitudes of (a) the net force acting on the electron and (b) the electric force F2
→ .
Section 4.4 The Vector Nature of Newton’s Second Law of Motion/Section 4.5 Newton’s Third Law of Motion 11. E Only two forces act on an object (mass = 3.00 kg), as in the drawing. Find the magnitude and
direction (relative to the x axis) of the acceleration of the object.
12. E At an instant when a soccer ball is in contact with the foot of a player kicking it, the horizontal or
x component of the ball’s acceleration is 810 m/s2 and the vertical or y component of its acceleration is 1100 m/s2. The ball’s mass is 0.43 kg. What is the
magnitude of the net force acting on the soccer ball
at this instant?
13. E SSM MMH A rocket of mass 4.50 × 105 kg is in fl ight. Its thrust is directed at an angle of 55.0° above the horizontal and has a magnitude of
7.50 × 106 N. Find the magnitude and direction of the rocket’s acceleration.
Give the direction as an angle above the horizontal.
14. E GO A billiard ball strikes and rebounds from the cushion of a pool table perpendicularly. The mass of the ball is 0.38 kg. The ball approaches
the cushion with a velocity of +2.1 m/s and rebounds with a velocity of
−2.0 m/s. The ball remains in contact with the cushion for a time of
3.3 × 10−3 s. What is the average net force (magnitude and direction) exerted
on the ball by the cushion?
15. E When a parachute opens, the air exerts a large drag force on it. This upward force is initially greater than the weight of the sky diver and, thus,
slows him down. Suppose the weight of the sky diver is 915 N and the drag
force has a magnitude of 1027 N. The mass of the sky diver is 93.4 kg. What
are the magnitude and direction of his acceleration?
16. E GO Two skaters, a man and a woman, are standing on ice. Neglect any friction between the skate blades and the ice. The mass of the man is 82
kg, and the mass of the woman is 48 kg. The woman pushes on the man with
a force of 45 N due east. Determine the acceleration (magnitude and direc-
tion) of (a) the man and (b) the woman. 17. M V-HINT A space probe has two engines. Each generates the same amount of force when fi red, and the directions of these forces can be in-
dependently adjusted. When the engines are fi red simultaneously and each
applies its force in the same direction, the probe, starting from rest, takes 28 s
to travel a certain distance. How long does it take to travel the same distance,
again starting from rest, if the engines are fi red simultaneously and the forces
that they apply to the probe are perpendicular?
18. H At a time when mining asteroids has become feasible, astronauts have connected a line between their 3500-kg space tug and a 6200-kg asteroid. Us-
ing their tug’s engine, they pull on the asteroid with a force of 490 N. Initially
the tug and the asteroid are at rest, 450 m apart. How much time does it take
for the tug and the asteroid to meet?
Problems
60.0 N
40.0 N
45.0°
+x
+y
PROBLEM 11
Problems 115
19. H SSM A 325-kg boat is sailing 15.0° north of east at a speed of 2.00 m/s. Thirty seconds later, it is sailing 35.0° north of east at a speed of 4.00 m/s.
During this time, three forces act on the boat: a 31.0-N force directed 15.0°
north of east (due to an auxiliary engine), a 23.0-N force directed 15.0° south
of west (resistance due to the water), and FW →
(due to the wind). Find the
magnitude and direction of the force FW →
. Express the direction as an angle
with respect to due east.
Section 4.7 The Gravitational Force 20. E GO A 5.0-kg rock and a 3.0 × 10−4-kg pebble are held near the sur- face of the earth. (a) Determine the magnitude of the gravitational force ex- erted on each by the earth. (b) Calculate the magnitude of the acceleration of each object when released.
21. E Mars has a mass of 6.46 × 1023 kg and a radius of 3.39 × 106 m. (a) What is the acceleration due to gravity on Mars? (b) How much would a 65- kg person weigh on this planet?
22. E On earth, two parts of a space probe weigh 11 000 N and 3400 N. These parts are separated by a center-to-center distance of 12 m and may be treated
as uniform spherical objects. Find the magnitude of the gravitational force that
each part exerts on the other out in space, far from any other objects.
23. E GO A raindrop has a mass of 5.2 × 10−7 kg and is falling near the surface of the earth. Calculate the magnitude of the gravitational force exerted (a) on the raindrop by the earth and (b) on the earth by the raindrop. 24. E The weight of an object is the same on two diff erent planets. The mass of planet A is only sixty percent that of planet B. Find the ratio rA/rB of the radii of the planets.
25. E SSM A bowling ball (mass = 7.2 kg, radius = 0.11 m) and a billiard ball (mass = 0.38 kg, radius = 0.028 m) may each be treated as uniform
spheres. What is the magnitude of the maximum gravitational force that each
can exert on the other?
26. E Review Conceptual Example 7 in preparation for this problem. In tests on earth a lunar surface exploration vehicle (mass = 5.90 × 103 kg) achieves
a forward acceleration of 0.220 m/s2. To achieve this same acceleration on the
moon, the vehicle’s engines must produce a drive force of 1.43 × 103 N. What
is the magnitude of the frictional force that acts on the vehicle on the moon?
27. E SSM Synchronous communications satellites are placed in a circular orbit that is 3.59 × 107 m above the surface of the earth. What is the mag-
nitude of the acceleration due to gravity at this distance?
28. E The drawing (not to scale) shows one alignment of the sun, earth, and moon. The gravitational force FSM
→ that the sun exerts on the moon is perpen-
dicular to the force FEM →
that the earth exerts on the moon. The masses are:
mass of sun = 1.99 × 1030 kg, mass of earth = 5.98 × 1024 kg, mass of moon =
7.35 × 1022 kg. The distances shown in the drawing are rSM = 1.50 × 1011 m and rEM = 3.85 × 108 m. Determine the magnitude of the net gravitational force on the moon.
Sun
Earth
Moon
rEM
rSM
FSM
FEM
PROBLEM 28
29. E The drawing shows three particles far away from any other objects and located on a straight line. The masses of these particles are mA = 363 kg,
mB = 517 kg, and mC = 154 kg. Find the magnitude and direction of the net gravitational force acting on (a) particle A, (b) particle B, and (c) particle C.
PROBLEM 29 0.500 m
A B C
0.250 m
30. E A space traveler weighs 540.0 N on earth. What will the traveler weigh on another planet whose radius is twice that of earth and whose mass
is three times that of earth?
31. E SSM Available in WileyPLUS. 32. M CHALK A spacecraft is on a journey to the moon. At what point, as measured from the center of the earth, does the gravitational force exerted
on the spacecraft by the earth balance that exerted by the moon? This point
lies on a line between the centers of the earth and the moon. The distance
between the earth and the moon is 3.85 × 108 m, and the mass of the earth is
81.4 times as great as that of the moon.
33. M V-HINT Available in WileyPLUS. 34. M GO A neutron star has a mass of 2.0 × 1030 kg (about the mass of our sun) and a radius of 5.0 × 103 m (about the height of a good-sized mountain).
Suppose an object falls from rest near the surface of such a star. How fast
would this object be moving after it had fallen a distance of 0.010 m?
(Assume that the gravitational force is constant over the distance of the fall
and that the star is not rotating.)
35. M SSM The sun is more massive than the moon, but the sun is farther from the earth. Which one exerts a greater gravitational force on a person
standing on the earth? Give your answer by determining the ratio Fsun/Fmoon of the magnitudes of the gravitational forces. Use the data on the inside of
the front cover.
36. M Available in WileyPLUS. 37. H Two particles are located on the x axis. Particle 1 has a mass m and is at the origin. Particle 2 has a mass 2m and is at x = +L. A third particle is placed between particles 1 and 2. Where on the x axis should the third particle be located so that the magnitude of the gravitational force on both particle 1 and particle 2 doubles? Express your answer in terms of L.
Section 4.8 The Normal Force/Section 4.9 Static and Kinetic Frictional Forces 38. E A 35-kg crate rests on a horizontal fl oor, and a 65-kg person is stand- ing on the crate. Determine the magnitude of the normal force that (a) the fl oor exerts on the crate and (b) the crate exerts on the person. 39. E SSM A 60.0-kg crate rests on a level fl oor at a shipping dock. The coeffi cients of static and kinetic friction are 0.760 and 0.410, respectively.
What horizontal pushing force is required to (a) just start the crate moving and (b) slide the crate across the dock at a constant speed? 40. E A rocket blasts off from rest and attains a speed of 45 m/s in 15 s. An astronaut has a mass of 57 kg. What is the astronaut’s apparent weight
during takeoff ?
41. E GO A car is traveling up a hill that is inclined at an angle θ above the horizontal. Determine the ratio of the magnitude of the normal force to the
weight of the car when (a) θ = 15° and (b) θ = 35°. 42. E A woman stands on a scale in a moving elevator. Her mass is 60.0 kg, and the combined mass of the elevator and scale is an additional 815 kg.
Starting from rest, the elevator accelerates upward. During the acceleration,
the hoisting cable applies a force of 9410 N. What does the scale read during
the acceleration?
43. E A Mercedes-Benz 300SL (m = 1700 kg) is parked on a road that rises 15° above the horizontal. What are the magnitudes of (a) the normal force and (b) the static frictional force that the ground exerts on the tires?
116 CHAPTER 4 Forces and Newton’s Laws of Motion
directed due west. What must be the magnitude and direction of the third
force, such that the object continues to move with a constant velocity?
54. E Available in WileyPLUS. 55. E BIO Available in WileyPLUS. 56. E Available in WileyPLUS. 57. E SSM A worker stands still on a roof sloped at an angle of 36° above the horizontal. He is prevented from slipping by a static frictional force of 390 N.
Find the mass of the worker.
58. E A stuntman is being pulled along a rough road at a constant velocity by a cable attached to a moving truck. The cable is parallel to the ground. The
mass of the stuntman is 109 kg, and the coeffi cient of kinetic friction between
the road and him is 0.870. Find the tension in the cable.
59. E GO Available in WileyPLUS. 60. E GO The drawing shows a circus clown who weighs 890 N. The coeffi cient of static friction between
the clown’s feet and the ground is 0.53. He pulls vertic-
ally downward on a rope that passes around three pulleys
and is tied around his feet. What is the minimum pulling
force that the clown must exert to yank his feet out from
under himself?
61. M V-HINT Available in WileyPLUS. 62. M V-HINT MMH During a storm, a tree limb breaks off and comes to rest across a barbed wire fence at a
point that is not in the middle between two fence posts. The limb exerts a
downward force of 151 N on the wire. The left section of the wire makes an
angle of 14.0° relative to the horizontal and sustains a tension of 447 N. Find
the magnitude and direction of the tension that the right section of the wire
sustains.
63. M SSM Available in WileyPLUS. 64. M GO Available in WileyPLUS. 65. M GO MMH A toboggan slides down a hill and has a constant velocity. The angle of the hill is 8.00° with respect to the horizontal. What is the coeffi cient of
kinetic friction between the surface of the hill and the toboggan?
66. M BIO V-HINT The person in the drawing is standing on crutches. Assume that the force
exerted on each crutch by the ground is dir-
ected along the crutch, as the force vectors in
the drawing indicate. If the coeffi cient of static
friction between a crutch and the ground is
0.90, determine the largest angle θ MAX that the crutch can have just before it begins to slip on
the fl oor.
67. H SSM A bicyclist is coasting straight down a hill at a constant speed. The combined
mass of the rider and bicycle is 80.0 kg, and the
hill is inclined at 15.0° with respect to the ho-
rizontal. Air resistance opposes the motion of
the cyclist. Later, the bicyclist climbs the same
hill at the same constant speed. How much force
(directed parallel to the hill) must be applied to
the bicycle in order for the bicyclist to climb the
hill?
68. H MMH A kite is hovering over the ground at the end of a straight 43-m line. The tension in the line has a magnitude of 16 N. Wind blowing on the
kite exerts a force of 19 N, directed 56° above the horizontal. Note that the line
attached to the kite is not oriented at an angle of 56° above the horizontal. Find the height of the kite, relative to the person holding the line.
69. H Available in WileyPLUS.
44. E GO Consult Multiple-Concept Example 9 to explore a model for solving this problem. A person pushes on a 57-kg refrigerator with a hori-
zontal force of −267 N; the minus sign indicates that the force points in the
−x direction. The coeffi cient of static friction is 0.65. (a) If the refrigerator does not move, what are the magnitude and direction of the static frictional
force that the fl oor exerts on the refrigerator? (b) What is the magnitude of the largest pushing force that can be applied to the refrigerator before it just
begins to move?
45. E SSM A 6.00-kg box is sliding across the horizontal fl oor of an el- evator. The coeffi cient of kinetic friction between the box and the fl oor is
0.360. Determine the kinetic frictional force that acts on the box when the
elevator is (a) stationary, (b) accelerating upward with an acceleration whose magnitude is 1.20 m/s2, and (c) accelerating downward with an acceleration whose magnitude is 1.20 m/s2.
46. E GO A cup of coff ee is on a table in an airplane fl ying at a constant altitude and a constant velocity. The coeffi cient of static friction between the
cup and the table is 0.30. Suddenly, the plane accelerates forward, its altitude
remaining constant. What is the maximum acceleration that the plane can
have without the cup sliding backward on the table?
47. E MMH An 81-kg baseball player slides into second base. The coeffi - cient of kinetic friction between the player and the ground is 0.49. (a) What is the magnitude of the frictional force? (b) If the player comes to rest after 1.6 s, what was his initial velocity?
48. M V-HINT Consult Multiple-Concept Example 10 in preparation for this problem. Traveling at a speed of 16.1 m/s, the driver of an automobile sud-
denly locks the wheels by slamming on the brakes. The coeffi cient of kinetic
friction between the tires and the road is 0.720. What is the speed of the auto-
mobile after 1.30 s have elapsed? Ignore the eff ects of air resistance.
49. M SSM A person is trying to judge whether a picture (mass = 1.10 kg) is properly positioned by temporarily pressing it against a wall. The pressing
force is perpendicular to the wall. The coeffi cient of static friction between
the picture and the wall is 0.660. What is the minimum amount of pressing
force that must be used?
50. M V-HINT Air rushing over the wings of high-performance race cars generates unwanted horizontal air resistance but also causes a vertical down- force, which helps the cars hug the track more securely. The coeffi cient of static friction between the track and the tires of a 690-kg race car is 0.87.
What is the magnitude of the maximum acceleration at which the car can
speed up without its tires slipping when a 4060-N downforce and an 1190-N
horizontal-air-resistance force act on it?
51. H While moving in, a new homeowner is pushing a box across the fl oor at a constant velocity. The coeffi cient of kinetic friction between the box and
the fl oor is 0.41. The pushing force is directed downward at an angle θ below the horizontal. When θ is greater than a certain value, it is not possible to move the box, no matter how large the pushing force is. Find that value of θ.
Section 4.10 The Tension Force/ Section 4.11 Equilibrium Applications of Newton’s Laws of Motion 52. E MMH The helicopter in the drawing is moving horizontally to the right at a constant velocity v→. The weight of the helicopter is W = 53 800 N. The lift force L→ generated by the rotating blade makes an angle of 21.0° with respect to the vertical. (a) What is the mag- nitude of the lift force? (b) Determine the magnitude of the air resistance R→ that opposes the motion. 53. E SSM Three forces act on a moving object. One force has a magnitude of 80.0 N and is directed
due north. Another has a magnitude of 60.0 N and is
L
R
W
21.0°
v
PROBLEM 52
F
θ
PROBLEM 66
PROBLEM 60
Problems 117
Section 4.12 Nonequilibrium Applications of Newton’s Laws of Motion 70. E A 1450-kg submarine rises straight up toward the surface. Seawater exerts both an upward buoyant force of 16 140 N on the submarine and a down-
ward resistive force of 1030 N. What is the submarine’s acceleration?
71. E SSM A 15-g bullet is fi red from a rifl e. It takes 2.50 × 10−3 s for the bullet to travel the length of the barrel, and it exits the barrel with a speed of
715 m/s. Assuming that the acceleration of the bullet is constant, fi nd the
average net force exerted on the bullet.
72. E A fi sherman is fi shing from a bridge and is using a “45-N test line.” In other words, the line will sustain a maximum force of 45 N without break-
ing. What is the weight of the heaviest fi sh that can be pulled up vertically
when the line is reeled in (a) at a constant speed and (b) with an acceleration whose magnitude is 2.0 m/s2?
73. E SSM Only two forces act on an object (mass = 4.00 kg), as in the drawing. Find the magnitude and
direction (relative to the x axis) of the acceleration of the object.
74. E A helicopter fl ies over the arctic ice pack at a constant altitude, towing an airborne 129-kg laser
sensor that measures the thickness of the ice (see the
drawing). The helicopter and the sensor both move
only in the horizontal direction and have a horizontal
acceleration of magnitude 2.84 m/s2. Ignoring air
resistance, fi nd the tension in the cable towing the
sensor.
PROBLEM 74
75. E Review Conceptual Example 16 as background for this problem. The water skier there has a mass of 73 kg. Find the magnitude of the net force
acting on the skier when (a) she is accelerated from rest to a speed of 11 m/s in 8.0 s and (b) she lets go of the tow rope and glides to a halt in 21 s. 76. E A rescue helicopter is lifting a man (weight = 822 N) from a capsized boat by means of a cable and harness. (a) What is the tension in the cable when the man is given an initial upward acceleration of 1.10 m/s2? (b) What is the tension during the remainder of the rescue when he is pulled upward
at a constant velocity?
77. E A car is towing a boat on a trailer. The driver starts from rest and accelerates to a velocity of +11 m/s in a time of 28 s. The combined mass of
the boat and trailer is 410 kg. The frictional force acting on the trailer can be
ignored. What is the tension in the hitch that connects the trailer to the car?
78. E GO A 292-kg motorcycle is accelerating up along a ramp that is in- clined 30.0° above the horizontal. The propulsion force pushing the motor-
cycle up the ramp is 3150 N, and air resistance produces a force of 250 N that
opposes the motion. Find the magnitude of the motorcycle’s acceleration.
79. E SSM A student is skateboarding down a ramp that is 6.0 m long and inclined at 18° with respect to the horizontal. The initial speed of the skate-
boarder at the top of the ramp is 2.6 m/s. Neglect friction and fi nd the speed
at the bottom of the ramp.
80. E A man seeking to set a world record wants to tow a 109 000-kg air- plane along a runway by pulling horizontally on a cable attached to the air-
plane. The mass of the man is 85 kg, and the coeffi cient of static friction
between his shoes and the runway is 0.77. What is the greatest acceleration
the man can give the airplane? Assume that the airplane is on wheels that
turn without any frictional resistance.
81. M V-HINT A 205-kg log is pulled up a ramp by means of a rope that is parallel to the surface of the ramp. The ramp is inclined at 30.0° with respect
to the horizontal. The coeffi cient of kinetic friction between the log and the
ramp is 0.900, and the log has an acceleration of magnitude 0.800 m/s2. Find
the tension in the rope.
82. M GO To hoist himself into a tree, a 72.0-kg man ties one end of a nylon rope around his waist and throws the other end over a branch of the tree.
He then pulls downward on the free end of the rope with a force of 358 N.
Neglect any friction between the rope and the branch, and determine the
man’s upward acceleration.
83. M CHALK SSM Two objects (45.0 and 21.0 kg) are connected by a mass- less string that passes over a massless, frictionless pulley. The pulley hangs
from the ceiling. Find (a) the acceleration of the objects and (b) the tension in the string.
84. M GO A train consists of 50 cars, each of which has a mass of 6.8 × 103 kg. The train has an acceleration of +8.0 × 10−2 m/s2. Ignore friction and
determine the tension in the coupling (a) between the 30th and 31st cars and (b) between the 49th and 50th cars. 85. M In Problem 80, an 85-kg man plans to tow a 109 000-kg airplane along a runway by pulling horizontally on a cable attached to it. Suppose that he instead
attempts the feat by pulling the cable at an angle of 9.0° above the horizontal. The
coeffi cient of static friction between his shoes and the runway is 0.77. What is the
greatest acceleration the man can give the airplane? Assume that the airplane is
on wheels that turn without any frictional resistance.
86. M MMH The drawing shows a large cube (mass = 25 kg) being ac- celerated across a horizontal frictionless surface by a horizontal force P→ . A small cube (mass = 4.0 kg) is in contact with the front surface of the large
cube and will slide downward unless P→ is suffi ciently large. The coeffi cient of static friction between the cubes is 0.71. What is the smallest magnitude that P→ can have in order to keep the small cube from sliding downward?
PROBLEM 86
Frictionless
P
μ s = 0.71
87. M V-HINT The alarm at a fi re station rings and an 86-kg fi reman, starting from rest, slides down a pole to the fl oor below (a distance of 4.0 m). Just
before landing, his speed is 1.4 m/s. What is the magnitude of the kinetic
frictional force exerted on the fi reman as he slides down the pole?
88. M GO Two blocks are sliding to the right across a horizontal surface, as the drawing shows. In Case A the mass of each block is 3.0 kg. In Case B the
mass of block 1 (the block behind) is 6.0 kg, and the mass of block 2 is 3.0 kg.
No frictional force acts on block 1 in either Case A or Case B. However, a
kinetic frictional force of 5.8 N does act on block 2 in both cases and opposes
the motion. For both Case A and Case B determine (a) the magnitude of the forces with which the blocks push against each other and (b) the magnitude of the acceleration of the blocks.
Block 1 Block 2Block 1
Case A Case B
m1 = 3.0 kg m2 = 3.0 kg m1 = 6.0 kg m2 = 3.0 kg
Block 2
PROBLEM 88
60.0 N
40.0 N
+y
+x
PROBLEM 73
118 CHAPTER 4 Forces and Newton’s Laws of Motion
89. M SSM A person whose weight is 5.20 × 102 N is being pulled up vertic- ally by a rope from the bottom of a cave that is 35.1 m deep. The maximum ten-
sion that the rope can withstand without breaking is 569 N. What is the shortest
time, starting from rest, in which the person can be brought out of the cave?
90. M CHALK A girl is sledding down a slope that is inclined at 30.0° with respect to the horizontal. The wind is aiding the motion by providing a steady
force of 105 N that is parallel to the motion of the sled. The combined mass of
the girl and the sled is 65.0 kg, and the coeffi cient of kinetic friction between
the snow and the runners of the sled is 0.150. How much time is required for the
sled to travel down a 175-m slope, starting from rest?
91. H Available in WileyPLUS. 92. H A small sphere is hung by a string from the ceiling of a van. When the van is stationary, the sphere hangs vertically. However, when the van
accelerates, the sphere swings backward so that the string makes an angle
of θ with respect to the vertical. (a) Derive an expression for the magnitude a of the acceleration of the van in terms of the angle θ and the magnitude g of the acceleration due to gravity. (b) Find the acceleration of the van when θ = 10.0°. (c) What is the angle θ when the van moves with a constant velocity?
93. H SSM A penguin slides at a constant velocity of 1.4 m/s down an icy incline. The incline slopes above the horizontal at an angle of 6.9°. At the
bottom of the incline, the penguin slides onto a horizontal patch of ice. The
coeffi cient of kinetic friction between the penguin and the ice is the same for
the incline as for the horizontal patch. How much time is required for the
penguin to slide to a halt after entering the horizontal patch of ice?
94. H Available in WileyPLUS.
95. E SSM Available in WileyPLUS. 96. E GO A person with a black belt in karate has a fi st that has a mass of 0.70 kg. Starting from rest, this fi st attains a velocity of 8.0 m/s in 0.15 s. What is the
magnitude of the average net force applied to the fi st to achieve this level of
performance?
97. E SSM A 95.0-kg person stands on a scale in an elevator. What is the apparent weight when the elevator is (a) accelerating upward with an acceleration of 1.80 m/s2, (b) moving upward at a constant speed, and (c) accelerating downward with an acceleration of 1.30 m/s2? 98. E MMH Two forces, F1
→ and F2
→ , act on the 7.00-kg block shown in the
drawing. The magnitudes of the forces are F1 = 59.0 N and F2 = 33.0 N. What is the horizontal acceleration (magnitude and direction) of the block?
PROBLEM 98
F1
F2
70.0°
7.00 kg
99. E SSM A student presses a book between his hands, as the drawing indicates. The forces that he exerts on the
front and back covers of the book are perpendicular to the
book and are horizontal. The book weighs 31 N. The coef-
fi cient of static friction between his hands and the book
is 0.40. To keep the book from falling, what is the mag-
nitude of the minimum pressing force that each hand
must exert?
100. E MMH The speed of a bobsled is increasing be- cause it has an acceleration of 2.4 m/s2. At a given instant in time, the forces
resisting the motion, including kinetic friction and air resistance, total 450
N. The combined mass of the bobsled and its riders is 270 kg. (a) What is the magnitude of the force propelling the bobsled forward? (b) What is the magnitude of the net force that acts on the bobsled?
101. E Available in WileyPLUS. 102. E In a European country a bathroom scale displays its reading in kilo- grams. When a man stands on this scale, it reads 92.6 kg. When he pulls down
on a chin-up bar installed over the scale, the reading decreases to 75.1 kg.
What is the magnitude of the force he exerts on the chin-up bar?
103. E SSM A 1380-kg car is moving due east with an initial speed of 27.0 m/s. After 8.00 s the car has slowed down to 17.0 m/s. Find the mag-
nitude and direction of the net force that produces the deceleration.
104. E When a 58-g tennis ball is served, it accelerates from rest to a speed of 45 m/s. The impact with the racket gives the ball a constant acceleration
over a distance of 44 cm. What is the magnitude of the net force acting on the
ball?
105. E In preparation for this problem, review Conceptual Example 7. A space traveler whose mass is 115 kg leaves earth. What are his weight and mass (a) on earth and (b) in interplanetary space where there are no nearby plan- etary objects?
106. E (a) Calculate the magnitude of the gravitational force exerted on a 425-kg satellite that is a distance of two earth radii from the center of the
earth. (b) What is the magnitude of the gravitational force exerted on the earth by the satellite? (c) Determine the magnitude of the satellite’s acceleration. (d) What is the magnitude of the earth’s acceleration? 107. M SSM MMH The drawing shows Robin Hood (mass = 77.0 kg) about to es-
cape from a dangerous situation. With one
hand, he is gripping the rope that holds up a
chandelier (mass = 195 kg). When he cuts
the rope where it is tied to the fl oor, the
chandelier will fall, and he will be pulled
up toward a balcony above. Ignore the fric-
tion between the rope and the beams over
which it slides, and fi nd (a) the accelera- tion with which Robin is pulled upward
and (b) the tension in the rope while Robin escapes.
108. M GO A skater with an initial speed of 7.60 m/s stops propelling himself and
begins to coast across the ice, eventually
coming to rest. Air resistance is negligible. (a) The coeffi cient of kinetic friction between the ice and the skate blades is 0.100. Find the deceleration caused by kinetic friction. (b) How far will the skater travel before coming to rest?
109. M V-HINT Available in WileyPLUS. 110. M GO A mountain climber, in the process of crossing between two cliff s by a rope, pauses to rest. She weighs 535 N. As the drawing shows, she
is closer to the left cliff than to the right cliff , with the result that the tensions
Additional Problems
PROBLEM 99
PROBLEM 107
Concepts and Calculations Problems 119
in the left and right sides of the rope are not the same. Find the tensions in the
rope to the left and to the right of the mountain climber.
65.0° 80.0°
PROBLEM 110
111. M SSM Available in WileyPLUS. 112. M V-HINT Consult Multiple-Concept Example 10 for insight into solv- ing this type of problem. A box is sliding up an incline that makes an angle
of 15.0° with respect to the horizontal. The coeffi cient of kinetic friction
between the box and the surface of the incline is 0.180. The initial speed of
the box at the bottom of the incline is 1.50 m/s. How far does the box travel
along the incline before coming to rest?
113. M V-HINT Available in WileyPLUS. 114. M V-HINT Available in WileyPLUS. 115. M SSM Available in WileyPLUS. 116. H As part a of the drawing shows, two blocks are connected by a rope that passes over a set of pulleys. One block has a weight of 412 N, and
the other has a weight of 908 N. The rope and the pulleys are massless and
there is no friction. (a) What is the acceleration of the lighter block? (b) Sup- pose that the heavier block is removed, and a downward force of 908 N is
provided by someone pulling on the rope, as part b of the drawing shows. Find the acceleration of the remaining block. (c) Explain why the answers in (a) and (b) are diff erent.
412 N 412 N 908 N
(a) (b)
908 N
PROBLEM 116
117. H SSM The three objects in the drawing are connected by strings that pass over massless and friction-free pulleys. The objects move, and the coef-
fi cient of kinetic friction between the middle object and the surface of the
table is 0.100. (a) What is the acceleration of the three objects? (b) Find the tension in each of the two strings.
PROBLEM 117
25.0 kg
80.0 kg
10.0 kg
118. H Available in WileyPLUS. 119. H Available in WileyPLUS. 120. M GO A fl atbed truck is carrying a crate up a hill of angle of inclin- ation θ = 10.0°, as the fi gure illustrates. The coeffi cient of static friction between the truck bed and the crate is μs = 0.350. Find the maximum acceleration that the truck can attain before the crate begins to slip backward
relative to the truck.
FN
W = mg
fs MAX
= 10.0° = 10.0°θ
θ
(a)
= 10.0°
mg cos
FN
fs MAX
θ
θ
W = mg
mg sin
(b) Free-body diagram of the crate
+x
+y
θ
PROBLEM 120
Newton’s three laws of motion provide the basis for understanding the eff ect
of forces on the motion of an object. The second law is especially important,
because it provides the quantitative relationship between net force and accel-
eration. The following problems serve as a review of the essential features of
this relationship.
121. M CHALK SSM The fi gure shows two forces, F→1 = +3000 N and F →
2 =
+5000 N, acting on a spacecraft; the plus signs indicate that the forces are
directed along the +x axis. A third force F3 →
also acts on the spacecraft but is not
shown in the drawing. Concepts: (i) Suppose the spacecraft were stationary.
What would be the direction of F3 →
? (ii) When the spacecraft is moving at a
constant velocity of +850 m/s, what is the direction of F3 →
? Calculations: Find the direction and magnitude of F3
→ .
F2
F1 +x
PROBLEM 121
Concepts and Calculations Problems
120 CHAPTER 4 Forces and Newton’s Laws of Motion
122. M CHALK On earth a block has a weight of 88 N. This block is sliding on a horizontal surface on the moon, where the acceleration due to gravity is
1.60 m/s2. As the fi gure shows, the block is being pulled by a horizontal rope
in which the tension is T = 24 N. The coeffi cient of kinetic friction between the block and the surface is μk = 0.20. Concepts: (i) Which of Newton’s laws of motion provides the best way to determine the acceleration of the block?
(ii) Does the net force in the x direction equal the tension T? Calculations: Determine the acceleration of the block.
T
ax
(a) (b) Free-body diagram for the block
+x
+y
FN
fk T
mg moon
PROBLEM 122
123. E Towing a Detector. You are in a helicopter towing a 129-kg laser detector that is mapping out the thickness of the Brunt Ice Shelf along the
coast of Antarctica. The original cable used to suspend the detector was
damaged and replaced by a lighter one with a maximum tension rating of
310 pounds, not much more than the weight of the detector. The replacement
cable would work without question in the case that the detector and heli-
copter were not accelerating. However, some acceleration of the helicopter
is inevitable. In order to monitor the tension force on the cable to make sure
the maximum is not exceeded (and therefore to not lose the very expensive
detector) you calculate the maximum angle the cable can make with the ver-
tical without the cable exceeding the tension limit. (a) Assuming straight and level fl ight of the helicopter, what is that maximum angle? (b) What is the corresponding acceleration? (c) Your colleague wants to add a 10-kg infrared camera to the detector. What is the maximum allowable angle now?
124. E Stuck on a Ledge. You and your friends pull your car off a moun- tain road onto an overlook to take pictures of the frozen lake below. You lose
your footing on the packed snow, fall over the cliff , and land in a soft snow
bank on a ledge, 10 feet below the edge. The cliff ’s wall is too smooth to
climb upwards and too steep and dangerous to climb the remaining 300 feet
to the bottom. While trying to think your way out of your predicament, you
realize one reason you had slipped was that you had misjudged how the cliff
sloped towards the edge (a decline of about 5–10 degrees). There is nothing
near the edge to which your friends can tie a rope, and they fear the footing
is too slippery for them to pull you to the top. However, they can get the car
close enough to the edge to tie the rope to the bumper and hang it over the
edge. You are worried, however, that the car might slip over the edge as well.
On your phone (which has survived the fall) you look up the coeffi cient of
static friction of snow tires on packed snow and fi nd that it ranges from 0.22
to 0.26, and that the model of your friends’ car weighs 3856 lb. Your own
weight fl uctuates between 120–130 lb. (a) What is the worst-case scenario in terms of the parameters given? (b) Assuming the worst-case scenario, should your friends bring the car close to the edge? (c) Next, should you risk tying the rope to the trailer hitch and trying to climb out? You assume the
hitch is low enough to the ground so that the tension force is parallel to the
slope near the edge of the cliff and that you climb up the rope at a constant
velocity.
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
5.1 Define uniform circular motion.
5.2 Solve uniform circular motion kinematic problems.
5.3 Solve uniform circular motion dynamic problems.
5.4 Solve problems involving banked curves.
5.5 Analyze circular gravitational orbits.
5.6 Solve application problems involving gravity and uniform circular motion.
5.7 Analyze vertical circular motion.
© G
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m s/
A ge
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ck
CHAPTER 5
Dynamics of Uniform Circular Motion
While performing a circular loop-the-loop stunt, the pilot of this small airplane experiences a net force and acceleration that points toward the center of the circle. We will now see how and why this net force and acceleration arise.
5.1 Uniform Circular Motion There are many examples of motion on a circular path. Of the many possibilities, we single out those that satisfy the following defi nition:
DEFINITION OF UNIFORM CIRCULAR MOTION Uniform circular motion is the motion of an object traveling at a constant (uniform) speed on a circular path.
As an example of uniform circular motion, Figure 5.1 shows a model airplane on a guideline. The speed of the plane is the magnitude of the velocity vector v→, and since the speed is constant, the vectors in the drawing have the same magnitude at all points on the circle.
Sometimes it is more convenient to describe uniform circular motion by specify- ing the period of the motion, rather than the speed. The period T is the time required to travel once around the circle—that is, to make one complete revolution. There is a relationship between period and speed, since speed υ is the distance traveled (here, the circumference of the circle = 2πr) divided by the time T:
υ = 2πr T
(5.1) 121
υυ
υ υ
FIGURE 5.1 The motion of a model airplane fl ying at a constant speed on a horizontal circular path is an example of uniform circular motion.
122 CHAPTER 5 Dynamics of Uniform Circular Motion
If the radius is known, as in Example 1, the speed can be calculated from the period, or vice versa.
EXAMPLE 1 A Tire-Balancing Machine
The wheel of a car has a radius of r = 0.29 m and is being rotated at 830 revolutions per minute (rpm) on a tire-balancing machine. Determine the speed (in m/s) at which the outer edge of the wheel is moving.
Reasoning The speed υ can be obtained directly from υ = 2πr/T, but fi rst the period T is needed. The period is the time for one revolution, and it must be expressed in seconds, because the problem asks for the speed in meters per second.
Solution Since the tire makes 830 revolutions in one minute, the number of minutes required for a single revolution is
1 830 revolutions/min
= 1.2 × 10−3 min/revolution
Therefore, the period is T = 1.2 × 10−3 min, which corresponds to 0.072 s. Equation 5.1 can now be used to fi nd the speed:
υ = 2πr T
= 2π (0.29 m)
0.072 s = 25 m/s
The defi nition of uniform circular motion emphasizes that the speed, or the magnitude of the velocity vector, is constant. It is equally signifi cant that the direction of the vector is not constant. In Figure 5.1, for instance, the velocity vector changes direction as the plane moves around the circle. Any change in the velocity vector, even if it is only a change in direction, means that an ac- celeration is occurring. This particular acceleration is called “centripetal acceleration,” because it points toward the center of the circle, as the next section explains.
5.2 Centripetal Acceleration In this section we determine how the magnitude ac of the centripetal acceleration depends on the speed υ of the object and the radius r of the circular path. We will see that ac = υ2/r.
In Figure 5.2a an object (symbolized by a dot •) is in uniform circular motion. At a time t0 the velocity is tangent to the circle at point O, and at a later time t the velocity is tangent at point P. As the object moves from O to P, the radius traces out the angle θ, and the velocity vector changes direction. To emphasize the change, part b of the picture shows the velocity vector removed from point P, shifted parallel to itself, and redrawn with its tail at point O. The angle β between the two vectors indicates the change in direction. Since the radii CO and CP are perpendicular to the tangents at points O and P, respectively, it follows that α + β = 90° and α + θ = 90°. Therefore, angle β and angle θ are equal.
As always, acceleration is the change ∆v→ in velocity divided by the elapsed time ∆t, or a→ = ∆v→/∆t. Figure 5.3a shows the two velocity vectors oriented at the angle θ with respect to one another, together with the vector ∆v→ that represents the change in velocity. The change ∆v→ is the increment that must be added to the velocity at time t0, so that the resultant velocity has the new direction after an elapsed time ∆t = t ‒ t0. Figure 5.3b shows the sector of the circle COP.
C
at time
O
P
(a)
t0
tv
at timev
θ
C
O
P
(b)
θ
α β
FIGURE 5.2 (a) For an object (•) in uniform circular motion, the velocity v→ has diff erent directions at diff erent places on the circle. (b) The velocity vector has been removed from point P, shifted parallel to itself, and redrawn with its tail at point O.
(b)
(a) P
O
C
r
r
at time
t0
t
t
v
v
at timev
θθ
Δ
Δ
υ
FIGURE 5.3 (a) The directions of the velocity vector at times t and t0 diff er by the angle θ. (b) When the object moves along the circle from O to P, the radius r traces out the same angle θ. Here, the sector COP has been rotated clockwise by 90° relative to its orientation in Figure 5.2.
5.2 Centripetal Acceleration 123
In the limit that ∆t is very small, the arc length OP is approximately a straight line whose length is the distance υ∆t traveled by the object. In this limit, COP is an isosceles triangle, as is the triangle in part a of the drawing. Note that both triangles have equal angles θ. This means that they are similar triangles, so that
∆υ υ =
υ ∆t r
This equation can be solved for ∆υ/∆t, to show that the magnitude ac of the centripetal accelera- tion is given by ac = υ2/r.
Centripetal acceleration is a vector quantity and, therefore, has a direction as well as a mag- nitude. The direction is toward the center of the circle, and Conceptual Example 2 helps us to set the stage for explaining this important fact.
CONCEPTUAL EXAMPLE 2 Which Way Will the Object Go?
In Figure 5.4 an object, such as a model airplane on a guideline, is in uni- form circular motion. The object is symbolized by a dot (•), and at point O it is released suddenly from its circular path. For instance, suppose that the guideline for a model plane is cut suddenly. Does the object move (a) along the straight tangent line between points O and A or (b) along the circular arc between points O and P?
Reasoning Newton’s fi rst law of motion (see Section 4.2) guides our reasoning. This law states that an object continues in a state of rest or in a state of motion at a constant velocity (i.e., at a constant speed along a straight line) unless compelled to change that state by a net force. When an object is suddenly released from its circular path, there is no longer a net force being applied to the object. In the case of the model airplane, the guideline cannot apply a force, since it is cut. Gravity certainly acts on the plane, but the wings provide a lift force that balances the weight of the plane.
Answer (b) is incorrect. An object such as a model airplane will remain on a circular path only if a net force keeps it there. Since there is no net force, it cannot travel on the circular arc.
Answer (a) is correct. In the absence of a net force, the plane or any object would continue to move at a constant speed along a straight line
in the direction it had at the time of release, consistent with Newton’s fi rst law. This speed and direction are given in Figure 5.4 by the velocity vector v→.
Related Homework: Problem 3
C
O
P
A
v
θ
FIGURE 5.4 If an object (•) moving on a circular path were released from its path at point O, it would move along the straight tangent line OA in the absence of a net force.
As Example 2 discusses, the object in Figure 5.4 would travel on a tangent line if it were released from its circular path suddenly at point O. It would move in a straight line to point A in the time it would have taken to travel on the circle to point P. It is as if, in the process of remain- ing on the circle, the object drops through the distance AP, and AP is directed toward the center of the circle in the limit that the angle θ is small. Thus, the object in uniform circular motion accelerates toward the center of the circle at every moment. Since the word “centripetal” means “moving toward a center,” the acceleration is called centripetal acceleration.
CENTRIPETAL ACCELERATION Magnitude: The centripetal acceleration of an object moving with a speed υ on a circular path of radius r has a magnitude ac given by
ac = υ 2
r (5.2)
Direction: The centripetal acceleration vector always points toward the center of the circle and continually changes direction as the object moves.
The following example illustrates the eff ect of the radius r on the centripetal acceleration.
124 CHAPTER 5 Dynamics of Uniform Circular Motion
In Section 4.11 we learned that an object is in equilibrium when it has zero acceleration. Conceptual Example 4 discusses whether an object undergoing uniform circular motion can ever be at equilibrium.
EXAMPLE 3 The Physics of a Bobsled Track
The bobsled track at the 1994 Olympics in Lillehammer, Norway, con- tained turns with radii of 33 m and 24 m, as Interactive Figure 5.5 illus- trates. Find the centripetal acceleration at each turn for a speed of 34 m/s, a speed that was achieved in the two-man event. Express the answers as multiples of g = 9.8 m/s2.
Reasoning In each case, the magnitude of the centripetal accelera- tion can be obtained from ac = υ2/r. Since the radius r is in the denomi- nator on the right side of this expression, we expect the acceleration to be smaller when r is larger.
Solution From ac = υ2/r it follows that
Radius = 33 m ac = (34 m/s)2
33 m = 35 m/s2 = 3.6 g
Radius = 24 m ac = (34 m/s)2
24 m = 48 m/s2 = 4.9 g
The centripetal acceleration is indeed smaller when the radius is larger. In fact, with r in the denominator on the right of ac = υ2/r, the accel- eration approaches zero when the radius becomes very large. Uniform circular motion along the arc of an infi nitely large circle entails no acceleration, because it is just like motion at a constant speed along a straight line.
r = 33 m
= 34 m/s
r = 24 m
υ
INTERACTIVE FIGURE 5.5 This bobsled travels at the same speed around two curves with diff erent radii. For the turn with the larger radius, the sled has a smaller centripetal acceleration.
CONCEPTUAL EXAMPLE 4 Uniform Circular Motion and Equilibrium
A car moves at a constant speed along a straight line as it approaches a circular turn. In which of the following parts of the motion is the car in equilibrium? (a) As it moves along the straight line toward the circular turn, (b) as it is go- ing around the turn, (c) as it moves away from the turn along a straight line.
Reasoning An object is in equilibrium when it has no acceleration, according to the defi nition given in Section 4.11. If the object’s velocity remains constant, both in magnitude and direction, its acceleration is zero.
Answer (b) is incorrect. As the car goes around the turn, the direction of travel changes, so the car has a centripetal acceleration that is characteristic
of uniform circular motion. Because of this acceleration, the car is not in equilibrium during the turn.
Answers (a) and (c) are correct. As the car either approaches the turn or moves away from the turn it is traveling along a straight line, and both the speed and direction of the motion are constant. Thus, the velocity vec- tor does not change, and there is no acceleration. Consequently, for these parts of the motion, the car is in equilibrium.
Related Homework: Problem 13
We have seen that going around tight turns (smaller r) and gentle turns (larger r) at the same speed entails diff erent centripetal accelerations. And most drivers know that such turns “feel” diff erent. This feeling is associated with the force that is present in uniform circular motion, and we turn to this topic in the next section.
5.3 Centripetal Force 125
Check Your Understanding
(The answers are given at the end of the book.) 1. The car in CYU Figure 5.1 is moving clockwise around a
circular section of road at a constant speed. What are the di- rections of its velocity and acceleration at (a) position 1 and (b) position 2? Specify your responses as north, east, south, or west.
2. The speedometer of your car shows that you are traveling at a constant speed of 35 m/s. Is it possible that your car is accelerating?
3. Consider two people, one on the earth’s surface at the equator and the other at the north pole. Which has the larger centripetal acceleration?
4. Which of the following statements about centripetal accelera- tion is true? (a) An object moving at a constant velocity cannot have a centripetal acceleration. (b) An object moving at a con- stant speed may have a centripetal acceleration.
5. A car is traveling at a constant speed along the road ABCDE shown in CYU Figure 5.2. Sections AB and DE are straight. Rank the accelerations in each of the four sections according to magnitude, listing the smallest fi rst.
5.3 Centripetal Force Newton’s second law indicates that whenever an object accelerates, there must be a net force to create the acceleration. Thus, in uniform circular motion there must be a net force to produce the centripetal acceleration. The second law gives this net force as the product of the object’s mass m and its acceleration υ2/r. The net force causing the centripetal acceleration is called the centripetal force Fc
→ and points in the same direction as the acceleration—that is, toward the
center of the circle.
CENTRIPETAL FORCE Magnitude: The centripetal force is the name given to the net force required to keep an object of mass m, moving at a speed υ, on a circular path of radius r, and it has a mag- nitude of
Fc = mυ 2
r (5.3)
Direction: The centripetal force always points toward the center of the circle and con- tinually changes direction as the object moves.
The phrase “centripetal force” does not denote a new and separate force created by nature. The phrase merely labels the net force pointing toward the center of the circular path, and this net force is the vector sum of all the force components that point along the radial direction. Some- times the centripetal force consists of a single force such as tension (see Example 5), friction (see Example 7), the normal force or a component thereof (see Examples 8 and 13), or the gravita- tional force (see Examples 9–11). However, there are circumstances when a number of diff erent forces contribute simultaneously to the centripetal force (see Section 5.7).
In some cases, it is easy to identify the source of the centripetal force, as when a model airplane on a guideline fl ies in a horizontal circle. The only force pulling the plane inward is the tension in the line, so this force alone (or a component of it) is the centripetal force. Example 5 illustrates the fact that higher speeds require greater tensions.
N
S
W E
1
2
A B
C
D E
CYU FIGURE 5.1
CYU FIGURE 5.2
126 CHAPTER 5 Dynamics of Uniform Circular Motion
Conceptual Example 6 deals with another case where it is easy to identify the source of the centripetal force.
When a car moves at a steady speed around an unbanked curve, the centripetal force keeping the car on the curve comes from the static friction between the road and the tires, as Figure 5.8 in-
dicates. It is static, rather than kinetic friction, because the tires are not slipping with respect to the radial direction. If the static frictional force is insuffi cient, given the speed and the radius of the turn, the car will skid off the road. Example 7 shows how an icy road can limit safe driving.
Static frictional
force FIGURE 5.8 When the car moves without skidding around a curve, static friction between the road and the tires provides the centripetal force to keep the car on the road.
EXAMPLE 5 The Eff ect of Speed on Centripetal Force
The model airplane in Figure 5.6 has a mass of 0.90 kg and moves at a constant speed on a circle that is parallel to the ground. The path of the airplane and its guideline lie in the same horizontal plane, because the weight of the plane is balanced by the lift generated by its wings. Find the tension in the guideline (length = 17 m) for speeds of 19 and 38 m/s.
Reasoning Since the plane fl ies on a circular path, it experiences a centripetal acceleration that is directed toward the center of the circle. According to Newton’s second law of motion, this acceleration is pro- duced by a net force that acts on the plane, and this net force is called the centripetal force. The centripetal force is also directed toward the center of the circle. Since the tension in the guideline is the only force pulling the plane inward, it must be the centripetal force.
Solution Equation 5.3 gives the tension directly: Fc = T = mυ2/r. Scale records tension
0 N
FIGURE 5.6 The scale records the tension in the guideline. See Example 5.
Speed = 19 m/s T = (0.90 kg)(19 m /s) 2
17 m = 19 N
Speed = 38 m/s T = (0.90 kg)(38 m /s) 2
17 m = 76 N
CONCEPTUAL EXAMPLE 6 The Physics of a Trapeze Act
In a circus, a man hangs upside down from a trapeze, legs bent over the bar and arms downward, holding his partner (see Figure 5.7). Is it harder for the man to hold his partner (a) when the partner hangs straight down and is stationary or (b) when the partner is swinging through the straight-down position?
Reasoning Whenever an object moves on a circular path, it experiences a centripetal acceleration that is directed toward the center of the path. A net force, known as the centripetal force, is required to produce this acceleration.
Answer (a) is incorrect. When the man and his partner are stationary, the man’s arms must support only his partner’s weight. When the two are swinging, however, the man’s arms must provide the additional force required to produce the partner’s centripetal acceleration. Thus, it is easier, not harder, for the man to hold his partner when the partner hangs straight down and is stationary.
Answer (b) is correct. When the two are swinging, the partner is mov- ing on a circular arc and, therefore, has a centripetal acceleration. The man’s arms must support the partner’s weight and must simultaneously exert an additional pull to provide the centripetal force that produces this
FIGURE 5.7 See Example 6 for a discussion of the role of centripetal force in this trapeze act. To
m R
os en
th al
/S up
er St
oc k
acceleration. Because of the additional pull, it is harder for the man to hold his partner while swinging.
Related Homework: Problems 17, 19
5.3 Centripetal Force 127
Modeling the Problem
STEP 1 Speed and Centripetal Force According to Equation 5.3, we have
Fc = mυ 2
r
Solving for the speed υ gives Equation 1 at the right. To use this result, it is necessary to consider the centripetal force Fc, which we do in Step 2.
STEP 2 Static Friction The force of static friction is the centripetal force, and the greater its value, the greater is the speed at which the car can negotiate the turn. The maximum force f sMAX of static friction is given by f sMAX = μsFN (Equation 4.7). Thus, the maximum available centripetal force is
Fc = f sMAX = μs FN
which we can substitute into Equation 1, as shown at the right. The next step considers the normal force FN.
STEP 3 The Normal Force The fact that the car does not accelerate in the vertical direction tells us that the normal force balances the car’s weight mg, or
FN = mg
This result for the normal force can now be substituted into Equation 2, as indicated at the right.
Solution Algebraically combining the results of each step, we fi nd that
υ = √rFcm = √ rμs FN
m = √rμs mgm
The mass m of the car is eliminated algebraically from this result, and we fi nd that the maximum speeds are
Dry road ( μs = 0.95) υ = √rμs g = √(51 m)(0.95)(9.8 m/s2) = 22 m/s
Icy road (μs = 0.10) υ = √rμs g = √(51 m)(0.10)(9.8 m/s2) = 7.1 m/s
As expected, the dry road allows a greater maximum speed.
Related Homework: Problems 15, 20, 25
Analyzing Multiple-Concept Problems
EXAMPLE 7 Centripetal Force and Safe Driving
At what maximum speed can a car safely negotiate a horizontal unbanked turn (radius = 51 m) in dry weather (coeffi cient of static friction = 0.95) and icy weather (coeffi cient of static friction = 0.10)?
Reasoning The speed υ at which the car of mass m can negotiate a turn of radius r is related to the centripetal force Fc that is available, according to Fc = mυ2/r (Equation 5.3). Static friction provides the centripetal force and can pro- vide a maximum force fsMAX given by fsMAX = μsFN (Equation 4.7), in which μs is the coeffi cient of static friction and FN is the normal force. Thus, we will use the fact that Fc = fsMAX to obtain the maximum speed from Equation 5.3. It will also be necessary to evaluate the normal force, which we will do by con- sidering that it must balance the weight of the car. Experience indicates that the maximum speed should be greater for the dry road than for the icy road.
Description Symbol Value Comment Radius of turn r 51 m
Coefficient of static friction μs 0.95 Dry conditions
Coefficient of static friction μs 0.10 Icy conditions
Unknown Variable Speed of car υ ?
Knowns and Unknowns The data for this problem are as follows:
?
υ = √rFcm (1)
STEP 1 STEP 2 STEP 3 Problem-Solving Insight When using an equation to obtain a numerical answer, algebraically solve for the unknown vari- able in terms of the known variables. Then substitute in the numbers for the known variables, as this example shows.
?
υ = √rFcm (1)
Fc = μs FN (2)
υ = √rFcm (1)
Fc = μs FN (2)
FN = mg
128 CHAPTER 5 Dynamics of Uniform Circular Motion
A passenger in Figure 5.8 must also experience a centripetal force to remain on the circular path. However, if the upholstery is very slippery, there may not be enough static friction to keep him in place as the car makes a tight turn at high speed. Then, when viewed from inside the car, he appears to be thrown toward the outside of the curve. What really happens is that the passenger slides off on a tangent to the circle, until he encounters a source of centripetal force to keep him in place while the car turns. This occurs when the passenger bumps into the side of the car, which pushes on him with the necessary force.
THE PHYSICS OF . . . flying an airplane in a banked turn. Sometimes the source of the centripetal force is not obvious. A pilot making a turn, for instance, banks or tilts the plane at an angle to create the centripetal force. As a plane fl ies, the air pushes upward on the wing surfaces with a net lifting force L
→ that is perpendicular to the wing surfaces, as Animated Figure 5.9a shows. Part b of the drawing illustrates that when the plane is banked at an angle θ, a component L sin θ of the lifting force is directed toward the center of the turn. It is this component that pro- vides the centripetal force. Greater speeds and/or tighter turns require greater centripetal forces. In such situations, the pilot must bank the plane at a larger angle, so that a larger component of the lift points toward the center of the turn. The technique of banking into a turn also has an application in the construction of high-speed roadways, where the road itself is banked to achieve a similar eff ect, as the next section discusses.
Check Your Understanding
(The answers are given at the end of the book.) 6. A car is traveling in uniform circular motion on a section of road whose radius is r (see CYU Figure 5.3).
The road is slippery, and the car is just on the verge of sliding. (a) If the car’s speed were doubled, what would be the smallest radius at which the car does not slide? Express your answer in terms of r. (b) What would be your answer to part (a) if the car were replaced by one that weighed twice as much, the car’s speed still being doubled?
7. Other things being equal, would it be easier to drive at high speed around an unbanked horizontal curve on the moon than to drive around the same curve on the earth?
8. What is the chance of a light car safely rounding an unbanked curve on an icy road as compared to that of a heavy car: worse, the same, or better? Assume that both cars have the same speed and are equipped with identical tires.
9. A penny is placed on a rotating turntable. Where on the turntable does the penny require the largest centrip- etal force to remain in place: at the center of the turntable or at the edge of the turntable?
r
CYU FIGURE 5.3
L
Path of plane
L sin
(a) (b)
1 2 –L
1 2 –L
θ
θ
ANIMATED FIGURE 5.9 (a) The air exerts an upward lifting force 12 L
→ on each
wing. (b) When a plane executes a circular turn, the plane banks at an angle θ. The lift component L sin θ is directed toward the center of the circle and provides the centripetal force.
5.4 Banked Curves 129
5.4 Banked Curves When a car travels without skidding around an unbanked curve, the static frictional force between the tires and the road provides the centripetal force. The reliance on friction can be eliminated completely for a given speed, however, if the curve is banked at an angle relative to the horizontal, much in the same way that a plane is banked while making a turn.
Ineractive Figure 5.10a shows a car going around a friction-free banked curve. The radius of the curve is r, where r is measured parallel to the horizontal and not to the slanted surface. Part b shows the normal force FN
→ that the road applies to the car, the normal force being perpendicular
to the road. Because the roadbed makes an angle θ with respect to the horizontal, the normal force has a component FN sin θ that points toward the center C of the circle and provides the centripetal force:
Fc = FN sin θ = mυ 2
r
The vertical component of the normal force is FN cos θ and, since the car does not accelerate in the vertical direction, this component must balance the weight mg of the car. Therefore, FN cos θ = mg. Dividing this equation into the previous one shows that
FN sin θ FN cos θ
= mυ2/r
mg
tan θ = υ2
rg (5.4)
Equation 5.4 indicates that, for a given speed υ, the centripetal force needed for a turn of radius r can be obtained from the normal force by banking the turn at an angle θ, independent of the mass of the vehicle. Greater speeds and smaller radii require more steeply banked curves— that is, larger values of θ. At a speed that is too small for a given θ, a car would slide down a frictionless banked curve; at a speed that is too large, a car would slide off the top. The next example deals with a famous banked curve.
EXAMPLE 8 The Physics of the Daytona International Speedway
The Daytona 500 is the major event of the NASCAR (National Association for Stock Car Auto Racing) season. It is held at the Daytona International Speedway in Daytona, Florida. The turns in this oval track have a maximum radius (at the top) of r = 316 m and are banked steeply, with θ = 31° (see Interactive Figure 5.10). Suppose these maximum-radius turns were fric- tionless. At what speed would the cars have to travel around them?
Reasoning In the absence of friction, the horizontal component of the normal force that the track exerts on the car must provide the centripetal force. Therefore, the speed of the car is given by Equation 5.4.
Solution From Equation 5.4, it follows that
υ = √rg tan θ = √(316 m)(9.80 m /s2) tan 31° = 43 m /s (96 mph)
Drivers actually negotiate the turns at speeds up to 195 mph, however, which requires a greater centripetal force than that implied by Equa- tion 5.4 for frictionless turns. Static friction provides the additional force.
(a)
C r
θ
C r
mg
FN sin
FN
FN cos
(b)
θ
θ θ
θ
INTERACTIVE FIGURE 5.10 (a) A car travels on a circle of radius r on a frictionless banked road. The banking angle is θ, and the center of the circle is at C. (b) The forces acting on the car are its weight mg→ and the normal force FN
→ .
A component FN sin θ of the normal force provides the centripetal force.
Check Your Understanding
(The answer is given at the end of the book.) 10. Go to Concept Simulation 5.2 at www.wiley.com/college/cutnell to review the concepts involved
in this question. Two cars are identical, except for the type of tread design on their tires. The cars are driven at the same speed and enter the same unbanked horizontal turn. Car A cannot negotiate the turn, but car B can. Which tread design, the one on car A or the one on car B, yields a larger coeffi cient of static friction between the tires and the road?
130 CHAPTER 5 Dynamics of Uniform Circular Motion
5.5 Satellites in Circular Orbits Today there are many satellites in orbit about the earth. The ones in circular orbits are examples of uniform circular motion. Like a model airplane on a guideline, each satellite is kept on its cir- cular path by a centripetal force. The gravitational pull of the earth provides the centripetal force and acts like an invisible guideline for the satellite.
There is only one speed that a satellite can have if the satellite is to remain in an orbit with a fi xed radius. To see how this fundamental characteristic arises, consider the gravitational force acting on the satellite of mass m in Figure 5.11. Since the gravitational force is the only force acting on the satellite in the radial direction, it alone provides the centripetal force. Therefore, using Newton’s law of gravitation (Equation 4.3), we have
Fc = G mME
r 2 =
mυ2
r
where G is the universal gravitational constant, ME is the mass of the earth, and r is the distance from the center of the earth to the satellite. Solving for the speed υ of the satellite gives
υ = √GMEr (5.5) If the satellite is to remain in an orbit of radius r, the speed must have precisely this value. Note that the radius r of the orbit is in the denominator in Equation 5.5. This means that the closer the satellite is to the earth, the smaller is the value for r and the greater the orbital speed must be.
The mass m of the satellite does not appear in Equation 5.5, having been eliminated algebra- ically. Consequently, for a given orbit, a satellite with a large mass has exactly the same orbital speed as a satellite with a small mass. However, more eff ort is certainly required to lift the larger- mass satellite into orbit. The orbital speed of one famous artifi cial satellite is determined in the following example.
r
Gravitational force
FIGURE 5.11 For a satellite in circular orbit around the earth, the gravitational force provides the centripetal force.
EXAMPLE 9 The Physics of the Hubble Space Telescope
Determine the speed of the Hubble Space Telescope (see Figure 5.12) orbiting at a height of 598 km above the earth’s surface.
Reasoning Before Equation 5.5 can be applied, the orbital radius r must be determined relative to the center of the earth. Since the radius of the earth is approximately 6.38 × 106 m, and the height of the telescope above the earth’s surface is 0.598 × 106 m, the orbital radius is r = 6.98 × 106 m.
Problem-Solving Insight The orbital radius r that appears in the relation υ = √GME /r is the distance from the satellite to the center of the earth (not to the surface of the earth).
Solution The orbital speed is
υ = √GMEr = √ (6.67 × 10−11 N ·m2/kg2)(5.98 × 1024 kg)
6.98 × 106 m
υ = 7.56 × 103 m /s (16 900 mi/h) FIGURE 5.12 The Hubble Space Telescope orbiting the earth.
Fr an
k W
hi tn
ey /G
et ty
Im ag
es , I
nc .
5.5 Satellites in Circular Orbits 131
THE PHYSICS OF . . . the Global Positioning System. Many applications of satellite technology aff ect our lives. An increasingly important application is the network of 24 satel- lites called the Global Positioning System (GPS), which can be used to determine the position of an object to within 15 m or less. Figure 5.13 illustrates how the system works. Each GPS satellite carries a highly accurate atomic clock, whose time is transmitted to the ground con- tinually by means of radio waves. In the drawing, a car carries a computerized GPS receiver that can detect the waves and is synchronized to the satellite clock. The receiver can therefore determine the distance between the car and a satellite from a knowledge of the travel time of the waves and the speed at which they move. This speed, as we will see in Chapter 24, is the speed of light and is known with great precision. A measurement using a single satellite locates the car somewhere on a circle, as Figure 5.13a shows, while a measurement using a second satellite locates the car on another circle. The intersection of the circles reveals two possible positions for the car, as in Figure 5.13b. With the aid of a third satellite, a third circle can be established, which intersects the other two and identifi es the car’s exact position, as in Figure 5.13c. The use of ground-based radio beacons to provide additional reference points leads to a system called Diff erential GPS, which can locate objects even more accurately than the satellite-based system alone. Navigational systems for automobiles and portable systems that tell hikers and people with visual impairments where they are located are two of the many uses for the GPS technique. GPS applications are so numerous that they have developed into a multibillion dollar industry.
Equation 5.5 applies to human-made satellites or to natural satellites like the moon. It also applies to circular orbits about any astronomical object, provided ME is replaced by the mass of the object on which the orbit is centered. Example 10, for instance, shows how scientists have applied this equation to conclude that a supermassive black hole is probably located at the center of the galaxy known as M87. This galaxy is located at a distance of about 50 million light-years away from the earth. (One light-year is the distance that light travels in a year, or 9.5 × 1015 m.)
(a) (b) (c)
FIGURE 5.13 The Navstar Global Positioning System (GPS) of satellites can be used with a GPS receiver to locate an object, such as a car, on the earth. (a) One satellite identifi es the car as being somewhere on a circle. (b) A second places it on another circle, which identifi es two possibilities for the exact spot. (c) A third provides the means for deciding where the car is.
EXAMPLE 10 The Physics of Locating a Black Hole
The Hubble Telescope has detected the light being emitted from diff erent regions of galaxy M87, which is shown in Figure 5.14. The black circle identifi es the center of the galaxy. From the characteristics of this light,
astronomers have determined that the orbiting speed is 7.5 × 105 m/s for matter located at a distance of 5.7 × 1017 m from the center. Find the mass M of the object located at the galactic center.
132 CHAPTER 5 Dynamics of Uniform Circular Motion
The period T of a satellite is the time required for one orbital revolution. As in any uniform circular motion, the period is related to the speed of the motion by υ = 2πr/T. Substituting υ from Equation 5.5 shows that
√GMEr = 2πr T
Solving this expression for the period T gives
T = 2πr3/2
√GME (5.6)
Although derived for earth orbits, Equation 5.6 can also be used for calculating the periods of those planets in nearly circular orbits about the sun, if ME is replaced by the mass MS of the sun and r is interpreted as the distance between the center of the planet and the center of the sun. The fact that the period is proportional to the three-halves power of the orbital radius is known as Kepler’s third law, and it is one of the laws discovered by Johannes Kepler (1571–1630) during his studies of planetary motion. Kepler’s third law also holds for elliptical orbits, which will be discussed in Chapter 9.
An important application of Equation 5.6 occurs in the fi eld of communications, where “syn- chronous satellites” are put into a circular orbit that is in the plane of the equator, as Figure 5.15 shows. The orbital period is chosen to be one day, which is also the time it takes for the earth to turn once about its axis. Therefore, these satellites move around their orbits in a way that is synchronized with the rotation of the earth. For earth-based observers, synchronous satellites have the useful char- acteristic of appearing in fi xed positions in the sky and can serve as “stationary” relay stations for communication signals sent up from the earth’s surface.
THE PHYSICS OF . . . digital satellite system TV. This is exactly what is done in the digital satellite systems that are a popular alternative to cable TV. As the blowup in Figure 5.15 indicates, a small “dish” antenna on your house picks up the digital TV signals relayed back to earth by the satellite. After being decoded, these signals are delivered to your TV set. All synchronous satellites are in orbit at the same height above the earth’s surface, as Example 11 shows.
Reasoning and Solution Replacing ME in Equation 5.5 with M gives υ = √GM /r, which can be solved to show that
M = υ2r G
= (7.5 × 105 m /s) 2 (5.7 × 1017 m)
6.67 ×10−11 N ·m2/kg2
= 4.8 × 1039 kg
Since the mass of our sun is 2.0 × 1030 kg, matter equivalent to 2.4 bil- lion suns is located at the center of galaxy M87. The volume of space in which this matter is located contains relatively few visible stars, so researchers believe that the data provide strong evidence for the existence of a supermassive black hole. The term “black hole” is used because the tremendous mass prevents even light from escaping. The light that forms the image in Figure 5.14 comes not from the black hole itself, but from matter that surrounds it.*
*More complete analysis shows that the mass of the black hole is equivalent to 6.6 billion suns (K. Gebhardt et al., The Astrophysical Journal, Vol. 729, 2011, p. 119).
Equator
Small dish antenna
TV signals from synchronous
satellite
FIGURE 5.15 A synchronous satellite orbits the earth once per day on a circular path in the plane of the equator. Digital satellite system television uses such satellites as relay stations. TV signals are sent up from the earth’s surface and then rebroadcast down to your own small dish antenna.
FIGURE 5.14 This image of the ionized gas (yellow) at the heart of galaxy M87 was obtained by the Hubble Space Telescope. The circle identifi es the center of the galaxy, at which a black hole is thought to exist.Co
ur te
sy N
A SA
a nd
S pa
ce T
el es
co pe
Sc
ie nc
e In
st itu
te
5.6 Apparent Weightlessness and Artificial Gravity 133
Check Your Understanding
(The answer is given at the end of the book.) 11. Two satellites are placed in orbit, one about Mars and the other about Jupiter, such
that the orbital speeds are the same. Mars has the smaller mass. Is the radius of the satellite in orbit about Mars less than, greater than, or equal to the radius of the satel- lite orbiting Jupiter?
5.6 Apparent Weightlessness and Artificial Gravity
The idea of life on board an orbiting satellite conjures up visions of astronauts fl oating around in a state of “weightlessness,” as in Figure 5.16. Actually, this state should be called “apparent weightlessness,” because it is similar to the condition of zero apparent weight that occurs in an elevator during free-fall. Conceptual Example 12 explores this similarity.
FIGURE 5.16 In a state of apparent weightlessness in orbit, as- tronaut and pilot Guy S. Gardner and mission specialist William M. Shepherd (in chair) fl oat, with Gardner appearing to “bal- ance” the chair on his nose.
C ou
rte sy
N A
SA
*Successive appearances of the sun defi ne the solar day of 24 h or 8.64 × 104 s. The sun moves against the background of the stars, however, and the time required for the earth to turn once on its axis relative to the fi xed stars is 23 h 56 min, which is called the sidereal day. The sidereal day should be used in Example 11, but the neglect of this eff ect introduces an error of less than 0.4% in the answer.
EXAMPLE 11 The Orbital Radius for Synchronous Satellites
What is the height H above the earth’s surface at which all synchronous satellites (regardless of mass) must be placed in orbit?
Reasoning The period T of a synchronous satellite is one day, so we can use Equation 5.6 to fi nd the distance r from the satellite to the center of the earth. To fi nd the height H of the satellite above the earth’s surface we will have to take into account the fact that the earth itself has a radius of 6.38 × 106 m.
Solution A period of one day* corresponds to T = 8.64 × 104 s. In using this value it is convenient to rearrange the equation T = 2πr3/2/√GME as follows:
r 3/2 = T√GME
2π =
(8.64 × 104 s)√(6.67 ×10−11 N ·m2/kg2)(5.98 ×1024 kg) 2π
By squaring and then taking the cube root, we fi nd that r = 4.23 × 107 m. Since the radius of the earth is approximately 6.38 × 106 m, the height of the satellite above the earth’s surface is
H = 4.23 × 107 m ‒ 0.64 × 107 m = 3.59 × 107 m (22 300 mi)
Math Skills In solving T = 2πr 3/2
√GME (Equation 5.6) for r, we
remember that whatever is done to one side of the equals sign must also be done to the other side. To isolate the term r3/2 on one side we multiply both sides by √GME and divide both sides by 2π:
T √GME
2π =
2πr 3/2
√GME √GME
2π or r 3/2 =
T √GME 2π
Next, we square both sides of the result for r3/2:
(r 3/2)2 = ( T√GME
2π ) 2
or r 3 = T 2GME
4π 2
Finally, taking the cube root of the result for r3 gives
√3 r 3 = √3 T 2GME 4π2
or (r 3)1/3 = ( T 2GME
4π2 ) 1/3
or r = T 2/3G 1/3M 1/3E
41/3π 2/3
Using values for T, G, and ME in the result for r shows that r = 4.23 × 107 m.
134 CHAPTER 5 Dynamics of Uniform Circular Motion
THE PHYSICS OF . . . artifi cial gravity. The physiological eff ects of prolonged appar- ent weightlessness are only partially known. To minimize such eff ects, it is likely that artifi cial gravity will be provided in large space stations of the future. To help explain artifi cial gravity, Figure 5.18 shows a space station rotating about an axis. Because of the rotational motion, any
object located at a point P on the interior surface of the station experiences a centripetal force directed toward the axis. The surface of the station provides this force by pushing on the feet of an astronaut, for instance. The centripetal force can be adjusted to match the astronaut’s earth-weight by properly selecting the rotational speed of the space station, as Example 13 illustrates.
CONCEPTUAL EXAMPLE 12 The Physics of Apparent Weightlessness
Figure 5.17 shows a person on a scale in a freely falling elevator and in a satellite in a circular orbit. Assume that when the person is standing stationary on the earth, his weight is 800 N (180 lb). In each case, what apparent weight is recorded by the scale? (a) The scale in the elevator records 800 N while that in the satellite records 0 N. (b) The scale in the elevator records 0 N while that in the satellite records 800 N. (c) Both scales record 0 N.
Reasoning As Section 4.8 discusses, apparent weight is the force that an object exerts on the platform of a scale. This force depends on whether or not the object and the platform are accelerating together.
Answer (a) is incorrect. The scale and the person in the free-falling elevator are accelerating toward the earth at the same rate. Therefore, they cannot push against one another, and so the scale does not record an apparent weight of 800 N.
Answer (b) is incorrect. The scale and the person in the satellite are accelerating toward the center of the earth at the same rate (they have the same centripetal acceleration). Therefore, they cannot push against one another, and so the scale does not record an apparent weight of 800 N.
Answer (c) is correct. The scale and the person in the elevator fall together and, therefore, they cannot push against one another. There- fore, the scale records an apparent weight of 0 N. In the orbiting satellite in Figure 5.17b, both the person and the scale are in uniform circular motion. Objects in uniform circular motion continually accelerate or “fall” toward the center of the circle in order to remain on the circular path. Consequently, both the person and the scale “fall” with the same acceleration toward the center of the earth and cannot push against one another. Thus, the apparent weight in the satellite is zero, just as it is in the freely falling elevator.
Earth
Orbit
Free-fall (a)
Free-fall (b)
FIGURE 5.17 (a) During free-fall, the elevator accelerates downward with the acceleration due to gravity, and the apparent weight of the person is zero. (b) The orbiting space station is also in free-fall toward the center of the earth.
P Fc
FIGURE 5.18 The surface of the rotating space station pushes on an object with which it is in contact and thereby provides the centripetal force that keeps the object moving on a circular path.
5.6 Apparent Weightlessness and Artificial Gravity 135
Analyzing Multiple-Concept Problems
EXAMPLE 13 Artificial Gravity
At what speed must the interior surface of the space station (r = 1700 m) move in Figure 5.18, so that the astronaut located at point P experiences a push on his feet that equals his weight on earth?
Reasoning The fl oor of the rotating space station exerts a normal force on the feet of the astronaut. This is the centripetal force (Fc = mυ2/r) that keeps the astronaut moving on a circular path. Since the magnitude of the normal force equals the astronaut’s weight on earth, we can determine the speed υ of the space station’s fl oor.
Knowns and Unknowns The data for this problem are given in the following table:
Description Symbol Value Radius of space station r 1700 m
Unknown Variable Speed of space station’s floor υ ?
Modeling the Problem
STEP 1 Speed and Centripetal Force The centripetal force acting on the astronaut is given by Equation 5.3 as
Fc = mυ 2
r
Solving for the speed υ gives Equation 1 at the right. Step 2 considers the centripetal force Fc that appears in this result.
STEP 2 Magnitude of the Centripetal Force The normal force applied to the astronaut’s feet by the fl oor is the centripetal force and has a magnitude equal to the astronaut’s earth-weight. This earth-weight is given by Equation 4.5 as the astronaut’s mass m times the magnitude g of the acceleration due to the earth’s gravity. Thus, we have for the centripetal force that
Fc = mg
which can be substituted into Equation 1, as indicated at the right.
Solution Algebraically combining the results of each step, we fi nd that
υ = √rFcm = √ rmg m
The astronaut’s mass m is eliminated algebraically from this result, so the speed of the space station fl oor is
υ = √rg = √(1700 m)(9.80 m/s2) = 130 m/s
Related Homework: Problem 34
STEP 1 STEP 2
Check Your Understanding
(The answer is given at the end of the book.) 12. The acceleration due to gravity on the moon is one-sixth that on earth. (a) Is the true weight of a person
on the moon less than, greater than, or equal to the true weight of the same person on earth? (b) Is the apparent weight of a person in orbit about the moon less than, greater than, or equal to the apparent weight of the same person in orbit about the earth?
υ = √rFcm (1) ?
υ = √rFcm (1)
Fc = mg
136 CHAPTER 5 Dynamics of Uniform Circular Motion
5.7 *Vertical Circular Motion Motorcycle stunt drivers perform a feat in which they drive their cycles around a vertical cir- cular track, as in Interactive Figure 5.19a. Usually, the speed varies in this stunt. When the speed of travel on a circular path changes from moment to moment, the motion is said to be nonuniform. Nonetheless, we can use the concepts that apply to uniform circular motion to gain considerable insight into the motion that occurs on a vertical circle.
There are four points on a vertical circle where the centripetal force can be identifi ed easily, as Interactive Figure 5.19b indicates. As you look at Interactive Figure 5.19b, keep in mind that the centripetal force is not a new and separate force of nature. Instead, at each point the centripetal force is the net sum of all the force components oriented along the radial direction, and it points toward the center of the circle. The drawing shows only the weight of the cycle plus rider (magnitude = mg) and the normal force pushing on the cycle (magnitude = FN). The propulsion and braking forces are omitted for simplicity, because they do not act in the radial direction. The magnitude of the centrip- etal force at each of the four points is given as follows in terms of mg and FN:
(1) FN1 − mg = mυ1 2
r (3) FN3 + mg = mυ3 2
r ⏟⎵⏟⎵⏟ ⏟⎵⏟⎵⏟
(2) FN2 = mυ2 2
r (4) FN4 = mυ4 2
r
Problem-Solving Insight Centripetal force is the name given to the net force that points toward the center of a circular path. As shown here, there may be more than one force that contributes to this net force.
THE PHYSICS OF . . . the loop-the-loop motorcycle stunt. As the cycle goes around, the magnitude of the normal force changes. It changes because the speed changes and because the weight does not have the same eff ect at every point. At the bottom, the normal force and the weight oppose one another, giving a centripetal force of magnitude FN1 ‒ mg. At the top, the normal force and the weight reinforce each other to provide a centripetal force whose magnitude is FN3 + mg. At points 2 and 4 on either side, only FN2 and FN4 provide the centripetal force. The weight is tangent to the circle at points 2 and 4 and has no component pointing toward the center. If the speed at each of the four places is known, along with the mass and the radius, the normal forces can be determined.
Riders who perform the loop-the-loop trick must have at least a minimum speed at the top of the circle to remain on the track. This speed can be determined by considering the centripetal force at point 3. The speed υ3 in the equation FN3 + mg = mυ 23 /r is a minimum when FN3 is zero. Then, the speed is given by υ3 = √rg. At this speed, the track does not exert a normal force to keep the cycle on the circle, because the weight mg provides all the centripetal force. Under these conditions, the rider experiences an apparent weightlessness like that discussed in Section 5.6, because for an instant the rider and the cycle are falling freely toward the center of the circle.
Check Your Understanding
(The answers are given at the end of the book.) 13. Would a change in the earth’s mass aff ect (a) the banking of airplanes as they turn, (b) the banking of
roadbeds, (c) the speeds with which satellites are put into circular orbits, and (d) the performance of the loop-the-loop motorcycle stunt?
14. A stone is tied to a string and whirled around in a circle at a constant speed. Is the string more likely to break when the circle is horizontal or when it is vertical? Assume that the constant speed is the same in each case.
= Fc1 = Fc3
⏟= Fc2 ⏟= Fc4
r
(a)
(b)
1
3
mg
mg
mg
mg
FN3
FN1
FN4 FN24 2
INTERACTIVE FIGURE 5.19 (a) A vertical loop-the-loop motorcycle stunt. (b) The normal force F→N and the weight mg→ of the cycle and the rider are shown here at four locations.
Concept Summary 137
EXAMPLE 14 BIO The Physics of g-Suits
Solution Since both forces on the pilot in Figure 5.20 point in toward the center of the circular motion, the centripetal force will be equal to the sum of the normal force and the weight: FC = FN + mg. Equa- tion 5.3 tells us that the centripetal force is equal to mυ2/r. Therefore, we
fi nd that mυ2
r = FN + mg. The problem tells us we want the normal
force on the pilot to be equal to his weight. Thus, we make that substi-
tution and fi nd the following: mυ 2
r = mg + mg = 2mg. Notice that the
mass of the pilot drops out, and we can solve for the speed of the plane: υ = √2rg = √2(1200 m)(9.8 m/s2) = 150 m/s
In addition to the importance of g-suits in this type of maneuver, this particular combination of forces can be very alarming for young pilots. Since the normal force on the pilot is equal to his weight, he feels as if he is sitting right side up, when in fact, he is upside down. This can lead to spatial disorientation.
Jet fi ghter pilots and astronauts often experience large accelerations from centripetal forces during fl ight. This is commonly referred to as “pulling g’s”. For example, pilots fl ying along the path of a vertical circle are sus- ceptible to the loss of consciousness (blackout) due to blood fl owing from the top of their head and pooling in their lower body. To help prevent this potentially dangerous situation, the pilot wears a device called a g-suit. The suit contains air-fi lled bladders that expand and squeeze on a pilot’s legs and abdomen. This helps prevent the blood from draining from the upper part of the body, thereby allowing the pilot to remain conscious during higher levels of acceleration. Consider the following situation shown in Figure 5.20, where a fi ghter pilot is fl ying upside down along a vertical circle whose radius is 1.2 km. What must be the speed of the plane, so that the normal force acting on the pilot is equal to his weight?
Reasoning The forces acting on the pilot are shown in Figure 5.20. Since we have circular motion, we should be able to identify the cen- tripetal force. We can then apply Equation 5.3 to calculate the speed of the plane.
Concept Summary 5.1 Uniform Circular Motion Uniform circular motion is the motion of an object traveling at a constant (uniform) speed on a circular path. The period T is the time required for the object to travel once around the circle. The speed υ of the object is related to the period and the radius r of the circle by Equation 5.1.
υ = 2πr T
(5.1)
5.2 Centripetal Acceleration An object in uniform circular motion exper- iences an acceleration, known as centripetal acceleration. The magnitude ac of the centripetal acceleration is given by Equation 5.2, where υ is the speed of the object and r is the radius of the circle. The direction of the centripetal acceleration vector always points toward the center of the circle and continu- ally changes as the object moves.
ac = υ 2
r (5.2)
5.3 Centripetal Force To produce a centripetal acceleration, a net force pointing toward the center of the circle is required. This net force is called the
centripetal force, and its magnitude Fc is given by Equation 5.3, where m and υ are the mass and speed of the object, and r is the radius of the circle. The direction of the centripetal force vector, like that of the centripetal accelera- tion vector, always points toward the center of the circle.
Fc = mυ 2
r (5.3)
5.4 Banked Curves A vehicle can negotiate a circular turn without relying on static friction to provide the centripetal force, provided the turn is banked at an angle relative to the horizontal. The angle θ at which a friction- free curve must be banked is related to the speed υ of the vehicle, the radius r of the curve, and the magnitude g of the acceleration due to gravity by Equation 5.4.
tan θ = υ 2
rg (5.4)
5.5 Satellites in Circular Orbits When a satellite orbits the earth, the gravitational force provides the centripetal force that keeps the satellite mov- ing in a circular orbit. The speed υ and period T of a satellite depend on the
υ
FN mg
FIGURE 5.20 The normal force and weight of a pilot both point down toward the center of the circular motion while fl ying upside down at the top of a vertical circle. The speed of the plane will change the magnitude of the normal force (i.e., how much the seat pushes against the pilot).
138 CHAPTER 5 Dynamics of Uniform Circular Motion
mass ME of the earth and the radius r of the orbit according to Equations 5.5 and 5.6, where G is the universal gravitational constant.
υ = √GMEr (5.5)
T = 2πr 3/2
√GME (5.6)
5.6 Apparent Weightlessness and Artifi cial Gravity The apparent weight of an object is the force that it exerts on a scale with which it is in
contact. All objects, including people, on board an orbiting satellite are in free-fall, since they experience negligible air resistance and they have an ac- celeration that is equal to the acceleration due to gravity. When a person is in free-fall, his or her apparent weight is zero, because both the person and the scale fall freely and cannot push against one another.
5.7 Vertical Circular Motion Vertical circular motion occurs when an object, such as a motorcycle, moves on a vertical circular path. The speed of the object often varies from moment to moment, and so do the magnitudes of the centripetal acceleration and centripetal force.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 5.2 Centripetal Acceleration 1. Two cars are traveling at the same constant speed υ. As the drawing in- dicates, car A is moving along a straight section of the road, while car B is rounding a circular turn. Which statement is true about the accelerations of the cars? (a) The acceleration of both cars is zero, since they are traveling at a constant speed. (b) Car A is accelerating, but car B is not accelerating. (c) Car A is not accelerating, but car B is accelerating. (d) Both cars are accelerating.
QUESTION 1
B
A
υ
υ
3. Two cars are driving at the same constant speed υ around a racetrack. However, they are traveling through turns that have diff erent radii, as shown in the drawing. Which statement is true about the magnitude of the centripetal acceleration of each car? (a) The magnitude of the centripetal acceleration of each car is the same, since the cars are moving at the same speed. (b) The magnitude of the centripetal acceleration of the car at A is greater than that of the car at B, since the radius of the circular track is smaller at A. (c) The magnitude of the centripetal acceleration of the car at A is greater than that of the car at B, since the radius of the circular track is greater at A. (d) The magnitude of the centripetal acceleration of the car at A is less than that of the car at B, since the radius of the circular track is smaller at A.
QUESTION 3
BA
υ
υ
Section 5.3 Centripetal Force 7. The drawing shows two identical stones attached to cords that are be- ing whirled on a tabletop at the same speed. The radius of the larger circle is twice that of the smaller circle. How is the tension T1 in the longer cord related to the tension T2 in the shorter cord? (a) T1 = T2 (b) T1 = 2T2 (c) T1 = 4T2 (d) T1 = 12T2 (e) T1 =
1 4T2
QUESTION 7 Path 1
Identical stones
Path 2
υ
υ
8. Three particles have the following masses (in multiples of m0) and move on three diff erent circles with the following speeds (in multiples of υ0) and radii (in multiples of r0):
Particle Mass Speed Radius 1 m0 2υ0 r0 2 m0 3υ0 3r0 3 2m0 2υ0 4r0
Rank the particles according to the magnitude of the centripetal force that acts on them, largest fi rst. (a) 1, 2, 3 (b) 1, 3, 2 (c) 2, 1, 3 (d) 2, 3, 1 (e) 3, 2, 1
Section 5.4 Banked Curves 10. Two identical cars, one on the moon and one on the earth, have the same speed and are rounding banked turns that have the same radius r. There are two forces acting on each car, its weight mg and the normal force FN exerted by the road. Recall that the weight of an object on the moon is about one- sixth of its weight on earth. How does the centripetal force on the moon com- pare with that on the earth? (a) The centripetal forces are the same. (b) The centripetal force on the moon is less than that on the earth. (c) The centripetal force on the moon is greater than that on the earth.
Section 5.5 Satellites in Circular Orbits 11. Two identical satellites are in orbit about the earth. As the drawing shows, one orbit has a radius r and the other 2r. The centripetal force on the
Focus on Concepts
Problems 139
satellite in the larger orbit is ________ as that on the satellite in the smaller orbit. (a) the same (b) twice as great (c) four times as great (d) half as great (e) one-fourth as great
QUESTION 11
r
2r
Earth
Section 5.7 Vertical Circular Motion 15. The drawing shows an extreme skier at the bottom of a ski jump. At this point the track is circular with a radius r. Two forces act on the skier, her weight mg and the normal force FN. Which relation describes how the net force acting on her is related to her mass m and speed υ and to the radius r? Assume that “up” is the positive direction.
(a) FN + mg = mυ 2
r (b) FN − mg =
mυ 2
r
(c) FN = mυ 2
r (d) −mg = mυ
2
r
QUESTION 15
FN
r
mg
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual MMH Problem-solving help GO Guided Online Tutorial V-HINT Video Hints CHALK Chalkboard Videos
BIO Biomedical application E Easy M Medium H Hard
Section 5.1 Uniform Circular Motion,
Section 5.2 Centripetal Acceleration 1. E SSM A car travels at a constant speed around a circular track whose radius is 2.6 km. The car goes once around the track in 360 s. What is the magnitude of the centripetal acceleration of the car?
2. E GO The following table lists data for the speed and radius of three examples of uniform circular motion. Find the magnitude of the centripetal acceleration for each example.
Radius Speed Example 1 0.50 m 12 m/s
Example 2 Infinitely large 35 m/s
Example 3 1.8 m 2.3 m/s
3. E Available in WileyPLUS. 4. E GO Speedboat A negotiates a curve whose radius is 120 m. Speedboat B negotiates a curve whose radius is 240 m. Each boat experiences the same centripetal acceleration. What is the ratio υA/υB of the speeds of the boats? 5. E SSM How long does it take a plane, traveling at a constant speed of 110 m/s, to fl y once around a circle whose radius is 2850 m?
6. E BIO The aorta is a major artery, rising upward from the left ventricle of the heart and curving down to carry blood to the abdomen and lower half of
the body. The curved artery can be approximated as a semicircular arch whose diameter is 5.0 cm. If blood fl ows through the aortic arch at a speed of 0.32 m/s, what is the magnitude (in m/s2) of the blood’s centripetal acceleration?
7. E MMH The blade of a windshield wiper moves through an angle of 90.0° in 0.40 s. The tip of the blade moves on the arc of a circle that has a radius of 0.45 m. What is the magnitude of the centripetal acceleration of the tip of the blade?
8. E V-HINT There is a clever kitchen gadget for drying lettuce leaves after you wash them. It consists of a cylindrical container mounted so that it can be rotated about its axis by turning a hand crank. The outer wall of the cyl- inder is perforated with small holes. You put the wet leaves in the container and turn the crank to spin off the water. The radius of the container is 12 cm. When the cylinder is rotating at 2.0 revolutions per second, what is the mag- nitude of the centripetal acceleration at the outer wall?
9. E SSM Computer-controlled display screens provide drivers in the Indi- anapolis 500 with a variety of information about how their cars are performing. For instance, as a car is going through a turn, a speed of 221 mi/h (98.8 m/s) and centripetal acceleration of 3.00 g (three times the acceleration due to gravity) are displayed. Determine the radius of the turn (in meters).
10. M V-HINT A computer is reading data from a rotating CD-ROM. At a point that is 0.030 m from the center of the disc, the centripetal acceleration is 120 m/s2. What is the centripetal acceleration at a point that is 0.050 m from the center of the disc?
11. M BIO A centrifuge is a device in which a small container of material is rotated at a high speed on a circular path. Such a device is used in medical laboratories, for instance, to cause the more dense red blood cells to settle through the less dense blood serum and collect at the bottom of the container. Suppose the centripetal acceleration of the sample is 6.25 × 103 times as large as the acceleration due to gravity. How many revolutions per minute is the sample making, if it is located at a radius of 5.00 cm from the axis of rotation?
12. M CHALK The earth rotates once per day about an axis passing through the north and south poles, an axis that is perpendicular to the plane of the equator. Assuming the earth is a sphere with a radius of 6.38 × 106 m, de- termine the speed and centripetal acceleration of a person situated (a) at the equator and (b) at a latitude of 30.0° north of the equator.
Problems
140 CHAPTER 5 Dynamics of Uniform Circular Motion
Section 5.3 Centripetal Force 13. E SSM Review Example 3, which deals with the bobsled in Interactive Figure 5.5. Also review Conceptual Example 4. The mass of the sled and its two riders in Interactive Figure 5.5 is 350 kg. Find the magnitude of the centripetal force that acts on the sled during the turn with a radius of (a) 33 m and (b) 24 m. 14. E At an amusement park there is a ride in which cylindrically shaped chambers spin around a central axis. People sit in seats facing the axis, their backs against the outer wall. At one instant the outer wall moves at a speed of 3.2 m/s, and an 83-kg person feels a 560-N force pressing against his back. What is the radius of the chamber?
15. E MMH Multiple-Concept Example 7 reviews the concepts that play a role in this problem. Car A uses tires for which the coeffi cient of static fric- tion is 1.1 on a particular unbanked curve. The maximum speed at which the car can negotiate this curve is 25 m/s. Car B uses tires for which the coeffi - cient of static friction is 0.85 on the same curve. What is the maximum speed at which car B can negotiate the curve?
16. E A speed skater goes around a turn that has a radius of 31 m. The skater has a speed of 14 m/s and experiences a centripetal force of 460 N. What is the mass of the skater?
17. E For background pertinent to this problem, review Conceptual Example 6. In Figure 5.7 the man hanging upside down is holding a partner who weighs 475 N. Assume that the partner moves on a circle that has a radius of 6.50 m. At a swinging speed of 4.00 m/s, what force must the man apply to his partner in the straight-down position?
18. E MMH A car is safely negotiating an unbanked circular turn at a speed of 21 m/s. The road is dry, and the maximum static frictional force acts on the tires. Suddenly a long wet patch in the road decreases the maximum static frictional force to one-third of its dry-road value. If the car is to continue safely around the curve, to what speed must the driver slow the car?
19. E See Conceptual Example 6 to review the concepts involved in this problem. A 9.5-kg monkey is hanging by one arm from a branch and is swinging on a vertical circle. As an approximation, assume a radial distance of 85 cm between the branch and the point where the monkey’s mass is located. As the monkey swings through the lowest point on the circle, it has a speed of 2.8 m/s. Find (a) the magnitude of the centripetal force acting on the monkey and (b) the magnitude of the tension in the monkey’s arm. 20. E GO Multiple-Concept Example 7 deals with the concepts that are important in this problem. A penny is placed at the outer edge of a disk (radius = 0.150 m) that rotates about an axis perpendicular to the plane of the disk at its center. The period of the rotation is 1.80 s. Find the minimum coef- fi cient of friction necessary to allow the penny to rotate along with the disk.
21. M CHALK SSM The hammer throw is a track-and-fi eld event in which a 7.3-kg ball (the “hammer”) is whirled around in a circle several times and released. It then moves upward on the familiar curving path of projectile motion and eventually returns to earth some distance away. The world record for this distance is 86.75 m, achieved in 1986 by Yuriy Sedykh. Ignore air resistance and the fact that the ball is released above the ground rather than at ground level. Furthermore, assume that the ball is whirled on a circle that has a radius of 1.8 m and that its velocity at the instant of release is directed 41° above the horizontal. Find the magnitude of the centripetal force acting on the ball just prior to the moment of release.
22. M V-HINT An 830-kg race car can drive around an unbanked turn at a maximum speed of 58 m/s without slipping. The turn has a radius of curvature of 160 m. Air fl owing over the car’s wing exerts a downward-pointing force (called the downforce) of 11 000 N on the car. (a) What is the coeffi cient of static friction between the track and the car’s tires? (b) What would be the maximum speed if no downforce acted on the car?
23. M CHALK MMH A “swing” ride at a carnival consists of chairs that are swung in a circle by 15.0-m cables attached to a vertical rotating pole, as
the drawing shows. Suppose the total mass of a chair and its occupant is 179 kg. (a) Determine the tension in the cable attached to the chair. (b) Find the speed of the chair.
PROBLEM 23
60.0° 15.0 m
Section 5.4 Banked Curves 24. E On a banked race track, the smallest circular path on which cars can move has a radius of 112 m, while the largest has a radius of 165 m, as the drawing illustrates. The height of the outer wall is 18 m. Find (a) the smallest and (b) the largest speed at which cars can move on this track without relying on friction.
PROBLEM 24
18 m
165 m
112 m
25. E V-HINT Before attempting this problem, review Examples 7 and 8. Two curves on a highway have the same radii. However, one is unbanked and the other is banked at an angle θ. A car can safely travel along the unbanked curve at a maximum speed υ0 under conditions when the coeffi cient of static friction between the tires and the road is μs = 0.81. The banked curve is fric- tionless, and the car can negotiate it at the same maximum speed υ0. Find the angle θ of the banked curve. 26. E GO A woman is riding a Jet Ski at a speed of 26 m/s and notices a seawall straight ahead. The farthest she can lean the craft in order to make a turn is 22°. This situation is like that of a car on a curve that is banked at an angle of 22°. If she tries to make the turn without slowing down, what is the minimum distance from the seawall that she can begin making her turn and still avoid a crash?
27. E Two banked curves have the same radius. Curve A is banked at an angle of 13°, and curve B is banked at an angle of 19°. A car can travel around curve A without relying on friction at a speed of 18 m/s. At what speed can this car travel around curve B without relying on friction?
28. M MMH A racetrack has the shape of an inverted cone, as the drawing shows. On this surface the cars race in circles that are parallel to the ground. For a speed of 34.0 m/s, at what value of the distance d should a driver locate his car if he wishes to stay on a circular path without depending on friction?
PROBLEM 28 40.0° d
40.0°
29. M GO A jet fl ying at 123 m/s banks to make a horizontal circular turn. The radius of the turn is 3810 m, and the mass of the jet is 2.00 × 105 kg. Calculate the magnitude of the necessary lifting force.
30. H The drawing shows a baggage carousel at an airport. Your suitcase has not slid all the way down the slope and is going around at a constant speed on a circle (r = 11.0 m) as the carousel turns. The coeffi cient of static friction between the suitcase and the carousel is 0.760, and the angle θ in the drawing is 36.0°. How much time is required for your suitcase to go around once?
Additional Problems 141
PROBLEM 30
r θ
Section 5.5 Satellites in Circular Orbits,
Section 5.6 Apparent Weightlessness and Artificial Gravity
31. E GO Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 360 km above the earth’s surface, while that for satellite B is at a height of 720 km. Find the orbital speed for each satellite.
32. E A rocket is used to place a synchronous satellite in orbit about the earth. What is the speed of the satellite in orbit?
33. E SSM A satellite is in a circular orbit around an unknown planet. The satellite has a speed of 1.70 × 104 m/s, and the radius of the orbit is 5.25 × 106 m. A second satellite also has a circular orbit around this same planet. The orbit of this second satellite has a radius of 8.60 × 106 m. What is the orbital speed of the second satellite?
34. E Available in WileyPLUS. 35. E GO A satellite is in a circular orbit about the earth (ME = 5.98 × 1024 kg). The period of the satellite is 1.20 × 104 s. What is the speed at which the satellite travels?
36. E A satellite circles the earth in an orbit whose radius is twice the earth’s radius. The earth’s mass is 5.98 × 1024 kg, and its radius is 6.38 × 106 m. What is the period of the satellite?
37. M SSM Available in WileyPLUS. 38. M GO A satellite has a mass of 5850 kg and is in a circular orbit 4.1 × 105 m above the surface of a planet. The period of the orbit is 2.00 hours. The radius of the planet is 4.15 × 106 m. What would be the true weight of the satellite if it were at rest on the planet’s surface?
39. M V-HINT Two newly discovered planets follow circular orbits around a star in a distant part of the galaxy. The orbital speeds of the planets are determined to be 43.3 km/s and 58.6 km/s. The slower planet’s orbital period is 7.60 years. (a) What is the mass of the star? (b) What is the orbital period of the faster planet, in years?
40. H Available in WileyPLUS.
Section 5.7 Vertical Circular Motion 41. E SSM A motorcycle has a constant speed of 25.0 m/s as it passes over the top of a hill whose radius of curvature is 126 m. The mass of the motor- cycle and driver is 342 kg. Find the magnitudes of (a) the centripetal force and (b) the normal force that acts on the cycle. 42. E BIO V-HINT Pilots of high-performance fi ghter planes can be sub- jected to large centripetal accelerations during high-speed turns. Because of these accelerations, the pilots are subjected to forces that can be much greater than their body weight, leading to an accumulation of blood in the abdomen and legs. As a result, the brain becomes starved for blood, and the pilot can lose consciousness (“black out”). The pilots wear “anti-G suits” to help keep the blood from draining out of the brain. To appreciate the forces that a fi ghter pilot must endure, consider the magnitude FN of the normal force that the pilot’s seat exerts on him at the bottom of a dive. The magnitude of the pilot’s weight is W. The plane is traveling at 230 m/s on a vertical circle of radius 690 m. Determine the ratio FN/W. For comparison, note that blackout can occur for values of FN/W as small as 2 if the pilot is not wearing an anti-G suit. 43. E SSM For the normal force in Interactive Figure 5.19 to have the same magnitude at all points on the vertical track, the stunt driver must ad- just the speed to be diff erent at diff erent points. Suppose, for example, that the track has a radius of 3.0 m and that the driver goes past point 1 at the bottom with a speed of 15 m/s. What speed must she have at point 3, so that the normal force at the top has the same magnitude as it did at the bottom?
44. E GO A special electronic sensor is embedded in the seat of a car that takes riders around a circular loop-the-loop ride at an amusement park. The sensor measures the magnitude of the normal force that the seat exerts on a rider. The loop-the-loop ride is in the vertical plane and its radius is 21 m. Sitting on the seat before the ride starts, a rider is level and stationary, and the electronic sensor reads 770 N. At the top of the loop, the rider is upside down and moving, and the sensor reads 350 N. What is the speed of the rider at the top of the loop?
45. E GO A 0.20-kg ball on a stick is whirled on a vertical circle at a con- stant speed. When the ball is at the three o’clock position, the stick tension is 16 N. Find the tensions in the stick when the ball is at the twelve o’clock and at the six o’clock positions.
46. M GO MMH A stone is tied to a string (length = 1.10 m) and whirled in a circle at the same constant speed in two diff erent ways. First, the circle is hori- zontal and the string is nearly parallel to the ground. Next, the circle is vertical. In the vertical case the maximum tension in the string is 15.0% larger than the tension that exists when the circle is horizontal. Determine the speed of the stone.
47. M GO A motorcycle is traveling up one side of a hill and down the other side. The crest of the hill is a circular arc with a radius of 45.0 m. Determine the maximum speed that the cycle can have while moving over the crest without losing contact with the road.
48. H Available in WileyPLUS.
49. E SSM In a skating stunt known as crack-the-whip, a number of skaters hold hands and form a straight line. They try to skate so that the line rotates about the skater at one end, who acts as the pivot. The skater farthest out has a mass of 80.0 kg and is 6.10 m from the pivot. He is skat- ing at a speed of 6.80 m/s. Determine the magnitude of the centripetal force that acts on him.
50. E BIO Available in WileyPLUS. 51. E GO MMH The second hand and the minute hand on one type of clock are the same length. Find the ratio (ac, second/ac, minute) of the centripetal acceler- ations of the tips of the second hand and the minute hand.
52. E MMH A child is twirling a 0.0120-kg plastic ball on a string in a hori- zontal circle whose radius is 0.100 m. The ball travels once around the circle in 0.500 s. (a) Determine the centripetal force acting on the ball. (b) If the speed is doubled, does the centripetal force double? If not, by what factor does the centripetal force increase?
53. E MMH Available in WileyPLUS. 54. E GO MMH Two cars are traveling at the same speed of 27 m/s on a curve that has a radius of 120 m. Car A has a mass of 1100 kg, and car B has a mass of 1600 kg. Find the magnitude of the centripetal acceleration and the magnitude of the centripetal force for each car.
Additional Problems
142 CHAPTER 5 Dynamics of Uniform Circular Motion
In uniform circular motion the concepts of acceleration and force play central roles. Problem 63 deals with acceleration, particularly in connection with the equations of kinematics. Problem 64 deals with force, and it stresses that centripetal force is the net force along the radial direction. This means that all forces along the radial direction must be taken into account when identifying the centripetal force.
63. M CHALK SSM At time t = 0 s, automobile A is traveling at a speed of 18 m/s along a straight road and is picking up speed with an acceleration that has a magnitude of 3.5 m/s2 as in part a of the fi gure. At t = 0 s, automobile B is traveling at a speed of 18 m/s in uniform circular motion as it negotiates a turn (part b of the fi gure). It has a centripetal acceleration whose magnitude
is also 3.5 m/s2. Concepts: (i) Which automobile has a constant acceleration? (ii) For which automobile do the equations of kinematics apply? Calcula- tions: Determine the speed of each automobile when t = 2 s. 64. M CHALK Ball A is attached to one end of a rigid massless rod, while an identical ball B is attached to the center of the rod, as shown in the fi gure. Each ball has a mass of m = 0.50 kg, and the length of each half of the rod is L = 0.40 m. This arrangement is held by the empty end and is whirled around in a horizontal circle at a constant rate, so that each ball is in uniform circular motion. Ball A travels at a constant speed of υA = 5.0 m/s. Concepts: (i) How many tension forces contribute to the centripetal force that acts on ball A? (ii) How many tension forces contribute to the centripetal force that acts on ball B? (iii) Is the speed of ball A the same as that of ball B? Calculations: Find the tension in each half of the rod.
Concepts and Calculations Problems
55. E SSM A roller coaster at an amusement park has a dip that bottoms out in a vertical circle of radius r. A passenger feels the seat of the car pushing up- ward on her with a force equal to twice her weight as she goes through the dip. If r = 20.0 m, how fast is the roller coaster traveling at the bottom of the dip? 56. E BIO The National Aeronautics and Space Administration (NASA) studies the physiological eff ects of large accelerations on astronauts. Some of these studies use a machine known as a centrifuge. This machine con- sists of a long arm, to one end of which is attached a chamber in which the astronaut sits. The other end of the arm is connected to an axis about which the arm and chamber can be rotated. The astronaut moves on a cir- cular path, much like a model airplane fl ying in a circle on a guideline. The chamber is located 15 m from the center of the circle. At what speed must the chamber move so that an astronaut is subjected to 7.5 times the acceleration due to gravity?
57. M SSM Available in WileyPLUS. 58. M V-HINT The large blade of a helicopter is rotating in a horizontal circle. The length of the blade is 6.7 m, measured from its tip to the center of the circle. Find the ratio of the centripetal acceleration at the end of the blade to that which exists at a point located 3.0 m from the center of the circle.
59. M A block is hung by a string from the inside roof of a van. When the van goes straight ahead at a speed of 28 m/s, the block hangs vertically down. But when the van maintains this same speed around an unbanked curve (radius = 150 m), the block swings toward the outside of the curve. Then the string makes an angle θ with the vertical. Find θ.
60. M GO A rigid massless rod is rotated about one end in a horizontal circle. There is a particle of mass m1 attached to the center of the rod and a particle of mass m2 attached to the outer end of the rod. The inner section of the rod sustains a tension that is three times as great as the tension that the outer section sustains. Find the ratio m1/m2. 61. H SSM Available in WileyPLUS. 62. M GO A space laboratory is rotating to create artifi cial gravity, as the fi gure indicates. Its period of rotation is chosen so that the outer ring (rO = 2150 m) simulates the acceleration due to gravity on earth (9.80 m/s2). What should be the radius r1 of the inner ring, so it simulates the acceleration due to gravity on the surface of Mars (3.72 m/s2)?
PROBLEM 62
rI rO
r
t = 0 s
t = 2.0 s
t = 2.0 st = 0 s
C
v
v0
v0 v
(a) Automobile A
(b) Automobile BPROBLEM 63
(b)
(c)
(a)
L
L
L
2L
B
B
A
A
TB TA
TA
PROBLEM 64
Team Problems 143
65. M Multilevel Artifi cial Gravity. You and your team have the task of designing a space station that will mimic the force due to gravity on the earth,
the moon, and Mars. The station’s purpose is to physically prepare astronauts
for the transition to the diff erent gravitational forces they will experience on
Mars and the moon, but also to acclimate them to Earth’s gravity when they
return. The space station should be constructed of concentric cylinders, with
a maximum allowed diameter of 300 m. (a) Draw a sketch of the space station and label the levels (i.e., the cylinders) according to the celestial body whose
gravitational force each cylinder simulates. (b) Determine the required radii of each cylinder. Assume the outermost cylinder has the maximum allowable
diameter. (c) What is the period of rotation of the station? (gEarth = 9.80 m/s2, gMars = 3.76 m/s
2, and gmoon = 1.62 m/s 2)
66. M A Dangerous Ride. You and your exploration team are stuck on a steep slope in the Andes Mountains in Argentina. A deadly winter storm is
approaching and you must get down the mountain before the storm hits. Your
path leads you around an extremely slippery, horizontal curve with a diameter
of 90 m and banked at an angle of 40.0° relative to the horizontal. You get
the idea to unpack the toboggan that you have been using to haul supplies,
load your team upon it, and ride it down the mountain to get enough speed to
get around the banked curve. You must be extremely careful, however, not to
slide down the bank: At the bottom of the curve is a steep cliff . (a) Neglecting friction and air resistance, what must be the speed of your toboggan in order
to get around the curve without sliding up or down its bank? Express your
answer in m/s and m.p.h. (b) You will need to climb up the mountain and ride the toboggan down in order to attain the speed you need to safely navigate
the curve (from part (a)). The mountain slope leading into the curve is at an
angle of 30.0° relative to the horizontal, and the coeffi cient of kinetic friction
between the toboggan and the surface of the slope is (μmountain = 0.15). How far up the mountain (distance along the slope, not elevation) from the curve
should you start your ride? Note: the path down the mountain levels off at the
bottom so that the toboggan enters the curve moving in the horizontal plane
(i.e., in the same plane as the curve).
Team Problems
144
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
6.1 Determine the work done by a constant force.
6.2 Relate work and kinetic energy.
6.3 Use gravitational potential energy.
6.4 Identify conservative and nonconservative forces.
6.5 Use the law of conservation of mechanical energy.
6.6 Solve problems involving nonconservative forces.
6.7 Solve problems involving power.
6.8 Employ the law of conservation of energy.
6.9 Determine the work done by a variable force.
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CHAPTER 6
Work and Energy
On the popular Behemoth roller coaster at Canada’s Wonderland amusement park, riders cresting the top of the hill will pick up speed on the way down, as they convert gravitational potential energy into kinetic energy. This conversion is governed by the principle of conservation of energy, a central topic in this chapter.
6.1 Work Done by a Constant Force Work is a familiar concept. For example, it takes work to push a stalled car. In fact, more work is done when the pushing force is greater or when the displacement of the car is greater. Force and displacement are, in fact, the two essential elements of work, as Figure 6.1 illustrates. The drawing shows a constant pushing force F
→ that points
in the same direction as the resulting displacement s→.* In such a case, the work W is defi ned as the magnitude F of the force times the magnitude s of the displacement: W = Fs. The work done to push a car is the same whether the car is moved north to south or east to west, provided that the amount of force used and the distance moved are the same. Since work does not convey directional information, it is a scalar quantity.
The equation W = Fs indicates that the unit of work is the unit of force times the unit of distance, or the newton · meter in SI units. One newton · meter is referred to
*When discussing work, it is customary to use the symbol s→ for the displacement, rather than x→ or y→ .
FF
s
FIGURE 6.1 Work is done when a force F→ pushes a car through a displacement s→.
6.1 Work Done by a Constant Force 145
as a joule (J) (rhymes with “cool”), in honor of James Joule (1818–1889) and his research into the nature of work, energy, and heat. Table 6.1 summarizes the units for work in several systems of measurement.
The defi nition of work as W = Fs does have one surprising feature: If the distance s is zero, the work is zero, even if a force is applied. Pushing on an immovable object, such as a brick wall, may tire your muscles, but there is no work done of the type we are discussing. In physics, the idea of work is intimately tied up with the idea of motion. If the object does not move, the force acting on the object does no work.
Often, the force and displacement do not point in the same direction. For instance, Figure 6.2a shows a suitcase-on-wheels being pulled to the right by a force that is applied along the handle. The force is directed at an angle 𝜃 relative to the displacement. In such a case, only the component of the force along the displacement is used in defi ning work. As Figure 6.2b shows, this compo- nent is F cos 𝜃, and it appears in the general defi nition below:
DEFINITION OF WORK DONE BY A CONSTANT* FORCE The work done on an object by a constant force F→ is
W = (F cos θ) s (6.1)
where F is the magnitude of the force, s is the magnitude of the displacement, and 𝜽 is the angle between the force and the displacement. SI Unit of Work: newton · meter = joule (J)
When the force points in the same direction as the displacement, then 𝜃 = 0°, and Equation 6.1 reduces to W = Fs. Example 1 shows how Equation 6.1 is used to calculate work.
TABLE 6.1 Units of Measurement for Work
System Force × Distance = Work
SI newton (N) meter (m) joule (J)
CGS dyne (dyn) centimeter (cm) erg
BE pound (lb) foot (ft) foot · pound (ft · 1b)
*Section 6.9 considers the work done by a variable force.
EXAMPLE 1 Pulling a Suitcase-on-Wheels
Find the work done by a 45.0-N force in pulling the suitcase in Figure 6.2a at an angle 𝜃 = 50.0° for a distance s = 75.0 m.
Reasoning The pulling force causes the suitcase to move a distance of 75.0 m and does work. However, the force makes an angle of 50.0° with the displacement, and we must take this angle into account by using the defi nition of work given by Equation 6.1.
Solution The work done by the 45.0-N force is
W = (F cos θ)s = [(45.0 N)cos 50.0°](75.0 m) = 2170 J
The answer is expressed in newton · meters or joules (J).
FF
(a) (b)
F cos
s s
F
F cos
F
θ θ θ
θ θθ
FIGURE 6.2 (a) Work can be done by a force F→ that points at an angle θ relative to the displacement s→. (b) The force component that points along the displacement is F cos θ.
146 CHAPTER 6 Work and Energy
The defi nition of work in Equation 6.1 takes into account only the component of the force in the direction of the displacement. The force component perpendicular to the displacement does no work. To do work, there must be a force and a displacement, and since there is no displace- ment in the perpendicular direction, there is no work done by the perpendicular component of the force. If the entire force is perpendicular to the displacement, the angle 𝜃 in Equation 6.1 is 90°, and the force does no work at all.
Work can be either positive or negative, depending on whether a component of the force points in the same direction as the displacement or in the opposite direction. Example 2 illustrates how positive and negative work arise.
EXAMPLE 2 BIO The Physics of Weight Lift ing
The weight lifter in Interactive Figure 6.3a is bench-pressing a barbell whose weight is 710 N. In part b of the fi gure, he raises the barbell a distance of 0.65 m above his chest, and in part c he lowers it the same dis- tance. The weight is raised and lowered at a constant velocity. Determine the work done on the barbell by the weight lifter during (a) the lifting phase and (b) the lowering phase.
Reasoning To calculate the work, it is necessary to know the force exerted by the weight lifter. The barbell is raised and lowered at a constant velocity and, therefore, is in equilibrium. Consequently, the force F→ exerted by the weight lifter must balance the weight of the barbell, so F = 710 N. During the lifting phase, the force F→ and displacement s→ are in the same direction, as Interactive Figure 6.3b shows. The angle between them is θ = 0°. When the barbell is lowered, however, the force and displacement are in opposite directions, as in Interactive Figure 6.3c. The angle between the force and the displacement is now 𝜃 = 180°. With these observations, we can fi nd the work.
Solution (a) During the lifting phase, the work done by the force F→ is given by Equation 6.1 as
W = (F cos θ)s = [(710 N)cos 0°](0.65 m) = 460 J
(b) The work done during the lowering phase is
W = (F cos θ)s
= [(710 N)cos 180°](0.65 m) = −460 J
since cos 180° = ‒1. The work is negative, because the force is oppo- site to the displacement. Weight lifters call each complete up-and-down movement of the barbell a repetition, or “rep.” The lifting of the weight is referred to as the positive part of the rep, and the lowering is known as the negative part.
INTERACTIVE FIGURE 6.3 (a) In the bench press, work is done during both the lifting and lowering phases. (b) During the lifting phase, the force F→ does positive work. (c) During the lowering phase, the force does negative work.
( )b
s
F
( )c
s
F
( )a
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Example 3 deals with the work done by a static frictional force when it acts on a crate that is resting on the bed of an accelerating truck.
EXAMPLE 3 Accelerating a Crate
Figure 6.4a shows a 120-kg crate on the fl atbed of a truck that is moving with an acceleration of a = +1.5 m/s2 along the positive x axis. The crate does not slip with respect to the truck as the truck undergoes a displace- ment whose magnitude is s = 65 m. What is the total work done on the crate by all of the forces acting on it?
Reasoning The free-body diagram in Figure 6.4b shows the forces that act on the crate: (1) the weight W→ of the crate, (2) the normal force FN →
exerted by the fl atbed, and (3) the static frictional force fs →
, which is exerted by the fl atbed in the forward direction and keeps the crate from slipping backward. The weight and the normal force are perpendicular to
6.2 The Work–Energy Theorem and Kinetic Energy 147
Check Your Understanding
(The answers are given at the end of the book.) 1. Two forces F1
→ and F2
→ are acting on the box shown in CYU
Figure 6.1, causing the box to move across the fl oor. The two force vectors are drawn to scale. Which one of the following statements is correct? (a) F2
→ does more work than F1
→ does.
(b) F1 →
does more work than F2 →
does. (c) Both forces do the same amount of work. (d) Neither force does any work.
2. A box is being moved with a velocity v→ by a force P→ (in the same direction as v→) along a level horizontal fl oor. The normal force is FN
→ , the kinetic frictional force is fk
→ , and the weight is mg→.
Which one of the following statements is correct? (a) P→ does positive work, FN
→ and fk
→ do zero work, and mg→ does negative
work. (b) FN →
does positive work, P → and fk
→ do zero work, and mg→ does negative work. (c) fk
→ does posi-
tive work, FN →
and mg→ do zero work, and P→ does negative work. (d) P→ does positive work, FN →
and mg→ do zero work, and fk
→ does negative work.
3. A force does positive work on a particle that has a displacement pointing in the +x direction. This same force does negative work on a particle that has a displacement pointing in the +y direction. In which quadrant of the x, y coordinate system does the force lie? (a) First (b) Second (c) Third (d) Fourth
4. A suitcase is hanging straight down from your hand as you ride an escalator. Your hand exerts a force on the suitcase, and this force does work. This work is (a) positive when you ride up and negative when you ride down, (b) negative when you ride up and positive when you ride down, (c) positive when you ride up or down, (d) negative when you ride up or down.
6.2 The Work–Energy Theorem and Kinetic Energy Most people expect that if you do work, you get something as a result. In physics, when a net force performs work on an object, there is always a result from the eff ort. The result is a change in the kinetic energy of the object. As we will now see, the relationship that relates work to the change in kinetic energy is known as the work–energy theorem. This theorem is obtained by bringing together three basic concepts that we’ve already learned about. First, we’ll apply Newton’s
CYU FIGURE 6.1
F2
F1
θ
the displacement, so they do no work. Only the static frictional force does work, since it acts in the x direction. To determine the frictional force, we note that the crate does not slip and, therefore, must have the same acceleration of a = +1.5 m/s2 as does the truck. The force creating this acceleration is the static frictional force, and, knowing the mass of the crate and its acceleration, we can use Newton’s second law to obtain its magnitude. Then, knowing the frictional force and the displacement, we can determine the total work done on the crate.
Solution From Newton’s second law, we fi nd that the magnitude fs of the static frictional force is
fs = ma = (120 kg)(1.5 m /s2) = 180 N
The total work is that done by the static frictional force and is
W = ( fs cos θ)s = (180 N)(cos 0°)(65 m) = 1.2 × 104 J (6.1)
The work is positive, because the frictional force is in the same direction as the displacement (𝜃 = 0°).
s
+y
+x
FN
fs
W
(a)
(b) Free-body diagram for the crate
FIGURE 6.4 (a) The truck and crate are accelerating to the right for a distance of s = 65 m. (b) The free-body diagram for the crate.
148 CHAPTER 6 Work and Energy
second law of motion, ΣF = ma, which relates the net force ΣF to the acceleration a of an object. Then, we’ll determine the work done by the net force when the object moves through a certain distance. Finally, we’ll use Equation 2.9, one of the equations of kinematics, to relate the distance and acceleration to the initial and fi nal speeds of the object. The result of this approach will be the work–energy theorem.
To gain some insight into the idea of kinetic energy and the work–energy theorem, look at Interactive Figure 6.5, where a constant net external force Σ F
→ acts on an airplane of mass m. This net
force is the vector sum of all the external forces acting on the plane, and, for simplicity, it is assumed to have the same direction as the displacement s→. According to Newton’s second law, the net force produces an acceleration a, given by a = ΣF/m. Consequently, the speed of the plane changes from an initial value of υ0 to a fi nal value of υf.* Multiplying both sides of ΣF = ma by the distance s gives
(ΣF)s = mas Work done by net ext. force
The left side of this equation is the work done by the net external force. The term as on the right side can be related to υ0 and υf by using υf2 = υ02 + 2as (Equation 2.9) from the equations of kinematics. Solving this equation gives
as = 12 (υf2 − υ02)
Substituting this result into (ΣF)s = mas shows that
(ΣF)s = 12 mυf 2 − 1 2 mυ0 2
{
Work done by net ext. force
{
Final KE
{ Initial
KE
This expression is the work–energy theorem. Its left side is the work W done by the net external force, whereas its right side involves the diff erence between two terms, each of which has the form 12(mass)(speed)
2. The quantity 12(mass)(speed) 2 is called kinetic energy (KE) and plays a
signifi cant role in physics, as we will see in this chapter and later on in other chapters as well.
DEFINITION OF KINETIC ENERGY The kinetic energy KE of an object with mass m and speed υ is given by
KE = 12 mυ2 (6.2)
SI Unit of Kinetic Energy: joule (J)
The SI unit of kinetic energy is the same as the unit for work, the joule. Kinetic energy, like work, is a scalar quantity. These are not surprising observations, because work and kinetic energy are closely related, as is clear from the following statement of the work–energy theorem.
THE WORK–ENERGY THEOREM When a net external force does work W on an object, the kinetic energy of the object changes from its initial value of KE0 to a fi nal value of KEf, the diff erence between the two values being equal to the work:
W = KEf − KE0 = 12 mυf2 − 1 2 mυ02 (6.3)
}
s
v0 vf
Final kinetic energy = m f
2_ 1 2
1 2
Initial kinetic energy = m 0
2_
ΣFΣF
υ υ
INTERACTIVE FIGURE 6.5 A constant net external force Σ F→ acts over a displacement s→ and does work on the plane. As a result of the work done, the plane’s kinetic energy changes.
*For extra emphasis, the fi nal speed is now represented by the symbol υf, rather than υ.
6.2 The Work–Energy Theorem and Kinetic Energy 149
The work–energy theorem may be derived for any direction of the force relative to the displace- ment, not just the situation in Interactive Figure 6.5. In fact, the force may even vary from point to point along a path that is curved rather than straight, and the theorem remains valid. According to the work–energy theorem, a moving object has kinetic energy, because work was done to accelerate the object from rest to a speed υf.† Conversely, an object with kinetic energy can perform work, if it is allowed to push or pull on another object. Example 4 illustrates the work–energy theorem and considers a single force that does work to change the kinetic energy of a space probe.
†Strictly speaking, the work–energy theorem, as given by Equation 6.3, applies only to a single particle, which occupies a mathematical point in space. A macroscopic object, however, is a collection or system of particles and is spread out over a region of space. Therefore, when a force is applied to a macroscopic object, the point of application of the force may be anywhere on the object. To take into account this and other factors, a discussion of work and energy is required that is beyond the scope of this text. The interested reader may refer to A. B. Arons, The Physics Teacher, October 1989, p. 506.
Analyzing Multiple-Concept Problems
EXAMPLE 4 The Physics of an Ion Propulsion Drive
The space probe Deep Space 1 was launched October 24, 1998, and it used a type of engine called an ion propulsion drive. An ion propulsion drive generates only a weak force (or thrust), but can do so for long periods of time using only small amounts of fuel. Suppose the probe, which has a mass of 474 kg, is traveling at an initial speed of 275 m/s. No forces act on it except the 5.60 × 10‒2-N thrust of its engine. This external force F
→ is directed parallel to the displacement s→, which has a magnitude
of 2.42 × 109 m (see Figure 6.6). Determine the fi nal speed of the probe, assuming that its mass remains nearly constant.
Reasoning If we can determine the fi nal kinetic energy of the space probe, we can determine its fi nal speed, since kinetic energy is related to mass and speed according to Equation 6.2 and the mass of the probe is known. We will use the work–energy theorem (W = KEf ‒ KE0), along with the defi nition of work, to fi nd the fi nal kinetic energy.
Knowns and Unknowns The following list summarizes the data for this problem:
Description Symbol Value Comment Explicit Data Mass m 474 kg
Initial speed υ0 275 m/s
Magnitude of force F 5.60 × 10‒2 N
Magnitude of displacement s 2.42 × 109 m
Implicit Data
Angle between force F→ and displacement s→ θ 0° The force is parallel to the displacement.
Unknown Variable Final speed υf ?
FIGURE 6.6 An ion propulsion drive generates a single force F →
that points in the same direction as the displacement s→. The force performs positive work, causing the space probe to gain kinetic energy.
v0 F vf
s
F
Modeling the Problem
STEP 1 Kinetic Energy An object of mass m and speed υ has a kinetic energy KE given by Equation 6.2 as KE = 12mυ2. Using the subscript f to denote the fi nal kinetic energy and the fi nal speed of the probe, we have that
KEf = 1 2mυ 2f
Solving for υf gives Equation 1 at the right. The mass m is known but the fi nal kinetic energy KEf is not, so we will turn to Step 2 to evaluate it.
?
υf = √2(KEf)m (1)
150 CHAPTER 6 Work and Energy
In Example 4 only the force of the engine does work. If several external forces act on an object, they must be added together vectorially to give the net force. The work done by the net force can then be related to the change in the object’s kinetic energy by using the work–energy theorem, as in the next example.
STEP 2 The Work–Energy Theorem The work–energy theorem relates the fi nal kinetic energy KEf of the probe to its initial kinetic energy KE0 and the work W done by the force of the engine. According to Equation 6.3, this theorem is W = KEf ‒ KE0. Solving for KEf shows that
KEf = KE0 + W
The initial kinetic energy can be expressed as KE0 = 1 2mυ 20 , so the expression for the fi nal kinetic
energy becomes
KEf = 1 2mυ 20 + W
This result can be substituted into Equation 1, as indicated at the right. Note from the data table that we know the mass m and the initial speed υ0. The work W is not known and will be evaluated in Step 3.
STEP 3 Work The work W is that done by the net external force acting on the space probe. Since there is only the one force F→ acting on the probe, it is the net force. The work done by this force is given by Equation 6.1 as
W = (F cos θ)s
where F is the magnitude of the force, θ is the angle between the force and the displacement, and s is the magnitude of the displacement. All the variables on the right side of this equation are known, so we can substitute it into Equation 2, as shown in the right column.
Solution Algebraically combining the results of the three steps, we have
υf = √2(KEf)m = √ 2( 12 mυ02 + W )
m = √2 [
1 2 mυ02 + (F cos θ)s]
m
The fi nal speed of the space probe is
υf = √2[ 1 2 mυ 20 + (F cos θ)s]
m
= √2[ 1 2 (474 kg)(275 m/s)
2 + (5.60 × 10−2 N)(cos 0°)(2.42 × 109 m)]
474 kg = 805 m/s
Related Homework: Problem 22
STEP 1 STEP 2 STEP 3
?
υf = √2(KEf)m (1) KEf =
1 2mυ 20 + W (2)
υf = √2(KEf)m (1) KEf =
1 2mυ 20 + W (2)
W = (F cos θ)s
Analyzing Multiple-Concept Problems
EXAMPLE 5 | Downhill Skiing
A 58-kg skier is coasting down a 25° slope, as Figure 6.7a shows. Near the top of the slope, her speed is 3.6 m/s. She accelerates down the slope because of the gravitational force, even though a kinetic frictional force of magnitude 71 N opposes her motion. Ignoring air resistance, determine the speed at a point that is displaced 57 m downhill.
Reasoning The skier’s speed at a point 57 m downhill (her fi nal speed) depends on her fi nal kinetic energy. According to the work– energy theorem, her fi nal kinetic energy is related to her initial kinetic energy (which we can calculate directly) and the work done by the net external force that acts on her. The work can be evaluated directly from its defi nition.
6.2 The Work–Energy Theorem and Kinetic Energy 151
s
vo
vf
fk
FN
mg sin 25°
mg
mg cos 25° +x
+y
25°
25°
(a) (b) Free-body diagram for the skier
FIGURE 6.7 (a) A skier coasting downhill. (b) The free-body diagram for the skier.
Description Symbol Value Comment Explicit Data Mass m 58 kg
Initial speed υ0 3.6 m/s
Magnitude of kinetic frictional force f k 71 N
Magnitude of skier’s displacement s 57 m
Angle of slope above horizontal 25°
Implicit Data Angle between net force acting on skier and her displacement
θ 0° The skier is accelerating down the slope, so the direction of the net force is parallel to her displacement.
Unknown Variable Final speed υf ?
Modeling the Problem
STEP 1 Kinetic Energy The fi nal speed υf of the skier is related to her fi nal kinetic energy KEf and mass m by Equation 6.2:
KEf = 1 2 mυ 2f
Solving for υf gives Equation 1 at the right. Her mass is known, but her fi nal kinetic energy is not, so we turn to Step 2 to evaluate it.
STEP 2 The Work–Energy Theorem The fi nal kinetic energy KEf of the skier is related to her initial kinetic energy KE0 and the work W done by the net external force acting on her. This is according to the work–energy theorem (Equation 6.3): KEf = KE0 + W. The initial kinetic energy can be written as KE0 =
1 2 mυ 20 , so the expression for the fi nal kinetic energy
becomes
KEf = 1 2mυ 20 + W
This result can be substituted into Equation 1, as indicated at the right. The mass m and the initial speed υ0 are known. The work W is not known, and will be evaluated in Steps 3 and 4.
STEP 3 Work The work W done by the net external force acting on the skier is given by Equation 6.1 s
W = ( ΣF cos θ)s
where ΣF is the magnitude of the net force, θ is the angle between the net force and the displace- ment, and s is the magnitude of the displacement. This result can be substituted into Equation 2, as shown at the right. The variables θ and s are known (see the table of knowns and unknowns), and the net external force will be determined in Step 4.
?
υf = √2(KEf)m (1)
?
υf = √2(KEf)m (1) KEf =
1 2mυ 20 + W (2)
?
υf = √2(KEf)m (1) KEf =
1 2mυ 20 + W (2)
W = ( ΣF cos θ)s (3)
Knowns and Unknowns The data for this problem are listed below:
152 CHAPTER 6 Work and Energy
STEP 4 The Net External Force Figure 6.7b is a free-body diagram for the skier and shows the three external forces acting on her: the gravitational force mg→, the kinetic friction- al force fk
→ , and the normal force FN
→ . The net external force along the y axis is zero, because
there is no acceleration in that direction (the normal force balances the component mg cos 25° of the weight perpendicular to the slope). Using the data from the table of knowns and unknowns, we fi nd that the net external force along the x axis is
ΣF = mg sin 25° − f k = (58 kg)(9.80 m/s2)sin 25° − 71 N = 170 N
All the variables on the right side of this equation are known, so we substitute this expression into Equation 3 for the net external force (see the right column).
υf = √2(KEf)m (1) KEf =
1 2mυ 20 + W (2)
W = ( ΣF cos θ)s (3)
ΣF = mg sin 25° − f k = 170 N
Math Skills In Figure 6.7b the angle between the gravitational force and the ‒y axis equals the 25° angle of the slope. Figure 6.8 uses 𝛽 for this angle and helps to explain why 𝛽 = 25°. It shows the vertical directional line along which the gravitational force acts, as well as the slope and the x, y axes. Since this directional line is perpendicular to the ground, the triangle ABC is a right triangle. It follows, then, that 𝛼 + 25° = 90° or 𝛼 = 65°. Since the y axis is perpendicular to the slope, it is also true that 𝛼 + 𝛽 = 90°. Solving this equation for the angle 𝛽 and substituting 𝛼 = 65° gives
β = 90° − α = 90° − 65° = 25°
FIGURE 6.8 Math Skills drawing.
+y
+x
90° 25°
B
A
Vertical direction
C
Ground
β α
Solution Algebraically combining the four steps, we arrive at the following expression for the fi nal speed of the skier:
υf = √2(KEf)m = √ 2(12 mυ02 + W )
m = √2[
1 2 mυ02 + (170 N) (cos θ)s]
m
Referring to the table of knowns and unknowns for the values of the symbols in this result, we fi nd that the fi nal speed of the skier is
υf = √2[ 1 2 mυ 20 + (170 N)(cos θ)s]
m
= √2[ 1 2(58 kg)(3.6 m /s)
2 + (170 N)(cos 0°)(57 m)]
58 kg = 19 m/s
Related Homework: Problems 24, 28
STEP 1 STEP 2 STEP 3 and 4
6.3 Gravitational Potential Energy 153
Problem-Solving Insight Example 5 emphasizes that the work–energy theorem deals with the work done by the net external force. The work–energy theorem does not apply to the work done by an individual force, unless that force happens to be the only one present, in which case it is the net force.
If the work done by the net force is positive, as in Example 5, the kinetic energy of the object increases. If the work done is negative, the kinetic energy decreases. If the work is zero, the kinetic energy remains the same. Conceptual Example 6 explores these ideas further in a situation where the component of the net force along the direction of the displacement changes during the motion.
Check Your Understanding
(The answers are given at the end of the book.) 5. A sailboat is moving at a constant velocity. Is work being done by a net external force acting on the boat? 6. A ball has a speed of 15 m/s. Only one external force acts on the ball. After this force acts, the speed of
the ball is 7 m/s. Has the force done (a) positive, (b) zero, or (c) negative work on the ball? 7. A rocket is at rest on the launch pad. When the rocket is launched, its kinetic energy increases. Consider
all of the forces acting on the rocket during the launch, and decide whether the following statement is true or false: The amount by which the kinetic energy of the rocket increases during the launch is equal to the work done by the force generated by the rocket’s engine.
8. A net external force acts on a particle that is moving along a straight line. This net force is not zero. Which one of the following statements is correct? (a) The velocity, but not the kinetic energy, of the particle is changing. (b) The kinetic energy, but not the velocity, of the particle is changing. (c) Both the velocity and the kinetic energy of the particle are changing.
6.3 Gravitational Potential Energy Work Done by the Force of Gravity The gravitational force is a well-known force that can do positive or negative work, and Figure 6.10 helps to show how the work can be determined. This drawing depicts a basketball of mass m
CONCEPTUAL EXAMPLE 6 Work and Kinetic Energy
Figure 6.9 illustrates a satellite moving about the earth in a circular orbit and in an elliptical orbit. The only external force that acts on the satellite is the gravitational force. In which orbit does the kinetic energy of the satellite change, (a) the circular orbit or (b) the elliptical orbit? Reasoning The gravitational force is the only force acting on the satel- lite, so it is the net force. With this fact in mind, we will apply the work– energy theorem, which states that the work done by the net force equals the change in the kinetic energy.
Answer (a) is incorrect. For the circular orbit in Figure 6.9a, the gravi- tational force F
→ does no work on the satellite since the force is perpen-
dicular to the instantaneous displacement s→ at all times. Thus, the work done by the net force is zero, and according to the work–energy theorem (Equation 6.3), the kinetic energy of the satellite (and, hence, its speed) remains the same everywhere on the orbit.
Answer (b) is correct. For the elliptical orbit in Figure 6.9b, the gravi- tational force F
→ does do work. For example, as the satellite moves toward
the earth in the top part of Figure 6.9b, there is a component of F →
that points in the same direction as the displacement. Consequently, F
→ does
positive work during this part of the orbit, and the kinetic energy of the satellite increases. When the satellite moves away from the earth, as in the
lower part of Figure 6.9b, F →
has a component that points opposite to the displacement and, therefore, does negative work. As a result, the kinetic energy of the satellite decreases.
Related Homework: Problem 18
F s
(a)
F
s
(b)
F
s
FIGURE 6.9 (a) In a circular orbit, the gravitational force F →
is always perpendicular to the displacement s→ of the satellite and does no work. (b) In an elliptical orbit, there can be a component of the force along the displacement, and, consequently, work can be done.
h0
mg
mg hf
s
FIGURE 6.10 Gravity exerts a force mg→ on the basketball. Work is done by the gravitational force as the basketball falls from a height of h0 to a height of hf.
154 CHAPTER 6 Work and Energy
moving vertically downward, the force of gravity mg→ being the only force acting on the ball. The initial height of the ball is h0, and the fi nal height is hf, both distances measured from the earth’s surface. The displacement s→ is downward and has a magnitude of s = h0 ‒ hf. To calculate the work Wgravity done on the ball by the force of gravity, we use W = (F cos 𝜃)s with F = mg and 𝜃 = 0°, since the force and displacement are in the same direction:
Wgravity = (mg cos 0°)(h0 − h f ) = mg(h0 − h f ) (6.4)
Equation 6.4 is valid for any path taken between the initial and fi nal heights, and not just for the straight-down path shown in Figure 6.10. For example, the same expression can be derived for both paths shown in Figure 6.11. Thus, only the diff erence in vertical distances (h0 ‒ hf) need be considered when calculating the work done by gravity. Since the diff erence in the vertical distances is the same for each path in the drawing, the work done by gravity is the same in each case. We are assuming here that the diff erence in heights is small compared to the radius of the earth, so that the magnitude g of the acceleration due to gravity is the same at every height. Moreover, for positions close to the earth’s surface, we can use the value of g = 9.80 m/s2.
Only the diff erence h0 ‒ hf appears in Equation 6.4, so h0 and hf themselves need not be mea- sured from the earth. For instance, they could be measured relative to a level that is one meter above the ground, and h0 ‒ hf would still have the same value. Example 7 illustrates how the work done by gravity is used with the work–energy theorem.
h0
hf
FIGURE 6.11 An object can move along diff erent paths in going from an initial height of h0 to a fi nal height of hf. In each case, the work done by the gravitational force is the same [Wgravity = mg(h0 ‒ hf)], since the change in vertical distance (h0 ‒ hf) is the same.
FIGURE 6.12 (a) A gymnast bounces on a trampoline. (b) The gymnast moves upward with an initial speed υ0 and reaches maximum height with a fi nal speed of zero.
f = 0 m/s
0hf
h0
(b)
υ
υ
(a)
© M
ic ha
el C
hr is
to ph
er B
ro w
n/ M
ag nu
m P
ho to
s
EXAMPLE 7 A Gymnast on a Trampoline
A gymnast springs vertically upward from a trampoline as in Figure 6.12a. The gymnast leaves the trampoline at a height of 1.20 m and reaches a maximum height of 4.80 m before falling back down. All heights are measured with respect to the ground. Ignoring air resis- tance, determine the initial speed υ0 with which the gymnast leaves the trampoline.
Reasoning We can fi nd the initial speed of the gymnast (mass = m) by using the work–energy theorem, provided the work done by the net external force can be determined. Since only the gravitational force acts on the gymnast in the air, it is the net force, and we can evaluate the work by using the relation Wgravity = mg(h0 ‒ hf).
Solution Figure 6.12b shows the gymnast moving upward. The initial and fi nal heights are h0 = 1.20 m and hf = 4.80 m, respectively. The initial speed is υ0 and the fi nal speed is υf = 0 m/s, since the gymnast comes to a momentary halt at the highest point. Since υf = 0 m/s, the fi nal kinetic energy is KEf = 0 J, and the work–energy theorem becomes W = KEf ‒ KE0 = ‒KE0. The work W is that due to gravity, so this theorem reduces to
Wgravity = mg(h0 − hf) = − 1 2 mυ 20
Solving for υ0 gives
υ0 = √−2g(h0 − hf) = √−2(9.80 m/s2)(1.20 m − 4.80 m) = 8.40 m /s
6.4 Conservative Versus Nonconservative Forces 155
Gravitational Potential Energy An object in motion has kinetic energy. There are also other types of energy. For example, an object may possess energy by virtue of its position relative to the earth and is said to have gravi- tational potential energy. A pile driver, for instance, is used to pound “piles,” or structural support beams, into the ground. The device contains a massive hammer that is raised to a height h and dropped (see Figure 6.13), so the hammer has the potential to do the work of driving the pile into the ground. The greater the height h, the greater is the potential for doing work, and the greater is the gravitational potential energy.
Now, let’s obtain an expression for the gravitational potential energy. Our starting point is Equation 6.4 for the work done by the gravitational force as an object moves from an initial height h0 to a fi nal height hf:
Wgravity =
mgh0 − mghf (6.4)
This shows that the work done by the gravitational force is equal to the diff erence between the initial and fi nal values of the quantity mgh. The value of mgh is larger when the height is larger and smaller when the height is smaller. We identify the quantity mgh as the gravitational poten- tial energy. The concept of potential energy is associated only with a type of force known as a “conservative” force, as we will discuss in Section 6.4.
DEFINITION OF GRAVITATIONAL POTENTIAL ENERGY The gravitational potential energy PE is the energy that an object of mass m has by virtue of its position relative to the surface of the earth. That position is measured by the height h of the object relative to an arbitrary zero level:
PE = mgh (6.5)
SI Unit of Gravitational Potential Energy: joule (J)
Gravitational potential energy, like work and kinetic energy, is a scalar quantity and has the same SI unit as they do—the joule. It is the diff erence between two potential energies that is related by Equation 6.4 to the work done by the force of gravity. Therefore, the zero level for the heights can be taken anywhere, as long as both h0 and hf are measured relative to the same zero level. The gravitational potential energy depends on both the object and the earth (m and g, respectively), as well as the height h. Therefore, the gravitational potential energy belongs to the object and the earth as a system, although one often speaks of the object alone as possessing the gravitational potential energy.
Check Your Understanding
(The answer is given at the end of the book.) 9. In a simulation on earth, an astronaut in his space suit climbs up a vertical ladder. On the moon, the same
astronaut makes the exact same climb. Which one of the following statements correctly describes how the gravitational potential energy of the astronaut changes during the climb? (a) It changes by a greater amount on the earth. (b) It changes by a greater amount on the moon. (c) The change is the same in both cases.
6.4 Conservative Versus Nonconservative Forces The gravitational force has an interesting property that when an object is moved from one place to another, the work done by the gravitational force does not depend on the choice of path. In Figure 6.11, for instance, an object moves from an initial height h0 to a fi nal height hf along two
Gravitational potential energy
PE0 (initial) {
Gravitational potential energy
PEf (fi nal)
{
mg
Hammer
Pile
h
FIGURE 6.13 In a pile driver, the gravitational potential energy of the hammer relative to the ground is PE = mgh.
156 CHAPTER 6 Work and Energy
diff erent paths. As Section 6.3 discusses, the work done by gravity depends only on the initial and fi nal heights, and not on the path between these heights. For this reason, the gravitational force is called a conservative force, according to version 1 of the following defi nition:
DEFINITION OF A CONSERVATIVE FORCE Version 1 A force is conservative when the work it does on a moving object is indepen- dent of the path between the object’s initial and fi nal positions. Version 2 A force is conservative when it does no net work on an object moving around a closed path, starting and fi nishing at the same point.
Figure 6.14 helps us to illustrate version 2 of the defi nition of a conservative force. The picture shows a roller coaster car racing through dips and double dips, ultimately returning to its starting point. This kind of path, which begins and ends at the same place, is called a closed path. Gravity provides the only force that does work on the car, assuming that there is no friction or air resistance. Of course, the track exerts a normal force, but this force is always directed per- pendicular to the motion and does no work. On the downward parts of the trip, the gravitational force does positive work, increasing the car’s kinetic energy. Conversely, on the upward parts of the motion, the gravitational force does negative work, decreasing the car’s kinetic energy. Over the entire trip, the gravitational force does as much positive work as negative work, so the net work is zero, and the car returns to its starting point with the same kinetic energy it had at the start. Therefore, consistent with version 2 of the defi nition of a conservative force, Wgravity = 0 J for a closed path.
The gravitational force is our fi rst example of a conservative force. Later, we will encounter others, such as the elastic force of a spring and the electrical force of electrically charged par- ticles. With each conservative force we will associate a potential energy, as we have already done in the gravitational case (see Equation 6.5). For other conservative forces, however, the algebraic form of the potential energy will diff er from that in Equation 6.5.
Not all forces are conservative. A force is nonconservative if the work it does on an object moving between two points depends on the path of the motion between the points. The kinetic frictional force is one example of a nonconservative force. When an object slides over a surface and kinetic friction is present, the frictional force points opposite to the sliding motion and does negative work. Between any two points, greater amounts of work are done over longer paths between the points, so that the work depends on the choice of path. Thus, the kinetic frictional force is nonconservative. Air resistance is another nonconservative force. The concept of poten- tial energy is not defi ned for a nonconservative force.
For a closed path, the total work done by a nonconservative force is not zero as it is for a conservative force. In Figure 6.14, for instance, a frictional force would oppose the motion and slow down the car. Unlike gravity, friction would do negative work on the car throughout the entire trip, on both the up and down parts of the motion. Assuming that the car makes it back to the starting point, the car would have less kinetic energy than it had originally. Table 6.2 gives some examples of conservative and nonconservative forces.
Start
FIGURE 6.14 A roller coaster track is an example of a closed path.
TABLE 6.2 Some Conservative and Nonconservative Forces
Conservative Forces Gravitational force (Ch. 4)
Elastic spring force (Ch. 10)
Electric force (Ch. 18, 19)
Nonconservative Forces Static and kinetic frictional forces
Air resistance
Tension
Normal force
Propulsion force of a rocket
6.5 The Conservation of Mechanical Energy 157
In normal situations, conservative forces (such as gravity) and nonconservative forces (such as friction and air resistance) act simultaneously on an object. Therefore, we write the work W done by the net external force as W = Wc + Wnc, where Wc is the work done by the conservative forces and Wnc is the work done by the nonconservative forces. According to the work–energy theorem, the work done by the net external force is equal to the change in the object’s kinetic energy, or Wc + Wnc =
1 2 mυf2 −
1 2 mυ02. If the only conservative force acting is the gravitational
force, then Wc = Wgravity = mg(h0 ‒ hf), and the work–energy theorem becomes
mg(h0 − hf) + Wnc = 1 2 mυf2 −
1 2 mυ02
The work done by the gravitational force can be moved to the right side of this equation, with the result that
Wnc = ( 1 2mυf 2 −
1 2 mυ0 2) + (mghf − mgh0 ) (6.6)
In terms of kinetic and potential energies, we fi nd that
Wnc =
(KEf − KE0) + (PEf − PE0 ) (6.7a)
Equation 6.7a states that the net work Wnc done by all the external nonconservative forces equals the change in the object’s kinetic energy plus the change in its gravitational potential energy. It is customary to use the delta symbol (∆) to denote such changes; thus, ∆KE = (KEf ‒ KE0) and ∆PE = (PEf ‒ PE0). With the delta notation, the work–energy theorem takes the form
Wnc = ∆KE + ∆PE (6.7b)
In the next two sections, we will show why the form of the work–energy theorem expressed by Equations 6.7a and 6.7b is useful.
⏟⎵⎵⏟⎵⎵⏟ Change in kinetic
energy
⏟⎵⎵⏟⎵⎵⏟ Change in
gravitational potential energy
Net work done by nonconservative
forces
⏟
6.5 The Conservation of Mechanical Energy The concept of work and the work–energy theorem have led us to the conclusion that an object can possess two kinds of energy: kinetic energy, KE, and gravitational potential energy, PE. The sum of these two energies is called the total mechanical energy E, so that E = KE + PE. Later on we will update this defi nition to include other types of potential energy in addition to the gravitational form. The concept of total mechanical energy will be extremely useful in describing the motion of objects.
Math Skills The change in both the kinetic and the potential energy is always the fi nal value minus the initial value: ∆KE = KEf ‒ KE0 and ∆PE = PEf ‒ PE0. For example, consider a skier starting from rest at the top of a steep ski jumping ramp, gathering speed on the way down, and leaving the end of the ramp at a high speed. The initial kinetic energy is KE0 = 0 J, since the skier is at rest at the top. The fi nal kinetic energy, however, is KEf =
1 2 mυ 2f , since the skier leaves the ramp at a high
speed υf. The kinetic energy increases from zero to a nonzero value, so the change in kinetic energy has a positive value of
∆KE = KEf − KE0 = 1 2 mυ 2f − 0 J =
1 2 mυ 2f
If ∆KE were written incorrectly as the initial value minus the fi nal value or ∆KE = KE0 ‒ KEf, the skier’s kinetic energy would appear to change by the following amount:
Incorrect Equation
∆KE = KE0 − KEf = 0 J − 1 2 mυ 2f = −
1 2 mυ 2f
This change is negative. It would imply that the skier, although starting at the top with zero kinetic energy, nevertheless loses kinetic energy on the way down! This is nonsense and would lead to serious errors in problem solving.
158 CHAPTER 6 Work and Energy
By rearranging the terms on the right side of Equation 6.7a, the work–energy theorem can be expressed in terms of the total mechanical energy:
Wnc = (KEf − KE0 ) + (PEf − PE0) (6.7a) = (KEf + PEf) − (KE0 + PE0 )
Ef E0 or
Wnc = Ef − E0 (6.8)
Remember: Equation 6.8 is just another form of the work–energy theorem. It states that Wnc, the net work done by external nonconservative forces, changes the total mechanical energy from an initial value of E0 to a fi nal value of Ef.
The conciseness of the work–energy theorem in the form Wnc = Ef ‒ E0 allows an important basic principle of physics to stand out. This principle is known as the conservation of mechanical energy. Suppose that the net work Wnc done by external nonconservative forces is zero, so Wnc = 0 J. Then, Equation 6.8 reduces to
Ef = E0 (6.9a)
12 mυf 2 + mghf = 1 2 mυ0 2 + mgh0 (6.9b)
Ef E0 Equation 6.9a indicates that the fi nal mechanical energy is equal to the initial mechanical energy. Consequently, the total mechanical energy remains constant all along the path between the ini- tial and fi nal points, never varying from the initial value of E0. A quantity that remains constant throughout the motion is said to be “conserved.” The fact that the total mechanical energy is conserved when Wnc = 0 J is called the principle of conservation of mechanical energy.
THE PRINCIPLE OF CONSERVATION OF MECHANICAL ENERGY The total mechanical energy (E = KE + PE) of an object remains constant as the object moves, provided that the net work done by external nonconservative forces is zero, Wnc = 0 J.
The principle of conservation of mechanical energy off ers keen insight into the way in which the physical universe operates. While the sum of the kinetic and potential energies at any point is conserved, the two forms may be interconverted or transformed into one another. Kinetic energy of motion is converted into potential energy of position, for instance, when a moving object coasts up a hill. Conversely, potential energy is converted into kinetic energy when an object is allowed to fall. Interactive Figure 6.15 shows such transformations of energy for a bobsled run, assuming that nonconservative forces, such as friction and wind resistance, can be ignored. The normal force, being directed perpendicular to the path, does no work. Only the force of gravity does work, so the total mechanical energy E remains constant at all points along the run. The conservation principle is well known for the ease with which it can be applied, as in the follow- ing example.
⏟⎵⎵⏟⎵⎵⏟ ⏟⎵⎵⏟⎵⎵⏟
⏟⎵⎵⎵⏟⎵⎵⎵⏟ ⏟⎵⎵⎵⏟⎵⎵⎵⏟
KE
0 J
200 000 J
400 000 J
600 000 J
PE
600 000 J
400 000 J
200 000 J
0 J
E = KE + PE
600 000 J
600 000 J
600 000 J
600 000 J
v0 = 0 m/s
INTERACTIVE FIGURE 6.15 If friction and wind resistance are ignored, a bobsled run illustrates how kinetic and potential energy can be interconverted, while the total mechanical energy remains constant. The total mechanical energy is 600 000 J, being all potential energy at the top and all kinetic energy at the bottom.
6.5 The Conservation of Mechanical Energy 159
Examples 9 and 10 emphasize that the principle of conservation of mechanical energy can be applied even when forces act perpendicular to the path of a moving object.
EXAMPLE 8 A Daredevil Motorcyclist
A motorcyclist is trying to leap across the canyon shown in Figure 6.16 by driving horizontally off the cliff at a speed of 38.0 m/s. Ignoring air resis- tance, fi nd the speed with which the cycle strikes the ground on the other side.
Reasoning Once the cycle leaves the cliff , no forces other than gravity act on the cycle, since air resistance is being ignored. Thus, the work done by external nonconservative forces is zero, Wnc = 0 J. Accordingly, the principle of conservation of mechanical energy holds, so the total mechanical energy is the same at the fi nal and initial positions of the motorcycle. We will use this important observation to determine the fi nal speed of the cyclist.
Problem-Solving Insight Be on the alert for factors, such as the mass m here in Example 8, that sometimes can be eliminated algebraically when using the conservation of mechanical energy.
Solution The principle of conservation of mechanical energy is written as
12 mυf 2 + mghf = 1 2 mυ0 2 + mgh0 (6.9b)
Ef E0 The mass m of the rider and cycle can be eliminated algebraically from this equation, since m appears as a factor in every term. Solving for υf gives
υf = √υ0 2 + 2g(h0 − hf)
υf = √(38.0 m /s) 2 + 2(9.80 m /s2)(70.0 m − 35.0 m) = 46.2 m /s
⏟⎵⎵⏟⎵⎵⏟ ⏟⎵⎵⎵⏟⎵⎵⎵⏟
0 = 38.0 m/s
f h0 = 70.0 m
hf = 35.0 m
υ
υ
FIGURE 6.16 A daredevil jumping a canyon.
CONCEPTUAL EXAMPLE 9 The Favorite Swimming Hole
A rope is tied to a tree limb. It is used by a swimmer who, starting from rest, swings down toward the water below, as in Figure 6.17. Only two forces act on him during his descent, the nonconservative force T→, which is due to the tension in the rope, and his weight, which is due to the con- servative gravitational force. There is no air resistance. His initial height h0 and fi nal height hf are known. Can we use the principle of conservation of mechanical energy to fi nd his speed υf at the point where he lets go of the rope, even though a nonconservative external force is present? (a) Yes. (b) No.
Reasoning The principle of conservation of mechanical energy can be used even in the presence of nonconservative forces, provided that the net work Wnc done by the nonconservative forces is zero. Wnc = 0 J.
Answer (b) is incorrect. The mere presence of nonconservative forces does not prevent us from applying the principle of conservation of mechan- ical energy. The deciding factor is whether the net work done by the non- conservative forces is zero. In this case, the tension force T→ is always perpendicular to the circle (see Figure 6.17). Thus, the angle 𝜃 between T→ and the instantaneous displacement of the person is always 90°. According
h0
hf
v0 = 0 m/s
T
vf
FIGURE 6.17 During the downward swing, the tension T→ in the rope acts perpendicular to the circular arc and, hence, does no work on the person.
160 CHAPTER 6 Work and Energy
The next example illustrates how the conservation of mechanical energy is applied to the breathtaking drop of a roller coaster.
to Equation 6.1, the work is proportional to the cosine of this angle, or cos 90°, which is zero, with the result that the work is also zero. As a result, the tension here does not prevent us from using the conservation principle.
Problem-Solving Insight When nonconservative forces are perpendicular to the motion, we can still use the principle of conservation of mechanical energy, because such “perpen- dicular” forces do no work.
Answer (a) is correct. As the person swings downward, he follows a circular path, as shown in Figure 6.17. Since the tension force is the only nonconservative force acting and is always perpendicular to this path, the corresponding net work is Wnc = 0 J, and we can apply the principle of conservation of mechanical energy to fi nd the speed υf.
Related Homework: Problems 42, 86
EXAMPLE 10 The Physics of a Giant Roller Coaster
The Kingda Ka is a giant among roller coasters (see Figure 6.18). Located in Jackson Township, New Jersey, the ride includes a vertical drop of 127 m. Suppose that the coaster has a speed of 6.0 m/s at the top of the drop. Neglect friction and air resistance and fi nd the speed of the riders at the bottom.
Reasoning Since we are neglecting friction and air resistance, we may set the work done by these forces equal to zero. A normal force from the seat acts on each rider, but this force is perpendicular to the motion, so it does not do any work. Thus, the work done by external nonconservative forces is zero, Wnc = 0 J, and we may use the principle of conservation of mechanical energy to fi nd the speed of the riders at the bottom.
Solution The principle of conservation of mechanical energy states that
12mυf 2 + mghf = 1 2mυ0 2 + mgh0 (6.9b)
Ef E0
The mass m of the rider appears as a factor in every term in this equation and can be eliminated algebraically. Solving for the fi nal speed gives
υf = √υ02 + 2g(h0 − hf)
υf = √(6.0 m /s)2 + 2(9.80 m /s2)(127 m) = 50.3 m /s (112 mi/h)
where the vertical drop is h0 ‒ hf = 127 m.
⏟⎵⎵⏟⎵⎵⏟ ⏟⎵⎵⎵⏟⎵⎵⎵⏟
FIGURE 6.18 The Kingda Ka roller coaster in Six Flags Great Adventure, located in Jackson Township, New Jersey, is a giant. It includes a vertical drop of 127 m.
Si x
Fl ag
s/ Sp
la sh
N ew
s/ N
ew sC
om
When applying the principle of conservation of mechanical energy in solving problems, we have been using the following reasoning strategy:
REASONING STRATEGY Applying the Principle of Conservation of Mechanical Energy 1. Identify the external conservative and nonconservative forces that act on the object.
For this principle to apply, the total work done by nonconservative forces must be zero, Wnc = 0 J. A nonconservative force that is perpendicular to the displacement of the object does no work, for example.
2. Choose the location where the gravitational potential energy is taken to be zero. This location is arbitrary but must not be changed during the course of solving a problem.
3. Set the fi nal total mechanical energy of the object equal to the initial total mechanical energy, as in Equations 6.9a and 6.9b. The total mechanical energy is the sum of the kinetic and potential energies.
6.6 Nonconservative Forces and the Work–Energy Theorem 161
Check Your Understanding
(The answers are given at the end of the book.) 10. Suppose the total mechanical energy of an object is conserved. Which one or more of the following
statements is/are true? (a) If the kinetic energy decreases, the gravitational potential energy increases. (b) If the gravitational potential energy decreases, the kinetic energy increases. (c) If the kinetic energy does not change, the gravitational potential energy also does not change.
11. In Example 10 the Kingda Ka roller coaster starts with a speed of 6.0 m/s at the top of the drop and at- tains a speed of 50.3 m/s when it reaches the bottom. If the roller coaster were then to start up an identi- cal hill, what speed would it attain when it reached the top? Assume that friction and air resistance are absent. (a) Greater than 6.0 m/s (b) Exactly 6.0 m/s (c) Between 0 m/s and 6.0 m/s (d) 0 m/s
12. CYU Figure 6.2 shows an empty fuel tank about to be released by three diff erent jet planes. At the moment of release, each plane has the same speed, and each tank is at the same height above the ground. However, the directions of the velocities of the planes are diff erent. Which tank has the largest speed upon hitting the ground? Ignore friction and air resistance. (a) A (b) B (c) C (d) Each tank hits the ground with the same speed.
13. In which one or more of the following situations is the principle of conservation of mechanical energy obeyed? (a) An object moves uphill with an increasing speed. (b) An object moves uphill with a decreas- ing speed. (c) An object moves uphill with a constant speed. (d) An object moves downhill with an increasing speed. (e) An ob- ject moves downhill with a de- creasing speed. (f) An object moves downhill with a constant speed.
6.6 Nonconservative Forces and the Work–Energy Theorem Most moving objects experience nonconservative forces, such as friction, air resistance, and pro- pulsive forces, and the work Wnc done by the net external nonconservative force is not zero. In these situations, the diff erence between the fi nal and initial total mechanical energies is equal to Wnc, according to Wnc = Ef − E0 (Equation 6.8). Consequently, the total mechanical energy is not conserved. The next two examples illustrate how Equation 6.8 is used when nonconservative forces are present and do work.
CBAFuel tank
CYU FIGURE 6.2
EXAMPLE 11 The Kingda Ka Revisited
In Example 10, we ignored nonconservative forces, such as friction. In reality, however, such forces are present when the roller coaster descends. The actual speed of the riders at the bottom is 45.0 m/s, which is less than that determined in Example 10. Assuming again that the coaster has a speed of 6.0 m/s at the top, fi nd the work done by nonconservative forces on a 55.0-kg rider during the descent from a height h0 to a height hf, where h0 ‒ hf = 127 m.
Reasoning Since the speed at the top, the fi nal speed, and the vertical drop are given, we can determine the initial and fi nal total mechanical energies of the rider. The work–energy theorem, Wnc = Ef ‒ E0, can then be used to determine the work Wnc done by the nonconservative forces.
Problem-Solving Insight As illustrated here and in Exam- ple 3, a nonconservative force such as friction can do nega- tive or positive work. It does negative work when it has a
component opposite to the displacement and slows down the object. It does positive work when it has a component in the direction of the displacement and speeds up the object.
Solution The work–energy theorem is
Wnc = ( 1 2 mυf
2 + mghf) − ( 1 2 mυ0
2 + mgh0 ) (6.8)
Ef E0 Rearranging the terms on the right side of this equation gives
Wnc = 1 2 m(υf
2 − υ02) − mg(h0 − hf)
Wnc = 1 2(55.0 kg)[(45.0 m/s)
2 − (6.0 m/s)2] −
(55.0 kg)(9.80 m/s2)(127 m) = −1.4 × 104 J
⏟⎵⎵⏟⎵⎵⏟ ⏟⎵⎵⎵⏟⎵⎵⎵⏟
162 CHAPTER 6 Work and Energy
Check Your Understanding
(The answers are given at the end of the book.) 14. A net external nonconservative force does positive work on a particle. Based solely on this informa-
tion, you are justifi ed in reaching only one of the following conclusions. Which one is it? (a) The kinetic and potential energies of the particle both decrease. (b) The kinetic and potential energies of the particle both increase. (c) Neither the kinetic nor the potential energy of the particle changes. (d) The total mechanical energy of the particle decreases. (e) The total mechanical energy of the particle increases.
15. In one case, a sports car, its engine running, is driven up a hill at a constant speed. In another case, a truck approaches a hill, and its driver turns off the engine at the bottom of the hill. The truck then coasts up the hill. Which vehicle is obeying the principle of conservation of mechanical energy? Ignore friction and air resistance. (a) Both the sports car and the truck (b) Only the sports car (c) Only the truck
6.7 Power In many situations, the time it takes to do work is just as important as the amount of work that is done. Consider two automobiles that are identical in all respects (e.g., both have the same mass), except that one has a “souped-up” engine. The car with the souped-up engine can go from 0 to 27 m/s (60 mph) in 4 seconds, while the other car requires 8 seconds to achieve the same speed. Each engine does work in accelerating its car, but one does it more quickly. Where cars are con- cerned, we associate the quicker performance with an engine that has a larger horsepower rating. A large horsepower rating means that the engine can do a large amount of work in a short time. In physics, the horsepower rating is just one way to measure an engine’s ability to generate power. The idea of power incorporates both the concepts of work and time, for power is work done per unit time.
EXAMPLE 12 Fireworks
A 0.20-kg rocket in a fi reworks display is launched from rest and follows an erratic fl ight path to reach the point P, as Figure 6.19 shows. Point P is 29 m above the starting point. In the process, 425 J of work is done on the rocket by the nonconservative force generated by the burning propellant. Ignoring air resistance and the mass lost due to the burning propellant, fi nd the speed υf of the rocket at the point P.
Reasoning The only nonconservative force acting on the rocket is the force generated by the burning propellant, and the work done by this force is Wnc = 425 J. Because work is done by a nonconservative force, we use the work–energy theorem in the form Wnc = Ef ‒ E0 to fi nd the fi nal speed υf of the rocket.
Solution From the work–energy theorem we have Wnc = (
1 2mυf2 + mghf) − (
1 2mυ02 + mgh0) (6.8)
Solving this expression for the fi nal speed of the rocket and noting that the initial speed of the rocket at rest is υ0 = 0 m/s, we get
υf = √2[Wnc + 1 2 mυ0
2 − mg(hf − h0) ] m
υf = √2[425 J + 1 2 (0.20 kg)(0 m/s)
2 − (0.20 kg)(9.80 m/s2)(29 m)]
0.20 kg
= 61 m/s
FIGURE 6.19 A fi reworks rocket, moving along an erratic fl ight path, reaches a point P that is 29 m above the launch point.
v0 = 0 m/s
hf
h0
29 m
P
vf
6.7 Power 163
DEFINITION OF AVERAGE POWER Average power P is the average rate at which work W is done, and it is obtained by dividing W by the time t required to perform the work:
P = Work Time
= W t
(6.10a)
SI Unit of Power: joule/s = watt (W)
The defi nition of average power presented in Equation 6.10a involves work. However, the work–energy theorem relates the work done by a net external force to the change in the energy of the object (see, for example, Equations 6.3 and 6.8). Therefore, we can also defi ne average power as the rate at which the energy is changing, or as the change in energy divided by the time during which the change occurs:
P = Change in energy
Time (6.10b)
Since work, energy, and time are scalars, power is also a scalar. The unit in which power is expressed is that of work divided by time, or a joule per second in SI units. One joule per second is called a watt (W), in honor of James Watt (1736–1819), developer of the steam engine. The unit of power in the BE system is the foot · pound per second (ft · lb/s), although the familiar horsepower (hp) unit is used frequently for specifying the power generated by electric motors and internal combustion engines:
1 horsepower = 550 foot · pounds/second = 745.7 watts Table 6.3 summarizes the units for power in the various systems of measurement.
BIO THE PHYSICS OF . . . human metabolism. Equation 6.10b provides the basis for understanding the production of power in the human body. In this context the “Change in energy” on the right-hand side of the equation refers to the energy produced by metabolic pro- cesses, which, in turn, is derived from the food we eat. Table 6.4 gives typical metabolic rates of energy production needed to sustain various activities. Running at 15 km/h (9.3 mi/h), for example, requires metabolic power suffi cient to operate eighteen 75-watt light bulbs, and the metabolic power used in sleeping would operate a single 75-watt bulb.
An alternative expression for power can be obtained from Equation 6.1, which indicates that the work W done when a constant net force of magnitude F points in the same direction as the displacement is W = (F cos 0°)s = Fs. Dividing both sides of this equation by the time t it takes for the force to move the object through the distance s, we obtain
W t
= Fs t
But W/t is the average power P, and s/t is the average speed υ, so that
P = F υ (6.11)
Check Your Understanding
(The answers are given at the end of the book.) 16. Engine A has a greater power rating than engine B. Which one of the following statements correctly
describes the abilities of these engines to do work? (a) Engines A and B can do the same amount of
TABLE 6.4 Human Metabolic Ratesa
Activity Rate (watts) Running (15 km/h) 1340 W
Skiing 1050 W
Biking 530 W
Walking (5 km/h) 280 W
Sleeping 77 W aFor a young 70-kg male.
TABLE 6.3 Units of Measurement for Power
System Work ÷ Time = Power SI joule (J) second (s) watt (W)
CGS erg second (s) erg per second (erg/s)
BE foot · pound (ft · lb) second (s) foot · pound per second (ft · lb/s)
164 CHAPTER 6 Work and Energy
work, but engine A can do it more quickly. (b) Engines A and B can do the same amount of work in the same amount of time. (c) In the same amount of time, engine B can do more work than engine A.
17. Is it correct to conclude that one engine is doing twice the work that another is doing just because it is generating twice the power? (a) Yes (b) No
6.8 Other Forms of Energy and the Conservation of Energy Up to now, we have considered only two types of energy, kinetic energy and gravitational poten- tial energy. There are many other types, however. Electrical energy is used to run electrical appli- ances. Energy in the form of heat is utilized in cooking food. Moreover, the work done by the kinetic frictional force often appears as heat, as you can experience by rubbing your hands back and forth. When gasoline is burned, some of the stored chemical energy is released and does the work of moving cars, airplanes, and boats. The chemical energy stored in food provides the energy needed for metabolic processes.
The research of many scientists, most notably Albert Einstein, led to the discovery that mass itself is one manifestation of energy. Einstein’s famous equation, E0 = mc2, describes how mass m and energy E0 are related, where c is the speed of light in a vacuum and has a value of 3.00 × 108 m/s. Because the speed of light is so large, this equation implies that very small masses are equivalent to large amounts of energy. The relationship between mass and energy will be dis- cussed further in Chapter 28.
We have seen that kinetic energy can be converted into gravitational potential energy and vice versa. In general, energy of all types can be converted from one form to another.
BIO THE PHYSICS OF . . . transforming chemical energy in food into mechanical energy. Part of the chemical energy stored in food, for example, is transformed into gravita- tional potential energy when a hiker climbs a mountain. Suppose a 65-kg hiker eats a 250-Calorie* snack, which contains 1.0 × 106 J of chemical energy. If this were 100% converted into potential energy mg(hf ‒ h0), the change in height would be
hf − h0 = 1.0 × 106 J
(65 kg)(9.8 m/s2) = 1600 m
At a more realistic conversion effi ciency of 50%, the change in height would be 800 m. Similarly, in a moving car the chemical energy of gasoline is converted into kinetic energy, as well as into electrical energy and heat.
Whenever energy is transformed from one form to another, it is found that no energy is gained or lost in the process; the total of all the energies before the process is equal to the total of the energies after the process. This observation leads to the following important principle:
THE PRINCIPLE OF CONSERVATION OF ENERGY Energy can neither be created nor destroyed, but can only be converted from one form to another.
Learning how to convert energy from one form to another more effi ciently is one of the main goals of modern science and technology.
6.9 Work Done by a Variable Force The work W done by a constant force (constant in both magnitude and direction) is given by Equation 6.1 as W = (F cos 𝜃)s. Quite often, situations arise in which the force is not constant but changes with the displacement of the object. For instance, Animated Figure 6.20a shows an
*Energy content in food is typically given in units called Calories, which we will discuss in Section 12.7.
6.9 Work Done by a Variable Force 165
archer using a high-tech compound bow. This type of bow consists of a series of pulleys and strings that produce a force–displacement graph like that in Animated Figure 6.20b. One of the key fea- tures of the compound bow is that the force rises to a maximum as the string is drawn back, and then falls to 60% of this maximum value when the string is fully drawn. The reduced force at s = 0.500 m makes it much easier for the archer to hold the fully drawn bow while aiming the arrow.
When the force varies with the displacement, as in Animated Figure 6.20b, we cannot use the relation W = (F cos 𝜃)s to fi nd the work, because this equation is valid only when the force is constant. However, we can use a graphical method. In this method we divide the total displace- ment into very small segments, Δs1, Δs2, and so on (see Figure 6.21a). For each segment, the average value of the force component is indicated by a short horizontal line. For example, the short horizontal line for segment Δs1 is labeled (F cos 𝜃)1 in Figure 6.21a. We can then use this average value as the constant-force component in Equation 6.1 and determine an approximate value for the work ΔW1 done during the fi rst segment: ΔW1 = (F cos 𝜃)1 Δs1. But this work is just the area of the colored rectangle in the drawing. The word “area” here refers to the area of a rect- angle that has a width of Δs1 and a height of (F cos 𝜃)1; it does not mean an area in square meters, such as the area of a parcel of land. In a like manner, we can calculate an approximate value for the work for each segment. Then we add the results for the segments to get, approximately, the work W done by the variable force:
W ≈ (F cos θ )1 ∆s1 + (F cos θ )2 ∆s2 + ⋅ ⋅ ⋅
The symbol ≈ means “approximately equal to.” The right side of this equation is the sum of all the rectangular areas in Figure 6.21a and is an approximate value for the area shaded in color under the graph in Figure 6.21b. If the rectangles are made narrower and narrower by decreas- ing each Δs, the right side of this equation eventually becomes equal to the area under the graph.
Problem-Solving Insight The work done by a variable force in moving an object is equal to the area under the graph of F cos 𝜃 versus s.
Example 13 illustrates how to use this graphical method to determine the approximate work done when a high-tech compound bow is drawn.
ANIMATED FIGURE 6.20 (a) A compound bow. (b) A plot of F cos θ versus s as the bowstring is drawn back.
F cos
180.0 N
0 0 s
(b) 0.500 m
9.00 N
2.78 × 10–2 m
108 N
θ
(a)© B
oc ca
be lla
D eb
bi e/
A ge
F ot
os to
ck
Δs1 Δs2 Δs3 Δs4 s s
Work
(a) (b)
(F cos )2
(F cos )1
F cos F cos θ θ
θ
θ
FIGURE 6.21 (a) The work done by the average-force component (F cos θ)1 during the small displacement ∆s1 is (F cos θ)1 ∆s1, which is the area of the colored rectangle. (b) The work done by a variable force is equal to the colored area under the graph of F cos θ versus s.
166 CHAPTER 6 Work and Energy
EXAMPLE 14 BIO The Physics of Seatbelts
Seatbelts are the most important safety feature for automobile drivers and passengers. Roughly 50% of passengers killed in auto accidents were not wearing seatbelts. In modern cars, seatbelts, along with sensors and air- bags, function as an advanced safety restraining system. The graph below shows the force applied to the chest wall as a function of displacement during a frontend collision. Modern seatbelts use a pretensioner eff ect when the collision is high-speed, and therefore particularly dangerous. This reduces the maximum force experienced by the chest wall from the seatbelt during the impact. Using the data in the graph, calculate the work done on the chest wall from the variable force applied by the seatbelt. Assume the force from the seatbelt is applied parallel to the chest wall displacement.
Reasoning The work is equal to the area under the orange curve. We see from the graph that this will consist of the combined area of two rect- angles (Areas I and III), and one triangle (Area II).
Solution The total area under the curve will be equal to Area I + Area II + Area III. From the data in Figure 6.22, we see that Area I = (5000 N – 0 N)(0.20 m – 0.00 m) = 1000 J. Area II = ½(0.20 m – 0.00 m)
(13 000 N – 5000 N) = 800 J. And fi nally, Area III = (13 000 N – 0 N) (0.45 m – 0.20 m) = 3300 J. The work done is therefore equal to 1000 J + 800 J + 3300 J = 5100 J
I
II III
Chest wall displacement (s)
Fo rc
e (N
)
0.00 m 0.20 m 0.45 m
13 000 N
5000 N
0 N
FIGURE 6.22 The variable force applied by a seatbelt to the chest wall as a function of the wall’s displacement. The work done by the seatbelt will be equal to the total area under the orange curve.
Concept Summary 6.1 Work Done by a Constant Force The work W done by a constant force acting on an object is given by Equation 6.1, where F is the magnitude of the force, s is the magnitude of the displacement, and θ is the angle between the force and the displacement vectors. Work is a scalar quantity and can be positive or negative, depending on whether the force has a component that points, re- spectively, in the same direction as the displacement or in the opposite direction. The work is zero if the force is perpendicular (θ = 90°) to the displacement.
W = (F cos θ)s (6.1)
6.2 The Work–Energy Theorem and Kinetic Energy The kinetic energy KE of an object of mass m and speed υ is given by Equation 6.2. The work– energy theorem states that the work W done by the net external force acting on an object equals the diff erence between the object’s fi nal kinetic energy KEf and initial kinetic energy KE0, according to Equation 6.3. The kinetic energy increases when the net force does positive work and decreases when the net force does negative work.
KE = 12mυ2 (6.2) W = KEf − KE0 (6.3)
6.3 Gravitational Potential Energy Work done by the force of gravity on an object of mass m is given by Equation 6.4, where h0 and hf are the initial and fi nal heights of the object, respectively.
Wgravity = mg(h0 − hf) (6.4)
PE = mgh (6.5)
Gravitational potential energy PE is the energy that an object has by virtue of its position. For an object near the surface of the earth, the gravitational potential energy is given by Equation 6.5, where h is the height of the object relative to an arbitrary zero level.
6.4 Conservative Versus Nonconservative Forces A conservative force is one that does the same work in moving an object between two points, independent of the path taken between the points. Alternatively, a force is conservative if the work it does in moving an object around any closed path is zero. A force is nonconservative if the work it does on an object moving between two points depends on the path of the motion between the points.
EXAMPLE 13 The Physics of a Compound Bow
Find the work that the archer must do in drawing back the string of the compound bow in Animated Figure 6.20a from 0 to 0.500 m.
Reasoning The work is equal to the colored area under the curved line in Animated Figure 6.20b. For convenience, this area is divided into a number of small squares, each having an area of (9.00 N)(2.78 × 10‒2 m) = 0.250 J. The area can be found by counting the number of squares under the curve and multiplying by the area per square.
Solution We estimate that there are 242 colored squares in the drawing. Since each square represents 0.250 J of work, the total work done is
W = (242 squares) (0.250 Jsquare) = 60.5 J When the arrow is fi red, part of this work is imparted to it as kinetic energy.
Focus on Concepts 167
6.5 The Conservation of Mechanical Energy The total mechanical en- ergy E is the sum of the kinetic energy and potential energy: E = KE + PE. The work–energy theorem can be expressed in an alternate form as shown in Equation 6.8, where Wnc is the net work done by the external nonconservat- ive forces, and Ef and E0 are the fi nal and initial total mechanical energies, respectively.
Wnc = Ef − E0 (6.8)
The principle of conservation of mechanical energy states that the total mechanical energy E remains constant along the path of an object, provided that the net work done by external nonconservative forces is zero. Whereas E is constant, KE and PE may be transformed into one another.
6.6 Nonconservative Forces and the Work–Energy Theorem/6.7 Power Average power P is the work done per unit time or the rate at which work is done, as shown in Equation 6.10a. It is also the rate at which energy changes, as shown in Equation 6.10b. When a force of magnitude F acts on
an object moving with an average speed υ, the average power is given by Equation 6.11.
P = Work Time
(6.10a)
P = Change in energy
Time (6.10b)
P = F υ (6.11)
6.8 Other Forms of Energy and the Conservation of Energy The prin- ciple of conservation of energy states that energy can neither be created nor destroyed, but can only be transformed from one form to another.
6.9 Work Done by a Variable Force The work done by a variable force of magnitude F in moving an object through a displacement of magnitude s is equal to the area under the graph of F cos θ versus s. The angle θ is the angle between the force and displacement vectors.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 6.1 Work Done by a Constant Force 1. The same force F→ pushes in three diff erent ways on a box moving with a velocity v→, as the drawings show. Rank the work done by the force F→ in ascending order (smallest fi rst): (a) A, B, C (b) A, C, B (c) B, A, C (d) C, B, A (e) C, A, B
A
v
F
B
vF
C
v
F
QUESTION 1
2. Consider the force F→ shown in the drawing. This force acts on an object that can move along the posit- ive or negative x axis, or along the positive or negative y axis. The work done by this force is positive when the displacement of the object is along the _______ axis or along the __________ axis: (a) ‒x, ‒y (b) ‒x, +y (c) +x, +y (d) +x, ‒y
Section 6.2 The Work–Energy Theorem and Kinetic Energy 8. Two forces F1
→ and F2
→ act on a particle. As a result the speed of the particle
increases. Which one of the following is NOT possible? (a) The work done by F1
→ is positive, and the work done by F2
→ is zero. (b) The work done by F1
→
is zero, and the work done by F2 →
is positive. (c) The work done by each force is positive. (d) The work done by each force is negative. (e) The work done by F1
→ is positive, and the work done by F2
→ is negative.
9. Force F1 →
acts on a particle and does work W1. Force F2 →
acts simultaneously on the particle and does work W2. The speed of the particle does not change. Which one of the following must be true? (a) W1 is zero and W2 is positive (b) W1 = ‒W2 (c) W1 is positive and W2 is zero (d) W1 is positive and W2 is positive
Section 6.4 Conservative Versus Nonconservative Forces 11. A person is riding on a Ferris wheel. When the wheel makes one complete turn, the net work done on the person by the gravitational force ____________. (a) is positive (b) is negative (c) is zero (d) depends on how fast the wheel moves (e) depends on the diameter of the wheel
Section 6.5 The Conservation of Mechanical Energy 13. In which one of the following circumstances could mechanical energy not possibly be conserved, even if friction and air resistance are absent? (a) A car moves up a hill, its velocity continually decreasing along the way. (b) A car moves down a hill, its velocity continually increasing along the way. (c) A car moves along level ground at a constant velocity. (d) A car moves up a hill at a constant velocity.
14. A ball is fi xed to the end of a string, which is attached to the ceiling at point P. As the drawing shows, the ball is projected downward at A with the launch speed υ0. Traveling on a circular path, the ball comes to a halt at point B. What enables the ball to reach point B, which is above point A? Ignore friction and air resistance. (a) The work done by the tension in the string (b) The ball’s initial gravitational potential energy (c) The ball’s initial kinetic energy (d) The work done by the gravitational force
Section 6.6 Nonconservative Forces and the Work–Energy Theorem 21. In which one of the following circumstances does the principle of conservation of mechanical energy apply, even though a nonconservative force acts on the moving object? (a) The nonconservative force points in the same direction as the displacement of the object. (b) The nonconser- vative force is perpendicular to the displacement of the object. (c) The nonconservative force has a direction that is opposite to the displacement of the object. (d) The nonconservative force has a component that points in the same direction as the displacement of the object. (e) The noncon- servative force has a component that points opposite to the displacement of the object.
Focus on Concepts
F +y
+x
QUESTION 2
B
A
P
v0
QUESTION 14
168 CHAPTER 6 Work and Energy
22. A 92.0-kg skydiver with an open parachute falls straight downward through a vertical height of 325 m. The skydiver’s velocity remains constant. What is the work done by the nonconservative force of air resistance, which is the only nonconservative force acting? (a) ‒2.93 × 105 J (b) 0 J (c) +2.93 × 105 J (d) The answer is not obtainable, because insuffi cient information about the skydiver’s speed is given.
Section 6.7 Power 25. The power needed to accelerate a projectile from rest to its launch speed υ in a time t is 43.0 W. How much power is needed to accelerate the same projectile from rest to a launch speed of 2υ in a time of 12 t?
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual MMH Problem-solving help GO Guided Online Tutorial V-HINT Video Hints CHALK Chalkboard Videos
BIO Biomedical application E Easy M Medium H Hard
Section 6.1 Work Done by a Constant Force 1. E SSM During a tug-of-war, team A pulls on team B by applying a force of 1100 N to the rope between them. The rope remains parallel to the ground. How much work does team A do if they pull team B toward them a distance of 2.0 m?
2. E GO You are moving into an apartment and take the elevator to the 6th fl oor. Suppose your weight is 685 N and that of your belongings is 915 N. (a) Determine the work done by the elevator in lifting you and your belong- ings up to the 6th fl oor (15.2 m) at a constant velocity. (b) How much work does the elevator do on you alone (without belongings) on the downward trip, which is also made at a constant velocity?
3. E The brakes of a truck cause it to slow down by applying a retarding force of 3.0 × 103 N to the truck over a distance of 850 m. What is the work done by this force on the truck? Is the work positive or negative? Why?
4. E A 75.0-kg man is riding an escalator in a shopping mall. The escalator moves the man at a constant velocity from ground level to the fl oor above, a vertical height of 4.60 m. What is the work done on the man by (a) the gravitational force and (b) the escalator? 5. E SSM Suppose in Figure 6.2 that +1.10 × 103 J of work is done by the force F→ (magnitude = 30.0 N) in moving the suitcase a distance of 50.0 m. At what angle 𝜃 is the force oriented with respect to the ground?
6. E A person pushes a 16.0-kg shopping cart at a constant velocity for a distance of 22.0 m. She pushes in a direction 29.0° below the horizontal. A 48.0-N frictional force opposes the motion of the cart. (a) What is the magnitude of the force that the shopper exerts? Determine the work done by (b) the pushing force, (c) the frictional force, and (d) the gravitational force.
7. E SSM MMH The drawing shows a plane diving toward the ground and then climbing back upward. During each of these motions, the lift force L→ acts perpendicular to the displacement s→, which has the same magnitude, 1.7 × 103 m, in each case. The engines of the plane exert a thrust T→, which points in the direction of the displacement and has the same magnitude dur- ing the dive and the climb. The weight W→ of the plane has a magnitude of 5.9 × 104 N. In both motions, net work is performed due to the combined action of the forces L→ , T→, and W→ . (a) Is more net work done during the dive
or the climb? Explain. (b) Find the diff erence between the net work done during the dive and the climb.
W(a) Dive (b) Climb 75°
L
T
W
115°
L T s
s
PROBLEM 7
8. E A person pulls a toboggan for a distance of 35.0 m along the snow with a rope directed 25.0° above the snow. The tension in the rope is 94.0 N. (a) How much work is done on the toboggan by the tension force? (b) How much work is done if the same tension is directed parallel to the snow?
9. M V-HINT As a sailboat sails 52 m due north, a breeze exerts a constant force F1
→ on the boat’s sails. This force is directed at an angle west of due
north. A force F2 →
of the same magnitude directed due north would do the same amount of work on the sailboat over a distance of just 47 m. What is the angle between the direction of the force F1
→ and due north?
10. M GO A 55-kg box is being pushed a distance of 7.0 m across the fl oor by a force P→ whose magnitude is 160 N. The force P→ is parallel to the displacement of the box. The coeffi cient of kinetic friction is 0.25. De- termine the work done on the box by each of the four forces that act on the box. Be sure to include the proper plus or minus sign for the work done by each force.
11. M V-HINT A 1.00 × 102-kg crate is being pushed across a horizontal fl oor by a force P→ that makes an angle of 30.0° below the horizontal. The coeffi cient of kinetic friction is 0.200. What should be the magnitude of P→, so that the net work done by it and the kinetic frictional force is zero? 12. H A 1200-kg car is being driven up a 5.0° hill. The frictional force is directed opposite to the motion of the car and has a magnitude of f = 524 N. A force F→ is applied to the car by the road and propels the car forward. In addition to these two forces, two other forces act on the car: its weight W
→ and the normal force FN
→ directed perpendicular to the road
surface. The length of the road up the hill is 290 m. What should be the magnitude of F→, so that the net work done by all the forces acting on the car is +150 kJ?
Section 6.2 The Work–Energy Theorem and Kinetic Energy 13. E A fi ghter jet is launched from an aircraft carrier with the aid of its own engines and a steam-powered catapult. The thrust of its engines is 2.3 × 105 N. In being launched from rest it moves through a distance of 87 m and has a kinetic energy of 4.5 × 107 J at lift-off . What is the work done on the jet by the catapult?
Problems
Problems 169
14. E MMH A golf club strikes a 0.045-kg golf ball in order to launch it from the tee. For simplicity, assume that the average net force applied to the ball acts parallel to the ball’s motion, has a magnitude of 6800 N, and is in contact with the ball for a distance of 0.010 m. With what speed does the ball leave the club?
15. E SSM It takes 185 kJ of work to accelerate a car from 23.0 m/s to 28.0 m/s. What is the car’s mass?
16. E Starting from rest, a 1.9 × 10‒4-kg fl ea springs straight upward. While the fl ea is pushing off from the ground, the ground exerts an average upward force of 0.38 N on it. This force does +2.4 × 10‒4 J of work on the fl ea. (a) What is the fl ea’s speed when it leaves the ground? (b) How far upward does the fl ea move while it is pushing off ? Ignore both air resistance and the fl ea’s weight.
17. E GO A water-skier is being pulled by a tow rope attached to a boat. As the driver pushes the throttle forward, the skier accelerates. A 70.3-kg water-skier has an initial speed of 6.10 m/s. Later, the speed increases to 11.3 m/s. Determine the work done by the net external force acting on the skier.
18. E As background for this problem, review Conceptual Example 6. A 7420-kg satellite has an elliptical orbit, as in Figure 6.9b. The point on the orbit that is farthest from the earth is called the apogee and is at the far right side of the drawing. The point on the orbit that is closest to the earth is called the perigee and is at the left side of the drawing. Suppose that the speed of the satellite is 2820 m/s at the apogee and 8450 m/s at the perigee. Find the work done by the gravitational force when the satellite moves from (a) the apogee to the perigee and (b) the perigee to the apogee. 19. E SSM The hammer throw is a track-and-fi eld event in which a 7.3 kg ball (the “hammer”), starting from rest, is whirled around in a circle several times and released. It then moves upward on the familiar curving path of projectile motion. In one throw, the hammer is given a speed of 29 m/s. For comparison, a .22 caliber bullet has a mass of 2.6 g and, starting from rest, exits the barrel of a gun at a speed of 410 m/s. Determine the work done to launch the motion of (a) the hammer and (b) the bullet. 20. E GO A 16-kg sled is being pulled along the horizontal snow-covered ground by a horizontal force of 24 N. Starting from rest, the sled attains a speed of 2.0 m/s in 8.0 m. Find the coeffi cient of kinetic friction between the runners of the sled and the snow.
21. E GO An asteroid is moving along a straight line. A force acts along the displacement of the asteroid and slows it down. The asteroid has a mass of 4.5 × 104 kg, and the force causes its speed to change from 7100 to 5500 m/s. (a) What is the work done by the force? (b) If the asteroid slows down over a distance of 1.8 × 106 m, determine the magnitude of the force.
22. M The concepts in this problem are similar to those in Multiple-Concept Example 4, except that the force doing the work in this problem is the tension in the cable. A rescue helicopter lifts a 79-kg person straight up by means of a cable. The person has an upward acceleration of 0.70 m/s2 and is lifted from rest through a distance of 11 m. (a) What is the tension in the cable? How much work is done by (b) the tension in the cable and (c) the person’s weight? (d) Use the work–energy theorem and fi nd the fi nal speed of the person.
23. E SSM Available in WileyPLUS. 24. M V-HINT Consult Multiple-Concept Example 5 for insight into solving this problem. A skier slides horizontally along the snow for a distance of 21 m before coming to rest. The coeffi cient of kinetic friction between the skier and the snow is μk = 0.050. Initially, how fast was the skier going?
25. M SSM Available in WileyPLUS. 26. M GO Under the infl uence of its drive force, a snowmobile is moving at a constant velocity along a horizontal patch of snow. When the drive force is shut off , the snowmobile coasts to a halt. The snowmobile and its rider have
a mass of 136 kg. Under the infl uence of a drive force of 205 N, it is moving at a constant velocity whose magnitude is 5.50 m/s. The drive force is then shut off . Find (a) the distance in which the snowmobile coasts to a halt and (b) the time required to do so. 27. H The model airplane in Figure 5.6 is fl ying at a speed of 22 m/s on a horizontal circle of radius 16 m. The mass of the plane is 0.90 kg. The person holding the guideline pulls it in until the radius becomes 14 m. The plane speeds up, and the tension in the guideline becomes four times greater. What is the net work done on the plane?
28. H Available in WileyPLUS.
Section 6.3 Gravitational Potential Energy,
Section 6.4 Conservative Versus Nonconservative Forces 29. E A 75.0-kg skier rides a 2830-m-long lift to the top of a mountain. The lift makes an angle of 14.6° with the horizontal. What is the change in the skier’s gravitational potential energy?
30. E Juggles and Bangles are clowns. Juggles stands on one end of a teeter-totter at rest on the ground. Bangles jumps off a platform 2.5 m above the ground and lands on the other end of the teeter-totter, launching Juggles into the air. Juggles rises to a height of 3.3 m above the ground, at which point he has the same amount of gravitational potential energy as Bangles had before he jumped, assuming both potential energies are measured using the ground as the reference level. Bangles’ mass is 86 kg. What is Juggles’ mass?
31. E A 0.60-kg basketball is dropped out of a window that is 6.1 m above the ground. The ball is caught by a person whose hands are 1.5 m above the ground. (a) How much work is done on the ball by its weight? What is the gravitational potential energy of the basketball, relative to the ground, when it is (b) released and (c) caught? (d) How is the change (PEf ‒ PE0) in the ball’s gravitational potential energy related to the work done by its weight?
32. E A pole-vaulter just clears the bar at 5.80 m and falls back to the ground. The change in the vaulter’s potential energy during the fall is ‒3.70 × 103 J. What is his weight?
33. E SSM A bicyclist rides 5.0 km due east, while the resistive force from the air has a magnitude of 3.0 N and points due west. The rider then turns around and rides 5.0 km due west, back to her starting point. The resistive force from the air on the return trip has a magnitude of 3.0 N and points due east. (a) Find the work done by the resistive force during the round trip. (b) Based on your answer to part (a), is the resistive force a conservative force? Explain.
34. E GO “Rocket Man” has a propulsion unit strapped to his back. He starts from rest on the ground, fi res the unit, and accelerates straight upward. At a height of 16 m, his speed is 5.0 m/s. His mass, including the propulsion unit, has the approximately constant value of 136 kg. Find the work done by the force generated by the propulsion unit.
35. E SSM A 55.0-kg skateboarder starts out with a speed of 1.80 m/s. He does +80.0 J of work on himself by pushing with his feet against the ground. In addition, friction does ‒265 J of work on him. In both cases, the forces doing the work are nonconservative. The fi nal speed of the skateboarder is 6.00 m/s. (a) Calculate the change (∆PE = PEf ‒ PE0) in the gravitational potential energy. (b) How much has the vertical height of the skater changed, and is the skater above or below the starting point?
Section 6.5 The Conservation of Mechanical Energy 36. E A 35-kg girl is bouncing on a trampoline. During a certain interval after she leaves the surface of the trampoline, her kinetic energy decreases to 210 J from 440 J. How high does she rise during this interval? Neglect air resistance.
170 CHAPTER 6 Work and Energy
37. E SSM MMH A gymnast is swinging on a high bar. The distance between his waist and the bar is 1.1 m, as the drawing shows. At the top of the swing his speed is momentarily zero. Ignoring friction and treating the gymnast as if all of his mass is located at his waist, fi nd his speed at the bottom of the swing.
PROBLEM 37
r = 1.1 m
38. E CHALK GO The skateboarder in the drawing starts down the left side of the ramp with an initial speed of 5.4 m/s. Neglect nonconservative forces, such as friction and air resistance, and fi nd the height h of the highest point reached by the skateboarder on the right side of the ramp.
PROBLEM 38
h
39. E MMH A slingshot fi res a pebble from the top of a building at a speed of 14.0 m/s. The building is 31.0 m tall. Ignoring air resistance, fi nd the speed with which the pebble strikes the ground when the pebble is fi red (a) hori- zontally, (b) vertically straight up, and (c) vertically straight down. 40. E GO The drawing shows two boxes resting on frictionless ramps. One box is relatively light and sits on a steep ramp. The other box is heavier and rests on a ramp that is less steep. The boxes are released from rest at A and allowed to slide down the ramps. The two boxes have masses of 11 and 44 kg. If A and B are 4.5 and 1.5 m, respectively, above the ground, determine the speed of (a) the lighter box and (b) the heavier box when each reaches B. (c) What is the ratio of the kinetic energy of the heavier box to that of the lighter box at B?
PROBLEM 40
= 0 m/s
A
B
hB = 1.5 m
hA = 4.5 m
A= 0 m/s A υυ
41. E A 47.0-g golf ball is driven from the tee with an initial speed of 52.0 m/s and rises to a height of 24.6 m. (a) Neglect air resistance and determine the kinetic energy of the ball at its highest point. (b) What is its speed when it is 8.0 m below its highest point?
42. E MMH Consult Conceptual Example 9 in preparation for this problem. The drawing shows a person who, starting from rest at the top of a cliff , swings down at the end of a rope, releases it, and falls into the water below.
There are two paths by which the person can enter the water. Suppose he enters the water at a speed of 13.0 m/s via path 1. How fast is he moving on path 2 when he releases the rope at a height of 5.20 m above the water? Ignore the eff ects of air resistance.
Path 1Path 2
PROBLEM 42
43. M GO SSM The drawing shows a skateboarder moving at 5.4 m/s along a horizontal section of a track that is slanted upward by 48° above the ho- rizontal at its end, which is 0.40 m above the ground. When she leaves the track, she follows the characteristic path of projectile motion. Ignoring fric- tion and air resistance, fi nd the maximum height H to which she rises above the end of the track.
H
5.4 m/s
0.40 m
PROBLEM 43
44. M CHALK GO A small lead ball, attached to a 0.75-m rope, is being whirled in a circle that lies in the vertical plane. The ball is whirled at a constant rate of three revolutions per second and is released on the upward part of the circular motion when it is 1.5 m above the ground. The ball travels straight upward. In the absence of air resistance, to what maximum height above the ground does the ball rise?
45. M SSM Available in WileyPLUS. 46. M CHALK A pendulum consists of a small object hanging from the ceil- ing at the end of a string of negligible mass. The string has a length of 0.75 m. With the string hanging vertically, the object is given an initial velocity of 2.0 m/s parallel to the ground and swings upward on a circular arc. Eventu- ally, the object comes to a momentary halt at a point where the string makes an angle 𝜃 with its initial vertical orientation and then swings back down- ward. Find the angle 𝜃.
47. M V-HINT A semitrailer is coasting downhill along a mountain highway when its brakes fail. The driver pulls onto a runaway-truck ramp that is in- clined at an angle of 14.0° above the horizontal. The semitrailer coasts to a stop after traveling 154 m along the ramp. What was the truck’s initial speed? Neglect air resistance and friction.
48. M GO The drawing shows two frictionless inclines that begin at ground level (h = 0 m) and slope upward at the same angle 𝜃. One track is longer than the other, however. Identical blocks are projected up each track with the same
Problems 171
initial speed υ0. On the longer track the block slides upward until it reaches a maximum height H above the ground. On the shorter track the block slides up- ward, fl ies off the end of the track at a height H1 above the ground, and then fol- lows the familiar parabolic trajectory of projectile motion. At the highest point of this trajectory, the block is a height H2 above the end of the track. The initial total mechanical energy of each block is the same and is all kinetic energy. The initial speed of each block is υ0 = 7.00 m/s, and each incline slopes upward at an angle of 𝜃 = 50.0°. The block on the shorter track leaves the track at a height of H1 = 1.25 m above the ground. Find (a) the height H for the block on the longer track and (b) the total height H1 + H2 for the block on the shorter track.
Longer track
H
0
Shorter track
H1
H2
0
θ θ
υ υ
PROBLEM 48
49. H A skier starts from rest at the top of a hill. The skier coasts down the hill and up a second hill, as the drawing illustrates. The crest of the second hill is circular, with a radius of r = 36 m. Neglect friction and air resistance. What must be the height h of the fi rst hill so that the skier just loses contact with the snow at the crest of the second hill?
h
r
PROBLEM 49
50. H A person starts from rest at the top of a large frictionless spherical surface, and slides into the water below (see the drawing). At what angle 𝜃 does the person leave the surface? (Hint: When the person leaves the surface, the normal force is zero.)
PROBLEM 50
r
θ
Section 6.6 Nonconservative Forces and the Work–Energy Theorem 51. E SSM A projectile of mass 0.750 kg is shot straight up with an initial speed of 18.0 m/s. (a) How high would it go if there were no air resistance? (b) If the projectile rises to a maximum height of only 11.8 m, determine the magnitude of the average force due to air resistance.
52. E A basketball player makes a jump shot. The 0.600-kg ball is released at a height of 2.00 m above the fl oor with a speed of 7.20 m/s. The ball goes through the net 3.10 m above the fl oor at a speed of 4.20 m/s. What is the work done on the ball by air resistance, a nonconservative force?
53. E Starting from rest, a 93-kg fi refi ghter slides down a fi re pole. The average frictional force exerted on him by the pole has a magnitude of 810 N, and his speed at the bottom of the pole is 3.4 m/s. How far did he slide down the pole?
54. E GO A student, starting from rest, slides down a water slide. On the way down, a kinetic frictional force (a nonconservative force) acts on her. The student has a mass of 83.0 kg, and the height of the water slide is 11.8 m. If the kinetic frictional force does ‒6.50 × 103 J of work, how fast is the stu- dent going at the bottom of the slide?
55. E SSM The (nonconservative) force propelling a 1.50 × 103-kg car up a mountain road does 4.70 × 106 J of work on the car. The car starts from rest at sea level and has a speed of 27.0 m/s at an altitude of 2.00 × 102 m above sea level. Obtain the work done on the car by the combined forces of friction and air resistance, both of which are nonconservative forces.
56. E GO In the sport of skeleton a participant jumps onto a sled (known as a skeleton) and proceeds to slide down an icy track, belly down and head fi rst. In the 2010 Winter Olympics, the track had sixteen turns and dropped 126 m in elevation from top to bottom. (a) In the absence of non- conservative forces, such as friction and air resistance, what would be the speed of a rider at the bottom of the track? Assume that the speed at the be- ginning of the run is relatively small and can be ignored. (b) In reality, the gold-medal winner (Canadian Jon Montgomery) reached the bottom in one heat with a speed of 40.5 m/s (about 91 mi/h). How much work was done on him and his sled (assuming a total mass of 118 kg) by nonconservative forces during this heat?
PROBLEM 56 Fr an
k G
un n/
A P/
W id
e W
or ld
P ho
to s
57. M V-HINT In attempting to pass the puck to a teammate, a hockey player gives it an initial speed of 1.7 m/s. However, this speed is inadequate to com- pensate for the kinetic friction between the puck and the ice. As a result, the puck travels only one-half the distance between the players before sliding to a halt. What minimum initial speed should the puck have been given so that it reached the teammate, assuming that the same force of kinetic friction acted on the puck everywhere between the two players?
58. M Available in WileyPLUS. 59. M MMH A 67.0-kg person jumps from rest off a 3.00-m-high tower straight down into the water. Neglect air resistance. She comes to rest 1.10 m under the surface of the water. Determine the magnitude of the average force that the water exerts on the diver. This force is nonconservative.
60. M At a carnival, you can try to ring a bell by striking a target with a 9.00-kg hammer. In response, a 0.400-kg metal piece is sent upward toward the bell, which is 5.00 m above. Suppose that 25.0% of the hammer’s kinetic energy is used to do the work of sending the metal piece upward. How fast must the hammer be moving when it strikes the target so that the bell just barely rings?
61. H SSM Available in WileyPLUS.
172 CHAPTER 6 Work and Energy
Section 6.7 Power 62. E A person is making homemade ice cream. She exerts a force of mag- nitude 22 N on the free end of the crank handle on the ice-cream maker, and this end moves on a circular path of radius 0.28 m. The force is always applied parallel to the motion of the handle. If the handle is turned once every 1.3 s, what is the average power being expended?
63. E BIO SSM Bicyclists in the Tour de France do enormous amounts of work during a race. For example, the average power per kilogram generated by seven-time-winner Lance Armstrong (m = 75.0 kg) is 6.50 W per kilogram of his body mass. (a) How much work does he do during a 135-km race in which his average speed is 12.0 m/s? (b) Often, the work done is expressed in nutri- tional Calories rather than in joules. Express the work done in part (a) in terms of nutritional Calories, noting that 1 joule = 2.389 × 10‒4 nutritional Calories.
64. E BIO GO You are working out on a rowing machine. Each time you pull the rowing bar (which simulates the oars) toward you, it moves a dis- tance of 1.2 m in a time of 1.5 s. The readout on the display indicates that the average power you are producing is 82 W. What is the magnitude of the force that you exert on the handle?
65. E MMH A car accelerates uniformly from rest to 20.0 m/s in 5.6 s along a level stretch of road. Ignoring friction, determine the average power required to accelerate the car if (a) the weight of the car is 9.0 × 103 N and (b) the weight of the car is 1.4 × 104 N. 66. E GO A helicopter, starting from rest, accelerates straight up from the roof of a hospital. The lifting force does work in raising the helicopter. An 810-kg helicopter rises from rest to a speed of 7.0 m/s in a time of 3.5 s. During this time it climbs to a height of 8.2 m. What is the average power generated by the lifting force?
67. M V-HINT The cheetah is one of the fastest-accelerating animals, because it can go from rest to 27 m/s (about 60 mi/h) in 4.0 s. If its mass is 110 kg, de- termine the average power developed by the cheetah during the acceleration phase of its motion. Express your answer in (a) watts and (b) horsepower. 68. M V-HINT In 2.0 minutes, a ski lift raises four skiers at constant speed to a height of 140 m. The average mass of each skier is 65 kg. What is the average power provided by the tension in the cable pulling the lift?
69. H SSM Available in WileyPLUS. 70. H Available in WileyPLUS.
Section 6.9 Work Done by a Variable Force 71. E SSM Available in WileyPLUS. 72. E The graph shows how the force component F cos 𝜃 along the dis- placement varies with the magnitude s of the displacement. Find the work
done by the force. (Hint: Recall how the area of a triangle is related to the triangle’s base and height.)
PROBLEM 72 0 1.60 m
62.0 N
0 s
F cosθ
73. E Available in WileyPLUS. 74. E The force component along the displacement varies with the mag- nitude of the displacement, as shown in the graph. Find the work done by the force in the interval from (a) 0 to 1.0 m, (b) 1.0 to 2.0 m, and (c) 2.0 to 4.0 m. (Note: In the last interval the force component is negative, so the work is negative.)
PROBLEM 74
+6.0 N
2.0 m
1.0 m
3.0 m 4.0 m s
F cos
−6.0 N
θ
75. E GO A net external force is applied to a 6.00-kg object that is initially at rest. The net force component along the displacement of the object varies with the magnitude of the displacement as shown in the drawing. What is the speed of the object at s = 20.0 m?
PROBLEM 75 0 20.0 m
10.0 N
0 10.0 m
s
F cos
5.00 N
θ
76. E A cable lifts a 1200-kg elevator at a constant velocity for a distance of 35 m. What is the work done by (a) the tension in the cable and (b) the elevator’s weight?
77. E SSM A 2.00-kg rock is released from rest at a height of 20.0 m. Ignore air resistance and determine the kinetic energy, gravitational potential en- ergy, and total mechanical energy at each of the following heights: 20.0, 10.0, and 0 m.
78. E Available in WileyPLUS. 79. E SSM Available in WileyPLUS.
80. E GO When an 81.0-kg adult uses a spiral staircase to climb to the second fl oor of his house, his gravitational potential energy increases by 2.00 × 103 J. By how much does the potential energy of an 18.0-kg child increase when the child climbs a normal staircase to the second fl oor?
81. M GO A husband and wife take turns pulling their child in a wagon along a horizontal sidewalk. Each exerts a constant force and pulls the wagon through the same displacement. They do the same amount of work, but the husband’s pulling force is directed 58° above the horizontal, and the wife’s pulling force is directed 38° above the horizontal. The husband pulls with a
Additional Problems
Concepts and Calculations Problems 173
force whose magnitude is 67 N. What is the magnitude of the pulling force exerted by his wife?
82. M V-HINT Some gliders are launched from the ground by means of a winch, which rapidly reels in a towing cable attached to the glider. What av- erage power must the winch supply in order to accelerate a 184-kg ultralight glider from rest to 26.0 m/s over a horizontal distance of 48.0 m? Assume that friction and air resistance are negligible, and that the tension in the winch cable is constant.
83. M SSM MMH Available in WileyPLUS. 84. M V-HINT A 63-kg skier coasts up a snow-covered hill that makes an angle of 25° with the horizontal. The initial speed of the skier is 6.6 m/s. After coasting 1.9 m up the slope, the skier has a speed of 4.4 m/s. (a) Find the work done by the kinetic frictional force that acts on the skis. (b) What is the magnitude of the kinetic frictional force?
85. M V-HINT A water slide is constructed so that swimmers, starting from rest at the top of the slide, leave the end of the slide traveling horizontally. As the drawing shows, one person hits the water 5.00 m from the end of the
slide in a time of 0.500 s after leaving the slide. Ignoring friction and air resistance, fi nd the height H in the drawing.
PROBLEM 85
Water slide
5.00 m
H
86. H Available in WileyPLUS. 87. H Available in WileyPLUS. 88. M GO A car, starting from rest, accelerates in the +x direction as in the fi gure. It has a mass of 1.10 × 103 kg and maintains an acceleration of +4.60 m/s2 for 5.00 s. Assume that a single horizontal force (not shown) accelerates the vehicle. Determine the average power generated by this force.
+x At rest
a
v
PROBLEM 88
Problem 89 reviews the important concept of work, and illustrates how forces can give rise to positive, negative, and zero work. Problem 90 examines the all-important conservation of mechanical energy.
89. M CHALK SSM The skateboarder in the fi gure is coasting down a ramp, and there are three forces acting on her: her weight W
→ (magnitude = 675 N),
a frictional force f →
(magnitude = 125 N) that opposes her motion, and a
normal force FN →
(magnitude = 612 N) Concepts: Part b of the fi gure shows each force, along with the displacement s→ of the skateboarder. By examin- ing these diagrams and without doing any numerical calculations, determine whether the work done by each force is positive, negative, or zero. Provide a reason for each answer. Calculations: Determine the net work done by the three forces when she coasts for a distance of 9.2 m.
90. M CHALK The fi gure shows a 0.41-kg block sliding from A to B along a frictionless surface. When the block reaches B, it continues to slide along the horizontal surface BC where the kinetic frictional force acts. As a result, the block slows down, coming to rest at C. The kinetic energy of the block at A is 37 J, and the heights of A and B are 12.0 and 7.0 m above the ground, respectively. Concepts: (i) Is the total mechanical energy of the block conserved as the block goes from A to B? Why or why not? (ii) When the block reaches point B, has its kinetic energy increased, decreased, or remained the same relative to what it was at A? Give a reason for your answer. (iii) Is the total mechanical energy of the block conserved as the block goes from B to C? Justify your answer. Calculations: (a) What is the value of the kinetic energy of the block when it reaches B? (b) How much work does the kinetic frictional force do during the BC segment of the trip?
PROBLEM 90
A
B
hB = 7.0 m
C
hC = 7.0 m
hA = 12.0 m
Concepts and Calculations Problems
Weight component
= 65.0°
= 180.0°
= 90.0°
s
W
s
FN
s
f
(b)
(a)
25.0°
s
W
f
FN
θ
θ
θ
PROBLEM 89
174 CHAPTER 6 Work and Energy
91. M A Makeshift Elevator. While exploring an elaborate tunnel system, you and your team get lost and fi nd yourselves at the bottom of a 450-m
vertical shaft. Suspended from a thick rope (near the fl oor) is a large rect-
angular bucket that looks like it had been used to transport tools and debris
up and down the tunnel. Mounted on the fl oor near one of the walls is a
gasoline engine (3.5 hp) that turns a pulley and rope, and a sign that reads
“Emergency Lift.” It is clear that the engine is used to drive the bucket up
the shaft. On the wall next to the engine is a sign indicating that a full tank
of gas will last exactly 15 minutes when the engine is running at full power.
You open the engine’s gas tank and estimate that it is ¼ full, and there are no
other sources of gasoline. (a) Assuming zero friction, if you send your team’s lightest member (who weighs 125 lb), and the bucket weighs 150 lb when
empty, how far up the shaft will the engine take her (and the bucket)? Will it
get her out of the mine? (b) Assuming an eff ective collective friction (from the pulleys, etc.) of 𝜇eff = 0.10 (so that Ff = 𝜇eff Mg, where M is the total mass of the bucket plus team member), will the engine (with a ¼-full tank of gas)
lift her to the top of the shaft?
92. M A Sledding Contest. You are in a sledding contest where you start at a height of 40.0 m above the bottom of a valley and slide down a hill that
makes an angle of 25.0° with respect to the horizontal. When you reach
the valley, you immediately climb a second hill that makes an angle of
15.0° with respect to the horizontal. The winner of the contest will be the
contestant who travels the greatest distance up the second hill. You must
now choose between using your fl at-bottomed plastic sled, or your “Blade
Runner,” which glides on two steel rails. The hill you will ride down is
covered with loose snow. However, the hill you will climb on the other side
is a popular sledding hill, and is packed hard and is slick. The two sleds
perform very diff erently on the two surfaces, the plastic one performing
better on loose snow, and the Blade Runner doing better on hard-packed
snow or ice. The performances of each sled can be quantifi ed in terms of
their respective coeffi cients of kinetic friction on the two surfaces. For the
plastic sled: 𝜇 = 0.17 on loose snow, and 𝜇 = 0.15 on packed snow or ice.
For the Blade Runner, 𝜇 = 0.19 on loose snow, and 𝜇 = 0.07 on packed
snow or ice. Assuming the two hills are shaped like inclined planes, and
neglecting air resistance, (a) how far does each sled make it up the second hill before stopping? (b) Assuming the total mass of the sled plus rider is 55.0 kg in both cases, how much work is done by nonconservative forces
(over the total trip) in each case?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
7.1 Apply the impulse–momentum theorem.
7.2 Apply the law of conservation of linear momentum.
7.3 Analyze one-dimensional collisions.
7.4 Analyze two-dimensional collisions.
7.5 Determine the location and the velocity of the center of mass.
S te
p h an
G o er
li ch
/A g e
F o to
st o ck
A m
er ic
a
CHAPTER 7
Impulse and Momentum
In the sport of jousting in the Middle Ages, two knights in armor rode their horses toward each other and,
using their lances, attempted to knock each other to the ground. Sometimes, however, the collision between a
lance and an opponent’s shield caused the lance to shatter and no one was unseated. In physics such a collision
is classifi ed as being inelastic. Inelastic collisions are one of the two basic types that this chapter introduces.
7.1 The Impulse–Momentum Theorem There are many situations in which the force acting on an object is not constant, but
varies with time. For instance, Figure 7.1a shows a baseball being hit, and part b of the fi gure illustrates approximately how the force applied to the ball by the bat changes
during the time of contact. The magnitude of the force is zero at the instant t0 just before the bat touches the ball. During contact, the force rises to a maximum and then
returns to zero at the time tf when the ball leaves the bat. The time interval ∆t = tf ‒ t0 during which the bat and ball are in contact is quite short, being only a few thousandths
of a second, although the maximum force can be very large, often exceeding thousands
of newtons. For comparison, the graph also shows the magnitude F of the average force exerted on the ball during the time of contact. Figure 7.2 depicts other situations in which a time-varying force is applied to a ball.
To describe how a time-varying force aff ects the motion of an object, we will
introduce two new ideas: the impulse of a force and the linear momentum of an object.
These ideas will be used with Newton’s second law of motion to produce an important
result known as the impulse–momentum theorem. This theorem plays a central role in
describing collisions, such as that between a ball and a bat. Later on, we will see also
that the theorem leads in a natural way to one of the most fundamental laws in physics,
the conservation of linear momentum. 175
176 CHAPTER 7 Impulse and Momentum
If a baseball is to be hit well, both the magnitude of the force and the time of contact are
important. When a large average force acts on the ball for a long enough time, the ball is hit
solidly. To describe such situations, we bring together the average force and the time of contact,
calling the product of the two the impulse of the force.
DEFINITION OF IMPULSE
The impulse J →
of a force is the product of the average force F→ and the time interval 𝚫t during which the force acts:
J →
= F→ ∆t (7.1)
Impulse is a vector quantity and has the same direction as the average force. SI Unit of Impulse: newton · second (N · s)
When a ball is hit, it responds to the value of the impulse. A large impulse produces a large
response; that is, the ball departs from the bat with a large velocity. However, we know from
experience that the more massive the ball, the less velocity it has after leaving the bat. Both mass
and velocity play a role in how an object responds to a given impulse, and the eff ect of each of
them is included in the concept of linear momentum, which is defi ned as follows:
DEFINITION OF LINEAR MOMENTUM The linear momentum p→ of an object is the product of the object’s mass m and velocity v→:
p→ = mv→ (7.2) Linear momentum is a vector quantity that points in the same direction as the velocity. SI Unit of Linear Momentum: kilogram · meter/second (kg · m/s)
Newton’s second law of motion can now be used to reveal a relationship between impulse
and momentum. Figure 7.3 shows a ball with an initial velocity v0→ approaching a bat, being struck by the bat, and then departing with a fi nal velocity vf→ . When the velocity of an object changes from v0→ to vf→ during a time interval ∆t, the average acceleration a→ is given by Equa- tion 2.4 as
a→ = v→f − v→0
∆t
According to Newton’s second law, ΣF→ = ma→, the average acceleration is produced by the net average force ΣF→. Here ΣF→ represents the vector sum of all the average forces that act on the object. Thus,
ΣF→ = m ( v→f − v→0
∆ t ) = mv→f − mv→0
∆ t (7.3)
FIGURE 7.1 (a) The collision time between a bat and a ball is very short, often less than a
millisecond, but the force can be quite large.
(b) When the bat strikes the ball, the magni- tude of the force exerted on the ball rises to a
maximum and then returns to zero when the
ball leaves the bat. The time interval during
which the force acts is ∆t, and the magnitude of the average force is F.
Force
t0 tf Time
F
(b)
Δt
C h u ck
S av
ag e/
C o rb
is /G
et ty
(a)
FIGURE 7.2 In each of these situations, the force applied to the ball varies with time. The time of contact is small, but the maximum force can be large.
M ik
e P
o w
el l/
G et
ty I
m ag
es
F ra
n k G
u n n /A
P /W
id e
W o rl
d P
h o to
s
v0
vf
F
FIGURE 7.3 When a bat hits a ball, an average force F→ is applied to the ball by the bat. As a result, the ball’s velocity changes
from an initial value of v0→ (top drawing) to a fi nal value of vf→ (bottom drawing).
7.1 The Impulse–Momentum Theorem 177
In this result, the numerator on the far right is the fi nal momentum minus the initial momentum,
which is the change in momentum. Thus, the net average force is given by the change in momentum
per unit of time.* Multiplying both sides of Equation 7.3 by ∆t yields Equation 7.4, which is known as the impulse–momentum theorem.
IMPULSE–MOMENTUM THEOREM When a net average force Σ F→ acts on an object during a time interval ∆ t the impulse of this force is equal to the change in momentum of the object:
(ΣF→)∆ t = mv→f − mv →
0 (7.4)
Impulse = Change in momentum
During a collision, it is often diffi cult to measure the net average force ΣF→, so it is not easy to determine the impulse (ΣF→)∆ t directly. On the other hand, it is usually straightforward to measure the mass and velocity of an object, so that its momentum mvf→ just after the collision and mv0→ just before the collision can be found. Thus, the impulse–momentum theorem allows us to gain information about the impulse indirectly by measuring the change in momentum
that the impulse causes (see Photo 7.1). Then, armed with a knowledge of the contact time ∆ t, we can evaluate the net average force. Examples 1 and 2 illustrate how the theorem is used in
this way.
Impulse Final
momentum
Initial
momentum
⏟⏟⏟ } }
*The equality between the net force and the change in momentum per unit time is the version of the second law of
motion presented originally by Newton.
PHOTO 7.1 During the launch of the space shuttle, the engines fi re and create a force
that applies an impulse to the shuttle and the
launch vehicle. This impulse causes the mo-
mentum of the shuttle and the launch vehicle
to increase, and the shuttle rises to its orbit.
StockTrek/Purestock/SuperStock
EXAMPLE 1 A Well-Hit Ball
A baseball (m = 0.14 kg) has an initial velocity of v0→ = −38 m/s as it ap- proaches a bat. We have chosen the direction of approach as the negative
direction. The bat applies an average force F→ that is much larger than the weight of the ball, and the ball departs from the bat with a fi nal velocity
of vf→ = +58 m/s. (a) Determine the impulse applied to the ball by the bat. (b) Assuming that the time of contact is ∆t = 1.6 × 10−3 s, fi nd the average force exerted on the ball by the bat.
Reasoning Two forces act on the ball during impact, and together they constitute the net average force: the average force F→ exerted by the bat, and the weight of the ball. Since F→ is much greater than the weight of the ball, we neglect the weight. Thus, the net average force is equal to F→, or ΣF→ = F→. In hitting the ball, the bat imparts an impulse to it. We cannot use Equation 7.1 ( J→ = F→ ∆ t) to determine the impulse F→ directly, since F→ is not known. We can fi nd the impulse indirectly, however, by turning to
the impulse–momentum theorem, which states that the impulse is equal
to the ball’s fi nal momentum minus its initial momentum. With values for
the impulse and the time of contact, Equation 7.1 can be used to deter-
mine the average force applied by the bat to the ball.
Problem-Solving Insight Momentum is a vector and, as such, has a magnitude and a direction. For motion in one dimension, be sure to indicate the direction by assigning a plus or minus sign to it, as in this example.
Solution (a) According to the impulse–momentum theorem, the impulse J→ applied to the ball is
J →
= mv→f − mv→0 = (0.14 kg )(+58 m /s) − (0.14 kg )(−38 m /s)
Final momentum Initial momentum
= +13.4 kg · m /s
(b) Now that the impulse is known, the contact time can be used in Equa- tion 7.1 to fi nd the average force F→ exerted by the bat on the ball:
F→ = J →
∆ t =
+13.4 kg ⋅ m /s
1.6 × 10−3 s
= +8400 N
The force is positive, indicating that it points opposite to the velocity of
the approaching ball. A force of 8400 N corresponds to 1900 lb, such a
large value being necessary to change the ball’s momentum during the
brief contact time.
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟ ⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟
178 CHAPTER 7 Impulse and Momentum
EXAMPLE 2 A Rainstorm
During a storm, rain comes straight down with a velocity of v0→ = ‒15 m/s and hits the roof of a car perpendicularly (see Figure 7.4). The mass of rain per second that strikes the car roof is 0.060 kg/s. Assuming that the
rain comes to rest upon striking the car (vf→ = 0 m/s), fi nd the average force exerted by the rain on the roof.
Reasoning This example diff ers from Example 1 in an important way. Example 1 gives information about the ball and asks for the force applied
to the ball. In contrast, the present example gives information about the
rain but asks for the force acting on the roof. However, the force exerted
on the roof by the rain and the force exerted on the rain by the roof have
equal magnitudes and opposite directions, according to Newton’s law of
action and reaction (see Section 4.5). Thus, we will fi nd the force exerted
on the rain and then apply the law of action and reaction to obtain the force
on the roof. Two forces act on the rain while it impacts with the roof: the
average force F→ exerted by the roof and the weight of the rain. These two forces constitute the net average force. By comparison, however, the force
F→ is much greater than the weight, so we may neglect the weight. Thus, the net average force becomes equal to F→, or ΣF→ = F→. The value of F→ can be obtained by applying the impulse–momentum theorem to the rain.
Solution The average force F→ needed to reduce the rain’s velocity from v0→ = ‒15 m/s to vf→ = 0 m/s is given by Equation 7.4 as
F→ = mv→ f − mv→0
∆ t = −( m∆ t) v
→
0
The term m/∆t is the mass of rain per second that strikes the roof, so that m/∆t = 0.060 kg/s. Thus, the average force exerted on the rain by the roof is
F→ = −(0.060 kg /s)(−15 m /s) = +0.90 N
This force is in the positive or upward direction, which is reasonable since
the roof exerts an upward force on each falling drop in order to bring it to
rest. According to the action–reaction law, the force exerted on the roof
by the rain also has a magnitude of 0.90 N but points downward: Force
on roof = −0.90 N .
v0
Raindrop
vf = 0 m/s
FIGURE 7.4 A raindrop falling on a car roof has an initial velocity of v0→ just before striking the roof. The fi nal velocity of the
raindrop is vf→ = 0 m/s, because it comes to rest on the roof.
As you reason through problems such as those in Examples 1 and 2, take advantage of the
impulse–momentum theorem. It is a powerful statement that can lead to signifi cant insights. The
following Conceptual Example further illustrates its use.
Answers (a) and (b) are incorrect. The change ∆v→ in the velocity of a raindrop is smaller than that of a hailstone, since a raindrop does not
rebound after striking the roof. According to the impulse–momentum
theorem, a smaller impulse acts on a raindrop. But impulse is the product
of the average force and the time interval ∆ t. Since the same amount of mass falls in the same time interval in either case, ∆ t is the same for both a raindrop and a hailstone. The smaller impulse acting on a raindrop,
then, means that the car roof exerts a smaller force on it. By Newton’s
v0
Hailstone
vf
FIGURE 7.5 Hailstones have a downward velocity of v0→ just before striking this car roof. They rebound
with an upward velocity of vf→ .
CONCEPTUAL EXAMPLE 3 Hailstones Versus Raindrops
In Example 2 rain is falling on the roof of a car and exerts a force on it.
Instead of rain, suppose hail is falling. The hail comes straight down at a
mass rate of m/∆t = 0.060 kg/s and an initial velocity of v0→ = ‒15 m/s and strikes the roof perpendicularly, just as the rain does in Example 2. How-
ever, unlike rain, hail usually does not come to rest after striking a surface.
Instead, the hailstones bounce off the roof of the car. If hail fell instead
of rain, would the force on the roof be (a) smaller than, (b) equal to, or (c) greater than that calculated in Example 2?
Reasoning The raindrops and the hailstones fall in the same manner. That is, both fall with the same initial velocity and mass rate, and both
strike the roof perpendicularly. However, there is an important diff er-
ence: the raindrops come to rest (see Figure 7.4) after striking the roof, whereas the hailstones bounce upward (see Figure 7.5). According to the impulse–momentum theorem (Equation 7.4), the impulse that acts
on an object is equal to the change in the object’s momentum. This
change is mvf→ ‒ mv0→ = m ∆v→ and is proportional to the change ∆v→ in the velocity. For a raindrop, the change in velocity is from v0→ (down- ward) to zero. For a hailstone, the change is from v0→ (downward) to vf→ (upward). Thus, a raindrop and a hailstone experience diff erent changes
in velocity, and, hence, diff erent changes in momentum and diff erent
impulses.
7.2 The Principle of Conservation of Linear Momentum 179
Check Your Understanding
(The answers are given at the end of the book.) 1. Two identical automobiles have the same speed, one traveling east and one traveling west. Do these cars
have the same momentum?
2. In Times Square in New York City, people celebrate on New Year’s Eve. Some just stand around, but many move about randomly. Consider a group consisting of all of these people. Approximately, what is
the total linear momentum of this group at any given instant?
3. Two objects have the same momentum. Do the velocities of these objects necessarily have (a) the same directions and (b) the same magnitudes?
4. (a) Can a single object have a kinetic energy but no momentum? (b) Can a group of two or more objects have a total kinetic energy that is not zero but a total momentum that is zero?
5. Suppose you are standing on the edge of a dock and jump straight down. If you land on sand your stop- ping time is much shorter than if you land on water. Using the impulse–momentum theorem as a guide,
determine which one of the following statements is correct. (a) In bringing you to a halt, the sand exerts a greater impulse on you than does the water. (b) In bringing you to a halt, the sand and the water exert the same impulse on you, but the sand exerts a greater average force. (c) In bringing you to a halt, the sand and the water exert the same impulse on you, but the sand exerts a smaller average force.
6. An airplane is fl ying horizontally with a constant momentum during a time interval ∆ t. (a) Is there a net impulse acting on the plane during this time? Use the impulse–momentum theorem to guide your thinking. (b) In the horizontal direction, both the thrust generated by the engines and air resistance act on the plane. Considering your answer to part (a), how is the impulse of the thrust related (in magnitude
and direction) to the impulse of the force due to the air resistance?
7.2 The Principle of Conservation of Linear Momentum It is worthwhile to compare the impulse–momentum theorem to the work–energy theorem dis-
cussed in Chapter 6. The impulse–momentum theorem states that the impulse produced by a net
force is equal to the change in the object’s momentum, whereas the work–energy theorem states that
the work done by a net force is equal to the change in the object’s kinetic energy. The work–energy
theorem leads directly to the principle of conservation of mechanical energy (see Section 6.5),
and, as we will shortly see, the impulse–momentum theorem also leads to a conservation prin-
ciple, known as the conservation of linear momentum.
We begin by applying the impulse–momentum theorem to a midair collision between two
objects. The two objects (masses m1 and m2) are approaching each other with initial velocities v01→ and v02→ , as Interactive Figure 7.6a shows. The collection of objects being studied is referred to as the “system.” In this case, the system contains only the two objects. They interact during the
collision in part b and then depart with the fi nal velocities vf1→ and vf2→ shown in part c. Because of the collision, the initial and fi nal velocities are not the same.
Two types of forces act on the system:
1. Internal forces: Forces that the objects within the system exert on each other. 2. External forces: Forces exerted on the objects by agents external to the system.
third law, this implies that a raindrop, not a hailstone, exerts a smaller
force on the roof.
Answer (c) is correct. A hailstone experiences a larger change in momentum than does a raindrop, since a hailstone rebounds after
striking the roof. Therefore, according to the impulse–momentum
theorem, a greater impulse acts on a hailstone. An impulse is the prod-
uct of the average force and the time interval ∆ t. Since the same amount
of mass falls in the same time interval in either case, ∆ t is the same for a hailstone as for a raindrop. The greater impulse acting on a hailstone
means that the car roof exerts a greater force on a hailstone than on a
raindrop. According to Newton’s action–reaction law (see Section 4.5)
then, the car roof experiences a greater force from the hail than from
the rain.
Related Homework: Problems 3, 7
m1 m2
v01
F12
vf1 vf2
F21
v02
(a) Before collision
(b) During collision
(c) After collision
INTERACTIVE FIGURE 7.6 (a) The velocities of the two objects before the collision are v01→ and v02→ . (b) During the collision, each object exerts a force on the other. These forces are
F12 →
and F21 →
. (c) The velocities after the collision are vf1→ and vf2→ .
180 CHAPTER 7 Impulse and Momentum
During the collision in Interactive Figure 7.6b, F12 →
is the force exerted on object 1 by object 2,
while F21 →
is the force exerted on object 2 by object 1. These forces are action–reaction forces
that are equal in magnitude but opposite in direction, so F12 →
= ‒F21 →
. They are internal forces,
since they are forces that the two objects within the system exert on each other. The force of
gravity also acts on the objects, their weights being W1 →
and W2 →
. These weights, however, are
external forces, because they are applied by the earth, which is outside the system. Friction and
air resistance would also be considered external forces, although these forces are ignored here
for the sake of simplicity. The impulse–momentum theorem, as applied to each object, gives the
following results:
Object 1 (W1 →
+ F→12) ∆t = m1vf1→ − m1v01→
Object 2 (W2 →
+ F→21) ∆t = m2vf 2→ − m2v02→
Adding these equations produces a single result for the system as a whole:
(W1 →
+ W2 →
+ F→12 + F →
21) ∆t = (m1vf1→ + m2vf2→ ) ‒ (m1v01→ + m2v02→ )
On the right side of this equation, the quantity m1vf1→ + m2vf2→ is the vector sum of the fi nal momenta for each object, or the total fi nal momentum Pf
→ of the system. Likewise, the quantity
m1v01→ + m2v02→ is the total initial momentum P0 →
. Therefore, the result above becomes
(Sum of averageexternal forces Sum of averageinternal forces+ ) ∆t = Pf →
− P0 →
(7.5)
The advantage of the internal/external force classifi cation is that the internal forces always
add together to give zero, as a consequence of Newton’s law of action–reaction; F→12 = ‒F →
21 so
that F→12 + F →
21 = 0. Cancellation of the internal forces occurs no matter how many parts there are
to the system and allows us to ignore the internal forces, as Equation 7.6 indicates:
(Sum of average external forces) ∆t = Pf →
‒ P0 →
(7.6)
We developed this result with gravity as the only external force. But, in general, the sum of the
external forces on the left includes all external forces. With the aid of Equation 7.6, it is possible to see how the conservation of linear momentum
arises. Suppose that the sum of the external forces is zero. A system for which this is true is called
an isolated system. Then Equation 7.6 indicates that
0 = Pf → − P0
→ or Pf → = P0
→ (7.7a)
Thus, the fi nal total momentum of the isolated system after the objects in Interactive Figure 7.6 collide is the same as the initial total momentum.* Explicitly writing out the fi nal and initial
momenta for the two-body collision, we obtain from Equation 7.7a that
m1vf1→ + m2vf2→ = m1v01→ + m2v02→ (7.7b)
Pf →
P0 →
This result is an example of a general principle known as the principle of conservation of linear momentum.
⏟ External
force
⏟ Internal
force
⏟ External
force
⏟ Internal
force
External
forces
Internal
forces
Total fi nal
momentum Pf →
Total initial
momentum P0 →
⏟⎵⏟⎵⏟ ⏟⎵⏟⎵⏟ ⏟⎵⎵⎵⏟⎵⎵⎵⏟ ⏟⎵⎵⎵⏟⎵⎵⎵⏟
⏟⎵⎵⎵⏟⎵⎵⎵⏟ ⏟⎵⎵⎵⏟⎵⎵⎵⏟
*Technically, the initial and fi nal momenta are equal when the impulse of the sum of the external forces is zero—that
is, when the left-hand side of Equation 7.6 is zero. Sometimes, however, the initial and fi nal momenta are very nearly
equal even when the sum of the external forces is not zero. This occurs when the time ∆t during which the forces act is so short that it is eff ectively zero. Then, the left-hand side of Equation 7.6 is approximately zero.
7.2 The Principle of Conservation of Linear Momentum 181
PRINCIPLE OF CONSERVATION OF LINEAR MOMENTUM The total linear momentum of an isolated system remains constant (is conserved). An isolated system is one for which the vector sum of the average external forces acting on the system is zero.
The conservation-of-momentum principle applies to a system containing any number of
objects, regardless of the internal forces, provided the system is isolated. Whether the system
is isolated depends on whether the vector sum of the external forces is zero. Judging whether a
force is internal or external depends on which objects are included in the system, as Conceptual
Example 4 illustrates.
CONCEPTUAL EXAMPLE 4 Is the Total Momentum Conserved?
Imagine two balls colliding on a billiard table that is friction-free. Using
the momentum-conservation principle as a guide, decide which statement
is correct: (a) The total momentum of the system that contains only one of the two balls is the same before and after the collision. (b) The total momentum of the system that contains both of the two balls is the same
before and after the collision.
Reasoning The total momentum of an isolated system is the same before and after the collision; in such a situation the total momentum is
said to be conserved. An isolated system is one for which the vector sum
of the average external forces acting on the system is zero. To decide
whether statement (a) or (b) is correct, we need to examine the one-ball
and two-ball systems and see if they are, in fact, isolated.
Answer (a) is incorrect. In Figure 7.7a only one ball is included in the system, as indicated by the rectangular dashed box. The forces acting on
this system are all external and include the weight W1 →
of the ball and the
normal force FN1 →
due to the table. Since the ball does not accelerate in the
vertical direction, the normal force must balance the weight, so the vector
sum of these two vertical forces is zero. However, there is a third external
force to consider. Ball 2 is outside the system, so the force F12 →
that it
applies to the system (ball 1) during the collision is an external force. As
a result, the vector sum of the three external forces is not zero. Thus, the
one-ball system is not an isolated system, and its momentum is not the
same before and after the collision.
Answer (b) is correct. The rectangular dashed box in Figure 7.7b shows that both balls are included in the system. The collision forces are
not shown, because they are internal forces and cannot cause the total
momentum of the two-ball system to change. The external forces include
the weights W1 →
and W2 →
of the balls and the upward-pointing normal
forces FN1 →
and FN2 →
. Since the balls do not accelerate in the vertical direc-
tion, FN1 →
balances W1 →
, and FN2 →
balances W2 →
. Furthermore, the table
is friction-free. Thus, there is no net external force to change the total
momentum of the two-ball system, and, as a result, the total momentum is
the same before and after the collision.
FIGURE 7.7 Two billiard balls collide on a pool table. (a) The rectangular dashed box emphasizes that only one of the balls (ball 1) is
included in the system; W1 →
is its weight, FN1 →
is the normal force exerted
on ball 1 by the pool table, and F12 →
is the force exerted on ball 1 by ball 2.
(b) Now both balls are included in the system; W2 →
is the weight of ball 2,
and FN2 →
is the normal force acting on it.
FN1
F12
(a)
W1
(b)
FN1 FN2
W1 W2
Next, we apply the principle of conservation of linear momentum to the problem of assem-
bling a freight train.
Reasoning The two boxcars constitute the system. The sum of the exter- nal forces acting on the system is zero, because the weight of each car is
balanced by a corresponding normal force, and friction is being neglected.
Thus, the system is isolated, and the principle of conservation of linear
momentum applies. The coupling forces that each car exerts on the other
are internal forces and do not aff ect the applicability of this principle.
EXAMPLE 5 Assembling a Freight Train
A freight train is being assembled in a switching yard, and Animated Figure 7.8 shows two boxcars. Car 1 has a mass of m1 = 65 × 103 kg and moves at a velocity of υ01 = +0.80 m/s. Car 2, with a mass of m2 = 92 × 103 kg and a velocity of υ02 = +1.3 m/s, overtakes car 1 and couples to it. Neglecting friction, fi nd the common velocity υf of the cars after they become coupled.
182 CHAPTER 7 Impulse and Momentum
In the previous example it can be seen that the velocity of car 1 increases, while the veloc-
ity of car 2 decreases as a result of the collision. The acceleration and deceleration arise at
the moment the cars become coupled, because the cars exert internal forces on each other. The
powerful feature of the momentum-conservation principle is that it allows us to determine the
changes in velocity without knowing what the internal forces are. Example 6 further illustrates
this feature.
Problem-Solving Insight It is important to realize that the total linear momentum may be conserved even when the kinetic energies of the individual parts of a system change.
Problem-Solving Insight The conservation of linear momentum is applicable only when the net external force acting on the system is zero. Therefore, the fi rst step in applying momentum conservation is to be sure that the net external force is zero.
Solution Momentum conservation indicates that
(m1 + m2 )υf = m1υ01 + m2υ02⏟⎵⎵⏟⎵⎵⏟ ⏟⎵⎵⎵⏟⎵⎵⎵⏟ Total momentum
after collision
Total momentum
before collision
This equation can be solved for υf, the common velocity of the two cars after the collision:
υf = m1υ01 + m2υ02
m1 + m2
= (65 × 103 kg )(0.80 m /s) + (92 × 103 kg )(1.3 m /s)
(65 × 103 kg + 92 × 103 kg )
= +1.1 m /s
v02
m2
v01
(a) Before coupling (b) After coupling
vf
m1
ANIMATED FIGURE 7.8 (a) The boxcar on the left eventually catches up with the other boxcar and (b) couples to it. The coupled cars move together with a common velocity after the collision.
(b) After pushoff
f1 f2
(a) Before pushoff
m2 m1
– +
υ υ
INTERACTIVE FIGURE 7.9 (a) In the absence of friction, two skaters pushing on each other constitute an isolated system. (b) As the skaters move away, the total linear momentum of the system remains zero, which is what it was initially.
EXAMPLE 6 Ice Skaters
Reasoning For a system consisting of the two skaters on level ice, the sum of the external forces is zero. This is because the weight of each skater
is balanced by a corresponding normal force and friction is negligible. The
skaters, then, constitute an isolated system, and the principle of conserva-
tion of linear momentum applies. We expect the man to have a smaller
Starting from rest, two skaters push off against each other on smooth level
ice, where friction is negligible. As Interactive Figure 7.9a shows, one is a woman (m1 = 54 kg), and one is a man (m2 = 88 kg). Part b of the draw- ing shows that the woman moves away with a velocity of υf1 = +2.5 m/s. Find the “recoil” velocity υf2 of the man.
7.2 The Principle of Conservation of Linear Momentum 183
In Example 6, for instance, the initial kinetic energy is zero, since the skaters are stationary.
But after they push off , the skaters are moving, so each has kinetic energy. The kinetic energy
changes because work is done by the internal force that each skater exerts on the other. How-
ever, internal forces cannot change the total linear momentum of a system, since the total linear
momentum of an isolated system is conserved in the presence of such forces.
When applying the principle of conservation of linear momentum, we have been following a
defi nite reasoning strategy that is summarized as follows:
REASONING STRATEGY Applying the Principle of Conservation of Linear Momentum 1. Decide which objects are included in the system. 2. Relative to the system that you have chosen, identify the internal forces and the external
forces. 3. Verify that the system is isolated. In other words, verify that the sum of the external forces
applied to the system is zero. Only if this sum is zero can the conservation principle be applied. If the sum of the average external forces is not zero, consider a diff erent system for analysis.
4. Set the total fi nal momentum of the isolated system equal to the total initial momentum. Remember that linear momentum is a vector. If necessary, apply the conservation principle separately to the various vector components.
Check Your Understanding
(The answers are given at the end of the book.) 7. An object slides along the surface of the earth and slows down because of kinetic friction. If the object
alone is considered as the system, the kinetic frictional force must be identifi ed as an external force
that, according to Equation 7.4, decreases the momentum of the system. (a) If both the object and the earth are considered to be the system, is the force of kinetic friction still an external force? (b) Can the frictional force change the total linear momentum of the two-body system?
8. A satellite explodes in outer space, far from any other body, sending thousands of pieces in all direc- tions. Is the linear momentum of the satellite before the explosion less than, equal to, or greater than
the total linear momentum of all the pieces after the explosion?
recoil speed for the following reason: The internal forces that the man
and woman exert on each other during pushoff have equal magnitudes but
opposite directions, according to Newton’s action–reaction law. The man,
having the larger mass, experiences a smaller acceleration according to
Newton’s second law. Hence, he acquires a smaller recoil speed.
Solution The total momentum of the skaters before they push on each other is zero, since they are at rest. Momentum conservation requires that
the total momentum remains zero after the skaters have separated, as in
Interactive Figure 7.9b:
m1υ f1 + m2υ f2 = 0
Solving for the recoil velocity of the man gives
υ f 2 = −m1υf1
m2 =
−(54 kg )(+2.5 m /s)
88 kg = −1.5 m /s
The minus sign indicates that the man moves to the left in the drawing.
After the skaters separate, the total momentum of the system remains
zero, because momentum is a vector quantity, and the momenta of the
man and the woman have equal magnitudes but opposite directions.
Total momentum
after pushing
Total momentum
before pushing
⏟⎵⎵⎵⏟⎵⎵⎵⏟ ⏟
Math Skills When you use the momentum-conservation prin- ciple, you must choose which direction to call positive. The choice
is arbitrary, but it is important. The results of using the principle can only be interpreted with respect to your choice of the positive direction. In Example 6, the direction to the right has been se- lected as the positive direction (see Interactive Figure 7.9), with the result that the velocity υf1 of the woman is given as υf1 = +2.5 m/s, and the answer for the velocity υf2 of the man is υf2 = ‒1.5 m/s. This answer means that the man moves off in the negative di-
rection, which is to the left in the drawing. Suppose, however, that
the positive direction in Interactive Figure 7.9 had been chosen to be to the left. Then, the velocity υf1 of the woman would have been given as υf1 = ‒2.5 m/s, and the calculation for the velocity of the man would have revealed that the answer for υf2 is
υf 2 = −m1υf1
m2 =
−(54 kg)(−2.5 m /s)
88 kg = +1.5 m /s
This answer means that the man moves off in the positive direction,
which is now the direction to the left. Thus, the momentum-conservation
principle leads to the same conclusion for the man. He moves off to
the left, irrespective of the arbitrary choice of the positive direction.
(Continued)
184 CHAPTER 7 Impulse and Momentum
9. On a distant asteroid, a large catapult is used to throw chunks of stone into space. Could such a device be used as a propulsion system to move the asteroid closer to the earth?
10. A canoe with two people aboard is coasting with an initial momentum of +110 kg · m/s. Then, one of the people (person 1) dives off the back of the canoe. During this time, the net average external force
acting on the system (the canoe and the two people) is zero. The table lists four possibilities for the fi nal
momentum of person 1 and the fi nal momentum of person 2 plus the canoe, immediately after person 1
dives off . Only one possibility could be correct. Which one is it?
Final Momenta Person 1 Person 2 and Canoe
(a) ‒60 kg · m/s +170 kg · m/s
(b) ‒30 kg · m/s +110 kg · m/s
(c) ‒40 kg · m/s ‒70 kg · m/s
(d) +80 kg · m/s ‒30 kg · m/s
11. You are a passenger on a jetliner that is fl ying at a constant velocity. You get up from your seat and walk toward the front of the plane. Because of this action, your forward momentum increases. Does the
forward momentum of the plane itself decrease, remain the same, or increase?
12. An ice boat is coasting on a frozen lake. Friction between the ice and the boat is negligible, and so is air resistance. Nothing is propelling the boat. From a bridge someone jumps straight down into the boat,
which continues to coast straight ahead. (a) Does the total horizontal momentum of the boat plus the jumper change? (b) Does the speed of the boat itself increase, decrease, or remain the same?
13. Concept Simulation 7.1 at www.wiley.com/college/cutnell reviews the concepts that are pertinent in this question. In movies, Superman hovers in midair, grabs a villain by the neck, and throws him
forward. Superman, however, remains stationary. This is not possible, because it violates which one or
more of the following: (a) The law of conservation of energy (b) Newton’s second law (c) Newton’s third law (d) The principle of conservation of linear momentum
14. The energy released by the exploding gunpowder in a cannon propels the cannonball forward. Simul- taneously, the cannon recoils. The mass of the cannonball is less than that of the cannon. Which has
the greater kinetic energy, the launched cannonball or the recoiling cannon? Assume that momentum
conservation applies.
7.3 Collisions in One Dimension As discussed in the previous section, the total linear momentum is conserved when two objects
collide, provided they constitute an isolated system. When the objects are atoms or subatomic
particles, the total kinetic energy of the system is often conserved also. In other words, the total
kinetic energy of the particles before the collision equals the total kinetic energy of the particles
after the collision, so that kinetic energy gained by one particle is lost by another.
In contrast, when two macroscopic objects collide, such as two cars, the total kinetic energy
after the collision is generally less than that before the collision. Kinetic energy is lost mainly
in two ways: (1) It can be converted into heat because of friction, and (2) it is spent in creating
permanent distortion or damage, as in an automobile collision. With very hard objects, such as
a solid steel ball and a marble fl oor, the permanent distortion suff ered upon collision is much
smaller than with softer objects and, consequently, less kinetic energy is lost.
Collisions are often classifi ed according to whether the total kinetic energy changes during
the collision:
1. Elastic collision: One in which the total kinetic energy of the system after the collision is equal to the total kinetic energy before the collision.
2. Inelastic collision: One in which the total kinetic energy of the system is not the same before and after the collision; if the objects stick together after colliding, the collision is said to be
completely inelastic.
7.3 Collisions in One Dimension 185
Problem-Solving Insight As long as the net external force is zero, the conservation of linear momentum applies to any type of collision. This is true whether the collision is elastic or inelastic.
The boxcars coupling together in Animated Figure 7.8 provide an example of a completely inelastic collision. When a collision is completely inelastic, the greatest amount of kinetic energy
is lost. Example 7 shows how one particular elastic collision is described using the conservation
of linear momentum and the fact that no kinetic energy is lost.
Analyzing Multiple-Concept Problems
EXAMPLE 7 A Head-On Collision
Figure 7.10 illustrates an elastic head-on collision between two balls. One ball has a mass of m1 = 0.250 kg and an initial velocity of +5.00 m/s. The other has a mass of m2 = 0.800 kg and is initially at rest. No exter- nal forces act on the balls. What are the velocities of the balls after the
collision?
Reasoning Three facts will guide our solution. The fi rst is that the col- lision is elastic, so that the kinetic energy of the two-ball system is the
same before and after the balls collide. The second fact is that the colli-
sion occurs head-on. This means that the velocities before and after the
balls collide all point along the same line. In other words, the collision
occurs in one dimension. Last, no external forces act on the balls, with the
result that the two-ball system is isolated and its total linear momentum is
conserved. We expect that ball 1, having the smaller mass, will rebound to
the left after striking ball 2, which is more massive. Ball 2 will be driven
to the right in the process.
Knowns and Unknowns The data for this problem are given in the following table:
Before collision
v01 v02 = 0 m/s
m1 m2
After collision
vf2vf1
– +
FIGURE 7.10 A 0.250-kg ball, traveling with an initial velocity of υ01 = +5.00 m/s, undergoes an elastic collision with a
0.800-kg ball that is initially at rest.
Description Symbol Value Comment Explicit Data Mass of ball 1 m1 0.250 kg
Initial velocity of ball 1 υ01 +5.00 m/s Before collision occurs.
Mass of ball 2 m2 0.800 kg
Implicit Data Initial velocity of ball 2 υ02 0 m/s Before collision occurs, ball is initially at rest.
Unknown Variables Final velocity of ball 1 υf1 ? After collision occurs.
Final velocity of ball 2 υf2 ? After collision occurs.
Modeling the Problem
STEP 1 Elastic Collision Since the collision is elastic, the kinetic energy of the two-ball system is the same before and after the balls collide:
1
2m1υf12 + 1
2m2υf22 = 1
2m1υ012 + 0
Here we have utilized the fact that ball 2 is at rest before the collision. Thus, its initial velocity υ02 is zero and so is its initial kinetic energy. Solving this equation for υf12, the square of the velocity of ball 1 after the collision, gives Equation 1 at the right. To use this result, we need a value for
υf2, which we will obtain in Step 2.
Total kinetic energy
after collision
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟ Total kinetic energy
before collision
⏟⎵⎵⏟⎵⎵⏟ ?
υf12 = υ012 − m2 m1
υf 22 (1)
186 CHAPTER 7 Impulse and Momentum
STEP 2 Conservation of Linear Momentum Total linear momentum of the two-ball system is conserved since no external forces act on the system. This fact does not depend on
whether the collision is elastic. Conservation of linear momentum indicates that
m1υf1 + m2υf2 = m1υ01 + 0
We have again utilized the fact that ball 2 is at rest before the collision; since its initial velocity
υ02 is zero, so is its initial momentum. Solving the expression above for υf2 gives
υf2 = m1 m2
(υ01 − υf1)
which can be substituted into Equation 1, as shown at the right.
Solution Algebraically combining the results of each step, we fi nd that
υf12 = υ012 − m2 m1
υf 22 = υ012 − m2 m1[
m1 m2
(υ01 − υf1) ] 2
Solving for υf1 shows that
υf1 = ( m1 − m2 m1 + m2) υ01 = (
0.250 kg − 0.800 kg
0.250 kg + 0.800 kg) (+5.00 m /s) = −2.62 m /s (7.8a)
Total momentum
after collision
⏟⎵⎵⎵⏟⎵⎵⎵⏟ Total momentum
before collision
⏟⎵⎵⏟⎵⎵⏟
STEP 1 STEP 2
Math Skills The equation υf12 = υ012 − m2 m1[
m1 m2
(υ01 − υf1) ] 2
is a quadratic equation,
because it contains the square of the unknown variable υf1. Such equations can always be solved using the quadratic formula (see Appendix C.4, Equation C-2), although it is often
awkward and time consuming to do so. A more sensible approach in this case is to begin
by rearranging the equation as follows:
υ 2f1 = υ 201 − m2 m1
m1 m2
m1 m2
(υ01 − υf1) 2 or υ 2f1 = υ 201 − m1 m2
(υ01 − υf1) 2
Further rearrangement and use of the fact that υ012 − υf12 = (υ01 − υf1) (υ01 + υf1) produces
υ012 − υf12 = m1 m2
(υ01 − υf1)2 or (υ01 − υf1) (υ01 + υf1) = m1 m2
(υ01 − υf1) (υ01 − υf1)
This result is equivalent to
υ01 + υf1 = m1 m2
υ01 − m1 m2
υf1 or ( m1 m2
+ 1) υf1 = ( m1 m2
− 1) υ01 Thus, we fi nd that
υf1 = (
m1 m2
− 1) (
m1 m2
+1) υ01 or υf1 = (
m1 − m2 m1 + m2) υ01
Substituting the expression for υf1 into Equation 2 gives
υf 2 = ( 2m1
m1 + m2) υ01 = [ 2(0.250 kg)
0.250 kg + 0.800 kg ](+5.00 m /s) = +2.38 m /s (7.8b) The negative value for υf1 indicates that ball 1 rebounds to the left after the collision in Figure 7.10, while the positive value for υf2 indicates that ball 2 moves to the right, as expected.
Related Homework: Problems 37, 46, 55
υf12 = υ012 − m2 m1
υf 22 (1)
υf2 = m1 m2
(υ01 − υf1) (2)
7.3 Collisions in One Dimension 187
We can get a feel for an elastic collision by dropping a steel ball onto a hard surface, such
as a marble fl oor. If the collision were elastic, the ball would rebound to its original height, as
Figure 7.11a illustrates. In contrast, a partially defl ated basketball exhibits little rebound from a relatively soft asphalt surface, as in part b, indicating that a fraction of the ball’s kinetic energy is dissipated during the inelastic collision. The very defl ated basketball in part c has no bounce at all, and a maximum amount of kinetic energy is lost during the completely inelastic collision.
The next example illustrates a completely inelastic collision in a device called a “ballistic
pendulum.” This device can be used to measure the speed of a bullet.
(a) Elastic collision (b) Inelastic collision (c) Completely inelastic collision
FIGURE 7.11 (a) A hard steel ball would rebound to its original height after striking
a hard marble surface if the collision were
elastic. (b) A partially defl ated basketball has little bounce on a soft asphalt surface. (c) A very defl ated basketball has no bounce at all.
Analyzing Multiple-Concept Problems
EXAMPLE 8 The Physics of Measuring the Speed of a Bullet
A ballistic pendulum can be used to measure the speed of a projectile,
such as a bullet. The ballistic pendulum shown in Figure 7.12a consists of a stationary 2.50-kg block of wood suspended by a wire of negligible
mass. A 0.0100-kg bullet is fi red into the block, and the block (with the
bullet in it) swings to a maximum height of 0.650 m above the initial po-
sition (see part b of the drawing). Find the speed with which the bullet is fi red, assuming that air resistance is negligible.
Reasoning The physics of the ballistic pendulum can be divided into two parts. The fi rst is the completely inelastic collision between the
bullet and the block. The total linear momentum of the system (block plus
bullet) is conserved during the collision, because the suspension wire sup-
ports the system’s weight, which means that the sum of the external forces
acting on the system is nearly zero. The second part of the physics is the
resulting motion of the block and bullet as they swing upward after the
collision. As the system swings upward, the principle of conservation of
mechanical energy applies, since nonconservative forces do no work (see
Section 6.5). The tension force in the wire does no work because it acts
perpendicular to the motion. Since air resistance is negligible, we can
ignore the work it does. The conservation principles for linear momentum
and mechanical energy provide the basis for our solution.
Knowns and Unknowns The data for this problem are as follows:
m1
v01
(a)
m1 + m2
vf
(b)
h f = 0.650 m
m2
FIGURE 7.12 (a) A bullet approaches a ballistic pendulum. (b) The block and bullet swing upward after the collision.
Description Symbol Value Comment Explicit Data Mass of bullet m1 0.0100 kg
Mass of block m2 2.50 kg
Height to which block plus bullet swings hf 0.650 m Maximum height of swing.
Implicit Data Initial velocity of block υ02 0 m/s Before collision, block is stationary.
Unknown Variable Speed with which bullet is fired υ01 ? Before collision with block.
188 CHAPTER 7 Impulse and Momentum
Modeling the Problem
STEP 1 Completely Inelastic Collision Just after the bullet collides with it, the block (with the bullet in it) has a speed υf. Since linear momentum is conserved, the total momentum of the block–bullet system after the collision is the same as it is before the collision:
(m1 + m2)υf = m1υ01 + 0
Note that the block is at rest before the collision (υ02 = 0 m/s), so its initial momentum is zero. Solving this equation for υ01 gives Equation 1 at the right. To fi nd a value for the speed υf in this equation, we turn to Step 2.
STEP 2 Conservation of Mechanical Energy The speed υf immediately after the collision can be obtained from the maximum height hf to which the system swings, by using the principle of conservation of mechanical energy:
(m1 + m2)ghf = 1
2(m1 + m2)υf2
This result can be solved for υf to show that
υf = √2ghf
which can be substituted into Equation 1, as shown at the right. In applying the energy-
conservation principle, it is tempting to say that the total potential energy at the top
of the swing is equal to the total kinetic energy of the bullet before it strikes the block
[(m1 + m2)ghf = 1
2m1υ021] and solve directly for υ01. This is incorrect, however, because the collision between the bullet and the block is inelastic, so that some of the bullet’s initial
kinetic energy is dissipated during the collision (due to friction and structural damage to the
block and bullet).
Solution Algebraically combining the results of each step, we fi nd that
υ01 = ( m1 + m2
m1 ) υf = ( m1 + m2
m1 ) √2ghf
υ01 = ( 0.0100 kg + 2.50 kg
0.0100 kg )√2(9.80 m /s2)(0.650 m) = +896 m /s
Related Homework: Problem 29
Total momentum
after collision
⏟⎵⎵⎵⏟⎵⎵⎵⏟ Total momentum
before collision
⏟⎵⎵⏟⎵⎵⏟
Total mechanical energy
at bottom of swing, all
kinetic
⏟⎵⎵⎵⏟⎵⎵⎵⏟ ⏟⎵⎵⎵⏟⎵⎵⎵⏟ Total mechanical energy
at top of swing, all
potential
STEP 1 STEP 2
υ01 = ( m1 + m2
m1 ) υf (1)
υf = √2ghf
υ01 = ( m1 + m2
m1 ) υf (1)
?
Check Your Understanding
(The answers are given at the end of the book.) 15. Two balls collide in a one-dimensional elastic collision. The two balls constitute a system, and the net
external force acting on them is zero. The table shows four possible sets of values for the initial and
fi nal momenta of the two balls, as well as their initial and fi nal kinetic energies. Only one set of values
could be correct. Which set is it?
7.5 Center of Mass 189
16. In an elastic collision, is the kinetic energy of each object the same before and after the collision? 17. Concept Simulation 7.2 at www.wiley.com/college/cutnell illustrates the concepts that are involved
in this question. Also review Multiple-Concept Example 7. Suppose two objects collide head on, as
in Example 7, where initially object 1 (mass = m1) is moving and object 2 (mass = m2) is stationary. Now assume that they have the same mass, so m1 = m2. Which one of the following statements is true? (a) Both objects have the same velocity (magnitude and direction) after the collision. (b) Object 1 rebounds with one-half its initial speed, while object 2 moves to the right, as in Figure 7.10, with one-half the speed that object 1 had before the collision. (c) Object 1 stops completely, while object 2 acquires the same velocity (magnitude and direction) that object 1 had before the collision.
7.4 Collisions in Two Dimensions The collisions discussed so far have been head-on, or one-dimensional, because the veloci-
ties of the objects all point along a single line before and after contact. Collisions often
occur, however, in two or three dimensions. Figure 7.13 shows a two-dimensional case in which two balls collide on a horizontal frictionless table.
For the system consisting of the two balls, the external forces include the weights of the
balls and the corresponding normal forces produced by the table. Since each weight is bal-
anced by a normal force, the sum of the external forces is zero, and the total momentum of
the system is conserved, as Equation 7.7b indicates. Momentum is a vector quantity, how-
ever, and in two dimensions the x and y components of the total momentum are conserved separately. In other words, Equation 7.7b is equivalent to the following two equations:
x Component m1υ f1x + m2υ f 2x = m1υ01x + m2υ02x (7.9a)
Pfx P0x y Component m1υ f1y + m2υ f 2y = m1υ01y + m2υ02y (7.9b)
Pfy P0y These equations are written for a system that contains two objects. If a system contains
more than two objects, a mass-times-velocity term must be included for each additional
object on either side of Equations 7.9a and 7.9b.
7.5 Center of Mass In previous sections, we have encountered situations in which objects interact with one another,
such as the two skaters pushing off in Example 6. In these situations, the mass of the system is
located in several places, and the various objects move relative to each other before, after, and
⏟⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⏟ ⏟⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⏟ ⏟⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⏟ ⏟⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⏟
Initial (Before Collision)
Final (After Collision)
Momentum Kinetic Energy Momentum
Kinetic Energy
(a) Ball 1: +4 kg · m/s 12 J ‒5 kg · m/s 10 J
Ball 2: ‒3 kg · m/s 5 J ‒1 kg · m/s 7 J
(b) Ball 1: +7 kg · m/s 22 J +5 kg · m/s 18 J
Ball 2: +2 kg · m/s 8 J +4 kg · m/s 15 J
(c) Ball 1: ‒5 kg · m/s 12 J ‒6 kg · m/s 15 J
Ball 2: ‒8 kg · m/s 31 J ‒9 kg · m/s 25 J
(d) Ball 1: +9 kg · m/s 25 J +6 kg · m/s 18 J
Ball 2: +4 kg · m/s 15 J +7 kg · m/s 22 J
50.0°
35.0° +x
+y
+y
+x
01 = 0.900 m/s m1 = 0.150 kg
02 = 0.540 m/s m2 = 0.260 kg
f2 = 0.700 m/s
f1y
f1x
f1
f1
(a)
(b)
υ υ
υ
υ
υ
υ
υ
θ
θ
FIGURE 7.13 (a) Top view of two balls colliding on a horizontal frictionless table. (b) This part of the drawing shows the x and y components of the velocity of ball 1 after the collision.
190 CHAPTER 7 Impulse and Momentum
even during the interaction. It is possible, however, to speak of a kind of average location for the
total mass by introducing a concept known as the center of mass (abbreviated as “cm”). With the aid of this concept, we will be able to gain additional insight into the principle of conservation
of linear momentum.
The center of mass is a point that represents the average location for the total mass of a system.
Figure 7.14, for example, shows two particles of mass m1 and m2 that are located on the x axis at the positions x1 and x2, respectively. The position xcm of the center-of-mass point from the origin is defi ned to be
Center of mass xcm = m1 x1 + m2 x2
m1 + m2 (7.10)
Each term in the numerator of this equation is the product of a particle’s mass and position, while
the denominator is the total mass of the system. If the two masses are equal, we expect the average
location of the total mass to be midway between the particles. With m1 = m2 = m, Equation 7.10 becomes xcm = (mx1 + mx2)/(m + m) =
1
2(x1 + x2), which indeed corresponds to the point midway between the particles. Alternatively, suppose that m1 = 5.0 kg and x1 = 2.0 m, while m2 = 12 kg and x2 = 6.0 m. Then we expect the average location of the total mass to be located closer to particle 2, since it is more massive. Equation 7.10 is also consistent with this expectation, for it gives
xcm = (5.0 kg)(2.0 m) + (12 kg)(6.0 m)
5.0 kg + 12 kg = 4.8 m
If a system contains more than two particles, the center-of-mass point can be determined by
generalizing Equation 7.10. For three particles, for instance, the numerator would contain a third
term m3x3, and the total mass in the denominator would be m1 + m2 + m3. For a macroscopic object, which contains many, many particles, the center-of-mass point is located at the geometric
center of the object, provided that the mass is distributed symmetrically about the center. Such
would be the case for a billiard ball. For objects such as a golf club, the mass is not distributed
symmetrically, and the center-of-mass point is not located at the geometric center of the club. The
driver used to launch a golf ball from the tee, for instance, has more mass in the club head than in
the handle, so the center-of-mass point is closer to the head than to the handle.
Equation 7.10 (and its generalization to more than two particles) deals with particles that
lie along a straight line. A system of particles, however, may include particles that do not all lie
along a single straight line. For particles lying in a plane, an equation like Equation 7.10 uses the
x coordinates of each particle to give the x coordinate of the center of mass. A similar equation uses the y coordinates of each particle to give the y coordinate of the center of mass. If a system contains rigid objects, each of them may be treated as if it were a particle with all of the mass
located at the object’s own center of mass. In this way, a collection of rigid objects becomes a
collection of particles, and the x and y coordinates of the center of mass of the collection can be determined as described earlier in this paragraph.
To see how the center-of-mass concept is related to momentum conservation, suppose that
the two particles in a system are moving, as they would be during a collision. With the aid of
Equation 7.10, we can determine the velocity υcm of the center-of-mass point. During a time interval ∆t, the particles experience displacements of ∆x1 and ∆x2, as Interactive Figure 7.15 shows. They have diff erent displacements during this time because they have diff erent velocities.
Equation 7.10 can be used to fi nd the displacement ∆xcm of the center of mass by replacing xcm by ∆xcm, x1 by ∆x1, and x2 by ∆x2:
∆xcm = m1 ∆x1 + m2 ∆x2
m1 + m2 Now we divide both sides of this equation by the time interval ∆t. In the limit as ∆t becomes infi ni- tesimally small, the ratio ∆xcm/∆t becomes equal to the instantaneous velocity υcm of the center of mass. (See Section 2.2 for a review of instantaneous velocity.) Likewise, the ratios ∆x1 /∆t and ∆x2 /∆t become equal to the instantaneous velocities υ1 and υ2, respectively. Thus, we have
Velocity of center of mass υcm = m1υ1 + m2υ2
m1 + m2 (7.11)
The numerator (m1υ1 + m2υ2) on the right-hand side in Equation 7.11 is the momentum of particle 1 (m1υ1) plus the momentum of particle 2 (m2υ2), which is the total linear momentum of
xcm
x1
x2
m1
cm
m2
FIGURE 7.14 The center of mass cm of the two particles is located on a line between
them and lies closer to the more massive
particle.
Δxcm
Δx2Δx1
INTERACTIVE FIGURE 7.15 During a time interval ∆ t, the displacements of the particles are ∆x1 and ∆x2, while the displacement of the center of mass is ∆xcm.
7.5 Center of Mass 191
the system. In an isolated system, the total linear momentum does not change because of an
interaction such as a collision. Therefore, Equation 7.11 indicates that the velocity υcm of the center of mass does not change either. To emphasize this important point, consider the colli-
sion discussed in Example 7. With the data from that example, we can apply Equation 7.11
to determine the velocity of the center of mass before and after the collision:
Before collision υcm = (0.250 kg)(+5.00 m /s) + (0.800 kg)(0 m /s)
0.250 kg + 0.800 kg = +1.19 m /s
After collision υcm = (0.250 kg)(−2.62 m /s) + (0.800 kg)(+2.38 m /s)
0.250 kg + 0.800 kg = +1.19 m /s
Thus, the velocity of the center of mass is the same before and after the objects interact during
a collision in which the total linear momentum is conserved.
In a two-dimensional collision, the velocity of the center of mass is also the same before
and after the collision, provided that the total linear momentum is conserved. Figure 7.16 illustrates this fact. The drawing reproduces Figure 7.13a, except that the initial and fi nal center-of-mass locations are indicated, along with the velocity vector for the center of mass
at these two places (see the vectors labeled υcm). As the drawing shows, this velocity vector is the same before and after the balls collide. Thus, the center of mass moves along a straight
line as the two balls approach the collision point and continues along the same straight line
following the collision.
Check Your Understanding
(The answers are given at the end of the book.) 18. Would you expect the center of mass of a baseball bat to be located halfway between the ends of the
bat, nearer the lighter end, or nearer the heavier end?
19. A sunbather is lying on a fl oating raft that is stationary. She then gets up and walks to one end of the raft. Consider the sunbather and raft as an isolated system. (a) What is the velocity of the center of mass of this system while she is walking? (b) Does the raft itself move while she is walking? If so, what is the direction of the raft’s velocity relative to that of the sunbather?
20. Water, dripping at a constant rate from a faucet, falls to the ground. At any instant there are many drops in the air between the faucet and the ground. Where does the center of mass of the drops lie relative
to the halfway point between the faucet and the ground? (a) Above it (b) Below it (c) Exactly at the halfway point
f2
cm
cm
+x
+y
01
02
f1Center of mass
υ
υ υ
υ
υ
υ
FIGURE 7.16 This drawing shows the two balls in Figure 7.13a and the path followed by the center- of-mass point as the balls approach the collision point and then move away from it. Because of momentum conservation, the velocity of the center of mass of the balls is the same before and after the collision (see the vectors labeled υcm). As a result, the center of mass moves along the same straight- line path before and after the collision.
mass by applying Equation 7.10 twice, once for the x-direction and once for the y-direction.
Solution We have three mass segments, so we will have three terms in the numerator and denominator of Equation 7.10. Let’s begin with the
x-direction:
xcm = mAxA + mBxB + mCxC
mA + mB + mC
= (39 kg)(99 cm) + (20 kg)(37 cm) + (1.9 kg)(0 cm)
39 kg + 20 kg + 1.9 kg = 76 cm
And now for the y-direction:
ycm = mAyA + mByB + mCyC
mA + mB + mC
= (39 kg)(36 cm) + (20 kg)(37 cm) + (1.9 kg)(0 cm)
39 kg + 20 kg + 1.9 kg = 35 cm
EXAMPLE 9 BIO The Physics of High Jumpers—The “Fosbury Flop”
Track athletes participating in the high jump often utilize a technique
known as the Fosbury Flop, which is named for Dick Fosbury, who
fi rst brought attention to the technique in the 1968 Summer Olympics.
Here, the athlete positions the body in the air so as to actually travel
“backwards” over the bar, as shown in Figure 7.17a. We can see why this is such an eff ective technique by calculating the position of the
athlete’s center of mass, as the body maintains this curved shape while
passing over the bar. In Figure 7.17b we approximate the athlete’s body as consisting of three diff erent linear mass segments. Segment A
represents the mass of the head, neck, trunk, and arms. Segment B
represents the mass from the upper and lower legs, and Segment C
represents the mass from the feet. The masses and positions of the
centers of mass of each segment are indicated in Figure 7.17b. Use this information to calculate the position of the overall center of mass
of the three segments.
Reasoning This is a 2-dimensional center of mass problem, where we can fi nd the x- and y-coordinates of the position of the overall center of
192 CHAPTER 7 Impulse and Momentum
Concept Summary 7.1 The Impulse–Momentum Theorem The impulse J
→ of a force is the
product of the average force F →
and the time interval ∆ t during which the force acts, according to Equation 7.1. Impulse is a vector that points in
the same direction as the average force.
The linear momentum p →
of an object is the product of the object’s mass m and velocity v→, according to Equation 7.2. Linear momentum is a vector that points in the same direction as the velocity. The total linear momentum of a
system of objects is the vector sum of the momenta of the individual objects.
The impulse–momentum theorem states that when a net average force ΣF→ acts on an object, the impulse of this force is equal to the change in momentum
of the object, as in Equation 7.4.
J →
= F→∆ t (7.1)
p→ = mv→ (7.2)
(ΣF→)∆t = mv→f − mv →
0 (7.4)
7.2 The Principle of Conservation of Linear Momentum External forces are those forces that agents external to the system exert on objects
within the system. An isolated system is one for which the vector sum of the
external forces acting on the system is zero.
The principle of conservation of linear momentum states that the total lin-
ear momentum of an isolated system remains constant. For a two-body sys-
tem, the conservation of linear momentum can be written as in Equation 7.7b,
where m1 and m2 are the masses, v→f1 and v→f2 are the fi nal velocities, and v→01 and v→02 are the initial velocities of the objects.
m1vf1→ + m2vf2→ = m1v01→ + m2v02→ (7.7b)
7.3 Collisions in One Dimension An elastic collision is one in which the total kinetic energy of the system after the collision is equal to the total kinetic
Initial total linear
momentum
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟ ⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟
Final total linear
momentum
energy of the system before the collision. An inelastic collision is one in
which the total kinetic energy of the system is not the same before and after
the collision. If the objects stick together after the collision, the collision is
said to be completely inelastic.
7.4 Collisions in Two Dimensions When the total linear momentum is conserved in a two-dimensional collision, the x and y components of the total linear momentum are conserved separately. For a collision between
two objects, the conservation of total linear momentum can be written as in
Equations 7.9a and 7.9b.
m1υ f1x + m2υ f 2x = m1υ01x + m2υ02x (7.9a)
m1υ f1y + m2υ f 2y = m1υ01y + m2υ02y (7.9b)
7.5 Center of Mass The location of the center of mass of two particles lying on the x axis is given by Equation 7.10, where m1 and m2 are the masses of the particles and x1 and x2 are their positions relative to the coordinate origin. If the particles move with velocities υ1 and υ2, the velo- city υcm of the center of mass is given by Equation 7.11. If the total linear momentum of a system of particles remains constant during an interac-
tion such as a collision, the velocity of the center of mass also remains
constant.
xcm = m1x1 + m2x2
m1 + m2 (7.10)
υcm = m1υ1 + m2υ2
m1 + m2 (7.11)
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟
x component of fi nal total linear momentum
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟
x component of initial total linear momentum
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟
y component of fi nal total linear momentum
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟
y component of initial total linear momentum
Therefore, the position of the overall center of mass is given by (xcm = 76 cm, ycm = 35 cm). What makes this technique so eff ective is that it keeps the high jumper’s center of mass close to the ground. In fact,
her center of mass actually passes below the bar. Keeping her center of
mass closer to the ground reduces the total energy she needs to clear
the bar.
FIGURE 7.17 (a) High jumper clearing the bar by performing the Fosbury Flop. This technique allows her to keep her center of mass closer to the ground. (b) Approximate distribution of the high jumper’s mass as she passes over the bar. The masses and locations of diff erent parts of her body are
represented by the three segments in the fi gure.
+x
+y
Segment B Position (37 cm, 37 cm) mB = 20 kg
Segment C Position (0, 0) mC = 1.9 kg
Segment A Position (99 cm, 36 cm) mA = 39 kg
Bar
Overall center of mass (xcm, ycm)
(b)(a)
P JF
M il
it ar
y C
o ll
ec ti
o n /A
la m
y S
to ck
P h o to
Focus on Concepts 193
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 7.1 The Impulse–Momentum Theorem 1. Two identical cars are traveling at the same speed. One is heading due east and the other due north, as the drawing shows. Which statement is true
regarding the kinetic energies and momenta of the cars? (a) They both have the same kinetic energies and the same momenta. (b) They have the same kinetic energies, but diff erent momenta. (c) They have diff erent kinetic energies, but the same momenta. (d) They have diff erent kinetic energies and diff erent momenta.
QUESTION 1 East
North
υ
υ
2. Six runners have the mass (in multiples of m0), speed (in multiples of υ0), and direction of travel that are indicated in the table. Which two runners have identical momenta? (a) B and C (b) A and C (c) C and D (d) A and E (e) D and F
Runner Mass Speed Direction of Travel A 1
2 m0 υ0 Due north
B m0 υ0 Due east
C m0 2υ0 Due south
D 2m0 υ0 Due west
E m0 1 2υ0 Due north
F 2m0 2υ0 Due west
6. A particle is moving along the +x axis, and the graph shows its mo- mentum p as a function of time t. Use the impulse–momentum theorem to rank (largest to smallest) the three regions according to the magnitude of the impulse applied to the particle. (a) A, B, C (b) A, C, B (c) A and C (a tie), B (d) C, A, B (e) B, A, C
QUESTION 6 0
A
B
C
7654321 t (s)
p
7. A particle moves along the +x axis, and the graph shows its momentum p as a function of time t. In each of the four regions a force, which may or may not be nearly zero, is applied to the particle. In which region is the
magnitude of the force largest and in which region is it smallest? (a) B largest,
D smallest (b) C largest, B smallest (c) A largest, D smallest (d) C largest, A smallest (e) A largest, C smallest
QUESTION 7 0
A
B
C
D 765432
2
4
6
8
1
p (kg∙m/s)
t (s)
Section 7.2 The Principle of Conservation of Linear Momentum 10. As the text discusses, the conservation of linear momentum is applicable only when the system of objects is an isolated system. Which of the systems
listed below are isolated systems?
1. A ball is dropped from the top of a building. The system is the ball. 2. A ball is dropped from the top of a building. The system is the ball and
the earth.
3. A billiard ball collides with a stationary billiard ball on a frictionless pool table. The system is the moving ball.
4. A car slides to a halt in an emergency. The system is the car. 5. A space probe is moving in deep space where gravitational and other
forces are negligible. The system is the space probe.
(a) Only 2 and 5 are isolated systems. (b) Only 1 and 3 are isolated systems. (c) Only 3 and 5 are isolated systems. (d) Only 4 and 5 are isolated systems. (e) Only 5 is an isolated system.
Section 7.3 Collisions in One Dimension 13. Two objects are involved in a completely inelastic one-dimensional collision. The net external force acting on them is zero. The table lists four
possible sets of the initial and fi nal momenta and kinetic energies of the two
objects. Which is the only set that could occur?
Initial (Before Collision)
Final (After Collision)
Momentum Kinetic Energy Momentum
Kinetic Energy
a. Object 1: +6 kg · m /s 15 J +8 kg · m /s 9 J
Object 2: 0 kg · m /s 0 J
b. Object 1: +8 kg · m /s 5 J +6 kg · m /s 12 J
Object 2: −2 kg · m /s 7 J
c. Object 1: −3 kg · m /s 1 J +1 kg · m /s 4 J
Object 2: +4 kg · m /s 6 J
d. Object 1: 0 kg · m /s 3 J −8 kg · m /s 11 J
Object 2: −8 kg · m /s 8 J
Focus on Concepts
194 CHAPTER 7 Impulse and Momentum
Section 7.4 Collisions in Two Dimensions 15. Object 1 is moving along the x axis with an initial momentum of +16 kg · m/s, where the + sign indicates that it is moving to the right. As the drawing shows, object 1 collides with a second object that is initially at rest.
The collision is not head-on, so the objects move off in diff erent directions
after the collision. The net external force acting on the two-object system
is zero. After the collision, object 1 has a momentum whose y component is ‒5 kg · m/s. What is the y component of the momentum of object 2 after the collision? (a) 0 kg · m/s (b) +16 kg · m/s (c) +5 kg · m/s (d) ‒16 kg · m/s (e) The y component of the momentum of object 2 cannot be determined.
QUESTION 15
+y
+x 2
2
1
1
Section 7.5 Center of Mass 17. The drawing shows three particles that are moving with diff erent velocities. Two of the particles have mass m, and the third has a mass 2m. At the instant shown, the center of mass (cm) of the three particles is at the
coordinate origin. What is the velocity υcm (magnitude and direction) of the center of mass?
cm
+4.0 m/s
m m
2m +6.0 m/s
–8.0 m/s
y
xcm = ?υ
QUESTION 17
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 7.1 The Impulse–Momentum Theorem 1. E SSM A 46-kg skater is standing still in front of a wall. By pushing against the wall she propels herself backward with a velocity of ‒1.2 m/s.
Her hands are in contact with the wall for 0.80 s. Ignore friction and wind
resistance. Find the magnitude and direction of the average force she exerts
on the wall (which has the same magnitude as, but opposite direction to, the
force that the wall applies to her).
2. E A model rocket is constructed with a motor that can provide a total impulse of 29.0 N · s. The mass of the rocket is 0.175 kg. What is the speed that this rocket achieves when launched from rest? Neglect the eff ects of
gravity and air resistance.
3. E Before starting this problem, review Conceptual Example 3. Suppose that the hail described there bounces off the roof of the car with a velocity of
+15 m/s. Ignoring the weight of the hailstones, calculate the force exerted by
the hail on the roof. Compare your answer to that obtained in Example 2 for
the rain, and verify that your answer is consistent with the conclusion reached
in Conceptual Example 3.
4. E GO In a performance test, each of two cars takes 9.0 s to accelerate from rest to 27 m/s. Car A has a mass of 1400 kg, and car B has a mass of
1900 kg. Find the net average force that acts on each car during the test.
5. E SSM A volleyball is spiked so that its incoming velocity of +4.0 m/s is changed to an outgoing velocity of −21 m/s. The mass of the volleyball is
0.35 kg. What impulse does the player apply to the ball?
6. E Two arrows are fi red horizontally with the same speed of 30.0 m/s. Each arrow has a mass of 0.100 kg. One is fi red due east and the other due
south. Find the magnitude and direction of the total momentum of this
two-arrow system. Specify the direction with respect to due east.
7. E Refer to Conceptual Example 3 as an aid in understanding this prob- lem. A hockey goalie is standing on ice. Another player fi res a puck (m = 0.17 kg) at the goalie with a velocity of +65 m/s. (a) If the goalie catches the puck with his glove in a time of 5.0 × 10‒3 s, what is the average force
(magnitude and direction) exerted on the goalie by the puck? (b) Instead of catching the puck, the goalie slaps it with his stick and returns the puck
straight back to the player with a velocity of ‒65 m/s. The puck and stick are
in contact for a time of 5.0 × 10‒3 s. Now what is the average force exerted
on the goalie by the puck? Verify that your answers to parts (a) and (b) are
consistent with the conclusion of Conceptual Example 3.
8. E BIO When jumping straight down, you can be seriously injured if you land stiff -legged. One way to avoid injury is to bend your knees upon landing
to reduce the force of the impact. A 75-kg man just before contact with the
ground has a speed of 6.4 m/s. (a) In a stiff -legged landing he comes to a halt in 2.0 ms. Find the average net force that acts on him during this time. (b) When he bends his knees, he comes to a halt in 0.10 s. Find the average net
force now. (c) During the landing, the force of the ground on the man points upward, while the force due to gravity points downward. The average net force
acting on the man includes both of these forces. Taking into account the direc-
tions of the forces, fi nd the force of the ground on the man in parts (a) and (b).
9. E A space probe is traveling in outer space with a momentum that has a magnitude of 7.5 × 107 kg · m/s. A retrorocket is fi red to slow down the probe. It applies a force to the probe that has a magnitude of 2.0 × 106 N
and a direction opposite to the probe’s motion. It fi res for a period of 12 s.
Determine the momentum of the probe after the retrorocket ceases to fi re.
Problems
Problems 195
10. M MMH A stream of water strikes a stationary turbine blade horizont- ally, as the drawing illustrates. The incident water stream has a velocity of
+16.0 m/s, while the exiting water stream has a velocity of ‒16.0 m/s. The
mass of water per second that strikes the blade is 30.0 kg/s. Find the mag-
nitude of the average force exerted on the water by the blade.
PROBLEM 10
Stationary turbine blade
f = –16.0 m/s
0 = +16.0 m/sυ
υ
11. M GO A student (m = 63 kg) falls freely from rest and strikes the ground. During the collision with the ground, he comes to rest in a time of
0.040 s. The average force exerted on him by the ground is +18 000 N, where
the upward direction is taken to be the positive direction. From what height
did the student fall? Assume that the only force acting on him during the
collision is that due to the ground.
12. M V-HINT A golf ball strikes a hard, smooth fl oor at an angle of 30.0° and, as the drawing shows, rebounds at the same angle. The mass of the ball
is 0.047 kg, and its speed is 45 m/s just before and after striking the fl oor.
What is the magnitude of the impulse applied to the golf ball by the fl oor?
(Hint: Note that only the vertical component of the ball’s momentum changes during impact with the fl oor, and ignore the weight of the ball.)
PROBLEM 12
45 m/s
30.0° 30.0°
45 m/s
13. M V-HINT An 85-kg jogger is heading due east at a speed of 2.0 m/s. A 55-kg jogger is heading 32° north of east at a speed of 3.0 m/s. Find the
magnitude and direction of the sum of the momenta of the two joggers.
14. M GO A basketball (m = 0.60 kg) is dropped from rest. Just before strik- ing the fl oor, the ball has a momentum whose magnitude is 3.1 kg · m/s. At what height was the basketball dropped?
15. H SSM A dump truck is being fi lled with sand. The sand falls straight downward from rest from a height of 2.00 m above the truck bed, and the
mass of sand that hits the truck per second is 55.0 kg/s. The truck is parked on
the platform of a weight scale. By how much does the scale reading exceed
the weight of the truck and sand?
Section 7.2 The Principle of Conservation of Linear Momentum 16. E MMH In a science fi ction novel two enemies, Bonzo and Ender, are fi ghting in outer space. From stationary positions they push against each
other. Bonzo fl ies off with a velocity of +1.5 m/s, while Ender recoils with a
velocity of ‒2.5 m/s. (a) Without doing any calculations, decide which person has the greater mass. Give your reasoning. (b) Determine the ratio mBonzo/ mEnder of the masses of these two enemies. 17. E A 2.3-kg cart is rolling across a frictionless, horizontal track toward a 1.5-kg cart that is held initially at rest. The carts are loaded with strong
magnets that cause them to attract one another. Thus, the speed of each cart
increases. At a certain instant before the carts collide, the fi rst cart’s velocity
is +4.5 m/s, and the second cart’s velocity is ‒1.9 m/s. (a) What is the total
momentum of the system of the two carts at this instant? (b) What was the velocity of the fi rst cart when the second cart was still at rest?
18. E GO As the drawing illustrates, two disks with masses m1 and m2 are moving horizontally to the right at a speed of υ0. They are on an air-hockey table, which supports them with an essentially frictionless cushion of air.
They move as a unit, with a compressed spring between them, which has a
negligible mass. Then the spring is released and allowed to push the disks
outward. Consider the situation where disk 1 comes to a momentary halt
shortly after the spring is released. Assuming that m1 = 1.2 kg, m2 = 2.4 kg, and υ0 = +5.0 m/s, fi nd the velocity of disk 2 at that moment.
PROBLEM 18
m1 m2 0υ
19. E SSM A lumberjack (mass = 98 kg) is standing at rest on one end of a fl oating log (mass = 230 kg) that is also at rest. The lumberjack runs to the
other end of the log, attaining a velocity of +3.6 m/s relative to the shore,
and then hops onto an identical fl oating log that is initially at rest. Neglect
any friction and resistance between the logs and the water. (a) What is the velocity of the fi rst log just before the lumberjack jumps off ? (b) Determine the velocity of the second log if the lumberjack comes to rest on it.
20. E GO MMH An astronaut in his space suit and with a propulsion unit (empty of its gas propellant) strapped to his back has a mass of 146 kg. The
astronaut begins a space walk at rest, with a completely fi lled propulsion unit.
During the space walk, the unit ejects some gas with a velocity of +32 m/s.
As a result, the astronaut recoils with a velocity of ‒0.39 m/s. After the gas is
ejected, the mass of the astronaut (now wearing a partially empty propulsion
unit) is 165 kg. What percentage of the gas was ejected from the completely
fi lled propulsion unit?
21. E SSM A two-stage rocket moves in space at a constant velocity of 4900 m/s. The two stages are then separated by a small explosive charge
placed between them. Immediately after the explosion the velocity of the
1200-kg upper stage is 5700 m/s in the same direction as before the explo-
sion. What is the velocity (magnitude and direction) of the 2400-kg lower
stage after the explosion?
22. M V-HINT A 40.0-kg boy, riding a 2.50-kg skateboard at a velocity of +5.30 m/s across a level sidewalk, jumps forward to leap over a wall. Just
after leaving contact with the board, the boy’s velocity relative to the side-
walk is 6.00 m/s, 9.50° above the horizontal. Ignore any friction between the
skateboard and the sidewalk. What is the skateboard’s velocity relative to the
sidewalk at this instant? Be sure to include the correct algebraic sign with
your answer.
23. M GO The lead female character in the movie Diamonds Are Forever is standing at the edge of an off shore oil rig. As she fi res a gun, she is driven
back over the edge and into the sea. Suppose the mass of a bullet is 0.010 kg
and its velocity is +720 m/s. Her mass (including the gun) is 51 kg. (a) What recoil velocity does she acquire in response to a single shot from a stationary
position, assuming that no external force keeps her in place? (b) Under the same assumption, what would be her recoil velocity if, instead, she shoots a
blank cartridge that ejects a mass of 5.0 × 10‒4 kg at a velocity of +720 m/s?
24. M MMH A 0.015-kg bullet is fi red straight up at a falling wooden block that has a mass of 1.8 kg. The bullet has a speed of 810 m/s when it strikes the
block. The block originally was dropped from rest from the top of a building
and has been falling for a time t when the collision with the bullet occurs. As a result of the collision, the block (with the bullet in it) reverses direction, rises,
and comes to a momentary halt at the top of the building. Find the time t. 25. M SSM By accident, a large plate is dropped and breaks into three pieces. The pieces fl y apart parallel to the fl oor. As the plate falls, its mo-
mentum has only a vertical component and no component parallel to the
fl oor. After the collision, the component of the total momentum parallel to
the fl oor must remain zero, since the net external force acting on the plate has
196 CHAPTER 7 Impulse and Momentum
no component parallel to the fl oor. Using the data shown in the drawing, fi nd
the masses of pieces 1 and 2.
PROBLEM 25
25.0°
m1
m3 = 1.30 kg
m2 45.0°
1.79 m/s
3.00 m/s
3.07 m/s
26. H Adolf and Ed are wearing harnesses and are hanging at rest from the ceiling by means of ropes attached to them. Face to face, they push off against
one another. Adolf has a mass of 120 kg, and Ed has a mass of 78 kg. Follow-
ing the push, Adolf swings upward to a height of 0.65 m above his starting
point. To what height above his own starting point does Ed rise?
27. H SSM Available in WileyPLUS.
Section 7.3 Collisions in One Dimension,
Section 7.4 Collisions in Two Dimensions 28. E After sliding down a snow-covered hill on an inner tube, Ashley is coasting across a level snowfi eld at a constant velocity of +2.7 m/s. Miranda
runs after her at a velocity of +4.5 m/s and hops on the inner tube. How fast
do the two slide across the snow together on the inner tube? Ashley’s mass
is 71 kg and Miranda’s is 58 kg. Ignore the mass of the inner tube and any
friction between the inner tube and the snow.
29. E Consult Multiple-Concept Example 8 for background pertinent to this problem. A 2.50-g bullet, traveling at a speed of 425 m/s, strikes the
wooden block of a ballistic pendulum, such as that in Figure 7.12. The block has a mass of 215 g. (a) Find the speed of the bullet–block combination im- mediately after the collision. (b) How high does the combination rise above its initial position?
30. E GO One object is at rest, and another is moving. The two collide in a one-dimensional, completely inelastic collision. In other words, they stick
together after the collision and move off with a common velocity. Momentum
is conserved. The speed of the object that is moving initially is 25 m/s. The
masses of the two objects are 3.0 and 8.0 kg. Determine the fi nal speed of the
two-object system after the collision for the case when the large-mass object
is the one moving initially and the case when the small-mass object is the
one moving initially.
31. E SSM Batman (mass = 91 kg) jumps straight down from a bridge into a boat (mass = 510 kg) in which a criminal is fl eeing. The velocity of the boat
is initially +11 m/s. What is the velocity of the boat after Batman lands in it?
32. E A car (mass = 1100 kg) is traveling at 32 m/s when it collides head- on with a sport utility vehicle (mass = 2500 kg) traveling in the opposite
direction. In the collision, the two vehicles come to a halt. At what speed was
the sport utility vehicle traveling?
33. E SSM A 5.00-kg ball, moving to the right at a velocity of +2.00 m/s on a frictionless table, collides head-on with a stationary 7.50-kg ball. Find the
fi nal velocities of the balls if the collision is (a) elastic and (b) completely inelastic.
34. E CHALK The drawing shows a collision between two pucks on an air- hockey table. Puck A has a mass of 0.025 kg and is moving along the x axis
with a velocity of +5.5 m/s. It makes a collision with puck B, which has a
mass of 0.050 kg and is initially at rest. The collision is not head-on. After
the collision, the two pucks fl y apart with the angles shown in the drawing.
Find the fi nal speeds of (a) puck A and (b) puck B.
PROBLEM 34 Before collision
A +5.5 m/s
At rest
65°
37°
A
B
B
After collision
35. E SSM A projectile (mass = 0.20 kg) is fi red at and embeds itself in a stationary target (mass = 2.50 kg). With what percentage of the projectile’s
incident kinetic energy does the target (with the projectile in it) fl y off after
being struck?
36. E GO Object A is moving due east, while object B is moving due north. They collide and stick together in a completely inelastic collision. Momentum
is conserved. Object A has a mass of mA = 17.0 kg and an initial velocity of v→0A= 8.00 m /s, due east. Object B, however, has a mass of mB = 29.0 kg and an initial velocity of v→0B = 5.00 m /s, due north. Find the magnitude and direction of the total momentum of the two-object system after the collision.
37. E Multiple-Concept Example 7 deals with some of the concepts that are used to solve this problem. A cue ball (mass = 0.165 kg) is at rest on a
frictionless pool table. The ball is hit dead center by a pool stick, which ap-
plies an impulse of +1.50 N · s to the ball. The ball then slides along the table and makes an elastic head-on collision with a second ball of equal mass that
is initially at rest. Find the velocity of the second ball just after it is struck.
38. M CHALK GO A ball is attached to one end of a wire, the other end being fastened to the ceiling. The wire is held horizontal, and the ball is released
from rest (see the drawing). It swings downward and strikes a block initially
at rest on a horizontal frictionless surface. Air resistance is negligible, and
the collision is elastic. The masses of the ball and block are, respectively,
1.60 kg and 2.40 kg, and the length of the wire is 1.20 m. Find the velocity
(magnitude and direction) of the ball (a) just before the collision, and (b) just after the collision.
PROBLEM 38
+x
+y
39. M V-HINT A girl is skipping stones across a lake. One of the stones ac- cidentally ricochets off a toy boat that is initially at rest in the water (see the
drawing). The 0.072-kg stone strikes the boat at a velocity of 13 m/s, 15° below
due east, and ricochets off at a velocity of 11 m/s, 12° above due east. After
being struck by the stone, the boat’s velocity is 2.1 m/s, due east. What is the
mass of the boat? Assume the water off ers no resistance to the boat’s motion.
PROBLEM 39
13 m/s
11 m/s15°
12°
East
East
Additional Problems 197
40. M GO A mine car (mass = 440 kg) rolls at a speed of 0.50 m/s on a horizontal track, as the drawing shows. A 150-kg chunk of coal has a speed
of 0.80 m/s when it leaves the chute. Determine the speed of the car–coal
system after the coal has come to rest in the car.
PROBLEM 40
150 kg
0.80 m/s
0.50 m/s
25.0°
440 kg
41. M SSM A 50.0-kg skater is traveling due east at a speed of 3.00 m/s. A 70.0-kg skater is moving due south at a speed of 7.00 m/s. They collide and
hold on to each other after the collision, managing to move off at an angle
θ south of east, with a speed of υf. Find (a) the angle θ and (b) the speed υf, assuming that friction can be ignored.
42. M CHALK GO A 4.00-g bullet is moving horizontally with a velocity of +355 m/s, where the +sign indicates that it is moving to the right (see part a of the drawing). The bullet is approaching two blocks resting on a horizontal
frictionless surface. Air resistance is negligible. The bullet passes completely
through the fi rst block (an inelastic collision) and embeds itself in the second one,
as indicated in part b. Note that both blocks are moving after the collision with the bullet. The mass of the fi rst block is 1150 g, and its velocity is +0.550 m/s
after the bullet passes through it. The mass of the second block is 1530 g.
(a) What is the velocity of the second block after the bullet embeds itself? (b) Find the ratio of the total kinetic energy after the collisions to that before the collisions.
PROBLEM 42
vblock 2
Block 1 +355 m/s
mblock 1 = 1150 g mblock 2 = 1530 g mbullet = 4.00 g
Block 2
(a) Before collisions
+0.550 m/s
(b) After collisions
43. M V-HINT An electron collides elastically with a stationary hydrogen atom. The mass of the hydrogen atom is 1837 times that of the electron.
Assume that all motion, before and after the collision, occurs along the same
straight line. What is the ratio of the kinetic energy of the hydrogen atom
after the collision to that of the electron before the collision?
44. M GO A 60.0-kg person, running horizontally with a velocity of +3.80 m/s, jumps onto a 12.0-kg sled that is initially at rest. (a) Ignoring the eff ects of fric- tion during the collision, fi nd the velocity of the sled and person as they move
away. (b) The sled and person coast 30.0 m on level snow before coming to rest. What is the coeffi cient of kinetic friction between the sled and the snow?
45. H SSM Starting with an initial speed of 5.00 m/s at a height of 0.300 m, a 1.50-kg ball swings downward and strikes a 4.60-kg ball that is at rest, as
the drawing shows. (a) Using the principle of conservation of mechanical energy, fi nd the speed of the 1.50-kg ball just before impact. (b) Assuming that the collision is elastic, fi nd the velocities (magnitude and direction) of
both balls just after the collision. (c) How high does each ball swing after the collision, ignoring air resistance?
PROBLEM 45
5.00 m/s 0.300 m
1.50 kg
4.60 kg
46. H MMH Available in WileyPLUS. 47. H Available in WileyPLUS.
Section 7.5 Center of Mass 48. E Two particles are moving along the x axis. Particle 1 has a mass m1 and a velocity υ1 = +4.6 m/s. Particle 2 has a mass m2 and a velocity υ2 = ‒6.1 m/s. The velocity of the center of mass of these two particles is zero.
In other words, the center of mass of the particles remains stationary, even
though each particle is moving. Find the ratio m1/m2 of the masses of the particles.
49. E SSM Available in WileyPLUS. 50. E GO John’s mass is 86 kg, and Barbara’s is 55 kg. He is standing on the x axis at xJ = +9.0 m, while she is standing on the x axis at xB = 12.0 m. They switch positions. How far and in which direction does their center of
mass move as a result of the switch?
51. E GO Two stars in a binary system orbit around their center of mass. The centers of the two stars are 7.17 × 10 11 m apart. The larger of the two
stars has a mass of 3.70 × 10 30 kg, and its center is 2.08 × 10 11 m from the
system’s center of mass. What is the mass of the smaller star?
52. M GO The drawing shows a sulfur dioxide molecule. It consists of two oxygen atoms and a sulfur atom. A sulfur atom is twice as massive as an
oxygen atom. Using this information and the data provided in the drawing, fi nd
(a) the x coordinate and (b) the y coordinate of the center of mass of the sulfur dioxide molecule. Express your answers in nanometers (1 nm = 10‒9 m).
PROBLEM 52
60.0°
0.143 nm0.143 nm
60.0°
Sulfur
Oxygen Oxygen
x
y
53. E SSM MMH Available in WileyPLUS. 54. E GO A golf ball bounces down a fl ight of steel stairs, striking several steps on the way down, but never hitting the edge of a step. The ball starts at
the top step with a vertical velocity component of zero. If all the collisions
with the stairs are elastic, and if the vertical height of the staircase is 3.00 m,
determine the bounce height when the ball reaches the bottom of the stairs.
Neglect air resistance.
55. E Available in WileyPLUS.
Additional Problems
198 CHAPTER 7 Impulse and Momentum
56. E MMH A baseball (m = 149 g) approaches a bat horizontally at a speed of 40.2 m/s (90 mi/h) and is hit straight back at a speed of 45.6 m/s
(102 mi/h). If the ball is in contact with the bat for a time of 1.10 ms, what
is the average force exerted on the ball by the bat? Neglect the weight of the
ball, since it is so much less than the force of the bat. Choose the direction of
the incoming ball as the positive direction.
57. E SSM Available in WileyPLUS. 58. E BIO MMH For tests using a ballistocardiograph, a patient lies on a horizontal platform that is supported on jets of air. Because of the air jets,
the friction impeding the horizontal motion of the platform is negligible.
Each time the heart beats, blood is pushed out of the heart in a direction
that is nearly parallel to the platform. Since momentum must be conserved,
the body and the platform recoil, and this recoil can be detected to provide
information about the heart. For each beat, suppose that 0.050 kg of blood
is pushed out of the heart with a velocity of +0.25 m/s and that the mass of
the patient and platform is 85 kg. Assuming that the patient does not slip
with respect to the platform, and that the patient and platform start from rest,
determine the recoil velocity.
59. E MMH Available in WileyPLUS. 60. E GO A wagon is rolling forward on level ground. Friction is negli- gible. The person sitting in the wagon is holding a rock. The total mass of
the wagon, rider, and rock is 95.0 kg. The mass of the rock is 0.300 kg. Initially
the wagon is rolling forward at a speed of 0.500 m/s. Then the person throws
the rock with a speed of 16.0 m/s. Both speeds are relative to the ground. Find
the speed of the wagon after the rock is thrown directly forward in one case
and directly backward in another.
61. M Available in WileyPLUS. 62. M MMH Available in WileyPLUS. 63. M V-HINT Two ice skaters have masses m1 and m2 and are initially stationary. Their skates are identical. They push against one another, as in
Interactive Figure 7.9, and move in opposite directions with diff erent speeds. While they are pushing against each other, any kinetic frictional forces acting
on their skates can be ignored. However, once the skaters separate, kinetic
frictional forces eventually bring them to a halt. As they glide to a halt, the
magnitudes of their accelerations are equal, and skater 1 glides twice as far
as skater 2. What is the ratio m1/m2 of their masses? 64. M BIO V-HINT The drawing shows a human fi gure in a sitting position. For purposes of this problem, there are three parts to the fi gure, and the center
of mass of each one is shown in the drawing. These parts are: (1) the torso,
neck, and head (total mass = 41 kg) with a center of mass located on the
y axis at a point 0.39 m above the origin, (2) the upper legs (mass = 17 kg) with a center of mass located on the x axis at a point 0.17 m to the right of the origin, and (3) the lower legs and feet (total mass = 9.9 kg) with a center
of mass located 0.43 m to the right of and 0.26 m below the origin. Find the
x and y coordinates of the center of mass of the human fi gure. Note that the
mass of the arms and hands (approximately 12% of the whole-body mass)
has been ignored to simplify the drawing.
PROBLEM 64
0.39 m
0.17 m 0.26 m
0.26 m
+x
+y
65. H SSM Available in WileyPLUS. 66. M GO For the situation depicted in the fi gure, use momentum con- servation to determine the magnitude and direction of the fi nal velocity of
ball 1 after the collision.
PROBLEM 66
50.0˚
35.0° +x
+y
+y
+x
01 = 0.900 m/s m1 = 0.150 kg
02 = 0.540 m/s m2 = 0.260 kg
f2 = 0.700 m/s
f1y
f1x
f1
f1
(a)
(b)
θ
θ
υ
υ
υ
υ
υ
υ
υ
(a) Top view of two balls colliding on a horizontal surface. (b) This part of the drawing shows the x and y components of the velocity of ball 1 after the collision.
Momentum and energy are two of the most fundamental concepts in physics.
As we have seen in this chapter, momentum is a vector and, like all vectors,
has a magnitude and a direction. In contrast, energy is a scalar quantity,
as Chapter 6 discusses, and does not have a direction associated with it.
Problem 67 provides the opportunity to review how the vector nature of
momentum and the scalar nature of kinetic energy infl uence calculations
using these quantities. Problem 68 explores some further diff erences between
momentum and kinetic energy.
67. M CHALK SSM Two joggers, Jim and Tom, are both running at a speed of 4.00 m/s (see the fi gure). Jim has a mass of 90.0 kg, and Tom
has a mass of 55.0 kg. Concepts: (i) Does the total kinetic energy of the two-jogger system have a smaller value in part a or b of the fi gure, or is it the same in both cases? (ii) Does their total momentum have a smaller
magnitude in part a or b of the fi gure, or is it the same for each? Calcu- lations: Find the kinetic energy and momentum of the two-jogger system when (a) Jim and Tom are both running due north as in part a of the
Concepts and Calculations Problems
Team Problems 199
fi gure, and (b) Jim is running due north and Tom is running due south, as in part b of the fi gure.
(a)
Jim Tom
+4.00 m/s +4.00 m/s
N
S
W E
(a)
Jim Tom
(b)
Jim
Tom
+4.00 m/s
–4.00 m/s
PROBLEM 67
68. M CHALK The table gives mass and speed data for the two objects in the fi gure. Concepts: (i) Is it possible for two objects to have diff erent speeds when their momenta have the same amplitude? Explain your answer. (ii) If
two objects have the same momenta do they necessarily have the same kinetic
energy? Explain. Calculations: Find the magnitude of the momentum and the kinetic energy for each object.
Mass Speed Object A 2.0 kg 6.0 m/s
Object B 6.0 kg 2.0 m/s PROBLEM 68
2.0 kg
6.0 m/s
2.0 m/s
6.0 kg
A
B
69. M Docking a Spaceship. You and your crew must dock your 25000 kg spaceship at Spaceport Alpha, which is orbiting Mars. In the process, Alpha’s
control tower has requested that you ram another vessel, a freight ship of mass
16500 kg, latch onto it, and use your combined momentum to bring it into
dock. The freight ship is not moving with respect to the colossal Spaceport
Alpha, which has a mass of 1.85 × 107 kg. Alpha’s automated system that
guides incoming spacecraft into dock requires that the incoming speed is less
than 2.0 m/s. (a) Assuming a perfectly linear alignment of your ship’s velo- city vector with the freight ship (which is stationary with respect to Alpha)
and Alpha’s docking port, what must be your ship’s speed (before colliding
with the freight ship) so that the combination of the freight ship and your ship
arrives at Alpha’s docking port with a speed of 1.50 m/s? (b) How does the velocity of Spaceport Alpha change when the combination of your vessel and
the freight ship successfully docks with it? (c) Suppose you made a mistake while maneuvering your vessel in an attempt to ram the freight ship and, rather
than latching on to it and making a perfectly inelastic collision, you strike it and
knock it in the direction of the spaceport with a perfectly elastic collision. What
is the speed of the freight ship in that case (assuming your ship had the same
initial velocity as that calculated in part (a))?
70. M Spaceship Malfunction. You and your team get a distress call from another ship indicating that there has been an explosion and their propulsion
and navigation systems are now off line. A large piece of their ship has been
jettisoned into space, and their life support systems are failing. They need
help as soon as possible. You try to track them, but are only able to pick up
the piece of the craft that had been projected away from them in the explosion.
You look up the make and model of their ship, a Galaxy Explorer 5000 (GE
5000), which has a total mass of 55000 kg. The piece heading in your direc-
tion is the ship’s storage module, and has a mass of 7500 kg. The GE 5000
was at rest with respect to your ship at the time of the explosion. (a) Assuming you received the distress call 20 minutes before the jettisoned storage module
passed by your ship at a speed of 750.0 m/s, what is the speed of the damaged
craft? (b) How far away is the Galaxy Explorer 5000 when its storage module passes by? (c) In which direction, and how fast must you go, in order to catch up with the GE 5000 before its life support systems fail. (The crew had
80 minutes of life support left when they made the distress call, so you have
60 minutes to get to them.)
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
8.1 Define angular displacement.
8.2 Define angular velocity and angular acceleration.
8.3 Solve rotational kinematics problems.
8.4 Relate angular and tangential variables.
8.5 Distinguish between centripetal and tangential accelerations.
8.6 Analyze rolling motion.
8.7 Use the right-hand rule to determine the direction of angular vectors.
M ik
h ai
l S
ta ro
d u b o v /S
h u tt
er st
o ck
CHAPTER 8
Rotational Kinematics
The fi gure shows the front view of a turbine jet engine on a commercial aircraft. The rotating fan blades
collect air into the engine before it is compressed, mixed with fuel, and ignited to produce thrust. The
rotational motion of the blades can be described using the concepts of angular displacement, angular
velocity, and angular acceleration within the framework of rotational kinematics.
8.1 Rotational Motion and Angular Displacement In the simplest kind of rotation, points on a rigid object move on circular paths. In
Figure 8.1, for example, we see the circular paths for points A, B, and C on a spinning skater. The centers of all such circular paths defi ne a line, called the axis of rotation.
The angle through which a rigid object rotates about a fi xed axis is called the
angular displacement. Figure 8.2 shows how the angular displacement is measured for a rotating compact disc (CD). Here, the axis of rotation passes through the center
of the disc and is perpendicular to its surface. On the surface of the CD we draw a
radial line, which is a line that intersects the axis of rotation perpendicularly. As the
CD turns, we observe the angle through which this line moves relative to a convenient
reference line that does not rotate. The radial line moves from its initial orientation at
angle 𝜃0 to a fi nal orientation at angle 𝜃 (Greek letter theta). In the process, the line
sweeps out the angle 𝜃 ‒ 𝜃0. As with other diff erences that we have encountered (Δx = x ‒ x0, Δυ = υ ‒ υ0, Δt = t ‒ t0), it is customary to denote the diff erence between the fi nal and initial angles by the notation Δ𝜃 (read as “delta theta”): Δ𝜃 = 𝜃 ‒ 𝜃0. The
angle Δ𝜃 is the angular displacement. A rotating object may rotate either counterclock-
wise or clockwise, and standard convention calls a counterclockwise displacement
positive and a clockwise displacement negative.
200
8.1 Rotational Motion and Angular Displacement 201
DEFINITION OF ANGULAR DISPLACEMENT When a rigid body rotates about a fi xed axis, the angular displacement is the angle Δ𝜽 swept out by a line passing through any point on the body and intersecting the axis of rotation perpendicularly. By convention, the angular displacement is positive if it is counterclockwise and negative if it is clockwise. SI Unit of Angular Displacement: radian (rad)*
Angular displacement is often expressed in one of three units. The fi rst is the familiar
degree, and it is well known that there are 360 degrees in a circle. The second unit is the revolution (rev), one revolution representing one complete turn of 360°. The most useful unit from a scientifi c viewpoint, however, is the SI unit called the radian (rad). Figure 8.3 shows how the radian is defi ned, again using a CD as an example. The picture focuses attention on
a point P on the disc. This point starts out on the stationary reference line, so that 𝜃0 = 0 rad, and the angular displacement is Δ𝜃 = 𝜃 ‒ 𝜃0 = 𝜃. As the disc rotates, the point traces out an
arc of length s, which is measured along a circle of radius r. Equation 8.1 defi nes the angle 𝜃 in radians:
θ(in radians) = Arc length
Radius =
s r (8.1)
According to this defi nition, an angle in radians is the ratio of two lengths; for example, meters/
meters. In calculations, therefore, the radian is treated as a number without units and has no eff ect
on other units that it multiplies or divides.
To convert between degrees and radians, it is only necessary to remember that the arc length
of an entire circle of radius r is the circumference 2𝜋r. Therefore, according to Equation 8.1, the number of radians that corresponds to 360°, or one revolution, is
θ = 2πr
r = 2π rad
Since 2𝜋 rad corresponds to 360°, the number of degrees in one radian is
1 rad = 360°
2π = 57.3°
It is useful to express an angle 𝜃 in radians, because then the arc length s subtended at any radius r can be calculated by multiplying 𝜃 by r. Example 1 illustrates this point and also shows how to convert between degrees and radians.
A
B
C
Axis of rotation
FIGURE 8.1 When a rigid object rotates, points on the object, such as A, B, or C, move on circular paths. The centers of the circles
form a line that is the axis of rotation.
*The radian is neither a base SI unit nor a derived one. It is regarded as a supplementary SI unit.
0
Reference line
Radial line
Axis of rotation
θ θ
θ Δ
FIGURE 8.2 The angular displace- ment of a CD is the angle Δ𝜃 swept
out by a radial line as the disc turns
about its axis of rotation.
P s
r Reference line
θ
FIGURE 8.3 In radian measure, the angle 𝜃 is defi ned to be the arc length s divided by the radius r.
202 CHAPTER 8 Rotational Kinematics
Conceptual Example 2 takes advantage of the radian as a unit for measuring angles and
explains the spectacular phenomenon of a total solar eclipse.
r
s
θ
FIGURE 8.4 Two adjacent synchronous satellites have an
angular separation of 𝜃 = 2.00°.
The distances and angles have
been exaggerated for clarity.
EXAMPLE 1 The Physics of Synchronous Communications Satellites
Synchronous or “stationary” communications satellites are put into an or-
bit whose radius is r = 4.23 × 107 m. The orbit is in the plane of the equa- tor, and two adjacent satellites have an angular separation of 𝜃 = 2.00°, as
Figure 8.4 illustrates. Find the arc length s (see the drawing) that separates the satellites.
Reasoning Since the radius r and the angle 𝜃 are known, we may fi nd the arc length s by using the relation 𝜃 (in radians) = s/r. But fi rst, the angle must be converted to radians from degrees.
Solution To convert 2.00° into radians, we use the fact that 2𝜋 radians is equivalent to 360°:
2.00° = (2.00 degrees)( 2π radians360 degrees) = 0.0349 radians From Equation 8.1, it follows that the arc length between the satellites is
s = rθ = (4.23 × 10 7 m)(0.0349 rad) = 1.48 × 10 6 m (920 miles)
The radian, being a unitless quantity, is dropped from the fi nal result,
leaving the answer expressed in meters.
INTERACTIVE FIGURE 8.5 (a) The angles subtended by the moon and sun at the eyes of the observer are 𝜃moon and 𝜃sun. (The distances and angles are exaggerated for the sake of clarity.) (b) Since the moon and sun subtend approximately the same angle, the moon blocks nearly all the sun’s light from reaching
the observer’s eyes. (c) The result is a total solar eclipse.
(a)
(b)
rmoon rsun
ssun smoon
moon
sun
θ
θ
B ab
ak T
af re
sh i/
S ci
en ce
S o u rc
e
(c)
CONCEPTUAL EXAMPLE 2 The Physics of a Total Solar Eclipse
The diameter of the sun is about 400 times greater than that of the
moon. By coincidence, the sun is also about 400 times farther from the
earth than is the moon. For an observer on earth, compare the angles
subtended by the sun and the moon. (a) The angle subtended by the sun is much greater than that subtended by the moon. (b) The angle subtended by the sun is much smaller than that subtended by the moon.
(c) The angles subtended by the sun and the moon are approximately equal.
Reasoning Equation 8.1 (𝜃 = s/r), which is the defi nition of an angle in radians, will guide us. The distance r between either the sun and the earth or the moon and the earth is great enough that the arc length s is very nearly equal to the diameter of the sun or the moon.
Answers (a) and (b) are incorrect. Interactive Figure 8.5a shows a person on earth viewing the sun and the moon. For the diameters s of the sun and the moon, we know that ssun ≈ 400 smoon (where the symbol ≈
8.2 Angular Velocity and Angular Acceleration 203
Check Your Understanding
(The answers are given at the end of the book.) 1. In CYU Figure 8.1, the fl at triangular sheet ABC is lying in the plane
of the paper. This sheet is going to rotate about fi rst one axis and then
another axis. Both of these axes lie in the plane of the paper and pass
through point A. For each of the axes the points B and C move on sepa- rate circular paths that have the same radii. Identify these two axes.
2. Three objects are visible in the night sky. They have the following diameters (in multiples of d) and subtend the following angles (in multiples of 𝜃0) at the eye of the observer. Object A has a diameter of
4d and subtends an angle of 2𝜃0. Object B has a diameter of 3d and subtends an angle of 𝜃0/2. Object C has a diameter of d/2 and subtends an angle of 𝜃0/8. Rank them in descending order (greatest fi rst) according to their distance from the observer.
8.2 Angular Velocity and Angular Acceleration
Angular Velocity In Section 2.2 we introduced the idea of linear velocity to describe how fast an object moves and
the direction of its motion. The average linear velocity v→ was defi ned as the linear displacement Δx→ of the object divided by the time Δt required for the displacement to occur, or v→ = ∆x→/∆t (see Equation 2.2). We now introduce the analogous idea of angular velocity to describe the
motion of a rigid object rotating about a fi xed axis. The average angular velocity ω (Greek letter omega) is defi ned as the angular displacement Δ𝜃 = 𝜃 ‒ 𝜃0 divided by the elapsed time Δt during which the displacement occurs.
DEFINITION OF AVERAGE ANGULAR VELOCITY
= Angular displacement
Elapsed time
ω = θ − θ0 t − t0
= ∆θ ∆t
(8.2)
SI Unit of Angular Velocity: radian per second (rad/s)
The SI unit for angular velocity is the radian per second (rad/s), although other units such as revo-
lutions per minute (rev/min or rpm) are also used. In agreement with the sign convention adopted
for angular displacement, angular velocity is positive when the rotation is counterclockwise and
negative when it is clockwise. Example 3 shows how the concept of average angular velocity is
applied to a gymnast.
C
A
B
CYU FIGURE 8.1
Average angular
velocity
θsun = ssun rsun
≈ 400 smoon 400 rmoon
= θmoon
Interactive Figure 8.5b shows what happens when the moon comes between the sun and the earth. Since the angles subtended by the sun and
the moon are nearly equal, the moon blocks most of the sun’s light from
reaching the observer’s eyes, and a total solar eclipse like that in Interactive Figure 8.5c occurs. Related Homework: Problems 8, 18
means “approximately equal to”). For the distances r between the sun and the earth or the moon and the earth, we know that rsun ≈ 400 rmoon. Because of these facts, the ratio s/r is approximately the same for the sun and for the moon. Therefore, the subtended angle (𝜃 = s/r) is approximately the same for the sun and the moon.
Answer (c) is correct. Applying Equation 8.1 to the case of the sun and the moon gives θsun = ssun /rsun and θmoon = smoon /rmoon. We know, however, that ssun ≈ 400 smoon and rsun ≈ 400 rmoon. Substitution into the expression for 𝜃sun gives
204 CHAPTER 8 Rotational Kinematics
The instantaneous angular velocity 𝜔 is the angular velocity that exists at any given instant. To measure it, we follow the same procedure used in Chapter 2 for the instantaneous
linear velocity. In this procedure, a small angular displacement Δ𝜃 occurs during a small
time interval Δt. The time interval is so small that it approaches zero (∆t → 0), and in this limit, the measured average angular velocity, ω = ∆θ/∆t, becomes the instantaneous angular velocity 𝜔:
ω = lim ∆ t → 0
ω = lim ∆ t → 0
∆θ ∆t
(8.3)
The magnitude of the instantaneous angular velocity, without reference to whether it is a positive
or negative quantity, is called the instantaneous angular speed. If a rotating object has a con- stant angular velocity, the instantaneous value and the average value are the same.
Angular Acceleration In linear motion, a changing velocity means that an acceleration is occurring. Such is also the case
in rotational motion; a changing angular velocity means that an angular acceleration is occur- ring. There are many examples of angular acceleration. For instance, as a compact disc recording
is played, the disc turns with an angular velocity that is continually decreasing. And when the
push buttons of an electric blender are changed from a lower setting to a higher setting, the angu-
lar velocity of the blades increases. We will defi ne the average angular acceleration in a fashion
analogous to that used for the average linear acceleration. Recall that the average linear accelera-
tion a→ is equal to the change Δv→ in the linear velocity of an object divided by the elapsed time Δt: a→ = ∆v→/∆t (Equation 2.4). When the angular velocity changes from an initial value of 𝜔0 at time t0 to a fi nal value of 𝜔 at time t, the average angular acceleration α (Greek letter alpha) is defi ned similarly:
DEFINITION OF AVERAGE ANGULAR ACCELERATION
Average angular acceleration = Change in angular velocity
Elapsed time
α = ω − ω0 t − t0
= ∆ω ∆t
(8.4)
SI Unit of Average Angular Acceleration: radian per second squared (rad/s2)
EXAMPLE 3 Gymnast on a High Bar
A gymnast on a high bar swings through two revolutions in a time of 1.90 s,
as Figure 8.6 suggests. Find the average angular velocity (in rad/s) of the gymnast.
Reasoning The average angular velocity of the gymnast in rad/s is the angular displacement in radians divided by the elapsed time. However,
the angular displacement is given as two revolutions, so we begin by con-
verting this value into radian measure.
Solution The angular displacement (in radians) of the gymnast is
∆θ = −2.00 revolutions ( 2π radians1 revolution) = −12.6 radians where the minus sign denotes that the gymnast rotates clockwise (see the
drawing). The average angular velocity is
ω = ∆θ ∆t
= −12.6 rad
1.90 s = −6.63 rad/s (8.2)
FIGURE 8.6 Swinging on a high bar.
8.3 The Equations of Rotational Kinematics 205
The SI unit for average angular acceleration is the unit for angular velocity divided by the unit
for time, or (rad/s)/s = rad/s2. An angular acceleration of +5 rad/s2, for example, means that the
angular velocity of the rotating object increases by +5 radians per second during each second of
acceleration.
The instantaneous angular acceleration 𝛼 is the angular acceleration at a given instant. In discussing linear motion, we assumed a condition of constant acceleration, so that the average
and instantaneous accelerations were identical (a→ = a→ ). Similarly, we assume that the angular acceleration is constant, so that the instantaneous angular acceleration 𝛼 and the average angu- lar acceleration α are the same (α = α). The next example illustrates the concept of angular acceleration.
EXAMPLE 4 A Jet Revving Its Engines
A jet awaiting clearance for takeoff is momentarily stopped on the runway.
As seen from the front of one engine, the fan blades are rotating with
an angular velocity of ‒110 rad/s, where the negative sign indicates a
clockwise rotation (see Figure 8.7). As the plane takes off , the angular velocity of the blades reaches ‒330 rad/s in a time of 14 s. Find the angular
acceleration, assuming it to be constant.
Reasoning Since the angular acceleration is constant, it is equal to the average angular acceleration. The average acceleration is the change in
the angular velocity, 𝜔 ‒ 𝜔0, divided by the elapsed time, t ‒ t0.
Solution Applying the defi nition of average angular acceleration given in Equation 8.4, we fi nd that
α = ω − ω0 t − t0
= (−330 rad/s) − (−110 rad/s)
14 s = −16 rad/s2
ω
FIGURE 8.7 The fan blades of a jet engine have an angular velocity 𝜔 in a clockwise direction.
Thus, the magnitude of the angular velocity increases by 16 rad/s during
each second that the blades are accelerating. The negative sign in the
answer indicates that the direction of the angular acceleration is also in
the clockwise direction.
Check Your Understanding
(The answers are given at the end of the book.) 3. A pair of scissors is being used to cut a piece of paper in half. Does each blade of the scissors have the
same angular velocity (both magnitude and direction) at a given instant?
4. An electric clock is hanging on a wall. As you are watching the second hand rotate, the clock’s battery stops functioning, and the second hand comes to a halt over a brief period of time. Which one of the
following statements correctly describes the angular velocity 𝜔 and angular acceleration 𝛼 of the second hand as it slows down? (a) 𝜔 and 𝛼 are both negative. (b) 𝜔 is positive and 𝛼 is negative. (c) 𝜔 is negative and 𝛼 is positive. (d) 𝜔 and 𝛼 are both positive.
8.3 The Equations of Rotational Kinematics In Chapters 2 and 3 the concepts of displacement, velocity, and acceleration were introduced. We
then combined these concepts and developed a set of equations called the equations of kinemat-
ics for constant acceleration (see Tables 2.1 and 3.1). These equations are a great aid in solving
problems involving linear motion in one and two dimensions.
We now take a similar approach for rotational motion by bringing together the ideas of angu-
lar displacement, angular velocity, and angular acceleration to produce a set of equations called
the equations of rotational kinematics for constant angular acceleration. These equations, like
those developed in Chapters 2 and 3 for linear motion, will prove very useful in solving problems
that involve rotational motion.
206 CHAPTER 8 Rotational Kinematics
A complete description of rotational motion requires values for the angular displacement
Δ𝜃, the angular acceleration 𝛼, the fi nal angular velocity 𝜔, the initial angular velocity 𝜔0, and the elapsed time Δt. In Example 4, for instance, only the angular displacement of the fan blades during the 14-s interval is missing. Such missing information can be calculated, however. For
convenience in the calculations, we assume that the orientation of the rotating object is given by
𝜃0 = 0 rad at time t0 = 0 s. Then, the angular displacement becomes Δ𝜃 = 𝜃 ‒ 𝜃0 = 𝜃, and the time interval becomes Δt = t ‒ t0 = t.
In Example 4, the angular velocity of the fan blades changes at a constant rate from an initial
value of 𝜔0 = ‒110 rad/s to a fi nal value of 𝜔 = ‒330 rad/s. Therefore, the average angular veloc- ity is midway between the initial and fi nal values:
ω = 12[(−110 rad/s) + (−330 rad/s)] = −220 rad/s
In other words, when the angular acceleration is constant, the average angular velocity is
given by
ω = 12 (ω0 + ω) (8.5)
With a value for the average angular velocity, Equation 8.2 can be used to obtain the angular
displacement of the fan blades:
θ = ωt = (−220 rad/s)(14 s) = −3100 rad
In general, when the angular acceleration is constant, the angular displacement can be obtained
from
θ = ωt = 12 (ω0 + ω)t (8.6)
This equation and Equation 8.4 provide a complete description of rotational motion under
the condition of constant angular acceleration. Equation 8.4 (with t0 = 0 s) and Equation 8.6 are compared with the analogous results for linear motion in the fi rst two rows of Table 8.1. The purpose of this comparison is to emphasize that the mathematical forms of Equations 8.4
and 2.4 are identical, as are the forms of Equations 8.6 and 2.7. Of course, the symbols used
for the rotational variables are diff erent from those used for the linear variables, as Table 8.2 indicates.
In Chapter 2, Equations 2.4 and 2.7 are used to derive the remaining two equations of kine-
matics (Equations 2.8 and 2.9). These additional equations convey no new information but are
convenient to have when solving problems. Similar derivations can be carried out here. The results
are listed as Equations 8.7 and 8.8 below and in Table 8.1; they can be inferred directly from their counterparts in linear motion by making the substitution of symbols indicated in Table 8.2:
θ = ω0t + 12 αt 2 (8.7)
ω2 = ω02 + 2αθ (8.8)
The four equations in the left column of Table 8.1 are called the equations of rotational kinematics for constant angular acceleration. The following example illustrates that they are used in the same fashion as the equations of linear kinematics.
TABLE 8.1 The Equations of Kinematics for Rotational and Linear Motion
Rotational Motion (α = constant)
Linear Motion (a = constant)
ω = ω0 + αt (8.4) υ = υ0 + at (2.4)
θ = 12 (ω0 + ω)t (8.6) x = 1
2 (υ0 + υ)t (2.7)
θ = ω0t + 1
2αt2 (8.7) x = υ0t + 1
2at2 (2.8)
ω2 = ω02 + 2αθ (8.8) υ2 = υ02 + 2ax (2.9)
TABLE 8.2 Symbols Used in Rotational and Linear Kinematics
Rotational Motion Quantity
Linear Motion
𝜃 Displacement x
𝜔0 Initial velocity υ0
𝜔 Final velocity υ
𝛼 Acceleration a
t Time t
8.3 The Equations of Rotational Kinematics 207
Problem-Solving Insight The equations of rotational kinematics can be used with any self- consistent set of units for 𝜃, 𝛼, 𝜔, 𝜔0, and t. Radians are used in Example 5 only because data are given in terms of radians. Had the data for 𝜃, 𝛼, and 𝜔0 been provided in rev, rev/s
2, and
rev/s, respectively, then Equation 8.8 could have been used to determine the answer for 𝜔
directly in rev/s. In any case, the reasoning strategy for applying the kinematics equations is
summarized as follows.
REASONING STRATEGY Applying the Equations of Rotational Kinematics 1. Make a drawing to represent the situation being studied, showing the direction of
rotation. 2. Decide which direction of rotation is to be called positive (+) and which direction is to
be called negative (–). In this text we choose the counterclockwise direction to be positive and the clockwise direction to be negative, but this is arbitrary. However, do not change your decision during the course of a calculation.
3. In an organized way, write down the values (with appropriate + and – signs) that are given for any of the fi ve rotational kinematic variables (𝜽, α, 𝝎, 𝝎0, and t). Be on the alert for implied data, such as the phrase “starts from rest,” which means that the value of the initial angular velocity is 𝝎0 = 0 rad/s. The data table in Example 5 is a good way to keep track of this information. In addition, identify the variable(s) that you are being asked to determine.
4. Before attempting to solve a problem, verify that the given information contains values for at least three of the fi ve kinematic variables. Once the three variables are identifi ed for which values are known, the appropriate relation from Table 8.1 can be selected.
5. When the rotational motion is divided into segments, the fi nal angular velocity of one segment is the initial angular velocity for the next segment.
6. Keep in mind that there may be two possible answers to a kinematics problem. Try to visualize the diff erent physical situations to which the answers correspond.
EXAMPLE 5 Blending with a Blender
The blades of an electric blender are whirling with an angular velocity of
+375 rad/s while the “puree” button is pushed in, as Figure 8.8 shows. When the “blend” button is pressed, the blades accelerate and reach a
greater angular velocity after the blades have rotated through an angular
displacement of +44.0 rad. The angular acceleration has a constant value
of +1740 rad/s2. Find the fi nal angular velocity of the blades.
Reasoning The three known variables are listed in the table below, along with a question mark indicating that a value for the fi nal angular
velocity 𝜔 is being sought.
𝜽 α 𝜔 𝜔0 t
+44.0 rad +1740 rad/s2 ? +375 rad/s
We can use Equation 8.8, because it relates the angular variables 𝜃, 𝛼, 𝜔, and 𝜔0.
Problem-Solving Insight Each equation of rotational kine- matics contains four of the fi ve kinematic variables, 𝜽, α, 𝝎, 𝝎0, and t. Therefore, it is necessary to have values for three of these variables if one of the equations is to be used to deter- mine a value for an unknown variable.
Axis of rotation
FIGURE 8.8 The angular velocity of the blades in an electric blender changes
each time a diff erent push button is
chosen.
Solution From Equation 8.8 (𝜔2 = 𝜔02 + 2𝛼𝜃) it follows that
ω = +√ω0 2 + 2αθ = +√(375 rad/s) 2 + 2(1740 rad/s2 ) (44.0 rad )
= +542 rad /s
The negative root is disregarded, since the blades do not reverse their
direction of rotation.
208 CHAPTER 8 Rotational Kinematics
Check Your Understanding
(The answers are given at the end of the book.) 5. The blades of a ceiling fan start from rest and, after two revolutions, have an angular speed of
0.50 rev/s. The angular acceleration of the blades is constant. What is the angular speed after eight
revolutions?
6. Equation 8.7 (θ = ω0t + 12 αt 2) is being used to solve a problem in rotational kinematics. Which one of the following sets of values for the variables 𝜔0, 𝛼, and t cannot be substituted directly into this equation to calculate a value for 𝜃? (a) 𝜔0 = 1.0 rad/s, 𝛼 = 1.8 rad/s2, and t = 3.8 s (b) 𝜔0 = 0.16 rev/s, 𝛼 = 1.8 rad/s2, and t = 3.8 s (c) 𝜔0 = 0.16 rev/s, 𝛼 = 0.29 rev/s2, and t = 3.8 s
8.4 Angular Variables and Tangential Variables In the familiar ice-skating stunt known as crack-the-whip, a number of skaters attempt to maintain
a straight line as they skate around the one person (the pivot) who remains in place. Figure 8.9 shows each skater moving on a circular arc and includes the corresponding velocity vector at
the instant portrayed in the picture. For every individual skater, the vector is drawn tangent to
the appropriate circle and, therefore, is called the tangential velocity vT→ . The magnitude of the tangential velocity is referred to as the tangential speed.
THE PHYSICS OF . . . “crack-the-whip.” Of all the skaters involved in the stunt, the one farthest from the pivot has the hardest job. Why? Because, in keeping the line straight, this skater covers more distance than anyone else. To accomplish this, he must skate faster than anyone else and, thus, must have the largest tangential speed. In fact, the line remains straight only if each person skates with the correct tangential speed. The skaters closer to the pivot must move with smaller tangential speeds than those farther out, as indicated by the magnitudes of the tangential velocity vectors in Figure 8.9.
With the aid of Figure 8.10, it is possible to show that the tangential speed of any skater is directly proportional to the skater’s distance r from the pivot, assuming a given angular speed for the rotating line. When the line rotates as a rigid unit for a time t, it sweeps out the angle 𝜃 shown in the drawing. The distance s through which a skater moves along a circular arc can be calculated from s = r𝜃 (Equation 8.1), provided that 𝜃 is measured in radians. Dividing both sides of this equation by t, we fi nd that s/t = r(𝜃/t). The term s/t is the tangential speed υT (e.g., in meters/second) of the skater, while 𝜃/t is the angular speed 𝜔 (in radians/ second) of the line:
υT = rω (ω in rad/s) (8.9)
In this expression, the terms υT and 𝜔 refer to the magnitudes of the tangential and angular veloci- ties, respectively, and are numbers without algebraic signs.
It is important to emphasize that the angular speed 𝜔 in Equation 8.9 must be expressed in radian measure (e.g., in rad/s); no other units, such as revolutions per second, are acceptable. This
restriction arises because the equation was derived by using the defi nition of radian measure,
s = r𝜃. The real challenge for the crack-the-whip skaters is to keep the line straight while making
it pick up angular speed—that is, while giving it an angular acceleration. To make the angular
speed of the line increase, each skater must increase his tangential speed, since the two speeds are
related according to υT = r𝜔. Of course, the fact that a skater must skate faster and faster means that he must accelerate, and his tangential acceleration aT can be related to the angular accelera- tion 𝛼 of the line. If the time is measured relative to t0 = 0 s, the defi nition of linear acceleration is given by Equation 2.4 as aT = (υT ‒ υT0)/t, where υT and υT0 are the fi nal and initial tangential speeds, respectively. Substituting υT = r𝜔 for the tangential speed shows that
aT = υT − υT0
t =
(rω) − (rω0) t
= r ( ω − ω0
t )
Stationary skater
or pivot
vT
FIGURE 8.9 When doing the stunt known as crack-the-whip, each skater along the radial
line moves on a circular arc. The tangential
velocity vT→ of each skater is represented by an arrow that is tangent to each arc.
Stationary skater
or pivot
s
r
θ
FIGURE 8.10 During a time t, the line of skaters sweeps through an angle 𝜃. An
individual skater, located at a distance r from the stationary skater, moves through
a distance s on a circular arc.
8.4 Angular Variables and Tangential Variables 209
Since 𝛼 = (𝜔 ‒ 𝜔0)/t according to Equation 8.4, it follows that
aT = rα (α in rad/s2) (8.10)
This result shows that, for a given value of 𝛼, the tangential acceleration aT is proportional to the radius r, so the skater farthest from the pivot must have the largest tangential acceleration. In this expression, the terms aT and 𝛼 refer to the magnitudes of the numbers involved, without reference to any algebraic sign. Moreover, as is the case for 𝜔 in υT = r𝜔, only radian measure can be used for 𝛼 in Equation 8.10.
There is an advantage to using the angular velocity 𝜔 and the angular acceleration 𝛼 to describe the rotational motion of a rigid object. The advantage is that these angular quantities
describe the motion of the entire object. In contrast, the tangential quantities υT and aT describe only the motion of a single point on the object, and Equations 8.9 and 8.10 indicate that diff er-
ent points located at diff erent distances r have diff erent tangential velocities and accelerations. Example 6 stresses this advantage.
EXAMPLE 6 A Helicopter Blade
A helicopter blade has an angular speed of 𝜔 = 6.50 rev/s and has an angular acceleration of 𝛼 = 1.30 rev/s2. For points 1 and 2 on the blade in Figure 8.11, fi nd the magnitudes of (a) the tangential speeds and (b) the tangential accelerations.
Reasoning Since the radius r for each point and the angular speed 𝜔 of the helicopter blade are known, we can fi nd the tangential speed υT for each point by using the relation υT = r𝜔. However, since this equation can be used only with radian measure, the angular speed 𝜔 must be converted to rad/s from rev/s. In a similar manner, the tangential acceleration aT for points 1 and 2 can be found using aT = r𝛼, provided the angular accelera- tion 𝛼 is expressed in rad/s2 rather than in rev/s2.
Problem-Solving Insight When using Equations 8.9 and 8.10 to relate tangential and angular quantities, remember that the angular quantity is always expressed in radian mea- sure. These equations are not valid if angles are expressed in degrees or revolutions.
Solution (a) Converting the angular speed 𝜔 to rad/s from rev/s, we obtain
ω = (6.50 revs ) ( 2π rad 1 rev ) = 40.8
rad
s
The tangential speed for each point is
Point 1 υT = rω = (3.00 m)(40.8 rad/s) = 122 m/s (273 mph) (8.9)
Point 2 υT = rω = (6.70 m)(40.8 rad/s) = 273 m/s (611 mph) (8.9)
2 3.00 m
6.70 m 1
FIGURE 8.11 Points 1 and 2 on the rotating blade of the helicopter have the
same angular speed and acceleration,
but they have diff erent tangential speeds and accelerations.
The rad unit, being dimensionless, does not appear in the fi nal answers.
(b) Converting the angular acceleration 𝛼 to rad/s2 from rev/s2, we fi nd
α = (1.30 revs2 ) ( 2π rad 1 rev ) = 8.17
rad
s2
The tangential accelerations can now be determined:
Point 1 aT = rα = (3.00 m)(8.17 rad/s2) = 24.5 m/s2 (8.10)
Point 2 aT = rα = (6.70 m)(8.17 rad/s2) = 54.7 m/s2 (8.10)
Check Your Understanding
(The answers are given at the end of the book.) 7. A thin rod rotates at a constant angular speed. In case A the axis of rotation is perpendicular to the rod
at its center. In case B the axis is perpendicular to the rod at one end. In which case, if either, are there
points on the rod that have the same tangential speeds?
8. It is possible to build a clock in which the tips of the hour hand and the second hand move with the same tangential speed. This is normally never done, however. Why? (a) The length of the hour hand would be 3600 times greater than the length of the second hand. (b) The hour hand and the second hand would
(Continued)
210 CHAPTER 8 Rotational Kinematics
have the same length. (c) The length of the hour hand would be 3600 times smaller than the length of the second hand.
9. The earth rotates once per day about its axis, which is perpendicular to the plane of the equator and passes through the north geographic pole. Where on the earth’s surface should you stand in order to
have the smallest possible tangential speed?
10. A building is located on the earth’s equator. As the earth rotates about its axis, which fl oor of the build- ing has the greatest tangential speed? (a) The fi rst fl oor (b) The tenth fl oor (c) The twentieth fl oor
11. The blade of a lawn mower is rotating at an angular speed of 17 rev/s. The tangential speed of the outer edge of the blade is 32 m/s. What is the radius of the blade?
8.5 Centripetal Acceleration and Tangential Acceleration When an object picks up speed as it moves around a circle, it has a tangential acceleration, as
discussed in the previous section. In addition, the object also has a centripetal acceleration, as
emphasized in Chapter 5. That chapter deals with uniform circular motion, in which a particle moves at a constant tangential speed on a circular path. The tangential speed υT is the magnitude of the tangential velocity vector. Even when the magnitude of the tangential velocity is constant,
an acceleration is present, since the direction of the velocity changes continually. Because the
resulting acceleration points toward the center of the circle, it is called the centripetal accelera-
tion. Interactive Figure 8.12a shows the centripetal acceleration ac→ for a model airplane fl ying in uniform circular motion on a guide wire. The magnitude of ac→ is
ac = υT2
r (5.2)
The subscript “T” has now been included in this equation as a reminder that it is the tangential
speed that appears in the numerator.
The centripetal acceleration can be expressed in terms of the angular speed 𝜔 by using υT = r𝜔 (Equation 8.9):
ac = υT2
r = (rω)2
r = rω 2 (ω in rad/s) (8.11)
Only radian measure (rad/s) can be used for 𝜔 in this result, since the relation υT = r𝜔 presumes radian measure.
While considering uniform circular motion in Chapter 5, we ignored the details of how the
motion is established in the fi rst place. In Interactive Figure 8.12b, for instance, the engine of the plane produces a thrust in the tangential direction, and this force leads to a tangential accel-
eration. In response, the tangential speed of the plane increases from moment to moment, until
the situation shown in the drawing results. While the tangential speed is changing, the motion is
called nonuniform circular motion. Interactive Figure 8.12b illustrates an important feature of nonuniform circular motion.
Since the direction and the magnitude of the tangential velocity are both changing, the airplane
experiences two acceleration components simultaneously. The changing direction means that
there is a centripetal acceleration ac→ . The magnitude of ac→ at any moment can be calculated using the value of the instantaneous angular speed and the radius: ac = r𝜔2. The fact that the magnitude of the tangential velocity is changing means that there is also a tangential accelera-
tion aT→ . The magnitude of aT→ can be determined from the angular acceleration 𝛼 according to aT = r𝛼, as the previous section explains. If the magnitude FT of the net tangential force and the mass m are known, aT also can be calculated using Newton’s second law, FT = maT. Interactive Figure 8.12b shows the two acceleration components. The total acceleration is given by the vector sum of ac→ and aT→ . Since ac→ and aT→ are perpendicular, the magnitude of the total accelera- tion a→ can be obtained from the Pythagorean theorem as a = √ac2 + aT2, while the angle 𝜙 in the drawing can be determined from tan 𝜙 = aT/ac. The next example applies these concepts to a discus thrower.
a aT
ac
r
r
(a) Uniform circular motion
(b) Nonuniform circular motion
ac
ϕ
INTERACTIVE FIGURE 8.12 (a) If a model airplane fl ying on a guide wire has a constant
tangential speed, the motion is uniform cir-
cular motion, and the plane experiences only
a centripetal acceleration ac→ . (b) Nonuniform circular motion occurs when the tangential
speed changes. Then there is a tangential
acceleration aT→ in addition to the centripetal acceleration.
8.5 Centripetal Acceleration and Tangential Acceleration 211
Analyzing Multiple-Concept Problems
EXAMPLE 7 A Discus Thrower
Discus throwers often warm up by throwing the discus with a twisting
motion of their bodies. Figure 8.13a illustrates a top view of such a warm-up throw. Starting from rest, the thrower accelerates the discus to a
fi nal angular velocity of +15.0 rad/s in a time of 0.270 s before releasing
it. During the acceleration, the discus moves on a circular arc of radius
0.810 m. Find the magnitude a of the total acceleration of the discus just before the discus is released.
Reasoning Since the tangential speed of the discus increases as the thrower turns, the discus simultaneously experiences a tangential accel-
eration aT→ and a centripetal acceleration ac→ that are oriented at right angles to each other (see the drawing). The magnitude a of the total acceleration is a = √ac2 + a T2, where ac and aT are the magnitudes of the centripetal and tangential accelerations. The magnitude of the cen-
tripetal acceleration can be evaluated from Equation 8.11 (ac = r𝜔2), and the magnitude of the tangential acceleration follows from Equation 8.10
(aT = r𝛼). The angular acceleration 𝛼 can be found from its defi nition in Equation 8.4.
Knowns and Unknowns The data for this problem are:
(a)
(b)
ac aT
ac aT
aϕ
FIGURE 8.13 (a) A discus thrower and the centripetal
acceleration ac→ and tangential acceleration aT→ of the discus. (b) The total acceleration a→ of the discus just before the discus
is released is the vector sum of
ac→ and aT→ .
Description Symbol Value Comment Explicit Data Final angular velocity 𝜔 +15.0 rad/s Positive, because discus moves counterclockwise (see drawing).
Time t 0.270 s
Radius of circular arc r 0.810 m
Implicit Data Initial angular velocity 𝜔0 0 rad/s Discus starts from rest.
Unknown Variable Magnitude of total acceleration a ?
Modeling the Problem
STEP 1 Total Acceleration Figure 8.13b shows the two perpendicular components of the ac- celeration of the discus at the moment of release. The centripetal acceleration ac→ arises because the discus is traveling on a circular path; this acceleration always points toward the center of the
circle (see Section 5.2). The tangential acceleration aT→ arises because the tangential velocity of the discus is increasing; this acceleration is tangent to the circle (see Section 8.4). Since ac→ and aT→ are perpendicular, we can use the Pythagorean theorem to fi nd the magnitude a of the total acceleration, as given by Equation 1 at the right. Values for ac and aT will be obtained in the next two steps.
STEP 2 Centripetal Acceleration The magnitude ac of the centripetal acceleration can be evaluated from Equation 8.11 as
ac = rω2
where r is the radius and 𝜔 is the angular speed of the discus. Both r and 𝜔 are known, so we can substitute this expression for ac into Equation 1, as indicated at the right. In Step 3, we will evaluate the magnitude aT of the tangential acceleration.
??
a = √ac2 + aT2 (1)
?
a = √ac2 + aT2 (1)
ac = rω2
212 CHAPTER 8 Rotational Kinematics
STEP 3 Tangential Acceleration According to Equation 8.10, the magnitude aT of the tan- gential acceleration is aT = r𝛼, where r is the radius of the path and 𝛼 is the magnitude of the angular acceleration. The angular acceleration is defi ned (see Equation 8.4) as the change 𝜔 – 𝜔0 in the angular velocity divided by the time t, or 𝛼 = (𝜔 – 𝜔0)/t. Thus, the tangential acceleration can be written as
aT = rα = r( ω − ω0
t ) All the variables on the right side of this equation are known, so we can substitute this expression
for aT into Equation 1 (see the right column).
Solution Algebraically combining the results of the three steps, we have:
a = √a 2c + a 2T = √r 2ω4 + α 2T = √r 2ω4 + r 2 ( ω − ω0
t ) 2
The magnitude of the total acceleration of the discus is
a = √r 2ω4 + r 2 ( ω − ω0
t ) 2
= √(0.810 m)2 (15.0 rad/s)4 + (0.810 m) 2 (15.0 rad/s − 0 rad/s0.270 s ) 2
= 188 m/s2
Note that we can also determine the angle 𝜙 between the total acceleration of the discus and its centripetal acceleration (see Figure 8.13b). From trigonometry, we have that tan 𝜙 = aT/ac, so
ϕ = tan−1 ( aT ac ) = tan−1[r (
ω − ω0 t )
rω2 ] = tan‒1[(
15.0 rad/s − 0 rad/s
0.270 s ) (15.0 rad/s)2
] = 13.9°
STEP 1 STEP 2 STEP 3
Math Skills Tan 𝜙 is the tangent function and is defi ned as tan 𝜙 = ho ha
(Equation 1.3).
As shown in Figure 8.14a, ho is the length of the side of a right triangle opposite the angle 𝜙, and ha is the length of the side adjacent to the angle 𝜙. As always, the fi rst step in applying such a trigonometric function is to identify this angle and its associated
right triangle. Figure 8.13b establishes the angle 𝜙 and is reproduced in Figure 8.14b. A comparison of the shaded right triangles in the drawing reveals that ho = aT and ha = ac.
Thus, it follows that tan ϕ = ho ha
= a T ac
, and 𝜙 is the angle whose tangent is aT ac
. This result
can be expressed by using the inverse tangent function (tan−1):
ϕ = tan−1( a T ac )
Related Homework: Problems 48, 50, 68
a = √ac2 + aT2 (1)
ac = rω2 aT = r( ω − ω0
t )
(b)(a)
90°
ha ac
a
aT
ho ϕ ϕ
FIGURE 8.14 Math Skills drawing.
8.6 Rolling Motion 213
Check Your Understanding
(The answers are given at the end of the book.) 12. A car is up on a hydraulic lift at a garage. The wheels are free to rotate, and the drive wheels are rotating
with a constant angular velocity. Which one of the following statements is true? (a) A point on the rim has no tangential and no centripetal acceleration. (b) A point on the rim has both a nonzero tangential acceleration and a nonzero centripetal acceleration. (c) A point on the rim has a nonzero tangential ac- celeration but no centripetal acceleration. (d) A point on the rim has no tangential acceleration but does have a nonzero centripetal acceleration.
13. Section 5.6 discusses how the uniform circular motion of a space station can be used to create artifi cial gravity. This can be done by adjusting the angular speed of the space station, so the centripetal accel-
eration at an astronaut’s feet equals g, the magnitude of the acceleration due to the earth’s gravity (see Figure 5.18). If such an adjustment is made, will the acceleration at the astronaut’s head due to the artifi cial gravity be (a) greater than, (b) equal to, or (c) less than g?
14. A bicycle is turned upside down, the front wheel is spinning (see CYU Figure 8.2), and there is an angular acceleration. At the instant shown, there are six points on the wheel that have arrows associated
with them. Which one of the following quantities could the arrows
not represent? (a) Tangential velocity (b) Centripetal acceleration (c) Tangential acceleration
15. A rotating object starts from rest and has a constant angular accel- eration. Three seconds later the centripetal acceleration of a point
on the object has a magnitude of 2.0 m/s2. What is the magnitude of
the centripetal acceleration of this point six seconds after the motion
begins?
8.6 Rolling Motion Rolling motion is a familiar situation that involves rotation, as Figure 8.15 illustrates for the case of an automobile tire. The essence of rolling motion is that there is no slipping at the point of contact where the tire touches the ground. To a good approximation, the tires on a normally
moving automobile roll and do not slip. In contrast, the squealing tires that accompany the start
of a drag race are rotating, but they are not rolling while they rapidly spin and slip against the
ground.
When the tires in Figure 8.15 roll, there is a relationship between the angular speed at which the tires rotate and the linear speed (assumed constant) at which the car moves forward. In part b of the drawing, consider the points labeled A and B on the left tire. Between these points we apply a coat of red paint to the tread of the tire; the length of this circular arc of paint is s. The tire then rolls to the right until point B comes in contact with the ground. As the tire rolls, all the paint comes off the tire and sticks to the ground, leaving behind the horizontal red line shown in the
drawing. The axle of the wheel moves through a linear distance d, which is equal to the length of the horizontal strip of paint. Since the tire does not slip, the distance d must be equal to the circular arc length s, measured along the outer edge of the tire: d = s. Dividing both sides of this equation by the elapsed time t shows that d/t = s/t. The term d/t is the speed at which the axle moves parallel to the ground—namely, the linear speed υ of the car. The term s/t is the tangential speed υT at which a point on the outer edge of the tire moves relative to the axle. In addition, υT is related to the angular speed 𝜔 about the axle according to υT = r𝜔 (Equation 8.9). Therefore, it follows that
υ = υT = rω (ω in rad/s) (8.12)
If the car in Figure 8.15 has a linear acceleration a→ parallel to the ground, a point on the tire’s outer edge experiences a tangential acceleration aT→ relative to the axle. The same kind of reasoning as that used in the previous paragraph reveals that the magnitudes of these accelerations
CYU FIGURE 8.2
⏟ Linear
speed
⏟⎵⏟⎵⏟ Tangential
speed
Linear velocity, v
AB
s r
BA d = s
(a)
(b)
FIGURE 8.15 (a) An automobile moves with a linear speed υ. (b) If the tires roll and do not slip, the distance d through which an axle moves equals the circular arc length s along the outer edge of a tire.
214 CHAPTER 8 Rotational Kinematics
are the same and that they are related to the angular acceleration 𝛼 of the wheel relative to the axle:
a = aT = rα (α in rad/s2) (8.13)
Equations 8.12 and 8.13 may be applied to any rolling motion, because the object does not slip
against the surface on which it is rolling.
Check Your Understanding
(The answers are given at the end of the book.) 16. The speedometer of a truck is set to read the linear speed of the truck, but uses a device that actually
measures the angular speed of the rolling tires that came with the truck. However, the owner replaces
the tires with larger-diameter versions. Does the reading on the speedometer after the replacement give
a speed that is (a) less than, (b) equal to, or (c) greater than the true linear speed of the truck? 17. Rolling motion is an example that involves rotation about an axis that is not fi xed. Give three other
examples of rotational motion about an axis that is not fi xed.
8.7 *The Vector Nature of Angular Variables We have presented angular velocity and angular acceleration by taking advantage of the analogy
between angular variables and linear variables. Like the linear velocity and the linear accelera-
tion, the angular quantities are also vectors and have a direction as well as a magnitude. As yet,
however, we have not discussed the directions of these vectors.
When a rigid object rotates about a fi xed axis, it is the axis that identifi es the motion, and the
angular velocity vector points along this axis. Interactive Figure 8.16 shows how to determine the direction using a right-hand rule:
Right-Hand Rule Grasp the axis of rotation with your right hand, so that your fi ngers circle the axis in the same sense as the rotation. Your extended thumb points along the axis
in the direction of the angular velocity vector.
No part of the rotating object moves in the direction of the angular velocity vector.
Angular acceleration arises when the angular velocity changes, and the acceleration vector
also points along the axis of rotation. The acceleration vector has the same direction as the change in the angular velocity. That is, when the magnitude of the angular velocity (which is the angular
speed) is increasing, the angular acceleration vector points in the same direction as the angular
velocity. Conversely, when the magnitude of the angular velocity is decreasing, the angular accelera-
tion vector points in the direction opposite to the angular velocity.
⏟ Linear
acceleration
⏟⎵⏟⎵⏟ Tangential
acceleration
Right hand
Right hand
𝛚
𝛚
INTERACTIVE FIGURE 8.16 The angular velocity vector ω→ of a rotating object points along the axis of rotation. The direction along
the axis depends on the sense of the rotation
and can be determined with the aid of a right-
hand rule (see the text).
EXAMPLE 8 BIO The Physics of a Centrifuge
One popular piece of equipment in research laboratories is a centrifuge
(Figure 8.17a). Typical applications of a centrifuge include separating immiscible liquids or suspended solids like blood, for example. Samples
are placed in tubes (Figure 8.17b) and then rotated at high speeds around a fi xed axis. The centripetal acceleration causes the denser substances
and particles to separate and settle at the bottom of the tubes. Suppose
a centrifuge starts from rest and reaches its maximum angular speed of
4510 rpm in 12.2 s. Through how many revolutions does the centrifuge
spin during this time?
Reasoning This is a standard rotational kinematics problem, with the following known variables:
𝜽 α 𝜔 𝜔0 t
? +4510 rpm 0 12.2 s
Given the information in the table, we can simply use Equation 8.6 to
calculate the angular displacement, 𝜃.
Concept Summary 215
Concept Summary 8.1 Rotational Motion and Angular Displacement When a rigid body rotates about a fi xed axis, the angular displacement is the angle swept out
by a line passing through any point on the body and intersecting the axis of
rotation perpendicularly. By convention, the angular displacement is positive
if it is counterclockwise and negative if it is clockwise.
The radian (rad) is the SI unit of angular displacement. The angle 𝜃 in radi-
ans is defi ned in Equation 8.1 as the circular arc of length s traveled by a point on the rotating body divided by the radial distance r of the point from the axis.
θ (in radians) = s r (8.1)
8.2 Angular Velocity and Angular Acceleration The average angular velocity ω is the angular displacement Δ𝜃 divided by the elapsed time Δt, according to Equation 8.2. As Δt approaches zero, the average angular velo- city becomes equal to the instantaneous angular velocity 𝜔. The magnitude of the instantaneous angular velocity is called the instantaneous angular speed.
The average angular acceleration α is the change Δ𝜔 in the angular velocity divided by the elapsed time Δt, according to Equation 8.4. As Δt approaches zero, the average angular acceleration becomes equal to the
instantaneous angular acceleration 𝛼.
ω = ∆θ ∆t
(8.2)
α = ∆ω ∆t
(8.4)
8.3 The Equations of Rotational Kinematics The equations of rotational kinematics apply when a rigid body rotates with a constant angular accelera-
tion about a fi xed axis. These equations relate the angular displacement 𝜃 ‒ 𝜃0,
the angular acceleration 𝛼, the fi nal angular velocity 𝜔, the initial angular velocity 𝜔0, and the elapsed time t ‒ t0. Assuming that 𝜃0 = 0 rad at t0 = 0 s, the equations of rotational kinematics are written as in Equations 8.4 and
8.6–8.8. These equations may be used with any self-consistent set of units
and are not restricted to radian measure.
ω = ω0 + αt (8.4)
θ = 12 (ω + ω0) t (8.6)
θ = ω0 t + 12αt 2 (8.7)
ω2 = ω0 2 + 2αθ (8.8)
8.4 Angular Variables and Tangential Variables When a rigid body rotates through an angle 𝜃 about a fi xed axis, any point on the body moves
on a circular arc of length s and radius r. Such a point has a tangential velo- city (magnitude = υT) and, possibly, a tangential acceleration (magnitude = aT). The angular and tangential variables are related by Equations 8.1, 8.9, and 8.10. These equations refer to the magnitudes of the variables involved,
without reference to positive or negative signs, and only radian measure can
be used when applying them.
s = rθ (θ in rad) (8.1)
υT = rω (ω in rad/s) (8.9)
aT = rα (α in rad/s2) (8.10)
8.5 Centripetal Acceleration and Tangential Acceleration The mag- nitude ac of the centripetal acceleration of a point on an object rotating with uniform or nonuniform circular motion can be expressed in terms of the
radial distance r of the point from the axis and the angular speed 𝜔, as shown in Equation 8.11. This point experiences a total acceleration a→ that is the vector sum of two perpendicular acceleration components, the centripetal
acceleration ac→ and the tangential acceleration aT→ ; a→ = ac→ + aT→ .
ac = rω2 (ω in rad/s) (8.11)
8.6 Rolling Motion The essence of rolling motion is that there is no slip- ping at the point where the object touches the surface upon which it is rolling.
As a result, the tangential speed υT of a point on the outer edge of a rolling object, measured relative to the axis through the center of the object, is equal
to the linear speed υ with which the object moves parallel to the surface. In other words, we have Equation 8.12.
The magnitudes of the tangential acceleration aT and the linear accelera- tion a of a rolling object are similarly related, as in Equation 8.13.
υ = υT = rω (ω in rad/s) (8.12)
a = a T = rα (α in rad/s2) (8.13)
8.7 The Vector Nature of Angular Variables The direction of the angu- lar velocity vector is given by a right-hand rule. Grasp the axis of rotation
with your right hand, so that your fi ngers circle the axis in the same sense
as the rotation. Your extended thumb points along the axis in the direction
of the angular velocity vector. The angular acceleration vector has the same
direction as the change in the angular velocity.
Solution In order to apply Equation 8.6, we need the value of the average angular speed, ω. We can calculate ω using Equation 8.5:
ω = 12(ω0 + ω ) = 1
2(0 + 4510 rpm) = 2260 rpm.
Now we can solve for the angular displacement. However, before we can
apply Equation 8.6, we need to have consistent units. We need to convert
the time given from seconds to minutes:
t = (12.2 s )(1 min60 s ) = 0.203 min. Now we can calculate the angular displacement:
𝜽 = ωt = (2260 rpm)(0.203 min) = 459 revolutions
(a) (b)
FIGURE 8.17 (a) Common laboratory centrifuge. (b) Drawing of a typical sample tube used in the centrifuge. The tubes are rotated at high
speed. The centripetal acceleration separates the materials in the tube by
density, with the more dense particles settling at the bottom of the tube.
sc o tt
h 2 3 /P
ix ab
ay
216 CHAPTER 8 Rotational Kinematics
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 8.1 Rotational Motion and Angular Displacement 1. The moon is 3.85 × 108 m from the earth and has a diameter of 3.48 × 106 m. You have a pea (diameter = 0.50 cm) and a dime (diameter = 1.8 cm).
You close one eye and hold each object at arm’s length (71 cm) between your
open eye and the moon. Which objects, if any, completely cover your view of
the moon? Assume that the moon and both objects are suffi ciently far from
your eye that the given diameters are equal to arc lengths when calculating
angles. (a) Both (b) Neither (c) Pea (d) Dime
Section 8.2 Angular Velocity and Angular Acceleration 3. The radius of the circle traced out by the second hand on a clock is 6.00 cm. In a time t the tip of the second hand moves through an arc length of 24.0 cm. Determine the value of t in seconds. 4. A rotating object has an angular acceleration of 𝛼 = 0 rad/s2. Which one or more of the following three statements is consistent with a zero angular
acceleration? A. The angular velocity is 𝜔 = 0 rad/s at all times. B. The angular velocity is 𝜔 = 10 rad/s at all times. C. The angular displacement 𝜃 has the same value at all times. (a) A, B, and C (b) A and B, but not C (c) A only (d) B only (e) C only
Section 8.3 The Equations of Rotational Kinematics 6. A rotating wheel has a constant angular acceleration. It has an angular velocity of 5.0 rad/s at time t = 0 s, and 3.0 s later has an angular velocity of 9.0 rad/s. What is the angular displacement of the wheel during the 3.0-s
interval? (a) 15 rad (b) 21 rad (c) 27 rad (d) There is not enough information given to determine the angular displacement.
7. A rotating object starts from rest at t = 0 s and has a constant angular acceleration. At a time of t = 7.0 s the object has an angular velocity of 𝜔 = 16 rad/s. What is its angular velocity at a time of t = 14 s?
Section 8.4 Angular Variables and Tangential Variables 10. A merry-go-round at a playground is a circular platform that is mounted parallel to the ground and can rotate about an axis that is perpendicular to
the platform at its center. The angular speed of the merry-go-round is con-
stant, and a child at a distance of 1.4 m from the axis has a tangential speed
of 2.2 m/s. What is the tangential speed of another child, who is located
at a distance of 2.1 m from the axis? (a) 1.5 m/s (b) 3.3 m/s (c) 2.2 m/s (d) 5.0 m/s (e) 0.98 m/s 11. A small fan has blades that have a radius of 0.0600 m. When the fan is turned on, the tips of the blades have a tangential acceleration of 22.0 m/s2
as the fan comes up to speed. What is the angular acceleration 𝛼 of the blades?
Section 8.5 Centripetal Acceleration and Tangential Acceleration 13. A wheel rotates with a constant angular speed 𝜔. Which one of the fol- lowing is true concerning the angular acceleration 𝛼 of the wheel, the tan- gential acceleration aT of a point on the rim of the wheel, and the centripetal acceleration ac of a point on the rim?
(a) 𝛼 = 0 rad/s2, aT = 0 m/s2, and ac = 0 m/s2
(b) 𝛼 = 0 rad/s2, aT ≠ 0 m/s2, and ac = 0 m/s2
(c) 𝛼 ≠ 0 rad/s2, aT = 0 m/s2, and ac = 0 m/s2
(d) 𝛼 = 0 rad/s2, aT = 0 m/s2, and ac ≠ 0 m/s2
(e) 𝛼 ≠ 0 rad/s2, aT ≠ 0 m/s2, and ac ≠ 0 m/s2
14. A platform is rotating with an angular speed of 3.00 rad/s and an angular acceleration of 11.0 rad/s2. At a point on the platform that is 1.25 m from the
axis of rotation, what is the magnitude of the total acceleration a?
Section 8.6 Rolling Motion 15. The radius of each wheel on a bicycle is 0.400 m. The bicycle travels a distance of 3.0 km. Assuming that the wheels do not slip, how many revolu-
tions does each wheel make?
(a) 1.2 × 103 revolutions (b) 2.4 × 102 revolutions (c) 6.0 × 103 revolutions (d) 8.4 × 10‒4 revolutions (e) Since the time of travel is not given, there is not enough information
for a solution.
Focus on Concepts
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 8.1 Rotational Motion and Angular Displacement,
Section 8.2 Angular Velocity and Angular Acceleration 1. E SSM A pitcher throws a curveball that reaches the catcher in 0.60 s. The ball curves because it is spinning at an average angular velocity of 330 rev/min
(assumed constant) on its way to the catcher’s mitt. What is the angular displace-
ment of the baseball (in radians) as it travels from the pitcher to the catcher?
2. E GO The table that follows lists four pairs of initial and fi nal angles of a wheel on a moving car. The elapsed time for each pair of angles is 2.0 s. For
Problems
Problems 217
each of the four pairs, determine the average angular velocity (magnitude and
direction as given by the algebraic sign of your answer).
Initial angle 𝜽0 Final angle 𝜽 (a) 0.45 rad 0.75 rad
(b) 0.94 rad 0.54 rad
(c) 5.4 rad 4.2 rad
(d) 3.0 rad 3.8 rad
3. E The earth spins on its axis once a day and orbits the sun once a year (365
1
4 days). Determine the average angular velocity (in rad/s) of the earth
as it (a) spins on its axis and (b) orbits the sun. In each case, take the positive direction for the angular displacement to be the direction of the earth’s
motion.
4. E Our sun rotates in a circular orbit about the center of the Milky Way galaxy. The radius of the orbit is 2.2 × 1020 m, and the angular speed of the
sun is 1.1 × 10‒15 rad/s. How long (in years) does it take for the sun to make
one revolution around the center?
5. E SSM Available in WileyPLUS. 6. E GO The initial angular velocity and the angular acceleration of four rotating objects at the same instant in time are listed in the table that follows.
For each of the objects (a), (b), (c), and (d), determine the fi nal angular speed after an elapsed time of 2.0 s.
Initial angular velocity 𝝎0
Angular acceleration α
(a) +12 rad/s +3.0 rad/s2
(b) +12 rad/s −3.0 rad/s2
(c) −12 rad/s +3.0 rad/s2
(d) −12 rad/s −3.0 rad/s2
7. E GO The table that follows lists four pairs of initial and fi nal angular velocities for a rotating fan blade. The elapsed time for each of the four pairs
of angular velocities is 4.0 s. For each of the four pairs, fi nd the average
angular acceleration (magnitude and direction as given by the algebraic sign
of your answer).
Initial angular velocity 𝝎0
Final angular velocity 𝝎
(a) +2.0 rad/s +5.0 rad/s
(b) +5.0 rad/s +2.0 rad/s
(c) −7.0 rad/s −3.0 rad/s
(d) +4.0 rad/s −4.0 rad/s
8. E Conceptual Example 2 provides some relevant background for this problem. A jet is circling an airport control tower at a distance of 18.0 km.
An observer in the tower watches the jet cross in front of the moon. As seen
from the tower, the moon subtends an angle of 9.04 × 10‒3 radians. Find the
distance traveled (in meters) by the jet as the observer watches the nose of the
jet cross from one side of the moon to the other.
9. E SSM A Ferris wheel rotates at an angular velocity of 0.24 rad/s. Start- ing from rest, it reaches its operating speed with an average angular ac-
celeration of 0.030 rad/s2. How long does it take the wheel to come up to
operating speed?
10. E GO A fl oor polisher has a rotating disk that has a 15-cm radius. The disk rotates at a constant angular velocity of 1.4 rev/s and is covered with a
soft material that does the polishing. An operator holds the polisher in one
place for 45 s, in order to buff an especially scuff ed area of the fl oor. How far
(in meters) does a spot on the outer edge of the disk move during this time?
11. M The sun appears to move across the sky, because the earth spins on its axis. To a person standing on the earth, the sun subtends an angle of 𝜃sun =
9.28 × 10‒3 rad (see Conceptual Example 2). How much time (in seconds)
does it take for the sun to move a distance equal to its own diameter?
12. M GO A propeller is rotating about an axis perpendicular to its center, as the drawing shows. The axis is parallel to the ground. An arrow is fi red
at the propeller, travels parallel to the axis, and passes through one of the
open spaces between the propeller blades. The angular open spaces between
the three propeller blades are each 𝜋/3 rad (60.0°). The vertical drop of the arrow may be ignored. There is a maximum value 𝜔 for the angular speed of the propeller, beyond which the arrow cannot pass through an open space
without being struck by one of the blades. Find this maximum value when the
arrow has the lengths L and speeds υ shown in the following table.
L υ
(a) 0.71 m 75.0 m/s
(b) 0.71 m 91.0 m/s
(c) 0.81 m 91.0 m/s
PROBLEM 12
A B
ω
13. M CHALK Two people start at the same place and walk around a circular lake in opposite directions. One walks with an angular speed of 1.7 × 10‒3
rad/s, while the other has an angular speed of 3.4 × 10‒3 rad/s. How long will
it be before they meet?
14. M A space station consists of two donut-shaped living chambers, A and B, that have the radii shown in the drawing. As the station rotates, an astro-
naut in chamber A is moved 2.40 × 102 m along a circular arc. How far along
a circular arc is an astronaut in chamber B moved during the same time?
PROBLEM 14
A
B
rA = 3.20 x 10 2 m
rB = 1.10 x 10 3 m
15. M V-HINT The drawing shows a device that can be used to measure the speed of a bullet. The device consists of two rotating disks, separated by a
distance of d = 0.850 m, and rotating with an angular speed of 95.0 rad/s. The
218 CHAPTER 8 Rotational Kinematics
bullet fi rst passes through the left disk and then through the right disk. It is
found that the angular displacement between the two bullet holes is 𝜃 = 0.240
rad. From these data, determine the speed of the bullet.
PROBLEM 15
Motor
Bullet
d
16. M GO An automatic dryer spins wet clothes at an angular speed of 5.2 rad/s. Starting from rest, the dryer reaches its operating speed with an
average angular acceleration of 4.0 rad/s2. How long does it take the dryer to
come up to speed?
17. M SSM A stroboscope is a light that fl ashes on and off at a constant rate. It can be used to illuminate a rotating object, and if the fl ashing rate is
adjusted properly, the object can be made to appear stationary. (a) What is the shortest time between fl ashes of light that will make a three-bladed propeller
appear stationary when it is rotating with an angular speed of 16.7 rev/s?
(b) What is the next shortest time? 18. H Available in WileyPLUS. 19. H The drawing shows a golf ball passing through a windmill at a mini- ature golf course. The windmill has 8 blades and rotates at an angular speed
of 1.25 rad/s. The opening between successive blades is equal to the width of
a blade. A golf ball (diameter 4.50 × 10‒2 m) has just reached the edge of one
of the rotating blades (see the drawing). Ignoring the thickness of the blades,
fi nd the minimum linear speed with which the ball moves along the ground, such that the ball will not be hit by the next blade.
PROBLEM 19
Golf ball
Section 8.3 The Equations of Rotational Kinematics 20. E A fi gure skater is spinning with an angular velocity of +15 rad/s. She then comes to a stop over a brief period of time. During this time, her angular
displacement is +5.1 rad. Determine (a) her average angular acceleration and (b) the time during which she comes to rest. 21. E SSM A gymnast is performing a fl oor routine. In a tumbling run she spins through the air, increasing her angular velocity from 3.00 to 5.00 rev/s
while rotating through one-half of a revolution. How much time does this
maneuver take?
22. E The angular speed of the rotor in a centrifuge increases from 420 to 1420 rad/s in a time of 5.00 s. (a) Obtain the angle through which the rotor turns. (b) What is the magnitude of the angular acceleration? 23. E A wind turbine is initially spinning at a constant angular speed. As the wind’s strength gradually increases, the turbine experiences a constant
angular acceleration of 0.140 rad/s2. After making 2870 revolutions, its angu-
lar speed is 137 rad/s. (a) What is the initial angular velocity of the turbine? (b) How much time elapses while the turbine is speeding up? 24. E GO A car is traveling along a road, and its engine is turning over with an angular velocity of +220 rad/s. The driver steps on the accelerator, and in a time
of 10.0 s the angular velocity increases to +280 rad/s. (a) What would have been the angular displacement of the engine if its angular velocity had remained con-
stant at the initial value of +220 rad/s during the entire 10.0-s interval? (b) What would have been the angular displacement if the angular velocity had been equal
to its fi nal value of +280 rad/s during the entire 10.0-s interval? (c) Determine the actual value of the angular displacement during the 10.0-s interval.
25. E SSM The wheels of a bicycle have an angular velocity of +20.0 rad/s. Then, the brakes are applied. In coming to rest, each wheel makes an angular
displacement of +15.92 revolutions. (a) How much time does it take for the bike to come to rest? (b) What is the angular acceleration (in rad/s2) of each wheel? 26. M BIO A dentist causes the bit of a high-speed drill to accelerate from an angular speed of 1.05 × 104 rad/s to an angular speed of 3.14 × 104 rad/s.
In the process, the bit turns through 1.88 × 104 rad. Assuming a constant
angular acceleration, how long would it take the bit to reach its maximum
speed of 7.85 × 104 rad/s, starting from rest?
27. M SSM MMH A motorcyclist is traveling along a road and accelerates for 4.50 s to pass another cyclist. The angular acceleration of each wheel is
+6.70 rad/s2, and, just after passing, the angular velocity of each wheel is
+74.5 rad/s, where the plus signs indicate counterclockwise directions. What
is the angular displacement of each wheel during this time?
28. M V-HINT A top is a toy that is made to spin on its pointed end by pulling on a string wrapped around the body of the top. The string has a length of
64 cm and is wound around the top at a spot where its radius is 2.0 cm. The
thickness of the string is negligible. The top is initially at rest. Someone pulls
the free end of the string, thereby unwinding it and giving the top an angular
acceleration of +12 rad/s2. What is the fi nal angular velocity of the top when
the string is completely unwound?
29. M MMH The drive propeller of a ship starts from rest and accelerates at 2.90 × 10‒3 rad/s2 for 2.10 × 103 s. For the next 1.40 × 103 s the propeller
rotates at a constant angular speed. Then it decelerates at 2.30 × 10‒3 rad/s2
until it slows (without reversing direction) to an angular speed of 4.00 rad/s.
Find the total angular displacement of the propeller.
30. M GO The drawing shows a graph of the angular velocity of a rotating wheel as a function of time. Although not shown in the graph, the angular
velocity continues to increase at the same rate until t = 8.0 s. What is the angular displacement of the wheel from 0 to 8.0 s?
PROBLEM 30 –9.0
–6.0
–3.0
0 1.0 5.0
+3.0
+6.0
3.0 Time (s)
A ng
ul ar
v el
oc it
y (r
ad /s
)
31. M V-HINT At the local swimming hole, a favorite trick is to run hori- zontally off a cliff that is 8.3 m above the water. One diver runs off the edge
of the cliff , tucks into a “ball,” and rotates on the way down with an average
angular speed of 1.6 rev/s. Ignore air resistance and determine the number of
revolutions she makes while on the way down.
32. M V-HINT A spinning wheel on a fi reworks display is initially rotating in a counterclockwise direction. The wheel has an angular acceleration of ‒4.00
rad/s2. Because of this acceleration, the angular velocity of the wheel changes
from its initial value to a fi nal value of ‒25.0 rad/s. While this change occurs,
the angular displacement of the wheel is zero. (Note the similarity to that of
a ball being thrown vertically upward, coming to a momentary halt, and then
falling downward to its initial position.) Find the time required for the change
in the angular velocity to occur.
33. H SSM Available in WileyPLUS.
Problems 219
Section 8.4 Angular Variables and Tangential Variables 34. E GO A fan blade is rotating with a constant angular acceleration of +12.0 rad/s2. At what point on the blade, as measured from the axis of
rotation, does the magnitude of the tangential acceleration equal that of the
acceleration due to gravity?
35. E BIO Some bacteria are propelled by biological motors that spin hair- like fl agella. A typical bacterial motor turning at a constant angular velocity
has a radius of 1.5 × 10‒8 m, and a tangential speed at the rim of 2.3 × 10‒5 m/s.
(a) What is the angular speed (the magnitude of the angular velocity) of this bacterial motor? (b) How long does it take the motor to make one revolution? 36. E An auto race takes place on a circular track. A car completes one lap in a time of 18.9 s, with an average tangential speed of 42.6 m/s. Find (a) the average angular speed and (b) the radius of the track. 37. E SSM A string trimmer is a tool for cutting grass and weeds; it utilizes a length of nylon “string” that rotates about an axis perpendicular to one end
of the string. The string rotates at an angular speed of 47 rev/s, and its tip has
a tangential speed of 54 m/s. What is the length of the rotating string?
38. E V-HINT In 9.5 s a fi sherman winds 2.6 m of fi shing line onto a reel whose radius is 3.0 cm (assumed to be constant as an approximation). The line
is being reeled in at a constant speed. Determine the angular speed of the reel.
39. E MMH Available in WileyPLUS. 40. E The earth has a radius of 6.38 × 106 m and turns on its axis once every 23.9 h. (a) What is the tangential speed (in m/s) of a person living in Ecuador, a country that lies on the equator? (b) At what latitude (i.e., the angle 𝜃 in the drawing) is the tangential speed one-third that of a person
living in Ecuador?
PROBLEM 40
Axis of rotation
Equator
θ
41. M SSM A baseball pitcher throws a baseball horizontally at a linear speed of 42.5 m/s (about 95 mi/h). Before being caught, the baseball travels
a horizontal distance of 16.5 m and rotates through an angle of 49.0 rad. The
baseball has a radius of 3.67 cm and is rotating about an axis as it travels,
much like the earth does. What is the tangential speed of a point on the
“equator” of the baseball?
42. M GO A person lowers a bucket into a well by turning the hand crank, as the drawing illustrates. The crank handle moves with a constant tangential
speed of 1.20 m/s on its circular path. The rope holding the bucket unwinds
without slipping on the barrel of the crank. Find the linear speed with which
the bucket moves down the well.
PROBLEM 42
0.100 m diameter
0.400 m diameter
43. M A thin rod (length = 1.50 m) is oriented vertically, with its bottom end attached to the fl oor by means of a frictionless hinge. The mass of the rod
may be ignored, compared to the mass of an object fi xed to the top of the rod.
The rod, starting from rest, tips over and rotates downward. (a) What is the angular speed of the rod just before it strikes the fl oor? (Hint: Consider using the principle of conservation of mechanical energy.) (b) What is the mag- nitude of the angular acceleration of the rod just before it strikes the fl oor?
44. H Available in WileyPLUS.
Section 8.5 Centripetal Acceleration and Tangential Acceleration 45. E SSM A racing car travels with a constant tangential speed of 75.0 m/s around a circular track of radius 625 m. Find (a) the magnitude of the car’s total acceleration and (b) the direction of its total acceleration relative to the radial direction.
46. E GO Two Formula One racing cars are negotiating a circular turn, and they have the same centripetal acceleration. However, the path of car A has a
radius of 48 m, while that of car B is 36 m. Determine the ratio of the angular
speed of car A to the angular speed of car B.
47. E SSM The earth orbits the sun once a year (3.16 × 107 s) in a nearly circular orbit of radius 1.50 × 1011 m. With respect to the sun, determine
(a) the angular speed of the earth, (b) the tangential speed of the earth, and (c) the magnitude and direction of the earth’s centripetal acceleration. 48. E MMH Review Multiple-Concept Example 7 in this chapter as an aid in solving this problem. In a fast-pitch softball game the pitcher is impressive
to watch, as she delivers a pitch by rapidly whirling her arm around so that
the ball in her hand moves on a circle. In one instance, the radius of the circle
is 0.670 m. At one point on this circle, the ball has an angular acceleration of
64.0 rad/s2 and an angular speed of 16.0 rad/s. (a) Find the magnitude of the total acceleration (centripetal plus tangential) of the ball. (b) Determine the angle of the total acceleration relative to the radial direction.
49. M GO A rectangular plate is rotating with a constant angular speed about an axis that passes perpendicularly through one corner, as the drawing
shows. The centripetal acceleration measured at corner A is n times as great as that measured at corner B. What is the ratio L1/L2 of the lengths of the sides of the rectangle when n = 2.00?
PROBLEM 49
A
B
L2
L1
50. M V-HINT Multiple-Concept Example 7 explores the approach taken in problems such as this one. The blades of a ceiling fan have a radius of 0.380 m
and are rotating about a fi xed axis with an angular velocity of +1.50 rad/s.
When the switch on the fan is turned to a higher speed, the blades acquire
an angular acceleration of +2.00 rad/s2. After 0.500 s has elapsed since the
switch was reset, what is (a) the total acceleration (in m/s2) of a point on the tip of a blade and (b) the angle 𝜙 between the total acceleration a→ and the centripetal acceleration ac
→ ? (See Interactive Figure 8.12b.)
51. M CHALK SSM The sun has a mass of 1.99 × 1030 kg and is moving in a circular orbit about the center of our galaxy, the Milky Way. The radius of
the orbit is 2.3 × 104 light-years (1 light-year = 9.5 × 1015 m), and the angular
speed of the sun is 1.1 × 10‒15 rad/s. (a) Determine the tangential speed of the sun. (b) What is the magnitude of the net force that acts on the sun to keep it moving around the center of the Milky Way?
52. H Available in WileyPLUS.
220 CHAPTER 8 Rotational Kinematics
Section 8.6 Rolling Motion Note: All problems in this section assume that there is no slipping of the surfaces in contact during the rolling motion. 53. E SSM A motorcycle accelerates uniformly from rest and reaches a lin- ear speed of 22.0 m/s in a time of 9.00 s. The radius of each tire is 0.280 m.
What is the magnitude of the angular acceleration of each tire?
54. E An automobile tire has a radius of 0.330 m, and its center moves forward with a linear speed of υ = 15.0 m/s. (a) Determine the angular speed of the wheel. (b) Relative to the axle, what is the tangential speed of a point located 0.175 m from the axle?
55. E MMH A car is traveling with a speed of 20.0 m/s along a straight horizontal road. The wheels have a radius of 0.300 m. If the car speeds up
with a linear acceleration of 1.50 m/s2 for 8.00 s, fi nd the angular displace-
ment of each wheel during this period.
56. E Suppose you are riding a stationary exercise bicycle, and the elec- tronic meter indicates that the wheel is rotating at 9.1 rad/s. The wheel has
a radius of 0.45 m. If you ride the bike for 35 min, how far would you have
gone if the bike could move?
57. M V-HINT A motorcycle, which has an initial linear speed of 6.6 m/s, decelerates to a speed of 2.1 m/s in 5.0 s. Each wheel has a radius of 0.65 m
and is rotating in a counterclockwise (positive) direction. What are (a) the constant angular acceleration (in rad/s2) and (b) the angular displacement (in rad) of each wheel?
58. M GO A dragster starts from rest and accelerates down a track. Each tire has a radius of 0.320 m and rolls without slipping. At a distance of 384 m, the
angular speed of the wheels is 288 rad/s. Determine (a) the linear speed of the dragster and (b) the magnitude of the angular acceleration of its wheels. 59. M MMH Available in WileyPLUS. 60. M GO A bicycle is rolling down a circular portion of a path; this portion of the path has a radius of 9.00 m. As the drawing illustrates, the angular
displacement of the bicycle is 0.960 rad. What is the angle (in radians)
through which each bicycle wheel (radius = 0.400 m) rotates?
PROBLEM 60
0.960 rad
61. M SSM The penny-farthing is a bicycle that was popular between 1870 and 1890. As the drawing shows, this type of bicycle has a large
front wheel and a small rear wheel. During a ride, the front wheel
(radius = 1.20 m) makes 276 revolutions. How many revolutions does the
rear wheel (radius = 0.340 m) make?
PROBLEM 61
62. M CHALK GO A ball of radius 0.200 m rolls with a constant linear speed of 3.60 m/s along a horizontal table. The ball rolls off the edge and falls a
vertical distance of 2.10 m before hitting the fl oor. What is the angular dis-
placement of the ball while the ball is in the air?
63. H Available in WileyPLUS.
64. E Available in WileyPLUS. 65. E SSM Available in WileyPLUS. 66. E A fl ywheel has a constant angular deceleration of 2.0 rad/s2. (a) Find the angle through which the fl ywheel turns as it comes to rest from an angular
speed of 220 rad/s. (b) Find the time for the fl ywheel to come to rest. 67. E SSM An electric fan is running on HIGH. After the LOW button is pressed, the angular speed of the fan decreases to 83.8 rad/s in 1.75 s. The
deceleration is 42.0 rad/s2. Determine the initial angular speed of the fan.
68. E Refer to Multiple-Concept Example 7 for insight into this problem. During a tennis serve, a racket is given an angular acceleration of magnitude
160 rad/s2. At the top of the serve, the racket has an angular speed of 14 rad/s.
If the distance between the top of the racket and the shoulder is 1.5 m, fi nd the
magnitude of the total acceleration of the top of the racket.
69. E MMH Available in WileyPLUS. 70. M BIO GO In a large centrifuge used for training pilots and astronauts, a small chamber is fi xed at the end of a rigid arm that rotates in a horizontal
circle. A trainee riding in the chamber of a centrifuge rotating with a constant
angular speed of 2.5 rad/s experiences a centripetal acceleration of 3.2 times
the acceleration due to gravity. In a second training exercise, the centrifuge
speeds up from rest with a constant angular acceleration. When the centri-
fuge reaches an angular speed of 2.5 rad/s, the trainee experiences a total
acceleration equal to 4.8 times the acceleration due to gravity. (a) How long is the arm of the centrifuge? (b) What is the angular acceleration of the cent- rifuge in the second training exercise?
71. M SSM A compact disc (CD) contains music on a spiral track. Music is put onto a CD with the assumption that, during playback, the music will
be detected at a constant tangential speed at any point. Since υT = r𝜔, a CD rotates at a smaller angular speed for music near the outer edge and a larger
angular speed for music near the inner part of the disc. For music at the outer
edge (r = 0.0568 m), the angular speed is 3.50 rev/s. Find (a) the constant tangential speed at which music is detected and (b) the angular speed (in rev/s) for music at a distance of 0.0249 m from the center of a CD.
72. M V-HINT After 10.0 s, a spinning roulette wheel at a casino has slowed down to an angular velocity of +1.88 rad/s. During this time, the wheel has
an angular acceleration of ‒5.04 rad/s2. Determine the angular displacement
of the wheel.
73. M GO At a county fair there is a betting game that involves a spinning wheel. As the drawing shows, the wheel is set into rotational motion with
the beginning of the angular section labeled “1” at the marker at the top of
the wheel. The wheel then decelerates and eventually comes to a halt on one
of the numbered sections. The wheel in the drawing is divided into twelve
sections, each of which is an angle of 30.0°. Determine the numbered section
on which the wheel comes to a halt when the deceleration of the wheel has a
Additional Problems
Concepts and Calculations Problems 221
magnitude of 0.200 rev/s2 and the initial angular velocity is (a) +1.20 rev/s and (b) +1.47 rev/s.
PROBLEM 73
12
Marker
1 11
0
2
10 3
9 4
8 5 7 6
ω
74. M V-HINT MMH A racing car, starting from rest, travels around a circular turn of radius 23.5 m. At a certain instant, the car is still accelerating, and its
angular speed is 0.571 rad/s. At this time, the total acceleration (centripetal
plus tangential) makes an angle of 35.0° with respect to the radius. (The situ-
ation is similar to that in Interactive Figure 8.12b.) What is the magnitude of the total acceleration?
75. H Available in WileyPLUS. 76. H MMH Available in WileyPLUS. 77. M GO SSM An automobile, starting from rest, has a linear acceleration to the right whose magnitude is 0.800 m/s2 (see the fi gure). During the next
20.0 s, the tires roll and do not slip. The radius of each wheel is 0.330 m.
At the end of this time, what is the angle through which each wheel has
rotated?
At rest t0 = 0 s
t = 20.0 s
θ
PROBLEM 77
In this chapter we have studied the concepts of angular displacement, angular
velocity, and angular acceleration. We now review some important aspects
of these quantities. Problem 78 illustrates that the angular acceleration and
the angular velocity can have the same or opposite direction, depending on
whether the angular speed is increasing or decreasing. Problem 79 reviews
the two diff erent types of acceleration, centripetal and tangential, that a car
can have when it travels on a circular road.
78. M CHALK A rider on a mountain bike is traveling to the left in the fi gure. Each wheel has an angular velocity of +21.7 rad/s, where, as usual, the plus
sign indicates that the wheel is rotating in the counterclockwise direction.
(a) To pass another cyclist, the rider pumps harder, and the angular velo- city of the wheels increases from +21.7 to +28.5 rad/s in a time of 3.50 s.
(b) After passing the cyclist, the rider begins to coast, and the angular velo- city of the wheels decreases from +28.5 to +15.3 rad/s in a time of 10.7 s.
Concepts: (i) Is the angular acceleration positive or negative when the rider is passing the cyclist and the angular speed of the wheels is increasing?
(ii) Is the angular acceleration positive or negative when the rider is coasting
and the angular speed of the wheels is decreasing? Calculations: In both instances, (a) and (b), determine the magnitude and direction of the angular acceleration (assumed constant) of the wheels.
79. M CHALK SSM Suppose you are driving a car in a counterclockwise direction on a circular road whose radius is r = 390 m (see the fi gure). You look at the speedometer and it reads a steady 32 m/s (about 72 mi/h). Concepts: (i) Does an object traveling at a constant tangential speed (for example,
υT = 32 m/s) along a circular path have an acceleration? (ii) Is there a tangen- tial acceleration a T→ when the angular speed of an object changes (e.g., when the car’s angular speed decreases to 4.9 × 10‒2 rad/s)? Calculations: (a) What is the angular speed of the car? (b) Determine the acceleration (magnitude and direction) of the car. (c) To avoid a rear-end collision with the vehicle ahead, you apply the brakes and reduce your angular speed to 4.9 × 10‒2 rad/s in
a time of 4.0 s. What is the tangential acceleration (magnitude and direction)
of the car?
(a) Constant angular speed (b) Decreasing angular speed
ac
r
ac aT
vT (decreasing)
vT
θ
PROBLEM 79
Concepts and Calculations Problems
(a) Angular speed increasing
(b) Angular speed decreasing
α ω
PROBLEM 78
222 CHAPTER 8 Rotational Kinematics
80. M Energy of a Bullet Dissipated by Plywood. As part of a criminal investigation, you need to determine how much of a bullet’s energy is dissip- ated by a 0.500-inch piece of plywood. You construct a device that consists of three disks that are separated by a distance d = 0.950 m and rotate on a common axis. The bullet is fi red through the fi rst disk (a few inches above its center), which is composed of a light plastic that has a negligible eff ect on the speed of the bullet. The bullet then passes through the second disk, which is composed of 0.500-inch plywood. Finally, the bullet strikes the third disk, where it becomes embedded. The disks rotate with an angular velocity of ω = 92.0 rad/s. The angular displacement between holes in the fi rst and second disks is Δ𝜃12 = 0.255 rad, and the angular displacement between the holes in the second and third disks is Δ𝜃23 = 0.273 rad. If the mass of the bullet is 15.0 g, fi nd (a) the initial speed of the bullet and (b) the energy dis- sipated by the 0.50-inch plywood.
81. M Three Wheels. Three rubber wheels are mounted on axles so that their outer edges make tight contact with each other and their centers are on a line. The wheel on the far left axle is connected to a motor that rotates it at 25.0 rpm, and drives the wheel in contact with it on its right, which, in turn, drives the wheel on its right. The left wheel (Wheel 1) has a diameter of d1 = 0.20 m, the middle wheel (Wheel 2) has d2 = 0.30 m, and the far right wheel (Wheel 3) has d3 = 0.45 m. (a) If Wheel 1 rotates clockwise, in which direction does Wheel 3 rotate? (b) What is the angular speed of Wheel 3, and what is the tangential speed on its outer edge? (c) What arrangement of the wheels gives the largest tangential speed on the outer edge of the wheel in the far right position (assuming the wheel in the far left position is driven at 25.0 rpm)?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
9.1 Distinguish between torque and force.
9.2 Analyze rigid objects in equilibrium.
9.3 Determine the center of gravity of rigid objects.
9.4 Analyze rotational dynamics using moments of inertia.
9.5 Apply the relation between rotational work and energy.
9.6 Solve problems using the conservation of angular momentum.
M r.
G re
en /S
h u tt
er st
o ck
CHAPTER 9
Rotational Dynamics
The large counterweight on the right side (short end) of this tall tower crane ensures its boom remains
balanced on its mast while lifting heavy loads. It is not equal weights on both sides of the tower that keep
it in equilibrium, but equal torques. Torque is the rotational analog of force, and is an important topic of
this chapter.
9.1 The Action of Forces and Torques on Rigid Objects The mass of most rigid objects, such as a propeller or a wheel, is spread out and not
concentrated at a single point. These objects can move in a number of ways. Figure 9.1a illustrates one possibility called translational motion, in which all points on the body
travel on parallel paths (not necessarily straight lines). In pure translation there is no
223
Translation( )a Combined translation and rotation( )b
FIGURE 9.1 Examples of (a) translational motion and (b) combined translational and rotational motions.
224 CHAPTER 9 Rotational Dynamics
rotation of any line in the body. Because translational motion can occur along a curved line, it is
often called curvilinear motion or linear motion. Another possibility is rotational motion, which
may occur in combination with translational motion, as is the case for the somersaulting gymnast
in Figure 9.1b. We have seen many examples of how a net force aff ects linear motion by causing an object
to accelerate. We now need to take into account the possibility that a rigid object can also have
an angular acceleration. A net external force causes linear motion to change, but what causes
rotational motion to change? For example, something causes the rotational velocity of a speed-
boat’s propeller to change when the boat accelerates. Is it simply the net force? As it turns out, it
is not the net external force, but rather the net external torque that causes the rotational velocity
to change. Just as greater net forces cause greater linear accelerations, greater net torques cause
greater rotational or angular accelerations.
Interactive Figure 9.2 helps to explain the idea of torque. When you push on a door with a force F
→ , as in part a, the door opens more quickly when the force is larger. Other
things being equal, a larger force generates a larger torque. However, the door does not open
as quickly if you apply the same force at a point closer to the hinge, as in part b, because the force now produces less torque. Furthermore, if your push is directed nearly at the hinge, as
in part c, you will have a hard time opening the door at all, because the torque is nearly zero. In summary, the torque depends on the magnitude of the force, on the point where the force
is applied relative to the axis of rotation (the hinge in Interactive Figure 9.2), and on the direction of the force.
For simplicity, we deal with situations in which the force lies in a plane that is perpendicular
to the axis of rotation. In Figure 9.3, for instance, the axis is perpendicular to the page and the force lies in the plane of the paper. The drawing shows the line of action and the lever arm of
the force, two concepts that are important in the defi nition of torque. The line of action is an extended line drawn colinear with the force. The lever arm is the distance ℓ between the line of action and the axis of rotation, measured on a line that is perpendicular to both. The torque is
represented by the symbol 𝜏 (Greek letter tau), and its magnitude is defi ned as the magnitude of the force times the lever arm:
DEFINITION OF TORQUE
Magnitude of torque = (Magnitude of the force) × (Lever arm) = Fℓ (9.1)
Direction: The torque 𝝉 is positive when the force tends to produce a counterclock- wise rotation about the axis, and negative when the force tends to produce a clockwise rotation.
SI Unit of Torque: newton ⋅ meter (N ⋅ m)
Equation 9.1 indicates that forces of the same magnitude can produce diff erent torques, depending on the value of the lever arm, and Example 1 illustrates this important feature.
F
F
F
( )a
Hinge (axis of rotation)
( )b
( )c
Door
INTERACTIVE FIGURE 9.2 With a force of a given magnitude, a door is easier to open
by (a) pushing at the outer edge than by (b) pushing closer to the axis of rotation (the hinge). (c) Pushing into the hinge makes it diffi cult to open the door.
EXAMPLE 1 Diff erent Lever Arms, Diff erent Torques
In Figure 9.3 a force (magnitude = 55 N) is applied to a door. However, the lever arms are diff erent in the three parts of the drawing: (a) ℓ = 0.80 m, (b) ℓ = 0.60 m, and (c) ℓ = 0 m. Find the torque in each case.
Reasoning In each case the lever arm is the perpendicular distance between the axis of rotation and the line of action of the force. In part a this perpendicular distance is equal to the width of the door. In parts b and c, however, the lever arm is less than the width. Because the lever arm is diff erent in each case, the torque is diff erent, even though the magnitude
of the applied force is the same.
Solution Using Equation 9.1, we fi nd the following values for the torques:
(a) 𝜏 = +Fℓ = +(55 N)(0.80 m) = +44 N · m (b) 𝜏 = +Fℓ = +(55 N)(0.60 m) = +33 N · m (c) 𝜏 = +Fℓ = +(55 N)(0 m) = 0 N · m
In parts a and b the torques are positive, since the forces tend to produce a counterclockwise rotation of the door. In part c the line of action of F→ passes through the axis of rotation (the hinge). Hence, the lever arm is
zero, and the torque is zero.
9.1 The Action of Forces and Torques on Rigid Objects 225
In our bodies, muscles and tendons produce torques about various joints. Example 2 illustrates
how the Achilles tendon produces a torque about the ankle joint.
Lever arm =
F
Axis of Rotation
( )a
F90°
( )b
90°
Line of action
Line of action Line of action
= 0, since line of action passes through axis
( )c
F
ℓ
ℓ
ℓ
FIGURE 9.3 In this top view, the hinges of a door appear as a black dot (•) and defi ne the axis of rotation. The line of action and lever arm ℓ are illustrated for a force applied to the door (a) perpen- dicularly and (b) at an angle. (c) The lever arm is zero because the line of action passes through the axis of rotation.
EXAMPLE 2 BIO The Physics of the Achilles Tendon
Figure 9.4a shows the ankle joint and the Achilles tendon attached to the heel at point P. The tendon exerts a force F→ (magnitude = 720 N), as Figure 9.4b indicates. Determine the torque (magnitude and direction) of this force about the ankle joint, which is located 3.6 × 10−2 m away from
point P.
Reasoning To calculate the magnitude of the torque, it is necessary to have a value for the lever arm ℓ. However, the lever arm is not the given
distance of 3.6 × 10−2 m. Instead, the lever arm is the perpendicular dis-
tance between the axis of rotation at the ankle joint and the line of action
of the force F→. In Figure 9.4b this distance is indicated by the dashed red line.
Solution From the drawing, it can be seen that the lever arm is ℓ = (3.6 × 10−2 m) cos 55°. The magnitude of the torque is
Fℓ = (720 N)(3.6 × 10−2 m) cos 55° = 15 N · m (9.1)
The force F→ tends to produce a clockwise rotation about the ankle joint, so the torque is negative: τ = −15 N · m .
( )a
Ankle joint P
Achilles tendon
( )b
Lever arm
55°
F
3.6 × 10–2 m
FIGURE 9.4 The force F→ generated by the Achilles tendon produces a clockwise (negative) torque about the ankle joint.
226 CHAPTER 9 Rotational Dynamics
Check Your Understanding
(The answers are given at the end of the book.) 1. CYU Figure 9.1 shows an overhead view of a hori-
zontal bar that is free to rotate about an axis perpen-
dicular to the page. Two forces act on the bar, and they
have the same magnitude. However, one force is per-
pendicular to the bar, and the other makes an angle 𝜙 with respect to it. The angle 𝜙 can be 90°, 45°, or 0°.
Rank the values of 𝜙 according to the magnitude of the
net torque (the sum of the torques) that the two forces
produce, largest net torque fi rst.
2. Sometimes, even with a wrench, one cannot loosen a nut that is frozen tightly to a bolt. It is often possible to loosen the nut by slipping one end of a long pipe over the wrench handle and pushing at
the other end of the pipe. With the aid of
the pipe, does the applied force produce
a smaller torque, a greater torque, or the
same torque on the nut?
3. Is it possible (a) for a large force to pro- duce a small, or even zero, torque and
(b) for a small force to produce a large torque?
4. CYU Figure 9.2 shows a woman strug- gling to keep a stack of boxes balanced
on a dolly. The woman’s left foot is on the
axle of the dolly. Assuming that the boxes
are identical, which one creates the great-
est torque with respect to the axle?
9.2 Rigid Objects in Equilibrium If a rigid body is in equilibrium, neither its linear motion nor its rotational motion changes. This
lack of change leads to certain equations that apply for rigid-body equilibrium. For instance, an
object whose linear motion is not changing has no acceleration a→. Therefore, the net force ΣF→ applied to the object must be zero, since ΣF→ = m a→ and a→ = 0. For two-dimensional motion the x and y components of the net force are separately zero: ΣFx = 0 and ΣFy = 0. In calculating the net force, we include only forces from external agents, or external forces.* In addition to linear motion, we must consider rotational motion, which also does not change under equilibrium con-
ditions. This means that the net external torque acting on the object must be zero, because torque
is what causes rotational motion to change. Using the symbol Στ to represent the net external torque (the sum of all positive and negative torques), we have
Στ = 0 (9.2)
We defi ne rigid-body equilibrium, then, in the following way.
EQUILIBRIUM OF A RIGID BODY A rigid body is in equilibrium if it has zero translational acceleration and zero angular acceleration. In equilibrium, the sum of the externally applied forces is zero, and the sum of the externally applied torques is zero:
ΣFx = 0 and ΣFy = 0 (4.9a and 4.9b)
Στ = 0 (9.2)
Bar (overhead view)
Axis (perpendicular to page)
F F
ϕ
CYU FIGURE 9.1
*We ignore internal forces that one part of an object exerts on another part, because they occur in action–reaction pairs,
each of which consists of oppositely directed forces of equal magnitude. The eff ect of one force cancels the eff ect of the
other, as far as the acceleration of the entire object is concerned.
H o w
ar d B
er m
an /S
to n e/
G et
ty I
m ag
es
CYU FIGURE 9.2
9.2 Rigid Objects in Equilibrium 227
The reasoning strategy for analyzing the forces and torques acting on a body in equilibrium
is given below. The fi rst four steps of the strategy are essentially the same as those outlined in
Section 4.11, where only forces are considered. Steps 5 and 6 have been added to account for any
external torques that may be present. Example 3 illustrates how this reasoning strategy is applied
to a diving board.
REASONING STRATEGY Applying the Conditions of Equilibrium to a Rigid Body 1. Select the object to which the equations for equilibrium are to be applied. 2. Draw a free-body diagram that shows all the external forces acting on the object. 3. Choose a convenient set of x, y axes and resolve all forces into components that lie along
these axes. 4. Apply the equations that specify the balance of forces at equilibrium: ΣFx = 0 and
ΣFy = 0. 5. Select a convenient axis of rotation. The choice is arbitrary. Identify the point where each
external force acts on the object, and calculate the torque produced by each force about the chosen axis. Set the sum of the torques equal to zero: Σ𝝉 = 0.
6. Solve the equations in Steps 4 and 5 for the desired unknown quantities.
EXAMPLE 3 A Diving Board
A woman whose weight is 530 N is poised at the right end of a diving
board with a length of 3.90 m. The board has negligible weight and is
bolted down at the left end, while being supported 1.40 m away by a
fulcrum, as Figure 9.5a shows. Find the forces F1 →
and F2 →
that the bolt and
the fulcrum, respectively, exert on the board.
Reasoning Part b of the fi gure shows the free-body diagram of the diving board. Three forces act on the board: F1
→ , F2
→ , and the force due
to the diver’s weight W→. In choosing the directions of F1 →
and F2 →
, we
have used our intuition: F1 →
points downward because the bolt must pull in
that direction to counteract the tendency of the board to rotate clockwise
about the fulcrum; F2 →
points upward, because the board pushes down-
ward against the fulcrum, which, in reaction, pushes upward on the board.
Since the board is stationary, it is in equilibrium.
Solution Since the board is in equilibrium, the sum of the vertical forces must be zero:
ΣFy = −F1 + F2 − W = 0 (4.9b)
Similarly, the sum of the torques must be zero, Σ𝜏 = 0. For calculat- ing torques, we select an axis that passes through the left end of the board
and is perpendicular to the page. (We will see shortly that this choice is
arbitrary.) The force F1 →
produces no torque since it passes through the
axis and, therefore, has a zero lever arm, while F2 →
creates a counterclock-
wise (positive) torque, and W →
produces a clockwise (negative) torque.
The free-body diagram shows the lever arms for the torques:
Στ = + F2ℓ2 − WℓW = 0 (9.2)
Solving this equation for F2 yields
F2 = WℓW
ℓ2 =
(530 N)(3.90 m)
1.40 m = 1480 N
This value for F2, along with W = 530 N, can be substituted into Equation 4.9b to show that F1 = 950 N .
+x
+y
+
Axis
2 = 1.40 m
w = 3.90 m
Free-body diagram of the diving board
Bolt
Fulcrum
( )a
( )b
ℓ
ℓF1
F2
W
FIGURE 9.5 (a) A diver stands at the end of a diving board. (b) The free-body diagram for the diving board. The box at the top left shows
the positive x and y directions for the forces, as well as the positive direction (counterclockwise) for the torques.
228 CHAPTER 9 Rotational Dynamics
In Example 3 the sum of the external torques is calculated using an axis that passes through
the left end of the diving board.
Problem-Solving Insight The choice of the axis is completely arbitrary, because if an object is in equilibrium, it is in equilibrium with respect to any axis whatsoever.
Thus, the sum of the external torques is zero, no matter where the axis is placed. (See Interac-
tive Learning Ware 9.2 at www.wiley.com/college/cutnell for a second version of Example 3 in which the axis is chosen diff erently.) One usually chooses the location so that the lines of action
of one or more of the unknown forces pass through the axis. Such a choice simplifi es the torque
equation, because the torques produced by these forces are zero. For instance, in Example 3
the torque due to the force F1 →
does not appear in Equation 9.2, because the lever arm of this force
is zero.
In a calculation of torque, the lever arm of the force must be determined relative to the axis
of rotation. In Example 3 the lever arms are obvious, but sometimes a little care is needed in
determining them, as in the next example.
ANIMATED FIGURE 9.6 (a) A ladder leaning against a smooth wall. (b) The free-body diagram for the ladder. (c) Three of the forces that act on the ladder and their lever arms. The axis of rotation is at the lower end of the ladder and is perpendicular to the page.
+x
+y
+
WL
Gx
G
P
P
y
WF
WL WF
( )a ( )cFree-body diagram of the ladder( )b
Pℓ
Lℓ
Fℓ
2. 30
m
4. 00
m
50.0°50.0°
50.0° Axis
EXAMPLE 4 Fighting a Fire
In Animated Figure 9.6a an 8.00-m ladder of weight WL = 355 N leans against a smooth vertical wall. The term “smooth” means that the
wall can exert only a normal force directed perpendicular to the wall
and cannot exert a frictional force parallel to it. A fi refi ghter, whose
weight is WF = 875 N, stands 6.30 m up from the bottom of the ladder. Assume that the ladder’s weight acts at the ladder’s center, and neglect
the hose’s weight. Find the forces that the wall and the ground exert on
the ladder.
Reasoning Animated Figure 9.6b shows the free-body diagram of the ladder. The following forces act on the ladder:
1. Its weight WL →
2. A force due to the weight WF → of the fi refi ghter
3. The force P→ applied to the top of the ladder by the wall and directed perpendicular to the wall
4. The forces Gx → and Gy
→ , which are the horizontal and vertical com- ponents of the force exerted by the ground on the bottom of the ladder
The ground, unlike the wall, is not smooth, so that the force Gx →
is produced
by static friction and prevents the ladder from slipping. The force Gy →
is the
normal force applied to the ladder by the ground. The ladder is in equilib-
rium, so the sum of these forces and the sum of the torques produced by
them must be zero.
Solution Since the net force acting on the ladder is zero, we have ΣFx = Gx − P = 0 (4.9a) ΣFy = Gy − WL − WF = 0 (4.9b) Solving Equation 4.9b gives
Gy = WL + WF = 355 N + 875 N = 1230 N
Equation 4.9a cannot be solved as it stands, because it contains two
unknown variables. However, we know that the net torque acting on an
object in equilibrium is zero. In calculating torques, we use an axis at the
left end of the ladder, directed perpendicular to the page, as Animated Figure 9.6c indicates. This axis is convenient, because Gx
→ and Gy
→ pro-
duce no torques about it, their lever arms being zero. Consequently,
9.2 Rigid Objects in Equilibrium 229
these forces will not appear in the equation representing the balance of
torques. The lever arms for the remaining forces are shown in Animated Figure 9.6c as red dashed lines of length ℓ. The following list summa- rizes these forces, their lever arms, and the torques:
Force Lever Arm Torque WL = 355 N ℓL = (4.00 m) cos 50.0° −WLℓL
P ℓP = (8.00 m) sin 50.0° +PℓP
WF = 875 N ℓF = (6.30 m) cos 50.0° −WFℓF
Setting the sum of the torques equal to zero gives
Στ = −WLℓL − WF ℓF + PℓP = 0 (9.2)
Solving this equation for P gives
P = WLℓL + WF ℓF
ℓP
= (355 N)(4.00 m) cos 50.0° + (875 N)(6.30 m) cos 50.0°
(8.00 m) sin 50.0° = 727 N
Substituting P = 727 N into Equation 4.9a reveals that
Gx = P = 727 N
Math Skills Sometimes it is necessary to use trigonometry to determine the lever arms from the distances given in a problem. As
examples, consider the lever arms for the forces WL →
and P→ (see Animated Figure 9.6c). To determine the lever arm ℓL for the force WL →
, we will use the cosine function. Equation 1.2 defi nes the cosine
of the angle 𝜃 as cos θ = ha h
, where ha is the side of a right triangle
adjacent to the angle 𝜃 and h is the hypotenuse of the right triangle, as shown by the smaller triangle in Figure 9.7a. By comparing this triangle with the smaller triangle in Figure 9.7b it can be seen that 𝜃 = 50.0° and that ha = ℓL and h = 4.00 m. As a result we have
cos 50.0° = ha h
= ℓL
4.00 m or ℓL = (4.00 m) cos 50.0°
To determine the lever arm ℓP for the force P →
, we will use the sine
function. Equation 1.1 defi nes the sine of the angle 𝜃 as sin θ = ho h
,
where ho is the side of a right triangle opposite the angle 𝜃 and h is the hypotenuse of the right triangle, as shown by the larger triangle
in Figure 9.7a. By comparing this triangle with the larger triangle in Figure 9.7b it can be seen that 𝜃 = 50.0° and that ho = ℓP and h = 8.00 m. As a result we have
sin 50.0° = ho h
= ℓP
8.00 m or ℓP = (8.00 m) sin 50.0°
P
WL
( )b
Pℓ
Lℓ
50.0°
50.0°
Axis
( )a
90°
90°
h
h
ha
θ
θ
4. 00
m
4. 00
m
ho
FIGURE 9.7 Math Skills drawing.
To a large extent the directions of the forces acting on an object in equilibrium can be deduced
using intuition. Sometimes, however, the direction of an unknown force is not obvious, and it is
inadvertently drawn reversed in the free-body diagram. This kind of mistake causes no diffi culty.
Problem-Solving Insight Choosing the direction of an unknown force backward in the free- body diagram simply means that the value determined for the force will be a negative number.
EXAMPLE 5 BIO The Physics of Bodybuilding
A bodybuilder holds a dumbbell of weight Wd →
as in Figure 9.8a. His arm is horizontal and weighs Wa = 31.0 N. The deltoid muscle is assumed to be the only muscle acting and is attached to the arm as shown. The maximum
force M →
that the deltoid muscle can supply has a magnitude of 1840 N.
Figure 9.8b shows the distances that locate where the various forces act on the arm. What is the weight of the heaviest dumbbell that can be held,
and what are the horizontal and vertical force components, Sx →
and Sy →
,
that the shoulder joint applies to the left end of the arm?
Reasoning Figure 9.8b is the free-body diagram for the arm. Note that Sx
→ is directed to the right, because the deltoid muscle pulls the arm
in toward the shoulder joint, and the joint pushes back in accordance
with Newton’s third law. The direction of the force Sy →
, however, is less
obvious, and we are alert for the possibility that the direction chosen in
the free-body diagram is backward. If so, the value obtained for Sy →
will
be negative.
Problem-Solving Insight When a force is negative, such as the vertical force Sy = –297 N in this example, it means that the direction of the force is opposite to that chosen originally.
230 CHAPTER 9 Rotational Dynamics
Check Your Understanding
(The answers are given at the end of the book.) 5. Three forces (magnitudes either F or 2F) in CYU Figure 9.3 act on each of the thin, square sheets
shown in the drawing. In parts A and B of the drawing, the force labeled 2F→ acts at the center of the sheet. When considering angular acceleration, use an axis of rotation that is perpendicular to the plane
of a sheet at its center. Determine in which drawing (a) the translational acceleration is equal to zero, but the angular acceleration is not equal to zero; (b) the translational acceleration is not equal to zero, but the angular acceleration is equal to zero; and (c) both the translational and angular accelerations are zero.
6. The free-body diagram in CYU Figure 9.4 shows the forces that act on a thin rod. The three forces are drawn to scale and lie in the plane of the paper. Are these forces suffi cient to keep the rod in equilib-
rium, or are additional forces necessary?
The condition specifying a zero net torque is
Στ = −Waℓa − Wdℓd + MℓM = 0 (9.2)
Solving this equation for Wd yields
Wd = −Waℓa + MℓM
ℓd
= −(31.0 N)(0.280 m) + (1840 N)(0.150 m) sin 13.0°
0.620 m = 86.1 N
Substituting this value for Wd into Equation 4.9b and solving for Sy gives Sy = −297 N . The minus sign indicates that the choice of direction for Sy in the free-body diagram is wrong. In reality, Sy has a magnitude of 297 N but is directed downward, not upward.
Solution The arm is in equilibrium, so the net force acting on it is zero:
ΣFx = Sx − M cos 13.0° = 0 (4.9a) or Sx = M cos 13.0° = (1840 N) cos 13.0° = 1790 N ΣFy = Sy + M sin 13.0° − Wa − Wd = 0 (4.9b)
Equation 4.9b cannot be solved at this point, because it contains two un-
knowns, Sy and Wd. However, since the arm is in equilibrium, the torques acting on the arm must balance, and this fact provides another equation.
To calculate torques, we choose an axis through the left end of the arm
and perpendicular to the page. With this axis, the torques due to Sx →
and
Sy →
are zero, because the line of action of each force passes through the
axis and the lever arm of each force is zero. The list below summarizes
the remaining forces, their lever arms (see Figure 9.8c), and the torques.
Force Lever Arm Torque Wa = 31.0 N ℓa = 0.280 m −Waℓa
Wd ℓd = 0.620 m −Wdℓd
M = 1840 N ℓM = (0.150 m) sin 13.0° +MℓM
Deltoid muscle
Shoulder joint
+y
+
0.280 m
0.620 m
Axis M
0.150 m
M
13.0°
a
d
M
+x
WdWa
Sx
Sy
Free-body diagram of the arm
Wa Wd
ℓ
ℓ
ℓ
13.0°
( )a
( )b
( )c
Dumbbell
FIGURE 9.8 (a) The fully extended, horizontal arm of a bodybuilder supports a dumbbell. (b) The free-body diagram for the arm. (c) Three of the forces that act on the arm and their lever arms. The axis of rotation at the left end of the arm is perpendicular to the page. Force vectors are not to scale.
9.3 Center of Gravity 231
F2FF
2F
F
2F F F
F
B CA
CYU FIGURE 9.3
F1
F2
F3
CYU FIGURE 9.4
9.3 Center of Gravity Often, it is important to know the torque produced by the weight of an extended body. In Examples 4 and 5, for instance, it is necessary to determine the torques caused by the weight
of the ladder and the arm, respectively. In both cases the weight is considered to act at a defi -
nite point for the purpose of calculating the torque. This point is called the center of gravity (abbreviated “cg”).
DEFINITION OF CENTER OF GRAVITY The center of gravity of a rigid body is the point at which its weight can be considered to act when the torque due to the weight is being calculated.
When an object has a symmetrical shape and its weight is distributed uniformly, the center
of gravity lies at its geometrical center. For instance, Figure 9.9 shows a thin, uniform, horizontal rod of length L attached to a vertical wall by a hinge. The center of gravity of the rod is located at the geometrical center. The lever arm for the weight W→ is L/2, and the magnitude of the torque is W(L/2). In a similar fashion, the center of gravity of any symmetrically shaped and uniform object, such as a sphere, disk, cube, or cylinder, is located at its geometrical center. However, this
does not mean that the center of gravity must lie within the object itself. The center of gravity of
a compact disc recording, for instance, lies at the center of the hole in the disc and is, therefore,
“outside” the object.
Suppose we have a group of objects, with known weights and centers of gravity, and it is
necessary to know the center of gravity for the group as a whole. As an example, Figure 9.10a shows a group composed of two parts: a horizontal uniform board (weight W1
→ ) and a uniform
box (weight W2 →
) near the left end of the board. The center of gravity can be determined by
calculating the net torque created by the board and box about an axis that is picked arbitrarily
to be at the right end of the board. Part a of the fi gure shows the weights W1 →
and W2 →
and their
corresponding lever arms x1 and x2. The net torque is Στ = W1x1 + W2 x2. It is also possible to calculate the net torque by treating the total weight W1
→ + W2
→ as if it were located at the center
of gravity and had the lever arm xcg, as part b of the drawing indicates: Στ = (W1 + W2 )xcg . The two values for the net torque must be the same, so that
W1 x1 + W2 x2 = (W1 + W2) xcg
This expression can be solved for xcg, which locates the center of gravity relative to the axis:
Center of gravity xcg =
W1x1 + W2 x2 + ⋅ ⋅ ⋅ W1 + W2 + ⋅ ⋅ ⋅
(9.3)
The notation “+ ⋅ ⋅ ⋅ ” indicates that Equation 9.3 can be extended to account for any number
of weights distributed along a horizontal line. Figure 9.10c illustrates that the group can be balanced by a single external force (due to the index fi nger), if the line of action of the force
passes through the center of gravity, and if the force is equal in magnitude, but opposite in direc-
tion, to the weight of the group. Example 6 demonstrates how to calculate the center of gravity
for the human arm.
W
Hinge (axis)
Center of gravity 1 2 – L
FIGURE 9.9 A thin, uniform, horizontal rod of length L is attached to a vertical wall by a hinge. The center of gravity of the rod is at its
geometrical center.
FIGURE 9.10 (a) A box rests near the left end of a horizontal board. (b) The total weight (W1
→ + W2
→ ) acts at the center of
gravity of the group. (c) The group can be balanced by applying an external force (due
to the index fi nger) at the center of gravity.
Axis
cg
x2
x1
W2
W1
xcg
cg
W1 + W2
( )a
( )b
( )c
232 CHAPTER 9 Rotational Dynamics
The center of gravity plays an important role in determining whether a group of objects
remains in equilibrium as the weight distribution within the group changes. A change in the
weight distribution causes a change in the position of the center of gravity, and if the change is
too great, the group will not remain in equilibrium. Conceptual Example 7 discusses a shift in the
center of gravity that led to an embarrassing result.
EXAMPLE 6 The Center of Gravity of an Arm
The horizontal arm illustrated in Figure 9.11 is composed of three parts: the upper arm (weight W1 = 17 N), the lower arm (W2 = 11 N), and the hand (W3 = 4.2 N). The drawing shows the center of gravity of each part, measured with respect to the shoulder joint. Find the center of gravity of
the entire arm, relative to the shoulder joint.
Reasoning and Solution The coordinate xcg of the center of gravity is given by
xcg = W1x1 + W2 x2 + W3 x3
W1 + W2 + W3 (9.3)
= (17 N)(0.13 m) + (11 N)(0.38 m) + (4.2 N)(0.61 m)
17 N + 11 N + 4.2 N = 0.28 m
0.61 m
Upper arm Lower arm Hand
W2
W3
W1
0.13 m Shoulder
joint
0.38 m
HandLower armUpper arm
FIGURE 9.11 The three parts of a human arm, and the
weight and center of gravity
for each.
FIGURE 9.12 (a) This stationary cargo plane is sitting on its tail at Los Angeles International Airport, after being overloaded toward the rear. (b) In a correctly loaded plane, the center of gravity is between the front and the rear landing gears. (c) When the plane is overloaded toward the rear, the center of gravity shifts behind the rear landing gear, and the accident in part a occurs.
(b) (c)
W
FN1
FN2
Axis
cg
W
FN2
Axis
cg
(a)
© A
P /W
id e
W o rl
d P
h o to
s
CONCEPTUAL EXAMPLE 7 Overloading a Cargo Plane
Figure 9.12a shows a stationary cargo plane with its front landing gear 9 meters off the ground. This accident occurred because the plane was
overloaded toward the rear. How did a shift in the center of gravity of the
loaded plane cause the accident?
Reasoning and Solution Figure 9.12b shows a drawing of a correctly loaded plane, with the center of gravity located between the front and the
rear landing gears. The weight W→ of the plane and cargo acts downward at the center of gravity, and the normal forces FN1
→ and FN2
→ act upward at
9.3 Center of Gravity 233
As we have seen in Example 7, the center of gravity plays an important role in the equilib-
rium orientation of airplanes. It also plays a similar role in the design of vehicles that can be
safely driven with minimal risk to the passengers. Example 8 discusses this role in the context of
sport utility vehicles.
any clockwise torque. Due to the unbalanced counterclockwise torque, the
plane rotates until its tail hits the ground, which applies an upward force to
the tail. The clockwise torque due to this upward force balances the coun-
terclockwise torque due to W→, and the plane comes again into an equilib- rium state, this time with the front landing gear 9 meters off the ground.
Related Homework: Problems 14, 19, 72
the front and at the rear landing gear, respectively. With respect to an axis
at the rear landing gear, the counterclockwise torque due to FN1 →
balances
the clockwise torque due to W→, and the plane remains in equilibrium. Figure 9.12c shows the plane with too much cargo loaded toward the rear, just after the plane has begun to rotate counterclockwise. Because of the
overloading, the center of gravity has shifted behind the rear landing gear.
The torque due to W→ is now counterclockwise and is not balanced by
Analyzing Multiple-Concept Problems
EXAMPLE 8 The Physics of the Static Stability Factor and Rollover
Figure 9.13a shows a sport utility vehicle (SUV) that is moving away from you and negotiating a horizontal turn. The radius of the turn is 16 m,
and its center is on the right in the drawing. The center of gravity of the
vehicle is 0.94 m above the ground and, as an approximation, is assumed
to be located midway between the wheels on the left and right sides. The
separation between these wheels is the track width and is 1.7 m. What is
the greatest speed at which the SUV can negotiate the turn without roll-
ing over?
d
r
cg Center of turnh
(a)
FN
fs
cg
(b) Free-body diagram for SUV
mg fs
cg
(c) Lever arms
ℓs = h
ℓN = d 1 2–
FN
FIGURE 9.13 (a) A sport utility vehicle (SUV) is shown moving away from you, following a road curving to the right. The radius of the turn is r. The SUV’s center of gravity ( ) is located at a height h above the ground, and its wheels are separated by a distance d. (b) This free-body diagram shows the SUV at the instant just before rollover toward the outside of the turn begins. The forces acting on it are its weight mg→, the total normal force FN
→ (acting only on the left-side tires), and the total force of static friction fs
→ (also
acting only on the left-side tires). (c) The lever arms ℓN (for FN →
) and ℓs (for fs →
) are for an axis passing through the center of gravity
and perpendicular to the page.
d
r
cg Center of turnh
(a)
FN
fs
cg
(b) Free-body diagram for SUV
mg fs
cg
(c) Lever arms
ℓs = h
ℓN = d 1 2–
FN
FIGURE 9.13 (REPEATED) (a) A sport utility vehicle (SUV) is shown moving away from you, following a road curving to the right. The radius of the turn is r. The SUV’s center of gravity ( ) is located at a height h above the ground, and its wheels are separated by a distance d. (b) This free-body diagram shows the SUV at the instant just before rollover toward the outside of the turn begins. The forces acting on it are its weight mg→, the total normal force FN
→ (acting only on the left-side tires), and the total
force of static friction fs →
(also acting only on the left-side tires). (c) The lever arms ℓN (for FN →
) and ℓs (for fs →
) are for an axis passing
through the center of gravity and perpendicular to the page.
234 CHAPTER 9 Rotational Dynamics
Modeling the Problem
STEP 1 Speed and Centripetal Force According to Equation 5.3, the magnitude of the cen- tripetal force (provided solely by the static frictional force of magnitude fs) is related to the speed 𝜐 of the car by
Fc = fs = mυ2
r Solving for the speed gives Equation 1 at the right. To use this result, we must have a value for
fs, which we obtain in Step 2.
STEP 2 Torques Figure 9.13b shows the free-body diagram for the SUV at the instant just before rollover begins, when the total normal force FN
→ and the total static frictional force
fs →
are acting only on the left-side wheels, the right-side wheels having just lost contact with the
ground. At this moment, the sum of the torques due to these two forces is zero for an axis through
the center of gravity and perpendicular to the page. Each torque has a magnitude given by Equa-
tion 9.1 as the magnitude of the force times the lever arm for the force, and part c of the drawing shows the lever arms. No lever arm is shown for the weight, because it passes through the axis
and, therefore, contributes no torque. The force fs →
produces a positive torque, since it causes a
counterclockwise rotation about the chosen axis, while the force FN →
produces a negative torque,
since it causes a clockwise rotation. Thus, we have
fsℓs − FN ℓN = 0 or fs = FNℓN
ℓs =
FNd 2h
This result for f s can be substituted into Equation 1, as illustrated at the right. We now proceed to Step 3, to obtain a value for FN.
STEP 3 The Normal Force The SUV does not accelerate in the vertical direction, so the normal force must balance the car’s weight mg, or
FN = mg
The substitution of this result into Equation 2 is shown at the right.
Solution The results of each step can be combined algebraically to show that
υ = √r fsm = √ rFNd 2hm
= √rmgd2hm The fi nal expression is independent of the mass of the SUV, since m has been eliminated algebra- ically. The greatest speed at which the SUV can negotiate the turn without rolling over is
υ = √rg( d 2h) = √(16 m)(9.80 m/s2)[
1.7 m
2(0.94 m) ] = 12 m/s
STEP 1 STEP 2 STEP 3
{
SSF
υ = √rfsm (1) ?
υ = √rfsm (1) fs =
FNd 2h
(2)
?
υ = √rfsm (1) fs =
FNd 2h
(2)
FN = mg
Description Symbol Value Comment Radius of turn r 16 m
Location of center of gravity h 0.94 m Height above ground.
Track width d 1.7 m Distance between left- and right-side wheels.
Unknown Variable Speed of SUV 𝜐 ?
Reasoning The free-body diagram in Figure 9.13b shows the SUV at the instant just before it begins to roll over toward the outside of the turn,
which is on the left side of the drawing. At this moment the right-side
wheels have just lost contact with the ground, so no forces are acting on
them. The forces acting on the SUV are its weight mg→, the total normal force FN
→ (acting only on the left-side tires), and the total force of static
friction fs →
(also acting only on the left-side tires). Since the SUV is mov-
ing around the turn, it has a centripetal acceleration and must be experi-
encing a centripetal force. The static frictional force fs →
alone provides the
centripetal force. The speed 𝜐 at which the SUV (mass m) negotiates the turn of radius r is related to the magnitude Fc of the centripetal force by Fc = m𝜐2/r (Equation 5.3). After applying this relation, we will consider rollover by analyzing the torques acting on the SUV with respect to an
axis through the center of gravity and perpendicular to the drawing. The
normal force FN →
will play a role in this analysis, and it will be evaluated
by using the fact that it must balance the weight of the vehicle.
Knowns and Unknowns We are given the following data:
9.3 Center of Gravity 235
At this speed, the SUV will negotiate the turn just on the verge of rolling over. In the fi nal result
and beneath the term d 2h
, we have included the label SSF, which stands for static stability factor.
The SSF provides one measure of how susceptible a vehicle is to rollover. Higher values of the
SSF are better, because they lead to larger values for 𝜐, the greatest speed at which the vehicle can
negotiate a turn without rolling over. Note that greater values for the track width d (more widely separated wheels) and smaller values for the height h (center of gravity closer to the ground) lead to higher values of the SSF. A Formula One racing car, for example, with its low center of gravity
and large track width, is much less prone to rolling over than is an SUV, when both are driven at
the same speed around the same curve.
Related Homework: Problem 17
The center of gravity of an object with an irregular shape and a nonuniform weight distribu-
tion can be found by suspending the object from two diff erent points P1 and P2, one at a time. Figure 9.14a shows the object at the moment of release, when its weight W→, acting at the center of gravity, has a nonzero lever arm ℓ relative to the axis shown in the drawing. At this instant the weight produces a torque about the axis. The tension force T→ applied to the object by the suspension cord produces no torque because its line of action passes through the axis. Hence, in
part a there is a net torque applied to the object, and the object begins to rotate. Friction eventu- ally brings the object to rest as in part b, where the center of gravity lies directly below the point of suspension. In such an orientation, the line of action of the weight passes through the axis,
so there is no longer any net torque. In the absence of a net torque the object remains at rest. By
suspending the object from a second point P2 (see Figure 9.14c), a second line through the object can be established, along which the center of gravity must also lie. The center of gravity, then,
must be at the intersection of the two lines.
The center of gravity is closely related to the center-of-mass concept discussed in Section 7.5.
To see why they are related, let’s replace each occurrence of the weight in Equation 9.3 by
W = mg, where m is the mass of a given object and g is the magnitude of the acceleration due to gravity at the location of the object. Suppose that g has the same value everywhere the objects are located. Then it can be algebraically eliminated from each term on the right side of
Equation 9.3. The resulting equation, which contains only masses and distances, is the same
as Equation 7.10, which defi nes the location of the center of mass. Thus, the two points are
identical. For ordinary-sized objects, like cars and boats, the center of gravity coincides with
the center of mass.
Check Your Understanding
(The answers are given at the end of the book.) 7. Starting in the spring, fruit begins to grow on the outer
end of a branch on a pear tree. As the fruit grows, does the
center of gravity of the pear-growing branch (a) move toward the pears at the end of the branch, (b) move away from the pears, or (c) not move at all?
8. CYU Figure 9.5 shows a wine rack for a single bottle of wine that seems to defy common sense as it balances on
a tabletop. Where is the center of gravity of the combined
wine rack and bottle of wine located? (a) At the neck of the bottle where it passes through the wine rack (b) Directly above the point where the wine rack touches the tabletop (c) At a location to the right of where the wine rack touches the tabletop
9. Bob and Bill have the same weight and wear identical shoes. When they both keep their feet fl at on the fl oor and their bodies straight, Bob can lean forward farther than Bill can before falling. Other things
being equal, whose center of gravity is closer to the ground when both are standing erect?
P1
P1
P1
P2
cg
cg
W
W
cg
W
T
Axis Lever arm = ℓ
(b)
(a)
(c)
FIGURE 9.14 The center of gravity (cg) of an object can be located by suspending the
object from two diff erent points, P1 and P2, one at a time.
Rack is not attached to the tabletop.
Wine rack
CYU FIGURE 9.5
236 CHAPTER 9 Rotational Dynamics
9.4 Newton’s Second Law for Rotational Motion About a Fixed Axis The goal of this section is to put Newton’s second law into a form suitable for describing
the rotational motion of a rigid object about a fi xed axis. We begin by considering a particle
moving on a circular path. Figure 9.15 presents a good approximation of this situation by using a small model plane on a guideline of negligible mass. The plane’s engine produces a
net external tangential force FT that gives the plane a tangential acceleration aT. In accord with Newton’s second law, it follows that FT = maT. The torque 𝜏 produced by this force is 𝜏 = FTr, where the radius r of the circular path is also the lever arm. As a result, the torque is 𝜏 = maTr. However, the tangential acceleration is related to the angular acceleration 𝛼 according to
aT = r𝛼 (Equation 8.10), where 𝛼 must be expressed in rad/s2. With this substitution for aT, the torque becomes
τ = (mr 2)α (9.4)
Equation 9.4 is the form of Newton’s second law we have been seeking. It indicates that the
net external torque 𝜏 is directly proportional to the angular acceleration 𝛼. The constant of pro-
portionality is I = mr2, which is called the moment of inertia of the particle. The SI unit for moment of inertia is kg · m2.
If all objects were single particles, it would be just as convenient to use the second law
in the form FT = maT as in the form 𝜏 = I𝛼. The advantage in using 𝜏 = I𝛼 is that it can be applied to any rigid body rotating about a fi xed axis, and not just to a particle. To illustrate
how this advantage arises, Figure 9.16a shows a fl at sheet of material that rotates about an axis perpendicular to the sheet. The sheet is composed of a number of mass particles, m1, m2, . . . , mN, where N is very large. Only four particles are shown for the sake of clarity. Each particle behaves in the same way as the model airplane in Figure 9.15 and obeys the relation 𝜏 = (mr2)𝛼:
τ1 = (m1r1 2 )α τ2 = (m2r2 2 )α
⋅
⋅
⋅
τN = (mNrN 2 )α
In these equations each particle has the same angular acceleration 𝛼, since the rotating object is
assumed to be rigid. Adding together the N equations and factoring out the common value of 𝛼, we fi nd that
Στ = (Σmr 2)α (9.5)
{
Moment
of inertia I
{
Moment
of inertia
Net
external torque
{
FIGURE 9.15 A model airplane on a guide- line has a mass m and is fl ying on a circle of radius r (top view). A net tangential force FT
→ acts on the plane.
FT
r 90°
(b)
Axis
f43
f34
f34 = – f43
Internal forces
m4 m3
Axis
m4 m3
m1
m2r2
r1
(a)
FIGURE 9.16 (a) A rigid body consists of a large number of particles, four of which are
shown. (b) The internal forces that particles 3 and 4 exert on each other obey Newton’s law
of action and reaction.
9.4 Newton’s Second Law for Rotational Motion About a Fixed Axis 237
where the expression Στ = τ1 + τ2 + ⋅ ⋅ ⋅ + τN is the sum of the external torques, and Σmr 2 = m1 r1 2 + m2 r2 2 + ⋅ ⋅ ⋅ + mN rN 2 represents the sum of the individual moments of inertia. The latter quantity is the moment of inertia I of the body:
Moment of inertia of a body I = m1r1
2 + m2r22 + . . . + mN rN2 = Σmr 2 (9.6)
In this equation, r is the perpendicular radial distance of each particle from the axis of rotation. Combining Equation 9.6 with Equation 9.5 gives the following result:
ROTATIONAL ANALOG OF NEWTON’S SECOND LAW FOR A RIGID BODY ROTATING ABOUT A FIXED AXIS
Net external torque = ( ) × ( ) Στ = Iα (9.7)
Requirement: α must be expressed in rad/s2.
The version of Newton’s second law given in Equation 9.7 applies only for rigid bodies. The
word “rigid” means that the distances r1, r2, r3, etc. that locate each particle m1, m2, m3, etc. (see Figure 9.16a) do not change during the rotational motion. In other words, a rigid body is one that does not change its shape while undergoing an angular acceleration in response to an applied net
external torque.
The form of the second law for rotational motion, Στ = Iα, is similar to the equation for translational (linear) motion, ΣF = ma, and is valid only in an inertial frame. The moment of inertia I plays the same role for rotational motion that the mass m does for translational motion. Thus, I is a measure of the rotational inertia of a body. When using Equation 9.7, 𝛼 must be expressed in rad/s2, because the relation aT = r𝛼 (which requires radian measure) was used in the derivation.
When calculating the sum of torques in Equation 9.7, it is necessary to include only the
external torques, those applied by agents outside the body. The torques produced by inter- nal forces need not be considered, because they always combine to produce a net torque of
zero. Internal forces are those that one particle within the body exerts on another particle.
They always occur in pairs of oppositely directed forces of equal magnitude, in accord with
Newton’s third law (see m3 and m4 in Figure 9.16b). The forces in such a pair have the same line of action, so they have identical lever arms and produce torques of equal magnitudes.
One torque is counterclockwise, while the other is clockwise, the net torque from the pair
being zero.
It can be seen from Equation 9.6 that the moment of inertia depends on both the mass of
each particle and its distance from the axis of rotation. The farther a particle is from the axis, the
greater is its contribution to the moment of inertia. Therefore, although a rigid object possesses
a unique total mass, it does not have a unique moment of inertia, as indicated by Example 9.
This example shows how the moment of inertia can change when the axis of rotation changes.
The procedure illustrated in Example 9 can be extended using integral calculus to evaluate the
moment of inertia of a rigid object with a continuous mass distribution, and Table 9.1 gives some typical results. These results depend on the total mass of the object, its shape, and the location
and orientation of the axis.
When forces act on a rigid object, they can aff ect its motion in two ways. They can produce
a translational acceleration a (components ax and ay). The forces can also produce torques, which can cause the object to have an angular acceleration 𝛼. In general, we can deal with the resulting
combined motion by using Newton’s second law. For the translational motion, we use the law in
the form ΣF = ma. For the rotational motion of a rigid object about a fi xed axis, we use the law in the form Σ𝜏 = I𝛼. When a (both components) and 𝛼 are zero, there is no acceleration of any kind, and the object is in equilibrium. This is the situation already discussed in Section 9.2. If any
component of a is nonzero or if 𝛼 is nonzero, we have accelerated motion, and the object is not in equilibrium. Examples 10 and 11 deal with this type of situation.
Moment of
inertia
Angular
acceleration
Thin-walled hollow cylinder or hoop
Solid cylinder or disk
Thin rod, axis perpendicular to rod and passing through center
Thin rod, axis perpendicular to rod and passing through one end
Solid sphere, axis through center
Solid sphere, axis tangent to surface
Thin-walled spherical shell, axis through center
Thin rectangular sheet, axis parallel to one edge and passing through center of other edge
Thin rectangular sheet, axis along one edge
I = MR225–
I = MR275–
I = MR223–
I = ML2112––
I = ML2112––
I = MR212–
I = MR2
R
R
R
L
L
L
L
R
I = ML21 3–
I = ML21 3–
R
TABLE 9.1 Moments of Inertia I for Various Rigid Objects of Mass M
238 CHAPTER 9 Rotational Dynamics
EXAMPLE 9 The Moment of Inertia Depends on Where the Axis Is
Two particles each have a mass M and are fi xed to the ends of a thin rigid rod, whose mass can be ignored. The length of the rod is L. Find the moment of inertia when this object rotates relative to an axis that is per-
pendicular to the rod at (a) one end and (b) the center. (See Interactive Figure 9.17.)
Reasoning When the axis of rotation changes, the distance r between the axis and each particle changes. In determining the moment of inertia
using I = ∑mr 2, we must be careful to use the distances that apply for each axis.
Problem-Solving Insight The moment of inertia depends on the location and orientation of the axis relative to the particles that make up the object.
Solution (a) Particle 1 lies on the axis, as part a of the drawing shows, and has a zero radial distance: r1 = 0. In contrast, particle 2 moves on a circle whose radius is r2 = L. Noting that m1 = m2 = M, we fi nd that the moment of inertia is
I = Σmr 2 = m1 r1 2 + m2 r2 2 = M(0)2 + M(L)2 = ML2 (9.6)
INTERACTIVE FIGURE 9.17 Two particles, masses m1 and m2, are attached to the ends of a massless rigid rod. The
moment of inertia of this object
is diff erent, depending on
whether the rod rotates about
an axis through (a) the end or (b) the center of the rod.
Axis
(a)
(b)
Axis
m1 m2 m2m1 r1 r2r2
(b) Part b of the drawing shows that particle 1 no longer lies on the axis but now moves on a circle of radius r1 = L/2. Particle 2 moves on a circle with the same radius, r2 = L/2. Therefore,
I = Σmr 2 = m1 r1 2 + m2 r2 2 = M(L /2) 2 + M(L /2) 2 = 12 ML2
This value diff ers from the value in part (a) because the axis of rotation
is diff erent, and the distances of the particles from the axis are diff erent.
Analyzing Multiple-Concept Problems
EXAMPLE 10 The Torque of an Electric Saw Motor
The motor in an electric saw brings the circular blade from rest up to the
rated angular velocity of 80.0 rev/s in 240.0 rev. One type of blade has a
moment of inertia of 1.41 × 10−3 kg · m2. What net torque (assumed con- stant) must the motor apply to the blade?
Reasoning Newton’s second law for rotational motion, Σ𝜏 = I𝛼 (Equa- tion 9.7), can be used to fi nd the net torque Σ𝜏. However, when using the
second law, we will need a value for the angular acceleration 𝛼, which can
be obtained by using one of the equations of rotational kinematics. In addi-
tion, we must remember that the value for 𝛼 must be expressed in rad/s2,
not rev/s2, because Equation 9.7 requires radian measure.
Knowns and Unknowns The given data are summarized in the following table:
Description Symbol Value Comment Explicit Data Final angular velocity 𝜔 80.0 rev/s Must be converted to rad/s.
Angular displacement θ 240.0 rev Must be converted to rad.
Moment of inertia I 1.41 × 10−3 kg · m2
Implicit Data Initial angular velocity 𝜔0 0 rad/s Blade starts from rest.
Unknown Variable Net torque applied to blade Σ𝜏 ?
Modeling the Problem
STEP 1 Newton’s Second Law for Rotation Newton’s second law for rotation (Equation 9.7) specifi es the net torque Στ applied to the blade in terms of the blade’s moment of inertia I and angular acceleration α. In Step 2, we will obtain the value for α that is needed in Equation 9.7.
Στ = Iα (9.7)
?
9.4 Newton’s Second Law for Rotational Motion About a Fixed Axis 239
BIO THE PHYSICS OF . . . wheelchairs. To accelerate a wheelchair, the rider applies a force to a handrail on each wheel. The magnitude of the torque generated by the force is
the product of the force-magnitude and the lever arm. As Figure 9.18 illustrates, the lever arm is the radius of the circular rail, which is designed to be as large as possible. Thus, a relatively large
torque can be generated for a given force, allowing for rapid acceleration.
Example 10 shows how Newton’s second law for rotational motion is used when design con-
siderations demand an adequately large angular acceleration. There are also situations in which
it is desirable to have as little angular acceleration as possible, and Conceptual Example 11 deals
with one of them.
STEP 2 Rotational Kinematics As the data table indicates, we have data for the angular displacement θ, the fi nal angular velocity 𝜔, and the initial angular velocity 𝜔0. With these data, Equation 8.8 from the equations of rotational kinematics can be used to determine the angular
acceleration 𝛼:
ω2 = ω 20 + 2αθ (8.8)
Solving for 𝛼 gives
α = ω2 − ω 20
2θ
which can be substituted into Equation 9.7, as shown at the right.
Solution The results of each step can be combined algebraically to show that
Σ𝜏 = I𝛼 = I ( ω2 − ω 20
2θ ) In this result for Σ𝜏, we must use radian measure for the variables ω, ω0, and θ. To convert from revolutions (rev) to radians (rad), we will use the fact that 1 rev = 2π rad. Thus, the net torque applied by the motor to the blade is
Στ = I( ω2 − ω 20
2θ )
= (1.41 × 10−3 kg · m2 ) {[( 80.0
rev
s )( 2π rad 1 rev )]
2
− (0 rad /s)2
2(240.0 rev) (2π rad1 rev ) } = 0.118 N · m Related Homework: Problems 31, 35, 37, 40
STEP 1 STEP 2
Στ = Iα (9.7)
α = ω2 − ω 20
2θ
F
FIGURE 9.18 A rider applies a force F →
to the circular handrail. The magnitude of the torque produced by
this force is the product of the force-magnitude and the lever arm ℓ about the axis of rotation.
Ja ck
ie J
o h n st
o n /©
A P
/W id
e W
o rl
d P
h o to
s
240 CHAPTER 9 Rotational Dynamics
CONCEPTUAL EXAMPLE 11 The Physics of Archery and Bow Stabilizers
Archers can shoot with amazing accuracy, especially using modern bows
such as the one in Figure 9.19. Notice the bow stabilizer, a long, thin rod that extends from the front of the bow and has a relatively massive cylin-
der at the tip. Advertisements claim that the stabilizer helps to steady the
archer’s aim. Which of the following explains why this is true? The addi-
tion of the stabilizer (a) decreases the bow’s moment of inertia, making it easier for the archer to hold the bow steady; (b) has nothing to do with the bow’s moment of inertia; (c) increases the bow’s moment of inertia, making it easier for the archer to hold the bow steady.
Reasoning An axis of rotation (the black dot) has been added to Figure 9.19. This axis passes through the archer’s left shoulder and is perpendicular to the plane of the paper. Any angular acceleration of the
archer’s body about this axis will lead to a rotation of the bow and, thus,
will degrade the archer’s aim. The angular acceleration will depend on
any unbalanced torques that occur while the archer’s tensed muscles try to
hold the drawn bow, as well as the bow’s moment of inertia.
Answers (a) and (b) are incorrect. Adding a stabilizer to the bow increases its mass. According to the defi nition of the moment of inertia
of a body (Equation 9.6), the increase in mass leads to an increase in the
bow’s moment of inertia.
Answer (c) is correct. Newton’s second law for rotational motion states that the angular acceleration 𝛼 of the bow is given by α = (Στ) /I (Equa- tion 9.7), where Σ𝜏 is the net torque acting on the bow and I is its moment of inertia. The stabilizer increases I, especially the relatively massive cylinder at the tip, since it is so far from the axis. Note that the moment of
inertia is in the denominator on the right side of this equation. Therefore,
to the extent that I is larger, a given net torque Σ𝜏 will create a smaller angular acceleration and, hence, less disturbance of the aim.
Tip of stabilizer
Unwanted rotation
Axis
FIGURE 9.19 The long, thin rod extending from the front of the bow is a stabilizer. The stabilizer helps to steady the archer’s aim, as Conceptual Example 11 discusses.
D av
id M
ad is
o n /G
et ty
I m
ag es
We have seen that Newton’s second law for rotational motion, Στ = Iα, has the same form as the law for translational motion, ΣF = ma, so each rotational variable has a translational analog: torque 𝜏 and force F are analogous quantities, as are moment of inertia I and mass m, and angu- lar acceleration 𝛼 and linear acceleration a. The other physical concepts developed for studying translational motion, such as kinetic energy and momentum, also have rotational analogs. For
future reference, Table 9.2 itemizes these concepts and their rotational analogs.
Check Your Understanding
(The answers are given at the end of the book.) 10. Three massless rods (A, B, and C) are free to rotate about an axis at their left end (see CYU Figure 9.6).
The same force F→ is applied to the right end of each rod. Objects with diff erent masses are attached to the rods, but the total mass (3m) of the objects is the same for each rod. Rank the angular acceleration of the rods, largest to smallest.
9.5 Rotational Work and Energy 241
11. A fl at triangular sheet of uniform material is shown in CYU Figure 9.7. There are three possible axes of rotation, each perpen-
dicular to the sheet and passing through one
corner, A, B, or C. For which axis is the
greatest net external torque required to
bring the triangle up to an angular speed
of 10.0 rad/s in 10.0 s, starting from rest?
Assume that the net torque is kept constant
while it is being applied.
12. At a given instant an object has an angular velocity. It also has an angular acceleration
due to torques that are present. Therefore,
the angular velocity is changing. Does the
angular velocity at this instant increase,
decrease, or remain the same (a) if addition- al torques are applied so as to make the net
torque suddenly equal to zero and (b) if all the torques are suddenly removed?
13. The space probe in CYU Figure 9.8 is ini- tially moving with a constant translational
velocity and zero angular velocity. (a) When the two engines are fi red, each generating a thrust of mag- nitude T, does the translational velocity increase, decrease, or remain the same? (b) Does the angular velocity increase, decrease, or remain the same?
A
CB
CYU FIGURE 9.7
−T
T
CYU FIGURE 9.8
9.5 Rotational Work and Energy Work and energy are among the most fundamental and useful concepts in physics. Chapter 6
discusses their application to translational motion. These concepts are equally useful for rota-
tional motion, provided they are expressed in terms of angular variables.
TABLE 9.2 Analogies Between Rotational and Translational Concepts
Physical Concept Rotational Translational Displacement 𝜃 s
Velocity 𝜔 𝜐
Acceleration 𝛼 a
The cause of acceleration Torque 𝜏 Force F
Inertia Moment of inertia I Mass m
Newton’s second law Στ = Iα Σ F = ma
Work τθ Fs
Kinetic energy 1 2 Iω 2
1
2 mυ2
Momentum L = Iω p = mυ
F
Rod (overhead view) F
Axis (perpendicular
to page)
A
F
B
C
m m m
m2m
3m
CYU FIGURE 9.6
242 CHAPTER 9 Rotational Dynamics
The work W done by a constant force that points in the same direction as the displacement is W = Fs (Equation 6.1), where F and s are the magnitudes of the force and the displace- ment, respectively. To see how this expression can be rewritten using angular variables, consider
Figure 9.20. Here a rope is wrapped around a wheel and is under a constant tension F. If the rope is pulled out a distance s, the wheel rotates through an angle 𝜃 = s/r (Equation 8.1), where r is the radius of the wheel and 𝜃 is in radians. Thus, s = r𝜃, and the work done by the tension force in turning the wheel is W = Fs = Fr𝜃. However, Fr is the torque 𝜏 applied to the wheel by the tension, so the rotational work can be written as follows:
DEFINITION OF ROTATIONAL WORK The rotational work WR done by a constant torque 𝞽 in turning an object through an angle 𝞱 is
WR = τθ (9.8)
Requirement: 𝞱 must be expressed in radians. SI Unit of Rotational Work: joule (J)
Section 6.2 discusses the work–energy theorem and kinetic energy. There we saw that the
work done on an object by a net external force causes the translational kinetic energy ( 1
2mυ 2) of the object to change. In an analogous manner, the rotational work done by a net external torque
causes the rotational kinetic energy to change. A rotating body possesses kinetic energy, because
its constituent particles are moving. If the body is rotating with an angular speed 𝜔, the tangential speed 𝜐T of a particle at a distance r from the axis is 𝜐T = r𝜔 (Equation 8.9). Figure 9.21 shows two such particles. If a particle’s mass is m, its kinetic energy is 12mυ 2T =
1
2mr 2ω2. The kinetic energy of the entire rotating body, then, is the sum of the kinetic energies of the particles:
Rotational KE = Σ ( 1
2 mr 2ω2) = 1
2 (Σmr2)ω2
In this result, the angular speed 𝜔 is the same for all particles in a rigid body and, therefore, has been factored outside the summation. According to Equation 9.6, the term in parentheses is the
moment of inertia, I = Σmr 2, so the rotational kinetic energy takes the following form:
DEFINITION OF ROTATIONAL KINETIC ENERGY The rotational kinetic energy KER of a rigid object rotating with an angular speed ω about a fi xed axis and having a moment of inertia I is
KER = 1
2 Iω2 (9.9)
Requirement: ω must be expressed in rad/s. SI Unit of Rotational Kinetic Energy: joule (J)
Kinetic energy is one part of an object’s total mechanical energy. The total mechanical
energy is the sum of the kinetic and potential energies and obeys the principle of conservation
of mechanical energy (see Section 6.5). Specifi cally, we need to remember that translational and
rotational motion can occur simultaneously. When a bicycle coasts down a hill, for instance, its
tires are both translating and rotating. An object such as a rolling bicycle tire has both transla-
tional and rotational kinetic energies, so that the total mechanical energy is
E = 12 mυ 2 + 1
2 Iω2 + mgh
Here m is the mass of the object, 𝜐 is the translational speed of its center of mass, I is its moment of inertia about an axis through the center of mass, 𝜔 is its angular speed, and h is the height of the object’s center of mass relative to an arbitrary zero level. Mechanical energy is conserved if
Wnc, the net work done by external nonconservative forces and external torques, is zero. If the total mechanical energy is conserved as an object moves, its fi nal total mechanical energy Ef equals its initial total mechanical energy E0: Ef = E0.
{
Moment of
inertia, I
{
Total
mechanical
energy
{
Translational
kinetic energy
{
Rotational
kinetic energy
{
Gravitational
potential energy
FIGURE 9.20 The force F→ does work in rotating the wheel through the angle 𝜃.
F
Axis of rotation
r
Rope
θ
s
m
r1
r2
FIGURE 9.21 The rotating wheel is composed of many particles, two of which
are shown.
9.5 Rotational Work and Energy 243
Example 12 illustrates the eff ect of combined translational and rotational motion in the con-
text of how the total mechanical energy of a cylinder is conserved as it rolls down an incline.
Zero level hf = 0 m
Hollow cylinder
Solid cylinder
h0
FIGURE 9.22 A hollow cylinder and a solid cylinder
start from rest and roll
down the incline plane. The
conservation of mechanical
energy can be used to show
that the solid cylinder, having
the greater translational speed,
reaches the bottom fi rst.
EXAMPLE 12 Rolling Cylinders
Since each cylinder rolls without slipping, the fi nal rotational speed 𝜔f and the fi nal translational speed 𝜐f of its center of mass are related by Equation 8.12, 𝜔f = 𝜐f/r, where r is the radius of the cylinder. Substituting this expres- sion for 𝜔f into the energy-conservation equation and solving for 𝜐f yields
υf = √ 2mgh0
m + I r 2
Setting m = mh, r = rh, and I = mr 2h for the hollow cylinder and then set- ting m = ms, r = rs, and I =
1
2mr 2s for the solid cylinder (see Table 9.1), we fi nd that the two cylinders have the following translational speeds at
the bottom of the incline:
Hollow cylinder υf = √gh0
Solid cylinder υf = √4gh03 = 1.15 √gh0 The solid cylinder has the greater translational speed at the bottom and,
thus, arrives there fi rst.
Check Your Understanding
(The answers are given at the end of the book.) 14. Two uniform solid balls are placed side by side at the top of an incline plane and, starting from rest, are
allowed to roll down the incline. Which ball, if either, has the greater translational speed at the bottom
if (a) they have the same radii, but one is more massive than the other and (b) they have the same mass, but one has a larger radius?
(Continued)
Math Skills To obtain the desired expression for the translational speed 𝜐f, we proceed as follows. The energy-conservation equation
is 1
2 mυ 2f + 1
2 Iω 2f = mgh0. Substituting ωf = υf r
(Equation 8.12) into
this equation gives
1
2 mυf2 + 1
2 I ( υf r )
2
= mgh0 or 1
2 (m + Ir 2)υf2 = mgh Multiplying both sides of the right-hand equation by 2 and dividing
both sides by m + I r 2
shows that
2 1
2 (m + I r 2)υ 2f
m + I r 2
= 2mgh
m + I r 2
or υ 2f = 2mgh
m + I r 2
Taking the square root of both sides of the right-hand equation
shows that
υf = √ 2mgh
m + I r 2
A thin-walled hollow cylinder (mass = mh, radius = rh) and a solid cylin- der (mass = ms, radius = rs) start from rest at the top of an incline (Figure 9.22). Both cylinders start at the same vertical height h0 and roll down the incline without slipping. All heights are measured relative to an arbitrarily
chosen zero level that passes through the center of mass of a cylinder
when it is at the bottom of the incline (see the drawing). Ignoring energy
losses due to retarding forces, determine which cylinder has the greatest
translational speed on reaching the bottom.
Reasoning Only the conservative force of gravity does work on the cyl- inders, so the total mechanical energy is conserved as they roll down. The
total mechanical energy E at any height h above the zero level is the sum of the translational kinetic energy (
1
2 mυ2), the rotational kinetic energy (
1
2Iω2) , and the gravitational potential energy (mgh):
E = 12 mυ2 + 1
2 Iω2 + mgh
As the cylinders roll down, potential energy is converted into kinetic energy,
but the kinetic energy is shared between the translational form ( 1
2 mυ2) and the rotational form (
1
2 Iω2). The object with more of its kinetic energy in the translational form will have the greater translational speed at the
bottom of the incline. We expect the solid cylinder to have the greater
translational speed, because more of its mass is located near the rotational
axis and, thus, possesses less rotational kinetic energy.
Solution The total mechanical energy Ef at the bottom (hf = 0 m) is the same as the total mechanical energy E0 at the top (h = h0, 𝜐0 = 0 m/s, 𝜔0 = 0 rad/s):
1
2 mυf 2 + 1
2 Iω f 2 + mghf = 1
2 mυ0 2 + 1
2 Iω0 2 + mgh0
1
2 mυf 2 + 1
2 Iω f 2 = mgh0
244 CHAPTER 9 Rotational Dynamics
15. A thin sheet of plastic is uniform and has the shape of an equilateral triangle. Consider two axes for rotation. Both are perpendicular to the plane of the triangle, axis A passing through the center of the
triangle and axis B passing through one corner. If the angular speed 𝜔 about each axis is the same, for which axis does the triangle have the greater rotational kinetic energy?
16. A hoop, a solid cylinder, a spherical shell, and a solid sphere are placed at rest at the top of an incline. All the objects have the same radius. They are then released at the same time. What is the order in
which they reach the bottom (fastest fi rst)?
9.6 Angular Momentum In Chapter 7 the linear momentum p of an object is defi ned as the product of its mass m and linear velocity 𝜐; that is, p = m𝜐. For rotational motion the analogous concept is called the angu- lar momentum L. The mathematical form of angular momentum is analogous to that of linear momentum, with the mass m and the linear velocity 𝜐 being replaced with their rotational coun- terparts, the moment of inertia I and the angular velocity 𝜔.
DEFINITION OF ANGULAR MOMENTUM The angular momentum L of a body rotating about a fi xed axis is the product of the body’s moment of inertia I and its angular velocity ω with respect to that axis:
L = Iω (9.10)
Requirement: ω must be expressed in rad/s. SI Unit of Angular Momentum: kg · m2/s
Linear momentum is an important concept in physics because the total linear momentum of
a system is conserved when the sum of the average external forces acting on the system is zero.
Then, the fi nal total linear momentum Pf and the initial total linear momentum P0 are the same: Pf = P0. In the case of angular momentum, a similar line of reasoning indicates that when the sum of the average external torques is zero, the fi nal and initial angular momenta are the same: Lf = L0, which is the principle of conservation of angular momentum.
PRINCIPLE OF CONSERVATION OF ANGULAR MOMENTUM The total angular momentum of a system remains constant (is conserved) if the net average external torque acting on the system is zero.
Example 13 illustrates an interesting consequence of the conservation of angular momentum.
(a) (b)
FIGURE 9.23 (a) A skater spins slowly on one skate, with both arms and one leg outstretched. (b) As she pulls her arms and leg in toward the rotational axis, her angular velocity 𝜔 increases.
CONCEPTUAL EXAMPLE 13 BIO The Physics of a Spinning Skater
In Figure 9.23a an ice skater is spinning with both arms and a leg out- stretched. In Figure 9.23b she pulls her arms and leg inward. As a result of this maneuver, her angular velocity 𝜔 increases dramatically. Why? Neglect any air resistance and assume that friction between her skates and
the ice is negligible. (a) A net external torque acts on the skater, causing 𝜔 to increase. (b) No net external torque acts on her; she is simply obeying the conservation of angular momentum. (c) Due to the movements of her arms and legs, a net internal torque acts on the skater, causing her angular
momentum and 𝜔 to increase. Reasoning Considering the skater as the system, we will use the conser- vation of angular momentum as a guide; it indicates that only a net external
torque can cause the total angular momentum of a system to change.
Answer (a) is incorrect. There is no net external torque acting on the skater, because air resistance and the friction between her skates and the
ice are negligible.
9.6 Angular Momentum 245
The next example involves a satellite and illustrates another application of the principle of
conservation of angular momentum.
Answer (c) is incorrect. The movements of her arms and legs do produce internal torques. However, only external torques, not internal torques, can change the angular momentum of a system.
Answer (b) is correct. Since any air resistance and friction are negli- gible, the net external torque acting on the skater is zero, and the skater’s
angular momentum is conserved as she pulls her arms and leg inward.
However, angular momentum is the product of the moment of inertia I
and the angular velocity 𝜔 (see Equation 9.10). By moving the mass of her arms and leg inward, the skater decreases the distance r of the mass from the axis of rotation and, consequently, decreases her moment of
inertia I (I = Σmr 2 ). Since the product of I and 𝜔 is constant, then 𝜔 must increase as I decreases. Thus, as she pulls her arms and leg inward, she spins with a larger angular velocity.
Related Homework: Problem 61
EXAMPLE 14 The Physics of a Satellite in an Elliptical Orbit
An artifi cial satellite is placed into an elliptical orbit about the earth, as
illustrated in Figure 9.24. Telemetry data indicate that its point of closest approach (called the perigee) is rP = 8.37 × 106 m from the center of the earth, and its point of greatest distance (called the apogee) is rA = 25.1 × 106 m from the center of the earth. The speed of the satellite at the perigee
is 𝜐P = 8450 m/s. Find its speed 𝜐A at the apogee.
Reasoning The only force of any signifi cance that acts on the satellite is the gravitational force of the earth. However, at any instant, this force is
directed toward the center of the earth and passes through the axis about
which the satellite instantaneously rotates. Therefore, the gravitational
force exerts no torque on the satellite (the lever arm is zero). Consequently, the net average external torque acting on the satellite is zero, and the angu-
lar momentum of the satellite remains constant at all times.
Solution Since the angular momentum is the same at the apogee (A) and the perigee (P), it follows that IA𝜔A = IP𝜔P. Furthermore, the orbiting satellite can be considered a point mass, so its moment of iner-
tia is I = mr2 (see Equation 9.4). In addition, the angular speed 𝜔 of the satellite is related to its tangential speed 𝜐T by 𝜔 = 𝜐T/r (Equation 8.9). If Equation 9.4 and Equation 8.9 are used at the apogee and perigee, the
conservation of angular momentum gives the following result:
IAωA = IP ωP or (mrA2) ( υA rA) = (mrP2) (
υP rP)
υA = rP υP rA
= (8.37 × 10 6 m)(8450 m /s)
25.1 ×10 6 m = 2820 m/s
The answer is independent of the mass of the satellite. The satellite be-
haves just like the skater in Figure 9.23, because its speed is smaller at the apogee, where the moment of inertia is greater, and greater at the perigee,
where the moment of inertia is smaller.
rA
rP
vP
vA
Apogee Perigee C
Earth
FIGURE 9.24 A satellite is moving in an elliptical orbit about the earth. The
gravitational force exerts no torque on
the satellite, so the angular momentum
of the satellite is conserved.
The result in Example 14 indicates that a satellite does not have a constant speed in an ellip-
tical orbit. The speed changes from a maximum at the perigee to a minimum at the apogee; the
closer the satellite comes to the earth, the faster it travels. Planets moving around the sun in ellip-
tical orbits exhibit the same kind of behavior, and Johannes Kepler (1571–1630) formulated his
famous second law based on observations of such characteristics of planetary motion. Kepler’s
second law states that, in a given amount of time, a line joining any planet to the sun sweeps
out the same amount of area no matter where the planet is on its elliptical orbit, as Figure 9.25 illustrates. The conservation of angular momentum can be used to show why the law is valid, by
means of a calculation similar to that in Example 14.
Check Your Understanding
(The answers are given at the end of the book.) 17. A woman is sitting on the spinning seat of a piano stool with her arms folded. Ignore any friction in the
spinning stool. What happens to her (a) angular velocity and (b) angular momentum when she extends her arms outward?
Sun
Planet
Elliptical orbit
These areas are equal if the time intervals
are equal.
FIGURE 9.25 Kepler’s second law of planetary motion states that a line joining a
planet to the sun sweeps out equal areas in
equal time intervals.(Continued)
246 CHAPTER 9 Rotational Dynamics
18. Review Conceptual Example 13 as an aid in answering this question. Suppose the ice cap at the South Pole were to melt and the water were distributed uniformly over the earth’s oceans. Would the earth’s
angular velocity increase, decrease, or remain the same?
19. Conceptual Example 13 provides background for this question. A cloud of interstellar gas is rotating. Because the gravitational force pulls the gas particles together, the cloud shrinks, and, under the right
conditions, a star may ultimately be formed. Would the angular velocity of the star be less than, equal
to, or greater than the angular velocity of the rotating gas?
20. A person is hanging motionless from a vertical rope over a swimming pool. She lets go of the rope and drops straight down. After letting go, is it possible for her to curl into a ball and start spinning?
EXAMPLE 15 BIO The Physics of the Rotational Kinetic Energy of a Figure Skater
In Conceptual Example 13 we saw how a spinning fi gure skater can
change her angular velocity by changing her moment of inertia. This
occurs because, in the absence of external torques, the skater’s angular
momentum is conserved. But what about her rotational kinetic energy?
Is that also conserved? Assume the skater in Figure 9.23a has a moment of inertia I0 and is rotating with an angular velocity 𝜔0. When she brings her arms in (Figure 9.23b) assume her rotational velocity doubles. Calcu- late the ratio of her fi nal rotational kinetic energy to her initial rotational
kinetic energy (KERf/KER0) and answer the question of whether or not her
rotational kinetic energy is conserved.
Reasoning We can calculate the skater’s rotational kinetic energy, both before and after she brings her arms in, by using Equation 9.9. To sim-
plify the ratio of her rotational kinetic energies, we can apply conserva-
tion of angular momentum.
Solution Applying Equation 9.9, the ratio of her rotational kinetic energy will be given by the following:
KERf
KER0 =
1
2 If ωf2 1
2 I0ω02 .
We can simplify this expression and rewrite it in the following way:
KERf
KER0 =
1
2 If ωf2 1
2 I0ω02 =
(If ωf)ωf (I0ω0)ω0
.
The product of Iω in the numerator and denominator represents the angular momentum, L, after and before the skater brings her arms in, respectively. We know these two quantities are equal, since the angular momentum in
this problem is conserved. Therefore, the ratio of her rotational kinetic
energies reduces to the ratio of her fi nal and initial angular velocities:
KERf
KER0 =
ωf ω0
.
Here, we are told that her angular velocity doubles. Thus, ωf = 2ω0, and KERf
KER0 =
2ω0 ω0
= 2 . While her angular momentum during this maneuver is
conserved, her rotational kinetic energy is not. Where does the extra ro-
tational kinetic energy come from? It comes from the work that she does
internally to move her arms closer to the axis of rotation.
(a) (b)
FIGURE 9.23 (REPEATED) (a) A skater spins slowly on one skate, with both arms and one leg outstretched. (b) As she pulls her arms and leg in toward the rotational axis, her angular velocity 𝜔 increases.
Concept Summary 9.1 The Action of Forces and Torques on Rigid Objects The line of ac- tion of a force is an extended line that is drawn colinear with the force. The
lever arm ℓ is the distance between the line of action and the axis of rotation,
measured on a line that is perpendicular to both.
The torque of a force has a magnitude that is given by the magnitude F of the force times the lever arm ℓ. The magnitude of the torque 𝜏 is given
by Equation 9.1, and 𝜏 is positive when the force tends to produce a coun-
terclockwise rotation about the axis, and negative when the force tends to
produce a clockwise rotation.
Magnitude of torque = Fℓ (9.1)
9.2 Rigid Objects in Equilibrium A rigid body is in equilibrium if it has zero translational acceleration and zero angular acceleration. In equilibrium,
the net external force and the net external torque acting on the body are zero,
according to Equations 4.9a, 4.9b, and 9.2.
Σ Fx = 0 and Σ Fy = 0 (4.9a and 4.9b)
Στ = 0 (9.2)
9.3 Center of Gravity The center of gravity of a rigid object is the point where its entire weight can be considered to act when calculating the torque
due to the weight. For a symmetrical body with uniformly distributed weight,
Focus on Concepts 247
the center of gravity is at the geometrical center of the body. When a number
of objects whose weights are W1, W2, . . . are distributed along the x axis at locations x1, x2, . . . , the center of gravity xcg is given by Equation 9.3. The center of gravity is identical to the center of mass, provided the acceleration
due to gravity does not vary over the physical extent of the objects.
xcg = W1x1 + W2 x2 + ⋅ ⋅ ⋅
W1 + W2 + ⋅ ⋅ ⋅ (9.3)
9.4 Newton’s Second Law for Rotational Motion About a Fixed Axis The moment of inertia I of a body composed of N particles is given by Equa- tion 9.6, where m is the mass of a particle and r is the perpendicular distance of the particle from the axis of rotation.
I = m1r12 + m2r22 + ⋅ ⋅ ⋅ + mN rN2 = Σmr 2 (9.6)
For a rigid body rotating about a fi xed axis, Newton’s second law for
rotational motion is stated as in Equation 9.7, where Σ𝜏 is the net external
torque applied to the body, I is the moment of inertia of the body, and 𝛼 is its angular acceleration.
Στ = Iα (𝛼 in rad/s2) (9.7)
9.5 Rotational Work and Energy The rotational work WR done by a constant torque 𝜏 in turning a rigid body through an angle 𝜃 is specifi ed by
Equation 9.8.
The rotational kinetic energy KER of a rigid object rotating with an angu-
lar speed 𝜔 about a fi xed axis and having a moment of inertia I is specifi ed by Equation 9.9.
The total mechanical energy E of a rigid body is the sum of its transla- tional kinetic energy (
1
2 mυ2), its rotational kinetic energy ( 1
2 Iω2), and its gravitational potential energy (mgh), according to Equation 1, where m is the mass of the object, 𝜐 is the translational speed of its center of mass, I is its moment of inertia about an axis through the center of mass, 𝜔 is its angular speed, and h is the height of the object’s center of mass relative to an arbitrary zero level.
The total mechanical energy is conserved if the net work done by external
nonconservative forces and external torques is zero. When the total mechani-
cal energy is conserved, the fi nal total mechanical energy Ef equals the initial total mechanical energy E0 : Ef = E0.
WR = τθ (𝜃 in radians) (9.8)
KER = 1
2 Iω2 (𝜔 in rad/s) (9.9)
E = 12 mυ2 + 1
2 Iω2 + mgh (1)
9.6 Angular Momentum The angular momentum of a rigid body rotating with an angular velocity 𝜔 about a fi xed axis and having a moment of inertia I with respect to that axis is given by Equation 9.10.
L = Iω (𝜔 in rad/s) (9.10)
The principle of conservation of angular momentum states that the total
angular momentum of a system remains constant (is conserved) if the net
average external torque acting on the system is zero. When the total angular
momentum is conserved, the fi nal angular momentum Lf equals the initial angular momentum L0: Lf = L0.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 9.1 The Action of Forces and Torques on Rigid Objects 1. The wheels on a moving bicycle have both translational (or linear) and ro- tational motions. What is meant by the phrase “a rigid body, such as a bicycle
wheel, is in equilibrium”? (a) The body cannot have translational or rotational motion of any kind. (b) The body can have translational motion, but it cannot have rotational motion. (c) The body cannot have translational motion, but it can have rotational motion. (d) The body can have translational and rotational mo- tions, as long as its translational acceleration and angular acceleration are zero.
Section 9.2 Rigid Objects in Equilibrium 3. The drawing illustrates an over- head view of a door and its axis of
rotation. The axis is perpendicular to
the page. There are four forces act-
ing on the door, and they have the
same magnitude. Rank the torque 𝜏
that each force produces, largest to
smallest. (a) 𝜏4, 𝜏3, 𝜏2, 𝜏1 (b) 𝜏3, 𝜏2, 𝜏1 and 𝜏4 (a two-way tie) (c) 𝜏2, 𝜏4, 𝜏3, 𝜏1 (d) 𝜏1, 𝜏4, 𝜏3, 𝜏2 (e) 𝜏2, 𝜏3 and 𝜏4 (a two-way tie), 𝜏1
6. Five hockey pucks are sliding across frictionless ice. The drawing shows a top view of the pucks and the three forces that act on each one. As shown, the
forces have diff erent magnitudes (F, 2F, or 3F), and are applied at diff erent points on the pucks. Only one of the fi ve pucks can be in equilibrium. Which
puck is it? (a) 1 (b) 2 (c) 3 (d) 4 (e) 5
(1)
F
2F
3F
2F
3FF
F
2F
F
F
2F
F
F F
2F
(2) (3) (4) (5)
QUESTION 6
8. The drawing shows a top view of a square box lying on a frictionless fl oor. Three forces,
which are drawn to scale, act on the box. Con-
sider an angular acceleration with respect to an
axis through the center of the box (perpendic-
ular to the page). Which one of the following
statements is correct? (a) The box will have a translational acceleration but not an angu-
lar acceleration. (b) The box will have both a translational and an angular acceleration.
(c) The box will have an angular acceleration but not a translational acceleration. (d) The box will have neither a transla- tional nor an angular acceleration. (e) It is not possible to determine whether the box will have a translational or an angular acceleration.
Focus on Concepts
Door (overhead view)
Axis of rotation
F1 F2 F3
F4
QUESTION 3
F1
F2
F3
QUESTION 8
248 CHAPTER 9 Rotational Dynamics
Section 9.4 Newton’s Second Law for Rotational Motion About a Fixed Axis 10. The drawing shows three objects ro- tating about a vertical axis. The mass of
each object is given in terms of m0, and its perpendicular distance from the axis is
specifi ed in terms of r0. Rank the three ob- jects according to their moments of inertia,
largest to smallest. (a) A, B, C (b) A, C, B (c) B, A, C (d) B, C, A (e) C, A, B
12. Two blocks are placed at the ends of a horizontal massless board, as in the drawing.
The board is kept from ro-
tating and rests on a support
that serves as an axis of rota-
tion. The moment of inertia
of this system relative to the
axis is 12 kg · m2. Determine the magnitude of the angular
acceleration when the system
is allowed to rotate.
13. The same force F→ is applied to the edge of two hoops (see the
drawing). The hoops have the
same mass, whereas the radius
of the larger hoop is twice the
radius of the smaller one. The en-
tire mass of each hoop is concen-
trated at its rim, so the moment of
inertia is I = Mr2, where M is the mass and r is the radius. Which hoop has the greater angular acceleration, and how many times as great is it
compared to the angular acceleration of the other hoop? (a) The smaller hoop;
two times as great (b) The smaller hoop; four times as great (c) The larger hoop; two times as great (d) The larger hoop; four times as great (e) Both have the same angular acceleration.
Section 9.5 Rotational Work and Energy 16. Two hoops, starting from rest, roll down
identical inclined planes.
The work done by non-
conservative forces, such
as air resistance, is zero
(Wnc = 0 J). Both have the same mass M, but, as the drawing shows,
one hoop has twice the
radius of the other. The moment of inertia for each hoop is I = Mr2, where r is its radius. Which hoop, if either, has the greater total kinetic energy (translational plus rotational) at the bottom of the incline? (a) The larger hoop (b) The smaller hoop (c) Both have the same total kinetic energy.
Section 9.6 Angular Momentum 17. Under what condition(s) is the angular momentum of a rotating body, such as a spinning ice skater, conserved? (a) Each external force acting on the body must be zero. (b) Each external force and each external torque acting on the body must be zero. (c) Each external force may be nonzero, but the sum of the forces must be zero. (d) Each external torque may be nonzero, but the sum of the torques must be zero.
18. An ice skater is spinning on frictionless ice with her arms extended out- ward. She then pulls her arms in toward her body, reducing her moment of
inertia. Her angular momentum is conserved, so as she reduces her moment
of inertia, her angular velocity increases and she spins faster. Compared
to her initial rotational kinetic energy, her fi nal rotational kinetic energy is
(a) the same (b) larger, because her angular speed is larger (c) smaller, be- cause her moment of inertia is smaller.
QUESTION 10
r0
2r0 2m0
10m0
m03r0
A
B
C
Axis of rotation
F
F
Axis
Axis
2R
R
QUESTION 13
12 kg 1.4 m
Axis Support
4.0 kg
0.60 m
QUESTION 12
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 9.1 The Action of Forces and Torques on Rigid Objects 1. E SSM MMH The wheel of a car has a radius of 0.350 m. The engine of the car applies a torque of 295 N · m to this wheel, which does not slip against the road surface. Since the wheel does not slip, the road must be applying a
force of static friction to the wheel that produces a countertorque. Moreover,
the car has a constant velocity, so this countertorque balances the applied
torque. What is the magnitude of the static frictional force?
2. E The steering wheel of a car has a radius of 0.19 m, and the steering wheel of a truck has a radius of 0.25 m. The same force is applied in the same
direction to each steering wheel. What is the ratio of the torque produced by
this force in the truck to the torque produced in the car?
3. E SSM You are installing a new spark plug in your car, and the manual specifi es that it be tightened to a torque that has a magnitude of 45 N · m. Using the data in the drawing, determine the magnitude F of the force that you must exert on the wrench.
PROBLEM 3
0.28 m
50.0° F
4. E GO Two children hang by their hands from the same tree branch. The branch is straight, and grows out from the tree trunk at an angle of 27.0°
Problems
Radius = R Mass = M
Radius = R Mass = M
1–– 2
QUESTION 16
Problems 249
above the horizontal. One child, with a mass of 44.0 kg, is hanging 1.30 m
along the branch from the tree trunk. The other child, with a mass of 35.0 kg,
is hanging 2.10 m from the tree trunk. What is the magnitude of the net
torque exerted on the branch by the children? Assume that the axis is located
where the branch joins the tree trunk and is perpendicular to the plane formed
by the branch and the trunk.
5. E SSM The drawing shows a jet engine suspended beneath the wing of an airplane. The weight W
→ of the engine is 10 200 N and acts as shown in the
drawing. In fl ight the engine produces a thrust T→ of 62 300 N that is parallel to the ground. The rotational axis in the drawing is perpendicular to the plane
of the paper. With respect to this axis, fi nd the magnitude of the torque due to
(a) the weight and (b) the thrust.
PROBLEM 5
Axis
32.0°
2.50 m
W
T
6. E A square, 0.40 m on a side, is mounted so that it can rotate about an axis that passes through the center of the square. The axis is perpendicular
to the plane of the square. A force of 15 N lies in this plane and is applied to
the square. What is the magnitude of the maximum torque that such a force
could produce?
7. M SSM A pair of forces with equal magnitudes, opposite directions, and diff erent lines of action is called a “couple.” When a couple acts on a rigid
object, the couple produces a torque that does not depend on the location of the axis. The drawing shows a couple acting on a tire wrench, each force
being perpendicular to the wrench. Determine an expression for the torque
produced by the couple when the axis is perpendicular to the tire and passes
through (a) point A, (b) point B, and (c) point C. Express your answers in terms of the magnitude F of the force and the length L of the wrench.
PROBLEM 7
–F
A
B
L– 2
L– 2
C
F
8. M GO One end of a meter stick is pinned to a table, so the stick can ro- tate freely in a plane parallel to the tabletop. Two forces, both parallel to the
tabletop, are applied to the stick in such a way that the net torque is zero.
The fi rst force has a magnitude of 2.00 N and is applied perpendicular to the
length of the stick at the free end. The second force has a magnitude of 6.00 N
and acts at a 30.0° angle with respect to the length of the stick. Where along
the stick is the 6.00-N force applied? Express this distance with respect to the
end of the stick that is pinned.
9. M V-HINT MMH A rod is lying on the top of a table. One end of the rod is hinged to the table so that the rod can rotate freely on the tabletop. Two
forces, both parallel to the tabletop, act on the rod at the same place. One
force is directed perpendicular to the rod and has a magnitude of 38.0 N. The
second force has a magnitude of 55.0 N and is directed at an angle 𝜃 with
respect to the rod. If the sum of the torques due to the two forces is zero, what
must be the angle 𝜃?
10. H A rotational axis is directed perpendicular to the plane of a square and is located as shown in the drawing. Two forces, F1
→ and F2
→ , are applied to diagon-
ally opposite corners, and act along the sides of the square, fi rst as shown in part
a and then as shown in part b of the drawing. In each case the net torque pro- duced by the forces is zero. The square is one meter on a side, and the magnitude
of F2 →
is three times that of F1 →
. Find the distances a and b that locate the axis.
PROBLEM 10
F2
F1 F2
F1
(a) (b)
b
a
b
a Axis
Section 9.2 Rigid Objects in Equilibrium,
Section 9.3 Center of Gravity 11. E BIO A person is standing on a level fl oor. His head, upper torso, arms, and hands together weigh 438 N and have a center of gravity that is 1.28 m
above the fl oor. His upper legs weigh 144 N and have a center of gravity that
is 0.760 m above the fl oor. Finally, his lower legs and feet together weigh
87 N and have a center of gravity that is 0.250 m above the fl oor. Relative to
the fl oor, fi nd the location of the center of gravity for his entire body.
12. E BIO The drawing shows a person (weight, W = 584 N) doing push- ups. Find the normal force exerted by the fl oor on each hand and each foot, assuming that the person holds this position.
PROBLEM 12
cg
0.840 m 0.410 m
13. E SSM MMH A hiker, who weighs 985 N, is strolling through the woods and crosses a small horizontal bridge. The bridge is uniform, weighs 3610 N,
and rests on two concrete supports, one at each end. He stops one-fi fth of
the way along the bridge. What is the magnitude of the force that a concrete
support exerts on the bridge (a) at the near end and (b) at the far end? 14. E Conceptual Example 7 provides useful background for this problem. Workers have loaded a delivery truck in such a way that its center of gravity
is only slightly forward of the rear axle, as shown in the drawing. The mass of
the truck and its contents is 7460 kg. Find the magnitudes of the forces exer-
ted by the ground on (a) the front wheels and (b) the rear wheels of the truck.
PROBLEM 14 2.30 m
0.63 m
cg
15. E BIO MMH A person exerts a horizontal force of 190 N in the test apparatus shown in the drawing. Find the horizontal force M
→ (magnitude
and direction) that his fl exor muscle exerts on his forearm.
250 CHAPTER 9 Rotational Dynamics
PROBLEM 15 Elbow joint
0.054 m
190 N
0.34 m Flexor muscle
M
16. E GO The drawing shows a rectangular piece of wood. The forces applied to corners B and D have the same magnitude of 12 N and are dir-
ected parallel to the long and short sides of the rectangle. The long side of
the rectangle is twice as long as the short side. An axis of rotation is shown
perpendicular to the plane of the rectangle at its center. A third force (not
shown in the drawing) is applied to corner A, directed along the short side of
the rectangle (either toward B or away from B), such that the piece of wood
is at equilibrium. Find the magnitude and direction of the force applied to
corner A.
PROBLEM 16 F
F
A
B C
D
Axis
17. E SSM Available in WileyPLUS. 18. E GO The wheels, axle, and handles of a wheelbarrow weigh 60.0 N. The load chamber and its contents weigh 525 N. The drawing shows these
two forces in two diff erent wheelbarrow designs. To support the wheelbar-
row in equilibrium, the man’s hands apply a force F→ to the handles that is directed vertically upward. Consider a rotational axis at the point where the
tire contacts the ground, directed perpendicular to the plane of the paper.
Find the magnitude of the man’s force for both designs.
PROBLEM 18
FF
60.0 N 60.0 N 525 N 525 N
0.400 m 0.600 m 0.700 m0.700 m 0.200 m
19. E MMH Review Conceptual Example 7 as background material for this problem. A jet transport has a weight of 1.00 × 106 N and is at rest on the
runway. The two rear wheels are 15.0 m behind the front wheel, and the
plane’s center of gravity is 12.6 m behind the front wheel. Determine the
normal force exerted by the ground on (a) the front wheel and on (b) each of the two rear wheels.
20. E Available in WileyPLUS. 21. E GO The drawing shows a uniform horizontal beam attached to a vertical wall by a frictionless hinge
and supported from below at an angle 𝜃 = 39° by a brace
that is attached to a pin. The beam has a weight of 340
N. Three additional forces keep the beam in equilibrium.
The brace applies a force P→ to the right end of the beam that is directed up- ward at the angle 𝜃 with respect to the horizontal. The hinge applies a force
to the left end of the beam that has a horizontal component H→ and a vertical component V
→ . Find the magnitudes of these three forces.
22. E BIO CHALK A man holds a 178-N ball in his hand, with the forearm horizontal (see the drawing). He can support the ball in this position because
of the fl exor muscle force M →
, which is applied perpendicular to the forearm.
The forearm weighs 22.0 N and has a center of gravity as indicated. Find
(a) the magnitude of M →
and (b) the magnitude and direction of the force applied by the upper arm bone to the forearm at the elbow joint.
PROBLEM 22
Elbow joint
Upper arm bone
Flexor muscle
0.0510 m
M
0.0890 m
cg
0.330 m
23. M SSM A uniform board is leaning against a smooth vertical wall. The board is at an angle 𝜃 above the horizontal ground. The coeffi cient of static
friction between the ground and the lower end of the board is 0.650. Find the
smallest value for the angle 𝜃, such that the lower end of the board does not
slide along the ground.
24. M V-HINT The drawing shows a bicycle wheel resting against a small step whose height is h = 0.120 m. The weight and radius of the wheel are W = 25.0 N and r = 0.340 m, respectively. A horizontal force F→ is applied to the axle of the wheel. As the magnitude of F→ increases, there comes a time when the wheel just begins to rise up and loses contact with the ground. What
is the magnitude of the force when this happens?
PROBLEM 24 h
r
F
25. M SSM A 1220-N uniform beam is attached to a vertical wall at one end and is supported by a cable at the other end. A 1960-N crate hangs from
the far end of the beam. Using the data shown in the drawing, fi nd (a) the magnitude of the tension in the wire and (b) the magnitudes of the horizontal and vertical components of the force that the wall exerts on the left end of
the beam.
PROBLEM 25
50.0° Beam
30.0°
1960 N
θ Beam
Brace
PinHinge
PROBLEM 21
Problems 251
26. M BIO GO A person is sitting with one leg outstretched and station- ary, so that it makes an angle of 30.0° with the horizontal, as the drawing
indicates. The weight of the leg below the knee is 44.5 N, with the center of
gravity located below the knee joint. The leg is being held in this position
because of the force M →
applied by the quadriceps muscle, which is attached
0.100 m below the knee joint (see the drawing). Obtain the magnitude of M →
.
PROBLEM 26
Knee joint 25.0°
30.0°
0.100 m
0.150 m cg
M
27. M V-HINT A wrecking ball (weight = 4800 N) is supported by a boom, which may be assumed to be uniform and has a weight of 3600 N. As the
drawing shows, a support cable runs from the top of the boom to the tractor.
The angle between the support cable and the horizontal is 32°, and the angle
between the boom and the horizontal is 48°. Find (a) the tension in the sup- port cable and (b) the magnitude of the force exerted on the lower end of the boom by the hinge at point P.
PROBLEM 27
Boom
Support cable
P 48°32°
28. H A man drags a 72-kg crate across the fl oor at a constant velocity by pulling on a strap attached to the bottom of the crate. The crate is tilted 25°
above the horizontal, and the strap is inclined 61° above the horizontal. The
center of gravity of the crate coincides with its geometrical center, as indic-
ated in the drawing. Find the magnitude of the tension in the strap.
PROBLEM 28 25°
0.90 m
0.40 m
61°
29. H SSM Available in WileyPLUS. 30. H The drawing shows an A-shaped stepladder. Both sides of the ladder are equal in length. This ladder is standing on a frictionless horizontal sur-
face, and only the crossbar (which has a negligible mass) of the “A” keeps
the ladder from collapsing. The ladder is uniform and has a mass of 20.0 kg.
Determine the tension in the crossbar of the ladder.
PROBLEM 30
Crossbar
1.00 m
4.00 m 30.0°
Section 9.4 Newton’s Second Law for Rotational Motion About a Fixed Axis 31. E Consult Multiple-Concept Example 10 to review an approach to problems such as this. A CD has a mass of 17 g and a radius of 6.0 cm. When
inserted into a player, the CD starts from rest and accelerates to an angular
velocity of 21 rad/s in 0.80 s. Assuming the CD is a uniform solid disk,
determine the net torque acting on it.
32. E A clay vase on a potter’s wheel experiences an angular acceleration of 8.00 rad/s2 due to the application of a 10.0-N · m net torque. Find the total moment of inertia of the vase and potter’s wheel.
33. E A solid circular disk has a mass of 1.2 kg and a radius of 0.16 m. Each of three identical thin rods has a mass of 0.15 kg. The rods are attached per-
pendicularly to the plane of the disk at its outer edge to form a three-legged
stool (see the drawing). Find the moment of inertia of the stool with respect
to an axis that is perpendicular to the plane of the disk at its center. (Hint: When considering the moment of inertia of each rod, note that all of the mass of each rod is located at the same perpendicular distance from the axis.)
PROBLEM 33
34. E A ceiling fan is turned on and a net torque of 1.8 N · m is applied to the blades. The blades have a total moment of inertia of 0.22 kg · m2. What is the angular acceleration of the blades?
35. E GO Multiple-Concept Example 10 provides one model for solving this type of problem. Two wheels have the same mass and radius of 4.0 kg
and 0.35 m, respectively. One has the shape of a hoop and the other the shape
of a solid disk. The wheels start from rest and have a constant angular accel-
eration with respect to a rotational axis that is perpendicular to the plane of
the wheel at its center. Each turns through an angle of 13 rad in 8.0 s. Find
the net external torque that acts on each wheel.
36. E A 9.75-m ladder with a mass of 23.2 kg lies fl at on the ground. A painter grabs the top end of the ladder and pulls straight upward with a force
of 245 N. At the instant the top of the ladder leaves the ground, the ladder ex-
periences an angular acceleration of 1.80 rad/s2 about an axis passing through
the bottom end of the ladder. The ladder’s center of gravity lies halfway
between the top and bottom ends. (a) What is the net torque acting on the ladder? (b) What is the ladder’s moment of inertia? 37. E SSM MMH Multiple-Concept Example 10 off ers useful background for problems like this. A cylinder is rotating about an axis that passes through
the center of each circular end piece. The cylinder has a radius of 0.0830 m,
an angular speed of 76.0 rad/s, and a moment of inertia of 0.615 kg · m2. A brake shoe presses against the surface of the cylinder and applies a tangential
frictional force to it. The frictional force reduces the angular speed of the
cylinder by a factor of two during a time of 6.40 s. (a) Find the magnitude of the angular deceleration of the cylinder. (b) Find the magnitude of the force of friction applied by the brake shoe.
38. E Available in WileyPLUS. 39. E SSM Available in WileyPLUS. 40. E BIO CHALK Multiple-Concept Example 10 reviews the approach and some of the concepts that are pertinent to this problem. The drawing shows
a model for the motion of the human forearm in throwing a dart. Because of
the force M →
applied by the triceps muscle, the forearm can rotate about an axis at the elbow joint. Assume that the forearm has the dimensions shown in
the drawing and a moment of inertia of 0.065 kg · m2 (including the eff ect of the dart) relative to the axis at the elbow. Assume also that the force M
→ acts
252 CHAPTER 9 Rotational Dynamics
perpendicular to the forearm. Ignoring the eff ect of gravity and any frictional
forces, determine the magnitude of the force M →
needed to give the dart a
tangential speed of 5.0 m/s in 0.10 s, starting from rest.
PROBLEM 40
0.28 m
0.025 m
Axis at elbow joint
M
41. M SSM Available in WileyPLUS. 42. M V-HINT A 15.0-m length of hose is wound around a reel, which is ini- tially at rest. The moment of inertia of the reel is 0.44 kg · m2, and its radius is 0.160 m. When the reel is turning, friction at the axle exerts a torque of
magnitude 3.40 N · m on the reel. If the hose is pulled so that the tension in it remains a constant 25.0 N, how long does it take to completely unwind the
hose from the reel? Neglect the mass and thickness of the hose on the reel,
and assume that the hose unwinds without slipping.
43. E GO The drawing shows two identical systems of objects; each con- sists of the same three small balls connected by massless rods. In both systems
the axis is perpendicular to the page, but it is located at a diff erent place, as
shown. The same force of magnitude F is applied to the same ball in each sys- tem (see the drawing). The masses of the balls are m1 = 9.00 kg, m2 = 6.00 kg, and m3 = 7.00 kg. The magnitude of the force is F = 424 N. (a) For each of the two systems, determine the moment of inertia about the given axis of
rotation. (b) Calculate the torque (magnitude and direction) acting on each system. (c) Both systems start from rest, and the direction of the force moves with the system and always points along the 4.00-m rod. What is the angular
velocity of each system after 5.00 s?
PROBLEM 43
4.00 m
3.00 m
5.00 m
Axis
System A
4.00 m
3.00 m
5.00 m
Axis
System B
F m1 m1
m2
m3 m3
m2
F
44. M GO The drawing shows the top view of two doors. The doors are uniform and identical. Door A rotates about an axis through its left edge, and
door B rotates about an axis through its center. The same force F→ is applied perpendicular to each door at its right edge, and the force remains perpen-
dicular as the door turns. No other force aff ects the rotation of either door.
Starting from rest, door A rotates through a certain angle in 3.00 s. How long
does it take door B (also starting from rest) to rotate through the same angle?
PROBLEM 44
Axis Door A
F
Axis
Door B
F
45. M SSM A stationary bicycle is raised off the ground, and its front wheel (m = 1.3 kg) is rotating at an angular velocity of 13.1 rad/s (see the drawing).
The front brake is then applied for 3.0 s, and the wheel slows down to
3.7 rad/s. Assume that all the mass of the wheel is concentrated in the rim,
the radius of which is 0.33 m. The coeffi cient of kinetic friction between each
brake pad and the rim is μk = 0.85. What is the magnitude of the normal force that each brake pad applies to the rim?
PROBLEM 45
Brake pads
0.33 m
46. M The parallel axis theorem provides a useful way to calculate the moment of inertia I about an arbitrary axis. The theorem states that I = Icm + Mh2, where Icm is the moment of inertia of the object relative to an axis that passes through the center of mass and is parallel to the axis of interest, M is the total mass of the object, and h is the perpendicular distance between the two axes. Use this theorem and information to determine an expression for
the moment of inertia of a solid cylinder of radius R relative to an axis that lies on the surface of the cylinder and is perpendicular to the circular ends.
47. H The crane shown in the drawing is lifting a 180-kg crate upward with an acceleration of 1.2 m/s2. The cable from the crate passes over a solid cyl-
indrical pulley at the top of the boom. The pulley has a mass of 130 kg. The
cable is then wound onto a hollow cylindrical drum that is mounted on the
deck of the crane. The mass of the drum is 150 kg, and its radius is 0.76 m.
The engine applies a counterclockwise torque to the drum in order to wind up
the cable. What is the magnitude of this torque? Ignore the mass of the cable.
PROBLEM 47
Pulley
Drum Boom
Section 9.5 Rotational Work and Energy 48. H Calculate the kinetic energy that the earth has because of (a) its ro- tation about its own axis and (b) its motion around the sun. Assume that the earth is a uniform sphere and that its path around the sun is circular. For
comparison, the total energy used in the United States in one year is about
1.1 × 1020 J.
49. E SSM Three objects lie in the x, y plane. Each rotates about the z axis with an angular speed of 6.00 rad/s. The mass m of each object and its per- pendicular distance r from the z axis are as follows: (1) m1 = 6.00 kg and r1 = 2.00 m, (2) m2 = 4.00 kg and r2 = 1.50 m, (3) m3 = 3.00 kg and r3 = 3.00 m. (a) Find the tangential speed of each object. (b) Determine the total kinetic energy of this system using the expression KE =
1
2 m1υ 21 + 1
2 m2υ 22 + 1
2 m3υ 23 . (c) Obtain the moment of inertia of the system. (d) Find the rotational kinetic energy of the system using the relation KER =
1
2 Iω2 to verify that the answer is the same as the answer to (b).
50. E GO Two thin rods of length L are rotating with the same angular speed ω (in rad/s) about axes that pass perpendicularly through one end. Rod A is massless but has a particle of mass 0.66 kg attached to its free end.
Rod B has a mass of 0.66 kg, which is distributed uniformly along its length.
Problems 253
The length of each rod is 0.75 m, and the angular speed is 4.2 rad/s. Find the
kinetic energies of rod A with its attached particle and of rod B.
51. E SSM A fl ywheel is a solid disk that rotates about an axis that is per- pendicular to the disk at its center. Rotating fl ywheels provide a means for
storing energy in the form of rotational kinetic energy and are being con-
sidered as a possible alternative to batteries in electric cars. The gasoline
burned in a 300-mile trip in a typical midsize car produces about 1.2 × 109 J
of energy. How fast would a 13-kg fl ywheel with a radius of 0.30 m have to
rotate to store this much energy? Give your answer in rev/min.
52. E A helicopter has two blades (see Figure 8.11); each blade has a mass of 240 kg and can be approximated as a thin rod of length 6.7 m. The blades
are rotating at an angular speed of 44 rad/s. (a) What is the total moment of inertia of the two blades about the axis of rotation? (b) Determine the rota- tional kinetic energy of the spinning blades.
53. M MMH A solid sphere is rolling on a surface. What fraction of its total kinetic energy is in the form of rotational kinetic energy about the center of
mass?
54. M GO Review Example 12 before attempting this problem. A marble and a cube are placed at the top of a ramp. Starting from rest at the same
height, the marble rolls without slipping and the cube slides (no kinetic
friction) down the ramp. Determine the ratio of the center-of-mass speed
of the cube to the center-of-mass speed of the marble at the bottom of
the ramp.
55. M V-HINT Starting from rest, a basketball rolls from the top of a hill to the bottom, reaching a translational speed of 6.6 m/s. Ignore frictional losses.
(a) What is the height of the hill? (b) Released from rest at the same height, a can of frozen juice rolls to the bottom of the same hill. What is the transla-
tional speed of the frozen juice can when it reaches the bottom?
56. M V-HINT Available in WileyPLUS. 57. M CHALK SSM A bowling ball encounters a 0.760-m vertical rise on the way back to the ball rack, as the drawing illustrates. Ignore frictional losses
and assume that the mass of the ball is distributed uniformly. The transla-
tional speed of the ball is 3.50 m/s at the bottom of the rise. Find the transla-
tional speed at the top.
PROBLEM 57
0.760 m
58. H A tennis ball, starting from rest, rolls down the hill in the drawing. At the end of the hill the ball becomes airborne, leaving at an angle of 35°
with respect to the ground. Treat the ball as a thin-walled spherical shell, and
determine the range x.
PROBLEM 58
1.8 m
35°
x
Section 9.6 Angular Momentum 59. E SSM Two disks are rotating about the same axis. Disk A has a mo- ment of inertia of 3.4 kg · m2 and an angular velocity of +7.2 rad/s. Disk B is rotating with an angular velocity of −9.8 rad/s. The two disks are then linked
together without the aid of any external torques, so that they rotate as a single
unit with an angular velocity of −2.4 rad/s. The axis of rotation for this unit
is the same as that for the separate disks. What is the moment of inertia of
disk B?
60. E When some stars use up their fuel, they undergo a catastrophic explo- sion called a supernova. This explosion blows much or all of the star’s mass outward, in the form of a rapidly expanding spherical shell. As a simple
model of the supernova process, assume that the star is a solid sphere of
radius R that is initially rotating at 2.0 revolutions per day. After the star explodes, fi nd the angular velocity, in revolutions per day, of the expanding
supernova shell when its radius is 4.0R. Assume that all of the star’s original mass is contained in the shell.
61. E GO Conceptual Example 13 provides useful background for this problem. A playground carousel is free to rotate about its center on friction-
less bearings, and air resistance is negligible. The carousel itself (without
riders) has a moment of inertia of 125 kg · m2. When one person is standing on the carousel at a distance of 1.50 m from the center, the carousel has an
angular velocity of 0.600 rad/s. However, as this person moves inward to
a point located 0.750 m from the center, the angular velocity increases to
0.800 rad/s. What is the person’s mass?
62. E Available in WileyPLUS. 63. E MMH A thin rod has a length of 0.25 m and rotates in a circle on a frictionless tabletop. The axis is perpendicular to the length of the rod at one
of its ends. The rod has an angular velocity of 0.32 rad/s and a moment of
inertia of 1.1 × 10−3 kg · m2. A bug standing on the axis decides to crawl out to the other end of the rod. When the bug (mass = 4.2 × 10−3 kg) gets where
it’s going, what is the angular velocity of the rod?
64. E GO As seen from above, a playground carousel is rotating counter- clockwise about its center on frictionless bearings. A person standing still on
the ground grabs onto one of the bars on the carousel very close to its outer
edge and climbs aboard. Thus, this person begins with an angular speed of
zero and ends up with a nonzero angular speed, which means that he un-
derwent a counterclockwise angular acceleration. The carousel has a radius
of 1.50 m, an initial angular speed of 3.14 rad/s, and a moment of inertia of
125 kg · m2. The mass of the person is 40.0 kg. Find the fi nal angular speed of the carousel after the person climbs aboard.
65. M V-HINT Available in WileyPLUS. 66. M GO A thin, uniform rod is hinged at its midpoint. To begin with, one- half of the rod is bent upward and is perpendicular to the other half. This bent
object is rotating at an angular velocity of 9.0 rad/s about an axis that is per-
pendicular to the left end of the rod and parallel to the rod’s upward half (see
the drawing). Without the aid of external torques, the rod suddenly assumes
its straight shape. What is the angular velocity of the straight rod?
PROBLEM 66
Hinge
Axis
67. H A small 0.500-kg object moves on a frictionless horizontal table in a circular path of radius 1.00 m. The angular speed is 6.28 rad/s. The object
is attached to a string of negligible mass that passes through a small hole in
the table at the center of the circle. Someone under the table begins to pull
the string downward to make the circle smaller. If the string will tolerate a
tension of no more than 105 N, what is the radius of the smallest possible
circle on which the object can move?
68. H Available in WileyPLUS.
254 CHAPTER 9 Rotational Dynamics
69. E BIO The drawing shows a lower leg being exercised. It has a 49-N weight attached to the foot and is extended at an angle 𝜃 with respect to the
vertical. Consider a rotational axis at the knee. (a) When 𝜃 = 90.0°, fi nd the magnitude of the torque that the weight creates. (b) At what angle 𝜃 does the magnitude of the torque equal 15 N · m?
PROBLEM 69
Axis 0.55 m
49 N
θ
70. E A solid disk rotates in the horizontal plane at an angular velocity of 0.067 rad/s with respect to an axis perpendicular to the disk at its center. The
moment of inertia of the disk is 0.10 kg · m2. From above, sand is dropped straight down onto this rotating disk, so that a thin uniform ring of sand is
formed at a distance of 0.40 m from the axis. The sand in the ring has a mass of
0.50 kg. After all the sand is in place, what is the angular velocity of the disk?
71. E A solid cylindrical disk has a radius of 0.15 m. It is mounted to an axle that is perpendicular to the circular end of the disk at its center. When a 45-N
force is applied tangentially to the disk, perpendicular to the radius, the disk
acquires an angular acceleration of 120 rad/s2. What is the mass of the disk?
72. E GO Review Conceptual Example 7 before starting this problem. A uniform plank of length 5.0 m and weight 225 N rests horizontally on two
supports, with 1.1 m of the plank hanging over the right support (see the
drawing). To what distance x can a person who weighs 450 N walk on the overhanging part of the plank before it just begins to tip?
PROBLEM 72
x
1.1 m
73. E SSM A rotating door is made from four rectangular sections, as indic- ated in the drawing. The mass of each section is 85 kg. A person pushes on the
outer edge of one section with a force of F = 68 N that is directed perpendicu- lar to the section. Determine the magnitude of the door’s angular acceleration.
PROBLEM 73
1.2 m
1.2 m
F
74. M V-HINT A block (mass = 2.0 kg) is hanging from a massless cord that is wrapped around a pulley (moment of inertia = 1.1 × 10−3 kg · m2), as the drawing shows. Initially the pulley is prevented from rotating and the block
is stationary. Then, the pulley is allowed to rotate as the block falls. The cord
does not slip relative to the pulley as the block falls. Assume that the radius of
the cord around the pulley remains constant at a value of 0.040 m during the
block’s descent. Find the angular acceleration of the pulley and the tension
in the cord.
PROBLEM 74
75. M BIO V-HINT The drawing shows an outstretched arm (0.61 m in length) that is parallel to the fl oor. The arm is pulling downward against
the ring attached to the pulley system, in order to hold the 98-N weight sta-
tionary. To pull the arm downward, the latissimus dorsi muscle applies the
force M →
in the drawing, at a point that is 0.069 m from the shoulder joint
and oriented at an angle of 29°. The arm has a weight of 47 N and a center
of gravity (cg) that is located 0.28 m from the shoulder joint. Find the mag-
nitude of M →
.
M
0.61 m
98 N
0.28 m
0.069 m
29°
Axis at shoulder
joint cg
PROBLEM 75
76. M GO A thin, rigid, uniform rod has a mass of 2.00 kg and a length of 2.00 m. (a) Find the moment of inertia of the rod relative to an axis that is perpendicular to the rod at one end. (b) Suppose all the mass of the rod were located at a single point. Determine the perpendicular distance of this point
from the axis in part (a), such that this point particle has the same moment
of inertia as the rod does. This distance is called the radius of gyration of the rod.
77. M SSM Available in WileyPLUS. 78. M GO Two identical wheels are moving on horizontal surfaces. The center of mass of each has the same linear speed. However, one wheel is
rolling, while the other is sliding on a frictionless surface without rolling.
Each wheel then encounters an incline plane. One continues to roll up the
incline, while the other continues to slide up. Eventually they come to a
momentary halt, because the gravitational force slows them down. Each
wheel is a disk of mass 2.0 kg. On the horizontal surfaces the center of
mass of each wheel moves with a linear speed of 6.0 m/s. (a) What is the
Additional Problems
Concepts and Calculations Problems 255
In this chapter we have seen that a rotational or angular acceleration results
when a net external torque acts on an object. In contrast, when a net external
force acts on an object, it leads to translational or linear acceleration, as dis-
cussed in Chapter 4. Torque and force are, then, fundamentally diff erent con-
cepts, and Problem 82 focuses on this fact. For rotational motion, the moment
of inertia and the net external torque determine the angular acceleration of
a rotating object, according to Newton’s second law. Newton’s second law
together with the equations of rotational kinematics are useful in accounting
for a wide variety of rotational motion. Problem 83 utilizes these concepts in
a situation where a rotating object is slowing down.
82. M CHALK The fi gure shows a uniform crate resting on a horizontal sur- face. The crate has a square cross section and a weight of W = 580 N, which is uniformly distributed. At the bottom right edge of the surface is a small ob-
struction that prevents the crate from sliding when a horizontal pushing force
P→ is applied to the left side. However, if this force is great enough, the crate will begin to tip and rotate over the obstruction. Concepts: (i) What causes the tipping—the force P→ or the torque that it creates? (ii) Where should P→ be applied so that a minimum force will be necessary to provide the necessary
torque? In other words, should the lever arm be a minimum or a maximum?
Calculations: Determine the minimum pushing force that leads to tipping.
Concepts and Calculations Problems
P
(a)
P
(b)
WObstruction Axis
p p
w
+x
+y
+
ℓ
ℓ
ℓ
(a) A horizontal pushing force P→ is applied to a uniform crate, which has a
square cross section and a weight W →
.
The crate rests on the ground, up against a
small obstruction. (b) Some of the forces acting on the crate and their lever arms.PROBLEM 82
total kinetic energy of each wheel? (b) Determine the maximum height reached by each wheel as it
moves up the incline.
79. H Available in WileyPLUS. 80. H MMH By means of a rope whose mass is negligible, two blocks are suspended over a pulley,
as the drawing shows. The pulley can be treated as a
uniform solid cylindrical disk. The downward accel-
eration of the 44.0-kg block is observed to be exactly
one-half the acceleration due to gravity. Noting that
the tension in the rope is not the same on each side of
the pulley, fi nd the mass of the pulley.
81. M GO SSM A crate of mass 451 kg is being lifted by the mechanism shown in part a of the fi gure. The two cables are wrapped around their respective pulleys, which have radii of 0.600 and 0.200 m. The pulleys are
fastened together to form a dual pulley and turn as a single unit about the
center axle, relative to which the combined moment of inertia is 46.0 kg · m2. The cables roll on the dual pulley without slipping. A tension of magnitude
2150 N is maintained in the cable attached to the motor. Find the angu-
lar acceleration of the dual pulley and the tension in the cable attached to
the crate. 11.0 kg
44.0 kg
PROBLEM 80
ℓ 1 = 0.600 m
Axis
Crate
Dual pulley
Motor
ℓ 2 = 0.200 mT1
P
+x
+τ
+y
ay
T2
T2́
(a) (b) Free-body diagram of pulley (c) Free-body diagram of crate
mg
Wp
PROBLEM 81
256 CHAPTER 9 Rotational Dynamics
83 M CHALK SSM Two spheres are each rotating at an angular speed of 24 rad/s about axes that pass through their centers. Each has a radius of 0.20 m
and a mass of 1.5 kg. However, as the fi gure shows, one is solid and the
other is a thin-walled spherical shell. Suddenly, a net external torque due to
friction (magnitude = 0.12 N · m) begins to act on each sphere and slows the motion down. Concepts: (i) Which sphere has the greater moment of inertia and why? (ii) Which sphere has the angular acceleration (a deceler-
ation) with the smaller magnitude? (iii) Which sphere takes a longer time
to come to a halt? Calculations: How long does it take each sphere to come to a halt? PROBLEM 83
Solid sphere Thin-walled spherical shell
ωω
84. M Smugglers. Rumor has it that a company has been smuggling gold out of the country using sealed, cylindrical barrels with hollow walls. They
pour molten gold into the hollows, and then fi ll the remainder of the barrel’s
internal volume with packing peanuts. The total mass of the gold-walled
barrel was designed so that it exactly matches those used to transport a volatile
chemical that cannot be exposed to air (and therefore the barrel cannot be
opened and checked). The X-ray machine usually used to screen containers
is suspiciously damaged and not available. (a) There are 20 barrels total, and they are all identical: mass m = 50.0 kg, height h = 1.20 m, and diameter D = 0.25 m. How do you determine which ones have walls fi lled with gold (and are essentially hollow on the interior except for packing peanuts) and
those completely fi lled with the volatile chemical (a tightly-packed powder)
where the mass is uniformly distributed? Hint: apply the concepts of mo-
ment of inertia. Assume that, in the case of the gold-fi lled barrels, the entire
mass is concentrated at the outer wall of the barrel and, in the case of the
barrels fi lled with the chemical, the mass is distributed evenly throughout the
volume of the cylinder. You can neglect the circular bottoms and the lids of
the barrels, and assume there is no slipping. (b) What is the acceleration of the center of mass of each of the barrels as they roll down a 30° inclined plane?
(c) How much time does it take each barrel to roll 10.0 m down the 30° plane? 85. M A Ride Inside a Tractor Tire. You and your friends plan to roll down a hill on the inside of 600-pound tractor tire (diameter D = 1.80 m). The hill is inclined at an angle of 25.0° and you initially plan to start from
a distance L = 100 m up the hill, but decide to fi rst check whether it will be safe. (a) Assuming the masses of the tire and your 105-pound body are con- centrated at the outer rim of a thin-walled cylinder/hoop, what is the eff ective
acceleration your body experiences at the bottom of the hill where your angu-
lar speed is greatest, i.e., how many “g’s” will you experience? Assuming the
human body can withstand a g-force of 8.00 g’s (1 g = 9.80 m/s2), is it safe
to make the ride from 100 m up the hill? (b) What is the maximum starting distance (Lmax) up the hill that is safe?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
10.1 Apply Hooke’s law to simple harmonic motion.
10.2 Apply simple harmonic motion relations to the reference circle.
10.3 Apply conservation-of-energy principles to solve simple harmonic motion problems involving springs.
10.4 Analyze pendulum motion.
10.5 Define damped harmonic motion.
10.6 Define driven harmonic motion.
10.7 Apply elastic deformations to define stress and strain.
10.8 Relate Hooke’s law to stress and strain. D
o n B
ar tl
et ti
/L o s
A n g el
es T
im es
/G et
ty I
m ag
es
CHAPTER 10
Simple Harmonic Motion and Elasticity
Sarah Reinertsen is a professional athlete who holds numerous world records in her disability division.
Her athletic performance is made possible by a high-tech prosthetic leg made of carbon fi ber, which fl exes
and stores elastic potential energy, like a spring does. The elastic potential energy stored by a spring is one
of the topics in this chapter.
10.1 The Ideal Spring and Simple Harmonic Motion Springs are familiar objects that have many applications, ranging from push-button
switches on electronic components, to automobile suspension systems, to mattresses. In
use, they can be stretched or compressed. For example, the top drawing in Figure 10.1 shows a spring being stretched. Here a hand applies a pulling force FxApplied to the spring. The subscript x reminds us that FxApplied lies along the x axis (not shown in the drawing), which is parallel to the length of the spring. In response, the spring stretches
and undergoes a displacement of x from its original, or “unstrained,” length. The bot- tom drawing in Figure 10.1 illustrates the spring being compressed. Now the hand applies a pushing force to the spring, and it again undergoes a displacement from its
unstrained length.
Experiment reveals that for relatively small displacements, the force FxApplied required to stretch or compress a spring is directly proportional to the displacement x,
257
258 CHAPTER 10 Simple Harmonic Motion and Elasticity
or FxApplied ∝ x. As is customary, this proportionality may be converted into an equation by intro- ducing a proportionality constant k:
F Appliedx = kx (10.1)
The constant k is called the spring constant, and Equation 10.1 shows that it has the dimensions of force per unit length (N/m). A spring that behaves according to FxApplied = kx is said to be an ideal spring. Example 1 illustrates one application of such a spring.
Unstrained length
x
x
Fx Applied
Fx AppliedFIGURE 10.1 An ideal spring obeys
the equation FxApplied = kx, where FxApplied is the force applied to the spring, x is the displacement of the spring from its
unstrained length, and k is the spring constant.
EXAMPLE 1 The Physics of a Tire Pressure Gauge
When a tire pressure gauge is pressed against a tire valve, as in Figure 10.2, the air in the tire pushes against a plunger attached to a spring. Suppose
the spring constant of the spring is k = 320 N/m and the bar indicator of the gauge extends 2.0 cm when the gauge is pressed against the tire valve.
What force does the air in the tire apply to the spring?
Reasoning We assume that the spring is an ideal spring, so that the relation FxApplied = kx is obeyed. The spring constant k is known, as is the displacement x. Therefore, we can determine the force applied to the spring.
Solution The force needed to compress the spring is given by Equa- tion 10.1 as
FxApplied = kx = (320 N/m)(0.020 m) = 6.4 N
Thus, the exposed length of the bar indicator indicates the force that the
air pressure in the tire exerts on the spring. We will see later that pres-
sure is force per unit area, so force is pressure times area. Since the area
of the plunger surface is fi xed, the bar indicator can be marked in units
of pressure.
2 .0
c m
Pressurized air
Tire valve
2 .0
c m
Plunger
Bar indicator
Fx Applied
FIGURE 10.2 In a tire pressure gauge, the pressurized
air from the tire exerts a force
FxApplied that compresses a spring.
Sometimes the spring constant k is referred to as the stiff ness of the spring, because a large value for k means the spring is “stiff ,” in the sense that a large force is required to stretch or compress it. Conceptual Example 2 examines what happens to the stiff ness of a spring when the
spring is cut into two shorter pieces.
10.1 The Ideal Spring and Simple Harmonic Motion 259
To stretch or compress a spring, a force must be applied to it. In accord with Newton’s third
law, the spring exerts an oppositely directed force of equal magnitude. This reaction force is
applied by the spring to the agent that does the pulling or pushing. In other words, the reaction
force is applied to the object attached to the spring. The reaction force is also called a “restoring
force,” for a reason that will be clarifi ed shortly. The restoring force of an ideal spring is obtained
from the relation FxApplied = kx by including the minus sign required by Newton’s action–reaction law, as indicated in Equation 10.2.
HOOKE’S LAW* RESTORING FORCE OF AN IDEAL SPRING The restoring force of an ideal spring is
Fx = −kx (10.2)
where k is the spring constant and x is the displacement of the spring from its unstrained length. The minus sign indicates that the restoring force always points in a direction opposite to the displacement of the spring from its unstrained length.
In Chapter 4 we encountered four types of forces: the gravitational force, the normal force,
frictional forces, and the tension force. These forces can contribute to the net external force,
which Newton’s second law relates to the mass and acceleration of an object. The restoring force
of a spring can also contribute to the net external force. Once again, we see the unifying theme
of Newton’s second law, in that individual forces contribute to the net force, which, in turn,
is responsible for the acceleration. Newton’s second law plays a central role in describing the
motion of objects attached to springs.
Interactive Figure 10.4 helps to explain why the phrase “restoring force” is used. In the picture, an object of mass m is attached to a spring on a frictionless table. In part A, the spring has been stretched to the right, so it exerts the leftward-pointing force Fx. When the object is
CONCEPTUAL EXAMPLE 2 Are Shorter Springs Stiff er Springs?
Figure 10.3a shows a 10-coil spring that has a spring constant k. When this spring is cut in half, so there are two 5-coil springs, is the spring
constant of each of the shorter springs (a) 12 k or (b) 2k?
Reasoning When the length of a spring is increased or decreased, the change in length is distributed over the entire spring. Greater forces are
required to cause changes that are a greater fraction of the spring’s ini-
tial length, since such changes distort the atomic structure of the spring
material to a greater extent.
Answer (a) is incorrect. When a force FxApplied is applied to the 10-coil spring, as in Figure 10.3a, the displacement of the spring from its unstrained length is x. If this same force were applied to a 5-coil spring that had a spring constant of
1
2 k, the displacement would be 2x because the spring is only half as stiff . Since this displacement would be a larger frac-
tion of the length of the 5-coil spring, it would require a force greater than
FxApplied, not equal to FxApplied. Therefore, the spring constant cannot be 1
2 k.
Answer (b) is correct. As indicated in Figure 10.3a, the displacement of the spring from its unstrained length is x when a force FxApplied is applied to the 10-coil spring. Figure 10.3b shows the spring divided in half between the fi fth and sixth coils (counting from the right). The spring is
in equilibrium, so the net force acting on the right half (coils 1–5) must be
zero. Thus, as part b shows, a force of −FxApplied must act on coil 5 in order to balance the force FxApplied that acts on coil 1. It is the adjacent coil 6 that exerts the force −FxApplied, and Newton’s action–reaction law now comes into play. It tells us that coil 5, in response, exerts an oppositely directed
force of equal magnitude on coil 6. In other words, the force FxApplied is also
exerted on the left half of the spring, as part b also indicates. As a result, the left half compresses by an amount that is one-half the displacement
x experienced by the 10-coil spring. We conclude, then, that the 5-coil spring must be twice as stiff as the 10-coil spring. In general, the spring
constant is inversely proportional to the number of coils in the spring, so
shorter springs are stiff er springs, other things being equal.
Related Homework: Problems 10, 19
FIGURE 10.3 (a) The 10-coil spring has a spring constant k. The applied force is FxApplied, and the displacement of the spring from its unstrained length is x. (b) The spring in part a is divided in half, so that the forces acting on the two 5-coil springs can be analyzed.
k
(a)
x
Fx Applied
–
(b)
Fx Applied
Fx Applied
Fx Applied
*As we will see in Section 10.8, Equation 10.2 is similar to a relationship fi rst discovered by Robert Hooke (1635–1703).
260 CHAPTER 10 Simple Harmonic Motion and Elasticity
released, this force pulls it to the left, restoring it toward its equilibrium position. However,
consistent with Newton’s fi rst law, the moving object has inertia and coasts beyond the equilibrium
position, compressing the spring as in part B. The force exerted by the spring now points to the right
and, after bringing the object to a momentary halt, acts to restore the object to its equilibrium posi-
tion. But the object’s inertia again carries it beyond the equilibrium position, this time stretching the
spring and leading to the restoring force Fx shown in part C. The back-and-forth motion illustrated in the drawing then repeats itself, continuing forever, since no friction acts on the object or the spring.
When the restoring force has the mathematical form given by Fx = –kx, the type of friction-free motion illustrated in Interactive Figure 10.4 is designated as “simple harmonic motion.” By attaching a pen to the object and moving a strip of paper past it at a steady rate, we can record the position of the vibrating object as time passes. Figure 10.5 illustrates the resulting graphical record of simple harmonic motion. The maximum excursion from equilibrium is the
amplitude A of the motion. The shape of this graph is characteristic of simple harmonic motion and is called “sinusoidal,” because it has the shape of a trigonometric sine or cosine function.
The restoring force also leads to simple harmonic motion when the object is attached to a
vertical spring, just as it does when the spring is horizontal. When the spring is vertical, however,
the weight of the object causes the spring to stretch, and the motion occurs with respect to the
equilibrium position of the object on the stretched spring, as Animated Figure 10.6 indicates. The amount of initial stretching d0 due to the weight can be calculated by equating the weight to the magnitude of the restoring force that supports it; thus, mg = kd0, which gives d0 = mg/k.
Unstrained length of the spring
x
x
A
B
x
C
Fx
Fx
Fx
INTERACTIVE FIGURE 10.4 The restoring force Fx (see blue arrows) produced by an
ideal spring always points
opposite to the displacement
x (see black arrows) of the spring and leads to a back-and-
forth motion of the object.
Displacement x
+A
–A
0 Time t
Pen
x = 0 m is the equilibrium position of the object.
Amplitude = A
Amplitude = A
FIGURE 10.5 When an object moves in simple harmonic motion, a graph of its position as a function of time has a sinusoidal shape with an amplitude A. A pen attached to the object records the graph.
Unstrained length
Equilibrium position
A
A d0
ANIMATED FIGURE 10.6 The weight of an object on a vertical spring stretches the
spring by an amount d0. Simple harmonic motion of amplitude A occurs with respect to the equilibrium position of the object on the
stretched spring.
10.2 Simple Harmonic Motion and the Reference Circle 261
Check Your Understanding
(The answers are given at the end of the book.) 1. A steel ball is dropped onto a very hard fl oor. Over and over again, the ball rebounds to its original
height (assuming that no energy is lost during the collision with the fl oor). Is the motion of the ball
simple harmonic motion?
2. CYU Figure 10.1 shows identical springs that are attached to a box in two diff erent ways. Initially, the springs are
unstrained. The box is then pulled to the right and released.
In each case the initial displacement of the box is the same.
At the moment of release, which box, if either, experiences
the greater net force due to the springs?
3. A 0.42-kg block is attached to the end of a horizontal ideal spring and rests on a frictionless surface. The block is pulled so that the spring stretches for 2.1 cm relative to its unstrained length. When the
block is released, it moves with an acceleration of 9.0 m/s2. What is the spring constant of the spring?
4. Two people pull on a horizontal spring that is attached to an immovable wall. Then, they detach it from the wall and pull on opposite ends of the horizontal spring. They pull just as hard in each case. In which
situation, if either, does the spring stretch more?
10.2 Simple Harmonic Motion and the Reference Circle Simple harmonic motion can be described in terms of displacement, velocity, and acceleration,
and the model in Figure 10.7 is helpful in explaining these characteristics. The model consists of a small ball attached to the top of a rotating turntable. The ball is moving in uniform circular
motion (see Section 5.1) on a path known as the reference circle. As the ball moves, its shadow falls on a strip of fi lm, which is moving upward at a steady rate and recording where the shadow
is. A comparison of the fi lm with the paper in Figure 10.5 reveals the same kind of patterns, sug- gesting that the model is useful.
Displacement Figure 10.8 shows the reference circle (radius = A) and indicates how to determine the displace- ment of the shadow on the fi lm. The ball starts on the x axis at x = +A and moves through the
CYU FIGURE 10.1
Light
Reference circle
Time t
Displacement x
FIGURE 10.7 The ball mounted on the turntable moves in uniform circular motion,
and its shadow, projected on a moving strip
of fi lm, executes simple harmonic motion.
262 CHAPTER 10 Simple Harmonic Motion and Elasticity
angle 𝜃 in a time t. The circular motion is uniform, so the ball moves with a constant angular speed 𝜔 (in rad/s), and the angle has a value (in rad) of 𝜃 = 𝜔t. The displacement x of the shadow is just the projection of the radius A onto the x axis:
x = A cos θ = A cos ωt (10.3)
Figure 10.9 shows a graph of this equation. As time passes, the shadow of the ball oscillates between the values of x = +A and x = −A, corresponding to the limiting values of +1 and −1 for the cosine of an angle. The radius A of the reference circle, then, is the amplitude of the simple harmonic motion.
As the ball moves one revolution or cycle around the reference circle, its shadow executes
one cycle of back-and-forth motion. For any object in simple harmonic motion, the time required
to complete one cycle is the period T, as Figure 10.9 indicates. The value of T depends on the angular speed 𝜔 of the ball because the greater the angular speed, the shorter the time it takes
to complete one revolution. We can obtain the relationship between 𝜔 and T by recalling that 𝜔 = Δ𝜃/Δt (Equation 8.2), where Δ𝜃 is the angular displacement of the ball and Δt is the time interval. For one cycle, ∆θ = 2π rad and ∆t = T, so that
ω = 2π T
(𝜔 in rad/s) (10.4)
Instead of the period, we often speak of the frequency f of the motion, the frequency being the number of cycles of the motion per second. For example, if an object on a spring completes
10 cycles in one second, the frequency is f = 10 cycles/s. The period T, or the time for one cycle, would be
1
10 s. Thus, frequency and period are related according to
f = 1
T (10.5)
Usually, one cycle per second is referred to as one hertz (Hz), the unit being named after Heinrich
Hertz (1857–1894). One thousand cycles per second is called one kilohertz (kHz). Thus, fi ve
thousand cycles per second, for instance, can be written as 5 kHz.
Using the relationships 𝜔 = 2𝜋/T and f = 1/T, we can relate the angular speed 𝜔 (in rad/s) to the frequency f (in cycles/s or Hz):
ω = 2π T
= 2πf (𝜔 in rad/s) (10.6)
Because 𝜔 is directly proportional to the frequency f, 𝜔 is often called the angular frequency.
Velocity The reference circle model can also be used to determine the velocity of an object in simple har-
monic motion. Figure 10.10 shows the tangential velocity vT→ of the ball on the reference circle. The drawing indicates that the velocity vx→ of the shadow is just the x component of the vector vT→ ; that is, 𝜐x = −𝜐T sin 𝜃, where 𝜃 = 𝜔t. The minus sign is necessary because vx→ points to the left, in
Film (top view)
x = 0 m
+ x x
x
A
Position at t = 0 s
Light
FIGURE 10.8 A top view of a ball on a turntable. The ball’s shadow on the fi lm has a
displacement x that depends on the angle 𝜃 through which the ball has moved on the
reference circle.
t
x
A+
A–
Period = T
1 cycle
FIGURE 10.9 For simple harmonic motion, the graph of displacement x versus time t is a sinusoidal curve. The period T is the time required for one complete motional cycle.
Film (top view)
x = 0 m
+ x
Light
vT vx
vx
FIGURE 10.10 The velocity vx→ of the ball’s shadow is the x component of the tangential velocity vx→ of the ball on the reference circle.
10.2 Simple Harmonic Motion and the Reference Circle 263
Simple harmonic motion is not just any kind of vibratory motion. It is a very specifi c kind
and, among other things, must have the velocity given by Equation 10.7. For instance, advertising
signs often use a “moving light” display to grab your attention. Conceptual Example 4 examines
the back-and-forth motion in one such display, to see whether it is simple harmonic motion.
EXAMPLE 3 The Physics of a Loudspeaker Diaphragm
The diaphragm of a loudspeaker moves back and forth in simple har-
monic motion to create sound, as in Figure 10.11. The frequency of the motion is f = 1.0 kHz and the amplitude is A = 0.20 mm. (a) What is the maximum speed of the diaphragm? (b) Where in the motion does this maximum speed occur?
Reasoning The maximum speed of an object vibrating in simple har- monic motion is υmax = Aω (𝜔 in rad/s), according to Equation 10.8. The angular frequency 𝜔 is related to the frequency f by ω = 2πf, according to Equation 10.6.
Solution (a) Using Equations 10.8 and 10.6, we fi nd that the maximum speed of the vibrating diaphragm is
υmax = Aω = A(2πf ) = (0.20 × 10−3 m)(2π) (1.0 × 103 Hz) = 1.3 m /s
(b) The speed of the diaphragm is zero when the diaphragm momentarily comes to rest at either end of its motion: x = +A and x = −A. Its maximum speed occurs midway between these two positions, or at x = 0 m.
Diaphragm
A A
x = 0 m
FIGURE 10.11 The diaphragm of a loudspeaker generates a sound by
moving back and forth in simple
harmonic motion.
the direction of the negative x axis. Since the tangential speed 𝜐T is related to the angular speed 𝜔 by 𝜐T = r𝜔 (Equation 8.9) and since r = A, it follows that 𝜐T = A𝜔. Therefore, the velocity in simple harmonic motion is given by
υx = −υT sin θ = −Aω sin ωt (𝜔 in rad/s) (10.7) This velocity is not constant, but varies between maximum and minimum values as time passes. When the shadow changes direction at either end of the oscillatory motion, the velocity is momen-
tarily zero. When the shadow passes through the x = 0 m position, the velocity has a maximum magnitude of A𝜔, since the sine of an angle is between +1 and −1: υmax = Aω (𝜔 in rad/s) (10.8) Both the amplitude A and the angular frequency 𝜔 determine the maximum velocity, as Example 3 emphasizes.
CONCEPTUAL EXAMPLE 4 Moving Lights
Over the entrance to a restaurant is mounted a strip of equally spaced light
bulbs, as Figure 10.12a illustrates. Starting at the left end, each bulb turns on in sequence for one-half second. Thus, a lighted bulb appears to move
from left to right. After the last bulb on the right turns on, the apparent
motion reverses. The lighted bulb then appears to move to the left, as part b of the drawing indicates. As a result, the lighted bulb appears to oscillate back
and forth. Is the apparent motion simple harmonic motion? (a) No (b) Yes Reasoning In simple harmonic motion the velocity of the moving object must have the velocity specifi ed by υ = −Aω sin ωt (Equation 10.7). This velocity is not constant as time passes.
Answer (b) is incorrect. Since the bulbs are equally spaced and each one remains lit for the same amount of time, the apparent motion in
Figure 10.12a (or in Figure 10.12b) occurs at a constant velocity and, therefore, cannot be simple harmonic motion.
Answer (a) is correct. The apparent motion is not simple harmonic motion. If it were, the speed would be zero at each end of the sign
and would increase to a maximum speed at the center, consistent with
(a)
(b)
FIGURE 10.12 The motion of a lighted bulb is from (a) left to right and then from (b) right to left.
Equation 10.7. However, the speed is constant because the bulbs are
equally spaced and each remains on for the same amount of time.
264 CHAPTER 10 Simple Harmonic Motion and Elasticity
Acceleration In simple harmonic motion, the velocity is not constant; consequently, there must be an accel-
eration. This acceleration can also be determined with the aid of the reference-circle model.
As Figure 10.13 shows, the ball on the reference circle moves in uniform circular motion, and, therefore, has a centripetal acceleration ac→ that points toward the center of the circle. The accel- eration ax→ of the shadow is the x component of the centripetal acceleration; ax = −ac cos θ. The minus sign is needed because the acceleration of the shadow points to the left. Recalling that the
centripetal acceleration is related to the angular speed ω by ac = r𝜔2 (Equation 8.11) and using r = A, we fi nd that ac = A𝜔2. With this substitution and the fact that 𝜃 = 𝜔t, the acceleration in simple harmonic motion becomes
ax = −ac cos θ = −Aω2 cos ωt (𝜔 in rad/s) (10.9)
The acceleration, like the velocity, does not have a constant value as time passes. The maximum magnitude of the acceleration is
amax = Aω2 (𝜔 in rad/s) (10.10)
Although both the amplitude A and the angular frequency 𝜔 determine the maximum value, the frequency has a particularly strong eff ect, because it is squared. Example 5 shows that the accel-
eration can be remarkably large in a practical situation.
Light
Film (top view)
x = 0 m
+ x
ac
ax
ax
θ
θ
FIGURE 10.13 The acceleration ax→ of the ball’s shadow is the x component of the centripetal acceleration ac→ of the ball on the reference circle.
Frequency of Vibration With the aid of Newton’s second law (ΣFx = max), it is possible to determine the frequency at which an object of mass m vibrates on a spring. We assume that the mass of the spring itself is negligible and that the only force acting on the object in the horizontal direction is due to the spring—that
is, the Hooke’s law restoring force. Thus, the net force is ΣFx = −kx, and Newton’s second law becomes −kx = max, where ax is the acceleration of the object. The displacement and acceleration of an oscillating spring are, respectively, x = A cos 𝜔t (Equation 10.3) and ax = −A𝜔2 cos 𝜔t (Equa- tion 10.9). Substituting these expressions for x and ax into the relation −kx = max, we fi nd that
−k(A cos ωt) = m(−Aω2 cos ωt)
which yields
ω = √ km (𝜔 in rad/s) (10.11)
EXAMPLE 5 The Loudspeaker Revisited—The Maximum Acceleration
The loudspeaker diaphragm in Figure 10.11 is vibrating at a frequency of f = 1.0 kHz, and the amplitude of the motion is A = 0.20 mm. (a) What is the maximum acceleration of the diaphragm, and (b) where does this maximum acceleration occur?
Reasoning The maximum acceleration of an object vibrating in simple harmonic motion is amax = A𝜔2 (𝜔 in rad/s), according to Equation 10.10. Equation 10.6 shows that the angular frequency 𝜔 is related to the
frequency f by 𝜔 = 2𝜋f.
Solution (a) Using Equations 10.10 and 10.6, we fi nd that the maximum acceleration of the vibrating diaphragm is
amax = Aω2 = A(2π f )2 = (0.20 × 10−3 m)[2π (1.0 × 103 Hz)] 2
= 7.9 × 103 m /s2
This is an incredible acceleration, being more than 800 times the accel-
eration due to gravity, and the diaphragm must be built to withstand it.
(b) The maximum acceleration occurs when the force acting on the dia- phragm is a maximum. The maximum force arises when the diaphragm
is at the ends of its path, where the displacement is greatest. Thus, the
maximum acceleration occurs at x = +A and x = −A in Figure 10.11.
Math Skills The angular frequency 𝜔 and the vibration fre- quency f are not the same thing, so you will need to be careful to distinguish between them when solving problems. The two quanti-
ties are proportional, but they diff er by a factor of 2𝜋. The relation
between them is
ω = 2πf (10.6)
You can always tell which quantity is being referred to in a problem
by looking at the given data. A value for 𝜔 is given in radians per second, whereas a value for f is given in hertz (cycles per second).
10.2 Simple Harmonic Motion and the Reference Circle 265
In this expression, the angular frequency 𝜔 must be in radians per second. Larger spring con-
stants k and smaller masses m result in larger frequencies. Example 6 illustrates an application of Equation 10.11.
Analyzing Multiple-Concept Problems
EXAMPLE 6 BIO The Physics of a Body-Mass Measurement Device
Astronauts who spend a long time in orbit measure their body masses
as part of their health-maintenance programs. On earth, it is simple to
measure body weight W with a scale and convert it to mass m using the magnitude g of the acceleration due to gravity, since W = mg. However, this procedure does not work in orbit, because both the scale and the as-
tronaut are in free fall and cannot press against each other (see Conceptual
Example 12 in Chapter 5). Instead, astronauts use a body-mass measurement
device, as Figure 10.14 illustrates. The device consists of a spring-mount- ed chair in which the astronaut sits. The chair is then started oscillating in
simple harmonic motion. The period of the motion is measured electroni-
cally and is automatically converted into a value of the astronaut’s mass,
after the mass of the chair is taken into account. The spring used in one
such device has a spring constant of 606 N/m, and the mass of the chair
is 12.0 kg. The measured oscillation period is 2.41 s. Find the mass of
the astronaut.
Reasoning Since the astronaut and chair are oscillating in simple har- monic motion, the total mass mtotal of the two is related to the angular
frequency 𝜔 of the motion by ω = √k /m total, or mtotal = k/𝜔2. The angular frequency, in turn, is related to the period of the motion by ω = 2π/T . These two relations will enable us to fi nd the total mass of the astronaut
and chair. From this result, we will subtract the mass of the chair to obtain
the mass of the astronaut.
Knowns and Unknowns The data for this problem are:
Description Symbol Value Spring constant k 606 N/m
Mass of chair mchair 12.0 kg
Period of oscillation T 2.41 s
Unknown Variable Mass of astronaut mastro ?
FIGURE 10.14 Astronaut Millie Hughes- Fulford trains to use a body-mass measurement
device developed for determining mass in
orbit.C o u rt
es y N
A S
A
Modeling the Problem
STEP 1 Angular Frequency of Vibration The mass mastro of the astronaut is equal to the total mass mtotal of the astronaut and chair minus the mass mchair of the chair:
mastro = mtotal − mchair (1)
The mass of the chair is known. Since the astronaut and chair oscillate in simple harmonic motion,
the angular frequency 𝜔 of the oscillation is related to the spring constant k of the spring and the total mass mtotal by Equation 10.11:
ω = √ kmtotal or mtotal = k
ω2
Substituting this result for mtotal into Equation 1 gives Equation 2 at the right. The spring con- stant and mass of the chair are known, but the angular frequency 𝜔 is not; we will evaluate it in
Step 2.
mastro = k
ω2 − mchair (2)
?
266 CHAPTER 10 Simple Harmonic Motion and Elasticity
STEP 2 Angular Frequency and Period The angular frequency 𝜔 of the oscillating motion is inversely related to its period T by
ω = 2π T
(10.4)
All the variables on the right side of this equation are known, and we substitute it into Equation 2, as indicated in the right column.
Solution Algebraically combining the results of the steps above, we have:
mastro = k
ω2 − mchair =
k
( 2π T )
2 − mchair =
kT 2
4π 2 − mchair
= (606 N/m)(2.41 s)2
4π 2 − 12.0 kg = 77.2 kg
Related Homework: Problems 77, 83
STEP 2STEP 1
mastro = k
ω2 − mchair (2)
ω = 2π T
(10.4)
THE PHYSICS OF . . . detecting and measuring small amounts of chemicals. Example 6 indicates that the mass of the vibrating object infl uences the frequency of simple harmonic motion. Electronic sensors are being developed that take advantage of this eff ect in detecting and measuring small amounts of chemicals. These sensors utilize tiny quartz crystals that vibrate when an electric current passes through them. If a crystal is coated with a substance that absorbs a particular chemical, then the mass of the coated crystal increases as the chemical is absorbed and, according to the relation f = 12π √k /m (Equations 10.6 and 10.11), the frequency of the simple harmonic motion decreases. The change in frequency is detected electronically, and the sensor is calibrated to give the mass of the absorbed chemical.
Check Your Understanding
(The answers are given at the end of the book.) 5. CYU Figure 10.2 shows plots of the displace-
ment x versus the time t for three objects under- going simple harmonic motion. Which object— I, II, or III—has the greatest maximum velocity?
6. In Figure 10.13 the shadow moves in simple harmonic motion. Where on the path of the shadow is the acceleration equal to zero?
7. A particle is oscillating in simple harmonic motion. The time required for the particle to travel through one complete cycle is equal to the period of the motion, no matter what the ampli- tude is. But how can this be, since larger ampli- tudes mean that the particle travels farther?
A
3A
2A
Object III
Object II
Object I +t
+x
CYU FIGURE 10.2
10.3 Energy and Simple Harmonic Motion 267
10.3 Energy and Simple Harmonic Motion We saw in Chapter 6 that an object above the surface of the earth has gravitational potential
energy. Therefore, when the object is allowed to fall, like the hammer of the pile driver in
Figure 6.13, it can do work. A spring also has potential energy when the spring is stretched or
compressed, which we refer to as elastic potential energy. Because of elastic potential energy, a stretched or compressed spring can do work on an object that is attached to the spring. THE PHYSICS OF . . . a door-closing unit. For instance, Figure 10.15 shows a door-closing unit that is often found on screen doors. When the door is opened, a spring inside the unit is
compressed and has elastic potential energy. When the door is released, the compressed spring
expands and does the work of closing the door.
To fi nd an expression for the elastic potential energy, we will determine the work done
by the spring force on an object. Figure 10.16 shows an object attached to one end of a stretched spring. When the object is released, the spring contracts and pulls the object from
its initial position x0 to its fi nal position xf. The work W done by a constant force is given by Equation 6.1 as W = (F cos 𝜃)s, where F is the magnitude of the force, s is the magnitude of the displacement (s = x0 − xf), and 𝜃 is the angle between the force and the displacement. The magnitude of the spring force is not constant, however. Equation 10.2 gives the spring force
as Fx = −kx, and as the spring contracts, the magnitude of this force changes from kx0 to kxf. In using Equation 6.1 to determine the work, we can account for the changing magnitude by
using an average magnitude Fx in place of the constant magnitude Fx. Because the dependence of the spring force on x is linear, the magnitude of the average force is just one-half the sum of the initial and fi nal values, or Fx =
1
2 (kx0 + kxf ) . The work Welastic done by the average spring force is, then,
Welastic = (Fx cos θ)s = 1
2 (kx0 + kxf) (cos 0°) (x0 − xf)
Welastic = 1
2 kx0 2 − 1
2 kxf 2 (10.12)
In the calculation above, 𝜃 is 0°, since the spring force has the same direction as the displacement.
Equation 10.12 indicates that the work done by the spring force is equal to the diff erence between
the initial and fi nal values of the quantity 1
2 kx2. The quantity 1
2 kx2 is analogous to the quantity mgh, which we identifi ed in Section 6.3 as the gravitational potential energy. Here, the quantity 1
2 kx2 is the elastic potential energy. Equation 10.13 indicates that the elastic potential energy is a maximum for a fully stretched or compressed spring and zero for a spring that is neither stretched
nor compressed (x = 0 m).
DEFINITION OF ELASTIC POTENTIAL ENERGY The elastic potential energy PEelastic is the energy that a spring has by virtue of being stretched or compressed. For an ideal spring that has a spring constant k and is stretched or compressed by an amount x relative to its unstrained length, the elastic potential energy is
PEelastic = 1
2 kx2 (10.13)
SI Unit of Elastic Potential Energy: joule (J)
The total mechanical energy E is a familiar idea that we originally defi ned to be the sum of the translational kinetic energy and the gravitational potential energy (see Section 6.5). Then,
we included the rotational kinetic energy (see Section 9.5). We now expand the total mechanical
energy to include the elastic potential energy, as shown in Equation 10.14.
E = 12 mυ 2 + 1
2 Iω2 + mgh + 1
2 kx2 (10.14)
⏟⏟⏟ Initial elastic
potential energy
⏟⏟⏟ Final elastic
potential energy
⏟⏟⏟ Total
mechanical
energy
⏟⏟⏟ Translational
kinetic
energy
⏟⏟⏟ Rotational
kinetic
energy
⏟⏟⏟ Gravitational
potential
energy
⏟⏟⏟ Elastic
potential
energy
Compressed spring
FIGURE 10.15 A door-closing unit. The elastic potential energy stored in the
compressed spring is used to close the door.
Position when spring is unstrained
x0 xf
FIGURE 10.16 When the object is released, its displacement changes from an initial value
of x0 to a fi nal value of xf.
268 CHAPTER 10 Simple Harmonic Motion and Elasticity
As Section 6.5 discusses, the total mechanical energy is conserved when external nonconser-
vative forces (such as friction) do no net work; that is, when Wnc = 0 J. Then, the fi nal and initial values of E are the same: Ef = E0. The principle of conservation of total mechanical energy is the subject of the next example.
EXAMPLE 7 An Object on a Horizontal Spring
Interactive Figure 10.17 shows an object of mass m = 0.200 kg that is vibrating on a horizontal frictionless table. The spring has a spring
constant of k = 545 N/m. The spring is stretched initially to x0 = 4.50 cm and is then released from rest (see part A of the drawing). Determine the fi nal translational speed 𝜐f of the object when the fi nal displacement of the
spring is (a) xf = 2.25 cm and (b) xf = 0 cm.
Reasoning The conservation of mechanical energy indicates that, in the absence of friction (a nonconservative force), the fi nal and initial total
mechanical energies are the same:
Ef = E0
1
2 mυf 2 + 1
2 Iωf 2 + mghf + 1
2 kxf 2 = 1
2 mυ0 2 + 1
2 Iω0 2 + mgh0 + 1
2 kx0 2
Since the object is moving on a horizontal table, the fi nal and initial
heights are the same: hf = h0. The object is not rotating, so its angular speed is zero: 𝜔f = 𝜔0 = 0 rad/s. Also, as the problem states, the initial
translational speed of the object is zero, 𝜐0 = 0 m/s. With these substitu-
tions, the conservation-of-energy equation becomes
1
2 mυf 2 + 1
2 kxf 2 = 1
2 kx0 2
from which we can obtain 𝜐f:
υf = √ km (x02 − xf2) Solution (a) Since x0 = 0.0450 m and xf = 0.0225 m, the fi nal transla- tional speed is
υ f = √545 N/m0.200 kg [(0.0450 m)2 − (0.0225 m)2] = 2.03 m/s The total mechanical energy at this point is composed partly of transla-
tional kinetic energy ( 1
2 mυf 2 = 0.414 J ) and partly of elastic potential energy (
1
2 kxf 2 = 0.138 J), as indicated in part B of Interactive Figure 10.17. The
total mechanical energy E is the sum of these two energies: E = 0.414 J + 0.138 J = 0.552 J. Because the total mechanical energy remains constant
during the motion, this value equals the initial total mechanical energy
when the object is stationary and the energy is entirely elastic potential
energy (E0 = 1
2 kx 20 = 0.552 J).
(b) When x0 = 0.0450 m and xf = 0 m, we have
υ f = √ km (x02 − x f2) = √ 545 N/m
0.200 kg [(0.0450 m) 2 − (0 m) 2]
= 2.35 m/s
Now the total mechanical energy is due entirely to the translational kinetic
energy ( 1
2 mυ 2f = 0.552 J), since the elastic potential energy is zero (see part C of Interactive Figure 10.17). Note that the total mechanical energy is the same as it is in Solution part (a). In the absence of friction, the
simple harmonic motion of a spring converts the diff erent types of energy
between one form and another, the total always remaining the same.
A
B
C
xf = 0 cm
xf
x0
v0 = 0 m/s
INTERACTIVE FIGURE 10.17 The total mechanical energy of this system
is entirely elastic potential energy (A), partly elastic potential energy and partly
kinetic energy (B), and entirely kinetic energy (C).
Conceptual Example 8 takes advantage of energy conservation to illustrate what happens to
the maximum speed, amplitude, and angular frequency of a simple harmonic oscillator when its
mass is changed suddenly at a certain point in the motion.
CONCEPTUAL EXAMPLE 8 Changing the Mass of a Simple Harmonic Oscillator
Figure 10.18a shows a box of mass m attached to a spring that has a force constant k. The box rests on a horizontal, frictionless surface. The spring is initially stretched to x = A and then released from rest. The box executes simple harmonic motion that is characterized by a maximum
speed 𝜐x max, an amplitude A, and an angular frequency 𝜔. When the box
is passing through the point where the spring is unstrained (x = 0 m), a second box of the same mass m and speed 𝜐xmax is attached to it, as in part b of the drawing. Discuss what happens to (a) the maximum speed,
(b) the amplitude, and (c) the angular frequency of the subsequent simple harmonic motion.
Reasoning and Solution (a) The maximum speed of an object in simple harmonic motion occurs when the object is passing through the point where
the spring is unstrained (x = 0 m), as in Figure 10.18b. Since the second box is attached at this point with the same speed, the maximum speed of the two-box system remains the same as that of the one-box system.
10.3 Energy and Simple Harmonic Motion 269
In the previous two examples, gravitational potential energy plays no role because the spring
is horizontal. The next example illustrates that gravitational potential energy must be taken into
account when a spring is oriented vertically.
(b) At the same speed, the maximum kinetic energy of the two boxes is twice that of a single box, since the mass is twice as much. Subsequently,
when the two boxes move to the left and compress the spring, their kinetic
energy is converted into elastic potential energy. Since the two boxes have
twice as much kinetic energy as one box alone, the two will have twice as
much elastic potential energy when they come to a halt at the extreme left.
Here, we are using the principle of conservation of mechanical energy,
which applies since friction is absent. But the elastic potential energy is
proportional to the amplitude squared (A2) of the motion, so the ampli- tude of the two-box system is √2 times as great as that of the one-box system.
(c) The angular frequency 𝜔 of a simple harmonic oscillator is 𝜔 = √k /m (Equation 10.11). Since the mass of the two-box system is twice the mass
of the one-box system, the angular frequency of the two-box system is √2 times as small as that of the one-box system.
Related Homework: Problem 39
m
m
(a)
(b)
m
x = 0 m
� x max
x = A 0 = 0 m/s�
� x max
� x max
x = 0 m
FIGURE 10.18 (a) A box of mass m, starting from rest at x = A, undergoes simple harmonic motion about x = 0 m. (b) When x = 0 m, a second box, with the same mass and speed, is attached.
Zero level for gravitational potential energy
Unstrained spring
h0
hf = 0 m
FIGURE 10.19 The ball is supported initially so that the spring is unstrained.
After being released from rest, the ball
falls through the distance h0 before being momentarily stopped by the spring.
EXAMPLE 9 A Falling Ball on a Vertical Spring
A 0.20-kg ball is attached to a vertical spring, as in Figure 10.19. The spring constant of the spring is 28 N/m. The ball, supported initially so
that the spring is neither stretched nor compressed, is released from rest.
In the absence of air resistance, how far does the ball fall before being
brought to a momentary stop by the spring?
Reasoning Since air resistance is absent, only the conservative forces of gravity and the spring act on the ball. Therefore, the principle of con-
servation of mechanical energy applies:
Ef = E0
1
2 mυf 2 + 1
2Iω f 2 + mghf + 1
2 kyf 2 = 1
2 mυ0 2 + 1
2Iω0 2 + mgh0 + 1
2 ky0 2
Note that we have replaced x with y in the elastic-potential-energy terms (
1
2 kyf 2 and 1
2 ky02) , in recognition of the fact that the spring is moving in the vertical direction. The problem states that the fi nal and initial trans-
lational speeds of the ball are zero: 𝜐f = 𝜐0 = 0 m/s. The ball and spring
do not rotate; therefore, the fi nal and initial angular speeds are also zero:
𝜔f = 𝜔0 = 0 rad/s. As Figure 10.19 indicates, the initial height of the ball is h0, and the fi nal height is hf = 0 m. In addition, the spring is unstrained (y0 = 0 m) to begin with, and so it has no elastic potential energy initially. With these substitutions, the conservation-of-mechanical-energy equation
reduces to
1
2 kyf 2 = mgh0
This result shows that the initial gravitational potential energy (mgh0) is converted into elastic potential energy (
1
2 ky 2f ) .When the ball falls to its lowest point, its displacement is yf = −h0, where the minus sign indicates that the displacement is downward. Substituting this result into the equa-
tion above and solving for h0 yields h0 = 2mg/k.
Problem-Solving Insight When evaluating the total mechan- ical energy E, always include a potential energy term for every conservative force acting on the system. In Example 9 there are two such terms, gravitational and elastic.
Solution The distance that the ball falls before coming to a momentary halt is
h0 = 2mg
k =
2(0.20 kg)(9.8 m/s2 )
28 N/m = 0.14 m
270 CHAPTER 10 Simple Harmonic Motion and Elasticity
Check Your Understanding
(The answers are given at the end of the book.) 8. Is more elastic potential energy stored in a spring when the spring is compressed by one centimeter than
when it is stretched by the same amount?
9. A block is attached to the end of a horizontal ideal spring and rests on a frictionless surface. The block is pulled so that the spring stretches relative to its unstrained length. In each of the following three
cases, the spring is stretched initially by the same amount. Rank the amplitudes of the resulting simple
harmonic motion in decreasing order (largest fi rst). (a) The block is released from rest. (b) The block is given an initial speed 𝜐0. (c) The block is given an initial speed 12 υ0.
10. A block is attached to a horizontal spring and slides back and forth on a frictionless horizontal surface. A second identical block is suddenly attached to the fi rst block. The attachment is accomplished by
joining the blocks at one extreme end of the oscillation cycle. The velocities of the blocks are exactly
matched at the instant of joining. How do the (a) amplitude, (b) frequency, and (c) maximum speed of the simple harmonic motion change?
10.4 The Pendulum A simple pendulum consists of a particle of mass m, attached to a frictionless pivot P by a cable of length L and negligible mass. When the particle is pulled away from its equilibrium position by an angle 𝜃 and released, it swings back and forth as Figure 10.20 shows. By attaching a pen to the bottom of the swinging particle and moving a strip of paper beneath
it at a steady rate, we can record the position of the particle as time passes. The graphical
record reveals a pattern that is similar (but not identical) to the sinusoidal pattern for simple
harmonic motion.
Gravity causes the back-and-forth rotation about the axis at P. The rotation speeds up as the particle approaches the lowest point and slows down on the upward part of the swing. Eventu-
ally the angular speed is reduced to zero, and the particle swings back. As Section 9.4 discusses,
a net torque is required to change the angular speed. The gravitational force mg→ produces this torque. (The tension T→ in the cable creates no torque, because it points directly at the pivot P and, therefore, has a zero lever arm.) According to Equation 9.1, the magnitude of the torque 𝜏 is the
product of the magnitude mg of the gravitational force and the lever arm ℓ, so that 𝜏 = −(mg)ℓ. The minus sign is included since the torque is a restoring torque; it acts to reduce the angle 𝜃 [the
angle 𝜃 is positive (counterclockwise), while the torque is negative (clockwise)]. The lever arm ℓ
is the perpendicular distance between the line of action of mg→ and the pivot P. In Figure 10.20, ℓ is very nearly equal to the arc length s of the circular path when the angle 𝜃 is small (about 10° or less). Furthermore, if 𝜃 is expressed in radians, the arc length and the radius L of the circular path are related, according to s = L𝜃 (Equation 8.1). It follows, then, that ℓ ≈ s = L𝜃, and the gravitational torque is
τ ≈ −mgL θ
In the equation above, the term mgL has a constant value kʹ, independent of 𝜃. For small angles, then, the torque that restores the pendulum to its vertical equilibrium position is pro- portional to the angular displacement 𝜃. The expression 𝜏 = −kʹ𝜃 has the same form as the Hooke’s law restoring force for an ideal spring, F = −kx. Therefore, we expect the frequency of the back-and-forth movement of the pendulum to be given by an equation analogous to
Equation 10.11 (ω = 2π f = √k /m). In place of the spring constant k, the constant k ′ = mgL will appear, and, as usual in rotational motion, in place of the mass m, the moment of inertia I will appear:
ω = 2πf = √mgLI (small angles only) (10.15)
{
kʹ
P
Pen
L
mg
s
P
L
T
θ
𝓁
FIGURE 10.20 A simple pendulum swinging back and forth about the pivot P. If the angle 𝜃 is small (about 10° or less), the swinging is
approximately simple harmonic motion.
10.4 The Pendulum 271
The moment of inertia of a particle of mass m, rotating at a radius r = L about an axis, is given by I = mL2 (Equation 9.6). Substituting this expression for I into Equation 10.15 reveals that for a simple pendulum
Simple pendulum ω = 2π f = √gL (small angles only) (10.16) The mass of the particle has been eliminated algebraically from this expression, so only the
length L and the magnitude g of the acceleration due to gravity determine the frequency of a simple pendulum. If the angle of oscillation is large, the pendulum does not exhibit simple har-
monic motion, and Equation 10.16 does not apply. Equation 10.16 provides the basis for using a
pendulum to keep time, as Example 10 demonstrates.
R o b er
t M
at h en
a/ F
u n d am
en ta
l P
h o to
g ra
p h s
FIGURE 10.21 This pendulum clock keeps time as the pendulum swings back and forth.
EXAMPLE 10 Keeping Time
Figure 10.21 shows a clock that uses a pendulum to keep time. Determine the length of a simple pendulum that will swing back and forth in simple
harmonic motion with a period of 1.00 s.
Reasoning When a simple pendulum is swinging back and forth in simple harmonic motion, its frequency f is given by Equation 10.16 as f = 12π √g /L, where g is the magnitude of the acceleration due to gravity and L is the length of the pendulum. We also know from Equation 10.5
that the frequency is the reciprocal of the period T, so f = 1/T. Thus, the equation above becomes 1/T = 12π √g/L. We can solve this equation for the length L.
Solution The length of the pendulum is
L = T 2g 4π2
= (1.00 s) 2(9.80 m /s2 )
4π2 = 0.248 m
It is not necessary that the object in Figure 10.20 be a particle at the end of a cable. It may be a rigid extended object, in which case the pendulum is called a physical pendulum. For small oscillations, Equation 10.15 still applies, but the moment of inertia I is no longer mL2. The proper value for the rigid object must be used. (See Section 9.4 for a discussion of moment of inertia.) In
addition, the length L for a physical pendulum is the distance between the axis at P and the center of gravity of the object. The next example deals with an important type of physical pendulum.
272 CHAPTER 10 Simple Harmonic Motion and Elasticity
Analyzing Multiple-Concept Problems
EXAMPLE 11 BIO The Physics of Walking
When we walk, our legs alternately swing forward about the hip joint as a
pivot. In this motion the leg is acting approximately as a physical pendu-
lum. Treating the leg as a thin uniform rod of length 0.80 m, fi nd the time
it takes for the leg to swing forward.
Reasoning The time it takes for the leg to swing forward is one-half of the period T of the pendulum motion, which is related to the frequency f of the motion by T = 1/f (Equation 10.5). The frequency of a physical pendulum is given by f = 12π √mgL /I (Equation 10.15), where m and I are, respectively, its mass and moment of inertia, and L is the distance between the pivot at the hip joint and the center of gravity of the leg. By
combining these two relations we will be able to fi nd the time it takes for
the leg to swing forward.
Knowns and Unknowns The data for this problem are:
Description Symbol Value Length of leg L leg 0.80 m
Unknown Variable Time for leg to swing forward t ?
t = 12 (1f ) (1)
?
t = 12 (1f ) (1)
f = 1
2π√ mg(12Lleg)
I (2)
?
t = 12 (1f ) (1)
f = 1
2π√ mg(12Lleg)
I (2)
I = 13 mL 2leg
Modeling the Problem
STEP 1 Period and Frequency The time t it takes for the leg to swing forward is one-half the period T, or
t = 12 T
The period, in turn, is related to the frequency f by T = 1/f (see Equation 10.5). Substituting this expression for T into the equation above for t gives Equation 1 at the right. The frequency of oscillation will be evaluated in Step 2.
STEP 2 The Frequency of a Physical Pendulum According to Equation 10.15, the frequency of a physical pendulum is given by
f = 1
2π√ mgL
I (10.15)
Since the leg is being approximated as a thin uniform rod, the distance L between the pivot and the center of gravity is one-half the length Lleg of the leg, so L =
1
2 L leg. Using this relation in Equation 10.15 gives Equation 2 at the right, which we then substitute into Equation 1, as shown.
The moment of inertia I will be evaluated in Step 3.
STEP 3 Moment of Inertia The leg is being approximated as a thin uniform rod of length Lleg that rotates about an axis that is perpendicular to one end. The moment of inertia I for such an object is given in Table 9.1 as
I = 13 mL 2leg
We substitute this expression for I into Equation 2, as shown in the right column.
Solution Algebraically combining the results of the steps above, we have:
t = 12 (1f ) = 12[ 1
1
2π √ mg (12L leg)
I ] = 12[ 1
1
2π √ mg (12L leg)
1
3mL leg 2 ]
= π √2L leg3g = π √ 2(0.80 m)
3(9.80 m/s2 ) = 0.73 s
Note that the mass m is algebraically eliminated from the fi nal result.
Related Homework: Problems 48, 49
STEP 2 STEP 3STEP 1
10.5 Damped Harmonic Motion 273
Check Your Understanding
(The answers are given at the end of the book.) 11. Suppose that a grandfather clock (a simple pendulum) is running slowly; that is, the time it takes to
complete each cycle is greater than it should be. Should you (a) shorten or (b) lengthen the pendulum to make the clock keep correct time?
12. Consult Concept Simulation 10.2 at www.wiley.com/college/cutnell to review the concept that is im- portant here. In principle, the motions of a simple pendulum and an object on an ideal spring can both
be used to provide the basic time interval or period used in a clock. Which of the two kinds of clocks
becomes more inaccurate when carried to the top of a high mountain?
13. Concept Simulation 10.2 at www.wiley.com/college/cutnell deals with the concept on which this question is based. Suppose you were kidnapped and held prisoner by space invaders in a completely
isolated room, with nothing but a watch and a pair of shoes (including shoe laces of known length).
How could you determine whether you were on earth or on the moon?
14. Two people are sitting on identical playground swings. One is pulled back 4° from the vertical and the other is pulled back 8°. They are both released at the same instant. Will they both come back to their
starting points at the same time? Assume simple-pendulum motion.
10.5 Damped Harmonic Motion In simple harmonic motion, an object oscillates with a constant amplitude, because there is no
mechanism for dissipating energy. In reality, however, friction or some other energy-dissipating
mechanism is always present. In the presence of energy dissipation, the oscillation amplitude
decreases as time passes, and the motion is no longer simple harmonic motion. Instead, it is
referred to as damped harmonic motion, the decrease in amplitude being called “damping.” THE PHYSICS OF . . . a shock absorber. One widely used application of damped
harmonic motion is in the suspension system of an automobile. Figure 10.22a shows a shock absorber attached to a main suspension spring of a car. A shock absorber is designed to introduce
damping forces, which reduce the vibrations associated with a bumpy ride. As part b of the draw- ing shows, a shock absorber consists of a piston in a reservoir of oil. When the piston moves in
response to a bump in the road, holes in the piston head permit the piston to pass through the oil.
Viscous forces that arise during this movement cause the damping.
Figure 10.23 illustrates the diff erent degrees of damping that can exist. As applied to the example of a car’s suspension system, these graphs show the vertical position of the chassis after
it has been pulled upward by an amount A0 at time t0 = 0 s and then released. Part a of the fi gure compares undamped or simple harmonic motion in curve 1 (red) to slightly damped motion in
curve 2 (green). In damped harmonic motion, the chassis oscillates with decreasing amplitude
and eventually comes to rest. As the degree of damping is increased from curve 2 to curve 3
(gold), the car makes fewer oscillations before coming to a halt.
Figure 10.23b shows that as the degree of damping is increased further, there comes a point when the car does not oscillate at all after it is released but, rather, settles directly back to its equilibrium
position, as in curve 4 (blue). The smallest degree of damping that completely eliminates the oscil-
lations is termed “critical damping,” and the motion is said to be critically damped. Figure 10.23b
Shock absorber
Suspension spring( )a
Oil
Hole
Piston
( )b
FIGURE 10.22 (a) A shock absorber mounted in the suspension system of an
automobile and (b) a simplifi ed, cutaway view of the shock absorber.
A0
Vertical position
Time
( )b
4
5A0
Vertical position
Time
( )a 3
1
2
FIGURE 10.23 Damped harmonic motion. The degree of damping increases from curve 1 to curve 5. Curve 1 (red) represents undamped or simple harmonic motion. Curves 2 (green) and 3 (gold) show
underdamped motion. Curve 4 (blue) represents critically damped harmonic motion. Curve 5 (purple)
shows overdamped motion.
274 CHAPTER 10 Simple Harmonic Motion and Elasticity
also shows that the car takes the longest time to return to its equilibrium position in curve 5 (purple),
where the degree of damping is above the value for critical damping. When the damping exceeds
the critical value, the motion is said to be overdamped. In contrast, when the damping is less than the critical level, the motion is said to be underdamped (curves 2 and 3). Typical automobile shock absorbers are designed to produce underdamped motion somewhat like that in curve 3.
Check Your Understanding
(The answer is given at the end of the book.) 15. The shock absorbers on a car are badly in need of replacement and introduce very little damping. Does
the number of occupants in the car aff ect the vibration frequency of the car’s suspension system?
10.6 Driven Harmonic Motion and Resonance In damped harmonic motion, a mechanism such as friction dissipates or reduces the energy of
an oscillating system, with the result that the amplitude of the motion decreases in time. This
section discusses the opposite eff ect—namely, the increase in amplitude that results when energy
is continually added to an oscillating system.
To set an object on an ideal spring into simple harmonic motion, some agent must apply
a force that stretches or compresses the spring initially. Suppose that this force is applied at all
times, not just for a brief initial moment. The force could be provided, for example, by a person
who simply pushes and pulls the object back and forth. The resulting motion is known as driven harmonic motion, because the additional force drives or controls the behavior of the object to a large extent. The additional force is identifi ed as the driving force.
Figure 10.24 illustrates one particularly important example of driven harmonic motion. Here, the driving force has the same frequency as the spring system and always points in the
direction of the object’s velocity. The frequency of the spring system is f = 12π √k /m and is called a natural frequency because it is the frequency at which the spring system naturally oscillates. Since the driving force and the velocity always have the same direction, positive work is done on the
object at all times, and the total mechanical energy of the system increases. As a result, the ampli-
tude of the vibration becomes larger and will increase without limit if there is no damping force
to dissipate the energy being added by the driving force. The situation depicted in Figure 10.24 is known as resonance.
RESONANCE Resonance is the condition in which a time-dependent force can transmit large amounts of energy to an oscillating object, leading to a large-amplitude motion. In the absence of damping, resonance occurs when the frequency of the force matches a natural frequency at which the object will oscillate.
The role played by the frequency of a driving force is a critical one. The matching of this fre-
quency with a natural frequency of vibration allows even a relatively weak force to produce a
large-amplitude vibration, because the eff ect of each push–pull cycle is cumulative.
THE PHYSICS OF . . . high tides at the Bay of Fundy. Resonance can occur with any object that can oscillate, and springs need not be involved. The greatest tides in the world occur in
the Bay of Fundy, which lies between the Canadian provinces of New Brunswick and Nova Scotia.
Figure 10.25 shows the enormous diff erence between the water level at high and low tides, a dif- ference that in some locations averages about 15 m. This phenomenon is partly due to resonance.
The time, or period, that it takes for the tide to fl ow into and ebb out of a bay depends on the size of
the bay, the topology of the bottom, and the confi guration of the shoreline. The ebb and fl ow of the
water in the Bay of Fundy has a period of 12.5 hours, which is very close to the lunar tidal period
of 12.42 hours. The tide then “drives” water into and out of the Bay of Fundy at a frequency (once
per 12.42 hours) that nearly matches the natural frequency of the bay (once per 12.5 hours). The
result is the extraordinary high tide in the bay. (You can create a similar eff ect in a bathtub full of
water by moving back and forth in synchronism with the waves you’re causing.)
Velocity
Driving force
FIGURE 10.24 Resonance occurs when the frequency of the driving force (blue arrows)
matches a frequency at which the object
naturally vibrates. The red arrows represent
the velocity of the object.
10.7 Elastic Deformation 275
Check Your Understanding
(The answer is given at the end of the book.) 16. A car travels at a constant speed over a road that contains a series of equally spaced bumps. The spacing
between bumps is d. The mass of the car is m, and the spring constant of the car’s suspension springs is k. Because of resonance, a particularly jarring ride results. Ignoring the eff ect of the car’s shock absorbers, derive an expression for the car’s speed 𝜐 in terms of d, m, and k, as well as some numerical constants.
10.7 Elastic Deformation
Stretching, Compression, and Young’s Modulus We have seen that a spring returns to its original shape when the force compressing or stretch-
ing it is removed. In fact, all materials become distorted in some way when they are squeezed or
stretched, and many of them, such as rubber, return to their original shape when the squeezing or
stretching is removed. Such materials are said to be “elastic.” From an atomic viewpoint, elastic
behavior has its origin in the forces that atoms exert on each other, and Figure 10.26 symbolizes these forces as springs. It is because of these atomic-level “springs” that a material tends to return
to its initial shape once the forces that cause the deformation are removed.
The interatomic forces that hold the atoms of a solid together are particularly strong, so
considerable force must be applied to stretch or compress a solid object. Experiments have shown
that the magnitude of the force can be expressed by the following relation, provided that the
amount of stretch or compression is small compared to the original length of the object:
F = Y(∆LL0 ) A (10.17) As Figure 10.27 shows, F denotes the magnitude of the stretching force applied perpendicularly to the surface at the end, A is the cross-sectional area of the rod, ΔL is the increase in length, and L0 is the original length. An analogous picture applies in the case of a force that causes com- pression. The term Y is a proportionality constant called Young’s modulus, after Thomas Young (1773–1829). Solving Equation 10.17 for Y shows that Young’s modulus has units of force per unit area (N/m2).
Problem-Solving Insight It should be noted that the magnitude of the force in Equation 10.17 is proportional to the fractional increase (or decrease) in length ΔL/L0, rather than the absolute change in length ΔL.
A n d re
w J
. M
ar ti
n ez
/S ci
en ce
S o u rc
e
A n d re
w J
. M
ar ti
n ez
/S ci
en ce
S o u rc
e
FIGURE 10.25 The Bay of Fundy, Canada, at (left) high tide and (right) low tide. In some places the water level changes by almost 15 m.
FIGURE 10.26 The forces between atoms act like springs. The atoms are represented
by red spheres, and the springs between some
atoms have been omitted for clarity.
F
L0 L
A
Δ
FIGURE 10.27 In this diagram, F→ denotes the stretching force, A the cross-sectional area, L0 the original length of the rod, and ΔL the amount of stretch.
276 CHAPTER 10 Simple Harmonic Motion and Elasticity
The magnitude of the force is also proportional to the cross-sectional area A, which need not be circular, but can have any shape (e.g., rectangular).
BIO THE PHYSICS OF . . . surgical implants. Table 10.1 reveals that the value of Young’s modulus depends on the nature of the material. The values for metals are much larger
than those for bone, for example. Equation 10.17 indicates that, for a given force, the material
with the greater value of Y undergoes the smaller change in length. This diff erence between the changes in length is the reason why surgical implants (e.g., artifi cial hip joints), which are often
made from stainless steel or titanium alloys, can lead to chronic deterioration of the bone that is
in contact with the implanted prosthesis.
BIO THE PHYSICS OF . . . bone structure. Forces that are applied as in Figure 10.27 and cause stretching are called “tensile” forces, because they create a tension in the material, much
like the tension in a rope. Equation 10.17 also applies when the force compresses the material
along its length. In this situation, the force is applied in a direction opposite to that shown
in Figure 10.27, and ΔL stands for the amount by which the original length L0 decreases. Table 10.1 indicates, for example, that bone has diff erent values of Young’s modulus for compression and tension, the value for tension being greater. Such diff erences are related
to the structure of the material. The solid part of bone consists of collagen fi bers (a protein
material) distributed throughout hydroxyapatite (a mineral). The collagen acts like the steel
rods in reinforced concrete and increases the value of Y for tension relative to the value of Y for compression.
Most solids have Young’s moduli that are rather large, refl ecting the fact that a large
force is needed to change the length of a solid object by even a small amount, as Example 12
illustrates.
TABLE 10.1 Values for the Young’s Modulus of Solid Materials
Material Young’s Modulus Y
(N/m2) Aluminum 6.9 × 1010
Bone
Compression 9.4 × 109
Tension 1.6 × 1010
Brass 9.0 × 1010
Brick 1.4 × 1010
Copper 1.1 × 1011
Mohair 2.9 × 109
Nylon 3.7 × 109
Pyrex glass 6.2 × 1010
Steel 2.0 × 1011
Teflon 3.7 × 108
Titanium 1.2 × 1011
Tungsten 3.6 × 1011
EXAMPLE 12 BIO The Physics of Bone Compression
A circus performer supports the combined weight (1080 N) of a number
of colleagues (see Figure 10.28). Each thighbone (femur) of this per- former has a length of 0.55 m and an eff ective cross-sectional area of
7.7 × 10−4 m2. Determine the amount by which each thighbone compresses
under the extra weight.
Reasoning The additional weight supported by each thighbone is F = 12(1080 N) = 540 N, and Table 10.1 indicates that Young’s modulus for bone compression is 9.4 × 109 N/m2. Since the length and cross-
sectional area of the thighbone are also known, we can use Equation
10.17 to fi nd the amount by which the additional weight compresses the
thighbone.
Solution The amount of compression ΔL of each thighbone is
∆L = FL0 YA
= (540 N)(0.55 m)
(9.4 × 10 9 N/m2)(7.7 ×10−4 m2)
= 4.1 × 10−5 m
This is a very small change, the fractional decrease being ΔL/L0 = 0.000 075.
FIGURE 10.28 The entire weight of the balanced group is supported by the legs of the performer who is lying on his back.
U w
e L
ei n /©
A P
/W id
e W
o rl
d P
h o to
s
10.7 Elastic Deformation 277
Shear Deformation and the Shear Modulus It is possible to deform a solid object in a way other than by stretching or compressing it. For
instance, place a book on a rough table and push on the top cover, as in Figure 10.29a. Notice that the top cover, and the pages below it, become shifted relative to the stationary bottom
cover. The resulting deformation is called a shear deformation and occurs because of the combined eff ect of the force F→ applied (by the hand) to the top of the book and the force −F→ applied (by the table) to the bottom of the book. In general, shearing forces cause a solid object
to change its shape. In Figure 10.29 the directions of the forces are parallel to the covers of the book, each of which has an area A, as illustrated in part b of the drawing. These two forces have equal magnitudes, but opposite directions, so the book remains in equilibrium. Equation
10.18 gives the magnitude F of the force needed to produce an amount of shear ΔX for an object with thickness L0:
F = S (∆XL 0 )A (10.18) This equation is very similar to Equation 10.17. The constant of proportionality S is called the shear modulus and, like Young’s modulus, has units of force per unit area (N/m2). The value of S depends on the nature of the material, and Table 10.2 gives some representative values. Example 13 illustrates how to determine the shear modulus of a familiar dessert.
F
(a) (b)
Area = A
F
–F
–F
L0
FIGURE 10.29 (a) An example of a shear deformation. The shearing forces F→ and −F→ are applied parallel to the top and bottom
covers of the book. (b) The shear deformation is ΔX. The area of each cover is A, and the thickness of the book is L0.
TABLE 10.2 Values for the Shear Modulus of Solid Materials
Material Shear Modulus S
(N/m2) Aluminum 2.4 × 1010
Bone 1.2 × 1010
Brass 3.5 × 1010
Copper 4.2 × 1010
Lead 5.4 × 109
Nickel 7.3 × 1010
Steel 8.1 × 1010
Tungsten 1.5 × 1011
EXAMPLE 13 J-E-L-L-O
A block of Jell-O is resting on a plate. Figure 10.30a gives the dimen- sions of the block. You are bored, impatiently waiting for dinner, and push
tangentially across the top surface with a force of F = 0.45 N, as in part b of the drawing. The top surface moves a distance ΔX = 6.0 × 10−3 m relative to the bottom surface. Use this idle gesture to measure the shear
modulus of Jell-O.
Reasoning The fi nger applies a force that is parallel to the top surface of the Jell-O block. The shape of the block changes, because the top sur-
face moves a distance ΔX relative to the bottom surface. The magnitude of the force required to produce this change in shape is given by Equation
10.18 as F = S(ΔX/L0)A. We know the values for all the variables in this relation except S, which, therefore, can be determined.
Solution Solving Equation 10.18 for the shear modulus S, we fi nd that S = FL0/(A ΔX), where A = (0.070 m)(0.070 m) is the area of the top surface, and L0 = 0.030 m is the thickness of the block:
S = FL0
A ∆X =
(0.45 N)(0.030 m)
(0.070 m)(0.070 m)(6.0 ×10−3 m) = 460 N/m2
Jell-O can be deformed easily, so its shear modulus is signifi cantly less
than that of a more rigid material like steel (see Table 10.2).
0.070 m
(a)
(b)
0.070 m
X
0.030 m
Δ
FIGURE 10.30 (a) A block of Jell-O and (b) a shearing force applied to it.
278 CHAPTER 10 Simple Harmonic Motion and Elasticity
Although Equations 10.17 and 10.18 are algebraically similar, they refer to diff erent kinds
of deformations. The tensile force in Figure 10.27 is perpendicular to the surface whose area is A, whereas the shearing force in Figure 10.29 is parallel to that surface. Furthermore, the ratio ΔL/L0 in Equation 10.17 is diff erent from the ratio ΔX/L0 in Equation 10.18. The distances ΔL and L0 are parallel, whereas ΔX and L0 are perpendicular. Young’s modulus refers to a change in length of one dimension of a solid object as a result of tensile or compressive forces. The shear modulus refers to a change in shape of a solid object as a result of shearing forces.
Volume Deformation and the Bulk Modulus When a compressive force is applied along one dimension of a solid, the length of that dimen-
sion decreases. It is also possible to apply compressive forces so that the size of every dimension
(length, width, and depth) decreases, leading to a decrease in volume, as Figure 10.31 illustrates. This kind of overall compression occurs, for example, when an object is submerged in a liquid,
and the liquid presses inward everywhere on the object. The forces acting in such situations are
applied perpendicular to every surface, and it is more convenient to speak of the perpendicular
force per unit area, rather than the amount of any one force in particular. The magnitude of the
perpendicular force per unit area is called the pressure P.
DEFINITION OF PRESSURE The pressure P is the magnitude F of the force acting perpendicular to a surface divided by the area A over which the force acts:
P = F A
(10.19)
Pressure is a scalar, not a vector, quantity.
SI Unit of Pressure: N/m2 = pascal (Pa)
Equation 10.19 indicates that the SI unit for pressure is the unit of force divided by the unit
of area, or newton/meter2 (N/m2). This unit of pressure is often referred to as a pascal (Pa), named after the French scientist Blaise Pascal (1623–1662).
Suppose we change the pressure on an object by an amount ΔP, where ΔP represents the fi nal pressure P minus the initial pressure P0: ΔP = P − P0. Because of this change in pressure, the volume of the object changes by an amount ΔV = V − V0, where V and V0 are the fi nal and initial volumes, respectively. Such a pressure change occurs, for example, when a swimmer dives
deeper into the water. Experiment reveals that the change ΔP in pressure needed to change the volume by an amount ΔV is directly proportional to the fractional change ΔV/V0 in the volume:
∆P = −B(∆VV0 ) (10.20) This relation is analogous to Equations 10.17 and 10.18, except that the area A in those equations does not appear here explicitly; the area is already taken into account by the concept of pressure
(magnitude of the force per unit area). The proportionality constant B is known as the bulk modulus. The minus sign occurs because an increase in pressure (ΔP positive) always creates a decrease in volume (ΔV negative), and B is given as a positive quantity. Like Young’s modulus and the shear modulus, the bulk modulus has units of force per unit area (N/m2), and its value depends on the
nature of the material. Table 10.3 gives representative values of the bulk modulus.
Check Your Understanding
(The answers are given at the end of the book.) 17. Young’s modulus for steel is greater than that for a particular unknown material. What does this mean
about how these materials compress when used in construction? (a) Steel compresses much more easily than the unknown material does. (b) The unknown material compresses more easily than steel does. (c) Young’s modulus has nothing to do with compression, so not enough information is given for an answer.
Initial volume
Final volume
FIGURE 10.31 The arrows denote the forces that push perpendicularly on every
surface of an object immersed in a liquid.
The magnitude of the force per unit area is
the pressure. When the pressure increases,
the volume of the object decreases.
TABLE 10.3 Values for the Bulk Modulus of Solid and Liquid Materials
Material Bulk Modulus B
[N/m2 (=Pa)] Solids Aluminum 7.1 × 1010
Brass 6.7 × 1010
Copper 1.3 × 1011
Diamond 4.43 × 1011
Lead 4.2 × 1010
Nylon 6.1 × 109
Osmium 4.62 × 1011
Pyrex glass 2.6 × 1010
Steel 1.4 × 1011
Liquids Ethanol 8.9 × 108
Oil 1.7 × 109
Water 2.2 × 109
10.8 Stress, Strain, and Hooke’s Law 279
18. Two rods are made from the same material. One has a circular cross section, and the other has a square cross section. The circle just fi ts within the square. When the same force is applied to stretch these rods,
they each stretch by the same amount. Which rod, if either, is longer?
19. A trash compactor crushes empty aluminum cans, thereby reducing the total volume, so that ΔV/V0 = −0.75 in Equation 10.20. Can the value given in Table 10.3 for the bulk modulus of aluminum be used to calculate the change ΔP in pressure generated in the trash compactor?
20. Both sides of the relation F = S(ΔX/L0)A (Equation 10.18) can be divided by the area A to give F/A on the left side. Can this F/A term be called a pressure, such as the pressure that appears in ΔP = −B(ΔV/V0) (Equation 10.20)?
10.8 Stress, Strain, and Hooke’s Law Equations 10.17, 10.18, and 10.20 specify the amount of force needed for a given amount of
elastic deformation, and they are repeated in Table 10.4 to emphasize their common features. The left side of each equation is the magnitude of the force per unit area required to cause an
elastic deformation. In general, the ratio of the magnitude of the force to the area is called the
stress. The right side of each equation involves the change in a quantity (ΔL, ΔX, or ΔV) divided by a quantity (L0 or V0) relative to which the change is compared. The terms ΔL/L0, ΔX/L0, and ΔV/V0 are unitless ratios, and each is referred to as the strain that results from the applied stress. In the case of stretch and compression, the strain is the fractional change in length, whereas in
volume deformation it is the fractional change in volume. In shear deformation the strain refers
to a change in shape of the object. Experiments show that these three equations, with constant
values for Young’s modulus, the shear modulus, and the bulk modulus, apply to a wide range of
materials. Therefore, stress and strain are directly proportional to one another, a relationship fi rst
discovered by Robert Hooke (1635–1703) and now referred to as Hooke’s law.
HOOKE’S LAW FOR STRESS AND STRAIN Stress is directly proportional to strain.
SI Unit of Stress: newton per square meter (N/m2) = pascal (Pa)
SI Unit of Strain: Strain is a unitless quantity.
In reality, materials obey Hooke’s law only up to a certain limit, as Figure 10.32 shows. As long as stress remains proportional to strain, a plot of stress versus strain is a straight line. The
point on the graph where the material begins to deviate from straight-line behavior is called the
“proportionality limit.” Beyond the proportionality limit stress and strain are no longer directly
proportional. However, if the stress does not exceed the “elastic limit” of the material, the object
will return to its original size and shape once the stress is removed. The “elastic limit” is the
point beyond which the object no longer returns to its original size and shape when the stress is
removed; the object remains permanently deformed.
Check Your Understanding
(The answer is given at the end of the book.) 21. The block in CYU Figure 10.3 rests on the ground. Which face—A,
B, or C—experiences the largest stress and which face experiences the
smallest stress when the block is resting on it?
Stress
Proportionality limit
Elastic limit
Strain
Stress is directly proportional to strain
FIGURE 10.32 Hooke’s law (stress is directly proportional to strain) is valid only
up to the proportionality limit of a material.
Beyond this limit, Hooke’s law no longer
applies. Beyond the elastic limit, the material
remains deformed even when the stress is
removed.
TABLE 10.4 Stress and Strain Relations for Elastic Behavior
F A
= Y (∆LL0 ) (10.17) F A
= S (∆XL0 ) (10.18) ∆P = B (−∆VV0 ) (10.20)
Stress
is
proportional
to Strain
CYU FIGURE 10.3
20.0 cm
10.0 cm
30.0 cmB
C
A
280 CHAPTER 10 Simple Harmonic Motion and Elasticity
EXAMPLE 14 BIO The Physics of the Mechanical Properties of Bone
Human bones also follow Hooke’s Law for Stress and Strain, as indicated
in Figure 10.33. This is essentially Figure 10.32, where we plot the stress versus strain specifi cally for a human femur—the largest bone in the body.
In Section 6.9, we plotted the average force versus displacement for a
variable force. The area under the curve was equal to the work done by the force. Now let’s apply a similar analysis to Figure 10.33. Calculate the area under the curve where Hooke’s law is valid (shaded region), and use
unit analysis to describe what this area represents.
Reasoning As we did in Section 6.9, we need to calculate the area of the shaded region. Since we are to consider only the range where Hooke’s law
is valid, the shaded region will have the shape of a triangle whose area is
equal to 1
2(base × height).
Solution Using the data in Figure 10.33 we calculate the area of the shaded region:
Area = 1
2(base × height) = 1
2(0.010)(200 × 10 6 Pa) = 1.00 × 106 Pa .
Since stress has the units of pressure, and strain is unitless, our answer also
has units of pressure, or Pa. However, we can gain a greater understand-
ing of the signifi cance of the area under the curve if we write pressure
as the stress P = F A
and the strain as ∆L L0
. Now when we calculate the area
under the curve in general, we have:
Area = 1
2 (FA)( ∆L L0 ).
Here, the force is given by Hooke’s law:
F = kx = k∆L.
If we substitute this into our equation for the area above, we get the following:
Area =
1
2 k(∆L)2
AL0 .
The numerator is equivalent to Equation 10.13 and represents the elas-
tic potential energy. The denominator is equal to an area times a length,
which has the units of volume. Therefore, in general, the area under the
curve is equivalent to energy per unit volume, or energy density:
Area = PE [J]
Vol [m3] .
For our simple example above, the result indicates that one million J/m3
of elastic potential energy is stored in the bone under compression. Of
course, the stored energy in a human femur is much smaller than one mil-
lion joules, as the change in volume under compression is much smaller
than 1 m3. However, if the energy delivered to the bone is greater than the
energy it can absorb, the bone will fail, and a fracture will occur.
Stress (MPa)
0
100
200
300
0 0.005 0.010 0.015 Strain
Proportionality limit
Elastic limit
FIGURE 10.33 Stress versus strain for a human
femur bone. Hooke’s
Law is obeyed up to the
proportionality limit.
Concept Summary 10.1 The Ideal Spring and Simple Harmonic Motion The force that must be applied to stretch or compress an ideal spring is given by Equation
10.1, where k is the spring constant and x is the displacement of the spring from its unstrained length.
Fx Applied = kx (10.1)
A spring exerts a restoring force on an object attached to the spring. The
restoring force Fx produced by an ideal spring is given by Equation 10.2, where the minus sign indicates that the restoring force points opposite to the
displacement of the spring.
Fx = −kx (10.2)
Simple harmonic motion is the oscillatory motion that occurs when a
restoring force of the form Fx = −kx acts on an object. A graphical record of position versus time for an object in simple harmonic motion is sinusoidal. The
amplitude A of the motion is the maximum distance that the object moves away from its equilibrium position.
10.2 Simple Harmonic Motion and the Reference Circle The period T of simple harmonic motion is the time required to complete one cycle of the motion, and the frequency f is the number of cycles per second that occurs. Frequency and period are related, according to Equation 10.5. The
frequency f (in Hz) is related to the angular frequency 𝜔 (in rad/s), according to Equation 10.6.
f = 1
T (10.5)
ω = 2π f (ω in rad/s) (10.6)
The maximum speed 𝜐max of an object moving in simple harmonic motion
is given by Equation 10.8, where A is the amplitude of the motion.
υmax = Aω (ω in rad/s) (10.8)
The maximum acceleration amax of an object moving in simple harmonic motion is given by Equation 10.10.
amax = Aω 2 (ω in rad/s) (10.10)
The angular frequency of simple harmonic motion is given by Equation 10.11.
ω = √ km (ω in rad/s) (10.11) 10.3 Energy and Simple Harmonic Motion The elastic potential energy of an object attached to an ideal spring is given by Equation 10.13. The total
mechanical energy E of such a system is the sum of its translational and
Focus on Concepts 281
rotational kinetic energies, gravitational potential energy, and elastic poten-
tial energy, according to Equation 10.14. If external nonconservative forces
like friction do no net work, the total mechanical energy of the system is
conserved, as indicated by Equation 1.
PEelastic = 1
2 kx2 (10.13)
E = 12 mυ2 + 1
2 Iω 2 + mgh + 1
2 kx2 (10.14)
E f = E0 (1)
10.4 The Pendulum A simple pendulum is a particle of mass m attached to a frictionless pivot by a cable whose length is L and whose mass is negli- gible. The small-angle (≤10°) back-and-forth swinging of a simple pendulum
is simple harmonic motion, but large-angle movement is not. The frequency
f of the small-angle motion is given by Equation 10.16.
2πf = √gL (small angles only) (10.16) A physical pendulum consists of a rigid object, with moment of inertia I
and mass m, suspended from a frictionless pivot. For small-angle displace- ments, the frequency f of simple harmonic motion for a physical pendulum is given by Equation 10.15, where L is the distance between the axis of rotation and the center of gravity of the rigid object.
2πf = √mgLI (small angles only) (10.15) 10.5 Damped Harmonic Motion Damped harmonic motion is motion in which the amplitude of oscillation decreases as time passes. Critical damping
is the minimum degree of damping that eliminates any oscillations in the
motion as the object returns to its equilibrium position.
10.6 Driven Harmonic Motion and Resonance Driven harmonic mo- tion occurs when a driving force acts on an object along with the restor-
ing force. Resonance is the condition under which the driving force can
transmit large amounts of energy to an oscillating object, leading to large-
amplitude motion. In the absence of damping, resonance occurs when the
frequency of the driving force matches a natural frequency at which the
object oscillates.
10.7 Elastic Deformation One type of elastic deformation is stretch and com- pression. The magnitude F of the force required to stretch or compress an object of length L0 and cross-sectional area A by an amount ΔL (see Figure 10.27) is given by Equation 10.17, where Y is a constant called Young’s modulus.
F = Y (∆LL0 ) A (10.17) Another type of elastic deformation is shear. The magnitude F of the
shearing force required to create an amount of shear ΔX for an object of thickness L0 and cross-sectional area A is (see Figure 10.29) given by Equa- tion 10.18, where S is a constant called the shear modulus.
F = S (∆XL0 ) A (10.18) A third type of elastic deformation is volume deformation, which has to
do with pressure. The pressure P is the magnitude F of the force acting per- pendicular to a surface divided by the area A over which the force acts, ac- cording to Equation 10.19. The SI unit for pressure is N/m2, a unit known as
a pascal (Pa): 1 Pa = 1 N/m2. The change ΔP in pressure needed to change the volume V0 of an object by an amount ΔV (see Figure 10.31) is given by Equation 10.20, where B is a constant known as the bulk modulus.
P = F A
(10.19)
∆P = −B (∆VV0 ) (10.20) 10.8 Stress, Strain, and Hooke’s Law Stress is the magnitude of the force per unit area applied to an object and causes strain. For stretch/compression,
the strain is the fractional change ΔL/L0 in length. For shear, the strain refl ects the change in shape of the object and is given by ΔX/L0 (see Figure 10.29). For volume deformation, the strain is the fractional change in volume ΔV/V0. Hooke’s law states that stress is directly proportional to strain.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 10.1 The Ideal Spring and Simple Harmonic Motion 2. Which one of the following graphs correctly represents the restoring force F of an ideal spring as a function of the displacement x of the spring from its unstrained length?
+F
+x
(a)
+F
+x
(c)
+F
+x
(b)
+F
+x
(d )
+F
+x
(e)
QUESTION 2
Section 10.2 Simple Harmonic Motion and the Reference Circle 3. You have two springs. One has a greater spring constant than the other. You also have two objects, one with a greater mass than the other. Which
object should be attached to which spring, so that the resulting spring–object
system has the greatest possible period of oscillation? (a) The object with the greater mass should be attached to the spring with the greater spring con-
stant. (b) The object with the greater mass should be attached to the spring with the smaller spring constant. (c) The object with the smaller mass should be attached to the spring with the smaller spring constant. (d) The object with the smaller mass should be attached to the spring with the greater spring
constant.
4. An object is oscillating in simple harmonic motion with an amplitude A and an angular frequency 𝜔. What should you do to increase the maximum
speed of the motion? (a) Reduce both A and 𝜔 by 10%. (b) Increase A by 10% and reduce 𝜔 by 10%. (c) Reduce A by 10% and increase 𝜔 by 10%. (d) Increase both A and 𝜔 by 10%.
Focus on Concepts
282 CHAPTER 10 Simple Harmonic Motion and Elasticity
Section 10.3 Energy and Simple Harmonic Motion 11. The kinetic energy of an object attached to a horizontal ideal spring is denoted by KE and the elastic potential energy by PE. For the simple har-
monic motion of this object the maximum kinetic energy and the maximum
elastic potential energy during an oscillation cycle are KEmax and PEmax,
respectively. In the absence of friction, air resistance, and any other non-
conservative forces, which of the following equations applies to the object–
spring system?
A. KE + PE = constant
B. KEmax = PEmax
(a) A, but not B (b) B, but not A (c) A and B (d) Neither A nor B
13. A block is attached to a horizontal spring. On top of this block rests another block. The two-block system slides back and forth in simple har-
monic motion on a frictionless horizontal surface. At one extreme end of
the oscillation cycle, where the blocks come to a momentary halt before
reversing the direction of their motion, the top block is suddenly lifted ver-
tically upward, without changing the zero velocity of the bottom block. The
simple harmonic motion then continues. What happens to the amplitude
and the angular frequency of the ensuing motion? (a) The amplitude re- mains the same, and the angular frequency increases. (b) The amplitude increases, and the angular frequency remains the same. (c) Both the amp- litude and the angular frequency remain the same. (d) Both the amplitude and the angular frequency decrease. (e) Both the amplitude and the angular frequency increase.
Section 10.4 The Pendulum 14. Five simple pendulums are shown in the drawings. The lengths of the pendulums are drawn to scale, and the masses are either m or 2m, as shown. Which pendulum has the smallest angular frequency of oscillation?
(a) A (b) B (c) C (d) D (e) E
QUESTION 14
D
m
BA
2m
C
2m
E
2m m
Section 10.5 Damped Harmonic Motion 16. An object on a spring is oscillating in simple harmonic motion. Sud- denly, friction appears and causes the energy of the system to be dissipated.
The system now exhibits ______. (a) driven harmonic motion (b) Hooke’s- law type of motion (c) damped harmonic motion
Section 10.6 Driven Harmonic Motion and Resonance 17. An external force (in addition to the spring force) is continually applied to an object of mass m attached to a spring that has a spring constant k. The frequency of this external force is such that resonance occurs. Then the fre-
quency of this external force is doubled, and the force is applied to one of the
spring systems shown in the drawing. With which system would resonance
occur? (a) A (b) B (c) C (d) D (e) E
QUESTION 17
DBA
2m
8k
4m
2k
6m
4k
3m
9k
5m
10k
C E
Section 10.7 Elastic Deformation 18. Drawings A and B show two cylinders that are identical in all respects, except that one is hollow. Identical forces are applied to each cylinder in
order to stretch them. Which cylinder, if either, stretches more? (a) A and B both stretch by the same amount. (b) A stretches more than B. (c) B stretches more than A. (d) Insuffi cient information is given for an answer.
QUESTION 18 A B
Section 10.8 Stress, Strain, and Hooke’s Law 20. A material has a shear modulus of 5.0 × 109 N/m2. A shear stress of 8.5 × 106 N/m2 is applied to a piece of the material. What is the resulting
shear strain?
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 10.1 The Ideal Spring and Simple Harmonic Motion 1. E SSM A hand exerciser utilizes a coiled spring. A force of 89.0 N is required to compress the spring by 0.0191 m. Determine the force needed to
compress the spring by 0.0508 m.
2. E The drawing shows three identical springs hanging from the ceiling. Nothing is attached to the fi rst spring, whereas a 4.50-N block hangs from the
second spring. A block of unknown weight hangs from the third spring. From
Problems
Problems 283
the drawing, determine (a) the spring constant (in N/m) and (b) the weight of the block hanging from the third spring.
PROBLEM 2
4.50 N
0 cm
10.0
20.0
30.0
40.0
50.0
60.0
3. E In a room that is 2.44 m high, a spring (unstrained length = 0.30 m) hangs from the ceiling. A board whose length is 1.98 m is attached to the free
end of the spring. The board hangs straight down, so that its 1.98-m length
is perpendicular to the fl oor. The weight of the board (104 N) stretches the
spring so that the lower end of the board just extends to, but does not touch,
the fl oor. What is the spring constant of the spring?
4. E GO A spring lies on a horizontal table, and the left end of the spring is attached to a wall. The other end is connected to a box. The box is pulled
to the right, stretching the spring. Static friction exists between the box and
the table, so when the spring is stretched only by a small amount and the
box is released, the box does not move. The mass of the box is 0.80 kg, and
the spring has a spring constant of 59 N/m. The coeffi cient of static friction
between the box and the table on which it rests is μs = 0.74. How far can the spring be stretched from its unstrained position without the box moving when
it is released?
5. E SSM A person who weighs 670 N steps onto a spring scale in the bath- room, and the spring compresses by 0.79 cm. (a) What is the spring con- stant? (b) What is the weight of another person who compresses the spring by 0.34 cm?
6. E A spring (k = 830 N/m) is hanging from the ceiling of an elevator, and a 5.0-kg object is attached to the lower end. By how much does the spring
stretch (relative to its unstrained length) when the elevator is accelerating
upward at a = 0.60 m/s2?
7. E CHALK A 0.70-kg block is hung from and stretches a spring that is at- tached to the ceiling. A second block is attached to the fi rst one, and the
amount that the spring stretches from its unstrained length triples. What is
the mass of the second block?
8. M V-HINT A uniform 1.4-kg rod that is 0.75 m long is suspended at rest from the ceiling by two springs, one at each end of the rod. Both springs
hang straight down from the ceiling. The springs have identical lengths when
they are unstretched. Their spring constants are 59 N/m and 33 N/m. Find the
angle that the rod makes with the horizontal.
9. M SSM In 0.750 s, a 7.00-kg block is pulled through a distance of 4.00 m on a frictionless horizontal surface, starting from rest. The block has a con-
stant acceleration and is pulled by means of a horizontal spring that is at-
tached to the block. The spring constant of the spring is 415 N/m. By how
much does the spring stretch?
10. M GO Review Conceptual Example 2 as an aid in solving this problem. An object is attached
to the lower end of a 100-coil spring that is hanging
from the ceiling. The spring stretches by 0.160 m.
The spring is then cut into two identical springs of
50 coils each. As the drawing shows, each spring
is attached between the ceiling and the object. By
how much does each spring stretch?
11. M CHALK SSM A small ball is attached to one end of a spring that has an unstrained length of 0.200 m. The spring is held by the other end, and
the ball is whirled around in a horizontal circle at a speed of 3.00 m/s.
The spring remains nearly parallel to the ground during the motion and is
observed to stretch by 0.010 m. By how much would the spring stretch if
it were attached to the ceiling and the ball allowed to hang straight down,
motionless?
12. M MMH To measure the static friction coeffi cient between a 1.6-kg block and a vertical wall, the setup shown in the drawing is used. A spring
(spring constant = 510 N/m) is attached to the block. Someone pushes on
the end of the spring in a direction perpendicular to the wall until the block
does not slip downward. The spring is compressed by 0.039 m. What is the
coeffi cient of static friction?
PROBLEM 12
13. H A 30.0-kg block is resting on a fl at horizontal table. On top of this block is resting a 15.0-kg block, to which a horizontal spring is attached, as
the drawing illustrates. The spring constant of the spring is 325 N/m. The
coeffi cient of kinetic friction between the lower block and the table is 0.600,
and the coeffi cient of static friction between the two blocks is 0.900. A hori-
zontal force F→ is applied to the lower block as shown. This force is increasing in such a way as to keep the blocks moving at a constant speed. At the point where the upper block begins to slip on the lower block, determine (a) the amount by which the spring is compressed and (b) the magnitude of the force F→ .
PROBLEM 13
15.0 kg
30.0 kg F
14. H A 15.0-kg block rests on a horizontal table and is attached to one end of a massless, horizontal spring. By pulling horizontally on the other end
of the spring, someone causes the block to accelerate uniformly and reach
a speed of 5.00 m/s in 0.500 s. In the process, the spring is stretched by
0.200 m. The block is then pulled at a constant speed of 5.00 m/s, during which time the spring is stretched by only 0.0500 m. Find (a) the spring constant of the spring and (b) the coeffi cient of kinetic friction between the block and the table.
Section 10.2 Simple Harmonic Motion and the Reference Circle 15. E BIO SSM When responding to sound, the human eardrum vibrates about its equilibrium position. Suppose an eardrum is vibrating with an am- plitude of 6.3 × 10−7 m and a maximum speed of 2.9 × 10−3 m/s. (a) What is the frequency (in Hz) of the eardrum’s vibration? (b) What is the maximum acceleration of the eardrum? 16. E The fan blades on a jet engine make one thousand revolutions in a time of 50.0 ms. Determine (a) the period (in seconds) and (b) the frequency (in Hz) of the rotational motion. (c) What is the angular frequency of the blades?
50-coil spring
PROBLEM 10
284 CHAPTER 10 Simple Harmonic Motion and Elasticity
17. E MMH A block of mass m = 0.750 kg is fastened to an unstrained ho- rizontal spring whose spring constant is k = 82.0 N/m. The block is given a displacement of +0.120 m, where the + sign indicates that the displacement
is along the +x axis, and then released from rest. (a) What is the force (mag- nitude and direction) that the spring exerts on the block just before the block
is released? (b) Find the angular frequency 𝜔 of the resulting oscillatory motion. (c) What is the maximum speed of the block? (d) Determine the magnitude of the maximum acceleration of the block.
18. E MMH An 0.80-kg object is attached to one end of a spring, as in Fig- ure 10.5, and the system is set into simple harmonic motion. The displace- ment x of the object as a function of time is shown in the drawing. With the aid of these data, determine (a) the amplitude A of the motion, (b) the angular frequency 𝜔, (c) the spring constant k, (d) the speed of the object at t = 1.0 s, and (e) the magnitude of the object’s acceleration at t = 1.0 s.
PROBLEM 18
0.080
0 Time (s)
x (m)
–0.080
1.0 3.0
2.0 4.0
19. E Refer to Conceptual Example 2 as an aid in solving this problem. A 100-coil spring has a spring constant of 420 N/m. It is cut into four shorter
springs, each of which has 25 coils. One end of a 25-coil spring is attached to
a wall. An object of mass 46 kg is attached to the other end of the spring, and
the system is set into horizontal oscillation. What is the angular frequency
of the motion?
20. M GO Objects of equal mass are oscillating up and down in simple har- monic motion on two diff erent vertical springs. The spring constant of spring
1 is 174 N/m. The motion of the object on spring 1 has twice the amplitude
as the motion of the object on spring 2. The magnitude of the maximum
velocity is the same in each case. Find the spring constant of spring 2.
21. M SSM MMH A spring stretches by 0.018 m when a 2.8-kg object is sus- pended from its end. How much mass should be attached to this spring so that
its frequency of vibration is f = 3.0 Hz? 22. M V-HINT An object attached to a horizontal spring is oscillating back and forth along a frictionless surface. The maximum speed of the object is
1.25 m/s, and its maximum acceleration is 6.89 m/s2. How much time elapses
between an instant when the object’s speed is at a maximum and the next
instant when its acceleration is at a maximum?
23. M GO MMH A vertical spring (spring constant = 112 N/m) is mounted on the fl oor. A 0.400-kg block is placed on top of the spring and pushed down
to start it oscillating in simple harmonic motion. The block is not attached to
the spring. (a) Obtain the frequency (in Hz) of the motion. (b) Determine the amplitude at which the block will lose contact with the spring.
24. H A tray is moved horizontally back and forth in simple harmonic mo- tion at a frequency of f = 2.00 Hz. On this tray is an empty cup. Obtain the coeffi cient of static friction between the tray and the cup, given that the cup
begins slipping when the amplitude of the motion is 5.00 × 10−2 m.
Section 10.3 Energy and Simple Harmonic Motion 25. E A pen contains a spring with a spring constant of 250 N/m. When the tip of the pen is in its retracted position, the spring is compressed 5.0 mm
from its unstrained length. In order to push the tip out and lock it into its
writing position, the spring must be compressed an additional 6.0 mm. How
much work is done by the spring force to ready the pen for writing? Be sure
to include the proper algebraic sign with your answer.
26. E GO The drawing shows three situations in which a block is attached to a spring. The position labeled “0 m” represents the unstrained position of
the spring. The block is moved from an initial position x0 to a fi nal position xf,
the magnitude of the displacement being denoted by the symbol s. Suppose the spring has a spring constant of k = 46.0 N/m. Using the data provided in the drawing, determine the total work done by the restoring force of the
spring for each situation.
PROBLEM 26
s
0 m +3.00 m–3.00 m
s
0 m +1.00 m–3.00 m
s
0 m +3.00 m+1.00 m
Position of box when spring is unstrained(a)
(b)
(c)
27. E A spring is hung from the ceiling. A 0.450-kg block is then attached to the free end of the spring. When released from rest, the block drops 0.150 m
before momentarily coming to rest, after which it moves back upward.
(a) What is the spring constant of the spring? (b) Find the angular frequency of the block’s vibrations.
28. E A 3.2-kg block is hanging stationary from the end of a vertical spring that is attached to the ceiling. The elastic potential energy of this spring-
block system is 1.8 J. What is the elastic potential energy of the system when
the 3.2-kg block is replaced by a 5.0-kg block?
29. E SSM A vertical spring with a spring constant of 450 N/m is mounted on the fl oor. From directly above the spring, which is unstrained, a 0.30-kg
block is dropped from rest. It collides with and sticks to the spring, which is
compressed by 2.5 cm in bringing the block to a momentary halt. Assuming
air resistance is negligible, from what height (in cm) above the compressed
spring was the block dropped?
30. E In preparation for shooting a ball in a pinball machine, a spring (k = 675 N/m) is compressed by 0.0650 m relative to its unstrained length. The
ball (m = 0.0585 kg) is at rest against the spring at point A. When the spring is released, the ball slides (without rolling). It leaves the spring and arrives at
point B, which is 0.300 m higher than point A. Ignore friction, and fi nd the
ball’s speed at point B.
31. E MMH A heavy-duty stapling gun uses a 0.140-kg metal rod that rams against the staple to eject it. The rod is attached to and pushed by a stiff
spring called a “ram spring” (k = 32 000 N/m). The mass of this spring may be ignored. The ram spring is compressed by 3.0 × 10−2 m from its
unstrained length and then released from rest. Assuming that the ram spring
is oriented vertically and is still compressed by 0.8 × 10−2 m when the down-
ward-moving ram hits the staple, fi nd the speed of the ram at the instant of
contact.
32. E A rifl e fi res a 2.10 × 10−2-kg pellet straight upward, because the pel- let rests on a compressed spring that is released when the trigger is pulled.
The spring has a negligible mass and is compressed by 9.10 × 10−2 m from
its unstrained length. The pellet rises to a maximum height of 6.10 m above
its position on the compressed spring. Ignoring air resistance, determine the
spring constant.
33. E SSM A 1.00 × 10−2-kg block is resting on a horizontal frictionless surface and is attached to a horizontal spring whose spring constant is 124 N/m.
The block is shoved parallel to the spring axis and is given an initial speed of
8.00 m/s, while the spring is initially unstrained. What is the amplitude of the
resulting simple harmonic motion?
34. M V-HINT An 86.0-kg climber is scaling the vertical wall of a mountain. His safety rope is made of nylon that, when stretched, behaves like a spring
Problems 285
with a spring constant of 1.20 × 103 N/m. He accidentally slips and falls
freely for 0.750 m before the rope runs out of slack. How much is the rope
stretched when it breaks his fall and momentarily brings him to rest?
35. M V-HINT A horizontal spring is lying on a frictionless surface. One end of the spring is attached to a wall, and the other end is connected to a mov-
able object. The spring and object are compressed by 0.065 m, released from
rest, and subsequently oscillate back and forth with an angular frequency of
11.3 rad/s. What is the speed of the object at the instant when the spring is
stretched by 0.048 m relative to its unstrained length? 36. M GO A spring is resting vertically on a table. A small box is dropped onto the top of the spring and compresses it. Suppose the spring has a spring
constant of 450 N/m and the box has a mass of 1.5 kg. The speed of the box
just before it makes contact with the spring is 0.49 m/s. (a) Determine the magnitude of the spring’s displacement at an instant when the acceleration of
the box is zero. (b) What is the magnitude of the spring’s displacement when the spring is fully compressed?
37. M CHALK SSM MMH A spring is compressed by 0.0620 m and is used to launch an object horizontally with a speed of 1.50 m/s. If the object
were attached to the spring, at what angular frequency (in rad/s) would it
oscillate?
38. M GO A 0.60-kg metal sphere oscillates at the end of a vertical spring. As the spring stretches from 0.12 to 0.23 m (relative to its unstrained length),
the speed of the sphere decreases from 5.70 to 4.80 m/s. What is the spring
constant of the spring?
39. M Available in WileyPLUS. 40. M A 1.1-kg object is suspended from a vertical spring whose spring constant is 120 N/m. (a) Find the amount by which the spring is stretched from its unstrained length. (b) The object is pulled straight down by an addi- tional distance of 0.20 m and released from rest. Find the speed with which
the object passes through its original position on the way up.
41. H SSM A 70.0-kg circus performer is fi red from a cannon that is elevated at an angle of 40.0° above the horizontal. The cannon uses strong elastic
bands to propel the performer, much in the same way that a slingshot fi res
a stone. Setting up for this stunt involves stretching the bands by 3.00 m
from their unstrained length. At the point where the performer fl ies free of
the bands, his height above the fl oor is the same as the height of the net into
which he is shot. He takes 2.14 s to travel the horizontal distance of 26.8 m
between this point and the net. Ignore friction and air resistance and deter-
mine the eff ective spring constant of the fi ring mechanism.
42. H A 1.00 × 10−2-kg bullet is fi red horizontally into a 2.50-kg wooden block attached to one end of a massless horizontal spring (k = 845 N/m). The other end of the spring is fi xed in place, and the spring is unstrained initially.
The block rests on a horizontal, frictionless surface. The bullet strikes the
block perpendicularly and quickly comes to a halt within it. As a result of
this completely inelastic collision, the spring is compressed along its axis
and causes the block/bullet to oscillate with an amplitude of 0.200 m. What
is the speed of the bullet?
Section 10.4 The Pendulum 43. E A simple pendulum is made from a 0.65-m-long string and a small ball attached to its free end. The ball is pulled to one side through a small
angle and then released from rest. After the ball is released, how much time
elapses before it attains its greatest speed?
44. E GO MMH Astronauts on a distant planet set up a simple pendulum of length 1.2 m. The pendulum executes simple harmonic motion and makes
100 complete vibrations in 280 s. What is the magnitude of the acceleration
due to gravity on this planet?
45. E GO The length of a simple pendulum is 0.79 m and the mass of the particle (the “bob”) at the end of the cable is 0.24 kg. The pendulum is pulled
away from its equilibrium position by an angle of 8.50° and released from
rest. Assume that friction can be neglected and that the resulting oscillatory
motion is simple harmonic motion. (a) What is the angular frequency of the motion? (b) Using the position of the bob at its lowest point as the reference level, determine the total mechanical energy of the pendulum as it swings
back and forth. (c) What is the bob’s speed as it passes through the lowest point of the swing?
46. E A spiral staircase winds up to the top of a tower in an old castle. To measure the height of the tower, a rope is attached to the top of the tower and
hung down the center of the staircase. However, nothing is available with
which to measure the length of the rope. Therefore, at the bottom of the rope
a small object is attached so as to form a simple pendulum that just clears the
fl oor. The period of the pendulum is measured to be 9.2 s. What is the height
of the tower?
47. E GO Two physical pendulums (not simple pendulums) are made from meter sticks that are suspended from the ceiling at one end. The sticks are
uniform and are identical in all respects, except that one is made of wood
(mass = 0.17 kg) and the other of metal (mass = 0.85 kg). They are set into
oscillation and execute simple harmonic motion. Determine the period of
(a) the wood pendulum and (b) the metal pendulum. 48. M V-HINT Available in WileyPLUS. 49. M V-HINT Available in WileyPLUS. 50. H A small object oscillates back and forth at the bottom of a frictionless hemispherical bowl, as the drawing illustrates. The radius of the bowl is R, and the angle 𝜃 is small enough that the object oscillates in simple harmonic
motion. Derive an expression for the angular frequency 𝜔 of the motion.
Express your answer in terms of R and g, the magnitude of the acceleration due to gravity.
PROBLEM 50
Hemispherical bowl
R θ
Section 10.7 Elastic Deformation,
Section 10.8 Stress, Strain, and Hooke’s Law 51. E SSM A tow truck is pulling a car out of a ditch by means of a steel cable that is 9.1 m long and has a radius of 0.50 cm. When the car just
begins to move, the tension in the cable is 890 N. How much has the cable
stretched?
52. E Two stretched cables both experience the same stress. The fi rst cable has a radius of 3.5 × 10−3 m and is subject to a stretching force of 270 N. The
radius of the second cable is 5.1 × 10−3 m. Determine the stretching force
acting on the second cable.
53. E SSM The pressure increases by 1.0 × 104 N/m2 for every meter of depth beneath the surface of the ocean. At what depth does the volume of a
Pyrex glass cube, 1.0 × 10−2 m on an edge at the ocean’s surface, decrease
by 1.0 × 10−10 m3?
54. E BIO V-HINT When subjected to a force of compression, the length of a bone decreases by 2.7 × 10−5 m. When this same bone is subjected to a
tensile force of the same magnitude, by how much does it stretch? 55. E A 59-kg water skier is being pulled by a nylon tow rope that is at- tached to a boat. The unstretched length of the rope is 12 m, and its cross-
sectional area is 2.0 × 10−5 m2. As the skier moves, a resistive force (due to
the water) of magnitude 130 N acts on her; this force is directed opposite to
286 CHAPTER 10 Simple Harmonic Motion and Elasticity
her motion. What is the change in the length of the rope when the skier has
an acceleration whose magnitude is 0.85 m/s2?
56. E A solid steel cylinder is standing (on one of its ends) vertically on the fl oor. The length of the cylinder is 3.6 m and its radius is 65 cm. When an
object is placed on top of the cylinder, the cylinder compresses by an amount
of 5.7 × 10−7 m. What is the weight of the object?
57. E The drawing shows a 160-kg crate hanging from the end of a steel bar. The length of the bar is 0.10 m, and its cross-sectional area is 3.2 ×
10−4 m2. Neglect the weight of the bar itself and determine (a) the shear stress on the bar and (b) the vertical defl ection ΔY of the right end of the bar.
PROBLEM 57
58. E A copper cube, 0.30 m on a side, is subjected to two shearing forces, each of which has a magnitude F = 6.0 × 106 N (see the drawing). Find the angle 𝜃 (in degrees), which is one measure of how the shape of the block has
been altered by shear deformation.
PROBLEM 58 F–
F
59. E SSM Two metal beams are joined together by four rivets, as the draw- ing indicates. Each rivet has a radius of 5.0 × 10−3 m and is to be exposed to
a shearing stress of no more than 5.0 × 108 Pa. What is the maximum tension
T→ that can be applied to each beam, assuming that each rivet carries one- fourth of the total load?
PROBLEM 59
Rivet
–T
T
60. E A copper cylinder and a brass cylinder are stacked end to end, as in the drawing. Each cylinder has a radius of 0.25 cm. A compressive force of
F = 6500 N is applied to the right end of the brass cylinder. Find the amount by which the length of the stack decreases.
PROBLEM 60
Copper
3.0 cm 5.0 cm
Brass F
61. E A piece of aluminum is surrounded by air at a pressure of 1.01 × 105 Pa. The aluminum is placed in a vacuum chamber where the pressure is
reduced to zero. Determine the fractional change ΔV/V0 in the volume of the aluminum.
62. E GO One end of a piano wire is wrapped around a cylindrical tuning peg and the other end is fi xed in place. The tuning peg is turned so as to
stretch the wire. The piano wire is made from steel (Y = 2.0 × 1011 N/m2). It has a radius of 0.80 mm and an unstrained length of 0.76 m. The radius of the
tuning peg is 1.8 mm. Initially, there is no tension in the wire, but when the
tuning peg is turned, tension develops. Find the tension in the wire when the
tuning peg is turned through two revolutions. Ignore the radius of the wire
compared to the radius of the tuning peg.
63. M Available in WileyPLUS. 64. M GO A piece of mohair taken from an Angora goat has a radius of 31 × 10−6 m. What is the least number of identical pieces of mohair needed to
suspend a 75-kg person, so the strain experienced by each piece is less than
0.010? Assume that the tension is the same in all the pieces.
65. M SSM Available in WileyPLUS. 66. M GO A square plate is 1.0 × 10−2 m thick, measures 3.0 × 10−2 m on a side, and has a mass of 7.2 × 10−2 kg. The shear modulus of the material
is 2.0 × 1010 N/m2. One of the square faces rests on a fl at horizontal surface,
and the coeffi cient of static friction between the plate and the surface is 0.91.
A force is applied to the top of the plate, as in Figure 10.29a. Determine (a) the maximum possible amount of shear stress, (b) the maximum possible amount of shear strain, and (c) the maximum possible amount of shear de- formation ΔX (see Figure 10.29b) that can be created by the applied force just before the plate begins to move.
67. M BIO A gymnast does a one-arm handstand. The humerus, which is the upper arm bone (between the elbow and the shoulder joint), may be ap-
proximated as a 0.30-m-long cylinder with an outer radius of 1.00 × 10−2 m
and a hollow inner core with a radius of 4.0 × 10−3 m. Excluding the arm,
the mass of the gymnast is 63 kg. (a) What is the compressional strain of the humerus? (b) By how much is the humerus compressed? 68. M BIO GO Depending on how you fall, you can break a bone easily. The severity of the break depends on how much energy the bone absorbs in
the accident, and to evaluate this let us treat the bone as an ideal spring. The
maximum applied force of compression that one man’s thighbone can endure
without breaking is 7.0 × 104 N. The minimum eff ective cross-sectional area
of the bone is 4.0 × 10−4 m2, its length is 0.55 m, and Young’s modulus is
Y = 9.4 × 109 N/m2. The mass of the man is 65 kg. He falls straight down without rotating, strikes the ground stiff -legged on one foot, and comes to a
halt without rotating. To see that it is easy to break a thighbone when fall-
ing in this fashion, fi nd the maximum distance through which his center of
gravity can fall without his breaking a bone.
69. M SSM Available in WileyPLUS. 70. M V-HINT Available in WileyPLUS. 71. M V-HINT Available in WileyPLUS. 72. H A 6.8-kg bowling ball is attached to the end of a nylon cord with a cross-sectional area of 3.4 × 10−5 m2. The other end of the cord is fi xed
to the ceiling. When the bowling ball is pulled to one side and released
from rest, it swings downward in a circular arc. At the instant it reaches
its lowest point, the bowling ball is 1.4 m lower than the point from which
it was released, and the cord is stretched 2.7 × 10−3 m from its unstrained
length. What is the unstrained length of the cord? (Hint: When calculating any quantity other than the strain, ignore the increase in the length of the cord.) 73. H SSM A solid brass sphere is subjected to a pressure of 1.0 × 105 Pa due to the earth’s atmosphere. On Venus the pressure due to the atmosphere
is 9.0 × 106 Pa. By what fraction Δr/r0 (including the algebraic sign) does the radius of the sphere change when it is exposed to the Venusian atmosphere?
Assume that the change in radius is very small relative to the initial radius.
Additional Problems 287
74. E A loudspeaker diaphragm is producing a sound for 2.5 s by moving back and forth in simple harmonic motion. The angular frequency of the motion is
7.54 × 104 rad/s. How many times does the diaphragm move back and forth?
75. E A person bounces up and down on a trampoline, while always staying in contact with it. The motion is simple harmonic motion, and it takes 1.90 s
to complete one cycle. The height of each bounce above the equilibrium
position is 45.0 cm. Determine (a) the amplitude and (b) the angular fre- quency of the motion. (c) What is the maximum speed attained by the person? 76. E A simple pendulum is swinging back and forth through a small angle, its motion repeating every 1.25 s. How much longer should the pendulum be
made in order to increase its period by 0.20 s?
77. E SSM Available in WileyPLUS. 78. E BIO
The femur is a bone in the leg whose minimum cross-sectional
area is about 4.0 × 10−4 m2. A compressional force in excess of 6.8 × 104 N
will fracture this bone. (a) Find the maximum stress that this bone can with- stand. (b) What is the strain that exists under a maximum-stress condition? 79. E An archer, about to shoot an arrow, is applying a force of +240 N to a drawn bowstring. The bow behaves like an ideal spring whose spring
constant is 480 N/m. What is the displacement of the bowstring?
80. E BIO Between each pair of vertebrae in the spinal column is a cyl- indrical disc of cartilage. Typically, this disc has a radius of about 3.0 × 10−2 m
and a thickness of about 7.0 × 10−3 m. The shear modulus of cartilage is
1.2 × 107 N/m2. Suppose that a shearing force of magnitude 11 N is applied
parallel to the top surface of the disc while the bottom surface remains fi xed
in place. How far does the top surface move relative to the bottom surface?
81. M V-HINT A block rests on a frictionless horizontal surface and is attached to a spring. When set into simple harmonic motion, the block oscillates back
and forth with an angular frequency of 7.0 rad/s. The drawing indicates the po-
sition of the block when the spring is unstrained. This position is labeled “x = 0 m.” The drawing also shows a small bottle located 0.080 m to the right of this
position. The block is pulled to the right, stretching the spring by 0.050 m, and
is then thrown to the left. In order for the block to knock over the bottle, it must
be thrown with a speed exceeding 𝜐0. Ignoring the width of the block, fi nd 𝜐0.
PROBLEM 81
x = 0 m
v0
0.080 m
0.050 m
82. M GO A vertical ideal spring is mounted on the fl oor and has a spring constant of 170 N/m. A 0.64-kg block is placed on the spring in two diff erent
ways. (a) In one case, the block is placed on the spring and not released until it rests stationary on the spring in its equilibrium position. Determine the
amount (magnitude only) by which the spring is compressed. (b) In a second situation, the block is released from rest immediately after being placed on
the spring and falls downward until it comes to a momentary halt. Determine
the amount (magnitude only) by which the spring is now compressed.
83. M Multiple-Concept Example 6 reviews the principles that play roles in this problem. A bungee jumper, whose mass is 82 kg, jumps from a tall plat-
form. After reaching his lowest point, he continues to oscillate up and down,
reaching the low point two more times in 9.6 s. Ignoring air resistance and as-
suming that the bungee cord is an ideal spring, determine its spring constant.
84. M MMH Available in WileyPLUS.
85. M GO When an object of mass m1 is hung on a vertical spring and set into vertical simple harmonic motion, it oscillates at a frequency of 12.0 Hz. When
another object of mass m2 is hung on the spring along with the fi rst object, the frequency of the motion is 4.00 Hz. Find the ratio m2/m1 of the masses. 86. M SSM Available in WileyPLUS. 87. H Available in WileyPLUS. 88. H SSM Available in WileyPLUS. 89. H BIO A cylindrically shaped piece of collagen (a substance found in the body in connective tissue) is being stretched by a force that increases
from 0 to 3.0 × 10−2 N. The length and radius of the collagen are, respect-
ively, 2.5 and 0.091 cm, and Young’s modulus is 3.1 × 106 N/m2. (a) If the stretching obeys Hooke’s law, what is the spring constant k for collagen? (b) How much work is done by the variable force that stretches the collagen? (See Section 6.9 for a discussion of the work done by a variable force.)
90. H SSM The drawing shows a top view of a frictionless horizontal sur- face, where there are two springs with particles of mass m1 and m2 attached to them. Each spring has a spring constant of 120 N/m. The particles are pulled
to the right and then released from the positions shown in the drawing. How
much time passes before the particles are side by side for the fi rst time at x = 0 m if (a) m1 = m2 = 3.0 kg and (b) m1 = 3.0 kg and m2 = 27 kg?
PROBLEM 90
m1
m2
Position of unstrained
spring (x = 0 m)
91. H Available in WileyPLUS. 92. M GO A helicopter is using a steel cable to lift a 2100-kg jeep (see the fi gure). The unstretched length of the cable is 16 m, and its radius is
5.0 × 10−3 m. By what amount does the cable stretch when the jeep is hoisted
straight upward with an acceleration of +1.5 m/s2?
Additional Problems
(a) (b) Free-body diagram for the jeep
ay = +1.5 m/s2
F
W
+y
(a) The jeep applies a force −F→ to the lower end of the cable, thereby stretching it. (b) The free-body diagram for the jeep, showing the two forces acting on it.
PROBLEM 92
288 CHAPTER 10 Simple Harmonic Motion and Elasticity
This chapter has examined an important kind of vibratory motion known
as simple harmonic motion. Specifi cally, it has discussed how the motion’s
displacement, velocity, and acceleration vary with time, and explained what
determines the frequency of the motion. In addition, we saw that the elastic
force is conservative, so that the total mechanical energy is conserved if
nonconservative forces, such as friction and air resistance, are absent. We
conclude now with some problems that review important features of simple
harmonic motion.
93. M CHALK SSM A 75-kg diver is standing at the end of a diving board while it is vibrating up and down in simple harmonic motion, as indic-
ated in the fi gure. The diving board has an eff ective spring constant of k = 4100 N/m, and the vertical distance between the highest and lowest points
in the motion is 0.30 m. Concepts: (i) How is the amplitude A related to the vertical distance between the highest and lowest points of the diver’s
motion? (ii) Starting from the top, where is the diver located one-quarter of
a period later, and what can be said about his speed at this point? (iii) If the
amplitude were to double, would the period also double? Explain. Calcula- tions: (a) What is the amplitude of the motion? (b) Starting when the diver is at the highest point, what is his speed one-quarter of a period later? (c) If the vertical distance between his highest and lowest points were changed to
0.10 m, what would be the time required for the diver to make one complete
motional cycle?
PROBLEM 93
0.30 m
94. M CHALK A 68.0-kg bungee jumper is standing on a tall platform (h0 = 46.0 m), as indicated in the fi gure. The bungee cord has a natural length of
L0 = 9.00 m and, when stretched, behaves like an ideal spring with a spring constant of k = 66.0 N/m. The jumper falls from rest, and it is assumed that the only forces acting on him are his weight and, for the latter part of the descent,
the elastic force of the bungee cord. Concepts: (i) Can we use the conservation of mechanical energy to fi nd his speed at any point along the descent? Explain
your answer. (ii) What type of energy does he have when he is standing on the
platform? (iii) What types of energy does he have at point A? (iv) What types
of energy does he have at point B? Calculations: What is his speed when he is at the following heights above the water: (a) hA = 37.0 m, and (b) hB = 15.0 m?
PROBLEM 94
L0 = 9.00 m
h0 = 46.0 m
hA = 37.0 m
hB = 15.0 m
A
B
Concepts and Calculations Problems
95. M Bungee Cord Escape. You are running from pirates on a tropical island somewhere in the Caribbean. You have somehow become separated from
the rest of your group and now fi nd yourself on the edge of a cliff with your
pursuers less than 10 minutes behind you. According to a sign posted on the
guardrail at the cliff ’s edge, the drop to the beach below is h =140 feet. Your team members (waiting for you on the beach, near your boat) have a rope, but
there is no time for anyone to climb the cliff to save you. You break into a deser-
ted cabin nearby, and rummage around for a rope. Instead, you fi nd a brand new,
still-in-package, bungee cord that must have been intended for tourists jumping
from a nearby bridge. You fi gure you might be able to attach it to the guardrail
and jump to the beach, letting go at the bottom before it reverses your motion.
You read the bungee cord specifi cations on the package: the total length of the
cord is L0 = 100 m, the maximum elastic deformation is 200% (i.e., it can safely triple its length), and the elastic constant is k = 75.0 N/m. (a) If you weigh 170 lb, how far is the bungee cord designed to let you fall before it stops you
and reverses your direction? Will this aff ord you a safe landing? (b) You realize that you don’t have to hang from the very end of the bungee, but rather from
some point in the middle. How far from the attached end should you grasp the
unstretched bungee cord so that you land softly on the beach? Will you be able
to perform the jump and stay under the elastic deformation limit?
96. M A Light-Beam Metronome. You are given the task of opening an antiquated “light lock,” which is unlocked by shining red light pulses of a
certain frequency for a long duration of time into a light sensor on the lock.
You are given a red laser pointer, a spring of unstretched length L = 15.0 cm and spring constant k = 7.20 N/m, a sheet of steel (ρ = 7.60 g/cm3) that is 0.125 inches thick, and some tools. You come up with the idea to take a piece
of the steel sheet (of mass m), cut a slot in it, and hang it from the spring. If you shine the laser through the slot and onto the sensor, and then stretch the
spring and let it go, the steel plate will oscillate and cause the beam to pass
through the slot periodically. (a) Assuming the beam is passing through the slot (and onto the lock’s sensor) when the spring-mass system is in equilib-
rium, how is the frequency at which the light pulses hit the sensor related to
the frequency of the spring/mass (i.e., steel plate) system. (b) Based on your answer for (a), what should be the frequency of the spring/mass system if
the unlocking frequency is 3.50 Hz? (c) What should be the mass m of the steel plate? (d) Calculate some reasonable dimensions for the steel plate (i.e., they should be consistent with the mass that is required for the spring-mass
system). You may assume the material removed to make the slot in the steel
plate is of negligible mass.
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
11.1 Define mass density.
11.2 Define pressure.
11.3 Relate pressure and depth in a static fluid.
11.4 Discriminate between gauge, atmospheric, and absolute pressures.
11.5 Apply Pascal’s principle.
11.6 Solve statics problems using the buoyant force.
11.7 Identify types of fluid flow.
11.8 Apply the equation of continuity.
11.9 Use Bernoulli’s equation to relate speed, pressure, and elevation.
11.10 Apply Bernoulli’s equation for moving fluids.
11.11 Analyze viscous flow in moving liquids.
D es
ig n P
ic s
In c/
A la
m y S
to ck
P h o to
CHAPTER 11
Fluids
The air is a fl uid, and this chapter examines the forces and pressures that fl uids exert when they are at rest
and when they are in motion. In a tornado the air is moving very rapidly, and as we will see, moving air
has a lower pressure than that of stationary air. This diff erence in air pressure is one of the reasons that
tornadoes, such as the one in this photograph, are so destructive.
11.1 Mass Density Fluids are materials that can fl ow, and they include both gases and liquids. Air is the
most common gas, and fl ows from place to place as wind. Water is the most famil-
iar liquid, and fl owing water has many uses, from generating hydroelectric power to
white-water rafting. The mass density of a liquid or gas is one of the important factors that determine its behavior as a fl uid. As indicated below, the mass density is the mass
per unit volume and is denoted by the Greek letter rho (ρ).
DEFINITION OF MASS DENSITY The mass density ρ is the mass m of a substance divided by its volume V:
ρ = m V
(11.1)
SI Unit of Mass Density: kg/m3
Equal volumes of diff erent substances generally have diff erent masses, so the
density depends on the nature of the material, as Table 11.1 indicates. Gases have the smallest densities because gas molecules are relatively far apart and a gas contains a
large fraction of empty space. In contrast, the molecules are much more tightly packed
in liquids and solids, and the tighter packing leads to larger densities. The densities
of gases are very sensitive to changes in temperature and pressure. However, for the
range of temperatures and pressures encountered in this text, the densities of liquids
and solids do not diff er much from the values in Table 11.1. 289
290 CHAPTER 11 Fluids
It is the mass of a substance, not its weight, that enters into the defi nition of density. In situ-
ations where weight is needed, it can be calculated from the mass density, the volume, and the
acceleration due to gravity, as Example 1 illustrates.
EXAMPLE 1 Blood as a Fraction of Body Weight
The body of a man whose weight is 690 N contains about 5.2 × 10−3 m3
(5.5 qt) of blood. (a) Find the blood’s weight and (b) express it as a percentage of the body weight.
Reasoning To fi nd the weight W of the blood, we need the mass m, since W = mg (Equation 4.5), where g is the magnitude of the acceleration due to gravity. According to Table 11.1, the density of blood is 1060 kg/ m3, so the mass of the blood can be found by using the given volume of
5.2 × 10−3 m3 in Equation 11.1.
Solution (a) According to Equation 4.5, the blood’s weight is W = mg. Equation 11.1 can be solved for m to show that the mass is m = ρV. Sub- stituting this result into Equation 4.5 gives
W = mg = (ρV )g = (1060 kg/m3)(5.2 × 10−3 m3)(9.80 m/s2) = 54 N
(b) The percentage of body weight contributed by the blood is
Percentage = 54 N
690 N × 100 = 7.8%
A convenient way to compare densities is to use the concept of specifi c gravity. The specifi c gravity of a substance is its density divided by the density of a standard reference material, usu-
ally chosen to be water at 4° C.
Specific gravity = Density of substance
Density of water at 4 °C =
Density of substance
1.000 ×103 kg/m3 (11.2)
Being the ratio of two densities, specifi c gravity has no units. For example, Table 11.1 reveals that diamond has a specifi c gravity of 3.52, since the density of diamond is 3.52 times the density
of water at 4 °C.
The next two sections deal with the important concept of pressure. We will see that the
density of a fl uid is one factor determining the pressure that a fl uid exerts.
TABLE 11.1 Mass Densitiesa of Common Substances
Substance Mass Density ρ
(kg/m3) Substance Mass Density ρ
(kg/m3) Solids Liquids Aluminum 2700 Blood (whole, 37 °C) 1060
Brass 8470 Ethyl alcohol 806
Concrete 2200 Mercury 13 600
Copper 8890 Oil (hydraulic) 800
Diamond 3520 Water (4 °C) 1.000 × 103
Gold 19 300 Gases Ice 917 Air 1.29
Iron (steel) 7860 Carbon dioxide 1.98
Lead 11 300 Helium 0.179
Quartz 2660 Hydrogen 0.0899
Silver 10 500 Nitrogen 1.25
Wood (yellow pine) 550 Oxygen 1.43
a Unless otherwise noted, densities are given at 0 °C and 1 atm pressure.
11.2 Pressure 291
11.2 Pressure People who have fi xed a fl at tire know something about pressure. The fi nal step in the job is to
reinfl ate the tire to the proper pressure. The underinfl ated tire is soft because it contains an insuf-
fi cient number of air molecules to push outward against the rubber and give the tire that solid feel.
When air is added from a pump, the number of molecules and the collective force they exert are
increased. The air molecules within a tire are free to wander throughout its entire volume, and in
the course of their wandering they collide with one another and the inner walls of the tire. The
collisions with the walls allow the air to exert a force against every part of the wall surface, as
Figure 11.1 shows. The pressure P exerted by a fl uid is defi ned in Section 10.7 (Equation 10.19) as the magnitude F of the force acting perpendicular to a surface divided by the area A over which the force acts:
P = F A
(11.3)
The SI unit for pressure is a newton/meter2 (N/m2), a combination that is referred to as a
pascal (Pa). A pressure of 1 Pa is a very small amount. Many common situations involve pres- sures of approximately 105 Pa, an amount referred to as one bar of pressure. Alternatively, force can be measured in pounds and area in square inches, so another unit for pressure is pounds per
square inch (lb/in.2), often abbreviated as “psi.”
Because of its pressure, the air in a tire applies a force to any surface with which the air is in
contact. Suppose, for instance, that a small cube is inserted inside the tire. As Figure 11.1 shows, the air pressure causes a force to act perpendicularly on each face of the cube. In a similar fash-
ion, a liquid such as water also exerts pressure. A swimmer, for example, feels the water pushing
perpendicularly inward everywhere on her body, as Figure 11.2 illustrates. In general, a static fl uid cannot produce a force parallel to a surface, for if it did, the surface would apply a reaction
force to the fl uid, consistent with Newton’s action–reaction law. In response, the fl uid would fl ow
and would not then be static.
While fl uid pressure can generate a force, which is a vector quantity, pressure itself is not a vector. In the defi nition of pressure, P = F/A, the symbol F refers only to the magnitude of the force, so that pressure has no directional characteristic. The force generated by the pres-
sure of a static fl uid is always perpendicular to the surface that the fl uid contacts, as Example 2
illustrates.
F
FIGURE 11.1 In colliding with the inner walls of the tire, the air molecules
(blue dots) exert a force on every part
of the wall surface. If a small cube
were inserted inside the tire, the cube
would experience forces (blue arrows)
acting perpendicular to each of its six
faces.
F
FIGURE 11.2 Water applies a force perpendicular to each surface within
the water, including the walls and
bottom of the swimming pool, and all
parts of the swimmer’s body.
292 CHAPTER 11 Fluids
A person need not be under water to experience the eff ects of pressure. Walking about on
land, we are at the bottom of the earth’s atmosphere, which is a fl uid and pushes inward on our
bodies just like the water in a swimming pool. As Figure 11.3 indicates, there is enough air above the surface of the earth to create the following pressure at sea level:
Atmospheric pressure 1.013 × 105 Pa = 1 atmosphereat sea level
This pressure corresponds to 14.70 lb/in.2 and is referred to as one atmosphere (atm), a signifi cant amount of pressure. Look, for instance, in Figure 11.3 at the results of pumping out the air from within a gasoline can. With no internal air to push outward, the inward push of the external air is
unbalanced and is strong enough to crumple the can.
THE PHYSICS OF . . . lynx paws. In contrast to the situation in Figure 11.3, reducing the pressure is sometimes benefi cial. Lynx, for example, are well suited for hunting on snow
because of their oversize paws (see Figure 11.4). The large paws act as snowshoes and distribute the weight over a large area. Thus, they reduce the weight per unit area, or the pressure that the
cat applies to the surface, which helps to keep it from sinking into the snow.
Check Your Understanding
(The answers are given at the end of the book.) 1. BIO As you climb a mountain, your ears “pop” because of the changes in atmospheric pressure. In
which direction, outward or inward, does your eardrum move (a) as you climb up and (b) as you climb down?
2. A bottle of juice is sealed under partial vacuum, with a lid on which a red dot or “button” is painted. Around the button the following phrase is printed: “Button pops up when seal is broken.” Why does
the button remain pushed in when the seal is intact? (a) The pressure inside the bottle is greater than the pressure outside the bottle. (b) The pressure inside the bottle is less than the pressure out- side the bottle. (c) There is a greater force acting on the interior surface of the seal than acts on the exterior surface.
3. A method for resealing a partially full bottle of wine under a vacuum uses a specially designed rubber stopper to close the bottle. A simple pump is attached to the stopper, and to remove air
from the bottle, the plunger of the pump is pulled up and then released. After about 15 pull-and-
release cycles the wine is under a partial vacuum. On the fi fteenth pull-and-release cycle, does it
require (a) more force, (b) less force, or (c) the same force to pull the plunger up than it did on the fi rst cycle?
EXAMPLE 2 The Force on a Swimmer
Suppose that the pressure acting on the back of a swimmer’s hand is
1.2 × 105 Pa, a realistic value near the bottom of the diving end of a pool.
The surface area of the back of the hand is 8.4 × 10−3 m2. (a) Determine the magnitude of the force that acts on it. (b) Discuss the direction of the force.
Reasoning From the defi nition of pressure in Equation 11.3, we can see that the magnitude of the force is the pressure times the area. The
direction of the force is always perpendicular to the surface that the water
contacts.
Problem-Solving Insight Force is a vector, but pressure is not.
Solution (a) A pressure of 1.2 × 105 Pa is 1.2 × 105 N/m2. From Equa- tion 11.3, we fi nd
F = PA = (1.2 × 105 N/m2)(8.4 ×10−3 m2) = 1.0 × 103 N
This is a rather large force, about 230 lb.
(b) In Figure 11.2, the hand (palm downward) is oriented parallel to the bottom of the pool. Since the water pushes perpendicularly against
the back of the hand, the force F →
is directed downward in the drawing.
This downward-acting force is balanced by an upward-acting force on the
palm, so that the hand is in equilibrium. If the hand were rotated by 90°,
the directions of these forces would also be rotated by 90°, always being
perpendicular to the hand.
Area of base = 1.000 m2
Force = 1.013 × 105 N
Crumpled can Pump
FIGURE 11.3 Atmospheric pressure at sea level is 1.013 × 105 Pa, which is suffi cient to
crumple a can if the inside air is pumped out.
Altrendo Nature/Getty Images
FIGURE 11.4 Lynx have large paws that act as natural snowshoes.
11.3 Pressure and Depth in a Static Fluid 293
11.3 Pressure and Depth in a Static Fluid The deeper an underwater swimmer goes, the more strongly the water pushes on his body and
the greater is the pressure that he experiences. To determine the relation between pressure and
depth, we turn to Newton’s second law ( ΣF→ = ma→). In using the second law, we will focus on two external forces that act on the fl uid. One is the gravitational force—that is, the weight of
the fl uid. The other is the collisional force that is responsible for fl uid pressure, as Section 11.2
discusses. Since the fl uid is at rest, its acceleration is zero ( a→ = 0 m/s2), and it is in equilibrium. By applying the second law in the form ΣF→ = 0, we will derive a relation between pressure and depth. This relation is especially important because it leads to Pascal’s principle (Section 11.5)
and Archimedes’ principle (Section 11.6), both of which are essential in describing the properties
of static fl uids.
Interactive Figure 11.5 shows a container of fl uid and focuses attention on one column of the fl uid. The free-body diagram in the fi gure shows all the vertical forces acting on the column.
On the top face (area = A), the fl uid pressure P1 generates a downward force whose magnitude is P1A. Similarly, on the bottom face, the pressure P2 generates an upward force of magnitude P2A. The pressure P2 is greater than the pressure P1 because the bottom face supports the weight of more fl uid than the upper one does. In fact, the excess weight supported by the bottom face
is exactly the weight of the fl uid within the column. As the free-body diagram indicates, this
weight is mg, where m is the mass of the fl uid and g is the magnitude of the acceleration due to gravity. Since the column is in equilibrium, we can set the sum of the vertical forces equal to
zero and fi nd that
ΣFy = P2 A − P1 A − mg = 0 or P2 A = P1 A + mg
The mass m is related to the density ρ and the volume V of the column by m = ρV (Equation 11.1). Since the volume is the cross-sectional area A times the vertical dimension h, we have m = ρAh. With this substitution, the condition for equilibrium becomes P2 A = P1A + ρAhg. The area A can be eliminated algebraically from this expression, with the result that
P2 = P1 + ρgh (11.4)
Equation 11.4 indicates that if the pressure P1 is known at a higher level, the larger pressure P2 at a deeper level can be calculated by adding the increment ρgh. In determining the pressure increment ρgh, we assumed that the density ρ is the same at any vertical distance h or, in other words, the fl uid is incompressible. The assumption is reasonable for liquids, since the bottom
layers can support the upper layers with little compression. In a gas, however, the lower layers
are compressed markedly by the weight of the upper layers, with the result that the density varies
with vertical distance. For example, the density of our atmosphere is larger near the earth’s sur-
face than it is at higher altitudes. When applied to gases, the relation P2 = P1 + ρgh can be used only when h is small enough that any variation in ρ is negligible.
h
+y axis
mg
(a) (b) Free-body diagram
of the column
Pressure Area
= P1 = A
Pressure Area
= P2 = A
P1A
P2A INTERACTIVE FIGURE 11.5 (a) A container
of fl uid in which one column of the fl uid is
outlined. The fl uid is at rest. (b) The free-body diagram, showing the vertical forces acting on
the column.
294 CHAPTER 11 Fluids
The next example deals further with the relationship between pressure and depth given by
Equation 11.4.
CONCEPTUAL EXAMPLE 3 The Hoover Dam
Lake Mead is the largest wholly artifi cial reservoir in the United States
and was formed after the completion of the Hoover Dam in 1936. As
Figure 11.6a suggests, the water in the reservoir backs up behind the dam for a considerable distance (about 200 km or 120 miles). Suppose that all
the water were removed, except for a relatively narrow vertical column in
contact with the dam. Figure 11.6b shows a side view of this hypotheti- cal situation, in which the water against the dam has the same depth as
in Figure 11.6a. How would the dam needed to contain the water in this hypothetical reservoir compare with the Hoover Dam? Would it need to
be (a) less massive or (b) equally massive?
Reasoning Imagine a small square in the inner face of the dam, located beneath the water. The magnitude of the force on this square is the prod-
uct of its area and the pressure of the water, according to Equation 11.3.
However, the relation P2 = P1 + ρgh (Equation 11.4) indicates that the pressure at a given point depends on the vertical distance h that the small square is below the water. Thus, the force exerted by the water at any
given location depends on the depth at that location.
Answer (a) is incorrect. Since our hypothetical reservoir contains much less water than Lake Mead, it is tempting to say that a less massive
structure would be required. Note from the Reasoning section that the
force exerted on a given section of the dam depends on how far below the
surface the section is located. The horizontal distance of the water backed
up behind the dam does not appear in Equation 11.4, and, therefore, has
no eff ect on the pressure and, hence, on the force.
Answer (b) is correct. The force exerted on a given section of the dam depends only on how far that section is located vertically below the
surface (see the Reasoning section). Certainly, as one goes deeper and
deeper, the water pressure and force become greater. But no matter how
deep one goes, the force that the water applies on a given section of the
dam does not depend on the amount of water backed up behind the dam.
Thus, the dam for our imaginary reservoir would sustain the same forces
that the Hoover Dam sustains and, therefore, would need to be equally
massive.
(a) (b)
FIGURE 11.6 (a) The Hoover Dam in Nevada and Lake Mead behind it. (b) A hypothetical reservoir formed by removing most of the water from Lake Mead. Conceptual Example 3
compares the dam needed for this hypothetical reservoir with the Hoover Dam.
A d am
G . S
y lv
es te
r/ S
ci en
ce S
o u rc
e
A signifi cant feature of Equation 11.4 is that the pressure increment ρgh is aff ected by the vertical distance h, but not by any horizontal distance within the fl uid. Conceptual Example 3 helps to clarify this feature.
11.3 Pressure and Depth in a Static Fluid 295
Figure 11.8 shows an irregularly shaped container of liquid. Reasoning similar to that used in Example 4 leads to the conclusion that the pressure is the same at points A, B, C, and D, since each is at the same vertical distance h beneath the surface. In eff ect, the arteries in our bodies are also an irregularly shaped “container” for the blood. The next example examines the blood pres-
sure at diff erent places in this “container.”
h
A B C D
FIGURE 11.8 Since points A, B, C, and D are at the same distance h beneath the liquid surface, the pressure at each of them is the same.
R ic
h ar
d M
eg n a/
F u n d am
en ta
l P
h o to
g ra
p h s
A´ B´
A B
5.50 m
FIGURE 11.7 The pressures at points A and B are the same, since both points are located at the same vertical
distance of 5.50 m beneath the surface of the water.
EXAMPLE 4 The Swimming Hole
Figure 11.7 shows the cross section of a swimming hole. Points A and B are both located at a distance of h = 5.50 m below the surface of the water. Find the pressure at each of these two points.
Reasoning The pressure at point B is the same as that at point A, since both are located at the same vertical distance beneath the surface and only the vertical distance h aff ects the pressure increment ρgh in Equa- tion 11.4. To understand this important feature more clearly, consider
the path AAʹBʹB in Figure 11.7. The pressure decreases on the way up along the vertical segment AAʹ and increases by the same amount on the way back down along segment BʹB. Since no change in pressure occurs along the horizontal segment AʹBʹ, the pressure is the same at A and B.
Problem-Solving Insight The pressure at any point in a fl uid depends on the vertical distance h of the point beneath the surface. However, for a given vertical distance, the pressure is the same, no matter where the point is located horizontally in the fl uid.
Solution The pressure acting on the surface of the water is the atmo- spheric pressure of 1.01 × 105 Pa. Using this value as P1 in Equation 11.4, we can determine a value for the pressure P2 at either point A or B, both
of which are located 5.50 m under the water. Table 11.1 gives the density of water as 1.000 × 103 kg/m3.
P2 = P1 + ρgh P2 = 1.01 × 105 Pa + (1.000 × 103 kg/m3 )(9.80 m/s2 )(5.50 m)
= 1.55 × 10 5 Pa
296 CHAPTER 11 Fluids
Sometimes fl uid pressure places limits on how a job can be done. Conceptual Example 6
illustrates how fl uid pressure restricts the height to which water can be pumped.
CONCEPTUAL EXAMPLE 6 The Physics of Pumping Water
Figure 11.10 shows two methods for pumping water from a well. In one method, the pump is submerged in the water at the bottom of the well,
while in the other, it is located at ground level. If the well is shallow,
either technique can be used. However, if the well is very deep, only one
of the methods works. Which pumping method works, (a) the submerged pump or (b) the pump located at ground level?
Reasoning To answer this question, we need to examine the nature of the job done by the pump in each place. The pump at the bottom of the
well pushes water up the pipe, while the pump at ground level does not
push water at all. Instead, the ground-level pump removes air from the
pipe, creating a partial vacuum within it. (It’s acting just like you do when
drinking through a straw. You draw some of the air out of the straw, and
the external air pressure pushes the liquid up into it.)
Answer (b) is incorrect. As the pump at ground level removes air from the pipe, the pressure above the water within the pipe is reduced (see point
A in the drawing). The greater air pressure outside the pipe (see point B) pushes water up the pipe. However, even the strongest pump can only
remove all of the air. Once the air is completely removed, an increase in pump strength does not increase the height to which the water is pushed
by the external air pressure. Thus, the ground-level pump can only cause
water to rise to a certain maximum height and cannot be used for very
deep wells.
Answer (a) is correct. For a very deep well, the column of water becomes very tall, and the pressure at the bottom of the pipe becomes
large, due to the pressure increment ρgh in the relation P2 = P1 + ρgh
(Equation 11.4). However, as long as the pump can push with suffi cient
strength to overcome the large pressure, it can shove the next increment of
water into the pipe, so the method can be used for very deep wells.
Related Homework: Problems 21, 93
Reduced air
pressure
A B
Pump
Pump
FIGURE 11.10 A water pump can be placed at the bottom of a well or at
ground level. Conceptual Example 6
discusses the two placements.
EXAMPLE 5 BIO The Physics of Blood Pressure
Blood in the arteries is fl owing, but as a fi rst approximation, the eff ects of
this fl ow can be ignored and the blood treated as a static fl uid. Estimate
the amount by which the blood pressure P2 in the anterior tibial artery at the foot exceeds the blood pressure P1 in the aorta at the heart when a person is (a) reclining horizontally as in Figure 11.9a and (b) standing as in Figure 11.9b.
Reasoning and Solution (a) When the body is horizontal, there is little or no vertical separation between the feet and the heart. Since
h = 0 m,
P2 − P1 = ρgh = 0 Pa (11.4)
(b) When an adult is standing up, the vertical separation between the feet and the heart is about 1.35 m, as Figure 11.9b indicates. Table 11.1 gives the density of blood as 1060 kg/m3, so that
P2 − P1 = ρgh = (1060 kg/m3 )(9.80 m/s2 )(1.35 m) =
= 1.40 × 104 Pa
1.35 m
Aorta
AortaAnterior tibial artery
Anterior tibial artery
Blood pressure = P1
Blood pressure = P2
(a)
(b)
FIGURE 11.9 The blood pressure in the feet can exceed
that in the heart, depending
on whether a person is
(a) reclining horizontally or (b) standing.
11.4 Pressure Gauges 297
Check Your Understanding
(The answers are given at the end of the book.) 4. A scuba diver is swimming under water, and CYU Fig-
ure 11.1 shows a plot of the water pressure acting on the diver as a function of time. In each of the three regions,
(a) A → B, (b) B → C, and (c) C → D, does the depth of the diver increase, decrease, or remain constant?
5. A 15-meter-high tank is closed and completely fi lled with water. A valve is then opened at the bottom of the tank and
water begins to fl ow out. When the water stops fl owing,
will the tank be completely empty, or will there still be a
noticeable amount of water in it?
6. Could you use a straw to sip a drink on the moon? (a) Yes. It would be no diff erent than drinking with a straw on earth. (b) No, because there is no air on the moon and, therefore, no air pressure to push the liquid up the straw. (c) Yes, and it is easier on the moon because the acceleration due to gravity on the moon is only
1
6 of that on the earth.
7. A scuba diver is below the surface of the water when a storm approaches, dropping the air pressure above the water. Would a suffi ciently sensitive pressure gauge attached to his wrist register this drop in
air pressure? Assume that the diver’s wrist does not move as the storm approaches.
11.4 Pressure Gauges One of the simplest pressure gauges is the mercury barometer used for measuring atmospheric
pressure. This device is a tube sealed at one end, fi lled completely with mercury, and then inverted,
so that the open end is under the surface of a pool of mercury (see Figure 11.11). Except for a negligible amount of mercury vapor, the space above the mercury in the tube is empty, and the
pressure P1 is nearly zero there. The pressure P2 at point A at the bottom of the mercury column is the same as the pressure at point B—namely, atmospheric pressure—because these two points are at the same level. With P1 = 0 Pa and P2 = Patm, it follows from Equation 11.4 that Patm = 0 Pa + ρgh. Thus, the atmospheric pressure can be determined from the height h of the mercury in the tube, the density ρ of mercury, and the acceleration due to gravity. Usually, weather forecasters report the pressure in terms of the height h, expressing it in millimeters or inches of mercury. For instance, using Patm = 1.013 × 105 Pa and ρ = 13.6 × 103 kg/m3 for the density of mercury, we fi nd that h = Patm /(ρg) = 760 mm (29.9 inches).* Slight variations from this value occur, depending on weather conditions and altitude.
Figure 11.12 shows another kind of pressure gauge, the open-tube manometer. The phrase “open-tube” refers to the fact that one side of the U-tube is open to atmospheric pressure. The
tube contains a liquid, often mercury, and its other side is connected to the container whose
pressure P2 is to be measured. When the pressure in the container is equal to the atmospheric pressure, the liquid levels in both sides of the U-tube are the same. When the pressure in the
container is greater than atmospheric pressure, as in Figure 11.12, the liquid in the tube is pushed downward on the left side and upward on the right side. The relation P2 = P1 + ρgh can be used to determine the container pressure. Atmospheric pressure exists at the top of the
right column, so that P1 = Patm. The pressure P2 is the same at points A and B, so we fi nd that P2 = Patm + ρgh, or
P2 − Patm = ρgh
The height h is proportional to P2 − Patm, which is called the gauge pressure. The gauge pres- sure is the amount by which the container pressure diff ers from atmospheric pressure. The actual
value for P2 is called the absolute pressure.
Time
A
B
C DP re
ss ur
e
CYU FIGURE 11.1
h
A
B (P2 = Atmospheric pressure)
Empty, except for a negligible amount of mercury vapor (P1 = 0 Pa)
FIGURE 11.11 A mercury barometer.
A
P1 = Patm
P2 > Patm
h
B
FIGURE 11.12 The U-shaped tube is called an open-tube manometer and can be used to
measure the pressure P2 in a container. *A pressure of one millimeter of mercury is sometimes referred to as one torr, to honor the inventor of the barometer, Evangelista Torricelli (1608–1647). Thus, one atmosphere of pressure is 760 torr.
298 CHAPTER 11 Fluids
Problem-Solving Insight When solving problems that deal with pressure, be sure to note the distinction between gauge pressure and absolute pressure.
BIO THE PHYSICS OF . . . a sphygmomanometer. The sphygmomanometer is a familiar device for measuring blood pressure. As Figure 11.13 illustrates, a squeeze bulb can be used to infl ate the cuff with air, which cuts off the fl ow of blood through the artery below
the cuff . When the release valve is opened, the cuff pressure drops. Blood begins to fl ow again
when the pressure created by the heart at the peak of its beating cycle exceeds the cuff pressure.
Using a stethoscope to listen for the initial fl ow, the operator can measure the corresponding
cuff gauge pressure with, for example, an open-tube manometer. This cuff gauge pressure is
called the systolic pressure. Eventually, there comes a point when even the pressure created by the heart at the low point of its beating cycle is suffi cient to cause blood to fl ow. Identifying this
point with the stethoscope, the operator can measure the corresponding cuff gauge pressure,
which is referred to as the diastolic pressure. The systolic and diastolic pressures are reported in millimeters of mercury, and values of less than 120 and 80, respectively, are typical of a
young, healthy heart.
11.5 Pascal’s Principle As we have seen, the pressure in a fl uid increases with depth, due to the weight of the fl uid
above the point of interest. A completely enclosed fl uid may be subjected to an additional
pressure by the application of an external force. For example, Figure 11.14a shows two inter- connected cylindrical chambers. The chambers have diff erent diameters and, together with
the connecting tube, are completely fi lled with a liquid. The larger chamber is sealed at the
top with a cap, while the smaller one is fi tted with a movable piston. Consider the pressure
P1 at a point immediately beneath the piston. According to the defi nition of pressure, it is the magnitude F1 of the external force divided by piston area A1, or P1 = F1/A1. If it is necessary to know the pressure P2 at any deeper place in the liquid, we just add to the value of P1 the increment ρgh, which takes into account the depth h below the piston: P2 = P1 + ρgh. The important feature here is this: The pressure P1 adds to the pressure ρgh due to the depth of the liquid at any point, whether that point is in the smaller chamber, the connecting tube, or the
larger chamber. Therefore, if the applied pressure P1 is increased or decreased, the pressure at any other point within the confi ned liquid changes correspondingly. This behavior is described
by Pascal’s principle.
PASCAL’S PRINCIPLE Any change in the pressure applied to a completely enclosed fl uid is transmitted undi- minished to all parts of the fl uid and the enclosing walls.
The usefulness of the arrangement in Figure 11.14a becomes apparent when we calculate the force F2 applied by the liquid to the cap on the right side. The area of the cap is A2 and the pressure there is P2. As long as the tops of the left and right chambers are at the same level, the pressure increment ρgh is zero, so that the relation P2 = P1 + ρgh becomes P2 = P1. Consequently, F2/A2 = F1/A1, and
F2 = F1(A2A1) (11.5) If area A2 is larger than area A1, a large force F2
→ can be applied to the cap on the right chamber,
starting with a smaller force F1 →
on the left. Depending on the ratio of the areas A2 /A1, the force F2 →
can be large indeed, as in the familiar hydraulic car lift shown in Figure 11.14b. In this device the force F2
→ is not applied to a cap that seals the larger chamber, but, rather, to a movable plunger
that lifts a car. Examples 7 and 8 deal with a hydraulic car lift.
Cuff
Stethoscope
Release valve
Squeeze bulb
Open-tube manometer
FIGURE 11.13 A sphygmomanometer is used to measure blood pressure.
F2
A1 A2
F1
(a)
A1
h
B F2
F1
A
(b)
FIGURE 11.14 (a) An external force F1 →
is
applied to the piston on the left. As a result, a
force F2 →
is exerted on the cap on the chamber
on the right. (b) The familiar hydraulic car lift.
11.5 Pascal’s Principle 299
EXAMPLE 7 The Physics of a Hydraulic Car Lift
In the hydraulic car lift shown in Figure 11.14b, the input piston on the left has a radius of r1 = 0.0120 m and a negligible weight. The output plunger on the right has a radius of r2 = 0.150 m. The combined weight of the car and the plunger is 20 500 N. Since the output force has a
magnitude of F2 = 20 500 N, it supports the car. Suppose that the bottom surfaces of the piston and plunger are at the same level, so that h = 0 m in Figure 11.14b. What is the magnitude F1 of the input force needed so that F2 = 20 500 N?
Reasoning When the bottom surfaces of the piston and plunger are at the same level, as in Figure 11.14a, Equation 11.5 applies, and we can use it to determine F1.
Problem-Solving Insight Note that the relation F1 = F2(A1/ A2), which results from Pascal’s principle, applies only when the points 1 and 2 lie at the same depth (h = 0 m) in the fl uid.
Solution According to Equation 11.5, we have
F2 = F1 ( A2 A1) or F1 = F2 (
A1 A2)
Using A = 𝜋r2 for the circular areas of the piston and plunger, we fi nd that
F1 = F2 ( A1 A2) = F2 (
πr12
πr 22 ) = (20 500 N) (0.0120 m)2
(0.150 m)2 = 131 N
F2
A1 A2
F1
(a)
A1
h
B F2
F1
A
(b)
FIGURE 11.14 (REPEATED) (a) An external force F1
→ is
applied to the piston on the
left. As a result, a force F2 →
is exerted on the cap on the
chamber on the right. (b) The familiar hydraulic car lift.
Analyzing Multiple-Concept Problems
EXAMPLE 8 A Car Lift Revisited
The data are the same as in Example 7. Suppose now, however, that the
bottom surfaces of the piston and plunger are at diff erent levels, such that h = 1.10 m in Figure 11.14b. The car lift uses hydraulic oil that has a density of 8.00 × 102 kg/m3. What is the magnitude F1 of the input force that is now needed to produce an output force having a magnitude of F2 = 20 500 N?
Reasoning Since the bottom surfaces of the piston and plunger are at dif- ferent levels, Equation 11.5 no longer applies. Our approach will be based
on the defi nition of pressure (Equation 11.3) and the relation between
pressure and depth given in Equation 11.4. It is via Equation 11.4 that
we will take into account the fact that the bottom of the output plunger is
h = 1.10 m below the bottom of the input piston.
Knowns and Unknowns We have the following data:
Description Symbol Value Comment Radius of input piston r1 0.0120 m
Radius of output piston r2 0.150 m
Magnitude of output force F2 20 500 N
Density of hydraulic oil ρ 8.00 × 102 kg/m3
Level difference between input
piston and output plunger
h 1.10 m See Figure 11.14b.
Unknown Variables Magnitude of input force F1 ?
300 CHAPTER 11 Fluids
Modeling the Problem
STEP 1 Force and Pressure The input force F1 is determined by the pressure P1 acting on the bottom surface of the input piston, which has an area A1. According to Equation 11.3, the input force is F1 = P1A1, where A1 = 𝜋r12 because the piston has a circular cross section with a radius r1. With this expression for the area A1, the input force can be written as in Equation 1 at the right. We have a value for r1, but P1 is unknown, so we turn to Step 2 in order to obtain it.
STEP 2 Pressure and Depth in a Static Fluid In Figure 11.14b, the bottom surface of the plunger at point B is at the same level as point A, which is at a depth h beneath the input piston. Equation 11.4 applies, so that
P2 = P1 + ρgh or P1 = P2 − ρgh
This result for P1 can be substituted into Equation 1, as shown at the right. Now it is necessary to have a value for P2, the pressure at the bottom surface of the output plunger, which we obtain in Step 3.
STEP 2 Pressure and Force By using Equation 11.3, we can relate the unknown pressure P2 to the given output force F2 and the area A2 of the bottom surface of the output plunger: P2 = F2/A2. The area A2 is a circle with a radius r2, so A2 = 𝜋r22. Thus, the pressure P2 is
P2 = F2 πr22
At the right, this result is substituted into Equation 2.
Solution Combining the results of each step algebraically, we fi nd that
F1 = P1πr12 = (P2 − ρgh)πr12 = ( F2
πr22 − ρgh)πr12
Thus, we fi nd that the necessary input force is
F1 = F2r12
r 22 − ρghπr12
= (20 500 N)(0.0120 m)2
(0.150 m)2 − (8.00 × 102 kg/m3)(9.80 m/s2)(1.10 m)π (0.0120 m)2
= 127 N
The answer here is less than the answer in Example 7 because the weight of the 1.10-m column
of hydraulic oil provides some of the input force to support the car and plunger.
Related Homework: Problem 35
STEP 1 STEP 2 STEP 3
F1 = P1πr12 (1)
?
F1 = P1πr12 (1)
P1 = P2 − ρgh (2)
?
F1 = P1πr12 (1)
P1 = P2 − ρgh (2)
P2 = F2 πr 22
In a device such as a hydraulic car lift, the same amount of work is done by both the input
and output forces in the absence of friction. The larger output force F2 →
moves through a smaller
distance, while the smaller input force F1 →
moves through a larger distance. The work, being the
product of the magnitude of the force and the distance, is the same in either case since mechanical
energy is conserved (assuming that friction is negligible).
An enormous variety of clever devices use hydraulic fl uids, just as the car lift does. In
Figure 11.15, for instance, a hydraulic fl uid multiplies a small input force into the large output force required to operate the digging scoop of the excavator.
11.6 Archimedes’ Principle Anyone who has tried to push a beach ball under the water has felt how the water pushes back
with a strong upward force. This upward force is called the buoyant force, and all fl uids apply such a force to objects that are immersed in them. The buoyant force exists because fl uid pressure
is larger at greater depths.
11.6 Archimedes’ Principle 301
In Interactive Figure 11.16 a cylinder of height h is being held under the surface of a liquid. The pressure P1 on the top face generates the downward force P1A, where A is the area of the face. Similarly, the pressure P2 on the bottom face generates the upward force P2 A. Since the pressure is greater at greater depths, the upward force exceeds the downward force. Consequently, the
liquid applies to the cylinder a net upward force, or buoyant force, whose magnitude FB is
FB = P2 A − P1A = (P2 − P1)A = ρghA
We have substituted P2 − P1 = ρgh from Equation 11.4 into this result. In so doing, we fi nd that the buoyant force equals ρghA. The quantity hA is the volume of liquid that the cylinder moves aside or displaces in being submerged, and ρ denotes the density of the liquid, not the density of the material from which the cylinder is made. Therefore, ρhA gives the mass m of the displaced fl uid, so that the buoyant force equals mg, the weight of the displaced fl uid. The phrase “weight of the displaced fl uid” refers to the weight of the fl uid that would spill out if the container were
fi lled to the brim before the cylinder is inserted into the liquid. The buoyant force is not a new
type of force. It is just the name given to the net upward force exerted by the fl uid on the object.
The shape of the object in Interactive Figure 11.16 is not important. No matter what its shape, the buoyant force pushes it upward in accord with Archimedes’ principle. It was an impressive accomplishment that the Greek scientist Archimedes (ca. 287–212 BC) discovered the
essence of this principle so long ago.
ARCHIMEDES’ PRINCIPLE Any fl uid applies a buoyant force to an object that is partially or completely immersed in it; the magnitude of the buoyant force equals the weight of the fl uid that the object displaces:
FB = Wfl uid (11.6)
The eff ect that the buoyant force has depends on its strength compared with the strengths of
the other forces that are acting. For example, if the buoyant force is strong enough to balance the
force of gravity, an object will fl oat in a fl uid. Figure 11.17 explores this possibility. In part a, a block that weighs 100 N displaces some liquid, and the liquid applies a buoyant force FB to the block, according to Archimedes’ principle. Nevertheless, if the block were released, it would fall
further into the liquid because the buoyant force is not suffi ciently strong to balance the weight
of the block. In part b, however, enough of the block is submerged to provide a buoyant force that can balance the 100-N weight, so the block is in equilibrium and fl oats when released. If
the buoyant force were not large enough to balance the weight, even with the block completely
submerged, the block would sink. Even if an object sinks, there is still a buoyant force acting on
it; it’s just that the buoyant force is not large enough to balance the weight. Example 9 provides
additional insight into what determines whether an object fl oats or sinks in a fl uid.
⏟⏟⏟ Magnitude of
buoyant force
⏟⏟⏟ Weight of
displaced fl uid
FIGURE 11.15 Excavators such as this one are a familiar sight at construction jobs. They
use hydraulic fl uids to generate the large
output forces necessary for digging. The
shiny cylinder attached to the digging scoop
is a sure sign that a hydraulic fl uid is at work.
Henrich van den Berg/Getty Images
h
A
P1A
P2A
INTERACTIVE FIGURE 11.16 The fl uid applies a downward force P1A to the top face of the submerged cylinder and an
upward force P2 A to the bottom face.
(a)
100 N FB
(b) Floating
FB = 100 N100 N
FIGURE 11.17 (a) An object of weight 100 N is being immersed in a liquid. The deeper the object is, the more liquid it displaces, and the stronger the buoyant force
is. (b) The buoyant force matches the 100-N weight, so the object fl oats.
302 CHAPTER 11 Fluids
In order to decide whether the raft will fl oat in part (a) of Example 9, we compared the
weight of the raft (ρpineVpine)g to the maximum possible buoyant force (ρwaterVwater)g = (ρwaterVpine)g. The comparison depends only on the densities ρpine and ρwater. The take-home message is this: Any object that is solid throughout will fl oat in a liquid if the density of the object is less than or equal to the density of the liquid. For instance, at 0 °C ice has a density of 917 kg/m3, whereas water
has a density of 1000 kg/m3. Therefore, ice fl oats in water.
Although a solid piece of a high-density material like steel will sink in water, such materials
can, nonetheless, be used to make fl oating objects. A supertanker, for example, fl oats because it is
not solid metal. It contains enormous amounts of empty space and, because of its shape, displaces enough water to balance its own large weight. Conceptual Example 10 focuses on an interesting
aspect of a fl oating ship.
EXAMPLE 9 A Swimming Raft
A solid, square pinewood raft measures 4.0 m on a side and is 0.30 m
thick. (a) Determine whether the raft fl oats in water, and (b) if so, how much of the raft is beneath the surface (see the distance h in Figure 11.18).
Reasoning To determine whether the raft fl oats, we will compare the weight of the raft to the maximum possible buoyant force and see whether
there could be enough buoyant force to balance the weight. If so, then
the value of the distance h can be obtained by utilizing the fact that the fl oating raft is in equilibrium, with the magnitude of the buoyant force
equaling the raft’s weight.
Solution (a) The weight of the raft is Wraft = mpineg (Equation 4.5), where mpine is the mass of the raft and can be calculated as mpine = ρpineVpine (Equation 11.1). The pinewood’s density is ρpine = 550 kg/m3 (Table 11.1), and its volume is Vpine = 4.0 m × 4.0 m × 0.30 m = 4.8 m3. Thus, we fi nd the weight of the raft to be
Wraft = m pine g = (ρpineVpine )g
= (550 kg /m3)(4.8 m3)(9.80 m/s2) = 26 000 N
The maximum possible buoyant force occurs when the entire raft is under
the surface, displacing a volume of water that is Vwater = Vpine = 4.8 m3. Ac- cording to Archimedes’ principle, the weight of this volume of water is the
maximum buoyant force FBMAX. It can be obtained using the density of water:
FBMAX = ρwaterVwater g = (1.000 × 103 kg/m3 )(4.8 m3 )(9.80 m /s2 ) = 47 000 N
Since the maximum possible buoyant force exceeds the 26 000-N weight
of the raft, the raft will fl oat only partially submerged at a distance h beneath the water.
(b) We now fi nd the value of h. The buoyant force balances the raft’s weight, so FB = 26 000 N. However, according to Equation 11.6, the mag- nitude of the buoyant force is also the weight of the displaced water, so
FB = 26 000 N = Wwater. Using the density of water, we can also express the weight of the displaced water as Wwater = ρwaterVwaterg, where the water volume is Vwater = 4.0 m × 4.0 m × h. As a result,
26 000 N = Wwater = ρwater (4.0 m × 4.0 m × h)g
h = 26 000 N
ρwater (4.0 m × 4.0 m)g
= 26 000 N
(1.000 × 103 kg/m3)(4.0 m × 4.0 m)(9.80 m/s2) = 0.17 m
4.0 m
Weight of raft FB
4.0 m
h
0.30 m FIGURE 11.18 A raft
fl oating with a distance h beneath the water.
CONCEPTUAL EXAMPLE 10 How Much Water Is Needed to Float a Ship?
to Archimedes’ principle, has a weight that equals the ship’s weight.
Although this wedge-shaped portion of water represents the water
displaced by the ship, it is not the amount that must be present to fl oat the ship, as part c illustrates. This part of the drawing shows a canal, the cross section of which matches the shape in part b. All that is needed, in principle, is a thin section of water that separates the hull of the fl oat- ing ship from the sides of the canal. This thin section of water could have a very small volume indeed.
A ship fl oating in the ocean is a familiar sight. But is all that water really
necessary? Can an ocean vessel fl oat in the amount of water that a swim-
ming pool contains, for instance?
Reasoning and Solution In principle, a ship can fl oat in much less than the amount of water in a swimming pool. To see why, look at Figure 11.19. Part a shows the ship fl oating in the ocean because it contains empty space within its hull and displaces enough water to balance its own
weight. Part b shows the water that the ship displaces, which, according
11.6 Archimedes’ Principle 303
THE PHYSICS OF . . . a state-of-charge battery indicator. Archimedes’ principle is used in some car batteries to alert the owner that recharging is necessary, via a state-of-charge
indicator, such as the one illustrated in Figure 11.20. The battery includes a viewing port that looks down through a plastic rod, which extends into the battery acid. Attached to the end of this
rod is a “cage” containing a green ball. The cage has holes in it that allow the acid to enter. When
the battery is charged, the density of the acid is great enough that its buoyant force makes the ball
rise to the top of the cage, to just beneath the plastic rod. The viewing port shows a green dot.
As the battery discharges, the density of the acid decreases. Since the buoyant force is the weight
of the acid displaced by the ball, the buoyant force also decreases. As a result, the ball sinks into
one of the two chambers oriented at an angle beneath the plastic rod (see Figure 11.20). With the ball no longer visible, the viewing port shows a dark or black dot, warning that the battery
charge is low.
Archimedes’ principle has allowed us to determine how an object can fl oat in a liquid. This
principle also applies to gases, as the next example illustrates.
(b) (c)(a)
FIGURE 11.19 (a) A ship fl oating in the ocean. (b) This is the water that the ship displaces. (c) The ship fl oats here in a canal that has a cross section similar in shape to
that in part b.
Port for viewing state-of-charge indicator
Green dot
Plastic rod
Battery acid
Cage
Black dot
Charged Discharged
FIGURE 11.20 A state-of-charge indicator for a car battery.
Analyzing Multiple-Concept Problems
EXAMPLE 11 The Physics of a Goodyear Airship
Normally, a Goodyear airship, such as the one in Figure 11.21, contains about 5.40 × 103 m3 of helium (He), whose density is 0.179 kg/m3. Find
the weight WL of the load that the airship can carry in equilibrium at an altitude where the density of air is 1.20 kg/m3.
Reasoning The airship and its load are in equilibrium. Thus, the buoy- ant force FB applied to the airship by the surrounding air balances the
weight WHe of the helium and the weight WL of the load, including the solid parts of the airship. The free-body diagram in Figure 11.21b shows these forces. The buoyant force is the weight of the air that the ship dis-
places, according to Archimedes’ principle. The weight of air or helium
is given as W = mg (Equation 4.5). Using the density ρ and volume V, we can express the mass m as m = ρV (Equation 11.1).
304 CHAPTER 11 Fluids
Description Symbol Value Volume of helium in airship VHe 5.40 × 103 m3
Density of helium ρHe 0.179 kg/m3
Density of air ρair 1.20 kg/m3
Unknown Variables Weight of load WL ?
FIGURE 11.21 (a) A helium-fi lled Goodyear airship. (b) The free-body diagram of the airship, including the load weight WL, the weight WHe of the helium, and the buoyant force FB.
FB
WL
WHe
(b) Free-body diagram of the airship(a)
E ri
c G
le n n /A
la m
y
Modeling the Problem
STEP 1 Equilibrium Because the forces in the free-body diagram (see Figure 11.21b) balance at equilibrium, we have
WHe + WL = FB
Rearranging this result gives Equation 1 at the right. Neither the buoyant force FB nor the weight WHe of the helium is known. We will determine them in Steps 2 and 3.
STEP 2 Weight and Density According to Equation 4.5, the weight is given by W = mg. On the other hand, the density ρ is defi ned as the mass m divided by the volume V (see Equation 11.1), so we know that m = ρV. Thus, the weight of the helium in the airship is
WHe = mHe g = ρ HeVHe g
The result can be substituted into Equation 1, as shown at the right. We turn now to Step 3 to
evaluate the buoyant force.
STEP 3 Archimedes’ Principle The buoyant force is given by Archimedes’ principle as the weight of the air displaced by the airship. Thus, following the approach in Step 2, we can write
the buoyant force as follows:
FB = Wair = ρ airVair g
In this result, Vair is very nearly the same as VHe, since the volume occupied by the materials of the ship’s outer structure is negligible compared to VHe. Assuming that Vair = VHe, we see that the expression for the buoyant force becomes
FB = ρairVHe g
Substitution of this value for the buoyant force into Equation 1 is shown at the right.
Knowns and Unknowns The following table summarizes the data:
WL = FB − WHe (1)
? ?
WL = FB − WHe (1)
WHe = ρ HeVHe g ?
WL = FB − WHe (1)
WHe = ρ HeVHe g
FB = ρairVHe g
11.7 Fluids in Motion 305
Check Your Understanding
(The answers are given at the end of the book.) 8. A glass is fi lled to the brim with water and has an ice cube fl oating in it. When the ice cube melts, what
happens? (a) Water spills out of the glass. (b) The water level in the glass drops. (c) The water level in the glass does not change.
9. A steel beam is suspended completely under water by a cable that is attached to one end of the beam, so it hangs vertically. Another identical beam is also suspended completely under water, but by a cable
that is attached to the center of the beam, so it hangs horizontally. Which beam, if either, experiences
the greater buoyant force? Neglect any change in water density with depth.
10. A glass beaker, fi lled to the brim with water, is resting on a scale. A solid block is then placed in the water, causing some of it to spill over. The water that spills is wiped away, and the beaker is still
fi lled to the brim. How do the initial and fi nal readings on the scale compare if the block is made
from (a) wood (whose density is less than that of water) and (b) iron (whose density is greater than that of water)?
11. On a distant planet the acceleration due to gravity is less than it is on earth. Would you fl oat more easily in water on this planet than on earth?
12. As a person dives toward the bottom of a swimming pool, the pressure increases noticeably. Does the buoyant force acting on her also increase? Neglect any change in water density with depth.
13. A pot is partially fi lled with water, in which a plastic cup is fl oating. Inside the fl oating cup is a small block of lead. When the lead block is removed from the cup and placed into the water,
it sinks to the bottom. When this happens, does the water level in the pot (a) rise, (b) fall, or (c) remain the same?
11.7 Fluids in Motion Fluids can move or fl ow in many ways. Water may fl ow smoothly and slowly in a quiet stream
or violently over a waterfall. The air may form a gentle breeze or a raging tornado. To deal with
such diversity, it helps to identify some of the basic types of fl uid fl ow.
Fluid fl ow can be steady or unsteady. In steady fl ow the velocity of the fl uid particles at any point is constant as time passes. For instance, in Figure 11.22 a fl uid particle fl ows with a velocity of v1→ = +2 m/s past point 1. In steady fl ow every particle passing through this point has this same velocity. At another location the velocity may be diff erent, as in a river, which usually
fl ows fastest near its center and slowest near its banks. Thus, at point 2 in the fi gure, the fl uid
velocity is v2→ = +0.5 m/s, and if the fl ow is steady, all particles passing through this point have a velocity of +0.5 m/s. Unsteady fl ow exists whenever the velocity at a point in the fl uid changes as time passes. Turbulent fl ow is an extreme kind of unsteady fl ow and occurs when there are sharp obstacles or bends in the path of a fast-moving fl uid, as in the rapids in Figure 11.23. In turbulent fl ow, the velocity at a point changes erratically from moment to moment, both in mag-
nitude and in direction.
Solution Combining the results of each step algebraically, we fi nd that
WL = FB − WHe = FB − ρ HeVHe g = ρairVHe g − ρ HeVHe g
The weight of the load that the airship can carry at an altitude where ρair = 1.20 kg/m3 is, then,
WL = (ρair − ρHe )VHe g = (1.20 kg/m3 − 0.179 kg/m3)(5.40 × 10 3 m3)(9.80 m/s2)
= 5.40 × 10 4 N
Related Homework: Problems 47, 87
STEP 1 STEP 2 STEP 3
v2 = +0.5 m/s
v1 = +2 m/s Fluid particles
2
1
FIGURE 11.22 Two fl uid particles in a stream. At diff erent locations in the stream
the particle velocities may be diff erent, as
indicated by v1→ and v2→ .
306 CHAPTER 11 Fluids
Fluid fl ow can be compressible or incompressible. Most liquids are nearly incompressible; that is, the density of a liquid remains almost constant as the pressure changes. To a good approx-
imation, then, liquids fl ow in an incompressible manner. In contrast, gases are highly compressible.
However, there are situations in which the density of a fl owing gas remains constant enough that
the fl ow can be considered incompressible.
Fluid fl ow can be viscous or nonviscous. A viscous fl uid, such as honey, does not fl ow readily and is said to have a large viscosity.* In contrast, water is less viscous and fl ows more
readily; water has a smaller viscosity than honey. The fl ow of a viscous fl uid is an energy-
dissipating process. The viscosity hinders neighboring layers of fl uid from sliding freely past one
another. A fl uid with zero viscosity fl ows in an unhindered manner with no dissipation of energy.
Although no real fl uid has zero viscosity at normal temperatures, some fl uids have negligibly
small viscosities. An incompressible, nonviscous fl uid is called an ideal fl uid. When the fl ow is steady, streamlines are often used to represent the trajectories of the
fl uid particles. A streamline is a line drawn in the fl uid such that a tangent to the streamline
at any point is parallel to the fl uid velocity at that point. Figure 11.24 shows the velocity vectors at three points along a streamline. The fl uid velocity can vary (in both magnitude and
direction) from point to point along a streamline, but at any given point, the velocity is con-
stant in time, as required by the condition of steady fl ow. In fact, steady fl ow is often called
streamline fl ow. Figure 11.25a illustrates a method for making streamlines visible by using small tubes to
release a colored dye into the moving liquid. The dye does not immediately mix with the liquid
and is carried along a streamline. In the case of a fl owing gas, such as that in a wind tunnel,
streamlines are often revealed by smoke streamers, as part b of the fi gure shows. In steady fl ow, the pattern of streamlines is steady in time, and, as Figure 11.25a indicates,
no two streamlines cross one another. If they did cross, every particle arriving at the crossing
point could go one way or the other. This would mean that the velocity at the crossing point
would change from moment to moment, a condition that does not exist in steady fl ow.
Check Your Understanding
(The answer is given at the end of the book.) 14. In steady fl ow, the velocity v→ of a fl uid particle at any point is constant in time. On the other hand,
the fl uid in a pipe accelerates when it moves from a larger-diameter section of the pipe into a smaller-
diameter section, so the velocity is increasing during the transition. Does the condition of steady fl ow
rule out such an acceleration?
Streamline
v3
v1
v2
FIGURE 11.24 At any point along a stream- line, the velocity vector of the fl uid particle at
that point is tangent to the streamline.
*See Section 11.11 for a discussion of viscosity.
FIGURE 11.25 (a) In the steady fl ow of a liquid, a colored dye reveals the streamlines. (b) A smoke streamer reveals a streamline pattern for the air fl owing around this skier, as he tests his position for air
resistance in a wind tunnel.
(b)(a)
T h e
C an
ad ia
n P
re ss
, N
at h an
D en
et te
/
© A
P /W
id e
W o rl
d P
h o to
s
FIGURE 11.23 The fl ow of water in white- water rapids is an example of turbulent fl ow.
Frans Lemmens/Getty Images
11.8 The Equation of Continuity 307
11.8 The Equation of Continuity Have you ever used your thumb to control the water fl owing from the end of a hose, as in Figure 11.26? If so, you have seen that the water velocity increases when your thumb reduces the cross- sectional area of the hose opening. This kind of fl uid behavior is described by the equation of continuity. This equation expresses the following simple idea: If a fl uid enters one end of a pipe at a certain rate (e.g., 5 kilograms per second), then fl uid must also leave at the same rate, assum-
ing that there are no places between the entry and exit points to add or remove fl uid. The mass of
fl uid per second (e.g., 5 kg/s) that fl ows through a tube is called the mass fl ow rate. Animated Figure 11.27 shows a small mass of fl uid or fl uid element (dark blue) moving
along a tube. Upstream at position 2, where the tube has a cross-sectional area A2, the fl uid has a speed 𝜐2 and a density ρ2. Downstream at location 1, the corresponding quantities are A1, 𝜐1, and ρ1. During a small time interval Δt, the fl uid at point 2 moves a distance of 𝜐2Δt, as the drawing shows. The volume of fl uid that has fl owed past this point is the cross-sectional
area times this distance, or A2𝜐2Δt. The mass Δm2 of this fl uid element is the product of the density and volume: Δm2 = ρ2 A2𝜐2Δt. Dividing Δm2 by Δt gives the mass fl ow rate (the mass per second):
Mass fl ow rate
at position 2 =
∆m 2 ∆ t
= ρ2 A2υ2 (11.7a)
Similar reasoning leads to the mass fl ow rate at position 1:
Mass fl ow rate
at position 1 =
∆m 1 ∆t
= ρ1 A1υ1 (11.7b)
Since no fl uid can cross the sidewalls of the tube, the mass fl ow rates at positions 1 and 2 must be
equal. However, these positions were selected arbitrarily, so the mass fl ow rate has the same value
everywhere in the tube, an important result known as the equation of continuity. The equation of continuity is an expression of the fact that mass is conserved (i.e., neither created nor destroyed)
as the fl uid fl ows.
EQUATION OF CONTINUITY The mass fl ow rate (ρAυ) has the same value at every position along a tube that has a single entry and a single exit point for fl uid fl ow. For two positions along such a tube
ρ1A1υ1 = ρ2 A2υ2 (11.8)
where ρ = fl uid density (kg/m3) A = cross-sectional area of tube (m2) υ = fl uid speed (m/s)
SI Unit of Mass Flow Rate: kg/s
The density of an incompressible fl uid does not change during fl ow, so that ρ1 = ρ2, and the equation of continuity reduces to
Incompressible fl uid A1υ1 = A2υ2 (11.9)
The quantity A𝜐 represents the volume of fl uid per second (measured in m3/s, for instance) that passes through the tube and is referred to as the volume fl ow rate Q: Q = Volume flow rate = Aυ (11.10)
FIGURE 11.26 When the end of a hose is partially closed off , thus reducing its cross-
sectional area, the fl uid velocity increases.
2 Δt 1 Δt
v2 v1A1
2
1
A2
υ υ
ANIMATED FIGURE 11.27 In general, a fl uid fl owing in a tube that
has diff erent cross-sectional areas A1 and A2 at positions 1 and 2 also has diff erent velocities v1→ and v2→ at these positions.
308 CHAPTER 11 Fluids
Equation 11.9 shows that where the tube’s cross-sectional area is large, the fl uid speed is small,
and, conversely, where the tube’s cross-sectional area is small, the speed is large. Example 12
explores this behavior in more detail for the hose in Figure 11.26.
EXAMPLE 12 A Garden Hose
A garden hose has an unobstructed opening with a cross-sectional area
of 2.85 × 10−4 m2, from which water fi lls a bucket in 30.0 s. The volume
of the bucket is 8.00 × 10−3 m3 (about two gallons). Find the speed of
the water that leaves the hose through (a) the unobstructed opening and (b) an obstructed opening with half as much area.
Reasoning If we can determine the volume fl ow rate Q, we can obtain the speed of the water from Equation 11.10 as 𝜐 = Q/A, since the area A is given. We can fi nd the volume fl ow rate from the volume of the bucket
and its fi ll time.
Solution (a) The volume fl ow rate Q is equal to the volume of the bucket divided by the fi ll time. Therefore, the speed of the water is
υ = Q A
= (8.00 × 10−3 m3) /(30.0 s)
2.85 × 10−4 m2 = 0.936 m/s (11.10)
(b) Water can be considered incompressible, so the equation of continuity can be applied in the form A1𝜐1 = A2𝜐2. When the opening of the hose is unobstructed, its area is A1, and the speed of the water is that determined in part (a)—namely, 𝜐1 = 0.936 m/s. Since A2 =
1
2 A1, we fi nd that
υ2 = ( A1 A 2)υ1 = (
A1 1
2 A1)(0.936 m/s) = 1.87 m/s (11.9)
EXAMPLE 13 BIO The Physics of a Clogged Artery
In the condition known as atherosclerosis, a deposit, or atheroma, forms
on the arterial wall and reduces the opening through which blood can fl ow.
In the carotid artery in the neck, blood fl ows three times faster through
a partially blocked region than it does through an unobstructed region.
Determine the ratio of the eff ective radii of the artery at the two places.
Reasoning Blood, like most liquids, is incompressible, and the equation of continuity in the form of A1𝜐1 = A2𝜐2 (Equation 11.9) can be applied. In applying this equation, we use the fact that the area of a circle is 𝜋r2.
Problem-Solving Insight The equation of continuity in the form A1ʋ1 = A2ʋ2 applies only when the density of the fl uid is constant. If the density is not constant, the equation of continuity is ρ1A1ʋ1 = ρ2A2ʋ2.
Solution From Equation 11.9, it follows that
(πrU2)υU = (πrO2)υO
The ratio of the radii is
rU rO
= √υOυU = √3 = 1.7
⏟⏟⏟ Unobstructed
volume fl ow rate
⏟⏟⏟ obstructed
volume fl ow rate
The next example applies the equation of continuity to the fl ow of blood.
Check Your Understanding
(The answers are given at the end of the book.) 15. Water fl ows from left to right through the fi ve sections (A, B, C, D, E) of the pipe shown in CYU
Figure 11.2. In which section(s) does the water speed increase, decrease, and remain constant? Treat the water as an incompressible fl uid.
Speed Increases Speed Decreases Speed Is Constant (a) A, B D, E C (b) D B A, C, E (c) D, E A, B C (d) B D A, C, E (e) A, B C, D E
11.9 Bernoulli’s Equation 309
EDCBA
CYU FIGURE 11.2
16. See Concept Simulation 11.1 at www.wiley.com/college/cutnell. In case A, water falls downward from a faucet. In case B, water shoots upward, as in a fountain. In each case, as the water moves down-
ward or upward, it has a cross-sectional area that (a) does not change, (b) becomes larger in A and smaller in B, (c) becomes smaller in A and larger in B, (d) becomes larger in both cases, (e) becomes smaller in both cases.
11.9 Bernoulli’s Equation For steady fl ow, the speed, pressure, and elevation of an incompressible and nonviscous fl uid are related by an equation discovered by Daniel Bernoulli (1700–1782). To derive Bernoulli’s equation, we will use the work–energy theorem. This theorem, which is introduced in Chapter 6, states that the net work Wnc done on an object by external nonconservative forces is equal to the change in the total mechanical energy of the object (see Equation 6.8). As mentioned earlier, the
pressure within a fl uid is caused by collisional forces, which are nonconservative. Therefore,
when a fl uid is accelerated because of a diff erence in pressures, work is being done by noncon-
servative forces (Wnc ≠ 0 J), and this work changes the total mechanical energy of the fl uid from an initial value of E0 to a fi nal value of Ef. The total mechanical energy is not conserved. We will now see how the work–energy theorem leads directly to Bernoulli’s equation.
To begin with, let us make two observations about a moving fl uid. First, whenever a fl uid is
fl owing in a horizontal pipe and encounters a region of reduced cross-sectional area, the pressure
of the fl uid drops, as the pressure gauges in Figure 11.28a indicate. The reason for this follows from Newton’s second law. When moving from the wider region 2 to the narrower region 1, the
fl uid speeds up or accelerates, consistent with the conservation of mass (as expressed by the
equation of continuity). According to the second law, the accelerating fl uid must be subjected to
an unbalanced force. However, there can be an unbalanced force only if the pressure in region 2
exceeds the pressure in region 1. We will see that the diff erence in pressures is given by Bernoulli’s
equation. The second observation is that if the fl uid moves to a higher elevation, the pressure at
the lower level is greater than the pressure at the higher level, as in Figure 11.28b. The basis for this observation is our previous study of static fl uids, and Bernoulli’s equation will confi rm it,
provided that the cross-sectional area of the pipe does not change.
To derive Bernoulli’s equation, consider Figure 11.29a. This drawing shows a fl uid element of mass m, upstream in region 2 of a pipe. Both the cross-sectional area and the elevation are diff erent at diff erent places along the pipe. The speed, pressure, and elevation in this region are
𝜐2, P2, and y2, respectively. Downstream in region 1 these variables have the values 𝜐1, P1, and y1. As Chapter 6 discusses, an object moving under the infl uence of gravity has a total mechani- cal energy E that is the sum of the kinetic energy KE and the gravitational potential energy PE: E = KE + PE = 12mυ 2 + mgy. When work Wnc is done on the fl uid element by external
2 1
v2 v1 v
v
Fluid accelerates to the right
in this region
Hi
Hi
Lo Lo
(a) (b)
FIGURE 11.28 (a) In this horizontal pipe, the pressure in region 2 is greater than that in
region 1. The diff erence in pressures leads to
the net force that accelerates the fl uid to the
right. (b) When the fl uid changes elevation, the pressure at the bottom is greater than the
pressure at the top, assuming that the cross-
sectional area of the pipe is constant.
310 CHAPTER 11 Fluids
nonconservative forces, the total mechanical energy changes. According to the work–energy
theorem, the work equals the change in the total mechanical energy:
Wnc = E1 − E2 = ( 12 mυ12 + mgy1) − ( 1
2 mυ22 + mgy2 ) (6.8)
Figure 11.29b helps us understand how the work Wnc arises. On the top surface of the fl uid element, the surrounding fl uid exerts a pressure P. This pressure gives rise to a force of magnitude F = PA, where A is the cross-sectional area. On the bottom surface, the sur- rounding fl uid exerts a slightly greater pressure, P + ΔP, where ΔP is the pressure diff erence between the ends of the element. As a result, the force on the bottom surface has a magnitude of
F + ΔF = (P + ΔP)A. The magnitude of the net force pushing the fl uid element up the pipe is ΔF = (ΔP)A. When the fl uid element moves through its own length s, the work done is the product of the magnitude of the net force and the distance: Work = (ΔF)s = (ΔP)As. The quantity As is the volume V of the element, so the work is (ΔP)V. The total work done on the fl uid element in moving it from region 2 to region 1 is the sum of the small increments of work
(ΔP)V done as the element moves along the pipe. This sum amounts to Wnc = (P2 − P1)V, where P2 − P1 is the pressure diff erence between the two regions. With this expression for Wnc, the work–energy theorem becomes
Wne = (P2 − P1)V = ( 1
2 mυ 21 + mgy1) − ( 1
2 mυ22 + mgy2)
By dividing both sides of this result by the volume V, recognizing that m/V is the density ρ of the fl uid, and rearranging terms, we obtain Bernoulli’s equation.
BERNOULLI’S EQUATION In the steady fl ow of a nonviscous, incompressible fl uid of density ρ, the pressure P, the fl uid speed υ, and the elevation y at any two points (1 and 2) are related by
P1 + 1
2ρυ12 + ρgy1 = P2 + 1
2ρυ22 + ρgy2 (11.11)
Since the points 1 and 2 were selected arbitrarily, the term P + 12 ρυ2 + ρgy has a constant value at all positions in the fl ow. For this reason, Bernoulli’s equation is sometimes expressed as
P + 12 ρυ2 + ρgy = constant. Equation 11.11 can be regarded as an extension of the earlier result that specifi es how the
pressure varies with depth in a static fl uid (P2 = P1 + ρgh), the terms 1
2ρυ12 and 1
2ρυ22 accounting for the eff ects of fl uid speed. Bernoulli’s equation reduces to the result for static fl uids when the
speed of the fl uid is the same everywhere (𝜐1 = 𝜐2), as it is when the cross-sectional area remains constant. Under such conditions, Bernoulli’s equation is P1 + ρgy1= P2 + ρgy2. After rearrange- ment, this result becomes
P2 = P1 + ρg( y1 − y2) = P1 + ρgh
which is the result (Equation 11.4) for static fl uids.
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟ Total mechanical
energy in region 2
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟ Total mechanical
energy in region 1
2
1
v2
P1
P + ΔP
F + ΔF
P
A
–F
P2
y2
sy1
(a) (b)
v1
FIGURE 11.29 (a) A fl uid element (dark blue) moving through a pipe whose cross-
sectional area and elevation change. (b) The fl uid element experiences a force −F→ on its top surface due to the fl uid above it, and a
force F→ + ∆F→ on its bottom surface due to the fl uid below it.
11.10 Applications of Bernoulli’s Equation 311
11.10 Applications of Bernoulli’s Equation When a moving fl uid is contained in a horizontal pipe, all parts of it have the same elevation
(y1 = y2), and Bernoulli’s equation simplifi es to
P1 + 1
2 ρυ12 = P2 + 1
2 ρυ22 (11.12)
Thus, the quantity P + 12 ρυ2 remains constant throughout a horizontal pipe; if 𝜐 increases, P decreases, and vice versa. This is the result that we deduced qualitatively from Newton’s second
law (Section 11.9). Conceptual Example 14 illustrates it.
CONCEPTUAL EXAMPLE 14 Tarpaulins and Bernoulli’s Equation
A tarpaulin is a piece of canvas that is used to cover a cargo, like that
pulled by the truck in Figure 11.30. Whenever the truck stops, the tar- paulin lies fl at. Why does it bulge outward whenever the truck is speeding
down the highway? (a) The air rushing over the outside surface of the canvas creates a higher pressure than does the stationary air inside the
cargo area. (b) The air rushing over the outside surface of the canvas creates a lower pressure than does the stationary air inside the cargo area.
(c) The air inside the cargo area heats up, thus increasing the pressure on the tarp and pushing it outward.
Reasoning When the truck is stationary, the air outside and inside the cargo area is stationary, so the pressure is the same in both places. This
pressure applies the same force to the outer and inner surfaces of the
canvas, with the result that the tarpaulin lies fl at. When the truck is mov-
ing, the outside air rushes over the top surface of the canvas, and the
pressure generated by the moving air is diff erent than the pressure of the
stationary air.
Answer (a) is incorrect. A higher pressure outside and a lower pres- sure in the cargo area would cause the tarpaulin to sink inward, not bulge
outward.
Answer (c) is incorrect. A heating eff ect would not disappear every time the truck stops and reappear only when the truck is moving.
Answer (b) is correct. In accord with Bernoulli’s equation (Equation 11.12), the moving air outside the canvas has a lower pressure than does
the stationary air inside the cargo area. The greater inside pressure gener-
ates a greater force on the inner surface of the canvas, and the tarpaulin
bulges outward.
Related Homework: Problem 62
Stationary
Tarpaulin is flat
Moving
Tarpaulin bulges outward
FIGURE 11.30 The tarpaulin that covers the cargo is fl at when the truck is stationary but
bulges outward when the truck is moving.
THE PHYSICS OF . . . household plumbing. The impact of fl uid fl ow on pressure is widespread. Figure 11.31, for instance, illustrates how household plumbing takes into account the implications of Bernoulli’s equation. The U-shaped section of pipe beneath the sink is called a
To sewer
(b) With vent
ATo sewer
(a) Without vent
A
Sink
B
Clothes washer
Water-filled trap
Roof
Vent (to outside)
B
FIGURE 11.31 In a household plumbing system, a vent is necessary to equalize the pressures at points A and B, thus preventing the trap from being emptied. An empty trap allows sewer gas to enter the house.
312 CHAPTER 11 Fluids
“trap,” because it traps water, which serves as a barrier to prevent sewer gas from leaking into the
house. Part a of the drawing shows poor plumbing. When water from the clothes washer rushes through the sewer pipe, the high-speed fl ow causes the pressure at point A to drop. The pressure at
point B in the sink, however, remains at the higher atmospheric pressure. As a result of this pres-
sure diff erence, the water is pushed out of the trap and into the sewer line, leaving no protection
against sewer gas. A correctly designed system is vented to the outside of the house, as in Figure 11.31b. The vent ensures that the pressure at A remains the same as that at B (atmospheric pres- sure), even when water from the clothes washer is rushing through the pipe. Thus, the purpose of
the vent is to prevent the trap from being emptied, not to provide an escape route for sewer gas.
THE PHYSICS OF . . . airplane wings. One of the most spectacular examples of how fl uid fl ow aff ects pressure is the dynamic lift on airplane wings. Figure 11.32a shows a wing moving to the right, with the air fl owing leftward past the wing. Hence, according to Bernoulli’s
equation, the pressures on the top of and beneath the wing are both lower than atmospheric pres-
sure. However, the pressure above the wing is reduced relative to the pressure under the wing.
This is due to the wing’s shape, which causes the air to travel faster (more reduction in pressure)
over the curved top surface and more slowly (less reduction in pressure) over the fl atter bottom.
Thus, the wing is lifted upward. Part b of the fi gure shows the wing of an airplane. THE PHYSICS OF . . . a curveball. The curveball, one of a baseball pitcher’s main
weapons, is another illustration of the eff ects of fl uid fl ow. Figure 11.33a shows a baseball moving to the right with no spin. The view is from above, looking down toward the ground. Here, air fl ows
with the same speed around both sides of the ball, and the pressure is reduced on both sides by the
same amount relative to atmospheric pressure. No net force exists to make the ball curve to either
side. However, when the ball is given a spin, the air close to its surface is dragged around with it,
and the situation changes. The speed of the air on one-half of the ball is increased, and the pressure
there is even more reduced relative to atmospheric pressure. On the other half of the ball, the speed
of the air is decreased, leading to a lesser reduction in pressure than occurs without spin. Part b of the picture shows the eff ects of a counterclockwise spin. The baseball experiences a net defl ection
force and curves on its way from the pitcher’s mound to the plate, as part c shows.*
(a) (b)(a
Faster air, pressure reduced more
Lift force
Slower air, pressure reduced less
FIGURE 11.32 (a) Air fl owing around an airplane wing. The wing is moving to the
right. (b) The end of this wing has roughly the shape indicated in part a.
Jo e
M cB
ri d e/
G et
ty I
m ag
es
(a) Without spin (b) With spin (c)
Spinning ball
Deflection forceFaster air, pressure reduced more
Slower air, pressure reduced less
FIGURE 11.33 These views of a baseball are from above, looking down toward the ground, with the ball moving to the right. (a) Without spin, the ball does not curve to either side. (b) A spinning ball curves in the direction of the defl ection force. (c) The spin in part b causes the ball to curve as shown here.
*In the jargon used in baseball, the pitch shown in Figure 11.33 parts b and c is called a “slider.”
11.10 Applications of Bernoulli’s Equation 313
As a fi nal application of Bernoulli’s equation, Figure 11.34a shows a large tank from which water is emerging through a small pipe near the bottom. Bernoulli’s equation can be used to
determine the speed (called the effl ux speed) at which the water leaves the pipe, as the next
example shows.
(b)(a)
2
1
h h FIGURE 11.34 (a) Bernoulli’s equation can
be used to determine the speed of the liquid
leaving the small pipe. (b) An ideal fl uid (no viscosity) will rise to the fl uid level in the
tank after leaving a vertical outlet nozzle.
EXAMPLE 15 Eff lux Speed
The tank in Figure 11.34a is open to the atmosphere at the top. Find an expression for the speed of the liquid leaving the pipe at the bottom.
Reasoning We assume that the liquid behaves as an ideal fl uid. There- fore, we can apply Bernoulli’s equation, and in preparation for doing so,
we locate two points in the liquid in Figure 11.34a. Point 1 is just outside the effl ux pipe, and point 2 is at the top surface of the liquid. The pressure
at each of these points is equal to the atmospheric pressure, a fact that will
be used to simplify Bernoulli’s equation.
Solution Since the pressures at points 1 and 2 are the same, we have P1 = P2, and Bernoulli’s equation becomes
1
2 ρυ12 + ρgy1 = 1
2ρυ22 + ρgy2 . The density ρ can be eliminated algebraically from this result, which can then be solved for the square of the effl ux speed 𝜐1:
υ12 = υ22 + 2g( y2 − y1) = υ22 + 2gh
We have substituted h = y2 − y1 for the height of the liquid above the effl ux tube. If the tank is very large, the liquid level changes only slowly, and the
speed at point 2 can be set equal to zero, so that υ1 = √2gh .
Math Skills To obtain the desired expression for υ12, we start with Bernoulli’s equation in the following form:
1
2ρυ 21 + ρgy1 = 1
2ρυ 22 + ρgy2 To solve this equation for υ12, we fi rst isolate the term
1
2ρυ 21 on the left side of the equals sign. To do this, we subtract ρgy1 from both sides of the equals sign:
1
2ρυ 21 + ρgy1 − ρgy1 = 1
2ρυ 22 + ρgy2 − ρgy1 or 1
2ρυ 21 = 1
2ρυ 22 + ρgy2 − ρgy1 Note that the density ρ appears in each term of the result. There- fore, it can be eliminated algebraically:
1
2 ρυ 21 = 1
2 ρυ 22 + ρgy2 − ρgy1 or 1
2 υ 21 = 1
2 υ 22 + gy2 − gy1 We can now simplify the resulting equation by factoring out the
term g that appears on the right side in the terms gy2 and gy1: 1
2 υ 21 = 1
2 υ 22 + g (y2 − y1)
Multiplying both sides of the equals sign by 2 yields
2 1
2 υ 21 = 2
1
2 υ 22 + 2g(y2 − y1) or υ 21 = υ 22 + 2g(y2 − y1)
In Example 15 the liquid is assumed to be an ideal fl uid, and the speed with which it leaves
the pipe is the same as if the liquid had freely fallen through a height h (see Equation 2.9 with x = h and a = g). This result is known as Torricelli’s theorem. If the outlet pipe were pointed directly upward, as in Figure 11.34b, the liquid would rise to a height h equal to the fl uid level above the pipe. However, if the liquid is not an ideal fl uid, its viscosity cannot be neglected. Then,
the effl ux speed would be less than that given by Bernoulli’s equation, and the liquid would rise
to a height less than h.
Check Your Understanding
(The answers are given at the end of the book.) 17. Fluid is fl owing from left to right through a pipe (see CYU Figure 11.3). Points A and B are at the
same elevation, but the cross-sectional areas of the pipe are diff erent. Points B and C are at diff erent
elevations, but the cross-sectional areas are the same. Rank the pressures at the three points, highest to
lowest: (a) A and B (a tie), C (b) C, A and B (a tie) (c) B, C, A (d) C, B, A (e) A, B, C (Continued)
314 CHAPTER 11 Fluids
CYU FIGURE 11.3
B A
C
18. Have you ever had a large truck (traveling in your direction) pass you from behind? You probably no- ticed that your car was pulled toward the truck as it passed. How does the speed of the air (and, hence,
its pressure) between your car and the truck compare to the speed of the air on the opposite side of
your car? The speed of the air between the two vehicles is (a) less and produces a smaller air pressure (b) less and produces a greater air pressure (c) greater and produces a smaller air pressure (d) greater and produces a greater air pressure.
19. Hold two sheets of paper by adjacent corners, so that they hang downward. The sheets should be paral- lel and slightly separated, so that you can see the fl oor through the gap between them. Blow air strongly
down through the gap. What happens to the sheets? (a) Nothing (b) The sheets move further apart. (c) The sheets come closer together.
20. Suppose that you are a right-handed batter in a baseball game, so the ball is moving from your left to your right. You are caught unprepared, looking directly at the ball as it passes by for a strike. If the ball
curves upward on its way to the plate, which way is it spinning? (a) Clockwise (b) Counterclockwise 21. You are sitting on a stationary train next to an open window, and the pressure of the air in your inner ear
is equal to the pressure outside your ear. The train starts up, and as it accelerates to a high speed, your
ears “pop.” Your eardrums respond to a decrease or increase in the air pressure by “popping” outward
or inward, respectively. Assume that the air pressure in your inner ear has not had time to change, so it
remains the same as when the train was stationary. Do your eardrums “pop” (a) outward or (b) inward? 22. Sometimes the weather conditions at an airport give rise to air that has an unusually low density. What
eff ect does such a low-density condition have on a plane’s ability to generate the required lift force for
takeoff ? (a) It has no eff ect. (b) It makes it easier. (c) It makes it harder.
11.11 *Viscous Flow In an ideal fl uid there is no viscosity to hinder the fl uid layers as they slide past one another. Within
a pipe of uniform cross section, every layer of an ideal fl uid moves with the same velocity, even
the layer next to the wall, as Figure 11.35a shows. When viscosity is present, the fl uid layers have diff erent velocities, as part b of the drawing illustrates. The fl uid at the center of the pipe has the greatest velocity. In contrast, the fl uid layer next to the wall surface does not move at all, because it
is held tightly by intermolecular forces. So strong are these forces that if a solid surface moves, the
adjacent fl uid layer moves along with it and remains at rest relative to the moving surface. To help introduce viscosity in a quantitative fashion, Figure 11.36a shows a viscous fl uid
between two parallel plates. The top plate is free to move, while the bottom one is stationary. If the
top plate is to move with a velocity v→ relative to the bottom plate, a force F →
is required. For a highly
viscous fl uid, like honey, a large force is needed; for a less viscous fl uid, like water, a smaller one
will do. As part b of the drawing suggests, we may imagine the fl uid to be composed of many thin horizontal layers. When the top plate moves, the intermediate fl uid layers slide over each other. The
velocity of each layer is diff erent, changing uniformly from v→ at the top plate to zero at the bottom plate. The resulting fl ow is called laminar fl ow, since a thin layer is often referred to as a lamina. As each layer moves, it is subjected to viscous forces from its neighbors. The purpose of the force F
→
is to compensate for the eff ect of these forces, so that any layer can move with a constant velocity.
The amount of force required in Figure 11.36a depends on several factors. Larger areas A, being in contact with more fl uid, require larger forces, so that the force is proportional to the
contact area (F ∝ A). For a given area, greater speeds require larger forces, with the result that the force is proportional to the speed (F ∝ 𝜐). The force is also inversely proportional to the perpendicular distance y between the top and bottom plates (F ∝ 1/y). The larger the distance y, the smaller is the force required to achieve a given speed with a given contact area. These three
proportionalities can be expressed simultaneously in the following way: F ∝ A𝜐/y. Equation 11.13
F
Stationary plate, v = 0 m/s
Viscous fluid
Area = A
(a)
(b)
v
v = 0 m/s
y
FIGURE 11.36 (a) A force F→ is applied to the top plate, which is in contact with a
viscous fl uid. (b) Because of the force F→, the top plate and the adjacent layer of fl uid move
with a constant velocity v→.
FIGURE 11.35 (a) In ideal (nonviscous) fl uid fl ow, all fl uid particles across the pipe
have the same velocity. (b) In viscous fl ow, the speed of the fl uid is zero at the surface of
the pipe and increases to a maximum along
the center axis.
(a)
(b)
v = 0 m/s at wall
v is a maximum at the center
v
11.11 Viscous Flow 315
expresses this relationship with the aid of a proportionality constant η (Greek letter eta), which is called the coeffi cient of viscosity or simply the viscosity.
FORCE NEEDED TO MOVE A LAYER OF VISCOUS FLUID WITH A CONSTANT VELOCITY The magnitude of the tangential force F
→ required to move a fl uid layer at a constant speed υ, when the layer has an area A and is located a perpendicular distance y from an immobile surface, is given by
F = ηAυ
y (11.13)
where η is the coeffi cient of viscosity.
SI Unit of Viscosity: Pa · s
Common or CGS Unit of Viscosity: poise (P)
By solving Equation 11.13 for the viscosity, η = Fy/(𝜐A), it can be seen that the SI unit for viscosity is N · m/[(m/s) · m2] = Pa · s. Another common unit for viscosity is the poise (P), which is used in the CGS system of units and is named after the French physician Jean Poiseuille
(1799–1869; pronounced, approximately, as Pwah-zoyʹ). The following relation exists between
the two units:
1 poise (P) = 0.1 Pa · s Values of viscosity depend on the nature of the fl uid. Under ordinary conditions, the vis-
cosities of liquids are signifi cantly larger than those of gases. Moreover, the viscosities of either liquids or gases depend markedly on temperature. Usually, the viscosities of liquids decrease as
the temperature is increased. Anyone who has heated honey or oil, for example, knows that these
fl uids fl ow much more freely at an elevated temperature. In contrast, the viscosities of gases
increase as the temperature is raised. An ideal fl uid has η = 0 P. Viscous fl ow occurs in a wide variety of situations, such as oil moving through a pipeline
or a liquid being forced through the needle of a hypodermic syringe. Figure 11.37 identifi es the factors that determine the volume fl ow rate Q (in m3/s) of the fl uid. First, a diff erence in pressures P2 − P1 must be maintained between any two locations along the pipe for the fl uid to fl ow. In fact, Q is proportional to P2 − P1, a greater pressure diff erence leading to a larger fl ow rate. Second, a long pipe off ers greater resistance to the fl ow than a short pipe does, and Q is inversely pro- portional to the length L. Third, high-viscosity fl uids fl ow less readily than low-viscosity fl uids, and Q is inversely proportional to the viscosity η. Finally, the volume fl ow rate is larger in a pipe of larger radius, other things being equal. The dependence on the radius R is a surprising one, Q being proportional to the fourth power of the radius, or R4. If, for instance, the pipe radius is reduced to one-half of its original value, the volume fl ow rate is reduced to one-sixteenth of its
original value, assuming the other variables remain constant. The mathematical relation for Q in terms of these parameters was discovered by Poiseuille and is known as Poiseuille’s law.
POISEUILLE’S LAW A fl uid whose viscosity is η, fl owing through a pipe of radius R and length L, has a volume fl ow rate Q given by
Q = πR 4(P2 − P1)
8ηL (11.14)
where P1 and P2 are the pressures at the ends of the pipe.
THE PHYSICS OF . . . pipeline pumping stations. The fact that Q is inversely pro- portional to L in Equation 11.14 has important consequences for long pipelines, such as the Alaskan pipeline (see Figure 11.38). Solving Equation 11.14 for P1 shows that
P1 = P2 − Q8ηL πR 4
Thus, the pressure P1 at the downstream end of a length of pipe is less than the pressure P2 at the upstream end. Long pipelines must have pumping stations at various places along the line to
compensate for the drop in pressure.
Example 16 illustrates the use of Poiseuille’s law.
12
Hi
Flow
Lo
L
R
P2 P1
FIGURE 11.37 For viscous fl ow, the diff er- ence in pressures P2 − P1, the radius R and length L of the tube, and the viscosity η of the fl uid infl uence the volume fl ow rate.
FIGURE 11.38 As oil fl ows along the Alaskan pipeline, the pressure drops because
oil is a viscous fl uid. Pumping stations are
located along the pipeline to compensate for
the drop in pressure.
Sam Chadwick/Shutterstock
316 CHAPTER 11 Fluids
EXAMPLE 16 BIO The Physics of a Hypodermic Syringe
A hypodermic syringe is fi lled with a solution whose viscosity is 1.5 ×
10−3 Pa · s. As Figure 11.39 shows, the plunger area of the syringe is 8.0 × 10−5 m2, and the length of the needle is 0.025 m. The internal radius
of the needle is 4.0 × 10−4 m. The gauge pressure in the vein that is in-
jected is 1900 Pa (14 mm of mercury). What force must be applied to the
plunger, so that 1.0 × 10−6 m3 of solution can be injected in 3.0 s?
Reasoning The necessary force is the pressure applied to the plunger times the area of the plunger. Since viscous fl ow is occurring, the pressure
is diff erent at diff erent points along the syringe. However, the barrel of the
syringe is so wide that little pressure diff erence is required to sustain the
fl ow up to point 2, where the fl uid encounters the narrow needle. Conse-
quently, the pressure applied to the plunger is nearly equal to the pressure
P2 at point 2. To fi nd this pressure, we apply Poiseuille’s law to the needle. Poiseuille’s law indicates that P2 − P1 = 8ηLQ/(𝜋R4). We note that the pressure P1 is given as a gauge pressure, which, in this case, is the amount of pressure in excess of atmospheric pressure. This causes no diffi culty,
because we need to fi nd the amount of force in excess of the force applied
to the plunger by the atmosphere. The volume fl ow rate Q can be obtained from the time needed to inject the known volume of solution.
Solution The volume fl ow rate is Q = (1.0 × 10−6 m3)/(3.0 s) = 3.3 × 10−7 m3/s. According to Poiseuille’s law (Equation 11.14), the required
pressure diff erence is
P2 − P1 = 8ηLQ πR 4 =
8(1.5 × 10−3 Pa ·s)(0.025 m)(3.3 × 10−7 m3/s) π (4.0 × 10−4 m)4 = 1200 Pa
Since P1 = 1900 Pa, the pressure P2 must be P2 = 1200 Pa + 1900 Pa = 3100 Pa. The force that must be applied to the plunger is this pressure
times the plunger area:
F = (3100 Pa)(8.0 × 10−5 m2) = 0.25 N
Area = 8.0 × 10–5 m2
F
2 1 P1P2
0.025 m
FIGURE 11.39 The diff erence in pressure P2 − P1 required to sustain the fl uid fl ow through a hypodermic needle can be found
with the aid of Poiseuille’s law.
EXAMPLE 17 BIO The Physics of an Abdominal Aortic Aneurysm
Example 13 demonstrated how the velocity of blood in an artery changes,
as clogging reduces the eff ective cross-sectional area of the artery. Here
we show that an increase in the cross-sectional area of an artery can be equally as dangerous. Figure 11.40 represents a person who has a poten- tially fatal condition known as an abdominal aortic aneurysm (AAA). The
aorta is the largest blood vessel in the body that carries blood away from
the heart, and factors such as smoking, high blood pressure, and genetic
history can lead to a weakening of the arterial wall that results in the for-
mation of a large bulge (aneurysm) in the artery (Figure 11.40a). If the wall weakens too much, the blood pressure can cause it to rupture, lead-
ing to a signifi cant loss of blood within the circulatory system. Because
the cross-sectional area of the artery increases in the region of the aneu-
rysm, the pressure will be diff erent there. We can model the normal aorta
and the aneurysm as two circular tubes with diff erent diameters (Figure 11.40b). Assume the diameter of a normal aorta in an adult is d1 = 2.0 cm, and the diameter of the aneurysm is d2 = 3.5 cm. The velocity of the blood in the normal part of the aorta is υ1 = 0.40 m/s. Use the equation of continuity and Bernoulli’s equation to calculate the diff erence in pressure
(ΔP = P2 – P1) between the aneurysm and the normal aorta. Assume the blood is an ideal fl uid and the patient is lying down horizontally, so that
the normal portion of the aorta and the aneurysm are at the same height.
Reasoning We can fi rst apply the Equation of Continuity (Equation 11.8) in order to fi nd υ2—the speed of the blood in the region of the aneurysm. Once we know υ2, then we can apply the Bernoulli Equation (Equation 11.11) to fi nd the pressure diff erence ΔP.
Solution We begin with Equation 11.8: ρ1A1υ1 = ρ2A2υ2. Here, the density of the fl uid is constant, and each area is circular, or equal to
π(d/2)2. Therefore, Equation 11.8 reduces to the following: d 12 υ1 = d 22 υ2.
Heart
Aneurysm
Normal aorta
P2
d2
d1
P1
(a)
(b)
1
2υ
υ
FIGURE 11.40 (a) Diagram of the human circulatory system showing the most common location of an AAA. (b) The normal aorta and aneurysm represented as circular tubes with diff erent cross-sectional areas. The
diff erent areas lead to diff erent blood velocities and pressures in each region.
Concept Summary 317
Thus, υ2 = (d1/d2)2υ1. Now we apply the Bernoulli Equation: P1 +
1
2 ρυ12 + ρgy1 = P2 + 1
2 ρυ22 + ρgy2. We now solve this for ΔP = P2 – P1, where we note that y1 = y2: ∆P =
1
2 ρ(υ12 − υ22) . We can substitute in our expression above for υ2 and obtain our fi nal result: ΔP =
1
2 ρυ12 (1 – (d1/d2)4) =
1
2(1060 kg/m 3)(0.40 m/s)2(1 – (2.0 cm/3.5 cm)4) = 76 Pa
Because the velocity of the blood slows down in the aneurysm due to its
larger cross-sectional area, the blood pressure increases. This creates a
dangerous cycle: As the aneurysm continues to grow, the pressure keeps
increasing. If left untreated, the increasing pressure can rupture the arte-
rial wall.
Concept Summary 11.1 Mass Density Fluids are materials that can fl ow, and they include gases and liquids. The mass density ρ of a substance is its mass m divided by its volume V, according to Equation 11.1.
ρ = m V
(11.1)
The specifi c gravity of a substance is its mass density divided by the
density of water at 4 °C (1.000 × 103 kg/m3), according to Equation 11.2.
Specific gravity = Density of substance
1.000 × 103 kg/m3 (11.2)
11.2 Pressure The pressure P exerted by a fl uid is the magnitude F of the force acting perpendicular to a surface embedded in the fl uid divided by the
area A over which the force acts, as shown by Equation 11.3. The SI unit for measuring pressure is the pascal (Pa); 1 Pa = 1 N/m2. One atmosphere of
pressure is 1.013 × 105 Pa or 14.7 lb/in.2
P = F A
(11.3)
11.3 Pressure and Depth in a Static Fluid In the presence of gravity, the upper layers of a fl uid push downward on the layers beneath, with the result
that fl uid pressure is related to depth. In an incompressible static fl uid whose
density is ρ, the relation is given by Equation 11.4, where P1 is the pressure at one level, P2 is the pressure at a level that is h meters deeper, and g is the magnitude of the acceleration due to gravity.
P2 = P1 + ρgh (11.4)
11.4 Pressure Gauges Two basic types of pressure gauges are the mer- cury barometer and the open-tube manometer.
The gauge pressure is the amount by which a pressure P diff ers from at- mospheric pressure. The absolute pressure is the actual value for P.
11.5 Pascal’s Principle Pascal’s principle states that any change in the pressure applied to a completely enclosed fl uid is transmitted undiminished
to all parts of the fl uid and the enclosing walls.
11.6 Archimedes’ Principle The buoyant force is the upward force that a fl uid applies to an object that is partially or completely immersed in it.
Archimedes’ principle states that the magnitude of the buoyant force equals
the weight of the fl uid that the partially or completely immersed object dis-
places, as indicated by Equation 11.6.
FB = Wfl uid (11.6)⏟⏟⏟ Magnitude of
buoyant force
⏟⏟⏟ Weight of
displaced fl uid
11.7 Fluids in Motion/11.8 The Equation of Continuity In steady fl ow, the velocity of the fl uid particles at any point is constant as time passes.
An incompressible, nonviscous fl uid is known as an ideal fl uid. The mass fl ow rate of a fl uid with a density ρ, fl owing with a speed 𝜐 in
a pipe of cross-sectional area A, is the mass per second (kg/s) fl owing past a point and is given by Equation 11.7.
Mass flow rate = ρAυ (11.7)
The equation of continuity expresses the fact that mass is conserved: what fl ows into one end of a pipe fl ows out the other end, assuming there are no additional entry or exit points in between. Expressed in terms of the mass fl ow rate, the equation of continuity is given by Equation 11.8, where the subscripts 1 and 2 denote any two points along the pipe.
ρ1A1υ1 = ρ2 A2υ2 (11.8)
If a fl uid is incompressible, the density at any two points is the same, ρ1 = ρ2. For an incompressible fl uid, the equation of continuity is expressed as in Equation 11.9. The product A𝜐 is known as the volume fl ow rate Q (in m3/s), according to Equation 11.10.
A1υ1 = A2υ2 (11.9)
Q = Volume flow rate = Aυ (11.10)
11.9 Bernoulli’s Equation/11.10 Applications of Bernoulli’s Equation In the steady fl ow of an ideal fl uid whose density is ρ, the pressure P, the fl uid speed 𝜐, and the elevation y at any two points (1 and 2) in the fl uid are related by Bernoulli’s equation (see Equation 11.11). When the fl ow is horizontal
(y1 = y2), Bernoulli’s equation indicates that higher fl uid speeds are associated with lower fl uid pressures.
P1 + 1
2 ρυ1 2 + ρgy1 = P2 + 1
2 ρυ2 2 + ρgy2 (11.11)
11.11 Viscous Flow The magnitude F of the tangential force required to move a fl uid layer at a constant speed 𝜐, when the layer has an area A and is located a perpendicular distance y from an immobile surface, is given by Equation 11.13, where η is the coeffi cient of viscosity.
F = ηAυ
y (11.13)
A fl uid whose viscosity is η, fl owing through a pipe of radius R and length L, has a volume fl ow rate Q given by Poiseuille’s law (see Equation 11.14), where P1 and P2 are the pressures at the downstream and upstream ends of the pipe, respectively.
Q = πR4 (P2 − P1)
8ηL (11.14)
318 CHAPTER 11 Fluids
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 11.3 Pressure and Depth in a Static Fluid 1. The drawing shows three containers fi lled to the same height with the same fl uid. In which container, if any, is the pressure at the bottom greatest?
(a) Container A, because its bottom has the greatest surface area. (b) All three containers have the same pressure at the bottom. (c) Container A, because it has the greatest volume of fl uid. (d) Container B, because it has the least volume of fl uid. (e) Container C, because its bottom has the least surface area.
QUESTION 1 A B C
4. Two liquids, 1 and 2, are in equilibrium in a U-tube that is open at both ends, as in the drawing. The liquids do not mix, and liquid 1 rests on top of liquid 2.
How is the density ρ1 of liquid 1 related to the density ρ2 of liquid 2? (a) ρ1 is equal to ρ2 because the liquids are in equilibrium. (b) ρ1 is greater than ρ2. (c) ρ1 is less than ρ2. (d) There is not enough information to tell which liquid has the greater density.
QUESTION 4
Liquid 1 Liquid 2
Section 11.6 Archimedes’ Principle 9. A beaker is fi lled to the brim with water. A solid object of mass 3.00 kg is lowered into the beaker so that the object
is fully submerged in the water (see the drawing). During
this process, 2.00 kg of water fl ows over the rim and out of
the beaker. What is the buoyant force that acts on the sub-
merged object, and, when released, does the object rise, sink,
or remain in place? (a) 29.4 N; the object rises. (b) 29.4 N; the object sinks. (c) 19.6 N; the object rises. (d)19.6 N; the object sinks. (e) 19.6 N; the object remains in place. 10. Three solid objects are fl oating in a liquid, as in the drawing. They have diff erent weights and volumes, but have the same thickness (the dimension
perpendicular to the page). Rank the objects according to their density,
largest fi rst. (a) A, B, C (b) A, C, B (c) B, A, C (d) B, C, A (e) C, A, B
QUESTION 10
A B
C
Section 11.8 The Equation of Continuity 12. A hollow pipe is submerged in a stream of water so that the length of the pipe is parallel to the velocity of the water. If the water speed doubles and
the cross-sectional area of the pipe triples, what happens to the volume fl ow
rate of the water passing through the pipe? (a) The volume fl ow rate does not change. (b) The volume fl ow rate increases by a factor of 2. (c) The volume fl ow rate increases by a factor of 3. (d) The volume fl ow rate increases by a factor of 4. (e) The volume fl ow rate increases by a factor of 6. 13. In the drawing, water fl ows from a wide section of a pipe to a narrow section. In which part of the pipe is the volume fl ow rate the greatest? (a) The wide section (b) The narrow section (c) The volume fl ow rate is the same in both sections of the pipe.
QUESTION 13
Section 11.9 Bernoulli’s Equation 16. Blood fl ows through a section of a horizontal artery that is partially blocked by a deposit along the artery wall. A hemoglobin molecule moves
from the narrow region into the wider region. What happens to the pres-
sure acting on the molecule? (a) The pressure increases. (b) The pressure decreases. (c) There is no change in the pressure.
QUESTION 16 Hemoglobin molecule
Deposit
18. Water is fl owing down through the pipe shown in the drawing. Point A is at a higher elevation than B and C are. The cross-sectional areas are the same
at A and B but are wider at C. Rank the pressures at the three points, largest
fi rst. (a) PA, PB, PC (b) PC, PB, PA (c) PB, PC, PA
QUESTION 18 B
A
C
Section 11.11 Viscous Flow 20. A viscous fl uid is fl owing through two horizontal pipes. The pressure diff erence P2 − P1 between the ends of each pipe is the same. The pipes have the same radius, although one is twice as long as the other. How does
the volume fl ow rate QB in the longer pipe compare with the rate QA in the shorter pipe? (a) QB is the same as QA. (b) QB is twice as large as QA. (c) QB is four times as large as QA. (d) QB is one-half as large as QA. (e) QB is one- fourth as large as QA.
L
QA
P2 P2P1 P1
QB
2L
QUESTION 20
Focus on Concepts
Object
QUESTION 9
Problems 319
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 11.1 Mass Density 1. E SSM One of the concrete pillars that support a house is 2.2 m tall and has a radius of 0.50 m. The density of concrete is about 2.2 × 103 kg/m3. Find
the weight of this pillar in pounds (1 N = 0.2248 lb).
2. E A cylindrical storage tank has a radius of 1.22 m. When fi lled to a height of 3.71 m, it holds 14 300 kg of a liquid industrial solvent. What is the
density of the solvent?
3. E SSM Accomplished silver workers in India can pound silver into in- credibly thin sheets, as thin as 3.00 × 10−7 m (about one-hundredth of the
thickness a sheet of paper). Find the area of such a sheet that can be formed
from 1.00 kg of silver.
4. E Neutron stars consist only of neutrons and have unbelievably high densities. A typical mass and radius for a neutron star might be 2.7 × 1028 kg
and 1.2 × 103 m. (a) Find the density of such a star. (b) If a dime (V = 2.0 × 10−7 m3) were made from this material, how much would it weigh (in
pounds)?
5. E One end of a wire is attached to a ceiling, and a solid brass ball is tied to the lower end. The tension in the wire is 120 N. What is the radius of the
brass ball?
6. M GO Planners of an experiment are evaluating the design of a sphere of radius R that is to be fi lled with helium (0 °C, 1 atm pressure). Ultrathin silver foil of thickness T will be used to make the sphere, and the designers claim that the mass of helium in the sphere will equal the mass of silver
used. Assuming that T is much less than R, calculate the ratio T/R for such a sphere.
7. M SSM A bar of gold measures 0.15 m × 0.050 m × 0.050 m. How many gallons of water have the same mass as this bar?
8. M A full can of black cherry soda has a mass of 0.416 kg. It contains 3.54 × 10−4 m3 of liquid. Assuming that the soda has the same density as
water, fi nd the volume of aluminum used to make the can.
9. M V-HINT A hypothetical spherical planet consists entirely of iron. What is the period of a satellite that orbits this planet just above its surface? Consult
Table 11.1 as necessary. 10. H An antifreeze solution is made by mixing ethylene glycol (ρ = 1116 kg/m3) with water. Suppose that the specifi c gravity of such a solution is
1.0730. Assuming that the total volume of the solution is the sum of its parts,
determine the volume percentage of ethylene glycol in the solution.
Section 11.2 Pressure 11. E SSM An airtight box has a removable lid of area 1.3 × 10−2 m2 and negligible weight. The box is taken up a mountain where the air pressure
outside the box is 0.85 × 105 Pa. The inside of the box is completely evacu-
ated. What is the magnitude of the force required to pull the lid off the box?
12. E A person who weighs 625 N is riding a 98-N mountain bike. Suppose that the entire weight of the rider and bike is supported equally by the two
tires. If the pressure in each tire is 7.60 × 105 Pa, what is the area of contact
between each tire and the ground?
13. E MMH A solid concrete block weighs 169 N and is resting on the ground. Its dimensions are 0.400 m × 0.200 m × 0.100 m. A number of
identical blocks are stacked on top of this one. What is the smallest number
of whole blocks (including the one on the ground) that can be stacked so that
their weight creates a pressure of at least two atmospheres on the ground
beneath the fi rst block?
14. E United States currency is printed using intaglio presses that gen- erate a printing pressure of 8.0 × 104 lb/in.2 A $20 bill is 6.1 in. by 2.6 in.
Calculate the magnitude of the force that the printing press applies to one
side of the bill.
15. E SSM A glass bottle of soda is sealed with a screw cap. The absolute pressure of the carbon dioxide inside the bottle is 1.80 × 105 Pa. Assuming
that the top and bottom surfaces of the cap each have an area of 4.10 × 10−4 m2,
obtain the magnitude of the force that the screw thread exerts on the cap
in order to keep it on the bottle. The air pressure outside the bottle is one
atmosphere.
16. M GO A 58-kg skier is going down a slope oriented 35° above the hori- zontal. The area of each ski in contact with the snow is 0.13 m2. Determine
the pressure that each ski exerts on the snow.
17. M GO A suitcase (mass m = 16 kg) is resting on the fl oor of an elevator. The part of the suitcase in contact with the fl oor measures 0.50 m × 0.15 m.
The elevator is moving upward with an acceleration of magnitude 1.5 m/s2.
What pressure (in excess of atmospheric pressure) is applied to the fl oor be-
neath the suitcase?
18. M CHALK A cylinder is fi tted with a piston, beneath which is a spring, as in the drawing. The cylinder is open
to the air at the top. Friction is absent. The spring constant
of the spring is 3600 N/m. The piston has a negligible mass
and a radius of 0.024 m. (a) When the air beneath the piston is completely pumped out, how much does the atmospheric
pressure cause the spring to compress? (b) How much work does the atmospheric pressure do in compressing the spring?
19. M BIO V-HINT As the initially empty urinary bladder fi lls with urine and expands, its internal pressure increases
by 3300 Pa, which triggers the micturition refl ex (the feeling of the need
to urinate). The drawing shows a horizontal, square section of the bladder
wall with an edge length of 0.010 m. Because the bladder is stretched, four
tension forces of equal magnitude T act on the square section, one at each edge, and each force is directed at an angle θ below the horizontal. What is the magnitude T of the tension force acting on one edge of the section when the internal bladder pressure is 3300 Pa and each of the four tension forces
is directed 5.0° below the horizontal?
PROBLEM 19 θ
θ
θ
θ
T
T
T
T
Problems
PROBLEM 18
320 CHAPTER 11 Fluids
Section 11.3 Pressure and Depth in a Static Fluid,
Section 11.4 Pressure Gauges 20. E The Mariana trench is located in the fl oor of the Pacifi c Ocean at a depth of about 11 000 m below the surface of the water. The density of
seawater is 1025 kg/m3. (a) If an underwater vehicle were to explore such a depth, what force would the water exert on the vehicle’s observation window
(radius = 0.10 m)? (b) For comparison, determine the weight of a jetliner whose mass is 1.2 × 105 kg.
21. E Review Conceptual Example 6 as an aid in understanding this problem. Consider the pump on the right side of Figure 11.10, which acts to reduce the air pressure in the pipe. The air pressure outside the pipe is one atmosphere.
Find the maximum depth from which this pump can extract water from the well.
22. E GO A meat baster consists of a squeeze bulb attached to a plastic tube. When the bulb is squeezed and released, with the open end of the tube
under the surface of the basting sauce, the sauce rises in the tube to a distance
h, as the drawing shows. Using 1.013 × 105 Pa for the atmospheric pressure and 1200 kg/m3 for the density of the sauce, fi nd the absolute pressure in the
bulb when the distance h is (a) 0.15 m and (b) 0.10 m.
PROBLEM 22
h
23. E SSM The main water line enters a house on the fi rst fl oor. The line has a gauge pressure of 1.90 × 105 Pa. (a) A faucet on the second fl oor, 6.50 m above the fi rst fl oor, is turned off . What is the gauge pressure at this faucet?
(b) How high could a faucet be before no water would fl ow from it, even if the faucet were open?
24. E BIO The drawing shows an intravenous feeding. With the distance shown, nutrient solution (ρ = 1030 kg/m3) can just barely enter the blood in the vein. What is the gauge pressure of the venous blood? Express your
answer in millimeters of mercury.
PROBLEM 24
Atmospheric pressure
0.610 m
25. E BIO The human lungs can function satisfactorily up to a limit where the pressure diff erence between the outside and inside of the lungs is
one-twentieth of an atmosphere. If a diver uses a snorkel for breathing, how
far below the water can she swim? Assume the diver is in salt water whose
density is 1025 kg/m3.
26. E BIO At a given instant, the blood pressure in the heart is 1.6 × 104 Pa. If an artery in the brain is 0.45 m above the heart, what is the pressure in the
artery? Ignore any pressure changes due to blood fl ow.
27. E SSM A water tower is a familiar sight in many towns. The purpose of such a tower is to provide storage capacity and to provide suffi cient pressure
in the pipes that deliver the water to customers. The drawing shows a spher-
ical reservoir that contains 5.25 × 105 kg of water when full. The reservoir is
vented to the atmosphere at the top. For a full reservoir, fi nd the gauge pres-
sure that the water has at the faucet in (a) house A and (b) house B. Ignore the diameter of the delivery pipes.
15.0 m
Faucet
A
B
Vent
7.30 mFaucet
PROBLEM 27
28. M GO A mercury barometer reads 747.0 mm on the roof of a building and 760.0 mm on the ground. Assuming a constant value of 1.29 kg/m3 for
the density of air, determine the height of the building.
29. M SSM A 1.00-m-tall container is fi lled to the brim, partway with mercury and the rest of the way with water. The container is open to the atmosphere.
What must be the depth of the mercury so that the absolute pressure on the
bottom of the container is twice the atmospheric pressure?
30. M CHALK Two identical containers are open at the top and are connected at the bottom via a tube of negligible volume and a valve that is closed. Both
containers are fi lled initially to the same height of 1.00 m, one with water, the
other with mercury, as the drawing indicates. The valve is then opened. Water
and mercury are immiscible. Determine the fl uid level in the left container
when equilibrium is reestablished.
PROBLEM 30 Water Mercury
Valve 1.00 m
31. M V-HINT The vertical surface of a reservoir dam that is in contact with the water is 120 m wide and 12 m high. The air pressure is one atmosphere.
Find the magnitude of the total force acting on this surface in a completely
fi lled reservoir. (Hint: The pressure varies linearly with depth, so you must use an average pressure.) 32. H A house has a roof with the dimensions shown in the drawing. De- termine the magnitude and direction of the net force that the atmosphere
applies to the roof when the outside pressure drops suddenly by 75.0 mm of
mercury before the air pressure in the attic can adjust. Express your answer
in (a) newtons and (b) pounds.
PROBLEM 32
30.0°
14.5 m 4.21 m
30.0°
Problems 321
Section 11.5 Pascal’s Principle 33. E SSM The atmospheric pressure above a swimming pool changes from 755 to 765 mm of mercury. The bottom of the pool is a rectangle
(12 m × 24 m). By how much does the force on the bottom of the pool
increase?
34. E A barber’s chair with a person in it weighs 2100 N. The output plunger of a hydraulic system begins to lift the chair when the barber’s foot
applies a force of 55 N to the input piston. Neglect any height diff erence
between the plunger and the piston. What is the ratio of the radius of the
plunger to the radius of the piston?
35. E MMH Multiple-Concept Example 8 presents an approach to problems of this kind. The hydraulic oil in a car lift has a density of 8.30 × 102 kg/m3.
The weight of the input piston is negligible. The radii of the input piston and
output plunger are 7.70 × 10−3 m and 0.125 m, respectively. What input force
F is needed to support the 24 500-N combined weight of a car and the output plunger, when (a) the bottom surfaces of the piston and plunger are at the same level, and (b) the bottom surface of the output plunger is 1.30 m above that of the input piston?
36. E GO In the process of changing a fl at tire, a motorist uses a hydraulic jack. She begins by applying a force of 45 N to the input piston, which has
a radius r1. As a result, the output plunger, which has a radius r2, applies a force to the car. The ratio r2/r1 has a value of 8.3. Ignore the height diff erence between the input piston and output plunger and determine the force that the
output plunger applies to the car.
37. M V-HINT A dump truck uses a hydraulic cylinder, as the drawing illustrates. When activated by the operator, a pump injects hydraulic oil into
the cylinder at an absolute pressure of 3.54 × 106 Pa and drives the output
plunger, which has a radius of 0.150 m. Assuming that the plunger remains
perpendicular to the fl oor of the load bed, fi nd the torque that the plunger
creates about the axis identifi ed in the drawing.
PROBLEM 37
Output plunger
Axis
3.50 m
Load bed Input for
hydraulic oil
38. M GO The drawing shows a hydraulic chamber with a spring (spring constant = 1600 N/m) attached to the input piston and a rock of mass 40.0 kg
resting on the output plunger. The piston and plunger are nearly at the same
height, and each has a negligible mass. By how much is the spring compressed
from its unstrained position?
PROBLEM 38 Area = 15 cm2 Area = 65 cm2
39. M SSM The drawing shows a hydraulic system used with disc brakes. The force F→ is applied perpendicularly to the brake pedal. The pedal rotates about the axis shown in the drawing and causes a force to be applied perpen-
dicularly to the input piston (radius = 9.50 × 10−3 m) in the master cylinder.
The resulting pressure is transmitted by the brake fl uid to the output plungers
(radii = 1.90 × 10−2 m), which are covered with the brake linings. The lin-
ings are pressed against both sides of a disc attached to the rotating wheel.
Suppose that the magnitude of F→ is 9.00 N. Assume that the input piston and
the output plungers are at the same vertical level, and fi nd the force applied
to each side of the rotating disc.
PROBLEM 39
0.0500 m 0.100 m
Plunger Lining
Brake fluid
Master cylinder
Brake pedal
Axis
Edge view of rotating disc attached to wheel
F
Section 11.6 Archimedes’ Principle 40. E The density of ice is 917 kg/m3, and the density of seawater is 1025 kg/m3. A swimming polar bear climbs onto a piece of fl oating ice that has
a volume of 5.2 m3. What is the weight of the heaviest bear that the ice can
support without sinking completely beneath the water?
41. E SSM A 0.10-m × 0.20-m × 0.30-m block is suspended from a wire and is completely under water. What buoyant force acts on the block?
42. E GO A hydrometer is a device used to mea- sure the density of a liquid. It is a cylindrical tube
weighted at one end, so that it fl oats with the heavier
end downward. The tube is contained inside a large
“medicine dropper,” into which the liquid is drawn
using the squeeze bulb (see the drawing). For use
with your car, marks are put on the tube so that the
level at which it fl oats indicates whether the liquid is
battery acid (more dense) or antifreeze (less dense).
The hydrometer has a weight of W = 5.88 × 10−2 N and a cross-sectional area of A = 7.85 × 10−5 m2. How far from the bottom of the tube should the mark
be put that denotes (a) battery acid (ρ = 1280 kg/m3) and (b) antifreeze (ρ = 1073 kg/m3)? 43. E A duck is fl oating on a lake with 25% of its volume beneath the water. What is the average density of the duck?
44. E A paperweight, when weighed in air, has a weight of W = 6.9 N. When completely immersed in water, however, it has a weight of Win water = 4.3 N. Find the volume of the paperweight.
45. E SSM An 81-kg person puts on a life jacket, jumps into the water, and fl oats. The jacket has a volume of 3.1 × 10−2 m3 and is completely submerged
under the water. The volume of the person’s body that is under water is 6.2 ×
10−2 m3. What is the density of the life jacket?
46. E V-HINT A lost shipping container is found resting on the ocean fl oor and completely submerged. The container is 6.1 m long, 2.4 m wide, and 2.6 m
high. Salvage experts attach a spherical balloon to the top of the container
and infl ate it with air pumped down from the surface. When the balloon’s
radius is 1.5 m, the shipping container just begins to rise toward the surface.
What is the mass of the container? Ignore the mass of the balloon and the air
within it. Do not neglect the buoyant force exerted on the shipping container by the water. The density of seawater is 1025 kg/m3.
47. M CHALK SSM Refer to Multiple-Concept Example 11 to see a problem similar to this one. What is the smallest number of whole logs (ρ = 725 kg/ m3, radius = 0.0800 m, length = 3.00 m) that can be used to build a raft that
will carry four people, each of whom has a mass of 80.0 kg?
48. M GO A hot-air balloon is accelerating upward under the infl uence of two forces, its weight and the buoyant force. For simplicity, consider the
weight to be only that of the hot air within the balloon, thus ignoring the
Hydrometer
Marks for two types of
liquids.
PROBLEM 42
322 CHAPTER 11 Fluids
balloon fabric and the basket. The hot air inside the balloon has a density of
ρhot air = 0.93 kg/m3, and the density of the cool air outside is ρcool air = 1.29 kg/ m3. What is the acceleration of the rising balloon?
49. M A hollow cubical box is 0.30 m on an edge. This box is fl oating in a lake with one-third of its height beneath the surface. The walls of the box
have a negligible thickness. Water from a hose is poured into the open top of
the box. What is the depth of the water in the box just at the instant that water
from the lake begins to pour into the box from the lake?
50. M GO To verify her suspicion that a rock specimen is hollow, a geo- logist weighs the specimen in air and in water. She fi nds that the specimen
weighs twice as much in air as it does in water. The density of the solid part
of the specimen is 5.0 × 103 kg/m3. What fraction of the specimen’s apparent
volume is solid?
51. H SSM A solid cylinder (radius = 0.150 m, height = 0.120 m) has a mass of 7.00 kg. This cylinder is fl oat-
ing in water. Then oil (ρ = 725 kg/m3) is poured on top of the water until the situation shown in the drawing
results. How much of the height of the cylinder is in
the oil?
52. H MMH Available in WileyPLUS. 53. H One kilogram of glass (ρ = 2.60 × 103 kg/m3) is shaped into a hollow spherical shell that just barely
fl oats in water. What are the inner and outer radii of the
shell? Do not assume that the shell is thin.
Section 11.8 The Equation of Continuity 54. E A fuel pump sends gasoline from a car’s fuel tank to the engine at a rate of 5.88 × 10−2 kg/s. The density of the gasoline is 735 kg/m3, and the
radius of the fuel line is 3.18 × 10−3 m. What is the speed at which the gasoline
moves through the fuel line?
55. E BIO SSM A patient recovering from surgery is being given fl uid in- travenously. The fl uid has a density of 1030 kg/m3, and 9.5 × 10−4 m3 of it
fl ows into the patient every six hours. Find the mass fl ow rate in kg/s.
56. E BIO MMH (a) The volume fl ow rate in an artery supplying the brain is 3.6 × 10−6 m3/s. If the radius of the artery is 5.2 mm, determine the average
blood speed. (b) Find the average blood speed at a constriction in the artery if the constriction reduces the radius by a factor of 3. Assume that the volume
fl ow rate is the same as that in part (a).
57. E A room has a volume of 120 m3. An air-conditioning system is to replace the air in this room every twenty minutes, using ducts that have a
square cross section. Assuming that air can be treated as an incompressible
fl uid, fi nd the length of a side of the square if the air speed within the ducts
is (a) 3.0 m/s and (b) 5.0 m/s. 58. E GO Water fl ows straight down from an open faucet. The cross- sectional area of the faucet is 1.8 × 10−4 m2, and the speed of the water is
0.85 m/s as it leaves the faucet. Ignoring air resistance, fi nd the cross-
sectional area of the water stream at a point 0.10 m below the faucet.
59. M BIO V-HINT The aorta carries blood away from the heart at a speed of about 40 cm/s and has a radius of approximately 1.1 cm. The aorta branches
eventually into a large number of tiny capillaries that distribute the blood
to the various body organs. In a capillary, the blood speed is approximately
0.07 cm/s, and the radius is about 6 × 10−4 cm. Treat the blood as an incom-
pressible fl uid, and use these data to determine the approximate number of
capillaries in the human body.
60. M GO MMH Three fi re hoses are connected to a fi re hydrant. Each hose has a radius of 0.020 m. Water enters the hydrant through an underground
pipe of radius 0.080 m. In this pipe the water has a speed of 3.0 m/s. (a) How many kilograms of water are poured onto a fi re in one hour by all three hoses?
(b) Find the water speed in each hose.
Section 11.9 Bernoulli’s Equation,
Section 11.10 Applications of Bernoulli’s Equation 61. E SSM Prairie dogs are burrowing rodents. They do not suff ocate in their burrows, because the eff ect of air speed on pressure creates suffi cient air
circulation. The animals maintain a diff erence in the shapes of two entrances
to the burrow, and because of this diff erence, the air (ρ = 1.29 kg/m3) blows past the openings at diff erent speeds, as the drawing indicates. Assuming that
the openings are at the same vertical level, fi nd the diff erence in air pressure
between the openings and indicate which way the air circulates.
PROBLEM 61
A = 8.5 m/s B = 1.1 m/sυ υ
62. E Review Conceptual Example 14 before attempting this problem. The truck in that example is traveling at 27 m/s. The density of air is 1.29 kg/m3.
By how much does the pressure inside the cargo area beneath the tarpaulin
exceed the outside pressure?
63. E SSM An airplane wing is designed so that the speed of the air across the top of the wing is 251 m/s when the speed of the air below the wing is
225 m/s. The density of the air is 1.29 kg/m3. What is the lifting force on a
wing of area 24.0 m2?
64. E GO Water fl owing out of a horizontal pipe emerges through a nozzle. The radius of the pipe is 1.9 cm, and the radius of the nozzle is 0.48 cm. The
speed of the water in the pipe is 0.62 m/s. Treat the water as an ideal fl uid,
and determine the absolute pressure of the water in the pipe.
65. E BIO The blood speed in a normal segment of a horizontal artery is 0.11 m/s. An abnormal segment of the artery is narrowed down by an arteri-
osclerotic plaque to one-fourth the normal cross-sectional area. What is the
diff erence in blood pressures between the normal and constricted segments
of the artery?
66. E MMH A small crack occurs at the base of a 15.0-m-high dam. The eff ective crack area through which water leaves is 1.30 × 10−3 m2.
(a) Ignoring viscous losses, what is the speed of water fl owing through the crack? (b) How many cubic meters of water per second leave the dam? 67. E Water is circulating through a closed system of pipes in a two-fl oor apartment. On the fi rst fl oor, the water has a gauge pressure of 3.4 × 105 Pa and
a speed of 2.1 m/s. However, on the second fl oor, which is 4.0 m higher, the
speed of the water is 3.7 m/s. The speeds are diff erent because the pipe diameters
are diff erent. What is the gauge pressure of the water on the second fl oor?
68. E GO A ship is fl oating on a lake. Its hold is the interior space beneath its deck; the hold is empty and is open to the atmosphere. The hull has a hole
in it, which is below the water line, so water leaks into the hold. The eff ective
area of the hole is 8.0 × 10−3 m2 and is located 2.0 m beneath the surface of
the lake. What volume of water per second leaks into the ship?
69. M SSM A Venturi meter is a device that is used for measuring the speed of a fl uid within a pipe. The drawing shows a gas fl owing at speed 𝜐2 through a horizontal section of pipe whose cross-sectional area is A2 = 0.0700 m2. The gas has a density of ρ = 1.30 kg/m3. The Venturi meter has a cross-sectional area of A1 = 0.0500 m2 and has been substituted for a section of the larger pipe. The pressure diff erence between the two sections is P2 − P1 = 120 Pa. Find (a) the speed 𝜐2 of the gas in the larger, original pipe and (b) the volume fl ow rate Q of the gas.
Oil
Water
PROBLEM 51
Additional Problems 323
Venturi meter
A1
A2 v2
Lo P1
Hi P2
A2 v2 v1
PROBLEM 69
70. M V-HINT A hand-pumped water gun is held level at a height of 0.75 m above the ground and fi red. The water stream from the gun hits the ground a
horizontal distance of 7.3 m from the muzzle. Find the gauge pressure of the
water gun’s reservoir at the instant when the gun is fi red. Assume that the speed
of the water in the reservoir is zero and that the water fl ow is steady. Ignore both
air resistance and the height diff erence between the reservoir and the muzzle.
71. M A liquid is fl owing through a horizontal pipe whose radius is 0.0200 m. The pipe bends straight upward through a height of 10.0 m and joins another
horizontal pipe whose radius is 0.0400 m. What volume fl ow rate will keep
the pressures in the two horizontal pipes the same?
72. M V-HINT An airplane has an eff ective wing surface area of 16 m2 that is generating the lift force. In level fl ight the air speed over the top of the wings
is 62.0 m/s, while the air speed beneath the wings is 54.0 m/s. What is the
weight of the plane?
73. M MMH The construction of a fl at rectangular roof (5.0 m × 6.3 m) allows it to withstand a maximum net outward force that is 22 000 N. The density
of the air is 1.29 kg/m3. At what wind speed will this roof blow outward?
74. M GO A pump and its horizontal intake pipe are located 12 m beneath the surface of a large reservoir. The speed of the water in the intake pipe
causes the pressure there to decrease, in accord with Bernoulli’s principle.
Assuming nonviscous fl ow, what is the maximum speed with which water
can fl ow through the intake pipe?
75. H SSM A uniform rectangular plate is hanging vertically downward from a hinge that passes along its left edge. By blowing air at 11.0 m/s over the top of the plate only, it is possible to keep the plate in a horizontal po- sition, as illustrated in part a of the drawing. To what value should the air speed be reduced so that the plate is kept at a 30.0° angle with respect to the
vertical, as in part b of the drawing? (Hint: Apply Bernoulli’s equation in the form of Equation 11.12.)
PROBLEM 75 (a) (b)
Moving air
Hinge Edge view of plate
30.0°
76. H Available in WileyPLUS.
Section 11.11 Viscous Flow 77. E BIO SSM Available in WileyPLUS. 78. E A pipe is horizontal and carries oil that has a viscosity of 0.14 Pa · s. The volume fl ow rate of the oil is 5.3 × 10−5 m3/s. The length of the pipe is
37 m, and its radius is 0.60 cm. At the output end of the pipe the pressure is
atmospheric pressure. What is the absolute pressure at the input end?
79. E BIO In the human body, blood vessels can dilate, or increase their radii, in response to various stimuli, so that the volume fl ow rate of the
blood increases. Assume that the pressure at either end of a blood vessel, the
length of the vessel, and the viscosity of the blood remain the same, and de-
termine the factor Rdilated/Rnormal by which the radius of a vessel must change in order to double the volume fl ow rate of the blood through the vessel.
80. E BIO GO A blood transfusion is being set up in an emergency room for an accident victim. Blood has a density of 1060 kg/m3 and a viscosity of
4.0 × 10−3 Pa · s. The needle being used has a length of 3.0 cm and an inner radius of 0.25 mm. The doctor wishes to use a volume fl ow rate through the
needle of 4.5 × 10−8 m3/s. What is the distance h above the victim’s arm where the level of the blood in the transfusion bottle should be located? As
an approximation, assume that the level of the blood in the transfusion bottle
and the point where the needle enters the vein in the arm have the same pres-
sure of one atmosphere. (In reality, the pressure in the vein is slightly above
atmospheric pressure.)
81. E SSM MMH Available in WileyPLUS. 82. E Available in WileyPLUS. 83. M GO Two hoses are connected to the same outlet using a Y-connector, as the drawing shows. The hoses A and B have the same length, but hose B has
the larger radius. Each is open to the atmosphere at the end where the water
exits. Water fl ows through both hoses as a viscous fl uid, and Poiseuille’s
law [Q = 𝜋R4(P2 − P1)/(8ηL)] applies to each. In this law, P2 is the pressure upstream, P1 is the pressure downstream, and Q is the volume fl ow rate. The ratio of the radius of hose B to the radius of hose A is RB/RA = 1.50. Find the ratio of the speed of the water in hose B to the speed in hose A.
PROBLEM 83 Hose A Hose B
Water from outlet
84. M Available in WileyPLUS.
85. E SSM Measured along the surface of the water, a rectangular swim- ming pool has a length of 15 m. Along this length, the fl at bottom of the pool
slopes downward at an angle of 11° below the horizontal, from one end to the
other. By how much does the pressure at the bottom of the deep end exceed
the pressure at the bottom of the shallow end?
86. E BIO One way to administer an inoculation is with a “gun” that shoots the vaccine through a narrow opening. No needle is necessary, for the vac-
cine emerges with suffi cient speed to pass directly into the tissue beneath the
skin. The speed is high, because the vaccine (ρ = 1100 kg/m3) is held in a reservoir where a high pressure pushes it out. The pressure on the surface of
Additional Problems
324 CHAPTER 11 Fluids
the vaccine in one gun is 4.1 × 106 Pa above the atmospheric pressure out-
side the narrow opening. The dosage is small enough that the vaccine’s sur-
face in the reservoir is nearly stationary during an inoculation. The vertical
height between the vaccine’s surface in the reservoir and the opening can be
ignored. Find the speed at which the vaccine emerges.
87. E SSM Available in WileyPLUS. 88. E BIO If a scuba diver descends too quickly into the sea, the internal pressure on each eardrum remains at atmospheric pressure, while the external
pressure increases due to the increased water depth. At suffi cient depths,
the diff erence between the external and internal pressures can rupture an
eardrum. Eardrums can rupture when the pressure diff erence is as little as
35 kPa. What is the depth at which this pressure diff erence could occur? The
density of seawater is 1025 kg/m3.
89. E A water bed for sale has dimensions of 1.83 m × 2.13 m × 0.229 m. The fl oor of the bedroom will tolerate an additional weight of no more than
6660 N. Find the weight of the water in the bed and determine whether the
bed should be purchased.
90. E GO An underground pump initially forces water through a horizontal pipe at a fl ow rate of 740 gallons per minute. After several years of operation,
corrosion and mineral deposits have reduced the inner radius of the pipe to
0.19 m from 0.24 m, but the pressure diff erence between the ends of the pipe
is the same as it was initially. Find the fi nal fl ow rate in the pipe in gallons per
minute. Treat water as a viscous fl uid.
91. E Available in WileyPLUS. 92. E V-HINT Available in WileyPLUS. 93. E Available in WileyPLUS. 94. E (a) The mass and the radius of the sun are, respectively, 1.99 × 1030 kg and 6.96 × 108 m. What is its density? (b) If a solid object is made from a material that has the same density as the sun, would it sink or fl oat
in water? Why? (c) Would a solid object sink or fl oat in water if it were made from a material whose density was the same as that of the planet
Saturn (mass = 5.7 × 1026 kg, radius = 6.0 × 107 m)? Provide a reason for
your answer.
95. M SSM A water line with an internal radius of 6.5 × 10−3 m is connec- ted to a shower head that has 12 holes. The speed of the water in the line is
1.2 m/s. (a) What is the volume fl ow rate in the line? (b) At what speed does the water leave one of the holes (eff ective hole radius = 4.6 × 10−4 m) in the
head?
96. M V-HINT A log splitter uses a pump with hydraulic oil to push a piston, which is attached to a chisel. The pump can generate a pressure of 2.0 × 107 Pa
in the hydraulic oil, and the piston has a radius of 0.050 m. In a stroke lasting
25 s, the piston moves 0.60 m. What is the power needed to operate the log
splitter’s pump?
97. M An object is solid throughout. When the object is completely sub- merged in ethyl alcohol, its apparent weight is 15.2 N. When completely
submerged in water, its apparent weight is 13.7 N. What is the volume of
the object?
98. M V-HINT Available in WileyPLUS.
99. M SSM Available in WileyPLUS.
100. M GO A gold prospector fi nds a solid rock that is composed solely of quartz and gold. The mass and volume of the rock are, respectively, 12.0 kg
and 4.00 × 10−3 m3. Find the mass of the gold in the rock.
101. M V-HINT Available in WileyPLUS.
102. H Available in WileyPLUS.
103. H Available in WileyPLUS.
104. H Available in WileyPLUS.
105. M GO SSM An aneurysm is an abnormal enlargement of a blood vessel such as the aorta. Because of the aneurysm, the normal cross-sectional area
A1 of the aorta increases to a value of A2 = 1.7A1. The speed of the blood (ρ = 1060 kg/m3) through a normal portion of the aorta is 𝜐1 = 0.40 m/s. As- suming that the aorta is horizontal (the person is lying down), determine the
amount by which the pressure P2 in the enlarged region exceeds the pressure P1 in the normal region.
Pressure plays an important role in the behavior of fl uids. As we have seen in
this chapter, pressure is the magnitude of the force acting perpendicular to a
surface divided by the area of the surface. Pressure should not be confused,
however, with the force itself. Problem 106 serves to emphasize that pres-
sure and force are diff erent concepts. Problem 107 focuses on the essence of
Archimedes’ principle and its application to the situation of a buoyant force
acting on a submerged object.
106. M CHALK The fi gure shows a rear view of a loaded two-wheeled wheelbarrow on a horizontal surface. It has balloon tires and a weight W = 684 N, which is uniformly distributed. The left tire has a contact area with
the ground of AL = 6.6 × 10−4 m2, whereas the right tire is underinfl ated and has a contact area of AR = 9.9 × 10−4 m2. Concepts: (i) Force is a vector. Therefore both a direction and a magnitude are needed to specify it. Are
both a direction and magnitude needed to specify a pressure? (ii) How is
the force each tire applies to the ground related to the force the ground ap-
plies to each tire? (iii) Do the left and right tires apply the same force to the
ground? Explain. (iv) Do the left and right tires apply the same pressure to
the ground? Calculations: Find the force and pressure that each tire applies to the ground.
PROBLEM 106
(a) Rear view of a wheelbarrow with balloon tires. (b) Free-body diagram of the wheel- barrow, showing its weight W
→ and the
forces FL →
and FR →
that the ground applies,
respectively, to the left and right tires.
ℓ ℓ
+y
(a) (b) Free-body diagram for the wheelbarrow
FL FR
W
Concepts and Calculations Problems
Team Problems 325
107. M CHALK SSM A father (weight W = 830 N) and his daughter (weight W = 340 N) are spending the day at the lake. They are each sitting on a beach ball that is just submerged beneath the water (see the fi gure).
Concepts: (i) Each ball is in equilibrium, being stationary and having no acceleration. Thus, the net force acting on each ball is zero. What balances
the downward-acting weight in each case? (ii) In which case is the buoyant
force greater? (iii) In this situation, what determines the magnitude of the
buoyant force? (iv) Which beach ball has the larger radius? Calculations: Ignoring the weight of the air in each ball, and the volumes of their legs that
are under the water, fi nd the radius of each ball.
PROBLEM 107
108. M Crossing a River. You and your team come to a slow fl owing river that you need to cross. The nearest bridge is 20 miles to the north, too dan-
gerous and too far to trek with your group. You explore the area down river
and discover an abandoned shed with a stash of 55-gallon drums (all empty
and weighing 35.0 lb each) and a stack of 10-foot planks: You will build a
raft. The six members of your team have a combined weight of 925 pounds
(assuming everyone was truthful). You also have a four-wheeler (all-terrain
vehicle), which weighs 450 lb, and other gear, which adds another 315 lb.
Your simple raft design is as follows: a platform of planks with barrels
strapped to the bottom. You estimate that the planks weigh about 45.0 lb
each, and you will need 20 of them to make a platform that can accom-
modate everything for the one-way trip. You measure the dimensions of the
cylindrical drums and fi nd they have diameter D = 22.5 inches and height h = 33.5 inches (note: not exactly “55 gallons”). (a) What is the minimum number of barrels that you will need so that the raft will fl oat when fully
loaded? (b) What is the minimum number of barrels you will need if you want the platform to be at least 6 inches above the water when fully loaded?
109. M A Spring Gun. A hydraulic press is used to compress a spring that will then be used to project a 25.0-kg steel ball. The system is similar, but
smaller in scale, to the car jack illustrated in Figure 11.14. In this case, the smaller cylinder has a diameter of d1 = 0.75 cm and has a manually operated plunger. The larger cylinder has a diameter of d2 = 10.0 cm, and its piston compresses the spring. The idea is that the gun operator pulls a lever that
pushes the plunger on the small cylinder, which transmits a pressure to the
larger piston that, in turn, exerts a force on the spring and compresses it. Once
the spring is compressed, the steel ball is loaded and the spring is released,
ejecting the ball. (a) If a force of 950 N is exerted on the primary (smaller) piston to compress the spring 1.25 m from its equilibrium (uncompressed)
position, what is the spring constant k of the spring? (b) What is the velocity of the steel ball just after it is ejected? (c) Neglecting air resistance, what is the maximum range of this “spring gun”?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
12.1 Convert temperature scales.
12.2 Define the Kelvin scale and absolute zero.
12.3 Identify types of thermometers.
12.4 Analyze linear thermal expansion.
12.5 Analyze volume thermal expansion.
12.6 Define heat and internal energy.
12.7 Solve specific heat problems.
12.8 Solve heat problems with phase changes.
12.9 Analyze phase equilibrium.
12.10 Solve humidity problems. N
A S
A /S
ci en
ce S
o u rc
e
CHAPTER 12
Temperature and Heat
As this artist’s rendition shows, the underside of the Space Shuttle consists of special ceramic tiles that
shield the Shuttle’s interior and fl ight crew from the high temperatures and heat produced upon reentering
the Earth’s atmosphere after a mission in space. In 2003 the Space Shuttle Columbia’s seven-member crew was killed when the shuttle disintegrated on reentry after suff ering damage to the heat shield during launch.
12.1 Common Temperature Scales To measure temperature we use a thermometer. Many thermometers make use of the fact
that materials usually expand with increasing temperature. For example, Figure 12.1 shows the common mercury-in-glass thermometer, which consists of a mercury-fi lled
glass bulb connected to a capillary tube. When the mercury is heated, it expands into
the capillary tube, the amount of expansion being proportional to the change in tem-
perature. The outside of the glass is marked with an appropriate scale for reading the
temperature.
A number of diff erent temperature scales have been devised, two popular choices
being the Celsius (formerly, centigrade) and Fahrenheit scales. Figure 12.1 illus- trates these scales. Historically,* both scales were defi ned by assigning two temper-
ature points on the scale and then dividing the distance between them into a number
of equally spaced intervals. One point was chosen to be the temperature at which ice
326
*Today, the Celsius and Fahrenheit scales are defi ned in terms of the Kelvin temperature scale; Section 12.2
discusses the Kelvin scale.
12.1 Common Temperature Scales 327
melts under one atmosphere of pressure (the “ice point”),
and the other was the temperature at which water boils
under one atmosphere of pressure (the “steam point”). On
the Celsius scale, an ice point of 0 °C (0 degrees Celsius)
and a steam point of 100 °C were selected. On the Fahren-
heit scale, an ice point of 32 °F (32 degrees Fahrenheit)
and a steam point of 212 °F were chosen. The Celsius
scale is used worldwide, while the Fahrenheit scale is
used mostly in the United States, often in home medical
thermometers.
There is a subtle diff erence in the way the temper-
ature of an object is reported, as compared to a change in its temperature. For example, the temperature of the
human body is about 37 °C, where the symbol °C stands
for “degrees Celsius.” However, the change between two temperatures is specifi ed in “Celsius degrees” (C°)—not
in “degrees Celsius.” Thus, if the body temperature rises
to 39 °C, the change in temperature is 2 Celsius degrees
or 2 C°, not 2 °C.
As Figure 12.1 indicates, the separation between the ice and steam points on the Celsius scale is divided into
100 Celsius degrees, while on the Fahrenheit scale the
separation is divided into 180 Fahrenheit degrees. There-
fore, the size of the Celsius degree is larger than that of
the Fahrenheit degree by a factor of 180
100 , or 9
5. Examples 1
and 2 illustrate how to convert between the Celsius and
Fahrenheit scales using this factor.
Ice and water Bulb
0 °C
100 °C
32 °F
212 °F
Boiling water
Fahrenheit scale
Celsius scale
1 0
0 C
el si
us d
eg re
es
1 8
0 F
ah re
nh ei
t de
gr ee
s
Steam point
Ice point
FIGURE 12.1 The Celsius and Fahrenheit temperature scales.
EXAMPLE 1 Converting from a Fahrenheit to a Celsius Temperature
A healthy person has an oral temperature of 98.6 °F. What would this
reading be on the Celsius scale?
Reasoning and Solution A temperature of 98.6 °F is 66.6 Fahrenheit degrees above the ice point of 32.0 °F. Since 1 C° =
9
5 F°, the diff erence
of 66.6 F° is equivalent to
(66.6 F°) (1 C°9 5 F° ) = 37.0 C°
Thus, the person’s temperature is 37.0 Celsius degrees above the ice
point. Adding 37.0 Celsius degrees to the ice point of 0 °C on the Celsius
scale gives a Celsius temperature of 37.0 °C .
EXAMPLE 2 Converting from a Celsius to a Fahrenheit Temperature
A time and temperature sign on a bank indicates that the outdoor temper-
ature is −20.0 °C. Find the corresponding temperature on the Fahrenheit
scale.
Reasoning and Solution The temperature of −20.0 °C is 20.0 Celsius degrees below the ice point of 0 °C. This number of Celsius degrees corresponds to
(20.0 C°) ( 9
5 F°
1 C°) = 36.0 F°
The temperature, then, is 36.0 Fahrenheit degrees below the ice point.
Subtracting 36.0 Fahrenheit degrees from the ice point of 32.0 °F on the
Fahrenheit scale gives a Fahrenheit temperature of −4.0 °F .
The reasoning strategy used in Examples 1 and 2 for converting between diff erent temperature
scales is summarized below.
328 CHAPTER 12 Temperature and Heat
REASONING STRATEGY Converting Between Diff erent Temperature Scales 1. Determine the magnitude of the diff erence between the stated temperature and the ice
point on the initial scale. 2. Convert this number of degrees from one scale to the other scale by using the appro-
priate conversion factor. For conversion between the Celsius and Fahrenheit scales, the factor is based on the fact that 1 C° = 95 F°
3. Add or subtract the number of degrees on the new scale to or from the ice point on the new scale.
Check Your Understanding
(The answer is given at the end of the book.) 1. On a new temperature scale the steam point is 348 °X, and the ice point is 112 °X. What is the temperature
on this scale that corresponds to 28.0 °C?
12.2 The Kelvin Temperature Scale Although the Celsius and Fahrenheit scales are widely used, the Kelvin temperature scale has greater scientifi c signifi cance. It was introduced by the Scottish physicist William Thompson
(Lord Kelvin, 1824–1907), and in his honor each degree on the scale is called a kelvin (K).
By international agreement, the symbol K is not written with a degree sign (°), nor is the word
“degrees” used when quoting temperatures. For example, a temperature of 300 K (not 300 °K)
is read as “three hundred kelvins,” not “three hundred degrees kelvin.” The kelvin is the SI base
unit for temperature.
Figure 12.2 compares the Kelvin and Celsius scales. The size of one kelvin is identical to the size of one Celsius degree because there are one hundred divisions between the ice and steam
points on both scales. As we will discuss shortly, experiments have shown that there exists a
lowest possible temperature, below which no substance can be cooled. This lowest temperature is
defi ned to be the zero point on the Kelvin scale and is referred to as absolute zero. The ice point (0 °C) occurs at 273.15 K on the Kelvin scale. Thus, the Kelvin temperature T
and the Celsius temperature Tc are related by
T = Tc + 273.15 (12.1)
The number 273.15 in Equation 12.1 is an experimental result, obtained in studies that utilize a
gas-based thermometer.
When a gas confi ned to a fi xed volume is heated, its pressure increases. Conversely, when the
gas is cooled, its pressure decreases. For example, the air pressure in automobile tires can rise by
as much as 20% after the car has been driven and the tires have become warm. The change in gas
pressure with temperature is the basis for the constant-volume gas thermometer. A constant-volume gas thermometer consists of a gas-fi lled bulb to which a pressure gauge
is attached, as in Figure 12.3. The gas is often hydrogen or helium at a low density, and the pressure gauge can be a U-tube manometer fi lled with mercury. The bulb is placed in thermal
contact with the substance whose temperature is being measured. The volume of the gas is held
constant by raising or lowering the right column of the U-tube manometer in order to keep the mercury level in the left column at the same reference level. The absolute pressure of the gas is proportional to the height h of the mercury on the right. As the temperature changes, the pressure changes and can be used to indicate the temperature, once the constant-volume gas thermometer
has been calibrated.
Suppose that the absolute pressure of the gas in Figure 12.3 is measured at diff erent tem- peratures. If the results are plotted on a pressure-versus-temperature graph, a straight line is
obtained, as in Figure 12.4. If the straight line is extended or extrapolated to lower and lower temperatures, the line crosses the temperature axis at −273.15 °C. In reality, no gas can be
cooled to this temperature, because all gases liquify before reaching it. However, helium and
Kelvin, K Celsius, °C
Steam point
Ice point
Absolute zero
One kelvin equals one
Celsius degree
0 – 273.15
0.00273.15
100.00373.15
FIGURE 12.2 A comparison of the Kelvin and Celsius temperature scales.
Gas-filled bulb
Evacuated space
Reference level
U-tube manometerSubstance whose
temperature is being measured
h
M er
cu ry
FIGURE 12.3 A constant-volume gas thermometer.
12.3 Thermometers 329
hydrogen liquify at such low temperatures that they are often used in the thermometer. This
kind of graph can be obtained for diff erent amounts and types of low-density gases. In all cases,
a straight line is found that extrapolates to −273.15 °C on the temperature axis, which suggests
that the value of −273.15 °C has fundamental signifi cance. The signifi cance of this number
is that it is the absolute zero point for temperature measurement. The phrase “absolute zero” means that temperatures lower than −273.15 °C cannot be reached by continually cooling a
gas or any other substance. If lower temperatures could be reached, then further extrapolation
of the straight line in Figure 12.4 would suggest that negative absolute gas pressures could exist. Such a situation would be impossible, because a negative absolute gas pressure has no
meaning. Thus, the Kelvin scale is chosen so that its zero temperature point is the lowest tem-
perature attainable.
12.3 Thermometers All thermometers make use of the change in some physical property with temperature. A prop-
erty that changes with temperature is called a thermometric property. For example, the ther- mometric property of the mercury thermometer is the length of the mercury column, while in the
constant-volume gas thermometer it is the pressure of the gas. Several other important thermo-
meters and their thermometric properties will now be discussed.
The thermocouple is a thermometer used extensively in scientifi c laboratories. It consists of thin wires of diff erent metals, welded together at the ends to form two junctions, as Figure 12.5 illustrates. Often the metals are copper and constantan (a copper–nickel alloy). One of the junc-
tions, called the “hot” junction, is placed in thermal contact with the object whose temperature is
being measured. The other junction, termed the “reference” junction, is kept at a known constant
temperature (usually an ice–water mixture at 0 °C). The thermocouple generates a voltage that
depends on the diff erence in temperature between the two junctions. This voltage is the thermo- metric property and is measured by a voltmeter, as the drawing indicates. With the aid of calibra-
tion tables, the temperature of the hot junction can be obtained from the voltage. Thermocouples
are used to measure temperatures as high as 2300 °C or as low as −270 °C.
Most substances off er resistance to the fl ow of electricity, and this resistance changes with
temperature. As a result, electrical resistance provides another thermometric property. Electrical resistance thermometers are often made from platinum wire, because platinum has excellent mechanical and electrical properties in the temperature range from −270 °C to +700 °C. The
resistance of platinum wire is known as a function of temperature. Thus, the temperature of a
substance can be determined by placing the resistance thermometer in thermal contact with the
substance and measuring the resistance of the wire.
Object
Hot junction
Reference junction
Constantan
Ice-point bath, 0 °C
(a)
Copper
Copper
Voltmeter
FIGURE 12.5 (a) A thermocouple is made from two diff erent types of wires, copper and constantan in this case. (b) A thermocouple junction between two diff erent wires.
(b)
Thermocouple junction
1 mm
C o u rt
es y o
f D
av id
Y o u n g a
n d S
h an
e S
ta d le
r
Temperature, °C
Absolute pressure
Hypothetical negative-pressure
region
–200 –100 +100 +200 0
–273.15 °C
FIGURE 12.4 A plot of absolute pressure versus temperature for a low-density gas at constant volume. The graph is a straight line and, when extrapolated (dashed line), crosses the temperature axis at −273.15 °C.
330 CHAPTER 12 Temperature and Heat
BIO THE PHYSICS OF . . . thermography. Radiation emitted by an object can also be used to indicate temperature. At low to moderate temperatures, the predominant radiation
emitted is infrared. As the temperature is raised, the intensity of the radiation increases substan-
tially. In one interesting application, an infrared camera registers the intensity of the infrared
radiation produced at diff erent locations on the human body. The camera is connected to a color
monitor that displays the diff erent infrared intensities as diff erent colors. This “thermal painting”
is called a thermograph or thermogram. Thermography is an important diagnostic tool in medi- cine. For example, breast cancer is indicated in the thermogram in Figure 12.6 by the elevated temperatures associated with malignant tissue. In another application, Figure 12.7 shows ther- mographic images of a smoker’s forearms before (left) and 5 minutes after (right) he has smoked
a cigarette. After smoking, the forearms are cooler due to the eff ect of nicotine, which causes
vasoconstriction (narrowing of the blood vessels) and reduces blood fl ow, a result that can lead to
a higher risk from blood clotting. Temperatures in these images range from over 34 °C to about
28 °C and are indicated in decreasing order by the colors white, red, yellow, green, and blue.
Oceanographers and meteorologists also use thermograms extensively, to map the temper-
ature distribution on the surface of the earth. For example, Figure 12.8 shows a satellite image of the sea-surface temperature of the Pacifi c Ocean. The region depicted in red is the 1997/98
El Niño, a large area of the ocean, approximately twice the width of the United States, where
temperatures reached abnormally high values. This El Niño caused major weather changes in
certain regions of the earth.
12.4 Linear Thermal Expansion
Normal Solids Have you ever found the metal lid on a glass jar too tight to open? One solution is to run hot water
over the lid, which loosens it because the metal expands more than the glass does. To varying
extents, most materials expand when heated and contract when cooled. The increase in any one
dimension of a solid is called linear expansion, linear in the sense that the expansion occurs along a line. Figure 12.9 illustrates the linear expansion of a rod whose length is L0 when the temperature is T0. When the temperature of the rod increases to T0 + ΔT, the length becomes L0 + ΔL, where ΔT and ΔL are the changes in temperature and length, respectively. Conversely, when the temperature decreases to T0 − ΔT, the length decreases to L0 − ΔL.
For modest temperature changes, experiments show that the change in length is directly
proportional to the change in temperature (ΔL ∝ ΔT). In addition, the change in length is propor- tional to the initial length of the rod, a fact that can be understood with the aid of Figure 12.10. Part a of the drawing shows two identical rods. Each rod has a length L0 and expands by ΔL when
FIGURE 12.6 The presence of breast cancer can be detected in a thermogram via the
elevated temperatures associated with the
malignant tissue. The healthy breast on the
right side of the thermogram registers pre-
dominantly blue (see the temperature coding
bar to the right of the image), indicating
temperatures that are not unusually elevated.
The breast on the left side of the thermogram,
however, registers the colors yellow,
orange, and red, which indicate the elevated
temperatures due to breast cancer.
S P
L /S
ci en
ce S
o u rc
e
FIGURE 12.7 Thermogram showing a smoker’s forearms before (left) and 5 minutes after (right) he has smoked a cigarette. Tem- peratures decrease from white (over 34 ºC) to
yellow, to red, to green, to blue (about 28 ºC).
D r.
A rt
h u r
T u ck
er /
S ci
en ce
P h o to
L ib
ra ry
/
S ci
en ce
S o u rc
e
FIGURE 12.8 A thermogram of the 1997/98 El Niño (red), a large region
of abnormally high temperatures in the
Pacifi c Ocean.
C o u rt
es y N
O A
A
Temperature = T0
Temperature = T0 + ΔT
L0 ΔL
FIGURE 12.9 When the temperature of a rod is raised by ΔT, the length of the rod increases by ΔL.
is equivalent to
2L0
2 ΔL
ΔL
ΔL
ΔL
L0
L0
L0
(a)
(b)
FIGURE 12.10 (a) Each of two identical rods expands by ΔL when heated. (b) When the rods are combined into a single rod of
length 2L0, the “combined” rod expands by 2 ΔL.
12.4 Linear Thermal Expansion 331
the temperature increases by ΔT. Part b shows the two heated rods combined into a single rod, for which the total expansion is the sum of the expansions of each part—namely, ΔL + ΔL = 2ΔL. Clearly, the amount of expansion doubles if the rod is twice as long to begin with. In other words,
the change in length is directly proportional to the original length (ΔL ∝ L0). Equation 12.2 expresses the fact that ΔL is proportional to both L0 and ΔT (ΔL ∝ L0ΔT) by using a proportion- ality constant 𝛼, which is called the coeffi cient of linear expansion.
LINEAR THERMAL EXPANSION OF A SOLID The length L0 of an object changes by an amount ΔL when its temperature changes by an amount ΔT:
∆L = αL0∆T (12.2)
where α is the coeffi cient of linear expansion.
Common Unit for the Coeffi cient of Linear Expansion: 1C° = (C°) −1
Solving Equation 12.2 for 𝛼 shows that 𝛼 = ΔL/(L0ΔT). Since the length units of ΔL and L0 algebraically cancel, the coeffi cient of linear expansion 𝛼 has the unit of (C°)−1 when the temperature diff erence ΔT is expressed in Celsius degrees (C°). Diff erent materials with the same initial length expand and contract by diff erent amounts as the temperature changes, so
the value of 𝛼 depends on the nature of the material. Table 12.1 shows some typical values.
TABLE 12.1 Coefficients of Thermal Expansion for Solids and Liquidsa
Coefficient of Thermal Expansion (C°)−1
Substance Linear (𝞪) Volume (𝞫) Solids Liquids Aluminum 23 × 10−6 69 × 10−6
Brass 19 × 10−6 57 × 10−6
Concrete 12 × 10−6 36 × 10−6
Copper 17 × 10−6 51 × 10−6
Glass (common) 8.5 × 10−6 26 × 10−6
Glass (Pyrex) 3.3 × 10−6 9.9 × 10−6
Gold 14 × 10−6 42 × 10−6
Iron or steel 12 × 10−6 36 × 10−6
Lead 29 × 10−6 87 × 10−6
Nickel 13 × 10−6 39 × 10−6
Quartz (fused) 0.50 × 10−6 1.5 × 10−6
Silver 19 × 10−6 57 × 10−6
Liquidsb
Benzene — 1240 × 10−6
Carbon tetrachloride — 1240 × 10−6
Ethyl alcohol — 1120 × 10−6
Gasoline — 950 × 10−6
Mercury — 182 × 10−6
Methyl alcohol — 1200 × 10−6
Water — 207 × 10−6
aThe values for 𝛼 and 𝛽 pertain to a temperature near 20°C. bSince liquids do not have fixed shapes, the coefficient of linear expansion is not defined for them.
332 CHAPTER 12 Temperature and Heat
Coeffi cients of linear expansion also vary somewhat depending on the range of temperatures
involved, but the values in Table 12.1 are adequate approximations. Example 3 deals with a situation in which a dramatic eff ect due to thermal expansion can be observed, even though the
change in temperature is small.
The buckling of a sidewalk is one consequence of not providing suffi cient room for thermal
expansion. To eliminate such problems, engineers incorporate expansion joints or spaces at in-
tervals along bridge roadbeds, as Figure 12.12 shows. BIO THE PHYSICS OF . . . an antiscalding device. Although Example 3 shows
how thermal expansion can cause problems, there are also times when it can be useful. For
instance, each year thousands of children are taken to emergency rooms suff ering from burns
caused by scalding tap water. Such accidents can be reduced with the aid of the antiscalding
device shown in Figure 12.13. This device screws onto the end of a faucet and quickly shuts off the fl ow of water when it becomes too hot. As the water temperature rises, the actuator spring
expands and pushes the plunger forward, shutting off the fl ow. When the water cools, the spring
contracts and the water fl ow resumes.
EXAMPLE 3 Buckling of a Sidewalk
A concrete sidewalk is constructed between two buildings on a day when
the temperature is 25 °C. The sidewalk consists of two slabs, each three
meters in length and of negligible thickness (Figure 12.11a). As the tem- perature rises to 38 °C, the slabs expand, but no space is provided for
thermal expansion. The buildings do not move, so the slabs buckle upward.
Determine the vertical distance y in part b of the drawing.
Reasoning The expanded length of each slab is equal to its original length plus the change in length ΔL due to the rise in temperature. We know the original length, and Equation 12.2 can be used to fi nd the change
in length. Once the expanded length has been determined, the Pythagorean
theorem can be employed to fi nd the vertical distance y in Figure 12.11b.
Solution The change in temperature is ∆T = 38 °C − 25 °C = 13 C°, and the coeffi cient of linear expansion for concrete is given in Table 12.1. The change in length of each slab associated with this temperature change is
∆L = αL0 ∆T = [12 × 10−6 (C°)−1](3.0 m)(13 C°) = 0.000 47 m (12.2)
The expanded length of each slab is, thus, 3.000 47 m. We can now de-
termine the vertical distance y by applying the Pythagorean theorem to the right triangle in Figure 12.11b:
y = √(3.000 47 m) 2 − (3.000 00 m) 2 = 0.053 m
Math Skills The calculation of the answer for y involves two num- bers, each of which has six signifi cant fi gures. Yet the answer has
only two signifi cant fi gures. This reduction in signifi cant fi gures
occurs because the calculation includes a subtraction step. Be on the lookout for subtractions, because they may reduce the number of signifi cant fi gures in your answers. For instance, in the present case we have y = √(3.000 47 m)2 − (3.000 00 m)2, which has the form of y = √a2 − b2 = √(a + b) (a − b) . Therefore, we can write the expression for y in the following way:
y = √(3.000 47 m)2 − (3.000 00 m)2
= √(3.000 47 m + 3.000 00 m)(3.000 47 m − 3.000 00 m)
In this result, the subtraction reduces the number of signifi cant
fi gures from six to two:
3.000 47 m − 3.000 00 m = 0.000 47 m
As a result, our expression for y becomes
y = √(6.000 47 m)(0.000 47 m) = 0.053 m
which limits the answer to two signifi cant fi gures.
(a)
Concrete
3.000 00 m 3.000 00 m
3.00 0 47
m
3.000 00 m
90° y
(b)
FIGURE 12.11 (a) Two concrete slabs completely fi ll the space between the buildings. (b) When the temperature increases, each slab expands, causing the sidewalk to buckle.
12.4 Linear Thermal Expansion 333
Thermal Stress If the concrete slabs in Figure 12.11 had not buckled upward, they would have been subjected to immense forces from the buildings. The forces needed to prevent a solid object from expand-
ing must be strong enough to counteract any change in length that would occur due to a change
in temperature. Although the change in temperature may be small, the forces—and hence the
stresses—can be enormous. They can, in fact, lead to serious structural damage. Example 4 illus-
trates just how large the stresses can be.
FIGURE 12.12 An expansion joint in a bridge.
D av
id R
. F
ra zi
er /S
ci en
ce S
o u rc
e
Water flow
Movable plunger
Actuator spring
FIGURE 12.13 An antiscalding device.
Analyzing Multiple-Concept Problems
EXAMPLE 4 The Physics of Thermal Stress
A steel beam is used in the roadbed of a bridge. The beam is mounted between
two concrete supports when the temperature is 23 °C, with no room provided
for thermal expansion (see Figure 12.14). What compressional stress must the concrete supports apply to each end of the beam, if they are to keep the beam
from expanding when the temperature rises to 42 °C? Assume that the dis-
tance between the concrete supports does not change as the temperature rises.
Reasoning When the temperature rises by an amount ΔT, the natural tendency of the beam is to expand. If the beam were free to expand, it
would lengthen by an amount ΔL = 𝛼L0ΔT (Equation 12.2). However, the concrete supports prevent this expansion from occurring by exerting
a compressional force on each end of the beam. The magnitude F of this force depends on ΔL through the relation F = YA(ΔL/L0) (Equation 10.17), where Y is Young’s modulus for steel and A is the cross-sectional area of
Beam
Concrete support
Concrete support
FIGURE 12.14 A steel beam is mounted between concrete
supports with no room provided
for thermal expansion.
the beam. According to the discussion in Section 10.8, the compressional
stress is equal to the magnitude of the compressional force divided by the
cross-sectional area, or Stress = F/A.
334 CHAPTER 12 Temperature and Heat
Modeling the Problem
STEP 1 Stress and Force The compressional stress is defi ned as the magnitude F of the com- pressional force divided by the cross-sectional area A of the beam (see Section 10.8), or
Stress = F A
According to Equation 10.17, the magnitude of the compressional force that the concrete supports
exert on each end of the steel beam is given by
F = YA(∆LL 0 ) where Y is Young’s modulus, ΔL is the change in length, and L0 is the original length of the beam. Substituting this expression for F into the defi nition of stress gives Equation 1 in the right column. Young’s modulus Y for steel is known (see Table 10.1), but we do not know either ΔL or L0. However, ΔL is proportional to L0, so we will focus on ΔL in Step 2.
STEP 2 Linear Thermal Expansion If it were free to do so, the beam would expand by an amount ΔL = 𝛼L0ΔT (Equation 12.2), where 𝛼 is the coeffi cient of linear expansion. The change in temperature is the fi nal temperature T minus the initial temperature T0, or ΔT = T − T0. Thus, the beam would have expanded by an amount
∆L = αL 0 (T − T0)
In this expression the variables T and T0 are known, and 𝛼 is available in Table 12.1. We substi- tute this relation for ΔL into Equation 1, as indicated in the right column.
Solution Algebraically combining the results of each step, we have
Stress = Y ∆L L0
= Y αL0(T − T0)
L0 = Yα (T − T0)
Note that the original length L0 of the beam is eliminated algebraically from this result. Taking the value of Y = 2.0 × 1011 N/m2 from Table 10.1 and 𝛼 = 12 × 10−6 (C°)−1 from Table 12.1, we fi nd that
Stress = Yα(T − T0) = (2.0 × 1011 N/m2)[12 × 10−6 (C°)−1](42 °C − 23 °C) = 4.6 × 107 N/m2
This is a large stress, equivalent to nearly one million pounds per square foot.
Related Homework: Problems 20, 24, 98
STEP 1 STEP 2
Stress = Y ∆L L0
(1)
?
Stress = Y ∆L L0
(1)
∆L = αL 0 (T − T0)
Knowns and Unknowns The data for this problem are listed in the table:
Description Symbol Value Initial temperature T0 23 °C
Final temperature T 42 °C
Unknown Variables Stress — ?
The Bimetallic Strip A bimetallic strip is made from two thin strips of metal that have diff erent coeffi cients of linear expansion, as Animated Figure 12.15a shows. Often brass [α = 19 × 10−6 (C°)−1] and steel [α = 12 × 10−6 (C°)−1] are selected. The two pieces are welded or riveted together. When the bimetallic strip is heated, the brass, having the larger value of α, expands more than the steel. Since the two metals are bonded together, the bimetallic strip bends into an arc as in part b, with
12.4 Linear Thermal Expansion 335
the longer brass piece having a larger radius than the steel piece. When the strip is cooled, the
bimetallic strip bends in the opposite direction, as in part c. THE PHYSICS OF . . . an automatic coffee maker. Bimetallic strips are frequently
used as adjustable automatic switches in electrical appliances. Figure 12.16 shows an automatic coff ee maker that turns off when the coff ee is brewed to the selected strength. In part a, while the brewing cycle is on, electricity passes through the heating coil that heats the water. The electricity
can fl ow because the contact mounted on the bimetallic strip touches the contact mounted on the
“strength” adjustment knob, thus providing a continuous path for the electricity. When the bimet-
allic strip gets hot enough to bend away, as in part b of the drawing, the contacts separate. The electricity stops because it no longer has a continuous path along which to fl ow, and the brewing
cycle is shut off . Turning the “strength” knob adjusts the brewing time by adjusting the distance
through which the bimetallic strip must bend for the contact points to separate.
The Expansion of Holes An interesting example of linear expansion occurs when there is a hole in a piece of solid ma-
terial. We know that the material itself expands when heated, but what about the hole? Does it
expand, contract, or remain the same? Conceptual Example 5 provides some insight into the
answer to this question.
Brass Steel
Heated Cooled(a) (b) (c)
ANIMATED FIGURE 12.15 (a) A bimetallic strip and how it behaves when (b) heated and (c) cooled.
Electricity
Heating coil "on"
Bimetallic strip (cold)
Contacts closed
Coffee "strength" adjustment knob
(a) Coffee pot "on" (b) Coffee pot "off"
Bimetallic strip (hot)
Contacts separated
Heating coil
FIGURE 12.16 A bimetallic strip controls whether this coff ee pot is (a) “on” (strip cold, straight) or (b) “off ” (strip hot, bent).
CONCEPTUAL EXAMPLE 5 Do Holes Expand or Contract When the Temperature Increases?
Interactive Figure 12.17a shows eight square tiles that are attached together and arranged to form a square pattern with a hole in the
center. If the tiles are heated, does the size of the hole (a) decrease or (b) increase?
(b) Heated(a) Unheated (c)
9th tile (heated)
Hole
Expanded hole
INTERACTIVE FIGURE 12.17 (a) The tiles are arranged to form a square pattern with a hole in the center. (b) When the tiles are heated, the pattern, including the hole in the center, expands. (c) The expanded hole is the same size as a heated tile.
336 CHAPTER 12 Temperature and Heat
Instead of the separate tiles in Example 5, we could have used a square plate with a square
hole in the center. The hole in the plate would have expanded just like the hole in the pattern of
tiles. Furthermore, the same conclusion applies to a hole of any shape. Thus, it follows that
Problem-Solving Insight A hole in a piece of solid material expands when heated and con- tracts when cooled, just as if it were fi lled with the material that surrounds it.
The equation ΔL = 𝛼L0ΔT can be used to fi nd the change in any linear dimension of the hole, such as its radius or diameter, if the hole is circular. Example 6 illustrates this type of linear ex-
pansion.
Reasoning We can analyze this problem by disassembling the pattern into separate tiles, heating them, and then reassembling the pattern. What
happens to each of the individual tiles can be explained using what we
know about linear expansion.
Answer (a) is incorrect. When a tile is heated both its length and width expand. It is tempting to think, therefore, that the hole in the pattern de-
creases as the surrounding tiles expand into it. However, this is not correct,
because any one tile is prevented from expanding into the hole by the
expansion of the tiles next to it.
Answer (b) is correct. Since each tile expands upon heating, the pat- tern also expands, and the hole along with it, as shown in Interactive
Figure 12.17b. In fact, if we had a ninth tile that was identical to the others and heated it to the same extent, it would fi t exactly into the hole,
as Interactive Figure 12.17c indicates. Thus, not only does the hole expand, it does so exactly as each of the tiles does. Since the ninth
tile is made of the same material as the others, we see that the hole
expands just as if it were made of the material of the surrounding tiles.
The thermal expansion of the hole and the surrounding material is
analogous to a photographic enlargement: everything is enlarged,
including holes.
Related Homework: Problems 13, 23
EXAMPLE 6 A Heated Engagement Ring
A gold engagement ring has an inner diameter of 1.5 × 10−2 m and
a temperature of 27 °C. The ring falls into a sink of hot water whose
temperature is 49 °C. What is the change in the diameter of the hole in
the ring?
Reasoning The hole expands as if it were fi lled with gold, so the change in the diameter is given by ΔL = 𝛼L0ΔT, where 𝛼 = 14 × 10−6 (C°)−1 is
the coeffi cient of linear expansion for gold (Table 12.1), L0 is the original diameter, and ∆T is the change in temperature.
Solution The change in the ring’s diameter is ∆L = αL0∆T = [14 × 10−6 (C°)−1](1.5 × 10−2 m)(49 °C − 27 °C)
= 4.6 × 10−6 m
The previous two examples illustrate that holes expand like the surrounding material when
heated. Therefore, holes in materials with larger coeffi cients of linear expansion expand more
than those in materials with smaller coeffi cients of linear expansion. Conceptual Example 7 explores
this aspect of thermal expansion.
CONCEPTUAL EXAMPLE 7 Expanding Cylinders
Figure 12.18 shows a cross-sectional view of three cylinders, A, B, and C. One is made from lead, one from brass, and one from steel. All
three have the same temperature, and they barely fi t inside each other.
As the cylinders are heated to the same higher temperature, C falls off ,
while A becomes tightly wedged against B. Which cylinder is made
from which material? (a) A is brass, B is lead, C is steel (b) A is lead, B is brass, C is steel (c) A is lead, B is steel, C is brass (d) A is brass, B is steel, C is lead (e) A is steel, B is brass, C is lead (f) A is steel, B is lead, C is brass
Reasoning We will consider how the outer and inner diameters of each cylinder change as the temperature is raised. In particular, with regard
to the inner diameter we note that a hole expands as if it were fi lled with
the surrounding material. According to Table 12.1, lead has the greatest
coeffi cient of linear expansion, followed by brass, and then by steel. Thus,
the outer and inner diameters of the lead cylinder change the most, while
those of the steel cylinder change the least.
Answers (a), (b), (e), and (f) are incorrect. Since the steel cylinder expands the least, it cannot be the outer one, for if it were, the greater expan-
sion of the middle cylinder would prevent the steel cylinder from falling
off , as outer cylinder C actually does. The steel cylinder also cannot be
the inner one, because then the greater expansion of the middle cylinder
would allow the steel cylinder to fall out, contrary to what is observed for
inner cylinder A.
Answers (c) and (d) are correct. Since the steel cylinder cannot be on the outside or on the inside, it must be the middle cylinder B. Figure 12.18a
12.5 Volume Thermal Expansion 337
Check Your Understanding
(The answers are given at the end of the book.) 2. A rod is hung from an aluminum frame, as CYU Figure 12.1 shows.
The rod and the frame have the same temperature, and there is a small
gap between the rod and the fl oor. The frame and rod are then heated
uniformly. Will the rod ever touch the fl oor if the rod is made from
(a) aluminum, (b) lead, (c) brass? 3. A simple pendulum is made using a long, thin metal wire. When the
temperature drops, does the period of the pendulum increase, de-
crease, or remain the same?
4. For added strength, many highways and buildings are constructed with reinforced concrete (concrete that is reinforced with embedded steel
rods). Table 12.1 shows that the coeffi cient of linear expansion 𝛼 for concrete is the same as that for steel. Why is it important that these two coeffi cients be the same?
5. One type of cooking pot is made from stainless steel and has a copper coating over the outside of the bottom. At room temperature the bottom of this pot is fl at, but when heated the bottom is not fl at. When
the bottom of this pot is heated, is it bowed outward or inward?
6. A metal ball has a diameter that is slightly greater than the diameter of a hole that has been cut into a metal plate. The coeffi cient of linear expansion for the metal from which the ball is made is greater than that for the metal of the plate. Which one or more of the following procedures can be used to make
the ball pass through the hole? (a) Raise the temperatures of the ball and the plate by the same amount. (b) Lower the temperatures of the ball and the plate by the same amount. (c) Heat the ball and cool the plate. (d) Cool the ball and heat the plate.
7. A hole is cut through an aluminum plate. A brass ball has a diameter that is slightly smaller than the diameter of the hole. The plate and the ball have the same temperature at all times. Should the plate and
ball both be heated or both be cooled to prevent the ball from falling through the hole?
12.5 Volume Thermal Expansion The volume of a normal material increases as the temperature increases. Most solids and liquids
behave in this fashion. By analogy with linear thermal expansion, the change in volume ΔV is proportional to the change in temperature ΔT and to the initial volume V0, provided the change in temperature is not too large. These two proportionalities can be converted into Equation 12.3
with the aid of a proportionality constant 𝛽, known as the coeffi cient of volume expansion. The algebraic form of this equation is similar to that for linear expansion, ΔL = 𝛼L0ΔT.
A
B
C
Brass
Lead
Steel
(a)
A
B
C
Lead
Brass
Steel
(b)
FIGURE 12.18 Conceptual Example 7 discusses the arrangements of the three cylinders shown in cutaway views in parts a and b.
CYU FIGURE 12.1
Aluminum frame
Rod
Small gap
shows the lead cylinder as the outer cylinder C. It will fall off as the tem-
perature is raised, since lead expands more than steel. The brass inner cyl-
inder A expands more than the steel cylinder that surrounds it and becomes
tightly wedged, as observed. Similar reasoning applies also to Figure 12.18b, which shows the brass cylinder as the outer cylinder and the lead cylinder as the inner one, since both brass and lead expand more than steel.
338 CHAPTER 12 Temperature and Heat
VOLUME THERMAL EXPANSION The volume V0 of an object changes by an amount ΔV when its temperature changes by an amount ΔT:
∆V = βV0 ∆T (12.3)
where β is the coeffi cient of volume expansion. Common Unit for the Coeffi cient of Volume Expansion: (C°)–1
The unit for 𝛽, like that for 𝛼, is (C°)−1. Values for 𝛽 depend on the nature of the material,
and Table 12.1 lists some examples measured near 20 °C. The values of 𝛽 for liquids are substantially larger than those for solids, because liquids typically expand more than solids,
given the same initial volumes and temperature changes. Table 12.1 also shows that, for most solids, the coeffi cient of volume expansion is three times as much as the coeffi cient of linear
expansion: 𝛽 = 3𝛼. If a cavity exists within a solid object, the volume of the cavity increases when the object
expands, just as if the cavity were fi lled with the surrounding material. The expansion of the
cavity is analogous to the expansion of a hole in a sheet of material. Accordingly, the change in
volume of a cavity can be found using the relation ΔV = 𝛽V0ΔT, where 𝛽 is the coeffi cient of volume expansion of the material that surrounds the cavity. Example 8 illustrates this point.
EXAMPLE 8 The Physics of the Overflow of an Automobile Radiator
A small plastic container, called the coolant reservoir, catches the radiator
fl uid that overfl ows when an automobile engine becomes hot (see Figure 12.19). The radiator is made of copper, and the coolant has a coeffi cient of volume expansion of 𝛽 = 4.10 × 10−4 (C°)−1. If the radiator is fi lled to its 15-quart capacity when the engine is cold (6.0 °C), how much over-
fl ow will spill into the reservoir when the coolant reaches its operating
temperature of 92 °C?
Reasoning When the temperature increases, both the coolant and the radiator expand. If they were to expand by the same amount, there would
be no overfl ow. However, the liquid coolant expands more than the radi-
ator, and the overfl ow volume is the amount of coolant expansion minus the amount of the radiator cavity expansion.
Solution When the temperature increases by 86 C°, the coolant expands by an amount
∆V = βV0∆T = [4.10 × 10−4 (C°)−1](15 quarts)(86 C°) (12.3)
= 0.53 quarts
The radiator cavity expands as if it were fi lled with copper [β = 51 × 10−6 (C°)−1 ; see Table 12.1]. The expansion of the radiator cavity is
∆V = βV0∆T = [51 × 10−6 (C°)−1](15 quarts)(86 C°) = 0.066 quarts
The overfl ow volume is 0.53 quarts − 0.066 quarts = 0.46 quarts .
Coolant reservoir
Radiator
FIGURE 12.19 An automobile radiator and a
coolant reservoir for catching
the overfl ow from the radiator.
Although most substances expand when heated, a few do not. For instance, if water at 0 °C
is heated, its volume decreases until the temperature reaches 4 °C. Above 4 °C water behaves normally, and its volume increases as the temperature increases. Because a given mass of water
has a minimum volume at 4 °C, the density (mass per unit volume) of water is greatest at 4 °C,
as Figure 12.20 shows. BIO THE PHYSICS OF . . . ice formation and the survival of aquatic life. The fact
that water has its greatest density at 4 °C, rather than at 0 °C, has important consequences for the
way in which a lake freezes. When the air temperature drops, the surface layer of water is chilled.
As the temperature of the surface layer drops toward 4 °C, this layer becomes more dense than the
warmer water below. The denser water sinks and pushes up the deeper and warmer water, which
in turn is chilled at the surface. This process continues until the temperature of the entire lake
reaches 4 °C. Further cooling of the surface water below 4 °C makes it less dense than the deeper layers; consequently, the surface layer does not sink but stays on top. Continued cooling of the top
12.6 Heat and Internal Energy 339
layer to 0 °C leads to the formation of ice that fl oats on the water, because ice has a smaller dens-
ity than water at any temperature. Below the ice, however, the water temperature remains above
0 °C. The sheet of ice acts as an insulator that reduces the loss of heat from the lake, especially
if the ice is covered with a blanket of snow, which is also an insulator. As a result, lakes usually
do not freeze solid, even during prolonged cold spells, so fi sh and other aquatic life can survive.
THE PHYSICS OF . . . bursting water pipes. The fact that the density of ice is smaller than the density of water has an important consequence for homeowners, who have to contend
with the possibility of bursting water pipes during severe winters. Water often freezes in a section
of pipe exposed to unusually cold temperatures. The ice can form an immovable plug that pre-
vents the subsequent fl ow of water, as Figure 12.21 illustrates. When water (larger density) turns to ice (smaller density), its volume expands by 8.3%. Therefore, when more water freezes at
the left side of the plug, the expanding ice pushes liquid back into the pipe leading to the street
connection, and no damage is done. However, when ice forms on the right side of the plug, the
expanding ice pushes liquid to the right—but it has nowhere to go if the faucet is closed. As ice
continues to form and expand, the water pressure between the plug and faucet rises. Even a small
increase in the amount of ice produces a large increase in the pressure. This situation is analog-
ous to the thermal stress discussed in Multiple-Concept Example 4, where a small change in the
length of the steel beam produces a large stress on the concrete supports. The entire section of
pipe to the right of the blockage experiences the same elevated pressure, according to Pascal’s
principle (Section 11.5). Therefore, the pipe can burst at any point where it is structurally weak,
even within the heated space of the building. If you should lose heat during the winter, there is a
simple way to prevent pipes from bursting. Simply open the faucet so it drips a little. The excess-
ive pressure will be relieved.
Check Your Understanding
(The answers are given at the end of the book.) 8. Suppose that liquid mercury and glass both had the same coeffi cient of volume expansion. Would a
mercury-in-glass thermometer still work?
9. Is the buoyant force provided by warmer water (above 4 °C) greater than, less than, or equal to the buoyant force provided by cooler water (also above 4 °C)?
12.6 Heat and Internal Energy An object with a high temperature is said to be hot, and the word “hot” brings to mind the word
“heat.” Heat fl ows from a hotter object to a cooler object when the two are placed in contact. It is for this reason that a cup of hot coff ee feels hot to the touch, while a glass of ice water feels cold.
When the person in Figure 12.22a touches the coff ee cup, heat fl ows from the hotter cup into the cooler hand. When the person touches the glass in part b of the drawing, heat again fl ows from hot to cold, in this case from the warmer hand into the colder glass. The response of the nerves in
the hand to the arrival or departure of heat prompts the brain to identify the coff ee cup as being
hot and the glass as being cold.
What exactly is heat? As the following defi nition indicates, heat is a form of energy, energy
in transit from hot to cold.
DEFINITION OF HEAT Heat is energy that fl ows from a higher-temperature object to a lower-temperature object because of the diff erence in temperatures.
SI Unit of Heat: joule (J)
Being a kind of energy, heat is measured in the same units used for work, kinetic energy, and
potential energy. Thus, the SI unit for heat is the joule.
The heat that fl ows from hot to cold in Figure 12.22 originates in the internal energy of the hot substance. The internal energy of a substance is the sum of the molecular kinetic energy
Closed faucet
To street connection
Ice
Water at normal
pressure
Water at very high pressure
FIGURE 12.21 As water freezes and expands, enormous pressure is applied to the
liquid water between the ice and the closed
faucet.
Heat flow
Heat flow
(a)
(b)
FIGURE 12.22 Heat is energy in transit from hot to cold. (a) Heat fl ows from the hotter coff ee cup to the colder hand. (b) Heat fl ows from the warmer hand to the colder
glass of ice water.
0 2 4 6 8 10 999.6
999.7
999.8
999.9
1000.0
Temperature, °C
D en
si ty
, k g/
m 3
Maximum density at 4 °C
FIGURE 12.20 The density of water in the temperature range from 0 to 10 °C. At 4 °C
water has a maximum density of 999.973 kg/m3.
(This value is equivalent to the often-quoted
density of 1.000 00 grams per milliliter.)
340 CHAPTER 12 Temperature and Heat
(due to random motion of the molecules), the molecular potential energy (due to forces that act
between the atoms of a molecule and between molecules), and other kinds of molecular energy.
When heat fl ows in circumstances where no work is done, the internal energy of the hot substance
decreases and the internal energy of the cold substance increases. Although heat may originate in
the internal energy supply of a substance, it is not correct to say that a substance contains heat. The substance has internal energy, not heat. The word “heat” only refers to the energy actually in
transit from hot to cold.
The next two sections consider some eff ects of heat. For instance, when preparing spaghetti,
the fi rst thing that a cook does is to heat the water. Heat from the stove causes the internal energy
of the water to increase. Associated with this increase is a rise in temperature. After a while,
the temperature reaches 100 °C, and the water begins to boil. During boiling, the added heat
causes the water to change from a liquid to a vapor phase (steam). The next section investigates
how the addition (or removal) of heat causes the temperature of a substance to change. Then,
Section 12.8 discusses the relationship between heat and phase change, such as that which occurs
when water boils.
12.7 Heat and Temperature Change: Specific Heat Capacity
Solids and Liquids Greater amounts of heat are needed to raise the temperature of solids or liquids to higher values.
A greater amount of heat is also required to raise the temperature of a greater mass of material.
Similar comments apply when the temperature is lowered, except that heat must be removed.
For limited temperature ranges, experiment shows that the heat Q is directly proportional to the change in temperature ΔT and to the mass m. These two proportionalities are expressed below in Equation 12.4, with the help of a proportionality constant c that is referred to as the specifi c heat capacity of the material.
HEAT SUPPLIED OR REMOVED IN CHANGING THE TEMPERATURE OF A SUBSTANCE The heat Q that must be supplied or removed to change the temperature of a substance of mass m by ΔT degrees is
Q = cm ΔT (12.4)
where c is the specifi c heat capacity of the substance.
Common Unit for Specifi c Heat Capacity: J/(kg · C°)
Solving Equation 12.4 for the specifi c heat capacity shows that c = Q/(m ΔT), so the unit for specifi c heat capacity is J/(kg · C°). Table 12.2 reveals that the value of the specifi c heat capacity depends on the nature of the material. Examples 9 and 10 illustrate the use of
Equation 12.4.
TABLE 12.2 Specific Heat Capacitiesa of Some Solids and Liquids
Substance
Specific Heat Capacity, c J/(kg · C°)
Solids Aluminum 9.00 × 102
Copper 387
Glass 840
Human body
(37 °C, average)
3500
Ice (−15 °C) 2.00 × 103
Iron or steel 452
Lead 128
Silver 235
Liquids Benzene 1740
Ethyl alcohol 2450
Glycerin 2410
Mercury 139
Water (15 °C) 4186
aExcept as noted, the values are for 25 °C and 1 atm of
pressure.
EXAMPLE 9 A Hot Jogger
In a half hour, a 65-kg jogger can generate 8.0 × 105 J of heat. This
heat is removed from the jogger’s body by a variety of means, includ-
ing the body’s own temperature-regulating mechanisms. If the heat
were not removed, how much would the jogger’s body temperature
increase?
Reasoning The increase in body temperature depends on the amount of heat Q generated by the jogger, her mass m, and the specifi c heat capacity c of the human body. Since numerical values are known for these three variables, we can determine the potential rise in temperature by using
Equation 12.4.
12.7 Heat and Temperature Change: Specific Heat Capacity 341
Gases As we will see in Section 15.6, the value of the specifi c heat capacity depends on whether the
pressure or volume is held constant while energy in the form of heat is added to or removed
from a substance. The distinction between constant pressure and constant volume is usually not
important for solids and liquids but is signifi cant for gases. In Section 15.6, we will see that a
greater value for the specifi c heat capacity is obtained for a gas at constant pressure than for a gas
at constant volume.
Heat Units Other than the Joule There are three heat units other than the joule in common use. One kilocalorie (1 kcal) was
defi ned historically as the amount of heat needed to raise the temperature of one kilogram of
water by one Celsius degree.* With Q = 1.00 kcal, m = 1.00 kg, and ΔT = 1.00 C°, the equation Q = cm ΔT shows that such a defi nition is equivalent to a specifi c heat capacity for water of c = 1.00 kcal/(kg · C°). Similarly, one calorie (1 cal) was defi ned as the amount of heat needed to raise the temperature of one gram of water by one Celsius degree, which yields a value of
FIGURE 12.23 Cats, such as this lion, often pant to get rid of excess heat.
A n u p S
h ah
/G et
ty I
m ag
es
Solution Table 12.2 gives the average specifi c heat capacity of the human body as 3500 J/(kg · C°). With this value, Equation 12.4 shows that
∆T = Q cm
= 8.0 × 105 J
[3500 J/ (kg · C°)](65 kg) = 3.5 C°
An increase in body temperature of 3.5 °C could be life-threatening. One
way in which the jogger’s body prevents it from occurring is to remove
excess heat by perspiring. In contrast, cats, such as the one in Figure 12.23, do not perspire but often pant to remove excess heat.
EXAMPLE 10 Taking a Hot Shower
Cold water at a temperature of 15 °C enters a heater, and the result-
ing hot water has a temperature of 61 °C. A person uses 120 kg of hot
water in taking a shower. (a) Find the energy needed to heat the water. (b) Assuming that the utility company charges $0.10 per kilowatt · hour for electrical energy, determine the cost of heating the water.
Reasoning The amount Q of heat needed to raise the water temperature can be found from the relation Q = cm ΔT, since the specifi c heat capacity, mass, and temperature change of the water are known. To determine the cost of this
energy, we multiply the cost per unit of energy ($0.10 per kilowatt · hour) by the amount of energy used, expressed in energy units of kilowatt · hours.
Solution (a) The amount of heat needed to heat the water is
Q = cm ΔT = [4186 J/(kg · C°)](120 kg)(61 °C − 15 °C) (12.4)
= 2.3 × 107 J
(b) The kilowatt · hour (kWh) is the unit of energy that utility companies use in your electric bill. To calculate the cost, we need to determine the
number of joules in one kilowatt · hour. Recall that 1 kilowatt is 1000 watts (1 kW = 1000 W), 1 watt is 1 joule per second (1 W = 1 J/s; see
Table 6.3), and 1 hour is equal to 3600 seconds (1 h = 3600 s). Thus,
1 kWh = (1 kWh) (1000 W1 kW ) ( 1 J /s
1 W ) ( 3600 s
1 h ) = 3.60 × 106 J The number of kilowatt · hours of energy used to heat the water is
(2.3 × 107 J ) ( 1 kWh3.60 × 106 J) = 6.4 kWh At a cost of $0.10 per kWh, the bill for the heat is $0.64 or 64 cents.
*From 14.5 to 15.5 °C.
342 CHAPTER 12 Temperature and Heat
c = 1.00 cal/(g · C°). (Nutritionists use the word “Calorie,” with a capital C, to specify the energy content of foods; this use is unfortunate, since 1 Calorie = 1000 calories = 1 kcal.) The British
thermal unit (Btu) is the other commonly used heat unit and was defi ned historically as the
amount of heat needed to raise the temperature of one pound of water by one Fahrenheit degree.
It was not until the time of James Joule (1818–1889) that the relationship between energy in
the form of work (in units of joules) and energy in the form of heat (in units of kilocalories) was
fi rmly established. Joule’s experiments revealed that the performance of mechanical work, like
rubbing your hands together, can make the temperature of a substance rise, just as the absorption
of heat can. His experiments and those of later workers have shown that
1 kcal = 4186 joules or 1 cal = 4.186 joules
Because of its historical signifi cance, this conversion factor is known as the mechanical equi- valent of heat.
Calorimetry In Section 6.8 we encountered the principle of conservation of energy, which states that energy
can be neither created nor destroyed, but can only be converted from one form to another. There
we dealt with kinetic and potential energies. In this chapter we have expanded our concept of
energy to include heat, which is energy that fl ows from a higher-temperature object to a lower-
temperature object because of the diff erence in temperature. No matter what its form, whether
kinetic energy, potential energy, or heat, energy can be neither created nor destroyed. This fact
governs the way objects at diff erent temperatures come to an equilibrium temperature when they
are placed in contact. If there is no heat loss to the external surroundings, the amount of heat
gained by the cooler objects equals the amount of heat lost by the hotter ones, a process that is
consistent with the conservation of energy. Just this kind of process occurs within a thermos. A
perfect thermos would prevent any heat from leaking out or in. However, energy in the form of
heat can fl ow between materials inside the thermos to the extent that they have diff erent temper- atures; for example, between ice cubes and warm tea. The transfer of energy continues until a
common temperature is reached at thermal equilibrium.
The kind of heat transfer that occurs within a thermos of iced tea also occurs within a
calorimeter, which is the experimental apparatus used in a technique known as calorimetry. Figure 12.24 shows that, like a thermos, a calorimeter is essentially an insulated container. It can be used to determine the specifi c heat capacity of a substance, as the next example illustrates.
Thermometer
Calorimeter cup
Insulating container
Unknown material
FIGURE 12.24 A calorimeter can be used to measure the specifi c heat capacity of an
unknown material.
EXAMPLE 11 Measuring the Specific Heat Capacity
The calorimeter cup in Figure 12.24 is made from 0.15 kg of aluminum and contains 0.20 kg of water. Initially, the water and the cup have a common
temperature of 18.0 °C. A 0.040-kg mass of unknown material is heated
to a temperature of 97.0 °C and then added to the water. The temperature
of the water, the cup, and the unknown material is 22.0 °C after thermal
equilibrium is reestablished. Ignoring the small amount of heat gained by
the thermometer, fi nd the specifi c heat capacity of the unknown material.
Reasoning Since energy is conserved and there is negligible heat fl ow between the calorimeter and the outside surroundings, the amount of heat
gained by the cold water and the aluminum cup as they warm up is equal
to the amount of heat lost by the unknown material as it cools down. Each
amount of heat can be calculated using the relation Q = cm ΔT, if we are careful to write the change in temperature ΔT as the higher temperature minus the lower temperature. The equation “Heat gained = Heat lost”
contains a single unknown quantity, the desired specifi c heat capacity.
Problem-Solving Insight In the equation “Heat gained = Heat lost,” both sides must have the same algebraic sign. Therefore, when calculating heat contributions for use in
this equation, write any temperature changes as the higher minus the lower temperature.
Solution (cm ∆T )Al + (cm ∆T )water = (cm ∆T )unknown
cunknown = cAlmAl ∆TAl + cwater m water ∆Twater
m unknown ∆Tunknown The changes in temperature of the substances are ΔTAl = ΔTwater = 22.0 °C − 18.0 °C = 4.0 C°, and ΔTunknown = 97.0 °C − 22.0 °C = 75.0 C°. Table 12.2 contains values for the specifi c heat capacities of aluminum and water. Substituting these data into the equation above, we fi nd that
cunknown = [9.00 × 102 J/ (kg · C°)](0.15 kg )(4.0 C°)
(0.040 kg )(75.0 C°)
+ [4186 J/ (kg · C°)](0.20 kg )(4.0 C°)
(0.040 kg )(75.0 C°)
= 1300 J/ (kg · C°)
⏟⎵⎵⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⎵⎵⏟
Heat gained by
aluminum and water
⏟⎵⎵⏟⎵⎵⏟
Heat lost by
unknown material
12.8 Heat and Phase Change: Latent Heat 343
Check Your Understanding
(The answers are given at the end of the book.) 10. Two diff erent objects are supplied with equal amounts of heat. Which one or more of the following
statements explain why their temperature changes would not necessarily be the same? (a) The objects have the same mass but are made from materials that have diff erent specifi c heat capacities. (b) The objects are made from the same material but have diff erent masses. (c) The objects have the same mass and are made from the same material.
11. Two objects are made from the same material but have diff erent masses. The two are placed in contact, and neither one loses any
heat to the environment. Which object experiences the temperature
change with the greater magnitude, or does each object experience a
temperature change of the same magnitude?
12. Consider an object of mass m that experiences a change ΔT in its temperature. Various possibilities for these variables are listed
in CYU Table 12.1. Rank these possibilities in descending order (largest fi rst) according to how much heat is needed to bring about
the change in temperature.
12.8 Heat and Phase Change: Latent Heat Surprisingly, there are situations in which the addition or removal of heat does not cause a tem-
perature change. Consider a well-stirred glass of iced tea that has come to thermal equilibrium.
Even though heat enters the glass from the warmer room, the temperature of the tea does not rise
above 0 °C as long as ice cubes are present. Apparently the heat is being used for some purpose
other than raising the temperature. In fact, the heat is being used to melt the ice, and only when
all of it is melted will the temperature of the liquid begin to rise.
An important point illustrated by the iced tea example is that there is more than one type or
phase of matter. For instance, some of the water in the glass is in the solid phase (ice) and some is
in the liquid phase. The gas or vapor phase is the third familiar phase of matter. In the gas phase,
water is referred to as water vapor or steam. All three phases of water are present in the scene
depicted in Figure 12.25, although the water vapor in the air is not visible in the photograph. Matter can change from one phase to another, and heat plays a role in the change. Figure 12.26
summarizes the various possibilities. A solid can melt or fuse into a liquid if heat is added, while the liquid can freeze into a solid if heat is removed. Similarly, a liquid can evaporate into a gas if heat is supplied, while the gas can condense into a liquid if heat is taken away. Rapid evap- oration, with the formation of vapor bubbles within the liquid, is called boiling. Finally, a solid can sometimes change directly into a gas if heat is provided. We say that the solid sublimes into a gas. Examples of sublimation are (1) solid carbon dioxide, CO2 (dry ice), turning into gaseous
CO2 and (2) solid naphthalene (moth balls) turning into naphthalene fumes. Conversely, if heat is
removed under the right conditions, the gas will condense directly into a solid.
Figure 12.27 displays a graph that indicates what typically happens when heat is added to a material that changes phase. The graph records temperature versus heat added and refers to water
at the normal atmospheric pressure of 1.01 × 105 Pa. The water starts off as ice at the subfreezing
temperature of −30 °C. As heat is added, the temperature of the ice increases, in accord with
the specifi c heat capacity of ice [2000 J/(kg · C°)]. Not until the temperature reaches the normal melting/freezing point of 0 °C does the water begin to change phase. Then, when heat is added,
the solid changes into the liquid, the temperature staying at 0 °C until all the ice has melted. Once all the material is in the liquid phase, additional heat causes the temperature to increase
again, now in accord with the specifi c heat capacity of liquid water [4186 J/(kg · C°)]. When the temperature reaches the normal boiling/condensing point of 100 °C, the water begins to change
from the liquid to the gas phase and continues to do so as long as heat is added. The temperature
remains at 100 °C until all liquid is gone. When all of the material is in the gas phase, additional heat once again causes the temperature to rise, this time according to the specifi c heat capacity of
water vapor at constant atmospheric pressure [2020 J/(kg · C°)]. Conceptual Example 12 applies the information in Figure 12.27 to a familiar situation.
FIGURE 12.25 This antarctic scene shows resting crabeater seals. The three phases
of water are present: solid ice is fl oating in
liquid water, and water vapor is present in the
air (invisible) and in the clouds in the sky.
Frank Krahmer/Getty Images
Solid Liquid
Freezing
C on
de ns
in g
Gas
S ub
lim in
g
C ondensing
E vaporating
Melting
FIGURE 12.26 Three familiar phases of matter—solid, liquid, and gas—and the phase
changes that can occur between any two of
them.
m (kg) ΔT (C°) (a) 2.0 15 (b) 1.5 40 (c) 3.0 25 (d) 2.5 20
CYU TABLE 12.1
344 CHAPTER 12 Temperature and Heat
When a substance changes from one phase to another, the amount of heat that must be added
or removed depends on the type of material and the nature of the phase change. The heat per
kilogram associated with a phase change is referred to as latent heat:
HEAT SUPPLIED OR REMOVED IN CHANGING THE PHASE OF A SUBSTANCE The heat Q that must be supplied or removed to change the phase of a mass m of a substance is
Q = mL (12.5)
where L is the latent heat of the substance.
SI Unit of Latent Heat: J/kg
The latent heat of fusion Lf refers to the change between solid and liquid phases, the latent heat of vaporization Lv applies to the change between liquid and gas phases, and the latent heat of sublimation Ls refers to the change between solid and gas phases.
Table 12.3 gives some typical values of latent heats of fusion and vaporization. For instance, the latent heat of fusion for water is Lf = 3.35 × 105 J/kg. Thus, 3.35 × 105 J of heat must be supplied to melt one kilogram of ice at 0 °C into liquid water at 0 °C; conversely, this amount of
heat must be removed from one kilogram of liquid water at 0 °C to freeze the liquid into ice at 0 °C.
BIO THE PHYSICS OF . . . steam burns. In comparison to the latent heat of fusion, Table 12.3 indicates that the latent heat of vaporization for water has the much larger value of Lv = 22.6 × 105 J/kg. When water boils at 100 °C, 22.6 × 105 J of heat must be supplied for each kilogram of liquid turned into steam. And when steam condenses at 100 °C, this amount of heat
is released from each kilogram of steam that changes back into liquid. Liquid water at 100 °C is
hot enough by itself to cause a bad burn, and the additional eff ect of the large latent heat can cause
severe tissue damage if condensation occurs on the skin.
THE PHYSICS OF . . . high-tech clothing. By taking advantage of the latent heat of fusion, designers can now engineer clothing that can absorb or release heat to help maintain
a comfortable and approximately constant temperature close to your body. As the photograph
in Figure 12.28 shows, the fabric in this type of clothing is coated with microscopic balls of
Te m
pe ra
tu re
, °C
Water boils
Water warms up
Water vapor warms up
Ice warms up
Ice melts
Heat
100
0
–30
FIGURE 12.27 The graph shows the way the temperature
of water changes as heat is
added, starting with ice at
−30 °C. The pressure is
atmospheric pressure.
CONCEPTUAL EXAMPLE 12 Saving Energy
Suppose you are cooking spaghetti, and the instructions say “boil the
pasta in water for ten minutes.” To cook spaghetti in an open pot using
the least amount of energy, should you (a) turn up the burner to its fullest so the water vigorously boils or (b) turn down the burner so the water barely boils?
Reasoning The spaghetti needs to cook at the temperature of boiling water for ten minutes. In an open pot the pressure is atmospheric pressure,
and water boils at 100 °C, regardless of whether it is vigorously boiling
or just barely boiling. To convert water into steam requires energy in the
form of heat from the burner, and the greater the amount of water converted,
the greater the amount of energy needed.
Answer (a) is incorrect. Causing the water to boil vigorously just wastes energy unnecessarily. All it accomplishes is to convert more water
into steam.
Answer (b) is correct. Keeping the water just barely boiling uses the least amount of energy to keep the spaghetti at 100 °C, because it minim-
izes the amount of water converted into steam.
12.8 Heat and Phase Change: Latent Heat 345
heat-resistant plastic that contain a substance known as a “phase-change material” (PCM). When
you are enjoying your favorite winter sport, for example, it is easy to become overheated. The
PCM prevents this by melting, absorbing excess body heat in the process. When you are taking
a break and cooling down, however, the PCM freezes and releases heat to keep you warm. The
temperature range over which the PCM can maintain a comfort zone is related to its melting/
freezing temperature, which is determined by its chemical composition.
Examples 13 and 14 illustrate how to take into account the eff ect of latent heat when using
the conservation-of-energy principle.
FIGURE 12.28 This highly magnifi ed image shows a high-tech fabric that can
automatically adjust in reaction to your body
heat and help maintain a constant temperature
next to your skin. See the text discussion.
Courtesy Outlast Technologies LLC,Golden, CO
TABLE 12.3 Latent Heatsa of Fusion and Vaporization
Substance Melting Point
(°C)
Latent Heat of Fusion, Lf
(J/kg) Boiling Point
(°C)
Latent Heat of Vaporization, Lf
(J/kg) Ammonia −77.8 33.2 × 104 −33.4 13.7 × 105
Benzene 5.5 12.6 × 104 80.1 3.94 × 105
Copper 1083 20.7 × 104 2566 47.3 × 105
Ethyl alcohol −114.4 10.8 × 104 78.3 8.55 × 105
Gold 1063 6.28 × 104 2808 17.2 × 105
Lead 327.3 2.32 × 104 1750 8.59 × 105
Mercury −38.9 1.14 × 104 356.6 2.96 × 105
Nitrogen −210.0 2.57 × 104 −195.8 2.00 × 105
Oxygen −218.8 1.39 × 104 −183.0 2.13 × 105
Water 0.0 33.5 × 104 100.0 22.6 × 105
aThe values pertain to 1 atm pressure.
EXAMPLE 13 Ice-Cold Lemonade
Ice at 0 °C is placed in a Styrofoam cup containing 0.32 kg of lemonade at
27 °C. The specifi c heat capacity of lemonade is virtually the same as that
of water; that is, c = 4186 J/(kg · C°). After the ice and lemonade reach an equilibrium temperature, some ice still remains. The latent heat of fusion
for water is Lf = 3.35 × 105 J/kg. Assume that the mass of the cup is so small that it absorbs a negligible amount of heat, and ignore any heat lost
to the surroundings. Determine the mass of ice that has melted.
Reasoning According to the principle of energy conservation, the amount of heat gained by the melting ice equals the amount of heat lost
by the cooling lemonade. According to Equation 12.5, the amount of
heat gained by the melting ice is Q = mLf, where m is the mass of the melted ice, and Lf is the latent heat of fusion for water. The amount of heat lost by the lemonade is given by Q = cm ΔT, where ΔT is the higher
temperature of 27 °C minus the lower equilibrium temperature. The equi-
librium temperature is 0 °C, because there is some ice remaining, and ice
is in equilibrium with liquid water when the temperature is 0 °C.
Solution (mL f) ice = (cm ∆T ) lemonade
The mass mice of ice that has melted is
m ice = (cm ∆T ) lemonade
Lf =
[4186 J/(kg ⋅C°)](0.32 kg )(27 °C − 0 °C)
3.35 × 105 J / kg
= 0.11 kg
⏟⏟⏟
Heat gained
by ice
⏟⎵⎵⏟⎵⎵⏟
Heat lost by
lemonade
EXAMPLE 14 Getting Ready for a Party
A 7.00-kg glass bowl [c = 840 J/(kg · C°)] contains 16.0 kg of punch at 25.0 °C. Two-and-a-half kilograms of ice [c = 2.00 × 103 J/(kg · C°)] are added to the punch. The ice has an initial temperature of −20.0 °C, having
been kept in a very cold freezer. The punch may be treated as if it were
water [c = 4186 J/(kg · C°)], and it may be assumed that there is no heat fl ow between the punch bowl and the external environment. The latent
heat of fusion for water is 3.35 × 105 J/kg. When thermal equilibrium is
reached, all the ice has melted, and the fi nal temperature of the mixture is
above 0 °C. Determine this temperature.
Reasoning The fi nal temperature can be found by using the conserva- tion of energy principle: the amount of heat gained is equal to the amount
346 CHAPTER 12 Temperature and Heat
of heat lost. Heat is gained (a) by the ice in warming up to the melting
point, (b) by the ice in changing phase from a solid to a liquid, and (c) by
the liquid that results from the ice warming up to the fi nal temperature;
heat is lost (d) by the punch and (e) by the bowl in cooling down. The
amount of heat gained or lost by each component in changing temperature
can be determined from the relation Q = cm ΔT, where ΔT is the higher temperature minus the lower temperature. The amount of heat gained
when water changes phase from a solid to a liquid at 0 °C is Q = mLf, where m is the mass of water and Lf is the latent heat of fusion.
Solution The amount of heat gained or lost by each component is listed as follows:
(a) Heat gained when = [2.00 × 103 J/(kg · C°)](2.50 kg) ice warms to 0.0 °C [0.0 °C − (−20.0 °C)]
(b) Heat gained when ice melts at 0.0 °C
= (2.50 kg)(3.35 × 105 J/kg)
(c) Heat gained when melted ice (liquid) = [4186 J/(kg · C°)](2.50 kg)(T − 0.0 °C) warms to temperature T
(d) Heat lost when punch cools to temperature T = [4186 J/(kg · C°)](16.0 kg)(25.0 °C − T)
(e) Heat lost when bowl cools to temperature T = [840 J/(kg · C°)](7.00 kg)(25.0 °C − T )
Setting the amount of heat gained equal to the amount of heat lost gives:
(a) + (b) + (c) = (d) + (e)
This equation can be solved to show that T = 11 °C .
⏟⎵⎵⏟⎵⎵⏟
Heat gained
⏟⏟⏟
Heat lost
Math Skills Carrying out the multiplications listed for the terms (a), (b), (c), (d), and (e), we fi nd that the heat-gained-equals-heat-
lost equation can be written as follows:
(1.00 × 10 5 ) + (8.38 × 10 5 ) + (1.05 × 10 4 ) T
= (1.67 × 106) − (6.70 × 10 4)T + (1.47 × 105) − (5.88 × 103)T
Units have been omitted for the sake of clarity. Combining terms
shows that
(9.38 × 10 5) + (1.05 × 10 4)T = (1.82 × 106) − (7.29 × 104)T (1)
In combining terms, we have paid particular attention to the fact that not all of the exponential powers of ten are the same. For example, in the shaded boxes on the right-hand side of our starting
equation, we have
(1.67 × 10 6 ) + (1.47 × 10 5 ) = 1.82 × 10 6
We do not have
(1.67 × 10 6 ) + (1.47 × 10 6 ) = 3.14 × 10 6 or (1.67 × 10 5 ) + (1.47 × 10 5 ) = 3.14 × 10 5
Rearranging and further combining terms in Equation 1 yields
(8.34 × 10 4 )T = 8.8 × 10 5 or T = 11 °C
⏟⎵⎵⏟⎵⎵⏟
(a)
⏟⎵⎵⏟⎵⎵⏟
(b)
⏟⎵⎵⏟⎵⎵⏟
(c)
⏟⎵⎵⎵⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⎵⎵⎵⏟
(d)
⏟⎵⎵⎵⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⎵⎵⎵⏟
(e)
THE PHYSICS OF . . . a dye-sublimation color printer. An interesting application of the phase change between a solid and a gas is found in one kind of color printer used with
computers. A dye-sublimation printer uses a thin plastic fi lm coated with separate panels of cyan
(blue), yellow, and magenta pigment or dye. A full spectrum of colors is produced by using com-
binations of tiny spots of these dyes. As Figure 12.29 shows, the coated fi lm passes in front of a print head that extends across the width of the paper and contains 2400 heating elements. When a
heating element is turned on, the dye in front of it absorbs heat and goes from a solid to a gas—it
sublimes—with no liquid phase in between. A coating on the paper absorbs the gaseous dye on
contact, producing a small spot of color. The intensity of the spot is controlled by the heating
element, since each element can produce 256 diff erent temperatures; the hotter the element, the
greater the amount of dye transferred to the paper. The paper makes three separate passes across
the print head, once for each of the dyes. The fi nal result is an image of near-photographic quality.
Some printers also employ a fourth pass, in which a clear plastic coating is deposited over the
photograph. This coating makes the print waterproof and also helps to prevent premature fading.
Check Your Understanding
(The answers are given at the end of the book.) 13. Fruit blossoms are permanently damaged at temperatures of about −4 °C (a hard freeze). Orchard own-
ers sometimes spray a fi lm of water over the blossoms to protect them when a hard freeze is expected.
Why does this technique off er protection?
14. When ice cubes are used to cool a drink, both their mass and temperature are important in how eff ective they are.
CYU Table 12.2 lists several possibilities for the mass and temperature of the ice cubes used to cool one par-
ticular drink. Rank the possibilities in descending order
(best fi rst) according to their cooling eff ectiveness. Note
that the latent heat of phase change and the specifi c heat
capacity must be considered.
Print head
Print head
Gaseous dye
Coated paper
Plastic film
Dye removed from film
Heating element
FIGURE 12.29 A dye-sublimation printer. As the plastic fi lm passes in front of the print
head, the heat from a given heating element
causes one of three pigments or dyes on the
fi lm to sublime from a solid to a gas. The
gaseous dye is absorbed onto the coated
paper as a dot of color. The size of the dots
on the paper has been exaggerated for clarity.
Mass of ice cubes
Temperature of ice cubes
(a) m −6.0 °C (b) 12 m −12 °C
(c) 2m −3.0 °C
CYU TABLE 12.2
12.9 Equilibrium Between Phases of Matter 347
12.9 *Equilibrium Between Phases of Matter Under specifi c conditions of temperature and pressure, a substance can exist at equilibrium in
more than one phase at the same time. Consider Interactive Figure 12.30, which shows a con- tainer kept at a constant temperature by a large reservoir of heated sand. Initially the container is
evacuated. Part a shows it just after it has been partially fi lled with a liquid and a few fast-moving molecules are escaping the liquid and forming a vapor phase. These molecules pick up the
required energy (the latent heat of vaporization) during collisions with neighboring molecules
in the liquid. However, the reservoir of heated sand replenishes the energy carried away, thus
maintaining the constant temperature. At fi rst, the movement of molecules is predominantly
from liquid to vapor, although some molecules in the vapor phase do reenter the liquid. As the
molecules accumulate in the vapor, the number reentering the liquid eventually equals the num-
ber entering the vapor, at which point equilibrium is established, as in part b. From this point on, the concentration of molecules in the vapor phase does not change, and the vapor pressure
remains constant. The pressure of the vapor that coexists in equilibrium with the liquid is called
the equilibrium vapor pressure of the liquid. The equilibrium vapor pressure does not depend on the volume of space above the liquid.
If more space were provided, more liquid would vaporize, until equilibrium was reestablished
at the same vapor pressure, assuming the same temperature is maintained. In fact, the equi-
librium vapor pressure depends only on the temperature of the liquid; a higher temperature
causes a higher pressure, as the graph in Figure 12.31 indicates for the specifi c case of water. Only when the temperature and vapor pressure correspond to a point on the curved line, which
is called the vapor pressure curve or the vaporization curve, do liquid and vapor phases coexist at equilibrium.
To illustrate the use of a vaporization curve, let’s consider what happens when water
boils in a pot that is open to the air. Assume that the air pressure acting on the water is 1.01 × 105 Pa (one atmosphere). When boiling occurs, bubbles of water vapor form throughout
the liquid, rise to the surface, and break. For these bubbles to form and rise, the pressure
of the vapor inside them must at least equal the air pressure acting on the surface of the
water. According to Figure 12.31, a value of 1.01 × 105 Pa corresponds to a temperature of 100 °C. Consequently, water boils at 100 °C at one atmosphere of pressure. In general, a
liquid boils at the temperature for which its vapor pressure equals the external pressure. Water will not boil, then, at sea level if the temperature is only 83 °C, because at this tem-
perature the vapor pressure of water is only 0.53 × 105 Pa (see Figure 12.31), a value less than the external pressure of 1.01 × 105 Pa. However, water does boil at 83 °C on a moun-
tain at an altitude of just under five kilometers, because the atmospheric pressure there is
0.53 × 105 Pa.
The fact that water can boil at a temperature less than 100 °C leads to an interesting phenomenon
that Conceptual Example 15 discusses.
Temperature, °C
P re
ss ur
e, P
a
0.53 × 105
1.01 × 105
2 × 105
3 × 105
4 × 105
0 0–50 50 83 100 150
83 °C
100 °C
0.53 × 105 Pa
1.01 × 105 Pa
FIGURE 12.31 A plot of the equilibrium vapor pressure versus temperature is called the vapor pressure curve or the vaporization curve, the example shown being that for the liquid/vapor equilibrium of water.
(a)
Constant-temperature heated sand
(b)
Constant-temperature heated sand
INTERACTIVE FIGURE 12.30 (a) Some of the molecules begin entering the vapor
phase in the evacuated space above the liquid.
(b) Equilibrium is reached when the number of molecules entering the vapor phase equals
the number returning to the liquid.
348 CHAPTER 12 Temperature and Heat
THE PHYSICS OF . . . spray cans. The operation of spray cans is based on the equilib- rium between a liquid and its vapor. Figure 12.33a shows that a spray can contains a liquid pro- pellant that is mixed with the product (such as hair spray). Inside the can, propellant vapor forms
over the liquid. A propellant is chosen that has an equilibrium vapor pressure that is greater than
atmospheric pressure at room temperature. Consequently, when the nozzle of the can is pressed,
as in part b of the drawing, the vapor pressure forces the liquid propellant and product up the tube in the can and out the nozzle as a spray. When the nozzle is released, the coiled spring reseals the
can and the propellant vapor builds up once again to its equilibrium value.
CONCEPTUAL EXAMPLE 15 How to Boil Water That Is Cooling Down
Figure 12.32a shows water boiling in an open fl ask. Shortly after the fl ask is removed from the burner, the boiling stops. A cork is then placed in the
neck of the fl ask to seal it, and water is poured over the neck of the fl ask,
as in part b of the drawing. To restart the boiling, should the water poured over the neck be (a) cold or (b) hot—but not boiling?
Reasoning When the open fl ask is removed from the burner, the water begins to cool and the pressure above its surface is one atmosphere
(1.01 × 105 Pa). Boiling quickly stops, because water cannot boil when
its temperature is less than 100 °C and the pressure above its surface is
one atmosphere. To restart the boiling, it is necessary either to reheat
the water to 100 °C or reduce the pressure above the water in the corked
fl ask to something less than one atmosphere so that boiling can occur at a
temperature less than 100 °C.
Answer (b) is incorrect. Certainly, pouring hot water over the corked fl ask will reheat the water. However, since the water being poured is not
boiling, its temperature must be less than 100 °C. Therefore, it cannot
reheat the water within the fl ask to 100 °C and restart the boiling.
Answer (a) is correct. When cold water is poured over the corked fl ask, it causes some of the water vapor inside to condense. Consequently, the
pressure above the liquid in the fl ask drops. When it drops to the value
of the vapor pressure of the water in the fl ask at its current temperature
(which is now less than 100 °C), the boiling restarts.
(b) Water boiling again
Cork
Water
(a) Water boiling
FIGURE 12.32 (a) Water is boiling at a temperature of 100 °C and a pressure of
one atmosphere. (b) The water boils at a temperature that is less than 100 °C, because
the cool water reduces the pressure above the
water in the fl ask.
Nozzle
High-pressure propellant
vapor
Liquid propellant
plus product
Tube
Spray
Liquid propellant plus product
(a) (b)
FIGURE 12.33 (a) A closed spray can containing liquid and vapor in equilibrium. (b) An open spray can.
12.9 Equilibrium Between Phases of Matter 349
As is the case for liquid/vapor equilibrium, a solid can be in equilibrium with its liquid phase
only at specifi c conditions of temperature and pressure. For each temperature, there is a single pres-
sure at which the two phases can coexist in equilibrium. A plot of the equilibrium pressure versus
equilibrium temperature is referred to as the fusion curve, and Figure 12.34a shows a typical curve for a normal substance. A normal substance expands on melting (e.g., carbon dioxide and sulfur).
Since higher pressures make it more diffi cult for such materials to expand, a higher melting tem-
perature is needed for a higher pressure, and the fusion curve slopes upward to the right. Part b of the picture illustrates the fusion curve for water, one of the few substances that contract when they
melt. Higher pressures make it easier for such substances to melt. Consequently, a lower melting
temperature is associated with a higher pressure, and the fusion curve slopes downward to the right.
It should be noted that just because two phases can coexist in equilibrium does not neces-
sarily mean that they will. Other factors may prevent it. For example, water in an open bowl may never come into equilibrium with water vapor if air currents are present. Under such conditions
the liquid, perhaps at a temperature of 25 °C, attempts to establish the corresponding equilibrium
vapor pressure of 3.2 × 103 Pa. If air currents continually blow the water vapor away, however,
equilibrium will never be established, and eventually the water will evaporate completely. Each
kilogram of water that goes into the vapor phase takes along the latent heat of vaporization.
Because of this heat loss, the remaining liquid would become cooler, except for the fact that the
surroundings replenish the loss.
BIO THE PHYSICS OF . . . evaporative cooling of the human body. In the case of the human body, water is exuded by the sweat glands and evaporates from a much larger area than
the surface of a typical bowl of water. The removal of heat along with the water vapor is called
evaporative cooling and is one mechanism that the body uses to maintain its constant temperature.
Check Your Understanding
(The answers are given at the end of the book.) 15. A camping stove is used to boil water high on a mountain, where the atmospheric pressure is lower than
it is at sea level. Does it necessarily follow that the same stove can boil water at sea level?
16. BIO Medical instruments are sterilized at a high temperature in an autoclave, which is essentially a pressure cooker that heats the instruments in water under a pressure greater than one atmosphere. Why
is the water in an autoclave able to reach a very high temperature, while water in an open pot can only
be heated to 100 °C?
17. A jar is half fi lled with boiling water. The lid is then screwed on the jar. After the jar has cooled to room temperature, the lid is diffi cult to remove. Why? Ignore the thermal expansion and contraction of the
jar and the lid.
18. A bottle of carbonated soda (sealed and under a pressure greater than one atmosphere) is left outside in subfreezing temperatures, although the soda remains liquid. When the soda is brought inside and
opened immediately, it suddenly freezes. Why?
19. When a bowl of water is placed in a closed container and the water vapor is pumped away rapidly enough, why does the remaining liquid turn into ice?
Temperature, °CTemperature, °C
P re
ss ur
e, P
a
1.01 × 105
P re
ss ur
e, P
a
Fusion curve
(a)
Normal melting/freezing point of H2O
Solid
Solid
Liquid Liquid
(b)
0
FIGURE 12.34 (a) The fusion curve for a normal substance that expands on melting. (b) The fusion curve for water, one of the few substances that contract on melting.
350 CHAPTER 12 Temperature and Heat
12.10 *Humidity Air is a mixture of gases, including nitrogen, oxygen, and water vapor. The total pressure of the
mixture is the sum of the partial pressures of the component gases. The partial pressure of a gas is the pressure it would exert if it alone occupied the entire volume at the same temperature
as the mixture. The partial pressure of water vapor in air depends on weather conditions. It can
be as low as zero or as high as the equilibrium vapor pressure of water at the given temperature.
THE PHYSICS OF . . . relative humidity. To provide an indication of how much water vapor is in the air, weather forecasters usually give the relative humidity. If the relative humidity is too low, the air contains such a small amount of water vapor that skin and mucous membranes
tend to dry out. If the relative humidity is too high, especially on a hot day, we become very
uncomfortable and our skin feels “sticky.” Under such conditions, the air holds so much water
vapor that the water exuded by sweat glands cannot evaporate effi ciently. The relative humidity
is defi ned as the ratio (expressed as a percentage) of the actual partial pressure of water vapor in
the air to the equilibrium vapor pressure at a given temperature.
Partial pressure
of water vapor
Equilibrium vapor pressure of
water at the existing temperature
Percent
relative
humidity
= × 100 (12.6)
The term in the denominator on the right of Equation 12.6 is given by the vaporization curve of
water and is the pressure of the water vapor in equilibrium with the liquid. At a given temperature,
the partial pressure of the water vapor in the air cannot exceed this value. If it did, the vapor would
not be in equilibrium with the liquid and would condense as dew or rain to reestablish equilibrium.
When the partial pressure of the water vapor equals the equilibrium vapor pressure of water
at a given temperature, the relative humidity is 100%. In such a situation, the vapor is said to be
saturated because it is present in the maximum amount, as it would be above a pool of liquid at equilibrium in a closed container. If the relative humidity is less than 100%, the water vapor is
said to be unsaturated. Example 16 demonstrates how to fi nd the relative humidity.
Temperature, °C
P re
ss ur
e, P
a
2.5 × 103
4.8 × 103
0 0
21 32
FIGURE 12.35 The vaporization curve of water.
EXAMPLE 16 Relative Humidities
One day, the partial pressure of water vapor in the air is 2.0 × 103 Pa.
Using the vaporization curve for water in Figure 12.35, determine the relative humidity if the temperature is (a) 32 °C and (b) 21 °C.
Reasoning and Solution (a) According to Figure 12.35, the equilib- rium vapor pressure of water at 32 °C is 4.8 × 103 Pa. Equation 12.6
reveals that the relative humidity is
Relative humidity at 32 °C = 2.0 × 103 Pa
4.8 × 103 Pa ×100 = 42%
(b) A similar calculation shows that
Relative humidity at 21 °C = 2.0 × 103 Pa
2.5 × 103 Pa × 100 = 80%
THE PHYSICS OF . . . fog formation. When air containing a given amount of wa- ter vapor is cooled, a temperature is reached in which the partial pressure of the vapor equals
the equilibrium vapor pressure. This temperature is known as the dew point. For instance, Figure 12.36 shows that if the partial pressure of water vapor is 3.2 × 103 Pa, the dew point is 25 °C. This partial pressure would correspond to a relative humidity of 100%, if the ambient
temperature were equal to the dew-point temperature. Hence, the dew point is the temperature
below which water vapor in the air condenses in the form of liquid drops (dew or fog). The closer
12.10 Humidity 351
the actual temperature is to the dew point, the closer the relative humidity is to 100%. Thus, for
fog to form, the air temperature must drop below the dew point. Similarly, water condenses on the
outside of a cold glass when the temperature of the air next to the glass falls below the dew point.
THE PHYSICS OF . . . a home dehumidifi er. The cold coils in a home dehumidifi er function very much in the same way that the cold glass does. The coils are kept cold by a circu-
lating refrigerant (see Figure 12.37). When the air blown across them by the fan cools below the dew point, water vapor condenses in the form of droplets, which collect in a receptacle.
Check Your Understanding
(The answers are given at the end of the book.) 20. A bowl of water is covered tightly and allowed to sit at a constant temperature of 23 °C for a long time.
What is the relative humidity in the space between the surface of the water and the cover?
21. Is it possible for dew to form on Tuesday night and not on Monday night, even though Monday night is the cooler night?
22. Two rooms in a mansion have the same temperature. One of these rooms contains an indoor swimming pool. On a cold day the windows of one of the two rooms are “steamed up.” Which room is it likely to
be? Explain.
Temperature, °C
P re
ss ur
e, P
a
2 × 103
3.2 × 103
4 × 103
0 0
20 40
Dew point of 25 °C
FIGURE 12.36 On the vaporization curve of water, the dew point is the temperature
that corresponds to the actual partial pressure
of water vapor in the air.
Dehumidified air
Humid air
Cold coils
Circulating refrigerant Receptacle
Fan
FIGURE 12.37 The cold coils of a dehu- midifi er cool the air blowing across them
to below the dew point, and water vapor
condenses out of the air.
EXAMPLE 17 BIO Heating Up Your Brain
The human brain is a remarkable organ. It only requires approximately 20 W
of power to function normally. For comparison, a man-made computer pro-
cessor with the same computational power as your brain would consume
10–20 MW of power! With that being said, the brain is the most energy-
hungry organ in the human body. It only accounts for 1/50 of the body’s total
weight, but it requires 1/5 (20%) of the body’s total energy. This power out-
put from the brain produces heat, which raises the temperature of the brain
and the surrounding bone and tissues. The brain contains approximately
1.2 kg of water, which accounts for 77% of its total mass. If a human brain
was operating at a constant power output of 20 W for one hour, what would
be the increase in its temperature? Assume it is composed of only the 1.2 kg
of water, and no heat transfer occurs between the brain and its surroundings.
Reasoning We can calculate the change in temperature (ΔT) of the water inside the brain by knowing the total heat (Q) produced
in 1 hour. Equation 12.4 then provides the relationship between Q and ΔT.
Solution We can relate the power output of the brain to the total heat produced, since P = Q/t. Therefore, Q = Pt. Now we apply Equation 12.4: Q = mc ΔT. Substituting in for Q and solving for ΔT, we get the follow- ing: ΔT = Pt/mc = (20 W)(60 s)/(1.2 kg)(4186 J/(kg · C°) = 0.24 °C
Although this is a small temperature change, we have done the calcu-
lation assuming the entire brain has a high specifi c heat capacity equal to
that of water. The actual rise in temperature will be higher if we consider
the rest of the brain that is not water. Studies have shown that after beha-
vioral stimuli, it is not unusual to observe a 2–3 °C temperature increase
in the brain. This is a signifi cant change and must be controlled by the
body’s temperature regulation system that consists of the circulatory sys-
tem and the surface of the skin.
352 CHAPTER 12 Temperature and Heat
Concept Summary 12.1 Common Temperature Scales On the Celsius temperature scale, there are 100 equal divisions between the ice point (0 °C) and the steam point
(100 °C). On the Fahrenheit temperature scale, there are 180 equal divisions
between the ice point (32 °F) and the steam point (212 °F).
12.2 The Kelvin Temperature Scale For scientifi c work, the Kelvin tem- perature scale is the scale of choice. One kelvin (K) is equal in size to one
Celsius degree. However, the temperature T on the Kelvin scale diff ers from the temperature Tc on the Celsius scale by an additive constant of 273.15, as indicated by Equation 12.1. The lower limit of temperature is called absolute
zero and is designated as 0 K on the Kelvin scale.
T = Tc + 273.15 (12.1)
12.3 Thermometers The operation of any thermometer is based on the change in some physical property with temperature; this physical property is
called a thermometric property. Examples of thermometric properties are the
length of a column of mercury, electrical voltage, and electrical resistance.
12.4 Linear Thermal Expansion Most substances expand when heated. For linear expansion, an object of length L0 experiences a change ΔL in length when the temperature changes by ΔT, as shown in Equation 12.2, where 𝛼 is the coeffi cient of linear expansion.
ΔL = αL 0ΔT (12.2)
For an object held rigidly in place, a thermal stress can occur when the
object attempts to expand or contract. The stress can be large, even for small
temperature changes.
When the temperature changes, a hole in a plate of solid material expands
or contracts as if the hole were fi lled with the surrounding material.
12.5 Volume Thermal Expansion For volume expansion, the change ΔV in the volume of an object of volume V0 is given by Equation 12.3, where 𝛽 is the coeffi cient of volume expansion. When the temperature changes, a cavity
in a piece of solid material expands or contracts as if the cavity were fi lled
with the surrounding material.
ΔV = βV0 ΔT (12.3)
12.6 Heat and Internal Energy The internal energy of a substance is the sum of the kinetic, potential, and other kinds of energy that the molecules of
the substance have. Heat is energy that fl ows from a higher-temperature ob-
ject to a lower-temperature object because of the diff erence in temperatures.
The SI unit for heat is the joule (J).
12.7 Heat and Temperature Change: Specifi c Heat Capacity The heat Q that must be supplied or removed to change the temperature of a substance of mass m by an amount ΔT is given by Equation 12.4, where c is a constant known as the specifi c heat capacity.
Q = cm ΔT (12.4)
When materials are placed in thermal contact within a perfectly insulated
container, the principle of energy conservation requires that the amount of
heat lost by warmer materials equals the amount of heat gained by cooler
materials.
Heat is sometimes measured with a unit called the kilocalorie (kcal). The
conversion factor between kilocalories and joules is known as the mechanical
equivalent of heat: 1 kcal = 4186 joules.
12.8 Heat and Phase Change: Latent Heat Heat must be supplied or re- moved to make a material change from one phase to another. The heat Q that must be supplied or removed to change the phase of a mass m of a substance is given by Equation 12.5, where L is the latent heat of the substance and has SI units of J/kg. The latent heats of fusion, vaporization, and sublimation
refer, respectively, to the solid/liquid, the liquid/vapor, and the solid/vapor
phase changes.
Q = mL (12.5)
12.9 Equilibrium Between Phases of Matter The equilibrium vapor pressure of a substance is the pressure of the vapor phase that is in equilib-
rium with the liquid phase. For a given substance, vapor pressure depends
only on temperature. For a liquid, a plot of the equilibrium vapor pressure
versus temperature is called the vapor pressure curve or vaporization curve.
The fusion curve gives the combinations of temperature and pressure for
equilibrium between solid and liquid phases.
12.10 Humidity The relative humidity is defi ned as in Equation 12.6.
Partial pressure
of water vapor
Equilibrium vapor
pressure of water at the
existing temperature
Percent
relative
humidity = × 100
(12.6)
The dew point is the temperature below which the water vapor in the air
condenses. On the vaporization curve of water, the dew point is the temperature
that corresponds to the actual pressure of water vapor in the air.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 12.2 The Kelvin Temperature Scale 1. Which one of the following statements correctly describes the Celsius and the Kelvin temperature scales? (a) The size of the degree on the Celsius scale is larger than that on the Kelvin scale by a factor of 9/5. (b) Both scales assign the same temperature to the ice point, but they assign diff erent temperatures
to the steam point. (c) Both scales assign the same temperature to the steam point, but they assign diff erent temperatures to the ice point. (d) The Celsius scale assigns the same values to the ice and the steam points that the Kelvin
scale assigns. (e) The size of the degree on each scale is the same.
Section 12.4 Linear Thermal Expansion 2. The drawing shows two thin rods, one made from aluminum [𝛼 = 23 × 10−6 (C°)−1] and the other from steel [𝛼 = 12 × 10−6 (C°)−1]. Each rod has the
same length and the same initial temperature and is attached at one end to an
immovable wall, as shown. The temperatures of the rods are increased, both by
Focus on Concepts
Problems 353
the same amount, until the gap between
the rods is closed. Where do the rods meet
when the gap is closed? (a) The rods meet exactly at the midpoint. (b) The rods meet to the right of the midpoint. (c) The rods meet to the left of the midpoint.
4. A ball is slightly too large to fi t through a hole in a fl at plate. The draw-
ing shows two arrangements of this situ-
ation. In Arrangement I the ball is made
from metal A and the plate from metal
B. When both the ball and the plate are
cooled by the same number of Celsius
degrees, the ball passes through the hole. In Arrangement II the ball is also
made from metal A, but the plate is made from metal C. Here, the ball passes
through the hole when both the ball and the plate are heated by the same number
of Celsius degrees. Rank the coeffi cients of linear thermal expansion of metals
A, B, and C in descending order (largest fi rst): (a) 𝛼B, 𝛼A, 𝛼C (b) 𝛼B, 𝛼C, 𝛼A (c) 𝛼C, 𝛼B, 𝛼A (d) 𝛼C, 𝛼A, 𝛼B (e) 𝛼A, 𝛼B, 𝛼C
Section 12.5 Volume Thermal Expansion 6. A solid sphere and a solid cube are made from the same material. The sphere would just fi t within the cube, if it could. Both begin at the same
temperature, and both are heated to the same temperature. Which object,
if either, has the greater change in volume? (a) The sphere. (b) The cube. (c) Both have the same change in volume. (d) Insuffi cient information is given for an answer.
7. A container can be made from steel [𝛽 = 36 × 10−6 (C°)−1] or lead [𝛽 = 87 × 10−6 (C°)−1]. A liquid is poured into the container, fi lling it to the brim.
The liquid is either water [𝛽 = 207 × 10−6 (C°)−1] or ethyl alcohol [𝛽 = 1120 × 10−6 (C°)−1]. When the full container is heated, some liquid spills out. To
keep the overfl ow to a minimum, from what material should the container
be made and what should the liquid be? (a) Lead, water (b) Steel, water (c) Lead, ethyl alcohol (d) Steel, ethyl alcohol
Section 12.7 Heat and Temperature Change: Specific Heat Capacity 9. Which of the following cases (if any) requires the greatest amount of heat? In each case the material is the same. (a) 1.5 kg of the material is to be heated by 7.0 C°. (b) 3.0 kg of the material is to be heated by 3.5 C°. (c) 0.50 kg of the material is to be heated by 21 C°. (d) 0.75 kg of the material is to be heated by 14 C°. (e) The amount of heat required is the same in each of the four previous cases.
10. The following three hot samples have the same temperature. The same amount of heat is removed from each sample. Which one experiences the
smallest drop in temperature, and which one experiences the largest drop?
Sample A. 4.0 kg of water [c = 4186 J/(kg · C°)] Sample B. 2.0 kg of oil [c = 2700 J/(kg · C°)] Sample C. 9.0 kg of dirt [c = 1050 J/(kg · C°)] (a) C smallest and A largest (b) B smallest and C largest (c) A smallest and B largest (d) C smallest and B largest (e) B smallest and A largest
Section 12.8 Heat and Phase Change: Latent Heat 13. The latent heat of fusion for water is 33.5 × 104 J/kg, while the latent heat of vaporization is 22.6 × 105 J/kg. What mass m of water must be frozen in order to release the amount of heat that 1.00 kg of steam releases when it
condenses?
Section 12.9 Equilibrium Between Phases of Matter 15. Which one or more of the following techniques can be used to freeze water?
A. Cooling the water below its normal freezing point of 0 °C at the normal atmospheric pressure of 1.01 × 105 Pa
B. Cooling the water below its freezing point of −1 °C at a pressure greater than 1.01 × 105 Pa
C. Rapidly pumping away the water vapor above the liquid in an insulated container (The insulation prevents heat fl owing from the surroundings into the remaining liquid.)
(a) Only A (b) Only B (c) Only A and B (d) A, B, and C (e) Only C
Section 12.10 Humidity 17. Which of the following three statements concerning relative humidity val- ues of 30% and 40% are true? Note that when the relative humidity is 30%, the
air temperature may be diff erent than it is when the relative humidity is 40%.
A. It is possible that at a relative humidity of 30% there is a smaller partial pressure of water vapor in the air than there is at a relative humidity of 40%.
B. It is possible that there is the same partial pressure of water vapor in the air at 30% and at 40% relative humidity.
C. It is possible that at a relative humidity of 30% there is a greater partial pressure of water vapor in the air than there is at a relative humidity of 40%.
(a) A, B, and C (b) Only A and B (c) Only A and C (d) Only B and C (e) Only A
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details. Note: For problems in this set, use the values of 𝛼 and 𝛽 in Table 12.1, and the values of c, Lf, and Lv in Tables 12.2 and 12.3, unless stated otherwise.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 12.1 Common Temperature Scales,
Section 12.2 The Kelvin Temperature Scale,
Section 12.3 Thermometers
1. E SSM Suppose you are hiking down the Grand Canyon. At the top, the temperature early in the morning is a cool 3 °C. By late afternoon, the tem-
perature at the bottom of the canyon has warmed to a sweltering 34 °C. What
is the diff erence between the higher and lower temperatures in (a) Fahrenheit degrees and (b) kelvins?
Problems
Aluminum
Midpoint
Steel
QUESTION 2
Arrangement I Arrangement II
B C
A A
QUESTION 4
354 CHAPTER 12 Temperature and Heat
2. E You are sick, and your temperature is 312.0 kelvins. Convert this tem- perature to the Fahrenheit scale.
3. E On the moon the surface temperature ranges from 375 K during the day to 1.00 × 102 K at night. What are these temperatures on the (a) Celsius and (b) Fahrenheit scales? 4. E BIO What’s your normal body temperature? It may not be 98.6 °F, the often-quoted average that was determined in the nineteenth century. A more
recent study has reported an average temperature of 98.2 °F. What is the dif- ference between these averages, expressed in Celsius degrees? 5. E BIO SSM Dermatologists often remove small precancerous skin lesions by freezing them quickly with liquid nitrogen, which has a tempera-
ture of 77 K. What is this temperature on the (a) Celsius and (b) Fahrenheit scales?
6. E GO The drawing shows two thermometers, A and B, whose temper- atures are measured in °A and °B. The ice and boiling points of water are
also indicated. (a) Using the data in the drawing, determine the number of B degrees on the B scale that correspond to 1 A° on the A scale. (b) If the temperature of a substance reads +40.0 °A on the A scale, what would that
temperature read on the B scale?
PROBLEM 6
–30.0 °A
Boiling point
Ice point
A B
+60.0 °A +130.0 °B
+20.0 °B
7. M GO A copper–constantan thermocouple generates a voltage of 4.75 × 10−3 volts when the temperature of the hot junction is 110.0 °C and the refer-
ence junction is kept at a temperature of 0.0 °C. If the voltage is proportional
to the diff erence in temperature between the junctions, what is the temperat-
ure of the hot junction when the voltage is 1.90 × 10−3 volts?
8. M V-HINT If a nonhuman civilization were to develop on Saturn’s largest moon, Titan, its scientists might well devise a temperature scale based on
the properties of methane, which is much more abundant on the surface than
water is. Methane freezes at −182.6 °C on Titan, and boils at −155.2 °C.
Taking the boiling point of methane as 100.0 °M (degrees Methane) and its
freezing point as 0 °M, what temperature on the Methane scale corresponds
to the absolute zero point of the Kelvin scale?
9. M SSM Available in WileyPLUS.
Section 12.4 Linear Thermal Expansion 10. E A steel section of the Alaskan pipeline had a length of 65 m and a temperature of 18 °C when it was installed. What is its change in length when
the temperature drops to a frigid −45 °C?
11. E SSM A steel aircraft carrier is 370 m long when moving through the icy North Atlantic at a temperature of 2.0 °C. By how much does the carrier
lengthen when it is traveling in the warm Mediterranean Sea at a temperature
of 21 °C?
12. E The Eiff el Tower is a steel structure whose height increases by 19.4 cm when the temperature changes from −9 to +41 °C. What is the ap-
proximate height (in meters) at the lower temperature?
13. E Conceptual Example 5 provides background for this problem. A hole is drilled through a copper plate whose temperature is 11 °C. (a) When the
temperature of the plate is increased, will the radius of the hole be larger
or smaller than the radius at 11 °C? Why? (b) When the plate is heated to 110 °C, by what fraction Δr/r0 will the radius of the hole change? 14. E A commonly used method of fastening one part to another part is called “shrink fi tting.” A steel rod has a diameter of 2.0026 cm, and a fl at
plate contains a hole whose diameter is 2.0000 cm. The rod is cooled so that
it just fi ts into the hole. When the rod warms up, the enormous thermal stress
exerted by the plate holds the rod securely to the plate. By how many Celsius
degrees should the rod be cooled?
15. E SSM When the temperature of a coin is raised by 75 C°, the coin’s diameter increases by 2.3 × 10−5 m. If the original diameter of the coin is
1.8 × 10−2 m, fi nd the coeffi cient of linear expansion.
16. E One January morning in 1943, a warm chinook wind rapidly raised the temperature in Spearfi sh, South Dakota, from below freezing to +12.0 °C.
As the chinook died away, the temperature fell to −20.0 °C in 27.0 minutes.
Suppose that a 19-m aluminum fl agpole were subjected to this temperature
change. Find the average speed at which its height would decrease, assuming
the fl agpole responded instantaneously to the changing temperature.
17. E GO One rod is made from lead and another from quartz. The rods are heated and experience the same change in temperature. The change in length
of each rod is the same. If the initial length of the lead rod is 0.10 m, what is
the initial length of the quartz rod?
18. M GO A thin rod consists of two parts joined together. One-third of it is silver and two-thirds is gold. The temperature decreases by 26 C°.
Determine the fractional decrease ∆L
L 0, Silver + L 0, Gold in the rod’s length,
where L0, Silver and L0, Gold are the initial lengths of the silver and gold rods. 19. M CHALK The brass bar and the aluminum bar in the drawing are each attached to an immovable wall. At 28 °C the air gap between the rods is
1.3 × 10−3 m. At what temperature will the gap be closed?
PROBLEM 19
Aluminum
1.0 m
Brass
2.0 m
20. M V-HINT Multiple-Concept Example 4 reviews the concepts that are involved in this problem. A ruler is accurate when the temperature is 25 °C.
When the temperature drops to −14 °C, the ruler shrinks and no longer meas-
ures distances accurately. However, the ruler can be made to read correctly
if a force of magnitude 1.2 × 103 N is applied to each end so as to stretch
it back to its original length. The ruler has a cross-sectional area of 1.6 ×
10−5 m2, and it is made from a material whose coeffi cient of linear expansion
is 2.5 × 10−5 (C°)−1. What is Young’s modulus for the material from which
the ruler is made?
21. M SSM A simple pendulum consists of a ball connected to one end of a thin brass wire. The period of the pendulum is 2.0000 s. The temperature
rises by 140 C°, and the length of the wire increases. Determine the period
of the heated pendulum.
22. M V-HINT As the drawing shows, two thin strips of metal are bolted to- gether at one end; both have the same temperature. One is steel, and the other
is aluminum. The steel strip is 0.10% longer than the aluminum strip. By how
much should the temperature of the strips be increased, so that the strips have
the same length?
PROBLEM 22
Steel
Aluminum
23. M Available in WileyPLUS. 24. M GO Consult Multiple-Concept Example 4 for insight into solving this problem. A copper rod is fastened securely at both ends to immovable
Problems 355
supports. When this rod is stretched, it will rupture when a tensile stress
of 2.3 × 107 N/m2 is applied at each end. The rod just fi ts between the
supports, so initially there is no stress applied to the rod. The rod is then
cooled. What is the magnitude |ΔT | of the change in temperature of the rod when it ruptures?
25. M GO A ball and a thin plate are made from diff erent materials and have the same initial temperature. The ball does not fi t through a hole in the
plate, because the diameter of the ball is slightly larger than the diameter of
the hole. However, the ball will pass through the hole when the ball and the
plate are both heated to a common higher temperature. In each of the arrange-
ments in the drawing the diameter of the ball is 1.0 × 10−5 m larger than the
diameter of the hole in the thin plate, which has a diameter of 0.10 m. The
initial temperature of each arrangement is 25.0 °C. At what temperature will
the ball fall through the hole in each arrangement?
Arrangement A
Gold
Arrangement B Arrangement C
Quartz
Lead Aluminum
Silver
Steel
PROBLEM 25
26. H An 85.0-N backpack is hung from the middle of an aluminum wire, as the drawing shows. The temperature of the wire then drops by
20.0 C°. Find the tension in the wire at the lower temperature. Assume
that the distance between the supports does not change, and ignore any
thermal stress.
3.00° 3.00°
L0L0
PROBLEM 26
27. H SSM Available in WileyPLUS.
Section 12.5 Volume Thermal Expansion 28. E A fl ask is fi lled with 1.500 L (L = liter) of a liquid at 97.1 °C. When the liquid is cooled to 15.0 °C, its volume is only 1.383 L, however. Neglect
the contraction of the fl ask and use Table 12.1 to identify the liquid. 29. E MMH A thin spherical shell of silver has an inner radius of 2.0 × 10−2 m when the temperature is 18 °C. The shell is heated to 147 °C. Find the change
in the interior volume of the shell.
30. E A test tube contains 2.54 × 10−4 m3 of liquid carbon tetrachloride at a temperature of 75.0 °C. The test tube and the carbon tetrachloride are
cooled to a temperature of −13.0 °C, which is above the freezing point of
carbon tetrachloride. Find the volume of carbon tetrachloride in the test tube
at −13.0 °C.
31. E SSM A copper kettle contains water at 24 °C. When the water is heated to its boiling point of 100.0 °C, the volume of the kettle expands by
1.2 × 10−5 m3. Determine the volume of the kettle at 24 °C.
32. E Suppose you are selling apple cider for two dollars a gallon when the temperature is 4.0 °C. The coeffi cient of volume expansion of the cider
is 280 × 10−6 (C°)−1. How much more money (in pennies) would you make
per gallon by refi lling the container on a day when the temperature is 26 °C?
Ignore the expansion of the container.
33. E MMH During an all-night cram session, a student heats up a one-half liter (0.50 × 10−3 m3) glass (Pyrex) beaker of cold coff ee. Initially, the
temperature is 18 °C, and the beaker is fi lled to the brim. A short time later
when the student returns, the temperature has risen to 92 °C. The coeffi cient
of volume expansion of coff ee is the same as that of water. How much coff ee
(in cubic meters) has spilled out of the beaker?
34. E MMH Many hot-water heating systems have a reservoir tank connec- ted directly to the pipeline, to allow for expansion when the water becomes
hot. The heating system of a house has 76 m of copper pipe whose inside
radius is 9.5 × 10−3 m. When the water and pipe are heated from 24 to 78 °C,
what must be the minimum volume of the reservoir tank to hold the overfl ow
of water?
35. E SSM Suppose that the steel gas tank in your car is completely fi lled when the temperature is 17 °C. How many gallons will spill out of the
twenty-gallon tank when the temperature rises to 35 °C?
36. E GO An aluminum can is fi lled to the brim with a liquid. The can and the liquid are heated so their temperatures change by the same amount.
The can’s initial volume at 5 °C is 3.5 × 10−4 m3. The coeffi cient of volume
expansion for aluminum is 69 × 10−6 (C°)−1. When the can and the liquid are
heated to 78 °C, 3.6 × 10−6 m3 of liquid spills over. What is the coeffi cient of
volume expansion of the liquid?
37. M V-HINT A spherical brass shell has an interior volume of 1.60 × 10−3 m3. Within this interior volume is a solid steel ball that has a volume of
0.70 × 10−3 m3. The space between the steel ball and the inner surface of the
brass shell is fi lled completely with mercury. A small hole is drilled through
the brass, and the temperature of the arrangement is increased by 12 C°.
What is the volume of the mercury that spills out of the hole?
38. M GO At the bottom of an old mercury-in-glass thermometer is a 45-mm3 reservoir fi lled with mercury. When the thermometer was placed
under your tongue, the warmed mercury would expand into a very narrow
cylindrical channel, called a capillary, whose radius was 1.7 × 10−2 mm.
Marks were placed along the capillary that indicated the temperature.
Ignore the thermal expansion of the glass and determine how far (in
mm) the mercury would expand into the capillary when the temperature
changed by 1.0 C°.
39. M SSM The bulk modulus of water is B = 2.2 × 109 N/m2. What change in pressure ΔP (in atmospheres) is required to keep water from expanding when it is heated from 15 to 25 °C?
40. M GO The density of mercury is 13 600 kg/m3 at 0 °C. What would its density be at 166 °C?
41. H SSM Two identical thermometers made of Pyrex glass contain, re- spectively, identical volumes of mercury and methyl alcohol. If the expan-
sion of the glass is taken into account, how many times greater is the distance
between the degree marks on the methyl alcohol thermometer than the dis-
tance on the mercury thermometer?
42. H The column of mercury in a barometer (see Figure 11.11) has a height of 0.760 m when the pressure is one atmosphere and the temperature
is 0.0 °C. Ignoring any change in the glass containing the mercury, what will
be the height of the mercury column for the same one atmosphere of pressure
when the temperature rises to 38.0 °C on a hot day? (Hint: The pressure in the barometer is given by Pressure = ρgh, and the density ρ of the mercury changes when the temperature changes.)
Section 12.6 Heat and Internal Energy,
Section 12.7 Heat and Temperature Change: Specific Heat Capacity 43. E SSM Ideally, when a thermometer is used to measure the temperature of an object, the temperature of the object itself should not change. However,
if a signifi cant amount of heat fl ows from the object to the thermometer, the
temperature will change. A thermometer has a mass of 31.0 g, a specifi c heat
356 CHAPTER 12 Temperature and Heat
capacity of c = 815 J/(kg · C°), and a temperature of 12.0 °C. It is immersed in 119 g of water, and the fi nal temperature of the water and thermometer is
41.5 °C. What was the temperature of the water before the insertion of the
thermometer?
44. E SSM Blood can carry excess energy from the interior to the surface of the body, where the energy is dispersed in a number of ways. While a person
is exercising, 0.6 kg of blood fl ows to the body’s surface and releases 2000 J
of energy. The blood arriving at the surface has the temperature of the body’s
interior, 37.0 °C. Assuming that blood has the same specifi c heat capacity
as water, determine the temperature of the blood that leaves the surface and
returns to the interior.
45. E An ice chest at a beach party contains 12 cans of soda at 5.0 °C. Each can of soda has a mass of 0.35 kg and a specifi c heat capacity of 3800
J/(kg · C°). Someone adds a 6.5-kg watermelon at 27 °C to the chest. The specifi c heat capacity of watermelon is nearly the same as that of water.
Ignore the specifi c heat capacity of the chest and determine the fi nal temper-
ature T of the soda and watermelon.
46. E A piece of glass has a temperature of 83.0 °C. Liquid that has a tem- perature of 43.0 °C is poured over the glass, completely covering it, and the
temperature at equilibrium is 53.0 °C. The mass of the glass and the liquid
is the same. Ignoring the container that holds the glass and liquid and
assuming that the heat lost to or gained from the surroundings is negligible,
determine the specifi c heat capacity of the liquid.
47. E BIO MMH When resting, a person has a metabolic rate of about 3.0 × 105 joules per hour. The person is submerged neck-deep into a tub containing
1.2 × 103 kg of water at 21.00 °C. If the heat from the person goes only into
the water, fi nd the water temperature after half an hour.
48. E GO Two bars of identical mass are at 25 °C. One is made from glass and the other from another substance. The specifi c heat capacity of glass is
840 J/(kg · C°). When identical amounts of heat are supplied to each, the glass bar reaches a temperature of 88 °C, while the other bar reaches 250.0 °C.
What is the specifi c heat capacity of the other substance?
49. E SSM At a fabrication plant, a hot metal forging has a mass of 75 kg and a specifi c heat capacity of 430 J/(kg · C°). To harden it, the forging is immersed in 710 kg of oil that has a temperature of 32 °C and
a specifi c heat capacity of 2700 J/(kg · C°). The fi nal temperature of the oil and forging at thermal equilibrium is 47 °C. Assuming that heat fl ows
only between the forging and the oil, determine the initial temperature of
the forging.
50. E BIO GO When you drink cold water, your body must expend meta- bolic energy in order to maintain normal body temperature (37 °C) by warm-
ing up the water in your stomach. Could drinking ice water, then, substitute
for exercise as a way to “burn calories?” Suppose you expend 430 kilocalories
during a brisk hour-long walk. How many liters of ice water (0 °C) would you
have to drink in order to use up 430 kilocalories of metabolic energy? For
comparison, the stomach can hold about 1 liter.
51. M MMH A 0.35-kg coff ee mug is made from a material that has a spe- cifi c heat capacity of 920 J/(kg · C°) and contains 0.25 kg of water. The cup and water are at 15 °C. To make a cup of coff ee, a small electric heater is im-
mersed in the water and brings it to a boil in three minutes. Assume that the
cup and water always have the same temperature and determine the minimum
power rating of this heater.
52. M GO Three portions of the same liquid are mixed in a container that prevents the exchange of heat with the environment. Portion A has a mass m and a temperature of 94.0 °C, portion B also has a mass m but a temperat- ure of 78.0 °C, and portion C has a mass mC and a temperature of 34.0 °C. What must be the mass of portion C so that the fi nal temperature Tf of the three-portion mixture is Tf = 50.0 °C? Express your answer in terms of m; for example, mC = 2.20 m.
53. M BIO MMH One ounce of a well-known breakfast cereal contains 110 Calories (1 food Calorie = 4186 J). If 2.0% of this energy could be converted
by a weight lifter’s body into work done in lifting a barbell, what is the heav-
iest barbell that could be lifted a distance of 2.1 m?
54. M V-HINT The heating element of a water heater in an apartment build- ing has a maximum power output of 28 kW. Four residents of the building
take showers at the same time, and each receives heated water at a volume
fl ow rate of 14 × 10−5 m3/s. If the water going into the heater has a temperat-
ure of 11 °C, what is the maximum possible temperature of the hot water that
each showering resident receives?
55. M SSM A rock of mass 0.20 kg falls from rest from a height of 15 m into a pail containing 0.35 kg of water. The rock and water have the same initial
temperature. The specifi c heat capacity of the rock is 1840 J/(kg · C°). Ignore the heat absorbed by the pail itself, and determine the rise in the temperature
of the rock and water.
56. H A steel rod (ρ = 7860 kg/m3) has a length of 2.0 m. It is bolted at both ends between immobile supports. Initially there is no tension in the rod,
because the rod just fi ts between the supports. Find the tension that develops
when the rod loses 3300 J of heat.
Section 12.8 Heat and Phase Change: Latent Heat 57. E SSM How much heat must be added to 0.45 kg of aluminum to change it from a solid at 130 °C to a liquid at 660 °C (its melting point)? The latent
heat of fusion for aluminum is 4.0 × 105 J/kg.
58. E Suppose that the amount of heat removed when 3.0 kg of water freezes at 0.0 °C were removed from ethyl alcohol at its freezing/melting
point of −114.4 °C. How many kilograms of ethyl alcohol would freeze?
59. E To help prevent frost damage, fruit growers sometimes protect their crop by spraying it with water when overnight temperatures are ex-
pected to go below freezing. When the water turns to ice during the night,
heat is released into the plants, thereby giving a measure of protection
against the cold. Suppose a grower sprays 7.2 kg of water at 0 °C onto a
fruit tree. (a) How much heat is released by the water when it freezes? (b) How much would the temperature of a 180-kg tree rise if it absorbed the heat released in part (a)? Assume that the specifi c heat capacity of the
tree is 2.5 × 103 J/(kg · C°) and that no phase change occurs within the tree itself.
60. E GO (a) Objects A and B have the same mass of 3.0 kg. They melt when 3.0 × 104 J of heat is added to object A and when 9.0 × 104 J is added
to object B. Determine the latent heat of fusion for the substance from which
each object is made. (b) Find the heat required to melt object A when its mass is 6.0 kg.
61. E SSM Find the mass of water that vaporizes when 2.10 kg of mercury at 205 °C is added to 0.110 kg of water at 80.0 °C.
62. E A mass m = 0.054 kg of benzene vapor at its boiling point of 80.1 °C is to be condensed by mixing the vapor with water at 41 °C. What is the
minimum mass of water required to condense all of the benzene vapor? As-
sume that the mixing and condensation take place in a perfectly insulating
container.
63. E BIO The latent heat of vaporization of H2O at body temperature (37.0 °C) is 2.42 × 106 J/kg. To cool the body of a 75-kg jogger [average
specifi c heat capacity = 3500 J/(kg · C°)] by 1.5 C°, how many kilograms of water in the form of sweat have to be evaporated?
64. E A certain quantity of steam has a temperature of 100.0 °C. To convert this steam into ice at 0.0 °C, energy in the form of heat must be removed from
the steam. If this amount of energy were used to accelerate the ice from rest,
what would be the linear speed of the ice? For comparison, bullet speeds of
about 700 m/s are common.
Problems 357
65. E A thermos contains 150 cm3 of coff ee at 85 °C. To cool the coff ee, you drop two 11-g ice cubes into the thermos. The ice cubes are initially at
0 °C and melt completely. What is the fi nal temperature of the coff ee? Treat
the coff ee as if it were water.
66. M V-HINT A snow maker at a resort pumps 130 kg of lake water per minute and sprays it into the air above a ski run. The water droplets freeze in
the air and fall to the ground, forming a layer of snow. If all the water pumped
into the air turns to snow, and the snow cools to the ambient air temperature of
−7.0 °C, how much heat does the snow-making process release each minute?
Assume that the temperature of the lake water is 12.0 °C, and use 2.00 ×
103 J/(kg ⋅ C°) for the specifi c heat capacity of snow.
67. M SSM CHALK MMH A 42-kg block of ice at 0 °C is sliding on a hori- zontal surface. The initial speed of the ice is 7.3 m/s and the fi nal speed is
3.5 m/s. Assume that the part of the block that melts has a very small mass
and that all the heat generated by kinetic friction goes into the block of ice.
Determine the mass of ice that melts into water at 0 °C.
68. M GO Water at 23.0 °C is sprayed onto 0.180 kg of molten gold at 1063 °C (its melting point). The water boils away, forming steam at 100.0 °C
and leaving solid gold at 1063 °C. What is the minimum mass of water that
must be used?
69. M SSM An unknown material has a normal melting/freezing point of −25.0 °C, and the liquid phase has a specifi c heat capacity of 160 J/(kg · C°). One-tenth of a kilogram of the solid at −25.0 °C is put into a 0.150-kg
aluminum calorimeter cup that contains 0.100 kg of glycerin. The tempera-
ture of the cup and the glycerin is initially 27.0 °C. All the unknown material
melts, and the fi nal temperature at equilibrium is 20.0 °C. The calorimeter
neither loses energy to nor gains energy from the external environment. What
is the latent heat of fusion of the unknown material?
70. M GO When it rains, water vapor in the air condenses into liquid water, and energy is released. (a) How much energy is released when 0.0254 m (one inch) of rain falls over an area of 2.59 × 106 m2 (one square mile)?
(b) If the average energy needed to heat one home for a year is 1.50 × 1011 J, how many homes could be heated for a year with the energy determined in
part (a)?
71. M SSM It is claimed that if a lead bullet goes fast enough, it can melt completely when it comes to a halt suddenly, and all its kinetic energy is con-
verted into heat via friction. Find the minimum speed of a lead bullet (initial
temperature = 30.0 °C) for such an event to happen.
72. M V-HINT Equal masses of two diff erent liquids have the same temperat- ure of 25.0 °C. Liquid A has a freezing point of −68.0 °C and a specifi c heat
capacity of 1850 J/(kg · C°). Liquid B has a freezing point of −96.0 °C and a specifi c heat capacity of 2670 J/(kg · C°). The same amount of heat must be removed from each liquid in order to freeze it into a solid at its respective
freezing point. Determine the diff erence Lf, A − Lf, B between the latent heats of fusion for these liquids.
73. M CHALK Occasionally, huge icebergs are found fl oating on the ocean’s currents. Suppose one such iceberg is 120 km long, 35 km wide, and 230 m
thick. (a) How much heat would be required to melt this iceberg (assumed to be at 0 °C) into liquid water at 0 °C? The density of ice is 917 kg/m3.
(b) The annual energy consumption by the United States is about 1.1 × 1020 J. If this energy were delivered to the iceberg every year, how many years
would it take before the ice melted?
Section 12.9 Equilibrium Between Phases of Matter,
Section 12.10 Humidity 74. E What atmospheric pressure would be required for carbon dioxide to boil at a temperature of 20 °C? See the vapor pressure curve for carbon
dioxide in the drawing.
PROBLEM 74 Temperature, °C
P re
ss ur
e, P
a
–50 500 0
2 × 106
4 × 106
6 × 106
8 × 106
75. E SSM At a temperature of 10 °C the percent relative humidity is R10, and at 40 °C it is R40. At each of these temperatures the partial pressure of water vapor in the air is the same. Using the vapor pressure curve for water
that accompanies this problem, determine the ratio R10/R40 of the two humid- ity values.
PROBLEM 75 0 10 20 30 40 50
0
1000
2000
3000
4000
Temperature, °C
Va po
r pr
es su
re o
f w
at er
, P a
5000
6000
7000
8000
76. E What is the relative humidity on a day when the temperature is 30 °C and the dew point is 10 °C? Use the vapor pressure curve that accompanies
Problem 75.
77. E BIO Suppose that air in the human lungs has a temperature of 37 °C, and the partial pressure of water vapor has a value of 5.5 × 103 Pa. What is
the relative humidity in the lungs? Consult the vapor pressure curve for water
that accompanies Problem 75.
78. E GO The vapor pressure of water at 10 °C is 1300 Pa. (a) What per- centage of atmospheric pressure is this? Take atmospheric pressure to be
1.013 × 105 Pa. (b) What percentage of the total air pressure at 10 °C is due to water vapor when the relative humidity is 100%? (c) The vapor pressure of water at 35 °C is 5500 Pa. What is the relative humidity at this temperature
if the partial pressure of water in the air has not changed from what it was at
10 °C when the relative humidity was 100%?
79. E GO The temperature of 2.0 kg of water is 100.0 °C, but the water is not boiling, because the external pressure acting on the water surface is
3.0 × 105 Pa. Using the vapor pressure curve for water given in Figure 12.31,
determine the amount of heat that must be added to the water to bring it to
the point where it just begins to boil.
80. M Available in WileyPLUS. 81. M SSM Available in WileyPLUS. 82. M Available in WileyPLUS. 83. M V-HINT Available in WileyPLUS. 84. H Available in WileyPLUS.
358 CHAPTER 12 Temperature and Heat
85. E An aluminum baseball bat has a length of 0.86 m at a temperature of 17 °C. When the temperature of the bat is raised, the bat lengthens by
0.000 16 m. Determine the fi nal temperature of the bat.
86. E BIO A person eats a container of strawberry yogurt. The Nutritional Facts label states that it contains 240 Calories (1 Calorie = 4186 J). What
mass of perspiration would one have to lose to get rid of this energy? At body
temperature, the latent heat of vaporization of water is 2.42 × 106 J/kg.
87. E SSM Available in WileyPLUS. 88. E A 0.200-kg piece of aluminum that has a temperature of −155 °C is added to 1.5 kg of water that has a temperature of 3.0 °C. At equilibrium
the temperature is 0.0 °C. Ignoring the container and assuming that the heat
exchanged with the surroundings is negligible, determine the mass of water
that has been frozen into ice.
89. E A thick, vertical iron pipe has an inner diameter of 0.065 m. A thin aluminum disk, heated to a temperature of 85 °C, has a diameter that is
3.9 × 10−5 m greater than the pipe’s inner diameter. The disk is laid on top of
the open upper end of the pipe, perfectly centered on it, and allowed to cool.
What is the temperature of the aluminum disk when the disk falls into the
pipe? Ignore the temperature change of the pipe.
90. E Available in WileyPLUS. 91. E SSM A lead object and a quartz object each have the same initial volume. The volume of each increases by the same amount, because the tem-
perature increases. If the temperature of the lead object increases by 4.0 C°,
by how much does the temperature of the quartz object increase?
92. E GO If the price of electrical energy is $0.10 per kilowatt ⋅ hour, what is the cost of using electrical energy to heat the water in a swimming pool
(12.0 m × 9.00 m × 1.5 m) from 15 to 27 °C?
93. M Concrete sidewalks are always laid in sections, with gaps between each section. For example, the drawing shows three identical 2.4-m sections,
the outer two of which are against immovable walls. The two identical gaps
between the sections are provided so that thermal expansion will not create
the thermal stress that could lead to cracks. What is the minimum gap width
necessary to account for an increase in temperature of 32 C°?
PROBLEM 93 Gap
2.4 m
94. M GO A constant-volume gas thermometer (see Figures 12.3 and 12.4) has a pressure of 5.00 × 103 Pa when the gas temperature is 0.00 °C. What is
the temperature (in °C) when the pressure is 2.00 × 103 Pa?
95. M SSM Available in WileyPLUS. 96. M V-HINT Available in WileyPLUS. 97. M When 4200 J of heat are added to a 0.15-m-long silver bar, its length increases by 4.3 × 10−3 m. What is the mass of the bar?
98. M V-HINT Available in WileyPLUS. 99. M SSM Available in WileyPLUS. 100. H A wire is made by attaching two segments together, end to end. One segment is made of aluminum and the other is steel. The eff ective coeffi cient
of linear expansion of the two-segment wire is 19 × 10−6 (C°)−1. What frac-
tion of the length is aluminum?
101. H An insulated container is partly fi lled with oil. The lid of the con- tainer is removed, 0.125 kg of water heated to 90.0 °C is poured in, and the
lid is replaced. As the water and the oil reach equilibrium, the volume of the
oil increases by 1.20 × 10−5 m3. The density of the oil is 924 kg/m3, its spe-
cifi c heat capacity is 1970 J/(kg · C°), and its coeffi cient of volume expansion is 721 × 10−6 (C°)−1. What is the temperature when the oil and the water
reach equilibrium?
102. H A steel bicycle wheel (without the rubber tire) is rotating freely with an angular speed of 18.00 rad/s. The temperature of the wheel changes from
−100.0 to +300.0 °C. No net external torque acts on the wheel, and the mass
of the spokes is negligible. (a) Does the angular speed increase or decrease as the wheel heats up? Why? (b) What is the angular speed at the higher temperature?
103. M GO SSM The fi gure shows a swimming pool on a sunny day. If the water absorbs 2.00 × 109 J of heat from the sun, what is the change in volume
of the water?
Additional Problems
Q
© L
H B
P h o to
/A la
m y
PROBLEM 103
Problem 104 provides insight on the variables involved when the length and
volume of an object change due to a temperature change. Problem 105 dis-
cusses how diff erent factors aff ect the temperature change of an object to
which heat is being added.
104. M CHALK The fi gure shows three rectangular blocks made from the same material. The initial dimensions of each are expressed as multiples of D, where D = 2.00 cm. The blocks are heated and their temperatures increase by 35.0 C°. The coeffi cients of linear and volume expansion are 𝛼 = 1.50 × 10−5 (C°)−1
Concepts and Calculations Problems
Team Problems 359
and 𝛽 = 4.50 × 10−5 (C°)−1, respectively. Concepts: (i) Does the change in the vertical height of a block depend only on its height, or does it also depend on
its width and depth? Without doing any calculations, rank the blocks according
to their change in height, largest fi rst. (ii) Does the change in the volume of a
block depend only on its height, or does it also depend on its width and depth?
Without doing any calculations, rank the blocks according to their change in
volume, largest fi rst. Calculations: Determine the change in the (a) vertical heights and (b) volumes of the blocks.
PROBLEM 104 2D 2DD
A B C2D
2D
D
D D
2D
105. M CHALK SSM Objects A and B in the fi gure are made from copper, but the mass of object B is three times that of object A. Object C is made from
glass and has the same mass as object B. The same amount of heat Q is sup- plied to each one: Q = 14 J. Concepts: (i) Which object, A or B, experiences a greater rise in temperature, and why? (ii) Which object, B or C, experiences
a greater rise in temperature, and why? Calculations: Determine the rise in temperature of each block.
PROBLEM 105
A B C
Copper
Glass
mA = 2.0 g mB = 6.0 g mC = 6.0 g
106. M A Crude Thermometer. You and your team are given the task of constructing a crude thermometer that covers a temperature range from 0 °C
to 60 °C. You have at your disposal an aluminum rod of length L0 = 2.00 m (at T = 0 °C) and diameter D = 0.50 cm, and a broken clock that is missing its hour hand, and its longer minute hand is hanging loose and pointing in
the six o’clock direction. The long hand of the clock is 8.20 inches long and
pivots loosely at the clock’s center. You get the idea to mount the rod hori-
zontally so that one end butts against a wall and the other end pushes against
the dangling minute hand of the clock. A temperature-induced change in
the length of the rod will then be refl ected in a change in the angle that the
minute hand makes with the vertical (i.e., relative to the six o’clock position).
(a) If you want the full temperature range to span the angle between the 6 and 7 markings (uniformly spaced) on the clock, how far from the central
pivot should the end of the rod make contact with the minute hand? (b) The current temperature in the room is 65.0 °F. At what angle relative to the
vertical (the six o’clock position) should the minute hand point at this tem-
perature if it is to point directly at 6 when T = 0 °C? (c) What would be the
angular range of your “clock-thermometer” if the rod were made of steel,
rather than aluminum? Assume that it is placed at the same position on the
minute hand as determined in (a).
107. M A Submerged Machine. You and your team are testing a device that is to be submerged in the cold waters of Antarctica. It is designed to rotate
a small wheel at a very precise rate. One component of the device consists
of a steel wheel (diameter Dsteel = 3.0000 cm at T = 78.400 °F) and a large aluminum wheel that drives it (diameter DAl = 150.000 cm at T = 78.400 °F). (a) If the aluminum wheel rotates at 35.0000 RPM, at what rate does the smaller, steel wheel turn while both wheels are at T = 78.400 °F? (b) You submerge the device in a large vat of water held at 32.800 °C, simulating its
working environment in the Antarctic seas. Assuming the larger, aluminum
driving wheel still rotates at 35.0000 RPM, at what rate does the smaller, steel
wheel rotate when the device is submerged in the cold water? (c) How should you adjust the rate of the aluminum driving wheel so that the steel wheel
rotates at the same rate as it had at T = 78.400 °F? Note: 𝛼Al = 23 × 10−6 and 𝛼steel = 12 × 10−6.
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
13.1 Define convection.
13.2 Solve conduction problems.
13.3 Solve radiation problems.
13.4 Analyze heat transfer applications.
R ad
iu s
Im ag
es /G
et ty
I m
ag es
CHAPTER 13
The Transfer of Heat
Igloos are constructed from ice and snow to provide protection from wintery conditions. One reason that
igloos do their job so well is that the ice and snow act as thermal insulation and minimize the loss of heat
from the inside. The physical process called conduction plays the primary role in how thermal insulation
works, and it is one of the three main processes by which heat is transferred from place to place.
13.1 Convection When heat is transferred to or from a substance, the internal energy of the sub-
stance can change, as we saw in Chapter 12. This change in internal energy
is accompanied by a change in temperature or a change in phase. The transfer of
heat aff ects us in many ways. For instance, within our homes furnaces distribute
heat on cold days, and air conditioners remove it on hot days. Our bodies con-
stantly transfer heat in one direction or another, to prevent the adverse eff ects of
hypo- and hyperthermia. And virtually all our energy originates in the sun and
is transferred to us over a distance of 150 million kilometers through the void of
space. Today’s sunlight provides the energy to drive photosynthesis in the plants
that provide our food and, hence, metabolic energy. Ancient sunlight nurtured
the organic matter that became the fossil fuels of oil, natural gas, and coal. This
chapter examines the three processes by which heat is transferred: convection,
conduction, and radiation.
When part of a fl uid is warmed, such as the air above a fi re, the volume of that part
of the fl uid expands, and the density decreases. According to Archimedes’ principle
(see Section 11.6), the surrounding cooler and denser fl uid exerts a buoyant force on
the warmer fl uid and pushes it upward. As warmer fl uid rises, the surrounding cooler
fl uid replaces it. This cooler fl uid, in turn, is warmed and pushed upward. Thus, a con-
tinuous fl ow is established, which carries along heat. Whenever heat is transferred by
360
13.1 Convection 361
the bulk movement of a gas or a liquid, the heat is said to be transferred by convection. The fl uid fl ow itself is called a convection current.
CONVECTION Convection is the process in which heat is carried from place to place by the bulk movement of a fl uid.
The smoke rising from a fi re, like the one in Figure 13.1, is one visible result of convec- tion. Figure 13.2 shows the less visible example of convection currents in a pot of water being heated on a gas burner. The currents distribute the heat from the burning gas to all parts of the
water. Conceptual Example 1 deals with some of the important roles that convection plays in
the home.
FIGURE 13.1 A plume of smoke originates from an oil burn near the site of the Deepwater Horizon oil spill disaster in the
Gulf of Mexico in 2010. The plume rises hundreds of meters
into the air because of convection.
C h ar
li e
N ei
b er
g al
l/ ©
A P
/W id
e W
o rl
d P
h o to
s
FIGURE 13.2 Convection currents are set up when a pot of
water is heated.
CONCEPTUAL EXAMPLE 1 The Physics of Heating and Cooling by Convection
Hot water baseboard heating units are frequently used in homes, and a
cooling coil is a major component of a refrigerator. The locations of these
heating and cooling devices are diff erent because each is designed to
maximize the production of convection currents. Where should the heat-
ing unit and the cooling coil be located? (a) Heating unit near the fl oor of the room and cooling coil near the top of the refrigerator (b) Heating unit near the ceiling of the room and cooling coil near the bottom of the
refrigerator
Reasoning An important goal for the heating system is to distribute heat throughout a room. The analogous goal for the cooling coil is to
remove heat from all of the space within a refrigerator. In each case, the
heating or cooling device must be positioned so that convection makes
the goal achievable.
Answer (b) is incorrect. If the heating unit were placed near the ceiling of the room, warm air from the unit would remain there, because warm air
does not fall (it rises). Thus, there would be very little natural movement
(or convection) of air to distribute the heat throughout the room. If the
cooling coil were located near the bottom of the refrigerator, the cool air
would remain there, because cool air does not rise (it sinks). There would
be very little convection to carry the heat from other parts of the refriger-
ator to the coil for removal.
Answer (a) is correct. The air above the baseboard unit is heated, like the air above a fi re. Buoyant forces from the surrounding cooler
air push the warm air upward. Cooler air near the ceiling is displaced
downward and then warmed by the baseboard heating unit, causing
the convection current illustrated in Animated Figure 13.3a. Within the refrigerator, air in contact with the top-mounted coil is cooled, its
volume decreases, and its density increases. The surrounding warmer
and less dense air cannot provide suffi cient buoyant force to support
the cooler air, which sinks downward. In the process, warmer air near
the bottom of the refrigerator is displaced upward and is then cooled
by the coil, establishing the convection current shown in Animated Figure 13.3b.
362 CHAPTER 13 The Transfer of Heat
THE PHYSICS OF . . . thermals. Another example of convection occurs when the ground, heated by the sun’s rays, warms the neighboring air. Surrounding cooler and denser air
pushes the heated air upward. The resulting updraft or “thermal” can be quite strong, depending
on the amount of heat that the ground can supply. As Figure 13.4 illustrates, these thermals can be used by glider pilots to gain considerable altitude. Birds such as eagles utilize thermals in a
similar fashion.
THE PHYSICS OF . . . an inversion layer. Sometimes meteorological conditions cause a layer to form in the atmosphere where the temperature increases with increasing altitude.
Such a layer is called an inversion layer because its temperature profi le is inverted compared to the usual situation, wherein the air temperature decreases with increasing altitude. In the usual
situation, upward convection currents occur and are important for dispersing pollutants from
industrial sources and automobile exhaust systems. An inversion layer, in contrast, arrests the
normal upward convection currents, causing a stagnant-air condition in which the concentration
of pollutants increases substantially. This condition leads to a smog layer that can often be seen
hovering over large cities.
We have been discussing natural convection, in which a temperature diff erence causes the density at one place in a fl uid to be diff erent from the density at another. Sometimes, natural convection is
inadequate to transfer suffi cient amounts of heat. In such cases forced convection is often used, and an external device such as a pump or a fan mixes the warmer and cooler portions of the fl uid.
BIO THE PHYSICS OF . . . rapid thermal exchange. Figure 13.5 shows an applic- ation of forced convection that is revolutionizing the way in which the eff ects of overheating are
being treated. Athletes, for example, are especially prone to overheating, and the device illustrated
in Figure 13.5 is appearing more and more frequently at athletic events. The technique is known as rapid thermal exchange and takes advantage of specialized blood vessels called arteriovenous
anastomoses (AVAs) that are found in the palms of the hands (and soles of the feet). These blood
vessels are used to help dissipate unwanted heat from the body. The device in the drawing consists
of a small chamber containing a curved metal plate, through which cool water is circulated from a
refrigerated supply. The overheated athlete inserts his hand into the chamber and places his palm
on the plate. The chamber seals around the wrist and is evacuated slightly to reduce the air pressure
and thereby promote circulation of blood through the hand. Forced convection plays two roles in
this treatment. It causes the water to circulate through the metal plate and remove heat from the
blood in the AVAs. Also, the cooled blood returns through veins to the heart, which pumps it
throughout the body, thus lowering the body temperature and relieving the eff ects of overheating.
Convection current
Hot water baseboard heating unit
Cooling coil
(a) (b)
ANIMATED FIGURE 13.3 (a) Air warmed by the baseboard heating unit is pushed to the top of the room by the cooler and denser air. (b) Air cooled by the cooling coil sinks to the bottom of the refrigerator. In both (a) and (b) a convection current is established.
Cooler ground
Cooler ground
Warmer ground
FIGURE 13.4 Updrafts, or thermals, are caused by the convective movement of air
that the ground has warmed.
13.2 Conduction 363
Figure 13.6 shows the application of forced convection in an automobile engine. As in the previous application, forced convection occurs in two ways. First, a pump circulates radiator fl uid
(water and antifreeze) through the engine to remove excess heat from the combustion process.
Second, a radiator fan draws air through the radiator. Heat is transferred from the hotter radiator
fl uid to the cooler air, thereby cooling the fl uid.
BIO THE PHYSICS OF . . . the windchill factor. Forced convection also plays the principal role in the windchill factor that is often mentioned in weather reports. The wind mixes
the cold ambient air with the warm layer of air that immediately surrounds the exposed portions
of your body. The forced convection removes heat from exposed body surfaces, thereby making
you feel colder than you would if there were no wind.
Check Your Understanding
(The answer is given at the end of the book.) 1. The transfer of heat by convection is smallest in (a) solids, (b) liquids, (c) gases.
13.2 Conduction Anyone who has fried a hamburger in an all-metal skillet knows that the metal handle becomes
hot. Somehow, heat is transferred from the burner to the handle. Clearly, heat is not being trans-
ferred by the bulk movement of the metal or the surrounding air, so convection can be ruled out.
Instead, heat is transferred directly through the metal by a process called conduction.
CONDUCTION Conduction is the process whereby heat is transferred directly through a material, with any bulk motion of the material playing no role in the transfer.
Cooler blood
Warmer blood
Warmer water
Curved plate
Cooler water
FIGURE 13.5 An overheated athlete uses a rapid-thermal-exchange device to cool down. He places the palm of his hand on a curved
metal plate within a slightly evacuated chamber. Forced convection
circulates cool water through the plate, which cools the blood
fl owing through the hand. The cooled blood returns through veins
to the heart, which circulates it throughout the body.
Cool fluid in
Pump Radiator fan
Hot fluid out
Cylinders
FIGURE 13.6 The forced convection generated by a pump circulates radiator
fl uid through an automobile engine to
remove excess heat.
364 CHAPTER 13 The Transfer of Heat
One mechanism for conduction occurs when the atoms or molecules in a hotter part of the
material vibrate or move with greater energy than those in a cooler part. By means of collisions,
the more energetic molecules pass on some of their energy to their less energetic neighbors. For
example, imagine a gas fi lling the space between two walls that face each other and are main-
tained at diff erent temperatures. Molecules strike the hotter wall, absorb energy from it, and
rebound with a greater kinetic energy than when they arrived. As these more energetic molecules
collide with their less energetic neighbors, they transfer some of their energy to them. Eventually,
this energy is passed on until it reaches the molecules next to the cooler wall. These molecules,
in turn, collide with the wall, giving up some of their energy to it in the process. Through such
molecular collisions, heat is conducted from the hotter to the cooler wall.
A similar mechanism for the conduction of heat occurs in metals. Metals are diff erent from
most substances in having a pool of electrons that are more or less free to wander throughout
the metal. These free electrons can transport energy and allow metals to transfer heat very well.
The free electrons are also responsible for the excellent electrical conductivity that metals have.
Those materials that conduct heat well are called thermal conductors, and those that con- duct heat poorly are known as thermal insulators. Most metals are excellent thermal conduct- ors; wood, glass, and most plastics are common thermal insulators. Thermal insulators have
many important applications. Virtually all new housing construction incorporates thermal insu-
lation in attics and walls to reduce heating and cooling costs. And the wooden or plastic handles
on many pots and pans reduce the fl ow of heat to the cook’s hand.
To illustrate the factors that infl uence the conduction of heat, Interactive Figure 13.7 dis- plays a rectangular bar. The ends of the bar are in thermal contact with two bodies, one of which
is kept at a constant higher temperature, while the other is kept at a constant lower temperature.
Although not shown for the sake of clarity, the sides of the bar are insulated, so the heat lost
through them is negligible. The amount of heat Q conducted through the bar from the warmer end to the cooler end depends on a number of factors:
1. Q is proportional to the time t during which conduction takes place (Q ∝ t). More heat fl ows in longer time periods.
2. Q is proportional to the temperature diff erence ΔT between the ends of the bar (Q ∝ ΔT). A larger diff erence causes more heat to fl ow. No heat fl ows when both ends have the same
temperature and ΔT = 0 C°. 3. Q is proportional to the cross-sectional area A of the bar (Q ∝ A). Interactive Figure 13.8
helps to explain this fact by showing two identical bars (insulated sides not shown) placed
between the warmer and cooler bodies. Clearly, twice as much heat fl ows through two bars
as through one, because the cross-sectional area has been doubled.
4. Q is inversely proportional to the length L of the bar (Q ∝ 1/L). Greater lengths of material conduct less heat. To experience this eff ect, put two insulated mittens (the pot holders that
Heat flowWarmer body
Cross-sectional area = A
L
Cooler body
INTERACTIVE FIGURE 13.7 Heat is conduc- ted through the bar when the ends of the bar
are maintained at diff erent temperatures. The
heat fl ows from the warmer to the cooler end.
Heat flow
Heat flow
Warmer body
Cooler body
Cross-sectional area = A
Cross-sectional area = A
INTERACTIVE FIGURE 13.8 Twice as much heat fl ows through two identical bars as through
one.
13.2 Conduction 365
cooks keep near the stove) on the same hand. Then, touch a hot pot and notice that it feels cooler than when you wear only one mitten, signifying that less heat passes through the
greater thickness (“length”) of material.
These proportionalities can be stated together as Q ∝ (AΔT)t/L. Equation 13.1 expresses this result with the aid of a proportionality constant k, which is called the thermal conductivity.
CONDUCTION OF HEAT THROUGH A MATERIAL The heat Q conducted during a time t through a bar of length L and cross-sectional area A is
Q = (kA ∆ T ) t
L (13.1)
where ΔT is the temperature diff erence between the ends of the bar (the higher temper- ature minus the lower temperature) and k is the thermal conductivity of the material. SI Unit of Thermal Conductivity: J/(s · m · C°)
Since k = QL/(tAΔT), the SI unit for thermal conductivity is J · m/(s · m2 · C°) or J/(s · m · C°). The SI unit of power is the joule per second (J/s), or watt (W), so the thermal conductivity
is also given in units of W/(m · C°). Diff erent materials have diff erent thermal conductivities, and Table 13.1 gives some rep-
resentative values. Because metals are such good thermal conductors, they have large thermal
conductivities. In comparison, liquids and gases generally have small thermal conductivities. In
fact, in most fl uids the heat transferred by conduction is negligible compared to that transferred
by convection when there are strong convection currents. Air, for instance, with its small thermal
conductivity, is an excellent thermal insulator when confi ned to small spaces where no appreciable
convection currents can be established. Goose down, Styrofoam, and wool derive their fi ne insu-
lating properties in part from the small dead-air spaces within them, as Figure 13.9 illustrates. THE PHYSICS OF . . . dressing warmly. We also take advantage of dead-air spaces
when we dress “in layers” during very cold weather and put on several layers of relatively thin
clothing rather than one thick layer. The air trapped between the layers acts as an excellent insulator.
Example 2 deals with the role that conduction through body fat plays in regulating body
temperature.
TABLE 13.1 Thermal Conductivitiesa of Selected Materials
Substance
Thermal Conductivity, k [J/(s · m · C°)] Substance
Thermal Conductivity, k [J/(s · m · C°)]
Metals Other Materials Aluminum 240 Asbestos 0.090
Brass 110 Body fat 0.20
Copper 390 Concrete 1.1
Iron 79 Diamond 2450
Lead 35 Glass 0.80
Silver 420 Goose down 0.025
Steel (stainless) 14 Ice (0 °C) 2.2
Gases Styrofoam 0.010 Air 0.0256 Water 0.60
Hydrogen (H2) 0.180 Wood (oak) 0.15
Nitrogen (N2) 0.0258 Wool 0.040
Oxygen (O2) 0.0265
aExcept as noted, the values pertain to temperatures near 20 °C.
Trapped air spaces
Very small convection currents
FIGURE 13.9 Styrofoam is an excellent thermal insulator because it contains many
small, dead-air spaces. These small spaces in-
hibit heat transfer by convection currents, and
air itself has a very low thermal conductivity.
366 CHAPTER 13 The Transfer of Heat
Example 3 uses Equation 13.1 to determine what the temperature is at a point between the
warmer and cooler ends of the bar in Interactive Figure 13.7.
EXAMPLE 2 BIO The Physics of Heat Transfer in the Human Body
When excessive heat is produced within the body, it must be transferred
to the skin and dispersed if the temperature at the body interior is to be
maintained at the normal value of 37.0 °C. One possible mechanism for
transfer is conduction through body fat. Suppose that heat travels through
0.030 m of fat in reaching the skin, which has a total surface area of
1.7 m2 and a temperature of 34.0 °C. Find the amount of heat that reaches
the skin in half an hour (1800 s).
Reasoning and Solution In Table 13.1 the thermal conductivity of body fat is given as k = 0.20 J/(s · m · C°). According to Equa- tion 13.1,
Q = (kA ∆ T ) t
L
Q = [0.20 J / (s · m · C°)](1.7 m2 )(37.0 °C − 34.0 °C)(1800 s)
0.030 m
= 6.1 × 104 J .
For comparison, a jogger can generate over ten times this amount of heat
in a half hour. Thus, conduction through body fat is not a particularly
eff ective way of removing excess heat. Heat transfer via blood fl ow to the
skin is more eff ective and has the added advantage that the body can vary
the blood fl ow as needed (see Problem 7).
Analyzing Multiple-Concept Problems
EXAMPLE 3 The Temperature at a Point Between the Ends of a Bar
In Interactive Figure 13.7 the temperatures at the ends of the bar are 85.0 °C at the warmer end and 27.0 °C at the cooler end. The bar has a length
of 0.680 m. What is the temperature at a point that is 0.220 m from the
cooler end of the bar?
Reasoning The point in question is closer to the cooler end than to the warmer end of the bar. It might be expected, therefore, that the
temperature at this point is less than halfway between 27.0 °C and
85.0 °C. We will demonstrate that this is, in fact, the case, by apply-
ing Equation 13.1. This expression applies because no heat escapes
through the insulated sides of the bar, and we will use it twice to de-
termine the desired temperature.
Knowns and Unknowns The available data are as follows:
Description Symbol Value Temperature at warmer end TW 85.0 °C
Temperature at cooler end TC 27.0 °C
Length of bar L 0.680 m
Distance from cooler end D 0.220 m
Unknown Variable Temperature at distance D from cooler end T ?
Modeling the Problem
STEP 1 The Conduction of Heat The heat Q conducted in a time t past the point in question (which is a distance D from the cooler end of the bar) is given by Equation 13.1 as
Q = k A( T − T C) t
D
where k is the thermal conductivity of the material from which the bar is made, A is the bar’s cross-sectional area, and T and TC are, respectively, the temperature at the point in question and at the cooler end of the bar. Solving for T gives Equation 1 at the right. The variables Q, k, A, and t are unknown, so we proceed to Step 2 to deal with them.
T = TC + QD kAt
(1)
13.2 Conduction 367
Virtually all homes contain insulation in the walls to reduce heat loss. Example 4 illustrates
how to determine this loss with and without insulation.
STEP 2 The Conduction of Heat Revisited The heat Q that is conducted from the point in question to the cooler end of the bar originates at the warmer end of the bar. Thus, since no
heat is lost through the sides, we may apply Equation 13.1 a second time to obtain an expres-
sion for Q:
Q = kA( TW − TC) t
L
where TW and TC are, respectively, the temperatures at the warmer and cooler ends of the bar, which has a length L. This expression for Q can be substituted into Equation 1, as indicated at the right. The terms k, A, and t remain to be dealt with. Fortunately, however, values for them are unnecessary, because they can be eliminated algebraically from the fi nal
calculation.
Solution Combining the results of each step algebraically, we fi nd that
T = TC + QD kAt
= TC + [
kA(TW − TC )t L ]D
kAt
Simplifying this result gives
T = TC +
k A(TW − TC)t L
D
k A t = TC +
(TW − TC )D L
= 27.0 °C + (85.0 °C − 27.0 °C)(0.220 m)
0.680 m = 45.8 °C
As expected, this temperature is less than halfway between 27.0 °C and 85.0 °C.
Related Homework: Problem 41
STEP 1 STEP 2
T = TC + QD kAt
(1)
Q = kA( TW − TC) t
L
EXAMPLE 4 The Physics of Layered Insulation
One wall of a house consists of 0.019-m-thick plywood backed by
0.076-m-thick insulation, as Figure 13.10 shows. The temperature at the inside surface is 25.0 °C, while the temperature at the outside surface is
4.0 °C, both being constant. The thermal conductivities of the insulation
and the plywood are, respectively, 0.030 and 0.080 J/(s · m · C°), and the area of the wall is 35 m2. Find the heat conducted through the wall in one
hour (a) with the insulation and (b) without the insulation.
Reasoning The temperature T at the insulation–plywood interface (see Figure 13.10) must be determined before the heat conducted through the wall can be obtained. In calculating this temperature, we use the fact
that no heat is accumulating in the wall because the inner and outer tem-
peratures are constant. Therefore, the heat conducted through the insula-
tion must equal the heat conducted through the plywood during the same
time; that is, Qinsulation = Qplywood. Each of the Q values can be expressed as Q = (kA ΔT)t/L, according to Equation 13.1, leading to an expres- sion that can be solved for the interface temperature. Once a value for
T is available, Equation 13.1 can be used to obtain the heat conducted through the wall.
Inside (25.0 °C)
Outside (4.0 °C)Heat
Insulation (0.076 m)
Plywood (0.019 m)
Interface temperature = T
FIGURE 13.10 Heat fl ows through the insu- lation and plywood from the warmer inside to
the cooler outside.
368 CHAPTER 13 The Transfer of Heat
THE PHYSICS OF . . . protecting fruit plants from freezing. Fruit growers some- times protect their crops by spraying them with water when overnight temperatures are expected
to drop below freezing. Some fruit crops, like the strawberries in Figure 13.11, can withstand temperatures down to freezing (0 °C), but not below freezing. When water is sprayed on the
plants, it can freeze and release heat (see Section 12.8), some of which goes into warming the
Problem-Solving Insight When heat is conducted through a multi-layered material (such as the plywood/insulation in this example) and the high and low temperatures are con- stant, the heat conducted through each layer is the same.
Solution (a) Using Equation 13.1 and the fact that Qinsulation = Qplywood, we fi nd that
[ (kA ∆T )t
L ]
insulation
= [ (kA ∆T )t
L ]
plywood
[0.030 J/(s · m · C°)]A(25.0 °C − T )t 0.076 m
= [0.080 J/(s · m · C°)] A (T − 4.0 °C)t
0.019 m
Note that on each side of the equals sign we have written ΔT as the higher temperature minus the lower temperature. Eliminating the area A and time t algebraically and solving this equation for T reveals that the temperature at the insulation–plywood interface is T = 5.8 °C.
The heat conducted through the wall is either Qinsulation or Qplywood, since the two quantities are equal. Choosing Qinsulation and using T = 5.8 °C in Equation 13.1, we fi nd that
Qinsulation = [0.030 J/ (s · m · C°)](35 m2)(25.0 °C − 5.8 °C)(3600 s)
0.076 m
= 9.5 × 10 5 J
(b) It is straightforward to use Equation 13.1 to calculate the amount of heat that would fl ow through the plywood in one hour if the insulation
were absent:
Qplywood = [0.080 J/ (s · m · C°)](35 m2)(25.0 °C − 4.0 °C)(3600 s)
0.019 m
= 110 × 10 5 J
Without insulation, the heat loss is increased by a factor of about 12.
Math Skills Without units (omitted for the sake of clarity), the equation that needs to be solved for the temperature T is
0.030 A (25.0 − T ) t 0.076
= 0.080 A ( T − 4.0) t
0.019 or
0.030 (25.0 − T ) 0.076
= 0.080 ( T − 4.0)
0.019
The terms A and t appear on both sides of the equation as factors in the numerator and, therefore, have been eliminated algebraic-
ally. Rearranging the result slightly and carrying out the indicated
divisions, we obtain
0.030
0.076 (25.0 − T ) =
0.080
0.019 (T − 4.0) or
0.394 (25.0 − T ) = 4.21( T − 4.0)
Expanding the terms on each side of the equals sign and rearranging
the result shows that
9.85 − 0.394T = 4.21T − 16.84 or 26.69 = 4.604T
In these results, in order to avoid round-off errors, we have carried
along more signifi cant fi gures than only the two justifi ed by the
original data. However, in solving the fi nal equation for T we round
off to two signifi cant fi gures and obtain T = 26.69
4.604 = 5.8 °C.
P ie
rr e
D u ch
ar m
e/ R
eu te
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ew sc
o m
FIGURE 13.11 When the temperature dips below freezing, strawberry growers spray their
plants with water to put a coat of ice on them.
Because of the heat released when the water
freezes and because of the relatively small thermal
conductivity of ice, this procedure protects the plants
against subfreezing temperatures. The photograph
shows berries that survived a temperature of −3 °C
with little or no damage.
13.2 Conduction 369
plant. In addition, water and ice have relatively small thermal conductivities, as Table 13.1 indic- ates. Thus, they also protect the crop by acting as thermal insulators that reduce heat loss from
the plants.
Although a layer of ice may be benefi cial to strawberries, it is not so desirable inside a refri-
gerator, as Conceptual Example 5 discusses.
CONCEPTUAL EXAMPLE 5 An Iced-up Refrigerator
In a refrigerator, heat is removed by a cold refrigerant fl uid that circulates
within a tubular space embedded inside a metal plate, as Figure 13.12 illustrates. A good refrigerator cools food as quickly as possible. Which
arrangement works best: (a) an aluminum plate coated with ice, (b) an aluminum plate without ice, (c) a stainless steel plate coated with ice, or (d) a stainless steel plate without ice?
Reasoning Figure 13.12 (see the blow-ups) shows the metal cooling plate with and without a layer of ice. Without ice, heat passes by conduc-
tion through the metal plate to the refrigerant fl uid within. For a given
temperature diff erence across the thickness of the metal, the rate of heat
transfer depends on the thermal conductivity of the metal. When the plate
becomes coated with ice, any heat that is removed by the refrigerant fl uid
must fi rst be transferred by conduction through the ice before it encoun-
ters the metal plate.
Answers (a), (c), and (d) are incorrect. For answers (a) and (c), the
relation Q = (kA ∆ T ) t
L (Equation 13.1) indicates that the heat conducted
per unit time (Q/t) is inversely proportional to the thickness L of the ice. As ice builds up, the heat removed per unit time by the cooling plate de-
creases. Thus, when covered with ice, the cooling plate—regardless of
whether it’s made from aluminum or stainless steel—does not work as
well as a plate that is ice-free. Answer (d)—the stainless steel plate without
ice—is incorrect, because heat is transferred more readily through a plate
that has a greater thermal conductivity, and stainless steel has a smaller
thermal conductivity than does aluminum (see Table 13.1).
Answer (b) is correct. The relation Q = (kA ∆ T ) t
L (Equation 13.1) shows
that the heat conducted per unit time (Q/t) is directly proportional to the thermal conductivity k of the metal plate. Since the thermal conductivity of aluminum is more than 17 times greater than the thermal conductivity
of stainless steel (see Table 13.1), aluminum is the preferred plate. The aluminum plate arrangement works best without an ice buildup. When
ice builds up, the heat removed per unit time decreases because of the
increased thickness of material through which the heat must pass.
Related Homework: Problem 12
Refrigerant fluid
eat
Metal Ice
Heat
Metal plate
Tubular space containing refrigerant fluid
FIGURE 13.12 In a refrigerator, cooling is accomplished by
a cold refrigerant fl uid that
circulates through a tubular space
embedded within a metal plate.
Sometimes the plate becomes
coated with a layer of ice.
Check Your Understanding
(The answers are given at the end of the book.) 2. A poker used in a fi replace is held at one end, while the other end is in the fi re. In terms of being
cooler to the touch, should a poker be made from (a) a high-thermal-conductivity material, (b) a low-thermal-conductivity material, or (c) can either type be used?
3. Several days after a snowstorm, the outdoor temperature remains below freezing. The roof on one house is uniformly covered with snow. On a neighboring house, however, the snow on the roof has
completely melted. Which house is better insulated?
4. Concrete walls often contain steel reinforcement bars. Does the steel (a) enhance, (b) degrade, or (c) have no eff ect on the insulating value of the concrete wall? (Consult Table 13.1.)
5. To keep your hands as warm as possible during skiing, should you wear mittens or gloves? (Mittens, except for the thumb, do not have individual fi nger compartments.) Assume that the mittens and gloves
are the same size and are made of the same material. You should wear: (a) gloves, because the individual (Continued)
370 CHAPTER 13 The Transfer of Heat
fi nger compartments mean that the gloves have a smaller thermal conductivity; (b) gloves, because the individual fi nger compartments mean that the gloves have a larger thermal conductivity; (c) mittens, because they have less surface area exposed to the cold air.
6. A water pipe is buried slightly beneath the ground. The ground is covered with a thick layer of snow, which contains a lot of small dead-air spaces within it. The air temperature suddenly drops to well
below freezing. The accumulation of snow (a) has no eff ect on whether the water in the pipe freezes, (b) causes the water in the pipe to freeze more quickly than if the snow were not there, (c) helps prevent the water in the pipe from freezing.
7. Some animals have hair strands that are hollow, air-fi lled tubes. Others have hair strands that are solid. Which kind, if either, would be more likely to give an animal an advantage for surviving in very cold
climates?
8. Two bars are placed between plates whose temperatures are Thot and Tcold (see CYU Figure 13.1). The thermal conduct- ivity of bar 1 is six times that of bar 2 (k1 = 6k2), but bar 1 has only one-third the cross-sectional area (A1 =
1
3 A2). Ignore any heat loss through the sides of the bars. What
can you conclude about the amounts of heat Q1 and Q2, respectively, that bar 1 and bar 2 conduct in a given
amount of time? (a) Q1 = 14 Q 2 (b) Q1 = 1
8 Q 2 (c) Q1 = 2Q2 (d) Q1 = 4Q2 (e) Q1 = Q2
9. A piece of Styrofoam and a piece of wood are joined to- gether to form a layered slab. The two pieces have the same
thickness and cross-sectional area, but the Styrofoam has the smaller thermal conductivity. The tem-
perature of the exposed Styrofoam surface is greater than the temperature of the exposed wood surface,
both temperatures being constant. Is the temperature of the Styrofoam–wood interface (a) closer to the higher temperature of the exposed Styrofoam surface, (b) closer to the lower temperature of the exposed wood surface, or (c) halfway between the two temperatures?
13.3 Radiation Energy from the sun is brought to earth by large amounts of visible light waves, as well as by
substantial amounts of infrared and ultraviolet waves. These waves are known as electromagnetic
waves, a class that also includes the microwaves used for cooking and the radio waves used for
AM and FM broadcasts. The sunbather in Figure 13.13 feels hot because her body absorbs energy from the sun’s electromagnetic waves. Anyone who has stood by a roaring fi re or put a
hand near an incandescent light bulb has experienced a similar eff ect. Thus, fi res and light bulbs
also emit electromagnetic waves, and when the energy of such waves is absorbed, it can have the
same eff ect as heat.
The process of transferring energy via electromagnetic waves is called radiation, and, unlike convection or conduction, it does not require a material medium. Electromagnetic waves from the
sun, for example, travel through the void of space during their journey to earth.
RADIATION Radiation is the process in which energy is transferred by means of electromagnetic waves.
All bodies continuously radiate energy in the form of electromagnetic waves. Even an ice
cube radiates energy, although so little of it is in the form of visible light that an ice cube cannot
be seen in the dark. Likewise, the human body emits insuffi cient visible light to be seen in the
dark. However, as Figures 12.6 and 12.7 illustrate, the infrared waves radiating from the body can be detected in the dark by electronic cameras. Generally, an object does not emit much
visible light until the temperature of the object exceeds about 1000 K. Then a characteristic
red glow appears, like that of a heating coil on an electric stove. When its temperature reaches
about 1700 K, an object begins to glow white-hot, like the tungsten fi lament in an incandescent
light bulb.
In the transfer of energy by radiation, the absorption of electromagnetic waves is just as
important as their emission. The surface of an object plays a signifi cant role in determining
Bar 1
Bar 2
Thot Tcold
CYU FIGURE 13.1
FIGURE 13.13 Suntans are produced by ultraviolet rays.
StockLite/Shutterstock
13.3 Radiation 371
how much radiant energy the object will absorb or emit. The two blocks in sunlight in Interactive Figure 13.14, for example, are identical, except that one has a rough surface coated with lampblack (a fi ne black soot), while the other has a highly polished silver surface. As the thermometers indicate,
the temperature of the black block rises at a much faster rate than that of the silvery block. This
is because lampblack absorbs about 97% of the incident radiant energy, while the silvery surface
absorbs only about 10%. The remaining part of the incident energy is refl ected in each case. We see
the lampblack as black in color because it refl ects so little of the light falling on it, while the silvery
surface looks like a mirror because it refl ects so much light. Since the color black is associated with
nearly complete absorption of visible light, the term perfect blackbody or, simply, blackbody is used when referring to an object that absorbs all the electromagnetic waves falling on it.
All objects emit and absorb electromagnetic waves simultaneously. When a body has the
same constant temperature as its surroundings, the amount of radiant energy being absorbed must
balance the amount being emitted in a given interval of time. The block coated with lampblack
absorbs and emits the same amount of radiant energy, and the silvery block does too. In either
case, if absorption were greater than emission, the block would experience a net gain in energy.
As a result, the temperature of the block would rise and not be constant. Similarly, if emission
were greater than absorption, the temperature would fall. Since absorption and emission are
balanced, a material that is a good absorber, like lampblack, is also a good emitter, and a material that is a poor absorber, like polished silver, is also a poor emitter. A perfect blackbody, being a perfect absorber, is also a perfect emitter.
THE PHYSICS OF . . . summer clothing. The fact that a black surface is both a good absorber and a good emitter is the reason people are uncomfortable wearing dark clothes during
the summer. Dark clothes absorb a large fraction of the sun’s radiation and then reemit it in all
directions. About one-half of the emitted radiation is directed inward toward the body and creates
the sensation of warmth. Light-colored clothes, in contrast, are cooler to wear, because they absorb
and reemit relatively little of the incident radiation.
THE PHYSICS OF . . . a white sifaka lemur warming up. The use of light colors for comfort also occurs in nature. Most lemurs, for instance, are nocturnal and have dark fur like the
lemur shown in Figure 13.15a. Since they are active at night, the dark fur poses no disadvantage in absorbing excessive sunlight. Figure 13.15b shows a species of lemur called the white sifaka, which lives in semiarid regions where there is little shade. The white color of the fur may help
in thermoregulation, by refl ecting sunlight, but during the cool mornings, refl ection of sunlight
would hinder warming up. However, these lemurs have black skin and only sparse fur on their
bellies, and to warm up in the morning, they turn their dark bellies toward the sun. The dark color
enhances the absorption of sunlight.
The amount of radiant energy Q emitted by a perfect blackbody is proportional to the radi- ation time interval t (Q ∝ t). The longer the time, the greater is the amount of energy radiated. Experiment shows that Q is also proportional to the surface area A (Q ∝ A). An object with a large surface area radiates more energy than one with a small surface area, other things being
equal. Finally, experiment reveals that Q is proportional to the fourth power of the Kelvin tem- perature T (Q ∝ T 4), so the emitted energy increases markedly with increasing temperature. If,
Lampblack-coated block
Silver-coated block
Temperature rises
rapidly
Temperature rises
slowly
INTERACTIVE FIGURE 13.14 The temperature of the block coated with lampblack
rises faster than the temperature of the block
coated with silver because the black surface
absorbs radiant energy from the sun at the
greater rate.
FIGURE 13.15 (a) Most lemurs, like this one, are nocturnal and have dark fur. (b) The species of lemur called the white sifaka, however, is active during the day and has white fur.
(a)
im ag
eB R
O K
E R
/A la
m y S
to ck
P h o to
(b)
E B
F o to
/S h u tt
er st
o ck
372 CHAPTER 13 The Transfer of Heat
for example, the Kelvin temperature of an object doubles, the object emits 24 or 16 times more
energy. Combining these factors into a single proportionality, we see that Q ∝ T4 At. This pro- portionality is converted into an equation by inserting a proportionality constant 𝜎, known as the
Stefan–Boltzmann constant. It has been found experimentally that 𝜎 = 5.67 × 10−8 J/(s · m2 · K4): Q = σT 4At
The relationship above holds only for a perfect emitter. Most objects are not perfect emitters,
however. Suppose that an object radiates only about 80% of the visible light energy that a perfect
emitter would radiate, so Q (for the object) = (0.80)𝜎T 4 At. The factor such as the 0.80 in this equation is called the emissivity e and is a dimensionless number between zero and one. The emissivity is the ratio of the energy an object actually radiates to the energy the object would
radiate if it were a perfect emitter. For visible light, the value of e for the human body, for in- stance, varies between about 0.65 and 0.80, the smaller values pertaining to lighter skin colors.
For infrared radiation, e is nearly one for all skin colors. For a perfect blackbody emitter, e = 1. Including the factor e on the right side of the expression Q = 𝜎T4 At leads to the Stefan– Boltzmann law of radiation.
THE STEFAN–BOLTZMANN LAW OF RADIATION The radiant energy Q, emitted in a time t by an object that has a Kelvin temperature T, a surface area A, and an emissivity e, is given by
Q = eσT 4 At (13.2)
where 𝝈 = 5.67 × 10−8 J/(s · m2 · K4) is the Stefan–Boltzmann constant.
In Equation 13.2, the Stefan–Boltzmann constant 𝜎 is a universal constant in the sense that its
value is the same for all bodies, regardless of the nature of their surfaces. The emissivity e, how- ever, depends on the condition of the surface. Example 6 shows how the Stefan–Boltzmann law
can be used to determine the size of a star.
EXAMPLE 6 A Supergiant Star
The supergiant star Betelgeuse has a surface temperature of about 2900 K
(about one-half that of our sun) and emits a radiant power (in joules per
second, or watts) of approximately 4 × 1030 W (about 10 000 times as
great as that of our sun). Assuming that Betelgeuse is a perfect emitter
(emissivity e = 1) and spherical, fi nd its radius.
Reasoning According to the Stefan–Boltzmann law, the power emitted is Q/t = e𝜎T4A. A star with a relatively small temperature T can have a relatively large radiant power Q/t only if its surface area A is large. As we will see, Betelgeuse has a very large surface area, so its radius is enormous.
Problem-Solving Insight First solve an equation for the unknown in terms of the known variables. Then substitute numbers for the known variables, as this example shows.
Solution Solving the Stefan–Boltzmann law for the surface area, we fi nd
A = Q / t eσT 4
But the surface area of a sphere is A = 4𝜋r2, so r = √A / (4π). Therefore, we have
r = √ Q/t4πeσT 4 = √ 4 × 1030 W
4π(1)[5.67 × 10−8 J/ (s · m2 · K4)](2900 K)4
= 3 × 1011 m
For comparison, Mars orbits the sun at a distance of 2.28 × 1011 m. Betel-
geuse is certainly a “supergiant.”
The next example explains how to apply the Stefan–Boltzmann law when an object, such as
a wood stove, simultaneously emits and absorbs radiant energy.
EXAMPLE 7 An Unused Wood-Burning Stove
An unused wood-burning stove has a constant temperature of 18 °C
(291 K), which is also the temperature of the room in which the stove
stands. The stove has an emissivity of 0.900 and a surface area of 3.50 m2.
What is the net radiant power generated by the stove?
Reasoning Power is the change in energy per unit time (Equation 6.10b), or Q/t, which, according to the Stefan–Boltzmann law, is Q/t = e𝜎T 4A (Equation 13.2). In this problem, however, we need to fi nd the net power produced by the stove. The net power is the power the stove emits
13.4 Applications 373
When an object has a higher temperature than its surroundings, the object emits a net radiant
power Pnet = (Q/t)net. The net power is the power the object emits minus the power it absorbs. Ap- plying the Stefan–Boltzmann law leads to the following expression for Pnet when the temperature of the object is T and the temperature of the environment is T0:
Pnet = eσA(T 4 − T 40 ) (13.3)
Check Your Understanding
(The answers are given at the end of the book.) 10. BIO One way that heat is transferred from place to place inside the human body is by the fl ow of blood.
Which one of the following heat transfer processes—forced convection, conduction, or radiation—best
describes this action of the blood?
11. Two strips of material, A and B, are identical, except that they have emissivities of 0.4 and 0.7, respect- ively. The strips are heated to the same temperature and have a red glow. A brighter glow signifi es that
more energy per second is being radiated. Which strip has the brighter glow?
12. One day during the winter the sun has been shining all day. Toward sunset a light snow begins to fall. It collects without melting on a cement playground, but melts instantly on contact with a black asphalt road
adjacent to the playground. Why the diff erence? (a) Being black, asphalt has a higher emissivity than cement, so the asphalt absorbs more radiant energy from the sun during the day and, consequently, warms
above the freezing point. (b) Being black, asphalt has a lower emissivity than cement, so it absorbs more radiant energy from the sun during the day and, consequently, warms above the freezing point.
13. BIO If you were stranded in the mountains in cold weather, it would help to minimize energy losses from your body if you curled up into the tightest ball possible. Which factor in the relation Q = e𝜎T4At (Equation 13.2) are you using to the best advantage by curling into a ball? (a) e (b) 𝜎 (c) T (d) A (e) t
14. Two identical cubes have the same temperature. One of them, however, is cut in two and the pieces are separated
(see CYU Figure 13.2). The radiant energy emitted by the cube cut into two pieces is Qtwo pieces and that emitted by the uncut cube is Qcube. What is true about the radiant energy emitted in a given time?
(a) Qtwo pieces = 2Qcube (b) Qtwo pieces = 4 3 Qcube (c) Qtwo pieces = Qcube (d) Qtwo pieces = 12Qcube (e) Qtwo pieces = 13Qcube 15. Two objects have the same size and shape. Object A has an emissivity of 0.3, and object B has an
emissivity of 0.6. Each radiates the same power. How is the Kelvin temperature TA of A related to the Kelvin temperature TB of B? (a) TA = TB (b) TA = 2TB (c) TA = 12TB (d) TA = √2 TB (e) TA = √
4 2 TB
13.4 Applications THE PHYSICS OF . . . rating thermal insulation by R values. To keep heating and air conditioning bills to a minimum, it pays to use good thermal insulation in your home. Insulation
inhibits convection between inner and outer walls and minimizes heat transfer by conduction.
With respect to conduction, the logic behind home insulation ratings comes directly from
minus the power the stove absorbs. The power the stove absorbs comes
from the walls, ceiling, and fl oor of the room, all of which emit radiation.
Solution Remembering that temperature must be expressed in kelvins when using the Stefan–Boltzmann law, we fi nd that
Power emitted
by unheated
stove at 18 °C
= Q t
= eσT 4A (13.2)
= (0.900)[5.67 × 10−8 J/ (s · m 2 · K4)](291 K) 4 (3.50 m2) = 1280 W
The fact that the unheated stove emits 1280 W of power and yet main-
tains a constant temperature means that the stove also absorbs 1280 W of
radiant power from its surroundings. Thus, the net power generated by the unheated stove is zero:
Net power
generated by
stove at 18 °C
= 1280 W − 1280 W = 0 W
Power emitted by
room at 18 °C and
absorbed by stove
⏟⏟⏟ Power emitted
by stove at
18 °C
⏟⏟⏟
Cube cut into two pieces
Uncut cube
CYU FIGURE 13.2
374 CHAPTER 13 The Transfer of Heat
Equation 13.1. According to this equation, the heat per unit time Q/t fl owing through a thickness of material is Q/t = kA ΔT/L. Keeping the value for Q/t to a minimum means using materials that have small thermal conductivities k and large thicknesses L. Construction engineers, however, prefer to use Equation 13.1 in the slightly diff erent form shown below:
Q t
= A ∆T L /k
The term L/k in the denominator is called the R value. An R value expresses in a single number the combined eff ects of thermal conductivity and thickness. Larger R values reduce the heat per unit time fl owing through the material and, therefore, mean better insulation. It is also convenient to use R values to describe layered slabs formed by sandwiching together a number of materials with diff erent
thermal conductivities and diff erent thicknesses. The R values for the individual layers can be added to give a single R value for the entire slab. It should be noted, however, that R values are expressed using units of feet, hours, F°, and BTU for thickness, time, temperature, and heat, respectively.
THE PHYSICS OF . . . regulating the temperature of an orbiting satellite. When it is in the earth’s shadow, an orbiting satellite is shielded from the intense electromagnetic waves
emitted by the sun. But when it moves out of the earth’s shadow, the satellite experiences the full
eff ect of these waves. As a result, the temperature within a satellite would decrease and increase
sharply during an orbital period and sensitive electronic circuitry would suff er, unless precautions
are taken. To minimize temperature fl uctuations, satellites are often covered with a highly refl ecting
and, hence, poorly absorbing metal foil, as Figure 13.16 shows. By refl ecting much of the sunlight, the foil minimizes temperature rises. Being a poor absorber, the foil is also a poor emitter and re-
duces radiant energy losses. Reducing these losses keeps the temperature from falling excessively.
THE PHYSICS OF . . . a thermos bottle. A thermos bottle, sometimes referred to as a Dewar fl ask, reduces the rate at which hot liquids cool down or cold liquids warm up. A thermos usu-
ally consists of a double-walled glass vessel with silvered inner walls (see Interactive Figure 13.17) and minimizes heat transfer via convection, conduction, and radiation. The space between the walls
is evacuated to reduce energy losses due to conduction and convection. The silvered surfaces refl ect
most of the radiant energy that would otherwise enter or leave the liquid in the thermos. Finally, little
heat is lost through the glass or the rubberlike gaskets and stopper, because these materials have
relatively small thermal conductivities.
THE PHYSICS OF . . . a halogen cooktop stove. Halogen cooktops use radiant energy to heat pots and pans. A halogen cooktop uses several quartz–iodine lamps, like the ones
in ultra-bright automobile headlights. These lamps are electrically powered and mounted below
a ceramic top. (See Figure 13.18.) The electromagnetic energy they radiate passes through the ceramic top and is absorbed directly by the bottom of the pot. Consequently, the pot heats up very
quickly, rivaling the time of a pot on an open gas burner.
FIGURE 13.16 The highly refl ective metal foil covering this satellite (the Hubble Space
Telescope) minimizes temperature changes.
StockTrek/Getty Images
Gasket
Gasket
Hot or cold
liquid
Silvered surfaces
Glass
Stopper
INTERACTIVE FIGURE 13.17 A thermos bottle minimizes energy
transfer due to convection, conduction,
and radiation.
Ceramic top
Quartz–iodine lamp
FIGURE 13.18 In a halogen cooktop, quartz–iodine lamps emit a large
amount of electromagnetic energy that
is absorbed directly by a pot or pan.
Focus on Concepts 375
EXAMPLE 8 BIO Staying Cool While Exercising
As warm-blooded animals, humans regulate their internal body temperat-
ure through the metabolism of food. These baseline metabolic processes
occur continuously in the body, even when the body is at rest or sleep-
ing. However, while exercising, the body’s muscles convert even more of
the chemical energy stored in food into mechanical work. Furthermore,
the body’s metabolic energy conversion is rather poor, where 60% of the
available energy is converted to heat. As an example, let’s say a jogger is
doing work with a power output of 250 W. She is running on a day when
the air temperature is 18 °C (291 K), and her skin temperature is 34 °C
(307 K). How much water must she evaporate per hour by sweating if she
is to maintain a skin temperature of 34 °C? Assume the surface area of
her skin is 1.4 m2 with an emissivity of 0.65, and she only loses heat by
radiation.
Reasoning Heat is carried away from her skin by radiation, and we can calculate the rate of heat loss by using Equation 13.3. Any excess heat
produced by physical activity must be removed by water evaporation. By
knowing the quantity of excess heat, we can calculate the amount of water
we need to evaporate by using Equation 12.5 and the latent heat of fusion
for water.
Solution We begin by calculating the radiation heat loss from the skin due to the diff erence in the skin and air temperature. Applying Equation 13.3,
we have: 𝑃𝑛et = 𝑒𝜎A(T 4 − T 40) = (0.65)[(5.67 × 10−8 J)/(s · m2 · K4)] (1.4 m2)[(307 K)4 − (291 K)4] = 88 W. Any excess power output above
88 W will produce heat that has to be removed to maintain her current
skin temperature. Her total power output that produces heat will be 60%
of 250 W, or (0.60)(250 W) = 150 W. Therefore, the additional power
output is 150 W – 88 W = 62 W, or 62 J/s. Thus, in one hour, or 3600 s,
this is an extra Q = (62 J/s)(3600 s) = 2.2 × 105 J of heat that must be removed by evaporation. Finally, we apply Equation 12.5 to calculate the
mass of water evaporated: m = Q/L = 2.2 × 105 J/22.6 × 105 J = 0.1 kg
Concept Summary 13.1 Convection Convection is the process in which heat is carried from place to place by the bulk movement of a fl uid. During natural convection,
the warmer, less dense part of a fl uid is pushed upward by the buoyant force
provided by the surrounding cooler and denser part. Forced convection occurs
when an external device, such as a fan or a pump, causes the fl uid to move.
13.2 Conduction Conduction is the process whereby heat is transferred directly through a material, with any bulk motion of the material playing no
role in the transfer. Materials that conduct heat well, such as most metals, are
known as thermal conductors. Materials that conduct heat poorly, such as
wood, glass, and most plastics, are referred to as thermal insulators. The heat
Q conducted during a time t through a bar of length L and cross-sectional area A is given by Equation 13.1, where ΔT is the temperature diff erence between the ends of the bar and k is the thermal conductivity of the material.
Q = (kA ∆T ) t
L (13.1)
13.3 Radiation Radiation is the process in which energy is transferred by means of electromagnetic waves. All objects, regardless of their temperature,
simultaneously absorb and emit electromagnetic waves. Objects that are
good absorbers of radiant energy are also good emitters, and objects that are
poor absorbers are also poor emitters. An object that absorbs all the radiation
incident upon it is called a perfect blackbody. A perfect blackbody, being a
perfect absorber, is also a perfect emitter.
The radiant energy Q emitted during a time t by an object whose surface area is A and whose Kelvin temperature is T is given by the Stefan–Boltzmann law of radiation (see Equation 13.2), where 𝜎 = 5.67 × 10−8 J/(s · m2 · K4) is the Stefan–Boltzmann constant and e is the emissivity, a dimensionless number characterizing the surface of the object. The emissivity lies be-
tween 0 and 1, being zero for a nonemitting surface and one for a perfect
blackbody.
Q = eσT 4 At (13.2)
The net radiant power is the power an object emits minus the power it
absorbs. The net radiant power Pnet emitted by an object with a temperature T located in an environment with a temperature T0 is given by Equation 13.3.
Pnet = eσA(T 4 − T0 4) (13.3)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 13.2 Conduction 1. The heat conducted through a bar depends on which of the following?
A. The coeffi cient of linear expansion B. The thermal conductivity
C. The specifi c heat capacity D. The length of the bar E. The cross-sectional area of the bar
(a) A, B, and D (b) A, C, and D (c) B, C, D, and E (d) B, D, and E (e) C, D, and E
2. Two bars are conducting heat from a region of higher temperature to a region of lower temperature. The bars have identical lengths and cross-
sectional areas, but are made from diff erent materials. In the drawing they are
placed “in parallel” between the two temperature regions in arrangement A,
Focus on Concepts
376 CHAPTER 13 The Transfer of Heat
whereas they are placed end to end in arrangement B. In which arrangement
is the heat that is conducted the greatest? (a) The heat conducted is the same in both arrangements. (b) Arrangement A (c) Arrangement B (d) It is not possible to determine which arrangement conducts more heat.
Aluminum
A
Copper
100 °C 0 °C
Aluminum
B
Copper
100 °C 0 °C
QUESTION 2
4. The drawing shows a composite slab consisting of three materials through which heat is conducted from left to right. The materials have identical
thicknesses and cross-sectional areas. Rank the materials according to their
thermal conductivities, largest fi rst. (a) k1, k2, k3 (b) k1, k3, k2 (c) k2, k1, k3 (d) k2, k3, k1 (e) k3, k2, k1
QUESTION 4 1
2 3
65 °C 45 °C
30 °C 25 °C
6. The long single bar on the left in the drawing has a thermal conduct- ivity of 240 J/(s · m · C°). The ends of the bar are at temperatures of 400 and 200 °C, and the temperature of its midpoint is halfway between these
two temperatures, or 300 °C. The two bars on the right are half as long
as the bar on the left, and the thermal conductivities of these bars are
diff erent (see the drawing). All of the bars have the same cross-sectional
area. What can be said about the temperature at the point where the two
bars on the right are joined together? (a) The temperature at the point where the two bars are joined together is 300 °C. (b) The temperature at the point where the two bars are joined together is greater than 300 °C.
(c) The temperature at the point where the two bars are joined together is less than 300 °C.
400 °C 200 °C400 °C 200 °C300 °C
k1 = 240 J/(s ⋅ m ⋅ C°)
k1 = 240 J/(s ⋅ m ⋅ C°) k2 = 120 J/(s ⋅ m ⋅ C°)
QUESTION 6
Section 13.3 Radiation 8. Three cubes are made from the same material. As the drawing indicates, they have diff erent sizes and temperatures. Rank the cubes according to the
radiant energy they emit per second, largest fi rst. (a) A, B, C (b) A, C, B (c) B, A, C (d) B, C, A (e) C, B, A
A B
C
L0
3L0 2L0
4T0 3T0
2T0
QUESTION 8
10. An astronaut in the space shuttle has two objects that are identical in all respects, except that one is painted black and the other is painted silver.
Initially, they are at the same temperature. When taken from inside the space
shuttle and placed in outer space, which object, if either, cools down at a
faster rate? (a) The object painted black (b) The object painted silver (c) Both objects cool down at the same rate. (d) It is not possible to determine which object cools down at the faster rate.
11. The emissivity e of object B is 116 that of object A, although both objects are identical in size and shape. If the objects radiate the same energy per
second, what is the ratio TB/TA of their Kelvin temperatures? (a) 116 (b) 1
4
(c) 12 (d) 2 (e) 4
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
Note: For problems in this set, use the values for thermal conductivities given in Table 13.1 unless stated otherwise.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 13.2 Conduction 1. E BIO The amount of heat per second conducted from the blood capillaries beneath the skin to the surface is 240 J/s. The energy is transferred
a distance of 2.0 × 10−3 m through a body whose surface area is 1.6 m2.
Assuming that the thermal conductivity is that of body fat, determine the
temperature diff erence between the capillaries and the surface of the skin.
2. E In an electrically heated home, the temperature of the ground in con- tact with a concrete basement wall is 12.8 °C. The temperature at the inside
surface of the wall is 20.0 °C. The wall is 0.10 m thick and has an area of
9.0 m2. Assume that one kilowatt · hour of electrical energy costs $0.10. How many hours are required for one dollar’s worth of energy to be conducted
through the wall?
3. E SSM MMH A person’s body is covered with 1.6 m2 of wool clothing. The thickness of the wool is 2.0 × 10−3 m. The temperature at the outside
surface of the wool is 11 °C, and the skin temperature is 36 °C. How much
heat per second does the person lose due to conduction?
4. E GO Two objects are maintained at constant temperatures, one hot and one cold. Two identical bars can be attached end to end, as in part a of the drawing, or one on top of the other, as in part b. When either of these
Problems
Problems 377
arrangements is placed between the hot and the cold objects for the same
amount of time, heat Q fl ows from left to right. Find the ratio Qa/Qb.
(a) (b)
PROBLEM 4
5. E SSM One end of an iron poker is placed in a fi re where the temperature is 502 °C, and the other end is kept at a temperature of 26 °C. The poker is
1.2 m long and has a radius of 5.0 × 10−3 m. Ignoring the heat lost along the
length of the poker, fi nd the amount of heat conducted from one end of the
poker to the other in 5.0 s.
6. E GO The block in the drawing has dimensions L0 × 2L0 × 3L0, where L0 = 0.30 m. The block has a thermal conductivity of 250 J/(s · m · C°). In drawings A, B, and C, heat is conducted through the block in three diff erent
directions; in each case the temperature of the warmer surface is 35 °C and
that of the cooler surface is 19 °C. Determine the heat that fl ows in 5.0 s for
each case.
PROBLEM 6
A B
C
L0
3L0
2L0
7. E BIO SSM In the conduction equation Q = (kA ΔT)t/L, the combination of terms kA/L is called the conductance. The human body has the ability to vary the conductance of the tissue beneath the skin by means of vasoconstric-
tion and vasodilation, in which the fl ow of blood to the veins and capillaries
is decreased and increased, respectively. The conductance can be adjusted
over a range such that the tissue beneath the skin is equivalent to a thickness
of 0.080 mm of Styrofoam or 3.5 mm of air. By what factor (high/low) can
the body adjust the conductance?
8. E GO A closed box is fi lled with dry ice at a temperature of −78.5 °C, while the outside temperature is 21.0 °C. The box is cubical, measuring
0.350 m on a side, and the thickness of the walls is 3.00 × 10−2 m. In one
day, 3.10 × 106 J of heat is conducted through the six walls. Find the thermal
conductivity of the material from which the box is made.
9. E MMH One end of a brass bar is maintained at 306 °C, while the other end is kept at a constant, but lower, temperature. The cross-sectional area
of the bar is 2.6 × 10−4 m2. Because of insulation, there is negligible heat
loss through the sides of the bar. Heat fl ows through the bar, however, at the
rate of 3.6 J/s. What is the temperature of the bar at a point 0.15 m from the
hot end?
10. E GO A wall in a house contains a single window. The window consists of a single pane of glass whose area is 0.16 m2 and whose thickness is 2.0 mm.
Treat the wall as a slab of the insulating material Styrofoam whose area and
thickness are 18 m2 and 0.10 m, respectively. Heat is lost via conduction
through the wall and the window. The temperature diff erence between the
inside and outside is the same for the wall and the window. Of the total heat
lost by the wall and the window, what is the percentage lost by the window?
11. E V-HINT MMH A composite rod is made from stainless steel and iron and has a length of 0.50 m.
The cross section of this composite rod is shown in
the drawing and consists of a square within a circle.
The square cross section of the steel is 1.0 cm on a
side. The temperature at one end of the rod is 78 °C,
while it is 18 °C at the other end. Assuming that no
heat exits through the cylindrical outer surface, fi nd
the total amount of heat conducted through the rod in
two minutes.
12. M CHALK Review Conceptual Example 5 before attempting this
problem. To illustrate the eff ect of
ice on the aluminum cooling plate,
consider the drawing shown here and
the data that it contains. Ignore any
limitations due to signifi cant fi gures.
(a) Calculate the heat per second per square meter that is conducted
through the ice–aluminum com-
bination. (b) Calculate the heat per second per square meter that would
be conducted through the aluminum
if the ice were not present. Notice
how much larger the answer is in (b) as compared to (a).
13. M A cubical piece of heat-shield tile from the space shuttle measures 0.10 m on a side and has a thermal conductivity of 0.065 J/(s · m · C°). The outer surface of the tile is heated to a temperature of 1150 °C, while the
inner surface is maintained at a temperature of 20.0 °C. (a) How much heat fl ows from the outer to the inner surface of the tile in fi ve minutes? (b) If this amount of heat were transferred to two liters (2.0 kg) of liquid water, by how
many Celsius degrees would the temperature of the water rise?
14. M GO Two pots are identical except that the fl at bottom of one is alu- minum, whereas that of the other is copper. Water in these pots is boiling
away at 100.0 °C at the same rate. The temperature of the heating element on
which the aluminum bottom is sitting is 155.0 °C. Assume that heat enters
the water only through the bottoms of the pots and fi nd the temperature of the
heating element on which the copper bottom rests.
15. M GO A pot of water is boiling under one atmosphere of pressure. As- sume that heat enters the pot only through its bottom, which is copper and
rests on a heating element. In two minutes, the mass of water boiled away is
m = 0.45 kg. The radius of the pot bottom is R = 6.5 cm, and the thickness is L = 2.0 mm. What is the temperature TE of the heating element in contact with the pot?
16. M V-HINT In a house the temperature at the surface of a window is 25 °C. The temperature outside at the window surface is 5.0 °C. Heat is lost
through the window via conduction, and the heat lost per second has a certain
value. The temperature outside begins to fall, while the conditions inside
the house remain the same. As a result, the heat lost per second increases.
What is the temperature at the outside window surface when the heat lost per
second doubles?
17. M SSM MMH Available in WileyPLUS. 18. H The drawing shows a solid cylindrical rod made from a center cylinder of lead and
an outer concentric jacket of copper. Except
for its ends, the rod is insulated (not shown),
so that the loss of heat from the curved surface
PROBLEM 11
Iron
Stainless steel
–25.0 °C
Aluminum
–10.0 °C
0.0050 m
0.0015 m
Ice
PROBLEM 12
Copper
r1
r2
Lead
PROBLEM 18
378 CHAPTER 13 The Transfer of Heat
is negligible. When a temperature diff erence is maintained between its ends,
this rod conducts one-half the amount of heat that it would conduct if it were
solid copper. Determine the ratio of the radii r1/r2. 19. H SSM Available in WileyPLUS.
Section 13.3 Radiation 20. E GO Light bulb 1 operates with a fi lament temperature of 2700 K, whereas light bulb 2 has a fi lament temperature of 2100 K. Both fi laments
have the same emissivity, and both bulbs radiate the same power. Find the
ratio A1/A2 of the fi lament areas of the bulbs. 21. E SSM The amount of radiant power produced by the sun is approxi- mately 3.9 × 1026 W. Assuming the sun to be a perfect blackbody sphere with
a radius of 6.96 × 108 m, fi nd its surface temperature (in kelvins).
22. E In an old house, the heating system uses radiators, which are hollow metal devices through which hot water or steam circulates. In one room the
radiator has a dark color (emissivity = 0.75). It has a temperature of 62 °C.
The new owner of the house paints the radiator a lighter color (emissivity =
0.50). Assuming that it emits the same radiant power as it did before being
painted, what is the temperature (in degrees Celsius) of the newly painted
radiator?
23. E SSM A person is standing outdoors in the shade where the temperat- ure is 28 °C. (a) What is the radiant energy absorbed per second by his head when it is covered with hair? The surface area of the hair (assumed to be fl at)
is 160 cm2 and its emissivity is 0.85. (b) What would be the radiant energy absorbed per second by the same person if he were bald and the emissivity
of his head were 0.65?
24. E The Kelvin temperature of an object is T1, and the object radiates a certain amount of energy per second. The Kelvin temperature of the object is
then increased to T2, and the object radiates twice the energy per second that it radiated at the lower temperature. What is the ratio T2/T1? 25. E BIO SSM A person eats a dessert that contains 260 Calories. (This “Calorie” unit, with a capital C, is the one used by nutritionists; 1 Calorie =
4186 J. See Section 12.7.) The skin temperature of this individual is 36 °C and
that of her environment is 21 °C. The emissivity of her skin is 0.75 and its sur-
face area is 1.3 m2. How much time would it take for her to emit a net radiant energy from her body that is equal to the energy contained in this dessert?
26. E BIO A person’s body is producing energy internally due to metabolic processes. If the body loses more energy than metabolic processes are generating,
its temperature will drop. If the drop is severe, it can be life-threatening.
Suppose that a person is unclothed and energy is being lost via radiation
from a body surface area of 1.40 m2, which has a temperature of 34 °C and
an emissivity of 0.700. Also suppose that metabolic processes are producing
energy at a rate of 115 J/s. What is the temperature of the coldest room in
which this person could stand and not experience a drop in body temperature?
27. E A baking dish is removed from a hot oven and placed on a cooling rack. As the dish cools down to 35 °C from 175 °C, its net radiant power de-
creases to 12.0 W. What was the net radiant power of the baking dish when it
was fi rst removed from the oven? Assume that the temperature in the kitchen
remains at 22 °C as the dish cools down.
28. E GO Sirius B is a white star that has a surface temperature (in kelvins) that is four times that of our sun. Sirius B radiates only 0.040 times the power
radiated by the sun. Our sun has a radius of 6.96 × 108 m. Assuming that
Sirius B has the same emissivity as the sun, fi nd the radius of Sirius B.
29. E BIO MMH Suppose the skin temperature of a naked person is 34 °C when the person is standing inside a room whose temperature is 25 °C. The
skin area of the individual is 1.5 m2. (a) Assuming the emissivity is 0.80, fi nd the net loss of radiant power from the body. (b) Determine the number of food Calories of energy (1 food Calorie = 4186 J) that are lost in one hour
due to the net loss rate obtained in part (a). Metabolic conversion of food into
energy replaces this loss.
30. E GO A solar collector is placed in direct sunlight where it absorbs energy at the rate of 880 J/s for each square meter of its surface. The emissivity
of the solar collector is e = 0.75. What equilibrium temperature does the collector reach? Assume that the only energy loss is due to the emission of
radiation.
31. M GO Liquid helium is stored at its boiling-point temperature of 4.2 K in a spherical container (r = 0.30 m). The container is a perfect blackbody radiator. The container is surrounded by a spherical shield whose temper-
ature is 77 K. A vacuum exists in the space between the container and the
shield. The latent heat of vaporization for helium is 2.1 × 104 J/kg. What
mass of liquid helium boils away through a venting valve in one hour?
32. M CHALK A solid sphere has a temperature of 773 K. The sphere is melted down and recast into a cube that has the same emissivity and emits
the same radiant power as the sphere. What is the cube’s temperature?
33. H SSM Available in WileyPLUS. 34. H Available in WileyPLUS.
35. E SSM Due to a temperature diff erence ΔT, heat is conducted through an aluminum plate that is 0.035 m thick. The plate is then replaced by a stain-
less steel plate that has the same temperature diff erence and cross-sectional
area. How thick should the steel plate be so that the same amount of heat per
second is conducted through it?
36. E GO A copper pipe with an outer radius of 0.013 m runs from an out- door wall faucet into the interior of a house. The temperature of the faucet is
4.0 °C, and the temperature of the pipe, at 3.0 m from the faucet, is 25 °C.
In fi fteen minutes, the pipe conducts a total of 270 J of heat to the outdoor
faucet from the house interior. Find the inner radius of the pipe. Ignore any
water inside the pipe.
37. E How many days does it take for a perfect blackbody cube (0.0100 m on a side, 30.0 °C) to radiate the same amount of energy that a one-hundred-
watt light bulb uses in one hour?
38. E GO An object is inside a room that has a constant temperature of 293 K. Via radiation, the object emits three times as much power as it absorbs
from the room. What is the temperature (in kelvins) of the object? Assume
that the temperature of the object remains constant.
39. E The concrete wall of a building is 0.10 m thick. The temperature inside the building is 20.0 °C, while the temperature outside is 0.0 °C. Heat
is conducted through the wall. When the building is unheated, the inside
temperature falls to 0.0 °C, and heat conduction ceases. However, the wall
does emit radiant energy when its temperature is 0.0 °C. The radiant energy
emitted per second per square meter at 0.0 °C is the same as the heat lost per
second per square meter due to conduction when the temperature inside the
building is 20.0 °C. What is the emissivity of the wall?
40. M GO Part a of the drawing shows a rectangular bar whose dimensions are L0 × 2L0 × 3L0. The bar is at the same constant temperature as the room
Additional Problems
Team Problems 379
(not shown) in which it is located. The bar is then cut, lengthwise, into two
identical pieces, as shown in part b of the drawing. The temperature of each piece is the same as that of the original bar. (a) What is the ratio of the power absorbed by the two bars in part b of the drawing to the single bar in part a? (b) Suppose that the temperature of the single bar in part a is 450.0 K. What would the temperature (in kelvins) of the room and the two bars in part b have to be so that the two bars absorb the same power as the single bar in part a?
PROBLEM 40 (a) (b)
L0
3L0 2L0
41. M V-HINT Multiple-Concept Example 3 discusses an approach to prob- lems such as this. The ends of a thin bar are maintained at diff erent temper-
atures. The temperature of the cooler end is 11 °C, while the temperature at a
point 0.13 m from the cooler end is 23 °C and the temperature of the warmer
end is 48 °C. Assuming that heat fl ows only along the length of the bar (the
sides are insulated), fi nd the length of the bar.
42. M CHALK GO A copper rod has a length of 1.5 m and a cross-sectional area of 4.0 × 10−4 m2. One end of the rod is in contact with boiling water and
the other with a mixture of ice and water. What is the mass of ice per second
that melts? Assume that no heat is lost through the side surface of the rod.
43. H SSM Available in WileyPLUS. 44. H Available in WileyPLUS. 45. M GO SSM A wood-burning stove (emissivity = 0.900 and surface area = 3.50 m2) is being used to heat a room. The fi re keeps the stove surface
at a constant 198 °C (471 K) and the room at a constant 29 °C (302 K). De-
termine the net radiant power generated by the stove.
Heat conduction is governed by Equation 13.1, as we have seen. Problem 46
illustrates a familiar application of this relation in the kitchen. It also gives us
the opportunity to review the idea of latent heat of vaporization. Problem 47
deals with a case in which heat loss by radiation leads to freezing of water.
It stresses the importance of the area from which the radiation occurs, and
reviews the concept of the latent heat of fusion.
46. M CHALK Two pots are identical, except that in one case the fl at bottom is aluminum and in the other it is copper. Each pot contains the same amount of
boiling water and sits on a heating element that has a temperature of 155 °C.
In the aluminum pot, the water boils away completely in 360 s. Concepts: (i) Is the heat needed to boil away the water in the aluminum-bottom pot less
than, greater than, or the same as the heat needed in the copper-bottom pot?
(ii) One of the factors in Equation 13.1 that infl uences the amount of heat
conducted through the bottom of each pot is the temperature diff erence ΔT between the upper and lower surfaces of the pot’s bottom. Is this temperature
diff erence for the aluminum-bottom pot less than, greater than, or the same
as that for the copper-bottom pot? (iii) Is the time required to boil away the
water completely in the copper- bottom pot less than, greater than, or the same
as that required for the aluminum-bottom pot? Calculations: Find the time it takes the water in the copper-bottom pot to boil away completely.
47. M CHALK SSM One half of a kilogram of liquid water at 273 K (0 °C) is placed outside on a day when the temperature is 261 K (−12 °C). Assume
that the heat is lost from the water only by means of radiation and that the
emissivity of the radiating surface is 0.60. Consider two cases: when the sur-
face area of the water is (a) 0.035 m2 (as it might be in a cup) and (b) 1.5 m2 (as it could be if the water were spilled out to form a thin sheet). Concepts: (i) In case (a) is the heat that must be removed to freeze the water less than,
greater than, or the same as in case (b)? (ii) The loss of heat by radiation
depends on the temperature of the radiating object. Does the temperature of
the water change as it freezes? (iii) The water both loses and gains heat by radiation. How, then, can heat transfer by radiation lead to freezing of the
water? (iv) Will it take longer for the water to freeze in case (a) when the area
is smaller or in case (b) when the area is larger? Calculations: For each case, (a) and (b), determine the time it takes the water to freeze into ice at 0 °C.
Concepts and Calculations Problems
48. M The Diamond Ring Solution. The processing chip on the computer that controls the navigation equipment on your spacecraft is overheating.
Unless you fi x the problem, the chip will be damaged and the navigation
system will shut down. You open the panel and fi nd that the small copper
disk that was supposed to bridge the gap between the smooth top of the chip
and the cooling plate is missing, leaving a 2.0 mm gap between them. In this
confi guration, the heat cannot escape the chip at the required rate. You notice
by the thin smudge of thermal grease (a highly thermally conductive material
used to promote good thermal contact between surfaces) that the missing
copper disk was 2.0 mm thick and had a diameter of 1.0 cm. You know that
the chip is designed to run below 75.0 °C, and the copper cooling plate is
held at a constant 5.0 °C. (a) What was the rate of heat fl ow from the chip to the copper plate when the original copper disk was in place and the chip
was at its maximum operating temperature? (b) The only material that you have available on board to bridge the gap between the chip and copper plate
is lead. If the cross-sectional area of the lead piece you plan to wedge into the
gap is 1.0 cm2, what is the rate of heat fl ow from the chip to the copper plate?
Does it match the value calculated in part (a)? (c) While brainstorming for other possible solutions to your problem, you happen to glance down at the
engagement ring on your fi nger: a large, glittering diamond. The top and bot-
tom surfaces are fl at and nearly rectangular (L = 0.75 cm and W = 0.50 cm), and the thickness looks to be about 2.0 mm, just right to bridge the gap. You
pry the diamond out of its holder and press it into the gap. What is the rate of
heat fl ow now? Good enough?
49. M Indirect Cooling With Liquid Nitrogen. You are designing a system to cool an insulated silver plate of dimensions 2.00 cm × 2.00 cm × 0.50 cm.
One end of a thermally insulated copper wire (diameter D = 2.50 mm and length L = 15.0 cm) is dipped into a vat of liquid nitrogen (T = 77.2 K), and the other end is attached to the bottom of the silver plate. (a) If the silver plate starts at room temperature (72.0 °F), what is the initial rate of heat fl ow
between the plate and the liquid nitrogen reservoir? (b) Assuming the rate of heat fl ow calculated in part (a), estimate the temperature of the silver plate
after 30.0 seconds.
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
14.1 Express the amount of a substance in moles.
14.2 Apply the ideal gas law.
14.3 Apply the kinetic theory of gases to ideal gases.
14.4 Solve diff usion problems.
G re
g A
m p tm
an /S
h u tt
er st
o ck
CHAPTER 14
The Ideal Gas Law and Kinetic Theory
A scuba diver carries his air supply in the tank on his back. To the extent that the air in a scuba tank behaves
like an ideal gas, its pressure, volume, and temperature are related by the ideal gas law. We will see that
it is possible to use this law to estimate how long a diver, using a tank of a given size, can stay under the
water at a given depth.
14.1 Molecular Mass, the Mole, and Avogadro’s Number Often, we wish to compare the mass of one atom with another. To facilitate the com-
parison, a mass scale known as the atomic mass scale has been established. To set up this scale, a reference value (along with a unit) is chosen for one of the elements.
The unit is called the atomic mass unit (symbol: u). By international agreement, the reference element is chosen to be the most abundant type or isotope* of carbon, which
is called carbon-12. Its atomic mass† is defi ned to be exactly twelve atomic mass units,
or 12 u. The relationship between the atomic mass unit and the kilogram is
1 u = 1.6605 × 10−27 kg
The atomic masses of all the elements are listed in the periodic table, part of
which is shown in Interactive Figure 14.1. The complete periodic table is given on
380
*Isotopes are discussed in Section 31.1. †In chemistry the expression “atomic weight” is frequently used in place of “atomic mass.”
14.1 Molecular Mass, the Mole, and Avogadro’s Number 381
the inside of the back cover. In general, the masses listed are average values and take into account
the various isotopes of an element that exist naturally. For brevity, the unit “u” is often omitted
from the table. For example, a magnesium atom (Mg) has an average atomic mass of 24.305 u,
whereas a lithium atom (Li) has an average atomic mass of 6.941 u. Thus, atomic magnesium
is more massive than atomic lithium by a factor of (24.305 u)/(6.941 u) = 3.502. In the periodic
table, the atomic mass of carbon (C) is given as 12.011 u, rather than exactly 12 u. This is because
a small amount (about 1%) of the naturally occurring material is an isotope called carbon-13. The
value of 12.011 u is an average that refl ects the small contribution of carbon-13.
The molecular mass of a molecule is the sum of the atomic masses of its atoms. For instance,
the elements hydrogen and oxygen have atomic masses of 1.007 94 u and 15.9994 u, respectively,
so the molecular mass of a water molecule (H2O) is, therefore, 2(1.007 94 u) + 15.9994 u =
18.0153 u.
Macroscopic amounts of materials contain large numbers of atoms or molecules. Even in a
small volume of gas, 1 cm3, for example, the number is enormous. It is convenient to express such
large numbers in terms of a single unit, the gram-mole, or simply the mole (symbol: mol). One gram-mole of a substance contains as many particles (atoms or molecules) as there are atoms in 12 grams of the isotope carbon-12. Experiment shows that 12 grams of carbon-12 contain 6.022 × 1023 atoms. The number of atoms per mole is known as Avogadro’s number NA, after the Italian scientist Amedeo Avogadro (1776–1856):
NA = 6.022 × 1023 mol−1
Thus, the number of moles n contained in any sample is the number of particles N in the sample divided by the number of particles per mole NA (Avogadro’s number):
n = N NA
Although defi ned in terms of carbon atoms, the concept of a mole can be applied to any
collection of objects by noting that one mole contains Avogadro’s number of objects. Thus, one
mole of atomic sulfur contains 6.022 × 1023 sulfur atoms, one mole of water contains 6.022 ×
1023 H2O molecules, and one mole of golf balls contains 6.022 × 10 23 golf balls. The mole is the
SI base unit for expressing “the amount of a substance.”
The number n of moles contained in a sample can also be found from its mass. To see how, multiply and divide the right-hand side of the previous equation by the mass mparticle of a single particle, expressed in grams:
n = mparticle N mparticle NA
= m
Mass per mole
The numerator mparticleN is the mass of a particle times the number of particles in the sample, which is the mass m of the sample expressed in grams. The denominator mparticleNA is the mass of a particle times the number of particles per mole, which is the mass per mole, expressed in
grams per mole.
Problem-Solving Insight The mass per mole (in g/mol) of any substance has the same numerical value as the atomic or molecular mass of the substance (in atomic mass units).
To understand this fact, consider the carbon-12 and sodium atoms as examples. The mass per
mole of carbon-12 is 12 g/mol, since, by defi nition, 12 grams of carbon-12 contain one mole of
atoms. On the other hand, the mass per mole of sodium (Na) is 22.9898 g/mol for the following
reason: as indicated in Interactive Figure 14.1, a sodium atom is more massive than a carbon-12 atom by the ratio of their atomic masses, (22.9898 u)/(12 u) = 1.915 82. Therefore, the mass per
mole of sodium is 1.915 82 times as great as that of carbon-12, which means equivalently that
(1.915 82)(12 g/mol) = 22.9898 g/mol. Thus, the numerical value of the mass per mole of sodium
(22.9898) is the same as the numerical value of its atomic mass.
Since one gram-mole of a substance contains Avogadro’s number of particles (atoms or
molecules), the mass mparticle of a particle (in grams) can be obtained by dividing the mass per mole (in g/mol) by Avogadro’s number:
mparticle = Mass per mole
NA
H Atomic number Atomic mass
1
Li 6.941
3 Be 9.01218
4
Na 22.9898
11 Mg 24.305
12
1.00794
INTERACTIVE FIGURE 14.1 A portion of the periodic table showing the atomic number
and atomic mass of each element. In the peri-
odic table it is customary to omit the symbol
“u” denoting the atomic mass unit.
382 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
Check Your Understanding
(The answers are given at the end of the book.) 1. Consider one mole of hydrogen (H2) and one mole of oxygen (O2). Which, if either, has the greater
number of molecules and which, if either, has the greater mass?
2. The molecules of substances A and B are composed of diff erent atoms. However, the two substances have the same mass densities. Consider the possibilities for the molecular masses of the two types of
molecules and decide whether 1 m3 of substance A contains the same number of molecules as 1 m3 of
substance B.
EXAMPLE 1 The Physics of Gemstones
Figure 14.2a shows the Hope diamond (44.5 carats), which is almost pure carbon. Figure 14.2b shows the Rosser Reeves ruby (138 carats), which is primarily aluminum oxide (Al2O3). One carat is equivalent to a mass of
0.200 g. Determine (a) the number of carbon atoms in the diamond and (b) the number of Al2O3 molecules in the ruby.
Reasoning The number N of atoms (or molecules) in a sample is the number of moles n times the number of atoms per mole NA (Avogadro’s number); N = nNA. We can determine the number of moles by dividing the mass of the sample m by the mass per mole of the substance.
Solution (a) The Hope diamond’s mass is m = (44.5 carats)[(0.200 g)/ (1 carat)] = 8.90 g. Since the average atomic mass of naturally occurring
carbon is 12.011 u (see the periodic table on the inside of the back cover),
the mass per mole of this substance is 12.011 g/mol. The number of moles
of carbon in the Hope diamond is
n = m
Mass per mole =
8.90 g
12.011 g/mol = 0.741 mol
The number of carbon atoms in the Hope diamond is
N = nNA = (0.741 mol)(6.022 × 1023 atoms/mol) = 4.46 × 1023 atoms
(b) The mass of the Rosser Reeves ruby is m = (138 carats)[(0.200 g)/ (1 carat)] = 27.6 g. The molecular mass of an aluminum oxide molecule
(Al2O3) is the sum of the atomic masses of its atoms, which are 26.9815 u
for aluminum and 15.9994 u for oxygen (see the periodic table on the
inside of the back cover):
Molecular mass = 2(26.9815 u) + 3(15.9994 u) = 101.9612 u
Thus, the mass per mole of Al2O3 is 101.9612 g/mol. Calculations like
those in part (a) reveal that the Rosser Reeves ruby contains 0.271 mol or
1.63 × 1023 molecules of Al2O3 .
⏟⎵⎵⏟⎵⎵⏟
Mass of 2
aluminum atoms
⏟⎵⎵⏟⎵⎵⏟
Mass of 3
oxygen atoms
FIGURE 14.2 (a) The Hope diamond surrounded by 16 smaller diamonds. (b) The Rosser Reeves ruby. Both gems are on display at the Smithsonian Institution in Washington, D.C.
(a)
C h ip
C la
rk /S
m it
h so
n ia
n I
n st
it u te
(b)
Ja m
es P
. B
la ir
/N at
io n al
G eo
g ra
p h ic
/G et
ty I
m ag
es
Example 1 illustrates how to use the concepts of the mole, atomic mass, and Avogadro’s
number to determine the number of atoms and molecules present in two famous gemstones.
14.2 The Ideal Gas Law 383
3. A gas mixture contains equal masses of the monatomic gases argon (atomic mass = 39.948 u) and neon (atomic mass = 20.179 u). These two are the only gases present. Of the total number of atoms in the
mixture, what percentage is neon?
14.2 The Ideal Gas Law An ideal gas is an idealized model for real gases that have suffi ciently low densities. The condi- tion of low density means that the molecules of the gas are so far apart that they do not interact
(except during collisions that are eff ectively elastic). The ideal gas law expresses the relationship
between the absolute pressure, the Kelvin temperature, the volume, and the number of moles of
the gas.
In discussing the constant-volume gas thermometer, Section 12.2 has already explained the
relationship between the absolute pressure and Kelvin temperature of a low-density gas. This
thermometer utilizes a small amount of gas (e.g., hydrogen or helium) placed inside a bulb and
kept at a constant volume. Since the density is low, the gas behaves as an ideal gas. Experiment
reveals that a plot of gas pressure versus temperature is a straight line, as in Figure 12.4. This plot
is redrawn in Animated Figure 14.3, with the change that the temperature axis is now labeled in kelvins rather than in degrees Celsius. The graph indicates that the absolute pressure P is dir- ectly proportional to the Kelvin temperature T (P ∝ T), for a fi xed volume and a fi xed number of molecules.
The relation between absolute pressure and the number of molecules of an ideal gas is
simple. Experience indicates that it is possible to increase the pressure of a gas by adding
more molecules; this is exactly what happens when a tire is pumped up. When the volume and
temperature of a low-density gas are kept constant, doubling the number of molecules doubles
the pressure. Thus, the absolute pressure of an ideal gas at constant temperature and constant
volume is proportional to the number of molecules or, equivalently, to the number of moles n of the gas (P ∝ n).
To see how the absolute pressure of a gas depends on the volume of the gas, look at the
partially fi lled balloon in Figure 14.4a. This balloon is “soft,” because the pressure of the air is low. However, if all the air in the balloon is squeezed into a smaller “bubble,” as in part b of the fi gure, the “bubble” has a tighter feel. This tightness indicates that the pressure in the smaller
volume is high enough to stretch the rubber substantially. Thus, it is possible to increase the
pressure of a gas by reducing its volume, and if the number of molecules and the temperature
are kept constant, the absolute pressure of an ideal gas is inversely proportional to its volume
V (P ∝ 1/V).
0 100 200 300 Temperature, K
A bs
ol ut
e pr
es su
re
Gas
ANIMATED FIGURE 14.3 The pressure inside a constant-volume gas thermometer is
directly proportional to the Kelvin temperature,
a proportionality that is characteristic of an
ideal gas.
FIGURE 14.4 (a) A partially fi lled balloon. (b) The air pressure in the partially fi lled balloon can be increased by decreasing the volume of the
balloon as shown.
A n d y W
as h n ik
(a)
A n d y W
as h n ik
(b)
384 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
The three relations just discussed for the absolute pressure of an ideal gas can be expressed
as a single proportionality, P ∝ nT/V. This proportionality can be written as an equation by inserting a proportionality constant R, called the universal gas constant. Experiments have shown that R = 8.31 J/(mol · K) for any real gas with a density suffi ciently low to ensure ideal gas behavior. The resulting equation is called the ideal gas law.
IDEAL GAS LAW The absolute pressure P of an ideal gas is directly proportional to the Kelvin temperature T and the number of moles n of the gas and is inversely proportional to the volume V of the gas: P = R(nT/V). In other words,
PV = nRT (14.1)
where R is the universal gas constant and has the value of 8.31 J/(mol · K).
Sometimes, it is convenient to express the ideal gas law in terms of the total number of
particles N, instead of the number of moles n. To obtain such an expression, we multiply and divide the right side of Equation 14.1 by Avogadro’s number NA = 6.022 × 1023 particles/mol* and recognize that the product nNA is equal to the total number N of particles:
PV = nRT = nNA ( RNA) T = N( R NA) T
The constant term R/NA is referred to as Boltzmann’s constant, in honor of the Austrian physi- cist Ludwig Boltzmann (1844–1906), and is represented by the symbol k:
k = R NA
= 8.31 J /(mol · K)
6.022 × 1023 mol−1 = 1.38 × 10−23 J/K
With this substitution, the ideal gas law becomes
PV = NkT (14.2)
Example 2 presents an application of the ideal gas law.
EXAMPLE 2 BIO The Physics of Oxygen in the Lungs
In the lungs, a thin respiratory membrane separates tiny sacs of air (ab-
solute pressure = 1.00 × 105 Pa) from the blood in the capillaries. These
sacs are called alveoli, and it is from them that oxygen enters the blood.
The average radius of the alveoli is 0.125 mm, and the air inside contains
14% oxygen. Assuming that the air behaves as an ideal gas at body tem-
perature (310 K), fi nd the number of oxygen molecules in one of the sacs.
Reasoning The pressure and temperature of the air inside an alveolus are known, and its volume can be determined since we know the radius.
Thus, the ideal gas law in the form PV = NkT can be used directly to fi nd the number N of air particles inside one of the sacs. The number of oxygen molecules is 14% of the number of air particles.
Problem-Solving Insight In the ideal gas law, the temper- ature T must be expressed on the Kelvin scale. The Celsius and Fahrenheit scales cannot be used.
Solution The volume of a spherical sac is V = 43 πr 3, where r is the radius. Solving Equation 14.2 for the number of air particles, we have
N = PV kT
= (1.00 × 105 Pa) [
4
3 π (0.125 × 10−3 m) 3 ] (1.38 × 10−23 J/ K)(310 K)
= 1.9 × 1014
The number of oxygen molecules is 14% of this value, or 0.14N = 2.7 × 1013 .
With the aid of the ideal gas law, it can be shown that one mole of an ideal gas occupies a
volume of 22.4 liters at a temperature of 273 K (0 °C) and a pressure of one atmosphere (1.013 ×
105 Pa). These conditions of temperature and pressure are known as standard temperature and pressure (STP). Conceptual Example 3 discusses another interesting application of the ideal gas law.
*“Particles” is not an SI unit and is often omitted. Then, particles/mol = 1/mol = mol−1.
14.2 The Ideal Gas Law 385
Historically, the work of several investigators led to the formulation of the ideal gas law.
The Irish scientist Robert Boyle (1627–1691) discovered that at a constant temperature, the
absolute pressure of a fi xed mass (fi xed number of moles) of a low-density gas is inversely
proportional to its volume (P ∝ 1/V). This fact is often called Boyle’s law and can be derived from the ideal gas law by noting that P = nRT/V = constant/V when n and T are constants. Alternatively, if an ideal gas changes from an initial pressure and volume (Pi, Vi) to a fi nal pressure and volume (Pf, Vf), it is possible to write PiVi = nRT and PfVf = nRT. Since the right sides of these equations are equal, we may equate the left sides to give the following concise
way of expressing Boyle’s law:
Constant T, constant n PiVi = PfVf (14.3)
Figure 14.6 illustrates how pressure and volume change according to Boyle’s law for a fi xed number of moles of an ideal gas at a constant temperature of 100 K. The gas begins with an ini-
tial pressure and volume of Pi and Vi and is compressed. The pressure increases as the volume decreases, according to P = nRT/V, until the fi nal pressure and volume of Pf and Vf are reached. The curve that passes through the initial and fi nal points is called an isotherm, meaning “same temperature.” If the temperature had been 300 K, rather than 100 K, the compression would have
occurred along the 300-K isotherm. Diff erent isotherms do not intersect. Example 4 deals with
an application of Boyle’s law to scuba diving.
CONCEPTUAL EXAMPLE 3 The Physics of Rising Beer Bubbles
If you look carefully at the bubbles rising in a glass of beer (see Figure 14.5), you’ll see them grow in size as they move upward, often doubling in volume by the time they reach the surface. Beer bubbles contain mostly
carbon dioxide (CO2), a gas that is dissolved in the beer because of the
fermentation process. Which variable describing the gas is responsible for
the growth of the rising bubbles? (a) The Kelvin temperature T (b) The absolute pressure P (c) The number of moles n
Reasoning The variables T, P, and n are related to the volume V of a bubble by the ideal gas law (V = nRT/P). We assume that this law applies and use it to guide our thinking. According to this law, an increase in
temperature, a decrease in pressure, or an increase in the number of moles
could account for the growth in size of the upward-moving bubbles.
Answers (a) and (b) are incorrect. Temperature can be eliminated immediately, since it is constant throughout the beer. Pressure cannot be
dismissed so easily. As a bubble rises, its depth decreases, and so does
the fl uid pressure that a bubble experiences. Since volume is inversely
proportional to pressure according to the ideal gas law, at least part of
the bubble growth is due to the decreasing pressure of the surrounding
beer. However, some bubbles double in volume on the way up. To account for the doubling, there would need to be two atmospheres of pressure at
the bottom of the glass, compared to the one atmosphere at the top. The
pressure increment due to depth is 𝜌gh (see Equation 11.4), so an extra pressure of one atmosphere at the bottom would mean 1.01 × 105 Pa =
𝜌gh. Solving for h with 𝜌 equal to the density of water reveals that h = 10.3 m. Since most beer glasses are only about 0.2 m tall, we can rule out
a change in pressure as the major cause of the change in volume.
Answer (c) is correct. The process of elimination brings us to the conclusion that the number of moles of CO2 in a bubble must somehow
be increasing on the way up. This is, in fact, the case. Each bubble acts
as a nucleation site for CO2 molecules dissolved in the surrounding
beer, so as a bubble moves upward, it accumulates carbon dioxide and
grows larger.
Related Homework: Problem 27
FIGURE 14.5 The bubbles in a glass of beer grow larger as they move upward.
C o u rt
es y R
ic h ar
d Z
ar e,
S ta
n fo
rd U
n iv
er si
ty
100-K isotherm
300-K isotherm
Vf
Pi
Pf
Vi Volume
P re
ss ur
e
FIGURE 14.6 A pressure-versus-volume plot for a gas at a constant temperature is called an
isotherm. For an ideal gas, each isotherm is a
plot of the equation P = nRT/V = constant/V.
386 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
Analyzing Multiple-Concept Problems
EXAMPLE 4 The Physics of Scuba* Diving
When a scuba diver descends to greater depths, the water pressure in-
creases. The air pressure inside the body cavities (e.g., lungs, sinuses)
must be maintained at the same pressure as that of the surrounding wa-
ter; otherwise the cavities would collapse. A special valve automatically
adjusts the pressure of the air coming from the scuba tank to ensure that
the air pressure equals the water pressure at all times. The scuba gear in
Figure 14.7a consists of a 0.0150-m3 tank fi lled with compressed air at an absolute pressure of 2.02 × 107 Pa. Assume that the diver consumes air at
the rate of 0.0300 m3 per minute and that the temperature of the air does
not change as the diver goes deeper into the water. How long (in minutes)
can a diver stay under water at a depth of 10.0 m? Take the density of
seawater to be 1025 kg/m3.
Reasoning The time (in minutes) that a scuba diver can remain under water is equal to the volume of air that is available divided by the volume per minute
consumed by the diver. The volume of air available to the diver depends on
the volume and pressure of the air in the scuba tank, as well as the pressure of
the air inhaled by the diver, according to Boyle’s law. The pressure of the air
inhaled equals the water pressure that acts on the diver. This pressure can be
found from a knowledge of the diver’s depth beneath the surface of the water.
h
P1 = Atmospheric pressure
P2 = Pressure at depth h
(b)
FIGURE 14.7 (a) The air pressure inside the body cavities of a scuba diver must be maintained at the same value as the pressure of the surrounding water. (b) The pressure P2 at a depth h is greater than the pressure P1 at the surface.
(a)
Z ac
M ac
au la
y /G
et ty
I m
ag es
Description Symbol Value Comment
Explicit Data
Volume of air in tank Vi 0.0150 m3
Pressure of air in tank Pi 2.02 × 107 Pa
Rate of air consumption C 0.0300 m3/min
Mass density of seawater 𝜌 1025 kg/m3
Depth of diver h 10.0 m
Implicit Data
Air pressure at surface of water P1 1.01 × 105 Pa Atmospheric pressure at sea level (see Section 11.2).
Unknown Variable
Time that diver can remain at 10.0-m depth t ?
*The word is an acronym for self-contained underwater breathing apparatus.
Knowns and Unknowns The data for this problem are listed below:
14.2 The Ideal Gas Law 387
Modeling the Problem
STEP 1 Duration of the Dive The air inside the scuba tank has an initial pressure of Pi and a volume of Vi (the volume of the tank). A scuba diver does not breathe the air directly from the tank, because the tank pressure of 2.02 × 107 Pa is nearly 200 times atmospheric pressure and
would cause his lungs to explode. Instead, a valve on the tank adjusts the pressure of the air being
sent to the diver so it equals the surrounding water pressure Pf. The time t (in minutes) that the diver can remain under water is equal to the total volume of air consumed by the diver divided by
the rate C (in cubic meters per minute) at which the air is consumed:
t = Total volume of air consumed
C
The total volume of air consumed is the volume Vf available at the breathing pressure Pf minus the volume Vi of the scuba tank, because this amount of air always remains behind in the tank. Thus, we have Equation 1 at the right. The volume Vi and the rate C are known, but the fi nal volume Vf is not, so we turn to Step 2 to evaluate it.
STEP 2 Boyle’s Law Since the temperature of the air remains constant, the air volume Vf available to the diver at the pressure Pf is related to the initial pressure Pi and volume Vi of air in the tank by Boyle’s law PiVi = PfVf (Equation 14.3). Solving for Vf yields
Vf = PiVi Pf
This expression for Vf can be substituted into Equation 1, as indicated at the right. The initial pressure Pi and volume Vi are given. However, we still need to determine the pressure Pf of the air inhaled by the diver, and we will evaluate it in the next step.
STEP 3 Pressure and Depth in a Static Fluid Figure 14.7b shows the diver at a depth h below the surface of the water. The absolute pressure P2 at this depth is related to the pressure P1 at the surface of the water by Equation 11.4: P2 = P1 + 𝜌gh, where 𝜌 is the mass density of seawater and g is the magnitude of the acceleration due to gravity. Since P1 is the air pressure at the surface of the water, it is atmospheric pressure. Recall that the valve on the scuba tank adjusts
the pressure Pf of the air inhaled by the diver to be equal to the pressure P2 of the surrounding water. Thus, P2 = Pf, and Equation 11.4 becomes
Pf = P1 + ρgh
We now substitute this expression for Pf into Equation 2, as indicated in the right column.
Problem-Solving Insight When using the ideal gas law, either directly or in the form of Boyle’s law, remember that the pressure P must be the absolute pressure, not the gauge pressure.
Solution Algebraically combining the results of the three steps, we have
t = Vf − Vi
C =
PiVi Pf
− Vi
C =
PiVi P1 + ρgh
− Vi
C The time that the diver can remain at a depth of 10.0 m is
t =
PiVi P1 + ρgh
− Vi
C
=
(2.02 × 10 7 Pa)(0.0150 m3)
1.01 × 10 5 Pa + (1025 kg/m3)(9.80 m/s2)(10.0 m) − 0.0150 m3
0.0300 m3/min = 49.6 min
Note that at a fi xed consumption rate C, greater values for h lead to smaller values for t. In other words, a deeper dive must have a shorter duration.
Related Homework: Problems 23, 27
t = Vf − Vi
C (1)
?
t = Vf − Vi
C (1)
Vf = PiVi Pf
(2)
?
t = Vf − Vi
C (1)
Vf = PiVi Pf
(2)
Pf = P1 + ρgh
STEP 1 STEP 2 STEP 3
388 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
Another investigator whose work contributed to the formulation of the ideal gas law was the
Frenchman Jacques Charles (1746–1823). He discovered that at a constant pressure, the volume
of a fi xed mass (fi xed number of moles) of a low-density gas is directly proportional to the Kelvin
temperature (V ∝ T). This relationship is known as Charles’ law and can be obtained from the ideal gas law by noting that V = nRT/P = (constant)T, if n and P are constant. Equivalently, when an ideal gas changes from an initial volume and temperature (Vi, Ti) to a fi nal volume and temperature (Vf, Tf), it is possible to write Vi/Ti = nR/P and Vf/Tf = nR/P. Thus, one way of stating Charles’ law is
Constant P, constant n Vi Ti
= Vf Tf
(14.4)
Check Your Understanding
(The answers are given at the end of the book.) 4. A tightly sealed house has a large ceiling fan that blows air out of the house and into the attic. The owners
turn the fan on and forget to open any windows or doors. What happens to the air pressure in the house
after the fan has been on for a while, and does it become easier or harder for the fan to do its job?
5. Above the liquid in a can of hair spray is a gas at a relatively high pressure. The label on the can includes the warning “DO NOT STORE AT HIGH TEMPERATURES.” Why is the warning given?
6. What happens to the pressure in a tightly sealed house when the electric furnace turns on and runs for a while?
7. BIO When you climb a mountain, your eardrums “pop” outward as the air pressure decreases. When you come down, they pop inward as the pressure increases. At the sea coast, you swim through a com-
pletely submerged passage and emerge into a pocket of air trapped within a cave. As the tide comes in,
the water level in the cave rises, and your eardrums pop. Is this popping analogous to what happens as
you climb up or climb down a mountain?
8. Atmospheric pressure decreases with increasing altitude. Given this fact, explain why helium-fi lled weather balloons are underinfl ated when they are launched from the ground. Assume that the temper-
ature does not change much as the balloon rises.
9. A slippery cork is being pressed into an almost full (but not 100% full) bottle of wine. When released, the cork slowly slides back out. However, if half the wine is removed from the bottle before the cork is
inserted, the cork does not slide out. Explain.
10. Consider equal masses of three monatomic gases: argon (atomic mass = 39.948 u), krypton (atomic mass = 83.80 u), and xenon (atomic mass = 131.29 u). The pressure and volume of each gas is the
same. Which gas has the greatest and which the smallest temperature?
14.3 Kinetic Theory of Gases As useful as it is, the ideal gas law provides no insight as to how pressure and temperature
are related to properties of the molecules themselves, such as their masses and speeds. To show
how such microscopic properties are related to the pressure and temperature of an ideal gas,
this section examines the dynamics of molecular motion. The pressure that a gas exerts on the
walls of a container is due to the force exerted by the gas molecules when they collide with the
walls. Therefore, we will begin by combining the notion of collisional forces exerted by a fl uid
(Section 11.2) with Newton’s second and third laws of motion (Sections 4.3 and 4.5). These con-
cepts will allow us to obtain an expression for the pressure in terms of microscopic properties.
We will then combine this with the ideal gas law to show that the average translational kinetic
energy KE of a particle in an ideal gas is KE = 3
2 kT, where k is Boltzmann’s constant and T is the Kelvin temperature. In the process, we will also see that the internal energy U of a monatomic ideal gas is U = 32 nRT, where n is the number of moles and R is the universal gas constant.
The Distribution of Molecular Speeds A macroscopic container fi lled with a gas at standard temperature and pressure contains a large
number of particles (atoms or molecules). These particles are in constant, random motion,
colliding with each other and with the walls of the container. In the course of one second, a
14.3 Kinetic Theory of Gases 389
300 K
1200 K
Most probable speed is near 400 m/s
Most probable speed is near 800 m/s
vrms = 484 m/s
vrms = 967 m/s
400 800 1200 1600 Molecular speed, m/s
P er
ce nt
ag e
of m
ol ec
ul es
p er
un it
s pe
ed in
te rv
al
FIGURE 14.8 The Maxwell distribution curves for molecular speeds in oxygen gas at
temperatures of 300 and 1200 K.
L
L
L
–υ
+υ
FIGURE 14.10 A gas particle is shown colliding elastically with the right wall of the container and rebounding from it.
particle undergoes many collisions, and each one changes the particle’s speed and direction of
motion. As a result, the atoms or molecules have diff erent speeds. It is possible, however, to
speak about an average particle speed. At any given instant, some particles have speeds less than,
some near, and some greater than the average. For conditions of low gas density, the distribution
of speeds within a large collection of molecules at a constant temperature was calculated by the
Scottish physicist James Clerk Maxwell (1831–1879). Figure 14.8 displays the Maxwell speed distribution curves for O2 gas at two diff erent temperatures. When the temperature is 300 K, the
maximum in the curve indicates that the most probable speed is about 400 m/s. At a temperature
of 1200 K, the distribution curve shifts to the right, and the most probable speed increases to
about 800 m/s. One particularly useful type of average speed, known as the rms speed and written
as υrms, is also shown in the drawing. When the temperature of the oxygen gas is 300 K the rms speed is 484 m/s, and it increases to 967 m/s when the temperature rises to 1200 K. The meaning
of the rms speed and the reason why it is so important will be discussed shortly.
Kinetic Theory If a ball is thrown against a wall, it exerts a force on the wall. As Figure 14.9 suggests, gas particles do the same thing, except that their masses are smaller and their speeds are greater. The
number of particles is so great and they strike the wall so often that the eff ect of their individual
impacts appears as a continuous force. Dividing the magnitude of this force by the area of the
wall gives the pressure exerted by the gas.
To calculate the force, consider an ideal gas composed of N identical particles in a cubical container whose sides have length L. Except for elastic* collisions, these particles do not interact. Figure 14.10 focuses attention on one particle of mass m as it strikes the right wall perpendic- ularly and rebounds elastically. While approaching the wall, the particle has a velocity +υ and linear momentum +mυ (see Section 7.1 for a review of linear momentum). The particle rebounds with a velocity −υ and momentum −mυ, travels to the left wall, rebounds again, and heads back toward the right. The time t between collisions with the right wall is the round-trip distance 2L divided by the speed of the particle; that is, t = 2L/υ. According to Newton’s second law of mo- tion, in the form of the impulse-momentum, the average force exerted on the particle by the wall
is given by the change in the particle’s momentum per unit time:
Average force = Final momentum − Initial momentum Time between successive collisions
(7.4)
= (−mυ) − (+mυ) 2 L/υ
= −mυ2
L
According to Newton’s law of action–reaction, the force applied to the wall by the particle is
equal in magnitude to this value, but oppositely directed (i.e., +mυ2/L). The magnitude F of the total force exerted on the right wall is equal to the number of particles that collide with the wall during the time t multiplied by the average force exerted by each particle. Since the N particles
FIGURE 14.9 The pressure that a gas exerts is caused by the collisions of its molecules
with the walls of the container.
*The term “elastic” is used here to mean that on the average, in a large number of particles, there is no gain or loss of translational kinetic energy because of collisions.
390 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
move randomly in three dimensions, one-third of them on the average strike the right wall during
the time t. Therefore, the total force is
F = (N3 ) ( mυ2 L )
In this result υ2 has been replaced by υ2, the average value of the squared speed. The collection of particles possesses a Maxwell distribution of speeds, so an average value for υ2 must be used, rather than a value for any individual particle. The square root of the quantity υ2 is called the root-mean-square speed, or, for short, the rms speed; υrms = √ υ2. With this substitution, the total force becomes
F = (N3 ) ( mυ2rms
L ) Pressure is force per unit area, so the pressure P acting on a wall of area L2 is
P = F L2
= (N3 ) ( mυ2rms
L3 ) = ( N 3 )(
mυ2rms V )
where V = L3 is the volume of the box. This result can be written as
PV = 23 N ( 1
2 mυ2rms ) (14.5)
Equation 14.5 relates the macroscopic properties of the gas—its pressure and volume—to
the microscopic properties of the constituent particles—their mass and speed. Since the term 1
2 mυ2rms is the average translational kinetic energy KE of an individual particle, it follows that
PV = 23 N (KE)
This result is similar to the ideal gas law, PV = NkT (Equation 14.2). Both equations have identical terms on the left, so the terms on the right must be equal:
2
3 N(KE) = NkT. Therefore,
KE = 1
2 mυ2rms = 3
2 kT (14.6)
Equation 14.6 is signifi cant, because it allows us to interpret temperature in terms of the motion
of gas particles. This equation indicates that the Kelvin temperature is directly proportional to the
average translational kinetic energy per particle in an ideal gas, no matter what the pressure and
volume are. On the average, the particles have greater kinetic energies when the gas is hotter than
when it is cooler. Conceptual Example 5 discusses a common misconception about the relation
between kinetic energy and temperature.
Math Skills It is important to note that the average of the squared speed υ2 is not the same thing as the square of the average speed, which is υ 2. To see why these two quantities are not equal, consider two particles with the following speeds: υA is the speed of particle A and υB is the speed of particle B. To compute the average of the squared speed and the square of the average speed, we proceed in the
usual fashion when computing averages. We calculate each average by adding the two values (one
for particle A and one for particle B) and then dividing the result by 2.
υ2 = υ 2A + υ 2B
2
υ 2 = ( υA + υB
2 ) 2
= υ 2A + 2υAυB + υ 2B
4
Clearly, υ2 is not equal to υ 2.
CONCEPTUAL EXAMPLE 5 Does a Single Particle Have a Temperature?
Each particle in a gas has kinetic energy. Furthermore, the equation 1
2 mυ2rms = 3
2 kT establishes the relationship between the average kinetic energy per particle and the temperature of an ideal gas. Is it valid, then, to
conclude that a single particle has a temperature?
Reasoning and Solution We know that a gas contains an enormous number of particles that are traveling with a distribution of speeds, such
as those indicated by the graphs in Figure 14.8. Therefore, the particles do
not all have the same kinetic energy, but possess a distribution of kinetic
14.3 Kinetic Theory of Gases 391
If two ideal gases have the same temperature, the relation 1
2 mυ2rms = 3
2 kT indicates that the average kinetic energy of each kind of gas particle is the same. In general, however, the rms
speeds of the diff erent particles are not the same, because the masses may be diff erent. Air,
for example, is primarily a mixture of nitrogen N2 (molecular mass = 28.0 u) and oxygen O2
(molecular mass = 32.0 u). If we assume that each behaves like an ideal gas and apply Equation
14.6, we fi nd the rms speeds of nitrogen and oxygen at room temperature (293 K) are 511 m/s
and 478 m/s, respectively. As a comparison, the speed of sound in air at the same temperature
is 343 m/s.
The equation KE = 3
2 kT has also been applied to particles much larger than atoms or molecules. The English botanist Robert Brown (1773–1858) observed through a microscope that
pollen grains suspended in water move on very irregular, zigzag paths. This Brownian motion
can also be observed with other particle suspensions, such as fi ne smoke particles in air. In 1905,
Albert Einstein (1879–1955) showed that Brownian motion could be explained as a response of
the large suspended particles to impacts from the moving molecules of the fl uid medium (e.g.,
water or air). As a result of the impacts, the suspended particles have the same average transla-
tional kinetic energy as the fl uid molecules—namely, KE = 3
2 kT. Unlike the molecules, however, the particles are large enough to be seen through a microscope and, because of their relatively
large mass, have a comparatively small average speed.
The Internal Energy of a Monatomic Ideal Gas Chapter 15 deals with the science of thermodynamics, in which the concept of internal energy
plays an important role. Using the results just developed for the average translational kinetic
energy, we conclude this section by expressing the internal energy of a monatomic ideal gas in a
form that is suitable for use later on.
The internal energy of a substance is the sum of the various kinds of energy that the atoms or
molecules of the substance possess. A monatomic ideal gas is composed of single atoms. These
atoms are assumed to be so small that the mass is concentrated at a point, with the result that the
moment of inertia I about the center of mass is negligible. Thus, the rotational kinetic energy 1
2 Iω2 is also negligible. Vibrational kinetic and potential energies are absent, because the atoms are not connected by chemical bonds and, except for elastic collisions, do not interact. As a result,
the internal energy U is the total translational kinetic energy of the N atoms that constitute the gas: U = N( 12 mυ2rms ) . Since
1
2 mυ2rms = 3
2 kT according to Equation 14.6, the internal energy can be written in terms of the Kelvin temperature as
U = N ( 32 kT )
Usually, U is expressed in terms of the number of moles n, rather than the number of atoms N. Using the fact that Boltzmann’s constant is k = R/NA, where R is the universal gas constant and NA is Avogadro’s number, and realizing that N/NA = n, we fi nd that
Monatomic ideal gas U = 32 nRT (14.7)
Thus, the internal energy depends on the number of moles and the Kelvin temperature of the gas.
In fact, it can be shown that the internal energy is proportional to the Kelvin temperature for any type of ideal gas (e.g., monatomic, diatomic, etc.). For example, when hot-air balloonists turn on the burner, they increase the temperature, and hence the internal energy per mole, of the air inside
the balloon (see Figure 14.11).
energies ranging from very nearly zero to extremely large values. If each
particle had a temperature that was associated with its kinetic energy,
there would be a whole range of diff erent temperatures within the gas.
This is not so, for a gas at thermal equilibrium has only one temperature
(see Section 15.2), a temperature that would be registered by a thermo-
meter placed in the gas. Thus, temperature is a property that characterizes
the gas as a whole, a fact that is inherent in the relation 1
2 mυ2rms = 3
2 kT.
The term υrms is a kind of average particle speed. Therefore, 1
2 mυ 2rms is the average kinetic energy per particle and is characteristic of the gas as a whole. Since the Kelvin temperature is proportional to
1
2 mυ2rms, it is also a characteristic of the gas as a whole and cannot be ascribed to
each gas particle individually. Thus, a single gas particle does not have a temperature.
FIGURE 14.11 When the burner is turned on to heat the air within a hot-air balloon,
the temperature of the air rises. Air behaves
approximately as an ideal gas, for which the
internal energy per mole is proportional to
the Kelvin temperature.
M u st
af a
Q u ra
is h i/
© A
P /W
id e
W o rl
d P
h o to
s
392 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
Check Your Understanding
(The answers are given at the end of the book.) 11. The kinetic theory of gases assumes that, for a given collision time, a gas molecule rebounds with the
same speed after colliding with the wall of a container. If the speed after the collision were less than
the speed before the collision, the duration of the collision remaining the same, would the pressure of
the gas be greater than, equal to, or less than the pressure predicted by kinetic theory?
12. If the temperature of an ideal gas were doubled from 50 to 100 °C, would the average translational kinetic energy of the gas particles also double?
13. The pressure of a monatomic ideal gas doubles, while the volume decreases to one-half its initial value. Does the internal energy of the gas increase, decrease, or remain unchanged?
14. The atoms in a container of helium (He) have the same translational rms speed as the atoms in a container of argon (Ar). Treating each gas as an ideal gas, decide which, if either, has the greater
temperature.
15. The pressure of a monatomic ideal gas is doubled, while its volume is reduced by a factor of four. What is the ratio of the new rms speed of the atoms to the initial rms speed?
14.4 *Diff usion You can smell the fragrance of a perfume at some distance from an open bottle because
perfume molecules leave the space above the liquid in the bottle, where they are relatively con-
centrated, and spread out into the air, where they are less concentrated. During their journey,
they collide with other molecules, so their paths resemble the zigzag paths characteristic of
Brownian motion. The process in which molecules move from a region of higher concentration
to one of lower concentration is called diff usion. Diff usion also occurs in liquids and solids, and Figure 14.12 illustrates ink diff using through water. However, compared to the rate of diff usion in gases, the rate is generally smaller in liquids and even smaller in solids. The host
medium, such as the air or water in the examples above, is referred to as the solvent, while the diff using substance, like the perfume molecules or the ink in Figure 14.12, is known as the solute. Relatively speaking, diff usion is a slow process, even in a gas. Conceptual Example 6 illustrates why.
Initially Later
FIGURE 14.12 A drop of ink placed in water eventually becomes completely dispersed
because of diff usion.
CONCEPTUAL EXAMPLE 6 Why Diff usion Is Relatively Slow
The fragrance from an open bottle of perfume takes several seconds or
sometimes even minutes to reach the other side of a room by the process
of diff usion. Which of the following accounts for the fact that diff usion
is relatively slow? (a) The nature of Brownian motion (b) The relatively slow translational rms speeds that characterize gas molecules at room
temperature
Reasoning The important characteristic of the paths followed by ob- jects in Brownian motion is their zigzag shapes.
Answer (b) is incorrect. A gas molecule near room temperature has a translational rms speed of hundreds of meters per second. Such speeds are
not slow. It would take a molecule traveling at such a speed just a fraction
of a second to cross an ordinary room.
Answer (a) is correct. When a perfume molecule diff uses through air, it makes millions of collisions each second with air molecules. As
Figure 14.13 illustrates, the velocity of the molecule changes abruptly because of each collision, but between collisions, it moves in a straight
line. Although it does move very fast between collisions, a perfume
molecule wanders only slowly away from the bottle because of the
zigzag path. It would take a long time indeed to diff use in this manner
across a room. Usually, however, convection currents are present and
carry the fragrance to the other side of the room in a matter of seconds
or minutes.
Related Homework: Problems 47, 51
FIGURE 14.13 A perfume molecule collides with millions
of air molecules during its
journey, so the path has a
zigzag shape. Although the
air molecules are shown as
stationary, they are also moving.
14.4 Diff usion 393
BIO THE PHYSICS OF . . . drug delivery systems. Diff usion is the basis for drug delivery systems that bypass the need to administer medication orally or via injections.
Interactive Figure 14.14 shows one such system, the transdermal patch. The word “transdermal” means “across the skin.” Such patches, for example, are used to deliver nicotine in programs
designed to help you stop smoking. The patch is attached to the skin using an adhesive, and the
backing of the patch contains the drug within a reservoir. The concentration of the drug in the
reservoir is relatively high, just like the concentration of perfume molecules above the liquid in a
bottle. The drug diff uses slowly through a control membrane and directly into the skin, where its
concentration is relatively low. Diff usion carries it into the blood vessels present in the skin. The
purpose of the control membrane is to limit the rate of diff usion, which can also be adjusted in the
reservoir by dissolving the drug in a neutral material to lower its initial concentration. Another
diff usion-controlled drug delivery system utilizes capsules that are inserted surgically beneath
the skin. Some contraceptives are administered in this fashion. The drug in the capsule diff uses
slowly into the bloodstream over extended periods that can be as long as a year.
The diff usion process can be described in terms of the arrangement in Interactive Figure 14.15a. A hollow channel of length L and cross-sectional area A is fi lled with a fl uid. The left end of the channel is connected to a container in which the solute concentration C2 is relatively high, while the right end is connected to a container in which the solute concentration C1 is lower. These concentrations are defi ned as the total mass of the solute molecules divided by the volume
of the solution (e.g., 0.1 kg/m3). Because of the diff erence in concentration between the ends of
the channel, ΔC = C2 − C1, there is a net diff usion of the solute from the left end to the right end.
Blood
Drug reservoir
Backing
Adhesive
Skin
Control membrane
Blood vessel
INTERACTIVE FIGURE 14.14 Using diff usion, a transdermal patch delivers a drug
directly into the skin, where it enters blood
vessels. The backing contains the drug within
the reservoir, and the control membrane
limits the rate of diff usion into the skin.
(a)
(b)
Heat flow
Cross-sectional area = A
Higher temperature
T2
Lower temperature
T1
Cross-sectional area = A
L
Lower concentration
C1
Higher concentration
C2
Solute mass flow
L
INTERACTIVE FIGURE 14.15 (a) Solute diff uses through the channel from the region
of higher concentration to the region of lower
concentration. (b) Heat is conducted along a bar whose ends are maintained at diff erent
temperatures.
394 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
Interactive Figure 14.15a is similar to Interactive Figure 13.7 for the conduction of heat along a bar, which, for convenience, is reproduced in Interactive Figure 14.15b. When the ends of the bar are maintained at diff erent temperatures, T2 and T1, the heat Q conducted along the bar in a time t is
Q = (kA ∆T ) t
L (13.1)
where ΔT = T2 − T1, and k is the thermal conductivity. Whereas conduction is the fl ow of heat from a region of higher temperature to a region of lower temperature, diff usion is the mass fl ow
of solute from a region of higher concentration to a region of lower concentration. By analogy
with Equation 13.1, it is possible to write an equation for diff usion: (1) replace Q by the mass m of solute that is diff using through the channel, (2) replace ΔT = T2 − T1 by the diff erence in concentrations ΔC = C2 − C1, and (3) replace k by a constant known as the diff usion constant D. The resulting equation, fi rst formulated by the German physiologist Adolf Fick (1829–1901), is
referred to as Fick’s law of diff usion.
FICK’S LAW OF DIFFUSION The mass m of solute that diff uses in a time t through a solvent contained in a channel of length L and cross-sectional area A is*
m = (DA ∆C ) t
L (14.8)
where ΔC is the concentration diff erence between the ends of the channel and D is the diff usion constant. SI Unit for the Diff usion Constant: m2/s
It can be verifi ed from Equation 14.8 that the diff usion constant has units of m2/s, the exact value
depending on the nature of the solute and the solvent. For example, the diff usion constant for ink
in water is diff erent from that for ink in benzene. Example 7 illustrates an important application
of Fick’s law.
EXAMPLE 7 BIO The Physics of Water Loss from Plant Leaves
Large amounts of water can be given off by plants. It has been estimated,
for instance, that a single sunfl ower plant can lose up to a pint of water a
day during the growing season. Figure 14.16 shows a cross-sectional view of a leaf. Inside the leaf, water passes from the liquid phase to the vapor
phase at the walls of the mesophyll cells. The water vapor then diff uses
through the intercellular air spaces and eventually exits the leaf through
small openings, called stomatal pores. The diff usion constant for water
vapor in air is D = 2.4 × 10−5 m2/s. A stomatal pore has a cross-sectional area of about A = 8.0 × 10−11 m2 and a length of about L = 2.5 × 10−5 m. The concentration of water vapor on the interior side of a pore is roughly
C2 = 0.022 kg/m3, whereas the concentration on the outside is approx- imately C1 = 0.011 kg/m3. Determine the mass of water vapor that passes through a stomatal pore in one hour.
Reasoning and Solution Fick’s law of diff usion shows that
m = (DA ∆C ) t
L (14.8)
m = (2.4 × 10−5 m2/s)(8.0 × 10−11 m2)(0.022 kg/m3 − 0.011 kg/m3)(3600 s)
2.5 × 10−5 m
= 3.0 × 10−9 kg
This amount of water may not seem signifi cant. However, a single leaf
may have as many as a million stomatal pores, so the water lost by an
entire plant can be substantial.
C2
Stomatal pore
Intercellular air space
Cuticle Upper epidermis
H2O diffusion
Mesophyll cells
Lower epidermis
C1
L
FIGURE 14.16 A cross- sectional view of a leaf. Water
vapor diff uses out of the leaf
through a stomatal pore.
*Fick’s law assumes that the temperature of the solvent is constant throughout the channel. Experiments indicate that
the diff usion constant depends strongly on the temperature.
Concept Summary 395
Check Your Understanding
(The answers are given at the end of the book.) 16. BIO In the lungs, oxygen in very small sacs called alveoli diff uses into the blood. The diff usion occurs
directly through the walls of the sacs, which have a thickness L. The total eff ective area A across which diff usion occurs is the sum of the individual areas (each quite small) of the various sac walls. Consider-
ing the fact that the mass m of oxygen that enters the blood per second needs to be large and referring to Fick’s law of
diff usion, what can you deduce about L and about the total number of sacs present in the lungs?
17. The same solute is diff using through the same solvent in each of three cases. For each case, CYU Table 14.1 gives the length and cross-sectional area of the diff usion channel.
The concentration diff erence between the ends of the dif-
fusion channel is the same in each case. Rank the diff usion
rates (in kg/s) in descending order (largest fi rst).
Case Length Cross-Sectional
Area (a) 12 L A
(b) L 12 A
(c) 13 L 2A
CYU TABLE 14.1
EXAMPLE 8 BIO The Energy in Your Lungs
How much internal energy is contained in the air within your lungs?
The result might surprise you. The volume of human adult lungs is
approximately 6 liters (6.0 × 10−3 m3), and the pressure in your lungs
is approximately 1 atm (1.0 × 105 Pa). Assume the temperature of the
air is close to internal body temperature or 37 °C (310 K). To simplify
the calculation, we will assume your lungs are fi lled with helium gas,
which is something many of you might have done to make your voice
sound funny!
Reasoning Since we are using helium gas in our calculation, which is monatomic, we can apply Equation 14.7 to calculate its internal energy.
The internal energy depends on n, the number of moles in the gas. This
quantity can be determined by applying the ideal gas law (Equation 14.1)
with the information given in the problem.
Solution We begin by calculating the number of moles of helium gas in the
lungs using Equation 14.1: n = PV RT
= (1.0 × 105 Pa)(6.0 × 10−3 m3)
[8.31 J/ (mol · K)](310 K) =
0.23 mol. Using this value for n, we can apply Equation 14.7 to calculate the internal energy of the gas: 𝑈 =
3
2 𝑛RT = 3
2(0.23 mol)[8.31 J/(mol · K)] (310 K) = 890 J
Is this a large energy? It is! This value is equivalent to the kinetic energy
of a baseball moving at 110 m/s, or almost 250 mph!
Concept Summary 14.1 Molecular Mass, the Mole, and Avogadro’s Number Each element in the periodic table is assigned an atomic mass. One atomic mass unit (u) is
exactly one-twelfth the mass of an atom of carbon-12. The molecular mass
of a molecule is the sum of the atomic masses of its atoms.
n = N NA
(1)
The number of moles n contained in a sample is equal to the number of particles N (atoms or molecules) in the sample divided by the number of particles per mole NA, as shown in Equation 1, where NA is called Avogadro’s number and has a value of NA = 6.022 × 1023 particles per mole. The number of moles is also equal to the mass m of the sample (expressed in grams) divided by the mass per mole (expressed in grams per mole), as shown in
Equation 2. The mass per mole (in g/mol) of a substance has the same numer-
ical value as the atomic or molecular mass of one of its particles (in atomic
mass units).
n = m
Mass per mole (2)
The mass mparticle of a particle (in grams) can be obtained by divid- ing the mass per mole (in g/mol) by Avogadro’s number, according to
Equation 3.
m particle = Mass per mole
NA (3)
14.2 The Ideal Gas Law The ideal gas law relates the absolute pressure P, the volume V, the number n of moles, and the Kelvin temperature T of an ideal gas, according to Equation 14.1, where R = 8.31 J/(mol · K) is the universal gas constant. An alternative form of the ideal gas law is given by
Equation 14.2, where N is the number of particles and k = R NA
is Boltzmann’s
constant. A real gas behaves as an ideal gas when its density is low enough that its particles do not interact, except via elastic collisions.
PV = nRT (14.1) PV = NkT (14.2)
396 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
A form of the ideal gas law that applies when the number of moles and
the temperature are constant is known as Boyle’s law. Using the subscripts
“i” and “f” to denote, respectively, initial and fi nal conditions, we can write
Boyle’s law as in Equation 14.3. A form of the ideal gas law that applies
when the number of moles and the pressure are constant is called Charles’
law and is given by Equation 14.4.
PiVi = PfVf (14.3)
Vi Ti
= Vf Tf
(14.4)
14.3 Kinetic Theory of Gases The distribution of particle speeds in an ideal gas at constant temperature is the Maxwell speed distribution (see
Figure 14.8). The kinetic theory of gases indicates that the Kelvin temperat- ure T of an ideal gas is related to the average translational kinetic energy KE of a particle, according to Equation 14.6, where υrms is the root-mean-square speed of the particles.
KE = 1
2 mυ2rms = 3
2 kT (14.6)
The internal energy U of n moles of a monatomic ideal gas is given by Equation 14.7. The internal energy of any type of ideal gas (e.g., monatomic,
diatomic) is proportional to its Kelvin temperature.
U = 32 nRT (14.7)
14.4 Diff usion Diff usion is the process whereby solute molecules move through a solvent from a region of higher solute concentration to a region of
lower solute concentration. Fick’s law of diff usion states that the mass m of solute that diff uses in a time t through the solvent in a channel of length L and cross-sectional area A is given by Equation 14.8, where ΔC is the solute concentration diff erence between the ends of the channel and D is the diff u- sion constant.
m = (DA ∆C ) t
L (14.8)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 14.1 Molecular Mass, the Mole, and Avogadro’s Number 1. All but one of the following statements are true. Which one is not true? (a) A mass (in grams) equal to the molecular mass (in atomic mass units) of a pure substance contains the same number of molecules, no matter what the
substance is. (b) One mole of any pure substance contains the same num- ber of molecules. (c) Ten grams of a pure substance contains twice as many molecules as fi ve grams of the substance. (d) Ten grams of a pure substance contains the same number of molecules, no matter what the substance is.
(e) Avogadro’s number of molecules of a pure substance and one mole of the substance have the same mass.
2. A mixture of ethyl alcohol (molecular mass = 46.1 u) and water (molecu- lar mass = 18.0 u) contains one mole of molecules. The mixture contains
20.0 g of ethyl alcohol. What mass m of water does it contain?
Section 14.2 The Ideal Gas Law 3. For an ideal gas, each of the following unquestionably leads to an increase in the pressure of the gas, except one. Which one is it? (a) Increasing the tem- perature and decreasing the volume, while keeping the number of moles of
the gas constant (b) Increasing the temperature, the volume, and the number of moles of the gas (c) Increasing the temperature, while keeping the volume and the number of moles of the gas constant (d) Increasing the number of moles of the gas, while keeping the temperature and the volume constant
(e) Decreasing the volume, while keeping the temperature and the number of moles of the gas constant.
4. The cylinder in the drawing contains 3.00 mol of an ideal gas. By moving the piston, the volume of the gas is reduced to one-fourth its initial value,
while the temperature is held constant. How many moles Δn of the gas must be allowed to escape through the valve, so that the pressure of the gas does
not change?
QUESTION 4
Valve
5. Carbon monoxide is a gas at 0 °C and a pressure of 1.01 × 105 Pa. It is a diatomic gas, each of its molecules consisting of one carbon atom (atomic
mass = 12.0 u) and one oxygen atom (atomic mass = 16.0 u). Assuming that
carbon monoxide is an ideal gas, calculate its density 𝜌.
Section 14.3 Kinetic Theory of Gases 6. If the speed of every atom in a monatomic ideal gas were doubled, by what factor would the Kelvin temperature of the gas be multiplied? (a) 4 (b) 2 (c) 1 (d) 12 (e)
1
4
7. The atomic mass of a nitrogen atom (N) is 14.0 u, while that of an oxygen atom (O) is 16.0 u. Three diatomic gases have the same temperature: nitrogen
(N2), oxygen (O2), and nitric oxide (NO). Rank these gases in ascending order
(smallest fi rst), according to the values of their translational rms speeds:
(a) O2, N2, NO (b) NO, N2, O2 (c) N2, NO, O2 (d) O2, NO, N2 (e) N2, O2, NO 8. The pressure of a monatomic ideal gas is doubled, while the volume is cut in half. By what factor is the internal energy of the gas multiplied? (a) 14 (b)
1
2
(c) 1 (d) 2 (e) 4
Section 14.4 Diff usion 9. The following statements concern how to increase the rate of diff usion (in kg/s). All but one statement are always true. Which one is not necessarily true?
(a) Increase the cross-sectional area of the diff usion channel, keeping constant its length and the diff erence in solute concentrations between its ends. (b) In- crease the diff erence in solute concentrations between the ends of the diff usion
channel, keeping constant its cross-sectional area and its length. (c) Decrease the length of the diff usion channel, keeping constant its cross-sectional area
and the diff erence in solute concentrations between its ends. (d) Increase the
Focus on Concepts
Problems 397
cross-sectional area of the diff usion channel, and decrease its length, keeping
constant the diff erence in solute concentrations between its ends. (e) Increase the cross-sectional area of the diff usion channel, increase the diff erence in
solute concentrations between its ends, and increase its length.
10. The diff usion rate for a solute is 4.0 × 10−11 kg/s in a solvent-fi lled chan- nel that has a cross-sectional area of 0.50 cm2 and a length of 0.25 cm. What
would be the diff usion rate m/t in a channel with a cross-sectional area of 0.30 cm2 and a length of 0.10 cm?
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
Note: The pressures referred to in these problems are absolute pressures, unless indicated otherwise.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 14.1 Molecular Mass, the Mole, and Avogadro’s Number 1. E SSM Hemoglobin has a molecular mass of 64 500 u. Find the mass (in kg) of one molecule of hemoglobin.
2. E BIO Manufacturers of headache remedies routinely claim that their own brands are more potent pain relievers than the competing brands. Their
way of making the comparison is to compare the number of molecules in the
standard dosage. Tylenol uses 325 mg of acetaminophen (C8H9NO2) as the
standard dose, whereas Advil uses 2.00 × 102 mg of ibuprofen (C13H18O2).
Find the number of molecules of pain reliever in the standard doses of
(a) Tylenol and (b) Advil. 3. E A mass of 135 g of a certain element is known to contain 30.1 × 1023 atoms. What is the element?
4. E GO A certain element has a mass per mole of 196.967 g/mol. What is the mass of a single atom in (a) atomic mass units and (b) kilograms? (c) How many moles of atoms are in a 285-g sample? 5. E BIO SSM The active ingredient in the allergy medication Claritin con- tains carbon (C), hydrogen (H), chlorine (Cl), nitrogen (N), and oxygen (O).
Its molecular formula is C22H23ClN2O2. The standard adult dosage utilizes
1.572 × 1019 molecules of this species. Determine the mass (in grams) of the
active ingredient in the standard dosage.
6. E GO The chlorophyll-a molecule (C55H72MgN4O5) is important in photosynthesis. (a) Determine its molecular mass (in atomic mass units). (b) What is the mass (in grams) of 3.00 moles of chlorophyll-a molecules? 7. M V-HINT A runner weighs 580 N (about 130 lb), and 71% of this weight is water. (a) How many moles of water are in the runner’s body? (b) How many water molecules (H2O) are there?
8. M GO Consider a mixture of three diff erent gases: 1.20 g of argon (mole- cular mass = 39.948 g/mol), 2.60 g of neon (molecular mass = 20.180 g/
mol), and 3.20 g of helium (molecular mass = 4.0026 g/mol). For this mix-
ture, determine the percentage of the total number of atoms that corresponds
to each of the components.
9. M BIO SSM The preparation of homeopathic “remedies” involves the re- peated dilution of solutions containing an active ingredient such as arsenic
trioxide (As2O3). Suppose one begins with 18.0 g of arsenic trioxide dis-
solved in water, and repeatedly dilutes the solution with pure water, each
dilution reducing the amount of arsenic trioxide remaining in the solution
by a factor of 100. Assuming perfect mixing at each dilution, what is the
maximum number of dilutions one may perform so that at least one molecule
of arsenic trioxide remains in the diluted solution? For comparison, homeo-
pathic “remedies” are commonly diluted 15 or even 30 times.
10. M V-HINT A cylindrical glass of water (H2O) has a radius of 4.50 cm and a height of 12.0 cm. The density of water is 1.00 g/cm3. How many moles of
water molecules are contained in the glass?
Section 14.2 The Ideal Gas Law 11. E SSM It takes 0.16 g of helium (He) to fi ll a balloon. How many grams of nitrogen (N2) would be required to fi ll the balloon to the same pressure,
volume, and temperature?
12. E A 0.030-m3 container is initially evacuated. Then, 4.0 g of water is placed in the container, and, after some time, all the water evaporates. If the
temperature of the water vapor is 388 K, what is its pressure?
13. E An ideal gas at 15.5 °C and a pressure of 1.72 × 105 Pa occupies a volume of 2.81 m3. (a) How many moles of gas are present? (b) If the volume is raised to 4.16 m3 and the temperature raised to 28.2 °C, what will be the
pressure of the gas?
14. E GO Four closed tanks, A, B, C, and D, each contain an ideal gas. The table gives the absolute pressure and volume of the gas in each tank. In each
case, there is 0.10 mol of gas. Using this number and the data in the table,
compute the temperature of the gas in each tank.
A B C D Absolute pressure (Pa) 25.0 30.0 20.0 2.0
Volume (m3) 4.0 5.0 5.0 75
15. E BIO CHALK SSM A young male adult takes in about 5.0 × 10−4 m3 of fresh air during a normal breath. Fresh air contains approximately 21%
oxygen. Assuming that the pressure in the lungs is 1.0 × 105 Pa and that air is
an ideal gas at a temperature of 310 K, fi nd the number of oxygen molecules
in a normal breath.
16. E A Goodyear blimp typically contains 5400 m3 of helium (He) at an absolute pressure of 1.1 × 105 Pa. The temperature of the helium is 280 K.
What is the mass (in kg) of the helium in the blimp?
17. E A clown at a birthday party has brought along a helium cylinder, with which he intends to fi ll balloons. When full, each balloon contains
0.034 m3 of helium at an absolute pressure of 1.2 × 105 Pa. The cylinder
contains helium at an absolute pressure of 1.6 × 107 Pa and has a volume of
0.0031 m3. The temperature of the helium in the tank and in the balloons is
the same and remains constant. What is the maximum number of balloons
that can be fi lled?
18. E GO The volume of an ideal gas is held constant. Determine the ratio P2/P1 of the fi nal pressure to the initial pressure when the temperature of the gas rises (a) from 35.0 to 70.0 K and (b) from 35.0 to 70.0 °C. 19. E SSM Available in WileyPLUS.
Problems
398 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
20. E Two ideal gases have the same mass density and the same absolute pressure. One of the gases is helium (He), and its temperature is 175 K. The
other gas is neon (Ne). What is the temperature of the neon?
21. E On the sunlit surface of Venus, the atmospheric pressure is 9.0 × 106 Pa, and the temperature is 740 K. On the earth’s surface the atmospheric
pressure is 1.0 × 105 Pa, while the surface temperature can reach 320 K.
These data imply that Venus has a “thicker” atmosphere at its surface than
does the earth, which means that the number of molecules per unit volume
(N/V) is greater on the surface of Venus than on the earth. Find the ratio (N/V)Venus/(N/V)Earth. 22. E V-HINT A tank contains 0.85 mol of molecular nitrogen (N2). Deter- mine the mass (in grams) of nitrogen that must be removed from the tank in order to lower the pressure from 38 to 25 atm. Assume that the volume and
temperature of the nitrogen in the tank do not change.
23. M V-HINT Multiple-Concept Example 4 reviews the principles that play roles in this problem. A primitive diving bell consists of a cylindrical tank with one end open and one end closed. The tank is lowered into a freshwater lake,
open end downward. Water rises into the tank, compressing the trapped air,
whose temperature remains constant during the descent. The tank is brought
to a halt when the distance between the surface of the water in the tank and the
surface of the lake is 40.0 m. Atmospheric pressure at the surface of the lake
is 1.01 × 105 Pa. Find the fraction of the tank’s volume that is fi lled with air.
24. M GO A tank contains 11.0 g of chlorine gas (Cl2) at a temperature of 82 °C and an absolute pressure of 5.60 × 105 Pa. The mass per mole of Cl2 is
70.9 g/mol. (a) Determine the volume of the tank. (b) Later, the temperature of the tank has dropped to 31 °C and, due to a leak, the pressure has dropped
to 3.80 × 105 Pa. How many grams of chlorine gas have leaked out of the tank?
25. M CHALK MMH The dimensions of a room are 2.5 m × 4.0 m × 5.0 m. Assume that the air in the room is composed of 79% nitrogen (N2) and 21%
oxygen (O2). At a temperature of 22 °C and a pressure of 1.01 × 10 5 Pa, what
is the mass (in grams) of the air?
26. M GO The drawing shows an ideal gas confi ned to a cylinder by a massless piston that is attached to an
ideal spring. Outside the cylinder is a vacuum. The
cross-sectional area of the piston is A = 2.50 × 10−3 m2. The initial pressure, volume, and temperature of the gas
are, respectively, P0, V0 = 6.00 × 10−4 m3, and T0 = 273 K, and the spring is initially stretched by an amount x0 = 0.0800 m with respect to its unstrained length. The gas
is heated, so that its fi nal pressure, volume, and temper-
ature are Pf, Vf, and Tf, and the spring is stretched by an amount xf = 0.1000 m with respect to its unstrained length. What is the fi nal temperature of the gas?
27. M SSM Multiple-Concept Example 4 and Conceptual Example 3 are pertinent to this problem. A bubble, located 0.200 m beneath the surface in
a glass of beer, rises to the top. The air pressure at the top is 1.01 × 105 Pa.
Assume that the density of beer is the same as that of fresh water. If the tem-
perature and number of moles of CO2 in the bubble remain constant as the
bubble rises, fi nd the ratio of the bubble’s volume at the top to its volume at
the bottom.
28. M V-HINT The relative humidity is 55% on a day when the temperature is 30.0 °C. Using the graph that accompanies Problem 75 in Chapter 12,
determine the number of moles of water vapor per cubic meter of air.
29. M MMH One assumption of the ideal gas law is that the atoms or mo- lecules themselves occupy a negligible volume. Verify that this assumption is
reasonable by considering gaseous xenon (Xe). Xenon has an atomic radius
of 2.0 × 10−10 m. For STP conditions, calculate the percentage of the total
volume occupied by the atoms.
30. H A spherical balloon is made from an amount of material whose mass is 3.00 kg. The thickness of the material is negligible compared to the 1.50-m
radius of the balloon. The balloon is fi lled with helium (He) at a temperature
of 305 K and just fl oats in air, neither rising nor falling. The density of the
surrounding air is 1.19 kg/m3. Find the absolute pressure of the helium gas.
31. H SSM Available in WileyPLUS. 32. H The mass of a hot-air balloon and its occupants is 320 kg (excluding the hot air inside the balloon). The air outside the balloon has a pressure
of 1.01 × 105 Pa and a density of 1.29 kg/m3. To lift off , the air inside the
balloon is heated. The volume of the heated balloon is 650 m3. The pressure
of the heated air remains the same as the pressure of the outside air. To what
temperature (in kelvins) must the air be heated so that the balloon just lifts
off? The molecular mass of air is 29 u.
Section 14.3 Kinetic Theory of Gases 33. E SSM MMH Very fi ne smoke particles are suspended in air. The trans- lational rms speed of a smoke particle is 2.8 × 10−3 m/s, and the temperature
is 301 K. Find the mass of a particle.
34. E GO Four tanks A, B, C, and D are fi lled with monatomic ideal gases. For each tank, the mass of an individual atom and the rms speed of the atoms
are expressed in terms of m and υrms, respectively (see the table). Suppose that m = 3.32 × 10−26 kg, and υrms = 1223 m/s. Find the temperature of the gas in each tank.
A B C D Mass m m 2m 2m
Rms speed υrms 2υrms υrms 2υrms
35. E GO Suppose a tank contains 680 m3 of neon (Ne) at an absolute pres- sure of 1.01 × 105 Pa. The temperature is changed from 293.2 to 294.3 K.
What is the increase in the internal energy of the neon?
36. E Two moles of an ideal gas are placed in a container whose volume is 8.5 × 10−3 m3. The absolute pressure of the gas is 4.5 × 105 Pa. What is the
average translational kinetic energy of a molecule of the gas?
37. E SSM Available in WileyPLUS. 38. E Two gas cylinders are identical. One contains the monatomic gas argon (Ar), and the other contains an equal mass of the monatomic gas
krypton (Kr). The pressures in the cylinders are the same, but the temperatures
are diff erent. Determine the ratio KEKrypton
KEArgon of the average kinetic energy of a
krypton atom to the average kinetic energy of an argon atom. 39. E Available in WileyPLUS. 40. E A container holds 2.0 mol of gas. The total average kinetic energy of the gas molecules in the container is equal to the kinetic energy of an 8.0 × 10−3-kg
bullet with a speed of 770 m/s. What is the Kelvin temperature of the gas?
41. M CHALK MMH The temperature near the surface of the earth is 291 K. A xenon atom (atomic mass = 131.29 u) has a kinetic energy equal to the average
translational kinetic energy and is moving straight up. If the atom does not collide
with any other atoms or molecules, how high up will it go before coming to rest?
Assume that the acceleration due to gravity is constant throughout the ascent.
42. M GO Compressed air can be pumped underground into huge caverns as a form of energy storage. The volume of a cavern is 5.6 × 105 m3, and the pres-
sure of the air in it is 7.7 × 106 Pa. Assume that air is a diatomic ideal gas whose
internal energy U is given by U = 52 nRT. If one home uses 30.0 kW · h of energy per day, how many homes could this internal energy serve for one day?
43. H SSM Available in WileyPLUS. 44. H A cubical box with each side of length 0.300 m contains 1.000 moles of neon gas at room temperature (293 K). What is the average rate (in atoms/s)
at which neon atoms collide with one side of the container? The mass of a
single neon atom is 3.35 × 10−26 kg.
Piston
PROBLEM 26
Additional Problems 399
Section 14.4 Diff usion 45. E BIO Insects do not have lungs as we do, nor do they breathe through their mouths. Instead, they have a system of tiny tubes, called tracheae, through
which oxygen diff uses into their bodies. The tracheae begin at the surface of an
insect’s body and penetrate into the interior. Suppose that a trachea is 1.9 mm
long with a cross-sectional area of 2.1 × 10−9 m2. The concentration of oxygen
in the air outside the insect is 0.28 kg/m3, and the diff usion constant is 1.1 ×
10−5 m2/s. If the mass per second of oxygen diff using through a trachea is 1.7 ×
10−12 kg/s, fi nd the oxygen concentration at the interior end of the tube.
46. E A tube has a length of 0.015 m and a cross-sectional area of 7.0 × 10−4 m2. The tube is fi lled with a solution of sucrose in water. The diff usion
constant of sucrose in water is 5.0 × 10−10 m2/s. A diff erence in concentration
of 3.0 × 10−3 kg/m3 is maintained between the ends of the tube. How much time
is required for 8.0 × 10−13 kg of sucrose to be transported through the tube?
47. E Available in WileyPLUS. 48. E GO The diff usion constant for the amino acid glycine in water has a value of 1.06 × 10−9 m2/s. In a 2.0-cm-long tube with a cross-sectional area of
1.5 × 10−4 m2, the mass rate of diff usion is m/t = 4.2 × 10−14 kg/s, because the glycine concentration is maintained at a value of 8.3 × 10−3 kg/m3 at one end of
the tube and at a lower value at the other end. What is the lower concentration?
49. E SSM A large tank is fi lled with methane gas at a concentration of 0.650 kg/m3. The valve of a 1.50-m pipe connecting the tank to the atmosphere
is inadvertently left open for twelve hours. During this time, 9.00 × 10−4 kg
of methane diff uses out of the tank, leaving the concentration of meth-
ane in the tank essentially unchanged. The diff usion constant for methane
in air is 2.10 × 10−5 m2/s. What is the cross-sectional area of the pipe?
Assume that the concentration of methane in the atmosphere is zero.
50. M V-HINT Carbon tetrachloride (CCl4) is diff using through benzene (C6H6), as the drawing illustrates. The concentration of CCl4 at the left end
of the tube is maintained at 1.00 × 10−2 kg/m3, and the diff usion constant is
20.0 × 10−10 m2/s. The CCl4 enters the tube at a mass rate of 5.00 × 10 −13 kg/s.
Using these data and those shown in the drawing, fi nd (a) the mass of CCl4 per second that passes point A and (b) the concentration of CCl4 at point A.
PROBLEM 50
Cross-sectional area = 3.00 × 10–4 m2
5.00 × 10–3 m
A
CCI4 + C6H6
51. M SSM Available in WileyPLUS. 52. H Available in WileyPLUS.
53. E At the start of a trip, a driver adjusts the absolute pressure in her tires to be 2.81 × 105 Pa when the outdoor temperature is 284 K. At the end of the
trip she measures the pressure to be 3.01 × 105 Pa. Ignoring the expansion of
the tires, fi nd the air temperature inside the tires at the end of the trip.
54. E GO When you push down on the handle of a bicycle pump, a piston in the pump cylinder compresses the air inside the cylinder. When the pressure in
the cylinder is greater than the pressure inside the inner tube to which the pump
is attached, air begins to fl ow from the pump to the inner tube. As a biker slowly
begins to push down the handle of a bicycle pump, the pressure inside the cyl-
inder is 1.0 × 105 Pa, and the piston in the pump is 0.55 m above the bottom of
the cylinder. The pressure inside the inner tube is 2.4 × 105 Pa. How far down
must the biker push the handle before air begins to fl ow from the pump to the
inner tube? Ignore the air in the hose connecting the pump to the inner tube, and
assume that the temperature of the air in the pump cylinder does not change.
55. E SSM In a diesel engine, the piston compresses air at 305 K to a volume that is one-sixteenth of the original volume and a pressure that is
48.5 times the original pressure. What is the temperature of the air after the
compression?
56. E GO When a gas is diff using through air in a diff usion channel, the diff usion rate is the number of gas atoms per second diff using from one end
of the channel to the other end. The faster the atoms move, the greater is the
diff usion rate, so the diff usion rate is proportional to the rms speed of the
atoms. The atomic mass of ideal gas A is 1.0 u, and that of ideal gas B is
2.0 u. For diff usion through the same channel under the same conditions, fi nd
the ratio of the diff usion rate of gas A to the diff usion rate of gas B.
57. E SSM Available in WileyPLUS. 58. E Near the surface of Venus, the rms speed of carbon dioxide molecules (CO2) is 650 m/s. What is the temperature (in kelvins) of the atmosphere at
that point?
59. E BIO SSM Oxygen for hospital patients is kept in special tanks, where the oxygen has a pressure of 65.0 atmospheres and a temperature of 288 K.
The tanks are stored in a separate room, and the oxygen is pumped to the
patient’s room, where it is administered at a pressure of 1.00 atmosphere and
a temperature of 297 K. What volume does 1.00 m3 of oxygen in the tanks
occupy at the conditions in the patient’s room?
60. M GO At the normal boiling point of a material, the liquid phase has a density of 958 kg/m3, and the vapor phase has a density of 0.598 kg/m3. The
average distance between neighboring molecules in the vapor phase is dvapor. The average distance between neighboring molecules in the liquid phase is
dliquid. Determine the ratio dvapor/dliquid. (Hint: Assume that the volume of each phase is fi lled with many cubes, with one molecule at the center of each cube.) 61. M V-HINT Available in WileyPLUS. 62. M GO Helium (He), a monatomic gas, fi lls a 0.010-m3 container. The pressure of the gas is 6.2 × 105 Pa. How long would a 0.25-hp engine have
to run (1 hp = 746 W) to produce an amount of energy equal to the internal
energy of this gas?
63. H BIO Available in WileyPLUS. 64. H A gas fi lls the right portion of a hori- zontal cylinder whose radius is 5.00 cm. The
initial pressure of the gas is 1.01 × 105 Pa.
A frictionless movable piston separates the
gas from the left portion of the cylinder,
which is evacuated and contains an ideal
spring, as the drawing shows. The piston is
initially held in place by a pin. The spring is initially unstrained, and the length
of the gas-fi lled portion is 20.0 cm. When the pin is removed and the gas is
allowed to expand, the length of the gas-fi lled chamber doubles. The initial
and fi nal temperatures are equal. Determine the spring constant of the spring.
65. M GO SSM Air is primarily a mixture of nitrogen N2 (molecular mass = 28.0 u) and oxygen O2 (molecular mass = 32.0 u). Assume that each behaves
like an ideal gas and determine the rms speed of the nitrogen and oxygen
molecules when the air temperature is 293 K.
Additional Problems
Unstrained spring Pin
PROBLEM 64
400 CHAPTER 14 The Ideal Gas Law and Kinetic Theory
This chapter introduces the ideal gas law, which is a relation between the
pressure, volume, temperature, and number of moles of an ideal gas. In
Section 10.1, we examined how the compression of a spring depends on the
forced applied to it. Problem 66 reviews how a gas produces a force and why
an ideal gas at diff erent temperatures causes a spring to compress by diff er-
ent amounts. The kinetic theory of gases is important because it allows us to
understand the relation between the macroscopic properties of a gas, such as
pressure and temperature, and the microscopic properties of molecules, such
as speed and mass. Problem 67 reveals the essential features of this theory.
66. M CHALK The fi gure shows three identical chambers containing a piston and a spring whose spring constant is k = 5.8 × 104 N/m. The chamber in part a is completely evacuated, and the piston just touches its left end. In this position, the spring is unstrained. In part b of the drawing, 0.75 mol of ideal gas 1 is introduced into the space between the left end of the chamber and the
piston, and the spring compresses by x1 = 15 cm. In part c, 0.75 mol of ideal gas 2 is introduced into the space between the left end of the chamber and the
piston, and the spring compresses by x2 = 24 cm. Concepts: (i) Which gas exerts a greater force on the piston? (ii) How is the force required to compress
a spring related to the displacement of the spring from the unstrained posi-
tion? (iii) Which gas exerts the greater pressure on the piston? (iv) Which gas
has the greater temperature? Calculations: Find the temperature of each gas. 67. M CHALK SSM In outer space the density of matter is extremely low, about one atom per cm3. The matter is mainly hydrogen atoms (m = 1.67 × 10−27 kg) whose rms speed is 260 m/s. A cubical box, 2.0 m on a side, is
placed in outer space, and the hydrogen atoms are allowed to enter. Concepts: (i) Why do hydrogen atoms exert a force on the wall of the box? (ii) Do the
atoms generate a pressure on the walls of the box? (iii) Do hydrogen atoms
in outer space have a temperature? If so, how is the temperature related to
the microscopic properties of the atoms? Calculations: (a) What is the mag- nitude of the force that the atoms exert on one wall of the box? (b) Determine the pressure that the atoms exert. (c) Does outer space have a temperature and, if so, what is it?
Concepts and Calculations Problems
Unstrained spring
Piston
Evacuated
(a)
Gas 1
x1
(b)
Evacuated
x2
Gas 2 (c)
Evacuated
PROBLEM 66
68. M A Gas Dosing Device. You and your team are given the task of designing a crude system to portion out a specifi c amount (moles) of
krypton (Kr) gas. You brainstorm and come up with the idea of a device
that consists of a cylinder (D = 11.0 cm) with a spring-loaded piston. The side of the piston with the spring is at atmospheric pressure. Krypton gas
is introduced into the cylinder on the other side of the piston (without the
spring), and the piston moves and compresses from its equilibrium position.
When the spring is in its equilibrium position, the piston is at the very end
of the cylinder, and the gas volume is zero. (a) If the spring (k = 8.20 × 104 N/m) compresses 12.5 cm when the Kr gas is introduced into the cylinder,
how many moles of Kr are contained in the cylinder? Treat it as an ideal,
monatomic gas, and assume that the temperature of the gas has equilibrated
with the outside environment (T = 72.0 °F) when you measure the com- pressed distance. (b) How far should the spring compress for 1.5 moles of Kr gas (at T = 72.0 °F)?
68. M An Underwater Gas Piston. You and your team have been given the task of preparing a gas piston device that is to be deployed to the bottom
of the Southern Sea, beneath the Brunt Ice Shelf off the coast of Antarctica.
The inner volume of the cylinder has a diameter of 9.00 cm and a length of
25.0 cm, and is fi tted with a movable piston that compresses the argon (Ar)
gas that it contains. Before deployment, the piston is located and held at the
very top of the cylinder, providing the maximum volume for the gas. When
the device is submerged, however, the piston will move inward due to the
water pressure created by the depth, and the change in temperature of the gas.
The device is to be taken to a depth of 350 m in salt water (density ρ = 1.03 g/cm3) at a temperature of 33.0 °F. If the maximum allowable compression
distance of the piston is 13.0 cm, what is the minimum gas pressure that must
be attained when the device is fi lled at the surface (at atmospheric pressure
and T = 59.0 °F) to prevent the maximum displacement of the piston from exceeding its maximum (13.0 cm) when submerged to a depth of 350 m?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
15.1 Identify thermodynamic systems and their surroundings.
15.2 Define the zeroth law of thermodynamics.
15.3 Define the first law of thermodynamics.
15.4 Analyze thermal processes.
15.5 Analyze thermal processes in an ideal gas.
15.6 Distinguish between diff erent forms of heat capacity.
15.7 Define the second law of thermodynamics.
15.8 Analyze heat engines.
15.9 Analyze Carnot engines.
15.10 Analyze the operation of refrigerators, air conditioners, and heat pumps.
15.11 Calculate the change in entropy in a thermodynamic process.
15.12 Define the third law of thermodynamics.
C h ri
st o p h er
F u rl
o n g /G
et ty
I m
ag es
CHAPTER 15
Thermodynamics
The heat associated with molten steel is part of every day on the job for this foundryman. The laws that
govern heat and work form the basis of thermodynamics, the subject of this chapter.
15.1 Thermodynamic Systems and Their Surroundings We have studied heat (Chapter 12) and work (Chapter 6) as separate topics. Often,
however, they occur simultaneously. In an automobile engine, for instance, fuel is
burned at a relatively high temperature, some of its internal energy is used for doing
the work of driving the pistons up and down, and the excess heat is removed by the
cooling system to prevent overheating. Thermodynamics is the branch of physics that is built upon the fundamental laws that heat and work obey.
In thermodynamics the collection of objects on which attention is being focused
is called the system, while everything else in the environment is called the surround- ings. For example, the system in an automobile engine could be the burning gaso- line, whereas the surroundings would then include the pistons, the exhaust system, the
radiator, and the outside air. The system and its surroundings are separated by walls
of some kind. Walls that permit heat to fl ow through them, such as those of the engine
block, are called diathermal walls. Perfectly insulating walls that do not permit heat to fl ow between the system and its surroundings are known as adiabatic walls.
To understand what the laws of thermodynamics have to say about the relation-
ship between heat and work, it is necessary to describe the physical condition or state of a system. We might be interested, for instance, in the hot air within one of the bal- loons in Figure 15.1. The hot air itself would be the system, and the skin of the balloon provides the walls that separate this system from the surrounding cooler air. The state
of the system would be specifi ed by giving values for the pressure, volume, temperature,
and mass of the hot air. 401
402 CHAPTER 15 Thermodynamics
As this chapter discusses, there are four laws of thermodynamics. We begin with the one
known as the zeroth law and then consider the remaining three.
15.2 The Zeroth Law of Thermodynamics The zeroth law of thermodynamics deals with the concept of thermal equilibrium. Two systems are said to be in thermal equilibrium if there is no net fl ow of heat between them when they are
brought into thermal contact. For instance, you are defi nitely not in thermal equilibrium with the water in Lake Michigan in January. Just dive into it, and you will fi nd out how quickly your
body loses heat to the frigid water. To help explain the central idea of the zeroth law of thermo-
dynamics, Figure 15.2a shows two systems labeled A and B. Each is within a container whose adiabatic walls are made from insulation that prevents the fl ow of heat, and each has the same
temperature, as indicated by a thermometer. In part b, one wall of each container is replaced by a thin silver sheet, and the two sheets are touched together. Silver has a large thermal conductivity,
so heat fl ows through it readily and the silver sheets behave as diathermal walls. Even though
the diathermal walls would permit it, no net fl ow of heat occurs in part b, indicating that the two systems are in thermal equilibrium. There is no net fl ow of heat because the two systems have
the same temperature. We see, then, that temperature is the indicator of thermal equilibrium in the sense that there is no net fl ow of heat between two systems in thermal contact that have the same temperature.
In Figure 15.2 the thermometer plays an important role. System A is in equilibrium with the thermometer, and so is system B. In each case, the thermometer registers the same temperature,
thereby indicating that the two systems are equally hot. Consequently, systems A and B are found
to be in thermal equilibrium with each other. In eff ect, the thermometer is a third system. The
fact that system A and system B are each in thermal equilibrium with this third system at the
same temperature means that they are in thermal equilibrium with each other. This fi nding is an
example of the zeroth law of thermodynamics.
THE ZEROTH LAW OF THERMODYNAMICS Two systems individually in thermal equilibrium with a third system* are in thermal equilibrium with each other.
The zeroth law establishes temperature as the indicator of thermal equilibrium and implies
that all parts of a system must be in thermal equilibrium if the system is to have a defi nable
single temperature. In other words, there can be no fl ow of heat within a system that is in thermal
equilibrium.
15.3 The First Law of Thermodynamics The atoms and molecules of a substance have kinetic and potential energy. These and other kinds
of molecular energy constitute the internal energy of a substance. When a substance participates
in a process involving energy in the form of work and heat, the internal energy of the substance
can change. The relationship between work, heat, and changes in the internal energy is known
as the fi rst law of thermodynamics. We will now see that the fi rst law of thermodynamics is an
expression of the conservation of energy.
Suppose that a system gains heat Q and that this is the only eff ect occurring. Consistent with the law of conservation of energy, the internal energy of the system increases from an initial value
of Ui to a fi nal value of Uf, the change being ΔU = Uf − Ui = Q. In writing this equation, we use the following convention.
Problem-Solving Insight Heat Q is positive when the system gains heat and negative when the system loses heat.
FIGURE 15.1 The air in one of these hot-air balloons is one example of a thermodynamic
system.
Steve Vidler/SuperStock
Same temperature
A
A
B
Adiabatic walls
(a)
Diathermal walls (silver) (b)
B
FIGURE 15.2 (a) Systems A and B are surrounded by adiabatic walls and register
the same temperature on a thermometer.
(b) When system A is put into thermal contact with system B through diathermal
walls, no net fl ow of heat occurs between
the systems. *The state of the third system is the same when it is in thermal equilibrium with either of the two systems. In Figure 15.2, for example, the mercury level is the same in the thermometer in either system.
15.3 The First Law of Thermodynamics 403
The internal energy of a system can also change because of work. If a system does work W on its surroundings and there is no heat fl ow, energy conservation indicates that the internal energy of
the system decreases from Ui to Uf, the change now being ΔU = Uf − Ui = −W. The minus sign is included with the work because we employ the following convention.
Problem-Solving Insight Work is positive when it is done by the system and negative when it is done on the system.
A system can gain or lose energy simultaneously in the form of heat Q and work W. The change in internal energy due to both factors is given by Equation 15.1. Thus, the fi rst law of thermo- dynamics is just the conservation-of-energy principle applied to heat, work, and the change in the internal energy.
THE FIRST LAW OF THERMODYNAMICS The internal energy of a system changes from an initial value Ui to a fi nal value of Uf due to heat Q and work W:
∆U = Uf − Ui = Q − W (15.1)
Q is positive when the system gains heat and negative when it loses heat. W is positive when work is done by the system and negative when work is done on the system.
Example 1 illustrates the use of Equation 15.1 and the sign conventions for Q and W.
EXAMPLE 1 Positive and Negative Work
Interactive Figure 15.3 illustrates a system and its surroundings. In part a, the system gains 1500 J of heat from its surroundings, and 2200 J of work is done by the system on the surroundings. In part b, the system also gains 1500 J of heat, but 2200 J of work is done on the system by the surroundings. In each case, determine the change in the internal energy
of the system.
Reasoning In Interactive Figure 15.3a the system loses more energy in doing work than it gains in the form of heat, so the internal energy of
the system decreases. Thus, we expect the change in the internal energy,
ΔU = Uf − Ui, to be negative. In part b of the drawing, the system gains energy in the form of both heat and work. The internal energy of the system
increases, and we expect ΔU to be positive.
Problem-Solving Insight When using the fi rst law of ther- modynamics, as expressed by Equation 15.1, be careful to follow the proper sign conventions for the heat Q and the work W.
Solution (a) The heat is positive, Q = +1500 J, since it is gained by the system. The work is positive, W = +2200 J, since it is done by the system. According to the fi rst law of thermodynamics
∆U = Q − W = (+1500 J) − (+2200 J) = −700 J (15.1)
The minus sign for ΔU indicates that the internal energy has decreased, as expected.
(b) The heat is positive, Q = +1500 J, since it is gained by the system. But the work is negative, W = −2200 J, since it is done on the system. Thus,
∆U = Q − W = (+1500 J) − (−2200 J) = +3700 J (15.1)
The plus sign for ΔU indicates that the internal energy has increased, as expected.
System
Surroundings
Work Heat
(a)
System
Surroundings
Work
(b)
Heat
INTERACTIVE FIGURE 15.3 (a) The system gains energy in the form of heat but loses
energy because work is done by the system.
(b) The system gains energy in the form of heat and also gains energy because work is
done on the system.
In the fi rst law of thermodynamics, the internal energy U, heat Q, and work W are energy quantities, and each is expressed in energy units such as joules. However, there is a fundamental
diff erence between U, on the one hand, and Q and W on the other. The next example sets the stage for explaining this diff erence.
404 CHAPTER 15 Thermodynamics
To understand the diff erence between U and either Q or W, consider the value for ΔU in Example 2. In both methods ΔU is the same. Its value is determined once the initial and fi nal temperatures are specifi ed because the internal energy of an ideal gas depends only on the tem-
perature. Temperature is one of the variables (along with pressure and volume) that defi ne the
state of a system.
Problem-Solving Insight The internal energy depends only on the state of a system, not on the method by which the system arrives at a given state.
In recognition of this characteristic, internal energy is referred to as a function of state.* In contrast, heat and work are not functions of state because they have diff erent values for each
diff erent method used to make the system change from one state to another, as in Example 2.
Check Your Understanding
(The answer is given at the end of the book.) 1. A gas is enclosed within a chamber that is fi tted with a frictionless piston. The piston is then pushed in,
thereby compressing the gas. Which statement below regarding this process is consistent with the fi rst
law of thermodynamics? (a) The internal energy of the gas will increase. (b) The internal energy of the gas will decrease. (c) The internal energy of the gas will not change. (d) The internal energy of the gas may increase, decrease, or remain the same, depending on the amount of heat that the gas gains or loses.
15.4 Thermal Processes A system can interact with its surroundings in many ways, and the heat and work that come into
play always obey the fi rst law of thermodynamics. This section introduces four common thermal
processes. In each case, the process is assumed to be quasi-static, which means that it occurs slowly enough that a uniform pressure and temperature exist throughout all regions of the system
at all times.
An isobaric process is one that occurs at constant pressure. For instance, Figure 15.4 shows a substance (solid, liquid, or gas) contained in a chamber fi tted with a frictionless piston. The pres-
sure P experienced by the substance is always the same, because it is determined by the external atmosphere and the weight of the piston and the block resting on it. Heating the substance makes
EXAMPLE 2 An Ideal Gas
The temperature of three moles of a monatomic ideal gas is reduced from
Ti = 540 K to Tf = 350 K by two diff erent methods. In the fi rst method 5500 J of heat fl ows into the gas, whereas in the second, 1500 J of heat
fl ows into it. In each case fi nd (a) the change in the internal energy and (b) the work done by the gas.
Reasoning Since the internal energy of a monatomic ideal gas is U = 32 nRT (Equation 14.7) and since the number of moles n is fi xed, only a change in temperature T can alter the internal energy. Because the change in T is the same in both methods, the change in U is also the same. From the given temperatures, the change ΔU in internal energy can be deter- mined. Then, the fi rst law of thermodynamics can be used with ΔU and the given heat values to calculate the work for each of the methods.
Solution (a) Using Equation 14.7 for the internal energy of a mona- tomic ideal gas, we fi nd for each method of adding heat that
∆U = 32 nR (Tf − Ti ) = 3
2 (3.0 mol)[8.31 J/ (mol · K)](350 K − 540 K)
= −7100 J
(b) Since ΔU is now known and the heat is given in each method, we can use Equation 15.1 (ΔU = Q − W) to determine the work:
1st method W = Q − ∆U = 5500 J − (−7100 J) = 12 600 J
2nd method W = Q − ∆U = 1500 J − (−7100 J) = 8600 J
In each method the gas does work, but it does more in the fi rst method.
*The fact that an ideal gas is used in Example 2 does not restrict our conclusion. Had a real (nonideal) gas or other
material been used, the only diff erence would have been that the expression for the internal energy would have been
more complicated. It might have involved the volume V, as well as the temperature T, for instance.
s
Movable piston
F = PA
Vf
F = PA
Vi
FIGURE 15.4 The substance in the chamber is expanding isobarically because the pressure
is held constant by the external atmosphere
and the weight of the piston and the block.
15.4 Thermal Processes 405
it expand and do work W in lifting the piston and block through the displacement s→. The work can be calculated from W = Fs (Equation 6.1), where F is the magnitude of the force and s is the magnitude of the displacement. The force is generated by the pressure P acting on the bottom sur- face of the piston (area = A), according to F = PA (Equation 10.19). With this substitution for F, the work becomes W = (PA)s. But the product A · s is the change in volume of the material, ΔV = Vf − Vi, where Vf and Vi are the fi nal and initial volumes, respectively. Thus, the relation is
Isobaric process W = P ∆V = P(Vf − Vi ) (15.2)
Consistent with our sign convention, this result predicts a positive value for the work done by a system when it expands isobarically (Vf exceeds Vi). Equation 15.2 also applies to an isobaric compression (Vf less than Vi). Then, the work is negative, since work must be done on the system to compress it. Example 3 emphasizes that W = PΔV applies to any system, solid, liquid, or gas, as long as the pressure remains constant while the volume changes.
Analyzing Multiple-Concept Problems
EXAMPLE 3 Isobaric Expansion of Water
One gram of water is placed in the cylinder in Figure 15.4, and the pres- sure is maintained at 2.0 × 105 Pa. The temperature of the water is raised
by 31 C°. In one case, the water is in the liquid phase, expands by the small
amount of 1.0 × 10−8 m3, and has a specifi c heat capacity of 4186 J/(kg · C°). In another case, the water is in the gas phase, expands by the much greater
amount of 7.1 × 10−5 m3, and has a specifi c heat capacity of 2020 J/(kg · C°). Determine the change in the internal energy of the water in each case.
Reasoning The change ΔU in the internal energy is given by the fi rst law of thermodynamics as ΔU = Q − W (Equation 15.1). The heat Q may be evaluated as Q = cm ΔT (Equation 12.4). Finally, since the process occurs at a constant pressure (isobaric), the work W may be found using W = P ΔV (Equation 15.2).
Knowns and Unknowns The following table summarizes the given data:
Modeling the Problem
STEP 1 The First Law of Thermodynamics The change ΔU in the internal energy is given by the fi rst law of thermodynamics, as shown at the right. In Equation 15.1, neither the heat Q nor the work W is known, so we turn to Steps 2 and 3 to evaluate them.
STEP 2 Heat and Specifi c Heat Capacity According to Equation 12.4, the heat Q needed to raise the temperature of a mass m of material by an amount ΔT is
Q = cm ∆T
where c is the material’s specifi c heat capacity. Data are available for all of the terms on the right side of this expression, which can be substituted into Equation 15.1, as shown at the right. The
remaining unknown variable in Equation 15.1 is the work W, and we evaluate it in Step 3.
Description Symbol Value Comment Mass of water m 1.0 g 0.0010 kg
Pressure on water P 2.0 × 105 Pa Pressure is constant.
Increase in temperature ΔT 31 C°
Increase in volume of liquid ΔVliquid 1.0 × 10−8 m3 Expansion occurs.
Specific heat capacity of liquid cliquid 4186 J/(kg · C°)
Increase in volume of gas ΔVgas 7.1 × 10−5 m3 Expansion occurs.
Specific heat capacity of gas cgas 2020 J/(kg · C°)
Unknown Variables Change in internal energy of liquid ΔUliquid ?
Change in internal energy of gas ΔUgas ?
∆U = Q − W (15.1)
? ?
∆U = Q − W (15.1)
Q = cm ∆T (12.4)
?
406 CHAPTER 15 Thermodynamics
It is often convenient to display thermal processes graphically. For instance, Interactive Figure 15.5 shows a plot of pressure versus volume for an isobaric expansion. Since the pressure is constant, the graph is a horizontal straight line, beginning at the initial volume Vi and ending at the fi nal volume Vf. In terms of such a plot, the work W = P(Vf − Vi) is the area under the graph, which is the shaded rectangle of height P and width Vf − Vi.
Another common thermal process is an isochoric process, one that occurs at constant volume. Figure 15.6a illustrates an isochoric process in which a substance (solid, liquid, or gas) is heated. The substance would expand if it could, but the rigid container keeps the volume constant, so the
pressure–volume plot shown in Figure 15.6b is a vertical straight line. Because the volume is con- stant, the pressure inside rises, and the substance exerts more and more force on the walls. Although
enormous forces can be generated in the closed container, no work is done (W = 0 J), since the walls do not move. Consistent with zero work being done, the area under the vertical straight line in
Figure 15.6b is zero. Since no work is done, the fi rst law of thermodynamics indicates that the heat in an isochoric process serves only to change the internal energy: ΔU = Q − W = Q.
A third important thermal process is an isothermal process, one that takes place at constant temperature. The next section illustrates the important features of an isothermal process when the system is an ideal gas.
Last, there is the adiabatic process, one that occurs without the transfer of heat. Since there is no heat transfer, Q equals zero, and the fi rst law indicates that ΔU = Q − W = −W. Thus, when work is done by a system adiabatically, W is positive and the internal energy decreases by exactly the amount of the work done. When work is done on a system adiabatically, W is negative and the internal energy increases correspondingly. The next section discusses an adiabatic process
for an ideal gas.
A process may be complex enough that it is not recognizable as one of the four just dis-
cussed. For instance, Figure 15.7 shows a process for a gas in which the pressure, volume, and temperature are changed along the straight line from X to Y. With the aid of integral calculus, the following can be proved.
P re
ss ur
e
Volume
0
P
Vi Vf
INTERACTIVE FIGURE 15.5 For an isobaric process, a pressure–volume plot is a
horizontal straight line. The work done
[W = P(Vf − Vi)] is the colored rectangular area under the graph.
STEP 3 Work Done at Constant Pressure Under constant-pressure, or isobaric, conditions, the work W done is given by Equation 15.2 as
W = P ∆V
where P is the pressure acting on the material and ΔV is the change in the volume of the material. Substitution of this expression into Equation 15.1 is shown at the right.
Solution Combining the results of each step algebraically, we fi nd that
∆U = Q − W = cm ∆T − W = cm ∆T − P ∆V
Applying this result to the liquid and to the gaseous water gives
∆Uliquid = c liquid m ∆T − P ∆Vliquid
= [4186 J/ (kg · C°)](0.0010 kg)(31 C°) − (2.0 × 105 Pa)(1.0 ×10−8 m3)
= 130 J − 0.0020 J = 130 J
∆Ugas = cgas m ∆T − P ∆Vgas
= [2020 J/ (kg · C°)](0.0010 kg)(31 C°) − (2.0 × 10 5 Pa)(7.1 × 10−5 m3)
= 63 J − 14 J = 49 J
For the liquid, virtually all the 130 J of heat serves to change the internal energy, since the volume
change and the corresponding work of expansion are so small. In contrast, a signifi cant fraction
of the 63 J of heat added to the gas causes work of expansion to be done, so that only 49 J is left
to change the internal energy.
Related Homework: Problem 17
STEP 1 STEP 2 STEP 3
∆U = Q − W (15.1)
Q = cm ∆T (12.4)
W = P ∆V (15.1)
15.4 Thermal Processes 407
Problem-Solving Insight The area under a pressure–volume graph is the work for any kind of process.
Thus, the area representing the work has been colored in Figure 15.7. The volume increases, so that work is done by the gas. This work is positive by convention, as is the area. In contrast, if
a process reduces the volume, work is done on the gas, and this work is negative by convention.
Correspondingly, the area under the pressure–volume graph would be assigned a negative value.
In Example 4, we determine the work for the case shown in Figure 15.7.
P re
ss ur
e
Volume
(a)
(b)
Pf
Pi
V
FIGURE 15.6 (a) The substance in the chamber is being heated
isochorically because the rigid
chamber keeps the volume constant.
(b) The pressure–volume plot for an isochoric process is a vertical straight
line. The area under the graph is zero,
indicating that no work is done.
P re
ss ur
e Volume
Y (High
temperature)
X (Low
temperature)
1.0 � 10 –4 m3
2.0 � 10 5 Pa
FIGURE 15.7 The colored area gives the work done by the gas for the process
from X to Y.
EXAMPLE 4 Work and the Area Under a Pressure–Volume Graph
Determine the work for the process in which the pressure, volume, and
temperature of a gas are changed along the straight line from X to Y in
Figure 15.7.
Reasoning The work is given by the area (in color) under the straight line between X and Y. Since the volume increases, work is done by the
gas on the surroundings, so the work is positive. The area can be found by
counting squares in Figure 15.7 and multiplying by the area per square.
Solution We estimate that there are 8.9 colored squares in the drawing. The area of one square is (2.0 × 105 Pa)(1.0 × 10−4 m3) = 2.0 × 101 J, so
the work is
W = +(8.9 squares)(2.0 × 101 J/square) = +180 J
Check Your Understanding
(The answers are given at the end of the book.) 2. Is it possible for the temperature of a substance to rise without heat fl owing into the substance?
(a) Yes, provided that the volume of the substance does not change. (b) Yes, provided that the substance expands and does positive work. (c) Yes, provided that work is done on the substance and it contracts.
3. CYU Figure 15.1 shows a pressure-versus-volume plot for a three-step process: A → B, B → C, and C → A. For each step, the work can be positive, negative, or zero. Which answer in CYU Table 15.1 correctly describes the work for the three steps?
(Continued)
408 CHAPTER 15 Thermodynamics
P re
ss ur
e
Volume
C
B
A
CYU TABLE 15.1 Work Done by the System
A → B B → C C → A
(a) Positive Negative Negative
(b) Positive Positive Negative
(c) Negative Negative Positive
(d) Positive Negative Zero
(e) Negative Positive ZeroCYU FIGURE 15.1
4. CYU Figure 15.2 shows a pressure–volume graph in which a gas expands at constant pressure from A to B, and then goes from B to C at constant volume. Complete CYU Table 15.2 by deciding whether each of the four unspecifi ed quantities is positive (+), negative (−), or zero (0).
CYU TABLE 15.2
ΔU Q W A → B + ? ?
B → C ? + ?
P re
ss ur
e
A B
C
Volume
CYU FIGURE 15.2
5. When a solid melts at constant pressure, the volume of the resulting liquid does not diff er much from the volume of the solid. According to the fi rst law of thermodynamics, how does the internal energy of
the liquid compare to the internal energy of the solid? The internal energy of the liquid is (a) greater than, (b) the same as, (c) less than the internal energy of the solid.
15.5 Thermal Processes Using an Ideal Gas
Isothermal Expansion or Compression When a system performs work isothermally, the temperature remains constant. In Animated Figure 15.8a, for instance, a metal cylinder contains n moles of an ideal gas, and the large mass of hot water maintains the cylinder and gas at a constant Kelvin temperature T. The piston is held in place initially so the volume of the gas is Vi. As the external force applied to the piston is reduced quasi-statically, the pressure decreases as the gas expands to the fi nal volume Vf. Animated Figure 15.8b gives a plot of pressure (P = nRT/V) versus volume for the process. The solid red line in the graph is called an isotherm (meaning “constant temperature”) and represents
the relation between pressure and volume when the temperature is held constant. The work W done by the gas is not given by W = P ΔV = P(Vf − Vi) because the pressure is not constant. Nevertheless, the work is equal to the area under the graph. The techniques of integral calculus
lead to the following result* for W:
Isothermal expansion or compression of an ideal gas
W = nRT ln(VfVi) (15.3)
Hot water at temperature T
Q
(a)
(b)
P re
ss ur
e
Volume
Isotherm
Vi Vf
P = V nRT
Metal cylinder
ANIMATED FIGURE 15.8 (a) The ideal gas in the cylinder is expanding isothermally at
temperature T. The force holding the piston in place is reduced slowly, so the expansion
occurs quasi-statically. (b) The work done by the gas is given by the colored area.
*In this result, “ln” denotes the natural logarithm to the base e = 2.71828. The natural logarithm is related to the common logarithm to the base ten by ln(Vf /Vi) = 2.303 log(Vf /Vi).
15.5 Thermal Processes Using an Ideal Gas 409
Where does the energy for this work originate? Since the internal energy of any ideal gas is
proportional to the Kelvin temperature (U = 32 nRT for a monatomic ideal gas, for example), the internal energy remains constant throughout an isothermal process, and the change in internal
energy is zero. As a result, the fi rst law of thermodynamics becomes ΔU = 0 = Q − W. In other words, Q = W, and the energy for the work originates in the hot water. Heat fl ows into the gas from the water, as Animated Figure 15.8a illustrates. If the gas is compressed isothermally, Equation 15.3 still applies, and heat fl ows out of the gas into the water. Example 5 deals with the
isothermal expansion of an ideal gas.
EXAMPLE 5 Isothermal Expansion of an Ideal Gas
Two moles of the monatomic gas argon expand isothermally at 298 K,
from an initial volume of Vi = 0.025 m3 to a fi nal volume of Vf = 0.050 m3. Assuming that argon behaves as an ideal gas, fi nd (a) the work done by the gas, (b) the change in the internal energy of the gas, and (c) the heat supplied to the gas.
Reasoning and Solution (a) The work done by the gas can be found from Equation 15.3:
W = nRT ln ( Vf Vi) = (2.0 mol)[8.31 J/(mol · K)](298 K) ln (
0.050 m3
0.025 m3) = +3400 J
(b) The internal energy of a monatomic ideal gas is U = 32 nRT (Equation 14.7) and does not change when the temperature is constant. Therefore,
∆U = 0 J . (c) The heat Q supplied can be determined from the fi rst law of thermo- dynamics:
Q = ∆U + W = 0 J + 3400 J = +3400 J (15.1)
Adiabatic Expansion or Compression When a system performs work adiabatically, no heat fl ows into or out of the system. Figure 15.9a shows an arrangement in which n moles of an ideal gas do work under adiabatic conditions, expanding quasi-statically from an initial volume Vi to a fi nal volume Vf. The arrangement is similar to that in Animated Figure 15.8 for isothermal expansion. However, a diff erent amount of work is done here, because the cylinder is now surrounded by insulating material that pre-
vents the fl ow of heat from occurring, so Q = 0 J. According to the fi rst law of thermodynamics, the change in internal energy is ΔU = Q − W = −W. Since the internal energy of an ideal mona- tomic gas is U = 32 nRT (Equation 14.7), it follows directly that ∆U = Uf − Ui =
3
2 nR(Tf − T i ) , where Ti and Tf are the initial and fi nal Kelvin temperatures. With this substitution, the relation ΔU = −W becomes
Adiabatic expansion or compression of a monatomic ideal gas
W = 32 nR(Ti − Tf ) (15.4)
When an ideal gas expands adiabatically, it does positive work, so W is positive in Equation 15.4. Therefore, the term Ti − Tf is also positive, so the fi nal temperature of the gas must be less than the initial temperature. The internal energy of the gas is reduced to provide the necessary
energy to do the work, and because the internal energy is proportional to the Kelvin temperature,
the temperature decreases. Figure 15.9b shows a plot of pressure versus volume for an adiabatic process. The adiabatic curve (red) intersects the isotherms (blue) at the higher initial temperature
[Ti = PiVi/(nR)] and also at the lower fi nal temperature [Tf = PfVf /(nR)]. The colored area under the adiabatic curve represents the work done.
The reverse of an adiabatic expansion is an adiabatic compression (W is negative), and Equa- tion 15.4 indicates that the fi nal temperature of the ideal gas exceeds the initial temperature. The
energy provided by the agent doing the work increases the internal energy of the gas. As a result,
the gas becomes hotter.
Insulating material (a)
(b)
P re
ss ur
e
Volume
Adiabatic curve
Vi Vf
Tf
Ti
Pf
Pi
Metal cylinder
FIGURE 15.9 (a) The ideal gas in the cylinder is expanding adiabatically. The force holding the piston in place is reduced slowly, so the expansion occurs quasi-statically. (b) A plot of pressure versus volume yields the adiabatic curve shown in red, which intersects the isotherms (blue) at the initial temperature Ti and the fi nal temperature Tf. The work done by the gas is given by the colored area.
410 CHAPTER 15 Thermodynamics
The equation that gives the adiabatic curve (red) between the initial pressure and volume
(Pi, Vi) and the fi nal pressure and volume (Pf, Vf) in Figure 15.9b can be derived using integral calculus. The result is
Adiabatic expansion or compression of an ideal gas
PiV γi = PfV γf (15.5)
where the exponent 𝛾 (Greek gamma) is the ratio of the specifi c heat capacities at constant pres-
sure and constant volume, 𝛾 = cP/cV. Equation 15.5 applies in conjunction with the ideal gas law, because each point on the adiabatic curve satisfi es the relation PV = nRT.
Table 15.1 summarizes the work done in the four types of thermal processes that we have been considering. For each process it also shows how the fi rst law of thermodynamics depends
on the work and other variables.
Math Skills Suppose it is necessary to solve Equation 15.5 for the variable Vi. If the value for 𝛾 were 𝛾 = 2 (which it never is for an ideal gas), we would begin by taking the square root of both sides of the equals sign in Equation 15.5 and would deal with the square root of V 2i (or V 2f ) as follows:
√V 2i = (V 2i )1/2 = V 2(1/2)i = V 1i = V i We will see in the next section that 𝛾 =
5
3 for a monatomic ideal gas, and we deal with such a case
in a similar way. We begin by raising both sides of Equation 15.5 to the power 1/𝛾:
PiV γi = PfVfγ or (PiViγ)1/γ = (PfV γf )1/γ
Simplifying the terms in the right-hand equation, we have
(Pi V γi )1/γ = (Pf V γf )1/γ or P 1/γi Viγ (1/γ) = P 1/γf V γf (1/γ) or P 1/γi Vi = P 1/γf Vf Dividing both sides of the far-right equation by Pi1/𝛾 gives
P 1/γi Vi P 1/γi
= P 1/γf Vf P 1/γi
or Vi = P 1/γf Vf P 1/γi
or Vi = ( Pf Pi)
1/γ
Vf
For 𝛾 = 5
3, the exponent of 1/𝛾 in the fi nal expression for Vi is 1 γ =
3
5.
TABLE 15.1 Summary of Thermal Processes
Type of Thermal Process Work Done First Law of Thermodynamics
(ΔU = Q − W) Isobaric
(constant pressure)
W = P(Vf − Vi) ∆U = Q − P(Vf − Vi)
Isochoric
(constant volume)
W = 0 J ∆U = Q − 0 J
Isothermal
(constant temperature) W = nRT ln ( Vf Vi)
(for an ideal gas)
0 J = Q − nRT ln ( Vf Vi)
Adiabatic
(no heat flow) W = 32 nR(Ti − Tf) (for a monatomic
ideal gas)
∆U = 0 J − 32 nR(Ti − Tf)
⏟⎵⏟⎵⏟
W {
Q
{
ΔU for an ideal gas
⏟⎵⎵⎵⏟⎵⎵⎵⏟
W
{
Q ⏟⎵⎵⏟⎵⎵⏟
W
Check Your Understanding
(The answers are given at the end of the book.) 6. One hundred joules of heat is added to a gas, and the gas expands at constant pressure. Is it possible
that the internal energy increases by 100 J? (a) Yes (b) No; the increase in the internal energy is less than 100 J, since work is done by the gas. (c) No; the increase in the internal energy is greater than 100 J, since work is done by the gas.
15.6 Specific Heat Capacities 411
7. A gas is compressed isothermally, and its internal energy increases. Is the gas an ideal gas? (a) No, because if the temperature of an ideal gas remains constant, its internal energy must also remain constant.
(b) No, because if the temperature of an ideal gas remains constant, its internal energy must decrease. (c) Yes, because if the temperature of an ideal gas remains constant, its internal energy must increase.
8. A material undergoes an isochoric process that is also adiabatic. Is the internal energy of the material at the end of the process (a) greater than, (b) less than, or (c) the same as it was at the start?
9. CYU Figure 15.3 shows an arrangement for an adiabatic free expansion or “throttling” process. The process is adiabatic because
the entire arrangement is contained within perfectly insulating
walls. The gas in chamber A rushes suddenly into chamber B
through a hole in the partition. Chamber B is initially evacuated,
so the gas expands there under zero external pressure and the
work (W = P ΔV) it does is zero. Assume that the gas is an ideal gas. How does the fi nal temperature of the gas after expansion
compare to its initial temperature? The fi nal temperature is (a) greater than, (b) less than, (c) the same as the initial temperature.
15.6 Specific Heat Capacities In this section the fi rst law of thermodynamics is used to gain an understanding of the factors
that determine the specifi c heat capacity of a material. Remember, when the temperature of a
substance changes as a result of heat fl ow, the change in temperature ΔT and the amount of heat Q are related according to Q = cm ΔT (Equation 12.4). In this expression c denotes the specifi c heat capacity in units of J/(kg · C°), and m is the mass in kilograms. Now, however, it is more convenient to express the amount of material as the number of moles n, rather than the number of kilograms. Therefore, we replace the expression Q = cm ΔT with the following analogous expression:
Q = Cn ∆T (15.6)
where the capital letter C (as opposed to the lowercase c) refers to the molar specifi c heat capacity in units of J/(mol · K). In addition, the unit for measuring the temperature change ΔT is the kelvin (K) rather than the Celsius degree (C°), and ΔT = Tf − Ti, where Tf and Ti are the fi nal and initial temperatures. For gases it is necessary to distinguish between the molar
specifi c heat capacities CP and CV, which apply, respectively, to conditions of constant pressure and constant volume. With the help of the fi rst law of thermodynamics and an ideal gas as an
example, it is possible to see why CP and CV diff er. To determine the molar specifi c heat capacities, we must fi rst calculate the heat Q needed to
raise the temperature of an ideal gas from Ti to Tf. According to the fi rst law, Q = ΔU + W. We also know that the internal energy of a monatomic ideal gas is U = 32 nRT (Equation 14.7). As a result, ∆U = Uf − Ui =
3
2 nR(Tf − Ti ) . When the heating process occurs at constant pressure, the work done is given by Equation 15.2: W = P ΔV = P(Vf − Vi). For an ideal gas, PV = nRT, so the work becomes W = nR(Tf − Ti). On the other hand, when the volume is constant, ΔV = 0 m3, and the work done is zero. The calculation of the heat is summarized below:
Q = ∆U + W
Qconstant pressure = 3
2 nR(Tf − Ti ) + nR(Tf − Ti ) = 5
2 nR(Tf − Ti )
Qconstant volume = 3
2 nR(Tf − Ti ) + 0
The molar specifi c heat capacities can now be determined, since Equation 15.6 indicates that
C = Q/[n(Tf − Ti)]:
Constant pressure for a monatomic ideal gas
CP = Qconstant pressure n(Tf − Ti )
= 5
2 R (15.7)
Constant volume for a monatomic ideal gas
CV = Qconstant volume n (Tf − Ti )
= 3
2 R (15.8)
A B
CYU FIGURE 15.3
412 CHAPTER 15 Thermodynamics
The ratio 𝛾 of the specifi c heats is
Monatomic ideal gas γ =
CP CV
=
5
2 R 3
2 R =
5
3 (15.9)
For real monatomic gases near room temperature, experimental values of CP and CV give ratios very close to the theoretical value of γ = 53.
Many gases are not monatomic. Instead, they consist of molecules formed from more than
one atom. The oxygen in our atmosphere, for example, is a diatomic gas, because it consists of
molecules formed from two oxygen atoms. Similarly, atmospheric nitrogen is a diatomic gas
consisting of molecules formed from two nitrogen atoms. Whereas the individual atoms in a
monatomic ideal gas can exhibit only translational motion, the molecules in a diatomic ideal gas
can exhibit translational and rotational motion, as well as vibrational motion at suffi ciently high
temperatures. The result of such additional motions is that Equations 15.7–15.9 do not apply
to a diatomic ideal gas. Instead, if the temperature is suffi ciently moderate that the diatomic
molecules do not vibrate, the molar specifi c heat capacities of a diatomic ideal gas are CP = 7
2 R and CV =
5
2 R, with the result that γ = CP CV
= 7
5.
The diff erence between CP and CV arises because work is done when the gas expands in response to the addition of heat under conditions of constant pressure, whereas no work is done
under conditions of constant volume. For a monatomic ideal gas, CP exceeds CV by an amount equal to R, the ideal gas constant:
CP − CV = R (15.10)
In fact, it can be shown that Equation 15.10 applies to any kind of ideal gas—monatomic,
diatomic, etc.
Check Your Understanding
(The answers are given at the end of the book.) 10. Suppose that a material contracts when it is heated. Following the same line of reasoning used in the
text to reach Equations 15.7 and 15.8, deduce the relationship between the specifi c heat capacity at
constant pressure (CP) and the specifi c heat capacity at constant volume (CV). Which of the following describes the relationship? (a) CP = CV (b) CP is greater than CV (c) CP is less than CV
11. You want to heat a gas so that its temperature will be as high as possible. Should you heat the gas under conditions of (a) constant pressure or (b) constant volume? (c) It does not matter what the conditions are.
15.7 The Second Law of Thermodynamics Ice cream melts when left out on a warm day. A cold can of soda warms up on a hot day at a
picnic. Ice cream and soda never become colder when left in a hot environment, for heat always
fl ows spontaneously from hot to cold, and never from cold to hot. The spontaneous fl ow of heat is
the focus of one of the most profound laws in all of science, the second law of thermodynamics.
THE SECOND LAW OF THERMODYNAMICS: THE HEAT FLOW STATEMENT Heat fl ows spontaneously from a substance at a higher temperature to a substance at a lower temperature and does not fl ow spontaneously in the reverse direction.
It is important to realize that the second law of thermodynamics deals with a diff erent aspect
of nature than does the fi rst law of thermodynamics. The second law is a statement about the
natural tendency of heat to fl ow from hot to cold, whereas the fi rst law deals with energy con-
servation and focuses on both heat and work. A number of important devices depend on heat
and work in their operation, and to understand such devices both laws are needed. For instance,
an automobile engine is a type of heat engine because it uses heat to produce work. In discuss-
ing heat engines, Sections 15.8 and 15.9 will bring together the fi rst and second laws to analyze
15.8 Heat Engines 413
engine effi ciency. Then, in Section 15.10 we will see that refrigerators, air conditioners, and heat
pumps also utilize heat and work and are closely related to heat engines. The way in which these
three appliances operate also depends on both the fi rst and second laws of thermodynamics.
15.8 Heat Engines THE PHYSICS OF . . . a heat engine. A heat engine is any device that uses heat to perform work. It has three essential features:
1. Heat is supplied to the engine at a relatively high input temperature from a place called the hot reservoir.
2. Part of the input heat is used to perform work by the working substance of the engine, which is the material within the engine that actually does the work (e.g., the gasoline–air mixture
in an automobile engine).
3. The remainder of the input heat is rejected to a place called the cold reservoir, which has a temperature lower than the input temperature.
Interactive Figure 15.10 illustrates these features. The symbol QH refers to the input heat, and the subscript H indicates the hot reservoir. Similarly, the symbol QC stands for the rejected heat, and the subscript C denotes the cold reservoir. The symbol W refers to the work done. The verti- cal bars enclosing each of these three symbols in the drawing are included to emphasize that we
are concerned here with the absolute values, or magnitudes, of the symbols. Thus, |QH| indicates the magnitude of the input heat, |QC| denotes the magnitude of the rejected heat, and |W| stands for the magnitude of the work done.
To be highly effi cient, a heat engine must produce a relatively large amount of work from as
little input heat as possible. Therefore, the effi ciency e of a heat engine is defi ned as the ratio of the magnitude of the work |W| done by the engine to the magnitude of the input heat |QH|:
e = ∣W ∣ ∣QH∣
(15.11)
If the input heat were converted entirely into work, the engine would have an effi ciency of 1.00,
since |W| = |QH|; such an engine would be 100% effi cient. Effi ciencies are often quoted as per- centages obtained by multiplying the ratio |W|/|QH| by a factor of 100. Thus, an effi ciency of 68% would mean that a value of 0.68 is used for the effi ciency in Equation 15.11.
An engine, like any device, must obey the principle of conservation of energy. Some of the
engine’s input heat |QH| is converted into work |W|, and the remainder |QC| is rejected to the cold reservoir. If there are no other losses in the engine, the principle of energy conservation requires that
∣QH∣ = ∣W∣ + ∣QC∣ (15.12)
Solving this equation for |W| and substituting the result into Equation 15.11 leads to the follow- ing alternative expression for the effi ciency e of a heat engine:
e = ∣QH∣ − ∣QC∣
∣QH∣ = 1 −
∣QC∣ ∣QH∣
(15.13)
Example 6 illustrates how the concepts of effi ciency and energy conservation are applied to a
heat engine.
Engine
Cold reservoir
�QC�
�W �
�QH�
Hot reservoir
INTERACTIVE FIGURE 15.10 This schematic representation of a heat engine shows the
input heat (magnitude = |QH|) that originates from the hot reservoir, the work (magnitude =
|W|) that the engine does, and the heat (magnitude = |QC|) that the engine rejects to the cold reservoir.
Math Skills The symbols |QH|, |QC|, and |W| refer to absolute values or magnitudes only. It is essential to re-
member that these symbols never have
negative values assigned to them when
they appear in equations. For example,
the value assigned to |W| is the same if W = −1830 J or W = +1830 J. This follows because
∣W∣ = ∣−1830 J∣ = 1830 J
and
∣W∣ = ∣+1830 J∣ = 1830 J
Analyzing Multiple-Concept Problems
EXAMPLE 6 An Automobile Engine
An automobile engine has an effi ciency of 22.0% and produces 2510 J of
work. How much heat is rejected by the engine?
Reasoning Energy conservation indicates that the amount of heat rejected to the cold reservoir is the part of the input heat that is not converted
into work. The work is given, and the input heat can be obtained since the
effi ciency of the engine is also given.
414 CHAPTER 15 Thermodynamics
In Example 6, less than one-quarter of the input heat is converted into work because the
effi ciency of the automobile engine is only 22.0%. If the engine were 100% effi cient, all the input
heat would be converted into work. Unfortunately, nature does not permit 100%-effi cient heat
engines to exist, as the next section discusses.
15.9 Carnot’s Principle and the Carnot Engine What is it that allows a heat engine to operate with maximum effi ciency? The French engineer
Sadi Carnot (1796–1832) proposed that a heat engine has maximum effi ciency when the pro-
cesses within the engine are reversible. A reversible process is one in which both the system and its environment can be returned to exactly the states they were in before the process occurred.
Modeling the Problem
STEP 1 The Conservation of Energy According to the energy-conservation principle, the magnitudes of the input heat |QH|, the work done |W|, and the rejected heat |QC| are related ac- cording to |QH| = |W| + |QC| (Equation 15.12). Solving for |QC| gives Equation 1 at the right. In this result, |W| is known, but |QH| is not, although it will be evaluated in Step 2.
STEP 2 Engine Effi ciency Equation 15.11 gives the engine effi ciency as e = |W|/|QH|. Solving for |QH|, we fi nd that
∣QH∣ = ∣W∣ e
which can be substituted into Equation 1 as shown in the right column.
Problem-Solving Insight When effi ciency is stated as a percentage (e.g., 22.0%), it must be converted to a decimal fraction (e.g., 0.220) before being used in an equation.
Solution Combining the results of each step algebraically, we fi nd that
∣QC∣ = ∣QH∣ − ∣W∣ =│ ∣W∣ e
− ∣W ∣
The magnitude of the rejected heat, then, is
∣QC∣ = ∣W∣(1e − 1) = (2510 J)( 1
0.220 − 1) = 8900 J
Related Homework: Problems 44, 84
STEP 1 STEP 2
Knowns and Unknowns The following data are available:
Description Symbol Value Efficiency of engine e 22.0% (0.220)
Magnitude of work |W| 2510 J
Unknown Variable Magnitude of rejected heat |QC| ?
∣QC∣ = ∣QH∣ − ∣W ∣ (1)
?
∣QC∣ = ∣QH∣ − ∣W ∣ (1)
∣QH∣ = ∣W∣ e
15.9 Carnot’s Principle and the Carnot Engine 415
In a reversible process, both the system and its environment can be returned to their initial states. Therefore, a process that involves an energy-dissipating mechanism, such as friction, cannot
be reversible because the energy wasted due to friction would alter the system or the environ-
ment or both. There are also reasons other than friction why a process may not be reversible. For
instance, the spontaneous fl ow of heat from a hot substance to a cold substance is irreversible,
even though friction is not present. For heat to fl ow in the reverse direction, work must be done,
as we will see in Section 15.10. The agent doing such work must be located in the environment of
the hot and cold substances, and, therefore, the environment must change while the heat is moved
back from cold to hot. Since the system and the environment cannot both be returned to their initial states, the process of spontaneous heat fl ow is irreversible. In fact, all spontaneous pro-
cesses are irreversible, such as the explosion of an unstable chemical or the bursting of a bubble.
When the word “reversible” is used in connection with engines, it does not just mean a gear that
allows the engine to operate a device in reverse. All cars have a reverse gear, for instance, but no
automobile engine is thermodynamically reversible, since friction exists no matter which way
the car moves.
Today, the idea that the effi ciency of a heat engine is a maximum when the engine operates
reversibly is referred to as Carnot’s principle.
CARNOT’S PRINCIPLE: AN ALTERNATIVE STATEMENT OF THE SECOND LAW OF THERMODYNAMICS No irreversible engine operating between two reservoirs at constant temperatures can have a greater effi ciency than a reversible engine operating between the same tempera- tures. Furthermore, all reversible engines operating between the same temperatures have the same effi ciency.
Carnot’s principle is quite remarkable, for no mention is made of the working substance
of the engine. It does not matter whether the working substance is a gas, a liquid, or a solid.
As long as the process is reversible, the effi ciency of the engine is a maximum. However,
Carnot’s principle does not state, or even imply, that a reversible engine has an effi ciency of 100%.
It can be shown that if Carnot’s principle were not valid, it would be possible for heat
to fl ow spontaneously from a cold substance to a hot substance, in violation of the second
law of thermodynamics. In eff ect, then, Carnot’s principle is another way of expressing the
second law.
No real engine operates reversibly. Nonetheless, the idea of a reversible engine provides a
useful standard for judging the performance of real engines. Figure 15.11 shows a reversible engine, called a Carnot engine, that is particularly useful as an idealized model. An impor- tant feature of a Carnot engine is that all input heat (magnitude = |QH|) originates from a hot reservoir at a single temperature TH and all rejected heat (magnitude = |QC|) goes into a cold reservoir at a single temperature TC. This important feature is emphasized in Problem 61, which focuses on a pressure–volume plot for a Carnot engine that utilizes an ideal gas as its
working substance.
Carnot’s principle implies that the effi ciency of a reversible engine is independent of the
working substance of the engine, and therefore can depend only on the temperatures of the
hot and cold reservoirs. Since effi ciency is e = 1 − |QC|/|QH| according to Equation 15.13, the ratio |QC|/|QH| can depend only on the reservoir temperatures. This observation led Lord Kelvin to propose a thermodynamic temperature scale. He proposed that the thermody- namic temperatures of the cold and hot reservoirs be defi ned such that their ratio is equal
to |QC|/|QH|. Thus, the thermodynamic temperature scale is related to the heats absorbed and rejected by a Carnot engine, and is independent of the working substance. If a reference
temperature is properly chosen, it can be shown that the thermodynamic temperature scale
is identical to the Kelvin scale introduced in Section 12.2 and used in the ideal gas law. As
a result, the ratio of the magnitude of the rejected heat |QC| to the magnitude of the input heat |QH| is
∣QC∣ ∣QH∣
= TC TH
(15.14)
where the temperatures TC and TH must be expressed in kelvins.
Engine
Cold reservoir
�QC�
�W �
�QH�
Temperature = TH
Temperature = TC
Hot reservoir
FIGURE 15.11 A Carnot engine is a reversible engine in which all input heat
(magnitude = |QH|) originates from a hot reservoir at a single temperature TH, and all rejected heat (magnitude = |QC|) goes into a cold reservoir at a single temperature TC.
416 CHAPTER 15 Thermodynamics
The effi ciency eCarnot of a Carnot engine can be written in a particularly useful way by substi- tuting Equation 15.14 into Equation 15.13 for the effi ciency, e = 1 − |QC|/|QH|:
Effi ciency of a Carnot engine eCarnot = 1 −
TC TH
(15.15)
This relation gives the maximum possible effi ciency for a heat engine operating between two Kelvin temperatures TC and TH, and the next example illustrates its application.
Math Skills When determining the effi ciency of a Carnot engine with Equation 15.15, be sure the temperatures TC and TH of the cold and hot reservoirs are expressed in kelvins; degrees Celsius or Fahr- enheit will lead to errors. Suppose, for example, that a Carnot engine has reservoir temperatures of
TC = 254 K (−19 °C) and TH = 294 K (21 °C). According to Equation 15.15, the effi ciency of this engine is
eCarnot = 1 − TC TH
= 1 − 254 K
294 K = 0.136 or 13.6%
For comparison, the incorrect calculation using Celsius degrees is shown below:
Incorrect Calculation eCarnot = 1 − TC TH
= 1 − −19 °C
21 °C = 1.90 or 190%
This result makes no sense, since it implies an impossible effi ciency of greater than 100%. The trouble
with the Celsius scale in the calculation is that it allows values that are below zero, or negative. The
Kelvin scale, in contrast, is chosen so that its zero temperature point is the lowest temperature attain-
able. Therefore, it cannot give effi ciencies greater than 100% when used in Equation 15.15.
EXAMPLE 7 The Physics of Extracting Work from a Warm Ocean
Water near the surface of a tropical ocean has a temperature of 298.2 K
(25.0 °C), whereas water 700 m beneath the surface has a temperature of
280.2 K (7.0 °C). It has been proposed that the warm water be used as
the hot reservoir and the cool water as the cold reservoir of a heat engine.
Find the maximum possible effi ciency for such an engine.
Reasoning The maximum possible effi ciency is the effi ciency that a Carnot engine would have (Equation 15.15) operating between tempera-
tures of TH = 298.2 K and TC = 280.2 K.
Solution Using TH = 298.2 K and TC = 280.2 K in Equation 15.15, we fi nd that
eCarnot = 1 − TC TH
= 1 − 280.2 K
298.2 K = 0.060 (6.0%)
In Example 7 the maximum possible effi ciency is only 6.0%. The small effi ciency arises
because the Kelvin temperatures of the hot and cold reservoirs are so close. A greater effi ciency
is possible only when there is a greater diff erence between the reservoir temperatures. However,
there are limits on how large the effi ciency of a heat engine can be, as Conceptual Example 8
discusses.
CONCEPTUAL EXAMPLE 8 Natural Limits on the Eff iciency of a Heat Engine
Consider a hypothetical engine that receives 1000 J of heat as input from
a hot reservoir and delivers 1000 J of work, rejecting no heat to a cold
reservoir whose temperature is above 0 K. Which law of thermodynamics
does this engine violate? (a) The fi rst law (b) The second law (c) Both the fi rst and second laws
Reasoning The fi rst law of thermodynamics is an expression of energy conservation. The second law states that no irreversible engine operat-
ing between two reservoirs at constant temperatures can have a greater
effi ciency than a reversible engine operating between the same two
reservoirs. The effi ciency of such a reversible engine is eCarnot, the effi ciency of a Carnot engine.
Answers (a) and (c) are incorrect. From the point of view of energy conservation, nothing is wrong with an engine that converts 1000 J of heat
into 1000 J of work. Energy has been neither created nor destroyed; it has
only been transformed from one form (heat) into another form (work).
Therefore, this engine does not violate the fi rst law of thermodynamics.
15.10 Refrigerators, Air Conditioners, and Heat Pumps 417
THE PHYSICS OF . . . thermal pollution. Example 8 has emphasized that even a perfect heat engine has an effi ciency that is less than 1.0 or 100%. In this regard, we note that the maximum possible effi ciency, as given by Equation 15.15, approaches 1.0 when TC approaches absolute zero (0 K). However, experiments have shown that it is not possible to cool a substance
to absolute zero (see Section 15.12), so nature does not allow a 100%-effi cient heat engine to
exist. As a result, there will always be heat rejected to a cold reservoir whenever a heat engine is
used to do work, even if friction and other irreversible processes are eliminated completely. This
rejected heat is a form of thermal pollution. The second law of thermodynamics requires that at
least some thermal pollution be generated whenever heat engines are used to perform work. This
kind of thermal pollution can be reduced only if society reduces its dependence on heat engines
to do work.
Check Your Understanding
(The answers are given at the end of the book.) 12. The second law of thermodynamics, in the form of Carnot’s principle, indicates that the most effi cient
heat engine operating between two temperatures is a reversible one. Does this mean that a reversible
engine operating between the temperatures of 600 and 400 K must be more effi cient than an irreversible engine operating between 700 and 300 K?
13. Concept Simulation 15.1 at www.wiley.com/college/cutnell allows you to explore the concepts that relate to this question. Three reversible engines, A, B, and C, use the same cold reservoir for their exhaust
heats. However, they use diff erent hot reservoirs that have the following temperatures: (A) 1000 K,
(B) 1100 K, and (C) 900 K. Rank these engines in order of increasing effi ciency (smallest effi ciency
fi rst). (a) A, C, B (b) C, B, A (c) B, A, C (d) C, A, B 14. In Concept Simulation 15.1 at www.wiley.com/college/cutnell you can explore the concepts that are
important in this question. Suppose that you wish to improve the effi ciency of a Carnot engine. Which
answer describes the best way? (a) Lower the Kelvin temperature of the cold reservoir by a factor of four. (b) Raise the Kelvin temperature of the hot reservoir by a factor of four. (c) Cut the Kelvin tem- perature of the cold reservoir in half and double the Kelvin temperature of the hot reservoir. (d) All three choices give the same improvement in effi ciency.
15. Consider a hypothetical device that takes 10 000 J of heat from a hot reservoir and 5000 J of heat from a cold reservoir (whose temperature is greater than 0 K) and produces 15 000 J of work. What can be said
about this device? (a) It violates the fi rst law of thermodynamics but not the second law. (b) It violates the second law of thermodynamics but not the fi rst law. (c) It violates both the fi rst and second laws of thermodynamics. (d) It does not violate either the fi rst or the second law of thermodynamics.
15.10 Refrigerators, Air Conditioners, and Heat Pumps The natural tendency of heat is to fl ow from hot to cold, as indicated by the second law of thermo-
dynamics. However, if work is used, heat can be made to fl ow from cold to hot, against its natural tendency. Refrigerators, air conditioners, and heat pumps are, in fact, devices that do just that. As
Figure 15.12 illustrates, these devices use work (magnitude = |W|) to extract heat (magnitude = |QC|) from the cold reservoir and deposit heat (magnitude = |QH|) into the hot reservoir. Gener- ally speaking, such a process is called a refrigeration process. A comparison of the left and right sides of this drawing shows that the directions of the arrows symbolizing heat and work in a
Answer (b) is correct. Since all of the input heat is converted into work, the effi ciency of the engine is 1, or 100%. But Equation 15.15,
which is based on the second law of thermodynamics, indicates that the
maximum possible effi ciency is eCarnot = 1 − TC/TH, where TC and TH are the temperatures of the cold and hot reservoirs, respectively. Since
we are told that TC is above 0 K, it is clear that the ratio TC/TH is greater than zero, so the maximum possible effi ciency is less than 1 (or less than
100%). The hypothetical engine, therefore, violates the second law of
thermodynamics, which limits the effi ciencies of heat engines to values
less than 100%.
418 CHAPTER 15 Thermodynamics
refrigeration process are opposite to those in an engine process. Nonetheless, energy is conserved
during a refrigeration process, just as it is in an engine process, so |QH| = |W| + |QC|. Moreover, if the process occurs reversibly, we have ideal devices that are called Carnot refrigerators, Carnot
air conditioners, and Carnot heat pumps. For these ideal devices, the relation |QC|/|QH| = TC/TH (Equation 15.14) applies, just as it does for a Carnot engine.
THE PHYSICS OF . . . refrigerators. In a refrigerator, the interior of the unit is the cold reservoir, while the warmer exterior is the hot reservoir. As Figure 15.13 illustrates, the refrigerator takes heat from the food inside and deposits it into the kitchen, along with the energy needed to do
the work of making the heat fl ow from cold to hot. For this reason, the outside surfaces (usually the
sides and back) of most refrigerators are warm to the touch while the units operate.
THE PHYSICS OF . . . air conditioners. An air conditioner is like a refrigerator, except that the room itself is the cold reservoir and the outdoors is the hot reservoir. Figure 15.14 shows a window unit, which cools a room by removing heat and depositing it outside, along with
the work used to make the heat fl ow from cold to hot. Conceptual Example 9 considers a common
misconception about refrigerators and air conditioners.
Cold reservoir
Hot reservoir
�W � �W�
�QH� �QH�
�QC� �QC�
Cold reservoir
Refrigeration Process Engine Process
Hot reservoir
FIGURE 15.12 In the refrigeration process on the left, work (magnitude = |W|) is used to remove heat (magnitude = |QC|) from the cold reservoir and deposit heat (magnitude = |QH|) into the hot reservoir. Compare this with the engine process on
the right.
Cold reservoir (inside
refrigerator)
Hot reservoir (outside
refrigerator)
Refrigerator
�QC�
�QH� = �W � + �QC�
�W � = Magnitude of work done by electrical energy
FIGURE 15.13 A refrigerator.
�W � = Magnitude of work done by electrical energy
Air cond.
�QC� (Cool room)
�QH� (Hot outdoors)
FIGURE 15.14 A window air condi- tioner removes heat from a room, which
is the cold reservoir, and deposits heat
outdoors, which is the hot reservoir.
15.10 Refrigerators, Air Conditioners, and Heat Pumps 419
The quality of a refrigerator or air conditioner is rated according to its coeffi cient of perfor-
mance. Such appliances perform well when they remove a relatively large amount of heat (mag-
nitude = |QC|) from a cold reservoir by using as small an amount of work (magnitude = |W|) as possible. Therefore, the coeffi cient of performance is defi ned as the ratio of |QC| to |W|, and the greater this ratio is, the better the performance is:
Refrigerator or air conditioner
Coeffi cient of performance =
∣QC∣ ∣W∣ (15.16)
Commercially available refrigerators and air conditioners have coeffi cients of performance in the
range 2 to 6, depending on the temperatures involved. The coeffi cients of performance for these
real devices are less than those for ideal, or Carnot, refrigerators and air conditioners.
In a sense, refrigerators and air conditioners operate like pumps. They pump heat “uphill”
from a lower temperature to a higher temperature, just as a water pump forces water uphill from a
lower elevation to a higher elevation. It would be appropriate to call them heat pumps. However,
the name “heat pump” is reserved for the device illustrated in Figure 15.15, which is a home heating appliance.
THE PHYSICS OF . . . heat pumps. The heat pump uses work (magnitude = |W|) to make heat (magnitude = |QC|) from the wintry outdoors (the cold reservoir) fl ow up the tempera- ture “hill” into a warm house (the hot reservoir). According to the conservation of energy, the heat
pump deposits inside the house an amount of heat |QH| = |W| + |QC|. The air conditioner and the heat pump do closely related jobs. The air conditioner refrigerates the inside of the house and heats
up the outdoors, whereas the heat pump refrigerates the outdoors and heats up the inside. These
jobs are so closely related that most heat pump systems serve in a dual capacity, being equipped
with a switch that converts them from heaters in the winter into air conditioners in the summer.
Heat pumps are popular for home heating in today’s energy-conscious world, and it is easy
to understand why. Suppose that 1000 J of energy is available for home heating. Figure 15.16 shows that a conventional electric heating system uses this 1000 J to heat a coil of wire, just as
in a toaster. A fan blows air across the hot coil, and forced convection carries the 1000 J of heat
into the house. In contrast, the heat pump in Figure 15.15 does not use the 1000 J directly as heat. Instead, it uses the 1000 J to do the work (magnitude = |W|) of pumping heat (magnitude = |QC|) from the cooler outdoors into the warmer house and, in so doing, delivers an amount of energy |QH| = |W| + |QC|. With |W| = 1000 J, this becomes |QH| = 1000 J + |QC|, so that the heat pump delivers more than 1000 J of heat, whereas the conventional electric heating system
delivers only 1000 J.
CONCEPTUAL EXAMPLE 9 You Can’t Beat the Second Law of Thermodynamics
Is it possible (A) to cool your kitchen by leaving the refrigerator door
open or (B) to cool your bedroom by putting a window air conditioner
on the fl oor by the bed? (a) Only A is possible. (b) Only B is possible. (c) Both are possible. (d) Neither is possible.
Reasoning During a refrigeration process (be it in a refrigerator or in an air conditioner), heat (magnitude = |QC|) is removed from a cold reservoir and heat (magnitude = |QH|) is deposited into a hot reservoir. Moreover, according to the second law of thermodynamics, work (magnitude = |W|) is required to move this heat from the cold reservoir to the hot reservoir. The
principle of conservation of energy states that |QH| = |W| + |QC| (Equation 15.12), and we will use this as a guide in assessing the possibilities.
Answers (a), (b), and (c) are incorrect. If you wanted to cool your kitchen by leaving the refrigerator door open, the refrigerator would have
to take heat from directly in front of the open door and pump less heat out the back of the unit and into the kitchen (since the refrigerator is sup-
posed to be cooling the entire kitchen). Likewise, if you tried to cool your
entire bedroom by placing the air conditioner on the fl oor by the bed, the
air conditioner would have to take heat (magnitude = |QC|) from directly
in front of the unit and deposit less heat (magnitude = |QH|) out the back. According to the second law of thermodynamics this cannot happen,
since |QH| = |W| + |QC|; that is, |QH| is greater than (not less than) |QC| because |W| is greater than zero.
Answer (d) is correct. The heat (magnitude = |QC|) removed from the air directly in front of the open refrigerator is deposited back into the
kitchen at the rear of the unit. Moreover, according to the second law of
thermodynamics, work (magnitude = |W|) is needed to move that heat from cold to hot, and the energy from this work is also deposited into the
kitchen as additional heat. Thus, the open refrigerator puts into the kitchen
an amount of heat |QH| = |W| + |QC|, which is more than it removes from in front of the open refrigerator. Thus, rather than cooling the kitchen, the
open refrigerator warms it up. Putting an air conditioner on the fl oor to
cool your bedroom is similarly a no-win game. The heat pumped out the
back of the air conditioner and into the bedroom is greater than the heat
pulled into the front of the unit. Consequently, the air conditioner actually
warms the bedroom.
Related Homework: Problem 71
FIGURE 15.15 In a heat pump the cold reservoir is the wintry outdoors, and the hot
reservoir is the inside of the house.
�QC� (Cold outdoors)
�QH� = �W � + �QC� (Warm house)
Heat pump
�W � = Magnitude of work done by
electrical energy
420 CHAPTER 15 Thermodynamics
It is also possible to specify a coeffi cient of performance for heat pumps. However, unlike
refrigerators and air conditioners, the job of a heat pump is to heat, not to cool. As a result, the
coeffi cient of performance of a heat pump is the ratio of the magnitude of the heat |QH| delivered into the house to the magnitude of the work |W| required to deliver it:
Heat pump
Coeffi cient of performance =
∣QH∣ ∣W∣ (15.17)
The coeffi cient of performance depends on the indoor and outdoor temperatures. Commercial
units have coeffi cients of about 3 to 4 under favorable conditions.
Check Your Understanding
(The answers are given at the end of the book.) 16. Each drawing in CYU Figure 15.4 represents a hypothetical heat engine or a hypothetical heat pump
and shows the corresponding heats and work. Only one of these hypothetical situations is allowed in
nature. Which is it?
Cold reservoir
(a)
�W � = 400 J �W � = 300 J
�QH� = 300 J
�QC� = 100 J
�W � = 100 J
�QH� = 500 J
�QC� = 400 J
�QH� = 100 J
�QC� = 400 J
Hot reservoir
Cold reservoir
Hot reservoir
Cold reservoir
Hot reservoir
�W � = 100 J
�QH� = 300 J
�QC� = 400 J
�W � = 400 J
�QH� = 400 J
�QC� = 0 J
Cold reservoir
Hot reservoir
Cold reservoir
Hot reservoir
(b) (c) (d) (e)
CYU FIGURE 15.4
17. A refrigerator is kept in a garage that is not heated in the cold winter or air-conditioned in the hot summer. Does it cost more for this refrigerator to make a kilogram of ice cubes in the winter or in the
summer? (a) In the summer (b) In the winter (c) It costs the same in both seasons. 18. The coeffi cient of performance of a heat pump that is removing heat from the cold outdoors (a) must
always be less than one, (b) can be either less than or greater than one, (c) must always be greater than one.
19. A kitchen air conditioner and a refrigerator both remove heat from a cold reservoir and deposit it in a hot reservoir. The air conditioner _________ the kitchen, whereas the refrigerator _________ the
kitchen. (a) cools, cools (b) cools, warms (c) warms, warms (d) warms, cools 20. On a summer day a window air conditioner cycles on and off , according to how the temperature within
the room changes. When are you more likely to be able to fry an egg on the outside part of the unit?
(a) When the unit is on (b) When the unit is off (c) It does not matter whether the unit is on or off .
15.11 Entropy A Carnot engine has the maximum possible effi ciency for its operating conditions because the
processes occurring within it are reversible. Irreversible processes, such as friction, cause real
engines to operate at less than maximum effi ciency, for they reduce our ability to use heat to
perform work. As an extreme example, imagine that a hot object is placed in thermal contact with
a cold object, so heat fl ows spontaneously, and hence irreversibly, from hot to cold. Eventually
both objects reach the same temperature, and TC = TH. A Carnot engine using these two objects as heat reservoirs is unable to do work, because the effi ciency of the engine is zero [eCarnot = 1 − (TC/TH) = 0]. In general, irreversible processes cause us to lose some, but not necessarily all, of the ability to perform work. This partial loss can be expressed in terms of a concept called entropy.
To introduce the idea of entropy we recall the relation |QC|/|QH| = TC/TH (Equation 15.14) that applies to a Carnot engine. It is possible to rearrange this equation as |QC|/TC = |QH|/TH,
1000 J
Heat = 1000 J
Heater coil
FIGURE 15.16 This conventional electric heating system is delivering 1000 J of heat to
the living room.
15.11 Entropy 421
which focuses attention on the heat Q divided by the Kelvin temperature T. The quantity Q/T is called the change in the entropy ΔS:
∆S = (QT )R (15.18) In this expression the temperature T must be in kelvins, and the subscript R refers to the word “reversible.” It can be shown that Equation 15.18 applies to any process in which heat enters (Q is positive) or leaves (Q is negative) a system reversibly at a constant temperature. Such is the case for the heat that fl ows into and out of the reservoirs of a Carnot engine. Equation 15.18 indicates
that the SI unit for entropy is a joule per kelvin (J/K).
Entropy, like internal energy, is a function of the state or condition of the system. Only the
state of a system determines the entropy S that a system has. Therefore, the change in entropy ΔS is equal to the entropy of the fi nal state of the system minus the entropy of the initial state.
We can now describe what happens to the entropy of a Carnot engine. As the engine operates,
the entropy of the hot reservoir decreases, since heat of magnitude |QH| departs reversibly at a Kelvin temperature TH. The corresponding change in the entropy is ΔSH = −|QH|/TH, where the minus sign is needed to indicate a decrease, since the symbol |QH| denotes only the magnitude of the heat. In contrast, the entropy of the cold reservoir increases by an amount ΔSC = +|QC|/TC, for the rejected heat reversibly enters the cold reservoir at a Kelvin temperature TC. The total change in entropy is
∆SC + ∆SH = + ∣QC∣ TC
− ∣QH∣ TH
= 0
because |QC|/TC = |QH|/TH according to Equation 15.14. The fact that the total change in entropy is zero for a Carnot engine is a specifi c illustration
of a general result. It can be proved that when any reversible process occurs, the change in the entropy of the universe is zero; ΔSuniverse = 0 J/K for a reversible process. The word “universe” means that ΔSuniverse takes into account the entropy changes of all parts of the system and all parts of the environment. Reversible processes do not alter the total entropy of the universe. To be sure, the entropy of one part of the universe may change because of a reversible process, but if so,
the entropy of another part changes in the opposite way by the same amount.
What happens to the entropy of the universe when an irreversible process occurs is more complex, because the expression ΔS = (Q/T)R does not apply directly. However, if a system changes irreversibly from an initial state to a fi nal state, this expression can be used to calcu-
late ΔS indirectly, as Figure 15.17 indicates. We imagine a hypothetical reversible process that causes the system to change between the same initial and fi nal states and then fi nd ΔS for this reversible process. The value obtained for ΔS also applies to the irreversible process that actually occurs, since only the nature of the initial and fi nal states, and not the path between them, deter-
mines ΔS. Example 10 illustrates this indirect method and shows that spontaneous (irreversible) processes increase the entropy of the universe.
Irreversible process
Hypothetical reversible process
Initial state
Final state
S for irreversible process
S for hypothetical reversible process
=∆ ∆
FIGURE 15.17 Although the relation ΔS = (Q/T)R applies to reversible processes, it can be used as part of an indirect procedure
to fi nd the entropy change for an irreversible
process. This drawing illustrates the procedure
discussed in the text.
EXAMPLE 10 The Entropy of the Universe Increases
Figure 15.18 shows 1200 J of heat fl owing spontaneously through a cop- per rod from a hot reservoir at 650 K to a cold reservoir at 350 K. Deter-
mine the amount by which this irreversible process changes the entropy
of the universe, assuming that no other changes occur.
Reasoning The hot-to-cold heat fl ow is irreversible, so the relation ΔS = (Q/T)R is applied to a hypothetical process whereby the 1200 J of heat is taken reversibly from the hot reservoir and added reversibly to the
cold reservoir.
Solution The total entropy change of the universe is the algebraic sum of the entropy changes for each reservoir:
∆Suniverse = − 1200 J
650 K +
1200 J
350 K = +1.6 J/K
The irreversible process causes the entropy of the universe to increase by
1.6 J/K.
{
Entropy lost
by hot reservoir
Entropy gained
by cold reservoir
⏟⏟⏟
FIGURE 15.18 Heat fl ows spontaneously from a hot reservoir
to a cold reservoir.
Cold reservoir TC = 350 K
Hot reservoir TH = 650 K
Copper rod
1200 J
422 CHAPTER 15 Thermodynamics
Example 10 is a specifi c illustration of a general result: Any irreversible process increases the entropy of the universe. In other words, ΔSuniverse > 0 J/K for an irreversible process. Revers- ible processes do not alter the entropy of the universe, whereas irreversible processes cause the
entropy to increase. Therefore, the entropy of the universe continually increases, like time itself,
and entropy is sometimes called “time’s arrow.” It can be shown that this behavior of the entropy
of the universe provides a completely general statement of the second law of thermodynamics,
which applies not only to heat fl ow but also to all kinds of other processes.
THE SECOND LAW OF THERMODYNAMICS STATED IN TERMS OF ENTROPY The total entropy of the universe does not change when a reversible process occurs (ΔSuniverse = 0 J/K) and increases when an irreversible process occurs (ΔSuniverse > 0 J/K).
When an irreversible process occurs and the entropy of the universe increases, the energy
available for doing work decreases, as the next example illustrates.
Example 11 shows that 240 J less work (920 J − 680 J) can be performed when the input
heat is obtained from the hot reservoir with the lower temperature. In other words, the irreversible
process of heat fl ow through the copper rod causes energy to become unavailable for doing work
in the amount of Wunavailable = 240 J. Example 10 shows that this irreversible process simultaneously causes the entropy of the universe to increase by an amount ΔSuniverse = +1.6 J/K. These values for Wunavailable and ΔSuniverse are in fact related. If you multiply ΔSuniverse by 150 K, which is the low- est Kelvin temperature in Example 11, you obtain Wunavailable = (150 K) × (1.6 J/K) = 240 J. This illustrates the following general result:
Wunavailable = T0 ∆Suniverse (15.19)
where T0 is the Kelvin temperature of the coldest heat reservoir. Since irreversible processes cause the entropy of the universe to increase, they cause energy to be degraded, in the sense that part of
EXAMPLE 11 Energy Unavailable for Doing Work
Suppose that 1200 J of heat is used as input for an engine under two dif-
ferent conditions. In Figure 15.19a the heat is supplied by a hot reservoir whose temperature is 650 K. In part b of the drawing, the heat fl ows irre- versibly through a copper rod into a second reservoir whose temperature
is 350 K and then enters the engine. In either case, a 150-K reservoir is
used as the cold reservoir. For each case, determine the maximum amount
of work that can be obtained from the 1200 J of heat.
Reasoning According to Equation 15.11, the work (magnitude = |W|) obtained from the engine is the product of its effi ciency e and the input heat (magnitude = |QH|), or |W| = e|QH|. For a given input heat, the maximum amount of work is obtained when the effi ciency is a maximum;
that is, when the engine is a Carnot engine. The effi ciency of a Carnot
engine is given by Equation 15.15 as eCarnot = 1 − TC/TH. Therefore, the effi ciency may be determined from the Kelvin temperatures of the hot and
cold reservoirs.
Solution
Before irreversible heat fl ow
eCarnot = 1 − TC TH
= 1 − 150 K
650 K = 0.77
∣W∣ = (eCarnot) (1200 J) = (0.77)(1200 J) = 920 J
After irreversible heat fl ow
eCarnot = 1 − TC TH
= 1 − 150 K
350 K = 0.57
∣W∣ = (eCarnot) (1200 J) = (0.57)(1200 J) = 680 J
Carnot engine
Cold reservoir TC = 150 K
∙QH∙ = 1200 J
∙QC∙ = 280 J
∙W ∙ = 920 J
Hot reservoir TH = 650 K
(a)
Carnot engine
Cold reservoir TC = 150 K
∙W ∙ = 680 J
∙QH∙ = 1200 J
∙QC∙ = 520 J
(b)
Copper rod
1200 J
650 K
Hot reservoir TH = 350 K
FIGURE 15.19 Heat in the amount of |QH| = 1200 J is used as input for an engine under two diff erent conditions in parts a and b.
When the 1200 J of input heat is taken from the 350-K reservoir instead
of the 650-K reservoir, the effi ciency of the Carnot engine is smaller.
As a result, less work (680 J versus 920 J) can be extracted from the
input heat.
15.11 Entropy 423
the energy becomes unavailable for the performance of work. In contrast, there is no penalty when
reversible processes occur, because for them ΔSuniverse = 0 J/K, and there is no loss of work. Entropy can also be interpreted in terms of order and disorder. As an example, consider
a block of ice (Figure 15.20) with each of its H2O molecules fi xed rigidly in place in a highly structured and ordered arrangement. In comparison, the puddle of water into which the ice melts
is disordered and unorganized, because the molecules in a liquid are free to move from place to
place. Heat is required to melt the ice and produce the disorder. Moreover, heat fl ow into a sys-
tem increases the entropy of the system, according to ΔS = (Q/T)R. We associate an increase in entropy, then, with an increase in disorder. Conversely, we associate a decrease in entropy with
a decrease in disorder or a greater degree of order. Example 12 illustrates an order-to-disorder
change and the increase of entropy that accompanies it.
Block of ice
Puddle of water
ΔS increase
ΔS decrease FIGURE 15.20 A block of ice is an example of an ordered system relative to a puddle of
water.
EXAMPLE 12 Order to Disorder
Find the change in entropy that results when a 2.3-kg block of ice melts
slowly (reversibly) at 273 K (0 °C).
Reasoning Since the phase change occurs reversibly at a constant tem- perature, the change in entropy can be found by using Equation 15.18,
ΔS = (Q/T)R, where Q is the heat absorbed by the melting ice. This heat can be determined by using the relation Q = mLf (Equation 12.5), where m is the mass and Lf = 3.35 × 105 J/kg is the latent heat of fusion of water (see Table 12.3).
Solution Using Equation 15.18 and Equation 12.5, we fi nd that the change in entropy is
∆S = ( Q T )R =
mL f T
= (2.3 kg)(3.35 × 105 J/kg)
273 K = +2.8 × 103 J/K
a result that is positive, since the ice absorbs heat as it melts.
Figure 15.21 shows another order-to-disorder change that can be described in terms of entropy.
Check Your Understanding
(The answers are given at the end of the book.) 21. Two equal amounts of water are mixed together in an insulated container, and no work is done in the
process. The initial temperatures of the water are diff erent, but the mixture reaches a uniform temperature.
Do the internal energy and entropy of the water increase, decrease, or remain constant as a result of the
mixing process (refer to CYU Table 15.3)?
CYU TABLE 15.3
Internal Energy of the Water
Entropy of the Water
(a) Increases Increases
(b) Decreases Decreases
(c) Remains constant Decreases
(d) Remains constant Increases
(e) Remains constant Remains constant
(Continued)
424 CHAPTER 15 Thermodynamics
22. An event happens somewhere in the universe and, as a result, the entropy of an object changes by −5 J/K. Consistent with the second law of thermodynamics, which one (or more) of the following is a possible
value for the entropy change for the rest of the universe? (a) −5 J/K (b) 0 J/K (c) +5 J/K (d) +10 J/K 23. In each of the following cases, which has the greater entropy, a handful of popcorn kernels or the
popcorn that results from them; a salad before or after it has been tossed; and a messy apartment or a
neat apartment?
24. A glass of water contains a teaspoon of dissolved sugar. After a while, the water evaporates, leaving behind sugar crystals. The entropy of the sugar crystals is less than the entropy of the dissolved sugar
because the sugar crystals are in a more ordered state. Why doesn’t this process violate the second
law of thermodynamics? (a) Because, considering what happens to the water, the total entropy of the universe also decreases. (b) Because, considering what happens to the water, the total entropy of the universe increases. (c) Because the second law does not apply to this situation.
25. A builder uses lumber to construct a building, which is unfortunately destroyed in a fi re. Thus, the lumber existed at one time or another in three diff erent states: (A) as unused building material, (B) as
a building, and (C) as a burned-out shell of a building. Rank these three states in order of decreasing
entropy (largest fi rst). (a) C, B, A (b) A, B, C (c) C, A, B (d) A, C, B (e) B, A, C
M ar
ti n H
u n te
r/ G
et ty
I m
ag es
FIGURE 15.21 With the aid of explosives, demolition experts caused this building to go from the ordered state (lower entropy), top photograph, to the disordered state (higher entropy), bottom photograph.
Concept Summary 425
Concept Summary 15.1 Thermodynamic Systems and Their Surroundings A thermody- namic system is the collection of objects on which attention is being focused,
and the surroundings are everything else in the environment. The state of a
system is the physical condition of the system, as described by values for
physical parameters, often pressure, volume, and temperature.
15.2 The Zeroth Law of Thermodynamics Two systems are in thermal equilibrium if there is no net fl ow of heat between them when they are
brought into thermal contact. Temperature is the indicator of thermal equi-
librium in the sense that there is no net fl ow of heat between two systems in
thermal contact that have the same temperature. The zeroth law of thermo-
dynamics states that two systems individually in thermal equilibrium with a
third system are in thermal equilibrium with each other.
15.3 The First Law of Thermodynamics The fi rst law of thermodynamics states that due to heat Q and work W, the internal energy of a system changes from its initial value of Ui to a fi nal value of Uf according to Equation 15.1. In this equation Q is positive when the system gains heat and negative when it loses heat. W is positive when work is done by the system and negative when work is done on the system. The fi rst law of thermodynamics is the
conservation-of-energy principle applied to heat, work, and the change in the
internal energy.
∆U = Uf − Ui = Q − W (15.1)
The internal energy is called a function of state because it depends only
on the state of the system and not on the method by which the system came
to be in a given state.
15.4 Thermal Processes A thermal process is quasi-static when it occurs slowly enough that a uniform pressure and temperature exist throughout the
system at all times. An isobaric process is one that occurs at constant
pressure. The work W done when a system changes at a constant pressure P from an initial volume Vi to a fi nal volume Vf is given by Equation 15.2. An iso- choric process is one that takes place at constant volume, and no work is done
in such a process. An isothermal process is one that takes place at constant
temperature. An adiabatic process is one that takes place without the transfer
of heat. The work done in any kind of quasi-static process is given by the area
under the corresponding pressure–volume graph.
W = P ∆V = P(Vf − Vi) (15.2)
15.5 Thermal Processes Using an Ideal Gas When n moles of an ideal gas change quasi-statically from an initial volume Vi to a fi nal volume Vf at a constant Kelvin temperature T, the work done is given by Equation 15.3, and the process is said to be isothermal.
W = n RT ln( Vf Vi) (15.3)
15.12 The Third Law of Thermodynamics To the zeroth, fi rst, and second laws of thermodynamics we add the third (and last) law. The third law of thermodynamics indicates that it is impossible to reach a temperature of absolute zero.
THE THIRD LAW OF THERMODYNAMICS It is not possible to lower the temperature of any system to absolute zero (T = 0 K) in a fi nite number of steps.
This law, like the second law, can be expressed in a number of ways, but a discussion of them is
beyond the scope of this text. The third law is needed to explain a number of experimental obser-
vations that cannot be explained by the other laws of thermodynamics.
EXAMPLE 13 BIO Refueling Your Lost Internal Energy
Your body acts like a heat engine and must obey the laws of thermodynam-
ics. Suppose you spend 1 hour jogging and do work with a power output of
170 W. During this time, you also give off 4.2 × 105 J of heat to your sur-
roundings. How many bananas would you have to eat to replace the inter-
nal energy you lost by jogging? Assume one banana contains 100 Calories.
Reasoning We can use the fi rst law of thermodynamics (Equation 15.1) to calculate the change in the jogger’s internal energy. This depends on
the heat (Q) lost or gained by the system and the work (W) done on or by the system. Once we know the jogger’s change in internal energy, then
we can use the mechanical equivalent of heat to calculate the Calories
(bananas) she must eat to replace this lost energy.
Solution We begin by using the fi rst law of thermodynamics (Equa- tion 15.1): ΔU = Q − W. The heat from the system (the jogger) is given
in the problem, and it will be negative, since it is lost by the system. The
work (W) will be positive, since it is done by the system. We can calculate the work using the power output and the time she runs: W = Pt = (170 W) (3600 s) = 6.1 × 105 J. Calculating the change in the internal energy, we
get: ΔU = −4.2 × 105 J − 6.1 × 105 J = −10.3 × 105 J. As expected, her change in internal energy is negative, and it’s this quantity that must be
replaced by the food she eats. Each banana contains 100 Calories, which
is equal to 100 kcal. This is equivalent to (100 kcal) × (4186 J/kcal) =
4.186 × 105 J per banana. The number of bananas required to replace
her lost internal energy will be: (10.3 × 105 J)/( 4.186 × 105 J/banana) =
2.5 bananas
There is a lot of energy content in food!
426 CHAPTER 15 Thermodynamics
When n moles of a monatomic ideal gas change quasi-statically and adia- batically from an initial temperature Ti to a fi nal temperature Tf, the work done is given by Equation 15.4. During an adiabatic process, and in addition
to the ideal gas law, an ideal gas obeys Equation 15.5, where 𝛾 = cP/cV is the ratio of the specifi c heat capacities at constant pressure and constant volume.
W = 32 n R (Ti − Tf ) (15.4)
PiV γi = PfV γf (15.5)
15.6 Specifi c Heat Capacities The molar specifi c heat capacity C of a substance determines how much heat Q is added or removed when the tem- perature of n moles of the substance changes by an amount ΔT, according to Equation 15.6. For a monatomic ideal gas, the molar specifi c heat capacities
at constant pressure and constant volume are given by Equations 15.7 and
15.8, respectively, where R is the ideal gas constant. For a diatomic ideal gas at moderate temperatures that do not allow vibration to occur, these values
are CP = 7
2 R and CV = 5
2 R. For any type of ideal gas, the diff erence between CP and CV is given by Equation 15.10.
Q = Cn ∆T (15.6)
CP = 5
2 R (15.7)
CV = 3
2 R (15.8)
CP − CV = R (15.10)
15.7 The Second Law of Thermodynamics The second law of thermo- dynamics can be stated in a number of equivalent forms. In terms of heat
fl ow, the second law declares that heat fl ows spontaneously from a substance
at a higher temperature to a substance at a lower temperature and does not
fl ow spontaneously in the reverse direction.
15.8 Heat Engines A heat engine produces work (magnitude = |W|) from input heat (magnitude = |QH|) that is extracted from a heat reservoir at a relatively high temperature. The engine rejects heat (magnitude = |QC|) into a reservoir at a relatively low temperature. The effi ciency e of a heat engine is given by Equation 15.11.
e = Work done
Input heat =
∣W∣ ∣QH∣
(15.11)
The conservation of energy requires that |QH| must be equal to |W| plus |QC|, as in Equation 15.12. By combining Equation 15.12 with Equation 15.11, the effi ciency of a heat engine can also be written as shown in Equation 15.13.
∣QH∣ = ∣W∣ + ∣QC∣ (15.12)
e = 1 − ∣QC∣ ∣QH∣
(15.13)
15.9 Carnot’s Principle and the Carnot Engine A reversible process is one in which both the system and its environment can be returned to exactly the states they were in before the process occurred.
Carnot’s principle is an alternative statement of the second law of thermo-
dynamics. It states that no irreversible engine operating between two reservoirs
at constant temperatures can have a greater effi ciency than a reversible engine
operating between the same temperatures. Furthermore, all reversible engines
operating between the same temperatures have the same effi ciency.
A Carnot engine is a reversible engine in which all input heat (magnitude =
|QH|) originates from a hot reservoir at a single Kelvin temperature TH and all rejected heat (magnitude = |QC|) goes into a cold reservoir at a single Kelvin temperature TC. For a Carnot engine, Equation 15.14 applies. The effi ciency eCarnot of a Carnot engine is the maximum effi ciency that an engine operating between two fi xed temperatures can have and is given by Equation 15.15.
∣QC∣ ∣QH∣
= TC TH
(15.14)
eCarnot = 1 − TC TH
(15.15)
15.10 Refrigerators, Air Conditioners, and Heat Pumps Refrigerators, air conditioners, and heat pumps are devices that utilize work (magnitude =
|W|) to make heat (magnitude = |QC|) fl ow from a lower Kelvin temperature TC to a higher Kelvin temperature TH. In the process (the refrigeration pro- cess) they deposit heat (magnitude = |QH|) at the higher temperature. The principle of the conservation of energy requires that |QH| = |W| + |QC|.
Coeffi cient of performance
of a refrigerator =
∣QC∣ ∣W∣
(15.16)
If the refrigeration process is ideal, in the sense that it occurs reversibly,
the devices are called Carnot devices and the relation |QC|/|QH| = TC/TH (Equation 15.14) holds.
The coeffi cient of performance of a refrigerator or an air conditioner is
given by Equation 15.16. The coeffi cient of performance of a heat pump,
however, is given by Equation 15.17.
Coeffi cient of performance
of a heat pump =
∣QH∣ ∣W∣
(15.17)
15.11 Entropy The change in entropy ΔS for a process in which heat Q enters or leaves a system reversibly at a constant Kelvin temperature T is given by Equation 15.18, where the subscript R stands for “reversible.”
∆S = ( Q T )R (15.18)
The second law of thermodynamics can be stated in a number of equiva-
lent forms. In terms of entropy, the second law states that the total entropy
of the universe does not change when a reversible process occurs (ΔSuniverse = 0 J/K) and increases when an irreversible process occurs (ΔSuniverse > 0 J/K).
Irreversible processes cause energy to be degraded in the sense that part of the
energy becomes unavailable for the performance of work. The energy Wunavailable that is unavailable for doing work because of an irreversible process is shown in
Equation 15.19, where ΔSuniverse is the total entropy change of the universe and T0 is the Kelvin temperature of the coldest reservoir into which heat can be rejected.
Wunavailable = T0 ∆Suniverse (15.19)
Increased entropy is associated with a greater degree of disorder and
decreased entropy with a lesser degree of disorder (more order).
15.12 The Third Law of Thermodynamics The third law of thermody- namics states that it is not possible to lower the temperature of any system to
absolute zero (T = 0 K) in a fi nite number of steps.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 15.3 The First Law of Thermodynamics
1. The fi rst law of thermodynamics states that the change ΔU in the internal energy of a system is given by ΔU = Q − W, where Q is the heat and W is
Focus on Concepts
Problems 427
the work. Both Q and W can be positive or negative numbers. Q is a positive number if ________, and W is a positive number if ________. (a) the system loses heat; work is done by the system (b) the system loses heat; work is done on the system (c) the system gains heat; work is done by the system (d) the system gains heat; work is done on the system
Section 15.4 Thermal Processes 4. The drawing shows the expansion of three ideal gases. Rank the gases according to the work they do, largest to smallest. (a) A, B, C (b) A and B (a tie), C (c) B and C (a tie), A (d) B, C, A (e) C, A, B
QUESTION 4
P re
ss ur
e
Volume
A
B
C
6. The pressure–volume graph shows three paths in which a gas expands from
an initial state A to a fi nal state B. The
change ∆UA→B in internal energy is the same for each of the paths. Rank the paths
according to the heat Q added to the gas, largest to smallest. (a) 1, 2, 3 (b) 1, 3, 2 (c) 2, 1, 3 (d) 3, 1, 2 (e) 3, 2, 1
Section 15.5 Thermal Processes Using an Ideal Gas 8. An ideal monatomic gas expands isotherm- ally from A to B, as the graph shows. What can
be said about this process? (a) The gas does no work. (b) No heat enters or leaves the gas. (c) The fi rst law of thermodynamics does not apply to an
isothermal process. (d) The ideal gas law is not valid during an isothermal process. (e) There is no change in the internal energy of the gas.
10. A monatomic ideal gas is thermally insulated, so no heat can fl ow between it and its surroundings. Is it possible for the temperature of the gas
to rise? (a) Yes. The temperature can rise if work is done by the gas. (b) No. The only way that the temperature can rise is if heat is added to the gas.
(c) Yes. The temperature can rise if work is done on the gas.
Section 15.8 Heat Engines 13. A heat engine takes heat QH from a hot reservoir and uses part of this energy to perform work W. Assuming that QH cannot be changed, how can the effi ciency of the engine be improved? (a) Increase the work W; the heat QC rejected to the cold reservoir increases as a result. (b) Increase the work W; the heat QC rejected to the cold reservoir remains unchanged. (c) Increase the work W; the heat QC rejected to the cold reservoir decreases as a result. (d) Decrease the work W; the heat QC rejected to the cold reservoir remains unchanged. (e) Decrease the work W; the heat QC rejected to the cold reservoir decreases as a result.
Section 15.9 Carnot’s Principle and the Carnot Engine 15. The three Carnot engines shown in the drawing operate with hot and cold reservoirs whose temperature diff erences are 100 K. Rank the effi ciencies
of the engines, largest to smallest. (a) All engines have the same effi ciency. (b) A, B, C (c) B, A, C (d) C, B, A (e) C, A, B
QUESTION 15
800 K
�W � �W � �W �
900 K
400 K
500 K
100 K
200 K
�QH� �QH� �QH�
�QC� �QC� �QC�
A B C
Section 15.10 Refrigerators, Air Conditioners, and Heat Pumps 17. A refrigerator operates for a certain time, and the work done by the elec- trical energy during this time is W = 1000 J. What can be said about the heat delivered to the room containing the refrigerator? (a) The heat delivered to the room is less than 1000 J. (b) The heat delivered to the room is equal to 1000 J. (c) The heat delivered to the room is greater than 1000 J.
Section 15.11 Entropy 19. Heat is transferred from the sun to the earth via electromagnetic waves (see Chapter 24). Because of this transfer, the entropy of the sun ________,
the entropy of the earth ________, and the entropy of the sun–earth system
________. (a) increases, decreases, decreases (b) decreases, increases, in- creases (c) increases, increases, increases (d) increases, decreases, increases (e) decreases, increases, decreases
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 15.3 The First Law of Thermodynamics 1. E In moving out of a dormitory at the end of the semester, a student does 1.6 × 104 J of work. In the process, his internal energy decreases by 4.2 × 104 J.
Determine each of the following quantities (including the algebraic sign):
(a) W (b) ΔU (c) Q
2. E The internal energy of a system changes because the system gains 165 J of heat and performs 312 J of work. In returning to its initial state,
the system loses 114 J of heat. During this return process, (a) what work is involved, and (b) is the work done by the system or on the system?
3. E SSM A system does 164 J of work on its environment and gains 77 J of heat in the process. Find the change in the internal energy of (a) the system and (b) the environment.
4. E GO A system does 4.8 × 104 J of work, and 7.6 × 104 J of heat fl ows into the system during the process. Find the change in the internal energy of
the system.
Problems
QUESTION 6
P re
ss ur
e
Volume
A
B
1
2 3
P re
ss ur
e
Volume
A
B
Isotherm
QUESTION 8
428 CHAPTER 15 Thermodynamics
5. E BIO GO In a game of football outdoors on a cold day, a player will begin to feel exhausted after using approximately 8.0 × 105 J of internal energy. (a) One player, dressed too lightly for the weather, has to leave the game after losing 6.8 × 105 J of heat. How much work has he done? (b) Another player, wearing clothes that off er better protection against heat loss, is able to remain
in the game long enough to do 2.1 × 105 J of work. What is the magnitude of
the heat that he has lost?
6. E V-HINT Three moles of an ideal monatomic gas are at a temperature of 345 K. Then, 2438 J of heat is added to the gas, and 962 J of work is done on
it. What is the fi nal temperature of the gas?
7. M BIO CHALK SSM In exercising, a weight lifter loses 0.150 kg of water through evaporation, the heat required to evaporate the water coming from
the weight lifter’s body. The work done in lifting weights is 1.40 × 105 J. (a) Assuming that the latent heat of vaporization of perspiration is 2.42 × 106 J/kg, fi nd the change in the internal energy of the weight lifter. (b) De- termine the minimum number of nutritional Calories of food (1 nutritional
Calorie = 4186 J) that must be consumed to replace the loss of internal
energy.
Section 15.4 Thermal Processes 8. E A system undergoes a two-step process. In the fi rst step, the internal energy of the system increases by 228 J when 166 J of work is done on the
system. In the second step, the internal energy of the system increases by 115 J
when 177 J of work is done on the system. For the overall process, fi nd the
heat. What type of process is the overall process? Explain.
9. E SSM When a .22-caliber rifl e is fi red, the expanding gas from the burning gunpowder creates a pressure behind the bullet. This pressure
causes the force that pushes the bullet through the barrel. The barrel has
a length of 0.61 m and an opening whose radius is 2.8 × 10−3 m. A bullet
(mass = 2.6 × 10−3 kg) has a speed of 370 m/s after passing through this
barrel. Ignore friction and determine the average pressure of the expand-
ing gas.
10. E GO A system gains 2780 J of heat at a constant pressure of 1.26 × 105 Pa, and its internal energy increases by 3990 J. What is the change in the
volume of the system, and is it an increase or a decrease?
11. E V-HINT A system gains 1500 J of heat, while the internal energy of the system increases by 4500 J and the volume decreases by 0.010 m3. Assume
that the pressure is constant and fi nd its value.
12. E The volume of a gas is changed along the curved line between A and B in the draw- ing. Do not assume that the curved line is an
isotherm or that the gas is ideal. (a) Find the magnitude of the work for the process, and (b) determine whether the work is positive or negative.
13. E SSM (a) Using the data presented in the accompanying pressure– volume
graph, estimate the magnitude of the
work done when the system changes
from A to B to C along the path shown. (b) Determine whether the work is done by the system or on the system
and, hence, whether the work is posit-
ive or negative.
14. E Sections 14.2 and 14.3 provide useful information for this problem.
When a monatomic ideal gas expands
at a constant pressure of 2.6 × 105 Pa,
the volume of the gas increases by 6.2 × 10−3 m3. (a) Determine the heat that fl ows into or out of the gas. (b) Specify the direction of the fl ow.
15. E CHALK A gas is contained in a chamber such as that in Figure 15.4. Suppose that the region outside the chamber is evacuated and the total mass
of the block and the movable piston is 135 kg. When 2050 J of heat fl ows
into the gas, the internal energy of the gas increases by 1730 J. What is the
distance s through which the piston rises? 16. M A piece of aluminum has a volume of 1.4 × 10−3 m3. The coeffi cient of volume expansion for aluminum is 𝛽 = 69 × 10−6 (C°)−1. The temperature of this object is raised from 20 to 320 °C. How much work is done by the
expanding aluminum if the air pressure is 1.01 × 105 Pa?
17. M SSM Refer to Multiple-Concept Example 3 to see how the concepts pertinent to this problem are used. The pressure of a gas remains constant
while the temperature, volume, and internal energy of the gas increase by
53.0 C°, 1.40 × 10−3 m3, and 939 J, respectively. The mass of the gas is 24.0 g,
and its specifi c heat capacity is 1080 J/(kg · C°). Determine the pressure. 18. M GO Refer to the drawing that accompanies Problem 13. When a system changes from A to B along the path shown on the pressure-versus- volume graph, it gains 2700 J of heat. What is the change in the internal
energy of the system?
19. H Water is heated in an open pan where the air pressure is one atmo- sphere. The water remains a liquid, which expands by a small amount as
it is heated. Determine the ratio of the work done by the water to the heat
absorbed by the water.
Section 15.5 Thermal Processes Using an Ideal Gas 20. E Six grams of helium (molecular mass = 4.0 u) expand isothermally at 370 K and do 9600 J of work. Assuming that helium is an ideal gas, determ-
ine the ratio of the fi nal volume of the gas to the initial volume.
21. E SSM Five moles of a monatomic ideal gas expand adiabatically, and its temperature decreases from 370 to 290 K. Determine (a) the work done (in- cluding the algebraic sign) by the gas, and (b) the change in its internal energy. 22. E GO Three moles of neon expand isothermally to 0.250 from 0.100 m3. Into the gas fl ows 4.75 × 103 J of heat. Assuming that neon is an ideal gas,
fi nd its temperature.
23. E The temperature of a monatomic ideal gas remains constant during a process in which 4700 J of heat fl ows out of the gas. How much work (in-
cluding the proper + or − sign) is done?
24. E GO One-half mole of a monatomic ideal gas expands adiabatically and does 610 J of work. By how many kelvins does its temperature change?
Specify whether the change is an increase or a decrease.
25. E SSM A monatomic ideal gas has an initial temperature of 405 K. This gas expands and does the same amount of work whether the expansion is
adiabatic or isothermal. When the expansion is adiabatic, the fi nal temper-
ature of the gas is 245 K. What is the ratio of the fi nal to the initial volume
when the expansion is isothermal?
26. E V-HINT Heat is added isothermally to 2.5 mol of a monatomic ideal gas. The temperature of the gas is 430 K. How much heat must be added to
make the volume of the gas double?
27. M MMH A diesel engine does not use spark plugs to ignite the fuel and air in the cylinders. Instead, the temperature required to ignite the fuel
occurs because the pistons compress the air in the cylinders. Suppose that
air at an initial temperature of 21 °C is compressed adiabatically to a tem-
perature of 688 °C. Assume the air to be an ideal gas for which γ = 75. Find the compression ratio, which is the ratio of the initial volume to the fi nal
volume.
28. M A monatomic ideal gas expands from point A to point B along the path shown in the drawing. (a) Determine the work done by the gas. (b) The temperature of the gas at point A is 185 K. What is its temperature at point B? (c) How much heat has been added to or removed from the gas during the process?
AC
P re
ss ur
e
Volume 0
0
2.0 × 10–3 m3
2.0 × 104 Pa
B
PROBLEM 12
A
P re
ss ur
e
Volume 0
0
2.0 × 10–3 m3
1.0 × 104 Pa
B
C
PROBLEM 13
Problems 429
PROBLEM 28
2.00
0
A B
2.000
Volume, m3
P re
ss ur
e (×
1 0
5 P
a)
4.00
6.00
4.00 6.00 8.00 10.0 12.0
29. M SSM The drawing refers to one mole of a monatomic ideal gas and
shows a process that has four steps, two
isobaric (A to B, C to D) and two iso- choric (B to C, D to A). Complete the following table by calculating ΔU, W, and Q (including the algebraic signs) for each of the four steps.
ΔU W Q
A to B
B to C
C to D
D to A
30. M GO A monatomic ideal gas (γ = 53 ) is contained within a perfectly in- sulated cylinder that is fi tted with a movable piston. The initial pressure of the
gas is 1.50 × 105 Pa. The piston is pushed so as to compress the gas, with the
result that the Kelvin temperature doubles. What is the fi nal pressure of the gas?
31. M The pressure and volume of an ideal monatomic gas change from
A to B to C, as the drawing shows. The curved line between A and C is an isotherm. (a) Determine the total heat for the process and (b) state whether the fl ow of heat is into or
out of the gas.
32. H The work done by one mole of a monatomic ideal gas (γ = 53 ) in expanding adiabatically is 825 J. The
initial temperature and volume of the gas are 393 K and 0.100 m3. Obtain (a) the fi nal temperature and (b) the fi nal volume of the gas. 33. H SSM The drawing shows an adiabat- ically isolated cylinder that is divided initially
into two identical parts by an adiabatic partition.
Both sides contain one mole of a monatomic
ideal gas (γ = 53 ), with the initial temperature being 525 K on the left and 275 K on the right.
The partition is then allowed to move slowly
(i.e., quasi-statically) to the right, until the pres-
sures on each side of the partition are the same.
Find the fi nal temperatures on the (a) left and (b) right.
Section 15.6 Specific Heat Capacities 34. E Argon is a monatomic gas whose atomic mass is 39.9 u. The tempera- ture of eight grams of argon is raised by 75 K under conditions of constant pres-
sure. Assuming that argon behaves as an ideal gas, how much heat is required?
35. E SSM The temperature of 2.5 mol of a monatomic ideal gas is 350 K. The internal energy of this gas is doubled by the addition of heat. How much heat
is needed when it is added at (a) constant volume and (b) constant pressure?
36. E GO Under constant-volume conditions, 3500 J of heat is added to 1.6 moles of an ideal gas. As a result, the temperature of the gas increases
by 75 K. How much heat would be required to cause the same temperature
change under constant-pressure conditions? Do not assume anything about
whether the gas is monatomic, diatomic, etc.
37. E SSM Heat is added to two identical samples of a monatomic ideal gas. In the fi rst sample the heat is added while the volume of the gas is kept
constant, and the heat causes the temperature to rise by 75 K. In the second
sample, an identical amount of heat is added while the pressure (but not the
volume) of the gas is kept constant. By how much does the temperature of
this sample increase?
38. E GO A monatomic ideal gas in a rigid container is heated from 217 K to 279 K by adding 8500 J of heat. How many moles of gas are there in the
container?
39. E Three moles of a monatomic ideal gas are heated at a constant volume of 1.50 m3. The amount of heat added is 5.24 × 103 J. (a) What is the change in the temperature of the gas? (b) Find the change in its internal energy. (c) Determine the change in pressure. 40. M V-HINT A monatomic ideal gas expands at constant pressure. (a) What percentage of the heat being supplied to the gas is used to increase the internal
energy of the gas? (b) What percentage is used for doing the work of expansion? 41. M CHALK Suppose a monatomic ideal gas is contained within a vertical cylinder that is fi tted with a movable piston. The piston is frictionless and has
a negligible mass. The area of the piston is 3.14 × 10−2 m2, and the pressure
outside the cylinder is 1.01 × 105 Pa. Heat (2093 J) is removed from the gas.
Through what distance does the piston drop?
42. M V-HINT A monatomic ideal gas is heated while at a constant volume of 1.00 × 10−3 m3, using a ten-watt heater. The pressure of the gas increases
by 5.0 × 104 Pa. How long was the heater on?
43. H Available in WileyPLUS.
Section 15.8 Heat Engines 44. E Multiple-Concept Example 6 provides a review of the concepts that play roles here. An engine has an effi ciency of 64% and produces 5500 J of
work. Determine (a) the input heat and (b) the rejected heat. 45. E BIO SSM Heat engines take input energy in the form of heat, use some of that energy to do work, and exhaust the remainder. Similarly, a person
can be viewed as a heat engine that takes an input of internal energy, uses
some of it to do work, and gives off the rest as heat. Suppose that a trained
athlete can function as a heat engine with an effi ciency of 0.11. (a) What is the magnitude of the internal energy that the athlete uses in order to do 5.1 ×
104 J of work? (b) Determine the magnitude of the heat the athlete gives off . 46. E GO Engine 1 has an effi ciency of 0.18 and requires 5500 J of input heat to perform a certain amount of work. Engine 2 has an effi ciency of
0.26 and performs the same amount of work. How much input heat does the
second engine require?
47. E Due to a tune-up, the effi ciency of an automobile engine increases by 5.0%. For an input heat of 1300 J, how much more work does the engine
produce after the tune-up than before?
48. M BIO GO A 52-kg mountain climber, starting from rest, climbs a vertical distance of 730 m. At the top, she is again at rest. In the process, her body
generates 4.1 × 106 J of energy via metabolic processes. In fact, her body acts
like a heat engine, the effi ciency of which is given by Equation 15.11 as e = |W|/|QH|, where |W| is the magnitude of the work she does and |QH| is the magnitude of the input heat. Find her effi ciency as a heat engine.
49. M SSM Due to design changes, the effi ciency of an engine increases from 0.23 to 0.42. For the same input heat |QH|, these changes increase the work done by the more effi cient engine and reduce the amount of heat rejec-
ted to the cold reservoir. Find the ratio of the heat rejected to the cold reser-
voir for the improved engine to that for the original engine.
D
0 0 Volume
200.0-K isotherm 400.0-K isotherm
800.0-K isotherm
P re
ss ur
e C
BA
PROBLEM 29
0 0
Volume, m3 0.200
4.00 × 105
0.400
P re
ss ur
e, P
a
A
BC
Isotherm
PROBLEM 31
Partition
525 K 275 K
PROBLEM 33
430 CHAPTER 15 Thermodynamics
50. H Engine A receives three times more input heat, produces fi ve times more work, and rejects two times more heat than engine B. Find the effi ciency
of (a) engine A and (b) engine B.
Section 15.9 Carnot’s Principle and the Carnot Engine 51. E A Carnot engine operates with an effi ciency of 27.0% when the tem- perature of its cold reservoir is 275 K. Assuming that the temperature of the
hot reservoir remains the same, what must be the temperature of the cold
reservoir in order to increase the effi ciency to 32.0%?
52. E An engine has a hot-reservoir temperature of 950 K and a cold- reservoir temperature of 620 K. The engine operates at three-fi fths maximum
effi ciency. What is the effi ciency of the engine?
53. E SSM A Carnot engine has an effi ciency of 0.700, and the temperature of its cold reservoir is 378 K. (a) Determine the temperature of its hot reser- voir. (b) If 5230 J of heat is rejected to the cold reservoir, what amount of heat is put into the engine?
54. E Available in WileyPLUS. 55. E An engine does 18 500 J of work and rejects 6550 J of heat into a cold reservoir whose temperature is 285 K. What would be the smallest possible
temperature of the hot reservoir?
56. E GO A Carnot engine has an effi ciency of 0.40. The Kelvin tempera- ture of its hot reservoir is quadrupled, and the Kelvin temperature of its cold
reservoir is doubled. What is the effi ciency that results from these changes?
57. E MMH A Carnot engine operates between temperatures of 650 and 350 K. To improve the effi ciency of the engine, it is decided either to raise
the temperature of the hot reservoir by 40 K or to lower the temperature of the
cold reservoir by 40 K. Which change gives the greater improvement? Justify
your answer by calculating the effi ciency in each case.
58. M The hot reservoir for a Carnot engine has a temperature of 890 K, while the cold reservoir has a temperature of 670 K. The heat input for this
engine is 4800 J. The 670-K reservoir also serves as the hot reservoir for a
second Carnot engine. This second engine uses the rejected heat of the fi rst
engine as input and extracts additional work from it. The rejected heat from
the second engine goes into a reservoir that has a temperature of 420 K. Find
the total work delivered by the two engines.
59. M SSM Suppose that the gasoline in a car engine burns at 631 °C, while the exhaust temperature (the temperature of the cold reservoir) is 139 °C and
the outdoor temperature is 27 °C. Assume that the engine can be treated as a
Carnot engine (a gross oversimplifi cation). In an attempt to increase mileage
performance, an inventor builds a second engine that functions between the
exhaust and outdoor temperatures and uses the exhaust heat to produce addi-
tional work. Assume that the inventor’s engine can also be treated as a Carnot
engine. Determine the ratio of the total work produced by both engines to that
produced by the fi rst engine alone.
60. M V-HINT A power plant taps steam superheated by geothermal energy to 505 K (the temperature of the hot reservoir) and uses the steam to do
work in turning the turbine of an electric generator. The steam is then con-
verted back into water in a condenser at 323 K (the temperature of the cold
reservoir), after which the water is pumped back down into the earth where
it is heated again. The output power (work per unit time) of the plant is
84 000 kilowatts. Determine (a) the maximum effi ciency at which this plant can operate and (b) the minimum amount of rejected heat that must be removed from the condenser every twenty-four hours.
61. H SSM Available in WileyPLUS. 62. H Available in WileyPLUS.
Section 15.10 Refrigerators, Air Conditioners, and Heat Pumps 63. E SSM A Carnot air conditioner maintains the temperature in a house at 297 K on a day when the temperature outside is 311 K. What is the coeffi cient
of performance of the air conditioner?
64. E GO The inside of a Carnot refrigerator is maintained at a temperature of 277 K, while the temperature in the kitchen is 299 K. Using 2500 J of work,
how much heat can this refrigerator remove from its inside compartment?
65. E A refrigerator operates between temperatures of 296 and 275 K. What would be its maximum coeffi cient of performance?
66. E GO Two Carnot air conditioners, A and B, are removing heat from diff erent rooms. The outside temperature is the same for both rooms, 309.0 K.
The room serviced by unit A is kept at a temperature of 294.0 K, while the
room serviced by unit B is kept at 301.0 K. The heat removed from either
room is 4330 J. For both units, fi nd the magnitude of the work required and
the magnitude of the heat deposited outside.
67. E The water in a deep underground well is used as the cold reservoir of a Carnot heat pump that maintains the temperature of a house at 301 K. To
deposit 14 200 J of heat in the house, the heat pump requires 800 J of work.
Determine the temperature of the well water.
68. E GO A Carnot engine has an effi ciency of 0.55. If this engine were run backward as a heat pump, what would be the coeffi cient of performance?
69. E A Carnot refrigerator is used in a kitchen in which the temperature is kept at 301 K. This refrigerator uses 241 J of work to remove 2561 J of heat
from the food inside. What is the temperature inside the refrigerator?
70. M V-HINT The wattage of a commercial ice maker is 225 W and is the rate at which it does work. The ice maker operates just like a refrigerator or
an air conditioner and has a coeffi cient of performance of 3.60. The water
going into the unit has a temperature of 15.0 °C, and the ice maker produces
ice cubes at 0.0 °C. Ignoring the work needed to keep stored ice from melt-
ing, fi nd the maximum amount (in kg) of ice that the unit can produce in one
day of continuous operation.
71. M SSM Available in WileyPLUS. 72. M MMH Available in WileyPLUS. 73. M SSM A Carnot refrigerator transfers heat from its inside (6.0 °C) to the room air outside (20.0 °C). (a) Find the coeffi cient of performance of the refrigerator. (b) Determine the magnitude of the minimum work needed to cool 5.00 kg of water from 20.0 to 6.0 °C when it is placed in the refrigerator.
74. H Available in WileyPLUS.
Section 15.11 Entropy 75. E Consider three engines that each use 1650 J of heat from a hot reser- voir (temperature = 550 K). These three engines reject heat to a cold reservoir
(temperature = 330 K). Engine I rejects 1120 J of heat. Engine II rejects 990 J
of heat. Engine III rejects 660 J of heat. One of the engines operates reversibly,
and two operate irreversibly. However, of the two irreversible engines, one
violates the second law of thermodynamics and could not exist. For each of
the engines determine the total entropy change of the universe, which is the
sum of the entropy changes of the hot and cold reservoirs. On the basis of your
calculations, identify which engine operates reversibly, which operates irre-
versibly and could exist, and which operates irreversibly and could not exist.
76. E Heat Q fl ows spontaneously from a reservoir at 394 K into a reser- voir at 298 K. Because of the spontaneous fl ow, 2800 J of energy is rendered
unavailable for work when a Carnot engine operates between the reservoir at
298 K and a reservoir at 248 K. Find Q. 77. E SSM Find the change in entropy of the H2O molecules when (a) three kilograms of ice melts into water at 273 K and (b) three kilograms of water changes into steam at 373 K. (c) On the basis of the answers to parts (a) and (b), discuss which change creates more disorder in the collection of H2O molecules.
78. E GO On a cold day, 24 500 J of heat leaks out of a house. The inside temperature is 21 °C, and the outside temperature is −15 °C. What is the
increase in the entropy of the universe that this heat loss produces?
79. M MMH (a) After 6.00 kg of water at 85.0 °C is mixed in a perfect thermos with 3.00 kg of ice at 0.0 °C, the mixture is allowed to reach equilibrium.
When heat is added to or removed from a solid or liquid of mass m and specifi c
Additional Problems 431
heat capacity c, the change in entropy can be shown to be ΔS = mc ln(Tf /Ti), where Ti and Tf are the initial and fi nal Kelvin temperatures. Using this expression and the change in entropy for melting, fi nd the change in entropy
that occurs. (b) Should the entropy of the universe increase or decrease as a result of the mixing process? Give your reasoning and state whether your
answer in part (a) is consistent with your answer here.
80. M V-HINT The sun is a sphere with a radius of 6.96 × 108 m and an aver- age surface temperature of 5800 K. Determine the amount by which the sun’s
thermal radiation increases the entropy of the entire universe each second.
Assume that the sun is a perfect blackbody, and that the average temperature
of the rest of the universe is 2.73 K. Do not consider the thermal radiation
absorbed by the sun from the rest of the universe.
81. M GO An irreversible engine operates between temperatures of 852 and 314 K. It absorbs 1285 J of heat from the hot reservoir and does 264 J of
work. (a) What is the change ΔSuniverse in the entropy of the universe associ- ated with the operation of this engine? (b) If the engine were reversible, what would be the magnitude |W| of the work it would have done, assuming that it operated between the same temperatures and absorbed the same heat as the
irreversible engine? (c) Using the results of parts (a) and (b), fi nd the diff er- ence between the work produced by the reversible and irreversible engines.
82. E The pressure of a monatomic ideal gas (γ = 53 ) doubles during an adiabatic compression. What is the ratio of the fi nal volume to the initial
volume?
83. E SSM One-half mole of a monatomic ideal gas absorbs 1200 J of heat while 2500 J of work is done by the gas. (a) What is the temperature change of the gas? (b) Is the change an increase or a decrease? 84. E Available in WileyPLUS. 85. E A gas, while expanding under isobaric conditions, does 480 J of work. The pressure of the gas is 1.6 × 105 Pa, and its initial volume is 1.5 ×
10−3 m3. What is the fi nal volume of the gas?
86. E V-HINT A lawnmower engine with an effi ciency of 0.22 rejects 9900 J of heat every second. What is the magnitude of the work that the engine does
in one second?
87. E SSM A process occurs in which the entropy of a system increases by 125 J/K. During the process, the energy that becomes unavailable for doing
work is zero. (a) Is this process reversible or irreversible? Give your reason- ing. (b) Determine the change in the entropy of the surroundings. 88. E A Carnot heat pump operates between an outdoor temperature of 265 K and an indoor temperature of 298 K. Find its coeffi cient of performance.
89. E The temperatures indoors and outdoors are 299 and 312 K, respect- ively. A Carnot air conditioner deposits 6.12 × 105 J of heat outdoors. How
much heat is removed from the house?
90. E GO Carnot engine A has an effi ciency of 0.60, and Carnot engine B has an effi ciency of 0.80. Both engines utilize the same hot reservoir, which
has a temperature of 650 K and delivers 1200 J of heat to each engine. Find
the magnitude of the work produced by each engine and the temperatures of
the cold reservoirs that they use.
91. E SSM The pressure and volume of a gas are changed along the path ABCA. Using the data shown in the graph, determine the work done (includ- ing the algebraic sign) in each segment of the path: (a) A to B, (b) B to C, and (c) C to A.
PROBLEM 91
3.0 × 105 A
B C
2.0 × 10–3
Volume, m3
P re
ss ur
e, P
a
5.0 × 10–3
7.0 × 105
92. M Available in WileyPLUS. 93. M SSM Available in WileyPLUS. 94. M V-HINT Available in WileyPLUS. 95. M BIO Available in WileyPLUS. 96. M V-HINT Available in WileyPLUS. 97. M MMH Available in WileyPLUS. 98. M GO An ideal gas is taken through the three processes (A → B, B → C, and C → A) shown in the drawing. In general, for each process the internal
energy U of the gas can change because heat Q can be added to or removed from the gas and work W can be done by the gas or on the gas. For the three processes shown in the drawing, fi ll in the fi ve missing entries in the follow-
ing table.
PROBLEM 98
P re
ss ur
e
Volume
CB
A
Process ΔU Q W
A → B (b) +561 J (a)
B → C +4303 J (c) +3740 J
C → A (d) (e) −2867 J
99. H SSM An engine has an efficiency e1. The engine takes input heat of magnitude |QH| from a hot reservoir and delivers work of magnitude |W1|. The heat rejected by this engine is used as input heat for a second engine, which has an efficiency e2 and delivers work of magnitude |W2|. The overall efficiency of this two-engine device is the magnitude of the
total work delivered (|W1| + |W2|) divided by the magnitude |QH| of the input heat. Find an expression for the overall efficiency e in terms of e1 and e2.
100. H Available in WileyPLUS. 101. M GO SSM An ideal, or Carnot, heat pump is used to heat a house to a temperature of 294 K (21 °C). How much work must the pump do to
deliver 3350 J of the heat into the house on a day when the outdoor tempera-
ture is 273 K (0 °C), and on another day when the temperature is 252 K
(−21 °C)?
Additional Problems
432 CHAPTER 15 Thermodynamics
The fi rst law of thermodynamics is basically a restatement of the conservation-
of-energy principle in terms of heat and work. Problem 102 emphasizes this
fact by showing that the conservation principle and the fi rst law provide the
same approach to the problem. It also provides a review of the concept of
the latent heat of sublimation and the ideal gas law. Problem 103 reviews
some of the central features of heat engines, as well as kinetic energy and the
work–energy theorem.
102. M CHALK The sublimation of zinc (mass per mole = 0.0654 kg/mol) takes place at a temperature of 6.00 × 102 K, and the latent heat of sublima-
tion is 1.99 × 106 J/kg. The pressure remains constant during the sublimation.
Assume that the zinc vapor can be treated as a monatomic ideal gas and that
the volume of solid zinc is negligible compared to the corresponding vapor.
Concepts: (i) What is sublimation, and what is the latent heat of sublimation? (ii) When a solid phase changes to a gas phase, does the volume of the ma- terial increase or decrease, and by how much? (iii) As the material changes
from a solid to a gas, does it do work on the environment, or does the envir-
onment do work on it? How much work is involved? (iv) In this problem we
begin with heat Q and realize that it is used for two purposes: First, it makes the solid change into a gas, which entails a change ΔU in the internal energy of the material, ΔU = Ugas − Usolid. Second, it allows the expanding material to do work W on the environment. According to the conservation-of-energy principle, how is Q related to ΔU and W? (v) According to the fi rst law of thermodynamics, how is Q related to ΔU and W? Calculations: What is the change in the internal energy of zinc when 1.50 kg of zinc sublimates?
103 M CHALK SSM Each of two Carnot engines uses the same cold reservoir at a temperature of 275 K for its exhaust heat. Each engine receives 1450 J
of input heat. The work from either of these engines is used to drive a pulley
arrangement that uses a rope to accelerate a 125-kg crate from rest along a
horizontal frictionless surface, as shown in the fi gure. With engine 1 the crate
attains a speed of 2.00 m/s, while with engine 2 it attains a speed of 3.00 m/s.
Concepts: (i) With which engine is the change in the crate’s energy greater? (ii) Which engine does more work? Explain your answer. (iii) For which
engine is the temperature of the hot reservoir greater? Calculations: Find the temperature of the hot reservoir for each engine.
PROBLEM 103
Cold reservoir
Engine
�QC�
�W �
�QH�
Temperature = TH
Hot reservoir
Temperature = TC
Concepts and Calculations Problems
104. M A High-Performance Engine. You and your team are tasked with evaluating the parameters of a high-performance engine. The engine com-
presses the fuel-air mixture in the cylinder to make it ignite rather than ignit-
ing it with a spark plug (this is how diesel engines operate). You are given
the compression ratio for the cylinders in the engine, which is the ratio of the initial volume of the cylinder (before the piston compresses the gas) to
the fi nal volume of the cylinder (after the gas is compressed): Vi:Vf. Assume that the fuel-gas mixture enters the cylinder at a temperature of 22.0 °C,
and that the gas behaves like an ideal gas with γ = 7/5. (a) If the compres- sion ratio is 15.4:1, what is the fi nal temperature of the gas if the compres-
sion is adiabatic? (b) With everything else the same as in (a), what is the fi nal temperature of the gas if the compression ratio is increased to 17.0:1?
(c) Everything else being the same, for which compression ratio do you think the engine runs more effi ciently? Give a qualitative argument for your answer.
105. M A Gas Lift. A monatomic gas is contained in a long, vertical cylin- der of inner radius r = 14.0 cm. A movable piston of negligible mass is inser- ted in the cylinder at a height h = 1.20 m. Initially, the gas inside the piston is at ambient temperature (23.5 °C) and standard pressure (1 atm). You place a
250.0 kg mass on the top of the piston and allow it to isothermally compress
the gas below it. (a) What is the fi nal pressure of the gas? (b) How far is the piston displaced from the equilibrium position? (c) Assuming an isobaric expansion, to what temperature should the gas inside the cylinder be heated
in order to lift the mass 15.0 cm above the original position of the cylinder
(i.e., to a height of 1.35 m)?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
16.1 Distinguish between transverse and longitudinal waves.
16.2 Calculate speed, frequency, and wavelength for a wave.
16.3 Calculate the speed of a wave on a string.
16.4 Use wave functions to describe a wave.
16.5 Examine sound waves.
16.6 Calculate the speed of a sound wave.
16.7 Analyze sound intensity.
16.8 Calculate sound intensity level.
16.9 Solve Doppler eff ect problems.
16.10 Describe applications of sound in medicine.
16.11 Examine the sensitivity of the human ear using Fletcher–Munson curves.
En si
gn J
oh n
G ay
/© A
P/ W
id e
W or
ld P
ho to
s
CHAPTER 16
Waves and Sound
In this chapter we will see that sound is a longitudinal wave of pressure fl uctuations and travels through air at a speed of 343 m/s when the temperature is 20 °C. Sound is produced by a vibrating object, such as the surfaces of an airplane in fl ight. When an airplane approaches and then exceeds the speed of sound, it is said to break through the sound barrier. The so-called “barrier” is formed due to sound waves previously emitted by the plane at speeds less than the speed of sound. Here, an F/A-18 Hornet fi ghter jet emerges from a cloud caused when it breaks through the sound barrier.
16.1 The Nature of Waves There are two features common to all waves:
1. A wave is a traveling disturbance. 2. A wave carries energy from place to place.
Consider a water wave, for instance. In Figure 16.1 the wave created by the motor- boat travels across the lake and disturbs the fi sherman. However, there is no bulk fl ow of water outward from the motorboat. The wave is not a bulk movement of water such as a river, but, rather, a disturbance traveling on the surface of the lake. Part of the wave’s energy in Figure 16.1 is transferred to the fi sherman and his boat.
We will consider two basic types of waves, transverse and longitudinal. Interactive Figure 16.2 (see next page) illustrates how a transverse wave can be generated using a Slinky, a remarkable toy in the form of a long, loosely coiled spring. If one end of the Slinky is jerked up and down, as in part a, an upward pulse is sent traveling toward the right. If the end is then jerked down and up, as in part b, a downward pulse is generated and also moves to the right. If the end is continually moved up and down in simple harmonic motion, an entire wave is produced. As part c illustrates, the wave consists of a series of alternating upward and downward sections that propagate to the right, disturbing the vertical position of the Slinky in the process. To focus attention on the disturbance, a colored dot is attached to the Slinky in part c of the drawing. As 433
434 CHAPTER 16 Waves and Sound
the wave advances, the dot is displaced up and down in simple harmonic motion. The motion of the dot occurs perpendicular, or transverse, to the direction in which the wave travels. Thus, a transverse wave is one in which the disturbance occurs perpendicular to the direction of travel of the wave. Radio waves, light waves, and microwaves are transverse waves. Transverse waves also travel on the strings of instruments such as guitars and banjos.
A longitudinal wave can also be generated with a Slinky, and Interactive Figure 16.3 demon- strates how. When one end is pushed forward along its length (i.e., longitudinally) and then pulled back to its starting point, as in part a, a region where the coils are compressed together is sent trave- ling to the right. If the end is pulled backward and then pushed forward to its starting point, as in part b, a region where the coils are stretched apart is formed and also moves to the right. If the end is continually moved back and forth in simple harmonic motion, an entire wave is created. As part c shows, the wave consists of a series of alternating compressed and stretched regions that travel to the right and disturb the coils. A colored dot is once again attached to the Slinky to emphasize the vibratory nature of the disturbance. In response to the wave, the dot moves back and forth in simple harmonic motion along the line of travel of the wave. Thus, a longitudinal wave is one in which the disturbance occurs parallel to the line of travel of the wave. A sound wave is a longitudinal wave.
A water wave is neither transverse nor longitudinal, since the motion of the water particles is not strictly perpendicular or strictly parallel to the line along which the wave travels. Instead, the motion includes both transverse and longitudinal components, since the water particles at the surface move on nearly circular paths, as Figure 16.4 indicates.
FIGURE 16.1 The wave created by the motorboat travels across the lake and disturbs the fi sherman.
(a)
(b)
(c)
INTERACTIVE FIGURE 16.2 (a) An upward pulse moves to the right, followed by (b) a downward pulse. (c) When the end of the Slinky is moved up and down continuously, a transverse wave is produced.
Compressed region
Compressed region
(a)
Stretched region
(b)
(c)
INTERACTIVE FIGURE 16.3 (a) A compressed region moves to the right, followed by (b) a stretched region. (c) When the end of the Slinky is moved back and forth continuously, a longitudinal wave is produced.
Direction of wave travel
Water particle moves on
circular path
Transverse component
Longitudinal component
FIGURE 16.4 A water wave is neither trans- verse nor longitudinal, since water particles at the surface move clockwise on nearly circular paths as the wave moves from left to right.
16.2 Periodic Waves 435
Check Your Understanding
(The answers are given at the end of the book.) 1. Considering the nature of a water wave (see Figure 16.4), which of the following statements correctly
describes how a fi shing fl oat moves on the surface of a lake when a wave passes beneath it? (a) It bobs up and down vertically. (b) It moves back and forth horizontally. (c) It moves in a vertical plane, exhibiting both motions described in (a) and (b) simultaneously.
2. Suppose that the longitudinal wave in Interactive Figure 16.3c moves to the right at a speed of 1 m/s. Does one coil of the Slinky move a distance of 1 mm to the right in a time of 1 ms?
16.2 Periodic Waves The transverse and longitudinal waves that we have been discussing are called periodic waves because they consist of cycles or patterns that are produced over and over again by the source. In Figures 16.2 and 16.3 the repetitive patterns occur as a result of the simple harmonic motion of the left end of the Slinky, so that every segment of the Slinky vibrates in simple harmonic motion. Sections 10.1 and 10.2 discuss the simple harmonic motion of an object on a spring and introduce the concepts of cycle, amplitude, period, and frequency. This same terminology is used to describe periodic waves, such as the sound waves we hear (discussed later in this chapter) and the light waves we see (discussed in Chapter 24).
Figure 16.5 uses a graphical representation of a transverse wave on a Slinky to review the terminology. One cycle of a wave is shaded in color in both parts of the drawing. A wave is a series of many cycles. In part a the vertical position of the Slinky is plotted on the vertical axis, and the corresponding distance along the length of the Slinky is plotted on the horizontal axis. Such a graph is equivalent to a photograph of the wave taken at one instant in time and shows the disturbance that exists at each point along the Slinky’s length. As marked on this graph, the amplitude A is the maximum excursion of a particle of the medium (i.e., the Slinky) in which the wave exists from the particle’s undisturbed position. The amplitude is the distance between a crest, or highest point on the wave pattern, and the undisturbed position; it is also the distance between a trough, or lowest point on the wave pattern, and the undisturbed position. The wave- length 𝜆 is the horizontal length of one cycle of the wave, as shown in Figure 16.5a. The wave- length is also the horizontal distance between two successive crests, two successive troughs, or any two successive equivalent points on the wave.
Part b of Figure 16.5 shows a graph in which time, rather than distance, is plotted on the horizontal axis. This graph is obtained by observing a single point on the Slinky. As the wave passes, the point under observation oscillates up and down in simple harmonic motion. As indi- cated on the graph, the period T is the time required for one complete up/down cycle, just as it is for an object vibrating on a spring. The period T is related to the frequency f, just as it is for any example of simple harmonic motion:
f = 1 T
(10.5)
Vertical position of the Slinky
Undisturbed position
(a) At a particular time
Distance
Wavelength = λ
A
A
Vertical position of one
point on the
Slinky
(b) At a particular location
Time
Period = T
A
A
FIGURE 16.5 One cycle of the wave is shaded in color, and the amplitude of the wave is denoted as A.
436 CHAPTER 16 Waves and Sound
The period is commonly measured in seconds, and frequency is measured in cycles per sec- ond, or hertz (Hz). If, for instance, one cycle of a wave takes one-tenth of a second to pass an observer, then ten cycles pass the observer per second, as Equation 10.5 indicates [f = 1/(0.1 s) = 10 cycles/s = 10 Hz].
A simple relation exists between the period, the wavelength, and the speed of any periodic wave, a relation that Figure 16.6 helps to introduce. Imagine waiting at a railroad crossing, while a freight train moves by at a constant speed 𝜐. The train consists of a long line of identical box- cars, each of which has a length 𝜆 and requires a time T to pass, so the speed is 𝜐 = 𝜆/T. This same equation applies for a wave and relates the speed of the wave to the wavelength 𝜆 and the period T. Since the frequency of a wave is f = 1/T, the expression for the speed is
υ = λ T
= f λ (16.1)
The terminology just discussed and the fundamental relations f = 1/T and 𝜐 = f𝜆 apply to longi- tudinal as well as to transverse waves. Example 1 shows how the wavelength of a wave is deter- mined by the wave speed and the frequency established by the source.
Velocity = v
The time for one car to pass is the period T
Wavelength = λ
FIGURE 16.6 A train moving at a constant speed serves as an analogy for a traveling wave.
EXAMPLE 1 The Wavelengths of Radio Waves
AM and FM radio waves are transverse waves consisting of electric and magnetic disturbances traveling at a speed of 3.00 × 108 m/s. A station broadcasts an AM radio wave whose frequency is 1230 × 103 Hz (1230 kHz on the dial) and an FM radio wave whose frequency is 91.9 × 106 Hz (91.9 MHz on the dial). Find the distance between adjacent crests in each wave.
Reasoning The distance between adjacent crests is the wavelength 𝜆. Since the speed of each wave is 𝜐 = 3.00 × 108 m/s and the frequencies are known, the relation 𝜐 = f𝜆 can be used to determine the wavelengths.
Problem-Solving Insight The equation 𝝊 = f𝝀 applies to any kind of periodic wave.
Solution
AM λ = υ f
= 3.00 × 10 8 m /s 1230 × 10 3 Hz
= 244 m
FM λ = υ f
= 3.00 × 10 8 m /s 91.9 × 10 6 Hz
= 3.26 m
Notice that the wavelength of an AM radio wave is longer than two and one-half football fi elds!
Check Your Understanding
(The answer is given at the end of the book.) 3. A sound wave (a periodic longitudinal wave) from a loudspeaker travels from air into water. The
frequency of the wave does not change, because the loudspeaker producing the sound determines the frequency. The speed of sound in air is 343 m/s, whereas the speed in fresh water is 1482 m/s. When the sound wave enters the water, does its wavelength increase, decrease, or remain the same?
16.3 The Speed of a Wave on a String The properties of the material* or medium through which a wave travels determine the speed of the wave. For example, Figure 16.7 shows a transverse wave on a string and draws attention to four string particles that have been drawn as colored dots. As the wave moves to the right, each particle is displaced, one after the other, from its undisturbed position. In the drawing, particles 1 and 2 have already been displaced upward, while particles 3 and 4 are not yet aff ected by the wave. Particle 3 will be next to move because the section of string immediately to its left (i.e., particle 2) will pull it upward.
*Electromagnetic waves (discussed in Chapter 24) can move through a vacuum, as well as through materials such as glass and water.
16.3 The Speed of a Wave on a String 437
Figure 16.7 leads us to conclude that the speed with which the wave moves to the right depends on how quickly one particle of the string is accelerated upward in response to the net pulling force exerted by its adjacent neighbors. In accord with Newton’s second law, a stronger net force results in a greater acceleration, and, thus, a faster-moving wave. The ability of one par- ticle to pull on its neighbors depends on how tightly the string is stretched—that is, on the tension (see Section 4.10 for a review of tension). The greater the tension, the greater the pulling force the particles exert on each other and the faster the wave travels, other things being equal. Along with the tension, a second factor infl uences the wave speed. According to Newton’s second law, the inertia or mass of particle 3 in Figure 16.7 also aff ects how quickly it responds to the upward pull of particle 2. For a given net pulling force, a smaller mass has a greater acceleration than a larger mass. Therefore, other things being equal, a wave travels faster on a string whose particles have a small mass, or, as it turns out, on a string that has a small mass per unit length. The mass per unit length is called the linear density of the string. It is the mass m of the string divided by its length L, or m/L. Eff ects of the tension F and the mass per unit length are evident in the following expression for the speed 𝜐 of a small-amplitude wave on a string:
υ = √ Fm /L (16.2) The motion of transverse waves along a string is important in the operation of musical instru-
ments, such as the guitar, the violin, and the piano. In these instruments, the strings are either plucked, bowed, or struck to produce transverse waves. Example 2 discusses the speed of the waves on the strings of a guitar.
1
2
3 4
υ
FIGURE 16.7 As a transverse wave moves to the right with speed υ, each string particle is displaced, one after the other, from its undisturbed position.
EXAMPLE 2 The Physics of Waves on Guitar Strings
Transverse waves travel on each string of an electric guitar after the string is plucked (see Figure 16.8). The length of each string between its two fi xed ends is 0.628 m, and the mass is 0.208 g for the highest pitched E string and 3.32 g for the lowest pitched E string. Each string is under a tension of 226 N. Find the speeds of the waves on the two strings.
Reasoning The speed of a wave on a guitar string, as expressed by Equation 16.2, depends on the tension F in the string and its linear density m/L. Since the tension is the same for both strings, and smaller linear densities give rise to greater speeds, we expect the wave speed to be great- est on the string with the smallest linear density.
Solution The speeds of the waves are given by Equation 16.2 as
υ = √ Fm /L = √ 226 N
(0.208 × 10−3 kg)/(0.628 m) = 826 m/s
υ = √ Fm /L = √ 226 N
(3.32 × 10−3 kg)/(0.628 m) = 207 m/s
High- pitched E
Low- pitched E
Notice how fast the waves move: the speeds correspond to 1850 and 463 mi/h.
Transverse vibration
of the string
FIGURE 16.8 Plucking a guitar string generates transverse waves.
Conceptual Example 3 off ers additional insight into the nature of a wave as a traveling disturbance.
438 CHAPTER 16 Waves and Sound
Check Your Understanding
(The answers are given at the end of the book.) 4. One end of each of two identical strings is attached to a wall. Each string is being pulled equally tight
by someone at the other end. A transverse pulse is sent traveling along string A. A bit later an identical pulse is sent traveling along string B. What, if anything, can be done to make the pulse on string B catch up with and pass the pulse on string A?
5. In Section 4.10 the concept of a massless rope is discussed. Considering Equation 16.2, would it take any time for a transverse wave to travel the length of a truly massless rope?
6. A wire is strung tightly between two immovable posts. Review Section 12.4 and decide whether the speed of a transverse wave on this wire would increase, decrease, or remain the same when the tem- perature increases. Ignore any change in the mass per unit length of the wire.
7. Examine Conceptual Example 3 before addressing this question. A wave moves on a string with a constant velocity. Does this mean that the particles of the string always have zero acceleration?
8. A rope of mass m is hanging down from the ceiling. Nothing is attached to the loose end of the rope. As a transverse wave travels upward on the rope, does the speed of the wave increase, decrease, or remain the same?
9. String I and string II have the same length. However, the mass of string I is twice the mass of string II, and the tension in string I is eight times the tension in string II. A wave of the same amplitude and frequency travels on each of these strings. Which of the drawings in CYU Figure 16.1 correctly shows the waves: (a) A (b) B (c) C?
A
I
II
B
I
II
C
I
II
CYU FIGURE 16.1
CONCEPTUAL EXAMPLE 3 Wave Speed Versus Particle Speed
As indicated in Figure 16.9, the speed of a transverse wave on a string is 𝜐wave, and the speed at which a string particle moves is 𝜐particle. Which of the following statements is correct? (a) The speeds 𝜐wave and 𝜐particle are identical. (b) The speeds 𝜐wave and 𝜐particle are diff erent.
Reasoning A wave moves on a string at a speed 𝜐wave that is determined by the properties of the string and has a constant value everywhere on the string at all times, assuming that these properties are the same every- where on the string. Each particle on the string, however, moves in simple harmonic motion, assuming that the source generating the wave (e.g., the hand in Interactive Figure 16.2c) moves in simple harmonic motion. Each particle has a speed 𝜐particle that is characteristic of simple harmonic motion.
Answer (a) is incorrect. The speed 𝜐wave has a constant value at all times. In contrast, 𝜐particle is not constant at all times, because it is the speed that characterizes simple harmonic motion and that speed varies as time passes. Thus, the two speeds are not identical.
Answer (b) is correct. The speed 𝜐wave is determined by the tension F and
the mass per unit length m/L of the string, according to υwave = √ Fm /L (see Equation 16.2). The speed 𝜐particle is characteristic of simple harmonic motion, according to 𝜐particle = A𝜔 sin 𝜔t (Equation 10.7 without the minus sign, since we deal here only with speed, which is the magnitude of the velocity). The particle speed depends on the amplitude A and the angular
frequency 𝜔 of the simple harmonic motion, as well as the time t; the speed is greatest when the particle is passing through the undisturbed position of the string, and it is zero when the particle has its maximum displacement. Thus, the two speeds are diff erent, because 𝜐wave depends on the properties of the string and 𝜐particle depends on the properties of the source creating the wave.
Related Homework: Problem 20
String particle particle
wave
Undisturbed position of string
υ
υ
FIGURE 16.9 A transverse wave on a string is moving to the right with a constant speed υwave. A string particle moves up and down in simple harmonic motion about the undisturbed position of the string. A string particle moves with a speed υparticle.
16.5 The Nature of Sound 439
16.4 *The Mathematical Description of a Wave When a wave travels through a medium, it displaces the particles of the medium from their undis- turbed positions. Suppose that a particle is located at a distance x from a coordinate origin. We would like to know the displacement y of this particle from its undisturbed position at any time t as the wave passes. For periodic waves that result from simple harmonic motion of the source, the expression for the displacement involves a sine or cosine, a fact that is not surprising. After all, in Chapter 10 simple harmonic motion is described using sinusoidal equations, and the graphs for a wave in Figure 16.5 look like a plot of displacement versus time for an object oscillating on a spring (see Figure 10.5).
Our approach will be to present the expression for the displacement and then show graphically that it gives a correct description. Equation 16.3 represents the displacement of a particle caused by a wave traveling in the +x direction (to the right), with an amplitude A, frequency f, and wavelength 𝜆. Equation 16.4 applies to a wave moving in the −x direction (to the left).
Wave motion toward +x y = A sin (2π ft − 2πxλ ) (16.3)
Wave motion toward −x y = A sin (2π ft + 2πxλ ) (16.4) These equations apply to transverse or longitudinal waves and assume that y = 0 m when x = 0 m and t = 0 s. The term (2𝜋ft − 2𝜋x/𝜆) in Equation 16.3 or the term (2𝜋ft + 2𝜋x/𝜆) in Equation 16.4 is called the phase angle of the wave. In either case the phase angle is measured in radians, not in degrees.
Consider a transverse wave moving in the +x direction along a string. A string particle located at the origin (x = 0 m) exhibits simple harmonic motion with a phase angle of 2𝜋ft; that is, its displacement as a function of time is y = A sin (2𝜋ft). A particle located at a distance x also exhibits simple harmonic motion, but its phase angle in Equation 16.3 is
2π ft − 2πx
λ = 2π f (t − xf λ) = 2π f (t −
x υ)
The quantity x/𝜐 is the time needed for the wave to travel the distance x. In other words, the simple harmonic motion that occurs at x is delayed by the time interval x/𝜐 compared to the motion at the origin.
Figure 16.10 shows the displacement y plotted as a function of position x along the string at a series of time intervals separated by one-fourth of the period T (t = 0 s, 14 T,
2 4 T,
3 4 T, T ). These
graphs are constructed by substituting the corresponding value for t into Equation 16.3, remem- bering that f = 1/T, and then calculating y at a series of values for x. The graphs are like photo- graphs taken at various times as the wave moves to the right. For reference, the colored square on each graph marks the place on the wave that is located at x = 0 m when t = 0 s. As time passes, the colored square moves to the right, along with the wave. In a similar manner, it can be shown that Equation 16.4 represents a wave moving in the −x direction.
16.5 The Nature of Sound Longitudinal Sound Waves Sound is a longitudinal wave that is created by a vibrating object, such as a guitar string, the human vocal cords, or the diaphragm of a loudspeaker. Moreover, sound can be created or trans- mitted only in a medium, such as a gas, liquid, or solid. As we will see, the particles of the medium must be present for the disturbance of the wave to move from place to place. Sound cannot exist in a vacuum.
THE PHYSICS OF . . . a loudspeaker diaphragm. To see how sound waves are produced and why they are longitudinal, consider the vibrating diaphragm of a loudspeaker.
y
+x
t = 0 s
t = T1–4
t = T2–4
t = T3–4
t = T
FIGURE 16.10 Equation 16.3 is plotted here at a series of times separated by one-fourth of the period T. The colored square in each graph marks the place on the wave that is located at x = 0 m when t = 0 s. As time passes, the wave moves to the right.
Math Skills Since the phase angles in Equation 16.3 and Equation 16.4 are measured in radians, a calculator must be set to its radian mode when it is used to evaluate the functions sin(2𝝅ft − 2𝝅x/𝝀) or sin(2𝝅ft + 2𝝅x/𝝀). Suppose, for instance, that 2𝝅ft − 2𝝅x/𝝀 = 0.500 radians, which corresponds to 28.6°. If your calculator is set to its radian mode when you evaluate sin 0.500, the cor- rect value of 0.479 is displayed. How- ever, with the calculator set to its degree mode, an incorrect value of 0.00873 is shown.
440 CHAPTER 16 Waves and Sound
INTERACTIVE FIGURE 16.11 (a) When the speaker diaphragm moves outward, it creates a condensation. (b) When the diaphragm moves inward, it creates a rarefaction. The condensation and rarefaction on the Slinky are included for comparison. In reality, the velocity of the wave on the Slinky v→Slinky is much smaller than the velocity of sound in air v→. For simplicity, the two waves are shown here to have the same velocity.
vSlinky
Condensation Normal air pressure
v
(a)
vSlinky
Rarefaction
v
Condensation
(b)
Normal air pressure
v
vSlinky
Wavelength = λ
FIGURE 16.12 Both the wave on the Slinky and the sound wave are longitudinal. The colored dots attached to the Slinky and to an air molecule vibrate back and forth parallel to the line of travel of the wave.
When the diaphragm moves outward, it compresses the air directly in front of it, as in Interactive Figure 16.11a. This compression causes the air pressure to rise slightly. The region of increased pressure is called a condensation, and it travels away from the speaker at the speed of sound. The condensation is analogous to the compressed region of coils in a longitudinal wave on a Slinky, which is included in Interactive Figure 16.11a for comparison. After producing a con- densation, the diaphragm reverses its motion and moves inward, as in part b of the drawing. The inward motion produces a region known as a rarefaction, where the air pressure is slightly less than normal. The rarefaction is similar to the stretched region of coils in a longitudinal Slinky wave. Following immediately behind the condensation, the rarefaction also travels away from the speaker at the speed of sound. Figure 16.12 further emphasizes the similarity between a sound wave and a longitudinal Slinky wave. As the wave passes, the colored dots attached both to the Slinky and to an air molecule execute simple harmonic motion about their undisturbed positions. The colored arrows on either side of the dots indicate that the simple harmonic motion occurs parallel to the line of travel. The drawing also shows that the wavelength 𝜆 is the distance between the centers of two successive condensations; 𝜆 is also the distance between the centers of two successive rarefactions.
Figure 16.13 illustrates a sound wave spreading out in space after being produced by a loudspeaker. When the condensations and rarefactions arrive at the ear, they force the eardrum to vibrate at the same frequency as the speaker diaphragm. The vibratory motion of the eardrum is interpreted by the brain as sound. It should be emphasized that sound is not a mass movement of air, like the wind. As the condensations and rarefactions of the sound wave travel outward from the vibrating diaphragm in Figure 16.13, the individual air molecules are not carried along with the wave. Rather, each molecule executes simple harmonic motion about a fi xed location. In doing so, one molecule collides with its neighbor and passes the condensations and rarefactions forward. The neighbor, in turn, repeats the process.
The Frequency of a Sound Wave Each cycle of a sound wave includes one condensation and one rarefaction, and the frequency is the number of cycles per second that passes by a given location. For example, if the diaphragm of a speaker vibrates back and forth in simple harmonic motion at a frequency of 1000 Hz, then 1000 condensations, each followed by a rarefaction, are generated every second, thus forming a sound wave whose frequency is also 1000 Hz. A sound with a single frequency is called a pure tone. Experiments have shown that a healthy young person hears all sound fre- quencies from approximately 20 to 20 000 Hz (20 kHz). The ability to hear the high frequen- cies decreases with age, however, and a normal middle-aged adult hears frequencies only up to 12–14 kHz.
THE PHYSICS OF . . . a touch-tone telephone. Pure tones are used in touch-tone telephones, such as the one shown in Figure 16.14. These phones simultaneously produce two
Vibration of an individual
air molecule
FIGURE 16.13 Condensations and rarefac- tions travel from the speaker to the listener, but the individual air molecules do not move with the wave. A given molecule vibrates back and forth about a fi xed location.
1209 Hz
1336 Hz
1477 Hz
770 Hz
852 Hz
941 Hz
697 Hz
For each row
For each
column
FIGURE 16.14 A touch-tone telephone and a schematic showing the two pure tones produced when each button is pressed.
16.5 The Nature of Sound 441
pure tones when each button is pressed, a diff erent pair of tones for each diff erent button. The tones are transmitted electronically to the central telephone offi ce, where they activate switching circuits that complete the call. For example, the drawing indicates that pressing the “5” button produces pure tones of 770 and 1336 Hz simultaneously. These frequencies are characteristic of the second row and second column of buttons, respectively. Similarly, the “9” button generates tones of 852 and 1477 Hz.
Sound can be generated whose frequency lies below 20 Hz or above 20 kHz, although humans normally do not hear it. Sound waves with frequencies below 20 Hz are said to be infra- sonic, while those with frequencies above 20 kHz are referred to as ultrasonic. Some species of bats known as microbats use ultrasonic frequencies up to 120 kHz for locating prey and for navigating (Figure 16.15), while rhinoceroses use infrasonic frequencies as low as 5 Hz to call one another (Figure 16.16).
Frequency is an objective property of a sound wave because frequency can be measured with an electronic frequency counter. A listener’s perception of frequency, however, is subjec- tive. The brain interprets the frequency detected by the ear primarily in terms of the subjective quality called pitch. A pure tone with a large (high) frequency is interpreted as a high-pitched sound, while a pure tone with a small (low) frequency is interpreted as a low-pitched sound. For instance, a piccolo produces high-pitched sounds, and a tuba produces low-pitched sounds.
The Pressure Amplitude of a Sound Wave Figure 16.17 illustrates a pure-tone sound wave traveling in a tube. Attached to the tube is a series of gauges that indicate the pressure variations along the wave. The graph shows that the
M er
lin D
. T ut
tle /S
ci en
ce S
ou rc
e
FIGURE 16.15 Some bats use ultrasonic sound waves for locating prey and for navigating. This bat has captured a katydid.
A da
m J
on es
/G et
ty Im
ag es
FIGURE 16.16 Rhinoceroses call to one another using infrasonic sound waves.
Lo
A ir
p re
ss ur
e
High
Distance
Atmospheric pressure
RarefactionLow
Condensation
Amplitude
Hi Lo Hi
FIGURE 16.17 A sound wave is a series of alternating condensations and rarefactions. The graph shows that the condensations are regions of higher than normal air pressure, and the rarefactions are regions of lower than normal air pressure.
442 CHAPTER 16 Waves and Sound
air pressure varies sinusoidally along the length of the tube. Although this graph has the appear- ance of a transverse wave, remember that the sound itself is a longitudinal wave. The graph also shows the pressure amplitude of the wave, which is the magnitude of the maximum change in pressure, measured relative to the undisturbed or atmospheric pressure. The pressure fl uctua- tions in a sound wave are normally very small. For instance, in a typical conversation between two people the pressure amplitude is about 3 × 10−2 Pa, certainly a small amount compared with the atmospheric pressure of 1.01 × 10+5 Pa. The ear is remarkable in being able to detect such small changes.
Loudness is an attribute of sound that depends primarily on the amplitude of the wave: the larger the amplitude, the louder the sound. The pressure amplitude is an objective property of a sound wave, since it can be measured. Loudness, on the other hand, is subjective. Each individual determines what is loud, depending on the acuteness of his or her hearing.
Check Your Understanding
(The answer is given at the end of the book.) 10. In a traveling sound wave, are there any particles that are always at rest as the wave passes by?
16.6 The Speed of Sound Gases Sound travels through gases, liquids, and solids at considerably diff erent speeds, as Table 16.1 reveals. Near room temperature, the speed of sound in air is 343 m/s (767 mi/h) and is markedly greater in liquids and solids. For example, sound travels more than four times faster in water and more than seventeen times faster in steel than it does in air. In general, sound travels slowest in gases, faster in liquids, and fastest in solids.
Like the speed of a wave on a guitar string, the speed of sound depends on the properties of the medium. In a gas, it is only when molecules collide that the condensations and rarefactions of a sound wave can move from place to place. It is reasonable, then, to expect the speed of sound in a gas to have the same order of magnitude as the average molecular speed between collisions. For an ideal gas this average speed is the translational rms speed given by Equation 14.6: 𝜐rms = √3kT /m, where T is the Kelvin temperature, m is the mass of a molecule, and k is Boltzmann’s constant. Although the expression for 𝜐rms overestimates the speed of sound, it does give the cor- rect dependence on Kelvin temperature and particle mass. Careful analysis shows that the speed of sound in an ideal gas is given by
Ideal gas υ = √γkTm (16.5) where 𝛾 = cP/cV is the ratio of the specifi c heat capacity at constant pressure cP to the specifi c heat capacity at constant volume cV.
The factor 𝛾 is introduced in Section 15.5, where the adiabatic compression and expansion of an ideal gas are discussed. In Section 15.6 it is shown that 𝛾 has the value of 𝛾 = 53 for ideal mona- tomic gases and a value of 𝛾 = 75 for ideal diatomic gases. The value of 𝛾 appears in Equation 16.5 because the condensations and rarefactions of a sound wave are formed by adiabatic compres- sions and expansions of the gas. The regions that are compressed (the condensations) become slightly warmed, and the regions that are expanded (the rarefactions) become slightly cooled. However, no appreciable heat fl ows from a condensation to an adjacent rarefaction because the distance between the two (half a wavelength) is relatively large for most audible sound waves and a gas is a poor thermal conductor. Thus, the compression and expansion process is adiabatic. Example 4 illustrates the use of Equation 16.5.
TABLE 16.1 Speed of Sound in Gases, Liquids, and Solids
Substance Speed (m/s) Gases Air (0 °C) 331
Air (20 °C) 343
Carbon dioxide (0 °C) 259
Oxygen (0 °C) 316
Helium (0 °C) 965
Liquids Chloroform (20 °C) 1004
Ethyl alcohol (20 °C) 1162
Mercury (20 °C) 1450
Fresh water (20 °C) 1482
Seawater (20 °C) 1522
Solids Copper 5010
Glass (Pyrex) 5640
Lead 1960
Steel 5960
16.6 The Speed of Sound 443
Analyzing Multiple-Concept Problems
EXAMPLE 4 The Physics of an Ultrasonic Ruler
Figure 16.18 shows an ultrasonic ruler that is used to measure the dis- tance to a target, such as a wall. To initiate the measurement, the ruler generates a pulse of ultrasonic sound that travels to the wall and, much like an echo, refl ects from it. The refl ected pulse returns to the ruler, which measures the time it takes for the round-trip. Using a preset value for the speed of sound, the unit determines the distance to the wall and displays it on a digital readout. Suppose that the round-trip travel time is 20.0 ms on a day when the air temperature is 32 °C. Assuming that air is an ideal diatomic gas (γ = 75 ) and that the average molecular mass
of air is 28.9 u, fi nd the distance between the ultrasonic ruler and the wall.
Reasoning The distance between the ruler and the wall is equal to the speed of sound multiplied by the time it takes for the sound pulse to reach the wall. The speed 𝜐 of sound can be determined from a knowledge of the air temperature T and the average mass m of an air molecule by using the relation υ = √γkT /m (Equation 16.5). The time can be deduced from the given data.
Knowns and Unknowns The data for this problem are listed below:
Description Symbol Value Comment Round-trip time of sound tRT 20.0 ms 20.0 ms = 20.0 × 10−3 s
Air temperature Tc 32 °C
Ratio of specific heats for air 𝛾 75
Average molecular mass of air m 28.9 u Must convert “u” to kilograms.
Unknown Variable Distance between ruler and wall x ?
Modeling the Problem
STEP 1 Kinematics Since sound moves at a constant speed, the distance x it travels is the product of its speed υ and the time t, or x = υt. The time for the sound to reach the wall is one-half the round-trip time tRT, so t =
1 2tRT. Thus, the distance to the wall is
x = υ( 12 t RT)
The round-trip time tRT is known, but the speed of sound in air at 32 °C is not. We will fi nd an expression for this speed in Step 2.
x = υ( 12 t RT) (1)
?
x
FIGURE 16.18 An ultrasonic ruler uses sound with a frequency greater than 20 kHz to measure the distance x to the wall. The blue arcs and blue arrow denote the outgoing sound wave, and the red arcs and red arrow denote the wave refl ected from the wall.
444 CHAPTER 16 Waves and Sound
STEP 2 Speed of Sound Since the air is assumed to be an ideal gas, the speed υ of sound is related to the Kelvin temperature T and the average mass m of an air molecule by
υ = √γ kTm (16.5) where 𝛾 is the ratio of the specifi c heat capacity of air at constant pressure to that at constant volume (see Section 15.5), and k is Boltzmann’s constant. The temperature in this expression must be the Kelvin temperature of the air, which is related to its Celsius temperature Tc by T = Tc + 273.15 (Equation 12.1). Thus, the speed of sound in air is
υ = √γk (Tc + 273.15)m This expression for υ can be substituted into Equation 1, as shown on the right.
Problem-Solving Insight When using the equation υ = √γkT/m to calculate the speed of sound in an ideal gas, be sure to express the temperature T in kelvins and not in degrees Celsius or Fahrenheit.
Solution Combining the results of the modeling steps, we have
x = υ( 12 tRT) = √γk (Tc + 273.15)m ( 12 tRT) Since the average mass of an air molecule is given in atomic mass units (28.9 u), we must convert
it to kilograms by using the conversion factor 1 u = 1.6605 × 10−27 kg (see Section 14.1). Thus,
m = (28.9 u)( 1.6605 × 10−27 kg
1 u ) = 4.80 × 10−26 kg The distance from the ultrasonic ruler to the wall is
x = √γk(Tc + 273.15)m ( 12 tRT)
= √ 7
5 (1.38 × 10 −23 J/K)(32 °C + 273.15)
4.80 × 10−2 kg [ 1
2 (20.0 × 10−3 s)] = 3.50 m
Related Homework: Problems 48, 50, 110
STEP 1 STEP 2
x = υ( 12 t RT) (1)
υ = √γk (Tc + 273.15)m
THE PHYSICS OF . . . sonar. Sonar (sound navigation ranging) is a technique for determining water depth and locating underwater objects, such as reefs, submarines, and
schools of fi sh. The core of a sonar unit consists of an ultrasonic transmitter and receiver
mounted on the bottom of a ship. The transmitter emits a short pulse of ultrasonic sound, and at
a later time the refl ected pulse returns and is detected by the receiver. The distance to the object
is determined from the electronically measured round-trip time of the pulse and a knowledge
of the speed of sound in water; the distance registers automatically on an appropriate meter.
Such a measurement is similar to the distance measurement discussed for the ultrasonic ruler
in Example 4.
Conceptual Example 5 illustrates how the speed of sound in air can be used to estimate the
distance to a thunderstorm, using a handy rule of thumb.
CONCEPTUAL EXAMPLE 5 Lightning, Thunder, and a Rule of Thumb
In a thunderstorm, lightning and thunder occur nearly simultaneously. The
light waves from the lightning travel at a speed of 𝜐light = 3.0 × 10 8 m/s,
whereas the sound waves from the thunder travel at 𝜐sound = 343 m/s.
There is a rule of thumb for estimating how far away a storm is. After you
see a lightning fl ash, count the seconds until you hear the thunder; divide
the number of seconds by fi ve to get the approximate distance (in miles)
to the storm. In this rule, which of the two speeds plays a role? (a) Both 𝜐sound and 𝜐light (b) Only 𝜐sound (c) Only 𝜐light
16.6 The Speed of Sound 445
Liquids In a liquid, the speed of sound depends on the density 𝜌 and the adiabatic bulk modulus Bad of the liquid:
Liquid υ = √Badρ (16.6) The bulk modulus is introduced in Section 10.7 in a discussion of the volume deformation of liquids and solids. There it is tacitly assumed that the temperature remains constant while the volume of the material changes; that is, the compression or expansion is isothermal. However, the condensations and rarefactions in a sound wave occur under adiabatic rather than isothermal conditions. Thus, the adiabatic bulk modulus Bad must be used when calculating the speed of sound in liquids. Values of Bad will be provided as needed in this text.
Table 16.1 gives some data for the speed of sound in liquids. In seawater, for instance, the speed is 1522 m/s, which is more than four times as great as the speed in air. The speed of sound is an important parameter in the measurement of distance, as discussed for the ultrasonic ruler in Example 4.
BIO THE PHYSICS OF . . . cataract surgery. Accurate distance measurements using ultrasonic sound also play an important role in medicine, where the sound often travels through liquid-like materials in the body. A routine preoperative procedure in cataract sur- gery, for example, uses an ultrasonic probe called an A-scan to measure the length of the eyeball in front of the lens, the thickness of the lens, and the length of the eyeball between the lens and the retina (see Figure 16.20). The measurement is similar to that discussed in Example 4 and relies on the fact that the speed of sound in the material in front of and behind the lens of the eye is 1532 m/s, whereas that within the lens is 1641 m/s. In cataract surgery, the cataractous lens is removed and often replaced with an implanted artifi cial lens. Data pro- vided by the A-scan facilitate the design of the lens implant (its size and the optical correction that it introduces).
Solid Bars When sound travels through a long, slender, solid bar, the speed of the sound depends on the properties of the medium according to
Long, slender, solid bar υ = √Yρ (16.7) where Y is Young’s modulus (defi ned in Section 10.7) and 𝜌 is the density.
Reasoning At a distance of one mile from a storm, the observer in Figure 16.19 detects either type of wave only after a time that is equal to the distance divided by the speed at which the wave travels. This fact will guide our analysis.
Answers (b) and (c) are incorrect. The rule involves the time that passes between seeing the lightning fl ash and hearing the thunder, not just the time at which either type of wave is detected. Therefore, both the speeds 𝜐light and 𝜐sound must play a role in the rule.
Answer (a) is correct. Light from the fl ash travels so rapidly that it reaches the observer almost instantaneously; its travel time for one mile (1.6 × 103 m) is only
t light = 1.6 × 10 3 m
υ light =
1.6 × 10 3 m 3.0 × 10 8 m/s
= 5 × 10−6 s
In comparison, the sound of the thunder travels very slowly; its travel time for one mile is
t sound = 1.6 × 10 3 m
υ sound =
1.6 × 10 3 m 343 m/s
= 5 s
Since tlight is negligible compared to tsound, the time between seeing the lightning fl ash and hearing the thunder is about 5 s for every mile of dis- tance from the storm.
vlight
vsound
1.0 mile (1.6 × 103 m)
FIGURE 16.19 A lightning bolt from a thunderstorm generates a fl ash of light and sound (thunder). The speed of light is much greater than the speed of sound. Therefore, the light reaches the person fi rst, followed later by the sound.
Lens
Retina
FIGURE 16.20 A cross-sectional view of the human eye.
446 CHAPTER 16 Waves and Sound
Check Your Understanding
(The answers are given at the end of the book.) 11. Do you expect an echo to return to you more quickly on a hot day or a cold day, other things being
equal?
12. Carbon monoxide (CO), hydrogen (H2), and nitrogen (N2) may be treated as ideal gases. Each has the same temperature and nearly the same value for the ratio of the specifi c heat capacities at constant pressure and constant volume. In which two of the three gases is the speed of sound approximately the same?
13. Jell-O starts out as a liquid and then sets to a gel. As the Jell-O sets and becomes more solid, does the speed of sound in this material increase, decrease, or remain the same?
16.7 Sound Intensity Sound waves carry energy that can be used to do work, like forcing the eardrum to vibrate. In an extreme case such as a sonic boom, the energy can be suffi cient to cause damage to windows and buildings. The amount of energy transported per second by a sound wave is called the power of the wave and is measured in SI units of joules per second (J/s) or watts (W).
When a sound wave leaves a source, such as the loudspeaker in Figure 16.21, the power spreads out and passes through imaginary surfaces that have increasingly larger areas. For instance, the same sound power passes through the surfaces labeled 1 and 2 in the drawing. How- ever, the power is spread out over a greater area in surface 2. We will bring together the ideas of sound power and the area through which the power passes and, in the process, will formulate the concept of sound intensity. The idea of wave intensity is not confi ned to sound waves. It will recur, for example, in Chapter 24 when we discuss another important type of waves, electromag- netic waves.
The sound intensity I is defi ned as the sound power P that passes perpendicularly through a surface divided by the area A of that surface:
I = P A
(16.8)
The unit of sound intensity is power per unit area, or W/m2. The next example illustrates how the sound intensity changes as the distance from a loudspeaker changes.
1
2
FIGURE 16.21 The power carried by a sound wave spreads out after leaving a source, such as a loudspeaker. Thus, the power passes perpendicularly through surface 1 and then through surface 2, which has the larger area.
EXAMPLE 6 Sound Intensities
In Figure 16.21, 12 × 10−5 W of sound power passes perpendicularly through the surfaces labeled 1 and 2. These surfaces have areas of A1 = 4.0 m2 and A2 = 12 m2. Determine the sound intensity at each surface and discuss why listener 2 hears a quieter sound than listener 1.
Reasoning The sound intensity I is the sound power P passing perpen- dicularly through a surface divided by the area A of that surface. Since the same sound power passes through both surfaces and surface 2 has the greater area, the sound intensity is less at surface 2.
Problem-Solving Insight Sound intensity I and sound power P are diff erent concepts. They are related, however, since intensity equals power per unit area.
Solution The sound intensity at each surface follows from Equation 16.8:
Surface 1 I1 = P A1
= 12 × 10−5 W
4.0 m2 = 3.0 × 10−5 W/m2
Surface 2 I2 = P A2
= 12 × 10−5 W
12 m2 = 1.0 × 10−5 W/m2
The sound intensity is less at the more distant surface, where the same power passes through a threefold greater area. The ear of a listener, with its fi xed area, intercepts less power where the intensity, or power per unit area, is smaller. Thus, listener 2 intercepts less of the sound power than listener 1. With less power striking the ear, the sound is quieter.
16.7 Sound Intensity 447
For a 1000-Hz tone, the smallest sound intensity that the human ear can detect is about 1 × 10−12 W/m2; this intensity is called the threshold of hearing. On the other extreme, con- tinuous exposure to intensities greater than 1 W/m2 can be painful and can result in permanent hearing damage. The human ear is remarkable for the wide range of intensities to which it is sensitive.
If a source emits sound uniformly in all directions, the intensity depends on distance in a simple way. Figure 16.22 shows such a source at the center of an imaginary sphere (for clarity only a hemisphere is shown). The radius of the sphere is r. Since all the radiated power P passes through the spherical surface of area A = 4𝜋r2, the intensity at a distance r is
Spherically uniform radiation I = P
4πr 2 (16.9)
From this we see that the intensity of a source that radiates sound uniformly in all directions varies as 1/r2. For example, if the distance increases by a factor of two, the sound intensity decreases by a factor of 22 = 4. Example 7 illustrates the eff ect of the 1/r2 dependence of intensity on distance.
Sound source at center of sphere
FIGURE 16.22 The sound source at the center of the sphere emits sound uniformly in all directions. In this drawing, only a hemisphere is shown for clarity.
EXAMPLE 7 Fireworks
During a fi reworks display, a rocket explodes high in the air above the observers. Assume that the sound spreads out uniformly in all directions and that refl ections from the ground can be ignored. When the sound reaches listener 2 in Figure 16.23, who is r2 = 640 m away from the explosion, the sound has an intensity of I2 = 0.10 W/m2. What is the sound intensity detected by listener 1, who is r1 = 160 m away from the explosion?
Reasoning Listener 1 is four times closer to the explosion than listener 2. Therefore, the sound intensity detected by listener 1 is 42 = 16 times greater than the sound intensity detected by listener 2.
Problem-Solving Insight Equation 16.9 can be used only when the sound spreads out uniformly in all directions and there are no refl ections of the sound waves.
Solution The ratio of the sound intensities can be found using Equa- tion 16.9:
I1 I2
=
P 4πr1 2
P 4πr 2 2
= r 2 2
r1 2 =
(640 m) 2
(160 m) 2 = 16
As a result, I1 = (16)I2 = (16)(0.10 W/m2) = 1.6 W/m2 .
r2
r1
2
1
FIGURE 16.23 If an explosion in a fi reworks display radiates sound uniformly in all directions, the intensity at any distance r is I = P/(4𝜋r2), where P is the sound power of the explosion.
Equation 16.9 is valid only when no walls, ceilings, fl oors, etc. are present to refl ect the sound and cause it to pass through the same surface more than once. Conceptual Example 8 demonstrates why this is so.
448 CHAPTER 16 Waves and Sound
Check Your Understanding
(The answers are given at the end of the book.) 14. BIO Some animals rely on an acute sense of hearing for survival, and the visible parts of the ears on
such animals are often relatively large. How does this anatomical feature help to increase the sensitivity of the animal’s hearing for low-intensity sounds?
15. A source is emitting sound uniformly in all directions. There are no refl ections anywhere. A fl at surface faces the source. Is the sound intensity the same at all points on the surface?
16.8 Decibels The decibel (dB) is a measurement unit used when comparing two sound intensities. The simplest method of comparison would be to compute the ratio of the intensities. For instance, we could compare I = 8 × 10−12 W/m2 to I0 = 1 × 10−12 W/m2 by computing I/I0 = 8 and stating that I is eight times as great as I0. However, because of the way in which the human hearing mechanism responds to intensity, it is more appropriate to use a logarithmic scale for the comparison. For this purpose, the intensity level 𝛽 (expressed in decibels) is defi ned as follows:
β = (10 dB) log ( II 0) (16.10) where “log” denotes the common logarithm to the base ten. I0 is the intensity of the reference level to which I is being compared and is sometimes the threshold of hearing; that is, I0 = 1.00 × 10−12 W/m2. With the aid of a calculator, the intensity level can be evaluated for the values of I and I0 given above:
β = (10 dB) log (8 × 10 −12 W/m 2
1 × 10−12 W/m 2) = (10 dB) log 8 = (10 dB)(0.9) = 9 dB This result indicates that I is 9 decibels greater than I0. Although 𝛽 is called the “intensity level,” it is not an intensity and does not have intensity units of W/m2. In fact, the decibel, like the radian, is dimensionless.
CONCEPTUAL EXAMPLE 8 Reflected Sound and Sound Intensity
Suppose that the person singing in the shower in Figure 16.24 produces a sound power P. Sound refl ects from the surrounding shower stall. At a distance r in front of the person, does the expression I = P/(4𝜋r2) (Equation 16.9) (a) overestimate, (b) underestimate, or (c) give the correct total sound intensity?
Reasoning In arriving at Equation 16.9, it was assumed that the sound spreads out uniformly from the source and passes only once through the imaginary surface that surrounds it (see Figure 16.22). In Figure 16.24, only part of this imaginary surface (colored blue) is shown, but nonethe- less, if Equation 16.9 is to apply, the same assumption must hold.
Answers (a) and (c) are incorrect. Equation 16.9 cannot overestimate the sound intensity, because it assumes that the sound passes through the imaginary surface only once and, hence, does not take into account the refl ected sound within the shower stall. For the same reason, neither can Equation 16.9 give the correct sound intensity.
Answer (b) is correct. Figure 16.24 illustrates three paths by which the sound passes through the imaginary surface. The “direct” sound travels along a path from its source directly to the surface. It is the intensity of this sound that is given by I = P/(4𝜋r2). The remaining paths are two of the many that characterize the sound refl ected from the shower stall. The total sound power that passes through the surface is the sum of the direct
and refl ected powers. Thus the total sound intensity at a distance r from the source is greater than the intensity of the direct sound alone, so Equa- tion 16.9 underestimates the sound intensity from the singing. People like to sing in the shower because their voices sound so much louder due to the enhanced intensity caused by the refl ected sound.
Related Homework: Problems 55, 72
Direct sound
Reflected sound
Reflected sound
FIGURE 16.24 When someone sings in the shower, the sound power passing through part of an imaginary spherical surface (shown in blue) is the sum of the direct sound power and the refl ected sound power.
Math Skills In Equation 16.10,
log ( II0) refers to the common logarithm and not the natural logarithm, which is
ln ( II0). Since most calculators provide single-button access to both types of logarithm, be careful to hit the “log” button and not the “ln” button when you evaluate the logarithm. For
example, if I I0
= 10.00, it follows that
log (10.00) = 1.000. But if you mistak- enly hit the “ln” button, your calculator will display 2.303, and the value that you determine for the intensity level 𝛽 in Equation 16.10 will be incorrect. When using Equation 16.10, also note
that the ratio I I0
cannot be a negative
number, since the logarithm of a nega- tive number is not defi ned.
16.8 Decibels 449
Notice that if both I and I0 are at the threshold of hearing, then I = I0, and the intensity level is 0 dB according to Equation 16.10:
β = (10 dB) log ( I0 I0) = (10 dB) log 1 = 0 dB
since log 1 = 0. Thus,
Problem-Solving Insight An intensity level of zero decibels does not mean that the sound intensity I is zero; it means that I = I0.
Intensity levels can be measured with a sound-level meter, such as the one in Figure 16.25. The intensity level 𝛽 is displayed on its scale, assuming that the threshold of hearing is 0 dB. Table 16.2 lists the intensities I and the associated intensity levels 𝛽 for some common sounds, using the threshold of hearing as the reference level.
When a sound wave reaches a listener’s ear, the sound is interpreted by the brain as loud or soft, depending on the intensity of the wave. Greater intensities give rise to louder sounds. However, the relation between intensity and loudness is not a simple proportionality, because doubling the intensity does not double the loudness, as we will now see.
Suppose you are sitting in front of a stereo system that is producing an intensity level of 90 dB. If the volume control on the amplifi er is turned up slightly to produce a 91-dB level, you would just barely notice the change in loudness. Hearing tests have revealed that a one- decibel (1-dB) change in the intensity level corresponds to approximately the smallest change in loudness that an average listener with normal hearing can detect. Since 1 dB is the smallest perceivable increment in loudness, a change of 3 dB—say, from 90 to 93 dB—is still a rather small change in loudness. Example 9 determines the factor by which the sound intensity must be increased to achieve such a change.
80 100 120 140
604020 0
Decibels
FIGURE 16.25 A sound-level meter and a close-up view of its decibel scale.
TABLE 16.2 Typical Sound Intensities and Intensity Levels Relative to the Threshold of Hearing
Intensity I (W/m2) Intensity Level 𝜷 (dB) Threshold of hearing 1.0 × 10−12 0
Rustling leaves 1.0 × 10−11 10
Whisper 1.0 × 10−10 20
Normal conversation (1 meter) 3.2 × 10−6 65
Inside car in city traffic 1.0 × 10−4 80
Car without muffler 1.0 × 10−2 100
Live rock concert 1.0 120
Threshold of pain 10 130
EXAMPLE 9 Comparing Sound Intensities
Audio system 1 produces an intensity level of 𝛽1 = 90.0 dB, and system 2 produces an intensity level of 𝛽2 = 93.0 dB. The corresponding intensities (in W/m2) are I1 and I2. Determine the ratio I2/I1.
Reasoning Intensity levels are related to intensities by logarithms (see Equation 16.10), and it is a property of logarithms (see Appendix D) that log A − log B = log (A/B). Subtracting the two intensity levels and using this property, we fi nd that
β2 − β1 = (10 dB) log ( I2 I0) − (10 dB) log (
I1 I0) = (10 dB) log (
I2 /I0 I1 /I0)
= (10 dB) log ( I2 I1)
Solution Using the result just obtained, we fi nd
93.0 dB − 90.0 dB = (10 dB) log ( I2 I1)
0.30 = log ( I2 I1) or
I2 I1
= 10 0.30 = 2.0
Doubling the intensity changes the loudness by only a small amount (3 dB) and does not double it, so there is no simple proportionality between intensity and loudness.
450 CHAPTER 16 Waves and Sound
To double the loudness of a sound, the intensity must be increased by more than a factor of two. Experiment shows that if the intensity level increases by 10 dB, the new sound seems approximately twice as loud as the original sound. For instance, a 70-dB intensity level sounds about twice as loud as a 60-dB level, and an 80-dB intensity level sounds about twice as loud as a 70-dB level. The factor by which the sound intensity must be increased to double the loudness can be determined as in Example 9:
β 2 − β1 = 10.0 dB = (10 dB) [ log (I 2I 0) − log ( I1 I 0)]
Solving this equation as in Example 9 reveals that I2/I1 = 10.0. Thus, increasing the sound inten- sity by a factor of ten will double the perceived loudness. Consequently, with both audio systems in Figure 16.26 set at maximum volume, the 200-watt system will sound only twice as loud as the much cheaper 20-watt system.
Check Your Understanding
(The answers are given at the end of the book.) 16. If two people talk simultaneously and each creates an intensity level of 65 dB at a certain point, does
the total intensity level at this point equal 130 dB?
17. Two observation points are located at distances r1 and r2 from a source of sound. The sound spreads out uniformly from the source, and there are no refl ecting surfaces in the environment. The sound inten- sity level at distance r2 is 6 dB less than the level at distance r1. (a) What is the ratio I2/I1 of the sound intensities at the two distances? (b) What is the ratio r2/r1 of the distances?
16.9 The Doppler Eff ect Have you ever heard an approaching fi re truck and noticed the distinct change in the sound of the siren as the truck passes? The eff ect is similar to what you get when you put together the two syllables “eee” and “yow” to produce “eee-yow.” While the truck approaches, the pitch of the siren is relatively high (“eee”), but as the truck passes and moves away, the pitch suddenly drops (“yow”). Something similar, but less familiar, occurs when an observer moves toward or away from a stationary source of sound. Such phenomena were fi rst identifi ed in 1842 by the Austrian physicist Christian Doppler (1803–1853) and are collectively referred to as the Doppler eff ect.
To explain why the Doppler eff ect occurs, we will bring together concepts that we have discussed previously—namely, the velocity of an object and the wavelength and frequency of a sound wave (Section 16.5). We will combine the eff ects of the velocities of the source and observer of the sound with the defi nitions of wavelength and frequency. In so doing, we will see that the Doppler eff ect is the change in frequency or pitch of the sound detected by an observer because the sound source and the observer have diff erent velocities with respect to the medium of sound propagation.
Moving Source To see how the Doppler eff ect arises, consider the sound emitted by a siren on the stationary fi re truck in Animated Figure 16.27a. Like the truck, the air is assumed to be stationary with respect to the earth. Each solid blue arc in the drawing represents a condensation of the sound wave. Since the sound pattern is symmetrical, listeners standing in front of or behind the truck detect the same number of condensations per second and, consequently, hear the same frequency. Once the truck begins to move, the situation changes, as part b of the picture illustrates. Ahead of the truck, the condensations are now closer together, resulting in a decrease in the wavelength of the sound. This “bunching-up” occurs because the moving truck “gains ground” on a previously
FIGURE 16.26 In spite of its tenfold greater power, the 200-watt audio system has only about double the loudness of the 20-watt system, when both are set for maximum volume.
200 watts 20 watts
Condensations Wavelength
Larger wavelength
Truck moving
(b)
(a)
Truck at rest
Smaller wavelength
ANIMATED FIGURE 16.27 (a) When the truck is stationary, the wavelength of the sound is the same in front of and behind the truck. (b) When the truck is moving, the wavelength in front of the truck becomes smaller, while the wavelength behind the truck becomes larger.
16.9 The Doppler Eff ect 451
emitted condensation before emitting the next one. Since the condensations are closer together, the observer standing in front of the truck senses more of them arriving per second than she does when the truck is stationary. The increased rate of arrival corresponds to a greater sound frequency, which the observer hears as a higher pitch. Behind the moving truck, the condensa- tions are farther apart than they are when the truck is stationary. This increase in the wavelength occurs because the truck pulls away from condensations emitted toward the rear. Consequently, fewer condensations per second arrive at the ear of an observer behind the truck, corresponding to a smaller sound frequency or lower pitch.
If the stationary siren in Animated Figure 16.27a emits a condensation at the time t = 0 s, it will emit the next one at time T, where T is the period of the wave. The distance between these two condensations is the wavelength 𝜆 of the sound produced by the stationary source, as Figure 16.28a indicates. When the truck is moving with a speed 𝜐s (the subscript “s” stands for the “source” of sound) toward a stationary observer, the siren also emits condensations at t = 0 s and at time T. However, prior to emitting the second condensation, the truck moves closer to the observer by a distance 𝜐sT, as Figure 16.28b shows. As a result, the distance between successive condensations is no longer the wavelength 𝜆 created by the stationary siren, but, rather, a wave- length 𝜆ʹ that is shortened by the amount 𝜐sT:
λ′ = λ − υsT
Let’s denote the frequency perceived by the stationary observer as fo, where the subscript “o” stands for “observer.” According to Equation 16.1, fo is equal to the speed of sound 𝜐 divided by the shortened wavelength 𝜆ʹ:
fo = υ λ′
= υ
λ − υsT
But for the stationary siren, we have 𝜆 = 𝜐/fs and T = 1/fs, where fs is the frequency of the sound emitted by the source (not the frequency fo perceived by the observer). With the aid of these sub- stitutions for 𝜆 and T, the expression for fo can be arranged to give the following result:
Source moving toward stationary observer
fo = fs ( 1
1 − υs υ
) (16.11) Since the term 1 − 𝜐s/𝜐 is in the denominator in Equation 16.11 and is less than one, the frequency fo heard by the observer is greater than the frequency fs emitted by the source. The diff erence between these two frequencies, fo − fs, is called the Doppler shift, and its magnitude depends on the ratio of the speed of the source 𝜐s to the speed of sound 𝜐.
When the siren moves away from, rather than toward, the observer, the wavelength 𝜆ʹ becomes greater than 𝜆 according to
λ′ = λ + υsT
Notice the presence of the “+” sign in this equation, in contrast to the “−” sign that appeared earlier. The same reasoning that led to Equation 16.11 can be used to obtain an expression for the observed frequency fo:
Source moving away from stationary observer
fo = fs ( 1
1 + υs υ
) (16.12) The denominator 1 + 𝜐s/𝜐 in Equation 16.12 is greater than one, so the frequency fo heard by the observer is less than the frequency fs emitted by the source. The next example illustrates how large the Doppler shift is in a familiar situation.
Truck moving
υs
υsT
Stationary observer
Truck at rest λ
λ′
Stationary observer
(b)
(a)
FIGURE 16.28 (a) When the fi re truck is stationary, the distance between successive condensations is one wavelength 𝜆. (b) When the truck moves with a speed 𝜐s, the wavelength of the sound in front of the truck is shortened to 𝜆ʹ.
EXAMPLE 10 The Sound of a Passing Train
A high-speed train is traveling at a speed of 44.7 m/s (100 mi/h) when the engineer sounds the 415-Hz warning horn. The speed of sound is 343 m/s. What are the frequency and wavelength of the sound, as perceived by
a person standing at a crossing, when the train is (a) approaching and (b) leaving the crossing?
452 CHAPTER 16 Waves and Sound
Moving Observer Figure 16.29 shows how the Doppler eff ect arises when the sound source is stationary and the observer moves. As in the case of the moving source, we assume that the air is sta- tionary. The observer moves with a speed 𝜐o (“o” stands for “observer”) toward the stationary source and covers a distance 𝜐ot in a time t. During this time, the moving observer encounters all the condensations that he would if he were stationary, plus an additional number. The additional number of condensations encountered is the distance 𝜐ot divided by the distance 𝜆 between successive condensations, or 𝜐ot/𝜆. Thus, the additional number of condensations encountered per second by the moving observer is 𝜐o/𝜆. Since a stationary observer would hear a frequency fs emitted by the source, the moving observer hears a greater frequency fo given by
fo = fs + υo λ
= fs (1 + υo f sλ)
Using the fact that 𝜐 = fs𝜆, where 𝜐 is the speed of sound, we fi nd that
Observer moving toward stationary source fo = fs (1 +
υo υ ) (16.13)
An observer moving away from a stationary source moves in the same direction as the sound wave and, as a result, intercepts fewer condensations per second than a stationary observer does. In this case, the moving observer hears a smaller frequency fo that is given by
Observer moving away from stationary source fo = fs (1 −
υo υ ) (16.14)
It should be noted that the physical mechanism producing the Doppler eff ect is diff erent when the source moves and the observer is stationary from when the observer moves and the source is stationary. When the source moves, as in Figure 16.28b, the wavelength of the sound perceived by the observer changes from 𝜆 to 𝜆ʹ. When the wavelength changes, the stationary observer hears a diff erent frequency fo than the frequency produced by the source. On the other hand, when the observer moves and the source is stationary, the wavelength 𝜆 does not change (see, for example, Figure 16.29). Instead, the moving observer intercepts a diff erent number of wave condensations per second than does a stationary observer and therefore detects a diff erent frequency fo.
Reasoning When the train approaches, the person at the crossing hears a sound whose frequency is greater than 415 Hz because of the Doppler eff ect. As the train moves away, the person hears a frequency that is less than 415 Hz. We may use Equations 16.11 and 16.12, respectively, to determine these frequencies. In either case, the observed wavelength can be obtained according to Equation 16.1 as the speed of sound divided by the observed frequency.
Solution (a) When the train approaches, the observed frequency is
fo = fs ( 1
1 − υs υ
) = (415 Hz) (
1
1 − 44.7 m /s 343 m /s
) = 477 Hz (16.11)
The observed wavelength is
λ′ = υ fo
= 343 m /s 477 Hz
= 0.719 m (16.1)
(b) When the train leaves the crossing, the observed frequency is
fo = fs ( 1
1 + υs υ
) = (415 Hz) (
1
1 + 44.7 m /s 343 m /s
) = 367 Hz (16.12) In this case, the observed wavelength is
λ′ = υ fo
= 343 m /s 367 Hz
= 0.935 m (16.1)
Stationary source
Moving observer
υot
υo
λ
FIGURE 16.29 An observer moving with a speed 𝜐o toward the stationary source intercepts more wave condensations per unit of time than does a stationary observer.
16.9 The Doppler Eff ect 453
General Case It is possible for both the sound source and the observer to move with respect to the medium of sound propagation. If the medium is stationary, Equations 16.11–16.14 may be combined to give
the observed frequency fo as
Source and observer both moving fo = fs (
1 ± υo υ
1 ∓ υs υ ) (16.15)
In the numerator, the plus sign applies when the observer moves toward the source, and the minus
sign applies when the observer moves away from the source. In the denominator, the minus sign
is used when the source moves toward the observer, and the plus sign is used when the source
moves away from the observer. The symbols 𝜐o, 𝜐s, and 𝜐 denote numbers without an algebraic
sign because the direction of travel has been taken into account by the plus and minus signs that
appear directly in this equation.
NEXRAD THE PHYSICS OF . . . NEXRAD. NEXRAD stands for Next Generation Weather Radar and is a nationwide system used by the National Weather Service to provide dramatically
improved early warning of severe storms, such as the tornado in Figure 16.30. The system is based on radar waves, which are a type of electromagnetic wave (see Chapter 24) and, like sound
waves, can exhibit the Doppler eff ect. The Doppler eff ect is at the heart of NEXRAD. As the
drawing illustrates, a tornado is a swirling mass of air and water droplets. Radar pulses are sent
out by a NEXRAD unit, whose protective covering is shaped like a soccer ball. The waves refl ect
from the water droplets and return to the unit, where the frequency is observed and compared
to the outgoing frequency. For instance, droplets at point A in the drawing are moving toward the unit, and the radar waves refl ected from them have their frequency Doppler-shifted to higher
values. Droplets at point B, however, are moving away from the unit, and the frequency of the waves refl ected from these droplets is Doppler-shifted to lower values. Computer processing of
the Doppler frequency shifts leads to color-enhanced views on display screens (see Figure 16.31). These views reveal the direction and magnitude of the wind velocity and can identify, from dis-
tances up to 140 mi, the swirling air masses that are likely to spawn tornadoes. The equations
that specify the Doppler frequency shifts are diff erent from those given for sound waves by Equa-
tions 16.11–16.15. The reason for the diff erence is that radar waves propagate from one place to
another by a diff erent mechanism than that of sound waves (see Section 24.5).
NEXRAD unit
Direction of swirling air and water droplets
B
A
(b)(a)
© W
av e/
C o rb
is
FIGURE 16.30 (a) A tornado is one of nature’s most dangerous storms. (b) The National Weather Service uses the NEXRAD system, which is based on Doppler-shifted radar, to identify the storms that are likely
to spawn tornadoes.
FIGURE 16.31 This color-enhanced view of a tornado shows circulating winds detected
by a NEXRAD station, which is located below
and to the right of the fi gure. The white dot
and arrow indicate the storm center and the
direction of wind circulation.
Courtesy Kurt Hondl, National Severe Storms
Laboratory, Norman, OK
454 CHAPTER 16 Waves and Sound
Check Your Understanding
(The answers are given at the end of the book.) 18. At a swimming pool, a music fan up on a diving platform is listening to a radio. As the radio is playing
a tone that has a constant frequency fs, it is accidentally knocked off the platform. Describe the Doppler eff ect heard by (a) the person on the platform and (b) a person down below in the water. In each case, state whether the observed frequency fo is greater or smaller than fs and describe how fo changes (if it changes) as the radio falls.
19. When a car is at rest, its horn emits a frequency of 600 Hz. A person standing in the middle of the street with this car behind him hears the horn with a frequency of 580 Hz. Does he need to jump out of the way?
20. A source of sound produces the same frequency under water as it does in air. This source has the same velocity in air as it does under water. Consider the ratio fo/fs of the observed frequency fo to the source frequency fs. Is this ratio greater in air or under water when the source (a) approaches and (b) moves away from the observer?
21. Two cars, one behind the other, are traveling in the same direction at the same speed. Does either driver hear the other’s horn at a frequency that is diff erent from the frequency heard when both cars are at rest?
22. When a truck is stationary, its horn produces a frequency of 500 Hz. You are driving your car, and this truck is following behind. You hear its horn at a frequency of 520 Hz. (a) Refer to Equation 16.15 and decide which algebraic sign should be used in the numerator and which in the denominator. (b) Which driver, if either, is driving faster?
16.10 Applications of Sound in Medicine BIO THE PHYSICS OF . . . ultrasonic imaging. When ultrasonic waves are used in
medicine for diagnostic purposes, high-frequency sound pulses are produced by a transmitter and directed into the body. As in sonar, refl ections occur. They occur each time a pulse encoun- ters a boundary between two tissues that have diff erent densities or a boundary between a tissue and the adjacent fl uid. By scanning ultrasonic waves across the body and detecting the echoes generated from various internal locations, it is possible to obtain an image, or sonogram, of the inner anatomy. Ultrasonic imaging is employed extensively in obstetrics to examine the develop- ing fetus (Figure 16.32). The fetus, surrounded by the amniotic sac, can be distinguished from other anatomical features so that fetal size, position, and possible abnormalities can be detected. Ultrasound is also used in other medically related areas. For instance, tumors in the liver, kidney, brain, and pancreas can be detected with ultrasound. Yet another application involves monitoring
D r.
N aj
ee b
La yy
ou s/
Sc ie
nc e
So ur
ce
B le
nd Im
ag es
/S up
er St
oc k
FIGURE 16.32 An ultrasonic scanner can be used to produce an image of the fetus as it develops in the uterus. Conventional scanning produces two-dimensional images. Three-dimensional scanning uses computer technology to produce images that are more detailed than the 2-D variety. The image on the right, for example, was obtained using 3-D scanning in the second trimester of pregnancy and illustrates the kind of detail that is achievable.
16.11 The Sensitivity of the Human Ear 455
the real-time movement of pulsating structures, such as heart valves (“echocardiography”) and
large blood vessels.
When ultrasound is used to form images of internal anatomical features or foreign objects in the
body, the wavelength of the sound wave must be about the same size as, or smaller than, the object
to be located. Therefore, high frequencies in the range from 1 to 15 MHz (1 MHz = 1 megahertz =
1 × 106 Hz) are the norm. For instance, the wavelength of 5-MHz ultrasound is 𝜆 = 𝜐/f = 0.3 mm, if a value of 1540 m/s is used for the speed of sound through tissue. A sound wave with a frequency
higher than 5 MHz and a correspondingly shorter wavelength is required for locating objects smaller
than 0.3 mm.
BIO THE PHYSICS OF . . . the cavitron ultrasonic surgical aspirator. Neuro- surgeons use a device called a cavitron ultrasonic surgical aspirator (CUSA) to remove brain tumors once thought to be inoperable. Ultrasonic sound waves cause the slender tip of the CUSA
probe (see Figure 16.33) to vibrate at approximately 23 kHz. The probe shatters any section of the tumor that it touches, and the fragments are fl ushed out of the brain with a saline solution.
Because the tip of the probe is small, the surgeon can selectively remove small bits of malignant
tissue without damaging the surrounding healthy tissue.
BIO THE PHYSICS OF . . . bloodless surgery with HIFU. Another application of ultrasound is in a new type of bloodless surgery, which can eliminate abnormal cells, such
as those in benign hyperplasia of the prostate gland. This technique is known as HIFU (high- intensity focused ultrasound). It is analogous to focusing the sun’s electromagnetic waves by using a magnifying glass and producing a small region where the energy carried by the waves
can cause localized heating. Ultrasonic waves can be used in a similar fashion. The waves enter
directly through the skin and come into focus inside the body over a region that is suffi ciently
well defi ned to be surgically useful. Within this region the energy of the waves causes localized
heating, leading to a temperature of about 56 °C (normal body temperature is 37 °C), which is
suffi cient to kill abnormal cells. The killed cells are eventually removed by the body’s natural
processes.
BIO THE PHYSICS OF . . . the Doppler flow meter. The Doppler fl ow meter is a particularly interesting medical application of the Doppler eff ect. This device measures the
speed of blood fl ow, using transmitting and receiving elements that are placed directly on the
skin, as in Figure 16.34. The transmitter emits a continuous sound whose frequency is typically about 5 MHz. When the sound is refl ected from the red blood cells, its frequency is changed in a
kind of Doppler eff ect because the cells are moving. The receiving element detects the refl ected
sound, and an electronic counter measures its frequency. From the change in frequency the speed
of the blood fl ow can be determined. Typically, the change in frequency is around 600 Hz for
fl ow speeds of about 0.1 m/s. The Doppler fl ow meter can be used to locate regions where blood
vessels have narrowed, since greater fl ow speeds occur in the narrowed regions, according to
the equation of continuity (see Section 11.8). In addition, the Doppler fl ow meter can be used to
detect the motion of a fetal heart as early as 8–10 weeks after conception.
16.11 *The Sensitivity of the Human Ear BIO THE PHYSICS OF . . . hearing. Although the ear is capable of detecting sound
intensities as small as 1 × 10–12 W/m2, it is not equally sensitive to all frequencies, as Figure 16.35 shows. This fi gure displays a series of graphs known as the Fletcher–Munson curves, after H. Fletcher and M. Munson, who fi rst determined them in 1933. In these graphs the audible
sound frequencies are plotted on the horizontal axis, and the sound intensity levels (in deci-
bels) are plotted on the vertical axis. Each curve is a constant loudness curve because it shows the sound intensity level needed at each frequency to make the sound appear to have
the same loudness. For example, the lowest (red) curve represents the threshold of hear-
ing. It shows the intensity levels at which sounds of diff erent frequencies just become audi-
ble. The graph indicates that the intensity level of a 100-Hz sound must be about 37 dB
greater than the intensity level of a 1000-Hz sound to be at the threshold of hearing. There-
fore, the ear is less sensitive to a 100-Hz sound than it is to a 1000-Hz sound. In general, Figure 16.35 reveals that the ear is most sensitive in the range of about 1–5 kHz, and becomes progressively less sensitive at higher and lower frequencies.
Tumor
CUSA probe
Skull
FIGURE 16.33 Neurosurgeons use a cavitron ultrasonic surgical aspirator (CUSA)
to “cut out” brain tumors without adversely
aff ecting the surrounding healthy tissue.
Skin
Incident sound
Reflected sound
Transmitter Receiver
υ s
Red blood cell
FIGURE 16.34 A Doppler fl ow meter measures the speed of red blood cells.
20 40 60 100 200 400
Frequency, Hz 1000
0
4000 10 000
120
100
80
60
In te
ns it
y le
ve l,
dB
40
20 20
40
60
80
100
120
0
Threshold of hearing
FIGURE 16.35 Each curve represents the intensity levels at which sounds of various
frequencies have the same loudness. The
curves are labeled by their intensity levels at
1000 Hz and are known as the Fletcher–
Munson curves.
456 CHAPTER 16 Waves and Sound
Each curve in Figure 16.35 represents a diff erent loudness, and each is labeled according to its intensity level at 1000 Hz. For instance, the curve labeled “60” represents all sounds that have
the same loudness as a 1000-Hz sound whose intensity level is 60 dB. These constant-loudness
curves become fl atter as the loudness increases, the relative fl atness indicating that the ear is
nearly equally sensitive to all frequencies when the sound is loud. Thus, when you listen to loud
sounds, you hear the low frequencies, the middle frequencies, and the high frequencies about
equally well. However, when you listen to quiet sounds, the high and low frequencies seem to be
absent, because the ear is relatively insensitive to these frequencies under such conditions.
EXAMPLE 11 BIO The Physics of Color Doppler Ultrasound
As discussed in Section 16.10, the technique of medical ultrasound can be
used to image many diff erent internal structures of the body. When com-
bined with the Doppler eff ect, the technique of Color Doppler Ultrasound
can provide information on the velocity of fl uids, such as blood, moving
in these structures. The Doppler information is converted by a computer
into a false-color image that is overlaid on the ultrasound image of the
structure, such as a blood vessel. The colors indicate the speed and direc-
tion of the blood fl ow (Figure 16.36). As an example, consider an ultra- sound image created with sound waves at a frequency of 5.00 MHz. The
sound waves travel at a speed of 1540 m/s through the body and refl ect
off of red blood cells fl owing toward the transmitter. A sound receiver,
also located in the transmitter, detects the refl ected sound waves with a
frequency that is 980 Hz higher than the sound sourced by the transmitter.
Calculate the speed of the blood moving toward the transmitter.
Reasoning This is a simple application of the Doppler eff ect equations, where we have to take into account two cases. First, as the sound wave is
sent from the transmitter toward the red blood cells, we have the case of the
observer (the blood) moving toward a stationary source (the transmitter/
receiver), or Equation 16.13. Next, the sound wave is refl ected off the red
blood cell back toward the receiver. Thus, the blood cell acts as the source,
and we have the case of a source moving toward a stationary observer, or
Equation 16.11. Therefore, we will need to use both Equation 16.13 and
Equation 16.11 to calculate the speed of the blood (𝜐B).
Solution The sound will be Doppler shifted on the way to the blood cells and also Doppler shifted upon refl ection. For the sound travel-
ing from the transmitter to the red blood cells, we use Equation 16.13:
fo = fs(1 + υo υ ) = fs(1 +
υB υ ), where we have represented the speed of
the observer (𝜐o) as 𝜐B, the speed of the blood. For the sound traveling back from the red blood cells to the receiver, we use Equation 16.11:
fo = fs( 1
1 − υs υ )
= fs ( 1
1− υB υ )
, where now, since the source of the
sound is the refl ection off of the red blood cells, we replace 𝜐S with 𝜐B. We can combine these two expressions by recognizing that the observed frequency in Equation 16.13 becomes the source frequency in
Equation 16.11. Making this substitution, we have: fo = fs ( 1 +
υB υ
1 − υB υ ) .
We can now rearrange this equation and solve for 𝜐B:
fo fs(1 −
υB υ ) = (1 +
υB υ ) ⇒ υB =
υ( fo − fs) (fo + fs)
= (1540 m/s)(980 Hz)
(10 000 980 Hz)
= 0.15 m/s
Concept Summary 16.1 The Nature of Waves A wave is a traveling disturbance and carries energy from place to place. In a transverse wave, the disturbance occurs per-
pendicular to the direction of travel of the wave. In a longitudinal wave, the
disturbance occurs parallel to the line along which the wave travels.
16.2 Periodic Waves A periodic wave consists of cycles or patterns that are produced over and over again by the source of the wave. The amplitude
of the wave is the maximum excursion of a particle of the medium from the
particle’s undisturbed position. The wavelength 𝜆 is the distance along the
FIGURE 16.36 Color Doppler ultrasound image showing the red and blue color overlay that provides information on the speed and direction
of blood fl ow within internal body structures. Blue indicates blood
fl ow toward the ultrasonic transducer, and red indicates fl ow away. This
particular image shows increased vascularity in the right fallopian tube
of an expecting mother, which, unfortunately, is evidence of an ectopic
pregnancy.
© 2
0 0 9 F
ab ri
ce C
u il
li er
Focus on Concepts 457
length of the wave between two successive equivalent points, such as two crests or two troughs. The period T is the time required for the wave to travel a distance of one wavelength. The frequency f (in hertz) is the number of wave cycles per second that passes an observer and is the reciprocal of the period (in seconds), as shown in Equation 10.5. The speed 𝜐 of a wave is related to its wavelength and frequency according to Equation 16.1.
f = 1 T
(10.5)
υ = f λ (16.1)
16.3 The Speed of a Wave on a String The speed of a wave depends on the properties of the medium in which the wave travels. For a transverse wave on a string that has a tension F and a mass per unit length m/L, the wave speed is given by Equation 16.2. The mass per unit length is also called the linear density.
υ = √ Fm /L (16.2) 16.4 The Mathematical Description of a Wave When a wave of amp- litude A, frequency f, and wavelength 𝜆 moves in the +x direction through a medium, the wave causes a displacement y of a particle at position x accord- ing to Equation 16.3. For a wave moving in the −x direction, the displace- ment y is given by Equation 16.4.
y = A sin (2π f t − 2πxλ ) (16.3)
y = A sin (2π f t + 2πxλ ) (16.4) 16.5 The Nature of Sound Sound is a longitudinal wave that can be created only in a medium; it cannot exist in a vacuum. Each cycle of a sound wave includes one condensation (a region of greater than normal pressure) and one rarefaction (a region of less than normal pressure).
A sound wave with a single frequency is called a pure tone. Frequen- cies less than 20 Hz are called infrasonic. Frequencies greater than 20 kHz are called ultrasonic. The brain interprets the frequency detected by the ear primarily in terms of the subjective quality known as pitch. A high-pitched sound is one with a large frequency (e.g., piccolo). A low-pitched sound is one with a small frequency (e.g., tuba).
The pressure amplitude of a sound wave is the magnitude of the maxi- mum change in pressure, measured relative to the undisturbed pressure. The pressure amplitude is associated with the subjective quality of loudness. The larger the pressure amplitude, the louder the sound.
16.6 The Speed of Sound The speed of sound 𝜐 depends on the properties of the medium. In an ideal gas, the speed of sound is given by Equation 16.5, where 𝛾 = cP/cV is the ratio of the specifi c heat capacities at constant pressure and constant volume, k is Boltzmann’s constant, T is the Kelvin temperature, and m is the mass of a molecule of the gas. In a liquid, the speed of sound is given by Equation 16.6, where Bad is the adiabatic bulk modulus and 𝜌 is the
mass density. In a solid that has a Young’s modulus of Y and the shape of a long slender bar, the speed of sound is given by Equation 16.7.
υ = √γkTm (16.5) υ = √Badρ (16.6) υ = √Yρ (16.7) 16.7 Sound Intensity The intensity I of a sound wave is the power P that passes perpendicularly through a surface divided by the area A of the surface, as shown in Equation 16.8. The SI unit for intensity is watts per square meter (W/m2). The smallest sound intensity that the human ear can detect is known as the threshold of hearing and is about 1 × 10−12 W/m2 for a 1-kHz sound. When a source radiates sound uniformly in all directions and no refl ections are present, the intensity of the sound is inversely proportional to the square of the distance from the source, according to Equation 16.9.
I = P A
(16.8)
I = P
4πr 2 (16.9)
16.8 Decibels The intensity level 𝛽 (in decibels) is used to compare a sound intensity I to the sound intensity I0 of a reference level, as indicated by Equation 16.10. The decibel, like the radian, is dimensionless. An intensity level of zero decibels means that I = I0. One decibel is approximately the smallest change in loudness that an average listener with healthy hearing can detect. An increase of ten decibels in the intensity level corresponds approx- imately to a doubling of the loudness of the sound.
β = (10 dB) log ( II0) (16.10) 16.9 The Doppler Eff ect The Doppler eff ect is the change in frequency detected by an observer because the sound source and the observer have dif- ferent velocities with respect to the medium of sound propagation. If the observer and source move with speeds 𝜐o and 𝜐s, respectively, and if the medium is stationary, the frequency fo detected by the observer is given by Equation 16.15, where fs is the frequency of the sound emitted by the source and 𝜐 is the speed of sound. In the numerator, the plus sign applies when the observer moves toward the source, and the minus sign applies when the observer moves away from the source. In the denominator, the minus sign is used when the source moves toward the observer, and the plus sign is used when the source moves away from the observer.
fo = fs ( 1 ±
υo υ
1 ∓ υs υ ) (16.15)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 16.1 The Nature of Waves 2. Domino toppling is an event in which a large number of dominoes are lined up close together and then allowed to topple, one after the other. The disturbance
that propagates along the line of dominoes is ________________. (a) partly transverse and partly longitudinal (b) transverse (c) longitudinal
Section 16.2 Periodic Waves 3. A transverse wave on a string has an amplitude A. A tiny spot on the string is colored red. As one cycle of the wave passes by, what is the total distance traveled by the red spot? (a) A (b) 2A (c) 12 A (d) 4A (e)
1 4 A
Focus on Concepts
458 CHAPTER 16 Waves and Sound
Section 16.3 The Speed of a Wave on a String 6. As a wave moves through a medium at a speed 𝜐, the particles of the me- dium move in simple harmonic motion about their undisturbed positions. The maximum speed of the simple harmonic motion is 𝜐max. When the amplitude of the wave doubles, ________________. (a) 𝜐 doubles, but 𝜐max remains the same (b) 𝜐 remains unchanged, but 𝜐max doubles (c) both 𝜐 and 𝜐max remain unchanged (d) both 𝜐 and 𝜐max double 7. A rope is attached to a hook in the ceiling and is hanging straight down. The rope has a mass m, and nothing is attached to the free end of the rope. As a transverse wave travels down the rope from the top, ________________. (a) the speed of the wave does not change (b) the speed of the wave increases (c) the speed of the wave decreases
Section 16.4 The Mathematical Description of a Wave 10. The equation that describes a transverse wave on a string is
y = (0.0120 m) sin[(483 rad /s) t − (3.00 rad /m) x]
where y is the displacement of a string particle and x is the position of the particle on the string. The wave is traveling in the +x direction. What is the speed 𝜐 of the wave?
Section 16.5 The Nature of Sound 11. As the amplitude of a sound wave in air decreases to zero, ________________. (a) nothing happens to the condensations and rarefac- tions of the wave (b) the condensations and rarefactions of the wave occupy more and more distance along the direction in which the wave is traveling (c) the condensations of the wave disappear, but nothing happens to the rarefac- tions (d) nothing happens to the condensations of the wave, but the rarefac- tions disappear (e) both the condensations and the rarefactions of the wave disappear
Section 16.6 The Speed of Sound 12. An echo is sound that returns to you after being refl ected from a distant surface (e.g., the side of a cliff ). Assuming that the distances involved are the same, an echo under water and an echo in air return to you ________________. (a) at diff erent times, the echo under water returning more slowly (b) at dif- ferent times, the echo under water returning more quickly (c) at the same time 13. A horn on a boat sounds a warning, and the sound penetrates the water. How does the frequency of the sound in the air compare to its frequency in the water? How does the wavelength in the air compare to the wavelength
in the water? (a) The frequency in the air is smaller than the frequency in the water, and the wavelength in the air is greater than the wavelength in the water. (b) The frequency in the air is greater than the frequency in the water, and the wavelength in the air is smaller than the wavelength in the water. (c) The frequency in the air is the same as the frequency in the water, and the wavelength in the air is the same as the wavelength in the water. (d) The fre- quency in the air is the same as the frequency in the water, and the wavelength in the air is smaller than the wavelength in the water. (e) The frequency in the air is the same as the frequency in the water, and the wavelength in the air is greater than the wavelength in the water.
Section 16.7 Sound Intensity 15. A source emits sound uniformly in all directions. There are no refl ec- tions of the sound. At a distance of 12 m from the source, the intensity of the sound is 5.0 × 10−3 W/m2. What is the total sound power P emitted by the source?
Section 16.8 Decibels 17. A source emits sound uniformly in all directions. There are no refl ections of the sound. At a distance r1 from the source, the sound is 7.0 dB louder than it is at a distance r2 from the source. What is the ratio r1/r2?
Section 16.9 The Doppler Eff ect 18. A red car and a blue car can move along the same straight one-lane road. Both cars can move only at one speed when they move (e.g., 60 mph). The driver of the red car sounds his horn. In which one of the following situations does the driver of the blue car hear the highest horn frequency? (a) Both cars are moving at the same speed, and they are moving apart. (b) Both cars are moving in the same direction at the same speed. (c) Both cars are moving at the same speed, and they are moving toward each other. (d) The red car is moving toward the blue car, which is stationary. (e) The blue car is moving toward the red car, which is stationary.
19. What happens to the Doppler eff ect in air (i.e., the shift in frequency of a sound wave) as the temperature increases? (a) It is greater at higher tem- peratures, but only in the case of a moving source and a stationary observer. (b) It is greater at higher temperatures, but only in the case of a moving observer and a stationary source. (c) It is greater at higher temperatures than at lower temperatures. (d) It is less at higher temperatures than at lower temperatures. (e) The Doppler eff ect does not change as the temperature increases.
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual MMH Problem-solving help GO Guided Online Tutorial V-HINT Video Hints CHALK Chalkboard Videos
BIO Biomedical application E Easy M Medium H Hard
Section 16.1 The Nature of Waves,
Section 16.2 Periodic Waves 1. E SSM Light is an electromagnetic wave and travels at a speed of 3.00 × 108 m/s. The human eye is most sensitive to yellow-green light, which has a wavelength of 5.45 × 10−7 m. What is the frequency of this light?
2. E Consider the freight train in Figure 16.6. Suppose that 15 boxcars pass by in a time of 12.0 s and each has a length of 14.0 m. (a) What is the fre- quency at which each boxcar passes? (b) What is the speed of the train?
Problems
Problems 459
3. E A woman is standing in the ocean, and she notices that after a wave crest passes, fi ve more crests pass in a time of 50.0 s. The distance between two successive crests is 32 m. Determine, if possible, the wave’s (a) period, (b) frequency, (c) wavelength, (d) speed, and (e) amplitude. If it is not pos- sible to determine any of these quantities, then so state.
4. E Tsunamis are fast-moving waves often generated by underwater earth- quakes. In the deep ocean their amplitude is barely noticeable, but upon reaching shore, they can rise up to the astonishing height of a six-story building. One tsunami, generated off the Aleutian islands in Alaska, had a wavelength of 750 km and traveled a distance of 3700 km in 5.3 h. (a) What was the speed (in m/s) of the wave? For reference, the speed of a 747 jetliner is about 250 m/s. Find the wave’s (b) frequency and (c) period. 5. E SSM In Interactive Figure 16.2c the hand moves the end of the Slinky up and down through two complete cycles in one second. The wave moves along the Slinky at a speed of 0.50 m/s. Find the distance between two adjacent crests on the wave.
6. E GO A person fi shing from a pier observes that four wave crests pass by in 7.0 s and estimates the distance between two successive crests to be 4.0 m. The timing starts with the fi rst crest and ends with the fourth. What is the speed of the wave?
7. E Using the data in the graphs that accompany this problem, determine the speed of the wave.
0.020 0.060
0.040
– 0.010
+ 0.010
0.080
At t = 0 s
x (m)
y (m)
0.10 0.30 0.20
– 0.010
+ 0.010
0.40
At x = 0 m
t (s)
y (m)
PROBLEM 7
8. M A 3.49-rad/s (3313 rpm) record has a 5.00-kHz tone cut in the groove. If the groove is located 0.100 m from the center of the record (see drawing), what is the wavelength in the groove?
PROBLEM 8
One wavelength
0.100 m
9. M V-HINT The speed of a transverse wave on a string is 450 m/s, and the wavelength is 0.18 m. The amplitude of the wave is 2.0 mm. How much time is required for a particle of the string to move through a total distance of 1.0 km?
10. M GO A jetskier is moving at 8.4 m/s in the direction in which the waves on a lake are moving. Each time he passes over a crest, he feels a bump. The bumping frequency is 1.2 Hz, and the crests are separated by 5.8 m. What is the wave speed?
11. H Available in WileyPLUS.
Section 16.3 The Speed of a Wave on a String 12. E The mass of a string is 5.0 × 10−3 kg, and it is stretched so that the ten- sion in it is 180 N. A transverse wave traveling on this string has a frequency of 260 Hz and a wavelength of 0.60 m. What is the length of the string?
13. E SSM The middle C string on a piano is under a tension of 944 N. The period and wavelength of a wave on this string are 3.82 ms and 1.26 m, respectively. Find the linear density of the string.
14. E A wire is stretched between two posts. Another wire is stretched between two posts that are twice as far apart. The tension in the wires is the same, and they have the same mass. A transverse wave travels on the shorter wire with a speed of 240 m/s. What would be the speed of the wave on the longer wire?
15. E MMH To measure the acceleration due to gravity on a distant planet, an astronaut hangs a 0.055-kg ball from the end of a wire. The wire has a length of 0.95 m and a linear density of 1.2 × 10−4 kg/m. Using electronic equipment, the astronaut measures the time for a transverse pulse to travel the length of the wire and obtains a value of 0.016 s. The mass of the wire is negligible compared to the mass of the ball. Determine the acceleration due to gravity.
16. E Two wires are parallel, and one is directly above the other. Each has a length of 50.0 m and a mass per unit length of 0.020 kg/m. However, the tension in wire A is 6.00 × 102 N, and the tension in wire B is 3.00 × 102 N. Transverse wave pulses are generated simultaneously, one at the left end of wire A and one at the right end of wire B. The pulses travel toward each other. How much time does it take until the pulses pass each other?
17. E SSM The drawing shows two transverse waves traveling on strings. The linear density of each string is 0.065 kg/m. The tension is provided by a 26-N block that is hanging from the string. Find the speed of the wave in part (a) and in part (b) of the drawing.
26 N
26 N (b)
(a)
PROBLEM 17
18. M GO A steel cable has a cross-sectional area 2.83 × 10−3 m2 and is kept under a tension of 1.00 × 104 N. The density of steel is 7860 kg/m3. Note that this value is not the linear density of the cable. At what speed does a trans- verse wave move along the cable?
19. M GO The drawing shows a graph of two waves traveling to the right at the same speed. (a) Using the data in the drawing, determine the wavelength of each wave. (b) The speed of the waves is 12 m/s; calculate the frequency of each one. (c) What is the maximum speed for a particle attached to each wave?
PROBLEM 19
0.50 m
0.25 m
–0.25 m
0
–0.50 m
4.0 6.02.0
x (m)
AB
20. M V-HINT Review Conceptual Example 3 before starting this prob- lem. The amplitude of a transverse wave on a string is 4.5 cm. The ratio of the maximum particle speed to the speed of the wave is 3.1. What is the wavelength (in cm) of the wave? 21. M CHALK The drawing shows a frictionless incline and pulley. The two blocks are connected by a wire (mass per unit length = 0.0250 kg/m) and remain stationary. A transverse wave on the wire has a speed of 75.0 m/s. Neglecting the weight of the wire relative to the tension in the wire, fi nd the masses m1 and m2 of the blocks.
PROBLEM 21 30.0°
m1
m2
460 CHAPTER 16 Waves and Sound
22. H Available in WileyPLUS. 23. H The drawing shows a 15.0-kg ball being whirled in a circular path on the end of a string. The motion occurs on a frictionless, horizontal table. The angular speed of the ball is 𝜔 = 12.0 rad/s. The string has a mass of 0.0230 kg. How much time does it take for a wave on the string to travel from the center of the circle to the ball?
PROBLEM 23
String
Ball
Section 16.4 The Mathematical Description of a Wave (Note: The phase angles (2𝜋ft − 2𝜋x/𝜆) and (2𝜋ft + 2𝜋x/𝜆) are measured in radians, not degrees.) 24. E GO A wave traveling along the x axis is described mathematically by the equation y = 0.17 sin (8.2𝜋t + 0.54𝜋x), where y is the displacement (in meters), t is in seconds, and x is in meters. What is the speed of the wave? 25. E V-HINT A wave has the following properties: amplitude = 0.37 m, period = 0.77 s, wave speed = 12 m/s. The wave is traveling in the −x direction. What is the mathematical expression (similar to Equation 16.3 or 16.4) for the wave?
26. E The drawing shows a graph that represents a transverse wave on a string. The wave is moving in the +x direction with a speed of 0.15 m/s. Using the information contained in the graph, write the mathematical expres- sion (similar to Equation 16.3 or 16.4) for the wave.
PROBLEM 26
0.10 0.30 0.20
– 0.010
+ 0.010
0.40
At x = 0 m
t (s)
y (m)
27. E SSM A wave traveling in the +x direction has an amplitude of 0.35 m, a speed of 5.2 m/s, and a frequency of 14 Hz. Write the equation of the wave in the form given by either Equation 16.3 or 16.4.
28. M GO A transverse wave is traveling on a string. The displacement y of a particle from its equilibrium position is given by y = (0.021 m) sin (25t − 2.0 x). Note that the phase angle 25t − 2.0x is in radians, t is in seconds, and x is in meters. The linear density of the string is 1.6 × 10−2 kg/m. What is the tension in the string?
29. M SSM The tension in a string is 15 N, and its linear density is 0.85 kg/m. A wave on the string travels toward the −x direction; it has an amplitude of 3.6 cm and a frequency of 12 Hz. What are the (a) speed and (b) wavelength of the wave? (c) Write down a mathematical expression (like Equation 16.3 or 16.4) for the wave, substituting numbers for the variables A, f, and 𝜆. 30. H A transverse wave on a string has an amplitude of 0.20 m and a fre- quency of 175 Hz. Consider the particle of the string at x = 0 m. It begins with a displacement of y = 0 m when t = 0 s, according to Equation 16.3 or 16.4. How much time passes between the fi rst two instants when this particle has a displacement of y = 0.10 m?
Section 16.5 The Nature of Sound,
Section 16.6 The Speed of Sound 31. E SSM For research purposes a sonic buoy is tethered to the ocean fl oor and emits an infrasonic pulse of sound (speed = 1522 m/s). The period of this sound is 71 ms. Determine the wavelength of the sound.
32. E To navigate, a porpoise emits a sound wave that has a wavelength of 1.5 cm. The speed at which the wave travels in seawater is 1522 m/s. Find the period of the wave.
33. E MMH At what temperature is the speed of sound in helium (ideal gas, 𝛾 = 1.67, atomic mass = 4.003 u) the same as its speed in oxygen at 0 °C?
34. E Have you ever listened for an approaching train by kneeling next to a railroad track and putting your ear to the rail? Young’s modulus for steel is Y = 2.0 × 1011 N/m2, and the density of steel is 𝜌 = 7860 kg/m3. On a day when the temperature is 20 °C, how many times greater is the speed of sound in the rail than in the air?
35. E SSM The speed of a sound in a container of hydrogen at 201 K is 1220 m/s. What would be the speed of sound if the temperature were raised to 405 K? Assume that hydrogen behaves like an ideal gas.
36. E GO Suppose you are part of a team that is trying to break the sound barrier with a jet-powered car, which means that it must travel faster than the speed of sound in air. In the morning, the air temperature is 0 °C, and the speed of sound is 331 m/s. What speed must your car exceed if it is to break the sound barrier when the temperature has risen to 43 °C in the afternoon? Assume that air behaves like an ideal gas.
37. E As the drawing illustrates, a siren can be made by blowing a jet of air through 20 equally spaced holes in a rotating disk. The time it takes for successive holes to move past the air jet is the period of the sound. The siren is to produce a 2200-Hz tone. What must be the angular speed 𝜔 (in rad/s) of the disk?
PROBLEM 37
Air j et
38. E At a height of ten meters above the surface of a freshwater lake, a sound pulse is generated. The echo from the bottom of the lake returns to the point of origin 0.110 s later. The air and water temperature are 20 °C. How deep is the lake?
39. E An observer stands 25 m behind a marksman practicing at a rifl e range. The marksman fi res the rifl e horizontally, the speed of the bullets is 840 m/s, and the air temperature is 20 °C. How far does each bullet travel before the observer hears the report of the rifl e? Assume that the bullets en- counter no obstacles during this interval, and ignore both air resistance and the vertical component of the bullets’ motion.
40. E GO An ultrasonic ruler, such as the one discussed in Example 4 in Section 16.6, displays the distance between the ruler and an object, such as a wall. The ruler sends out a pulse of ultrasonic sound and measures the time it takes for the pulse to refl ect from the object and return. The ruler uses this time, along with a preset value for the speed of sound in air, to determine the distance. Suppose that you use this ruler under water, rather than in air. The actual distance from the ultrasonic ruler to an object is 25.0 m. The adiabatic bulk modulus and density of seawater are Bad = 2.37 × 109 Pa and 𝜌 = 1025 kg/ m3, respectively. Assume that the ruler uses a preset value of 343 m/s for the speed of sound in air. Determine the distance reading that the ruler displays.
41. E An explosion occurs at the end of a pier. The sound reaches the other end of the pier by traveling through three media: air, fresh water, and a slender metal handrail. The speeds of sound in air, water, and the handrail are 343, 1482, and 5040 m/s, respectively. The sound travels a distance of 125 m in each medium. (a) Through which medium does the sound arrive fi rst, second, and third? (b) After the fi rst sound arrives, how much later do the second and third sounds arrive?
42. M V-HINT A sound wave travels twice as far in neon (Ne) as it does in krypton (Kr) in the same time interval. Both neon and krypton can be treated
Problems 461
as monatomic ideal gases. The atomic mass of neon is 20.2 u, and the atomic mass of krypton is 83.8 u. The temperature of the krypton is 293 K. What is the temperature of the neon?
43. M SSM A hunter is standing on fl at ground between two vertical cliff s that are directly opposite one another. He is closer to one cliff than to the other. He fi res a gun and, after a while, hears three echoes. The second echo arrives 1.6 s after the fi rst, and the third echo arrives 1.1 s after the second. Assuming that the speed of sound is 343 m/s and that there are no refl ections of sound from the ground, fi nd the distance between the cliff s.
44. M GO A monatomic ideal gas (𝛾 = 1.67) is contained within a box whose volume is 2.5 m3. The pressure of the gas is 3.5 × 105 Pa. The total mass of the gas is 2.3 kg. Find the speed of sound in the gas.
45. M V-HINT A long slender bar is made from an unknown material. The length of the bar is 0.83 m, its cross-sectional area is 1.3 × 10−4 m2, and its mass is 2.1 kg. A sound wave travels from one end of the bar to the other end in 1.9 × 10−4 s. From which one of the materials listed in Table 10.1 is the bar most likely to be made?
46. M CHALK As the drawing shows, one microphone is located at the ori- gin, and a second microphone is located on the +y axis. The microphones are separated by a distance of D = 1.50 m. A source of sound is located on the +x axis, its distances from microphones 1 and 2 being L1 and L2, respectively. The speed of sound is 343 m/s. The sound reaches microphone 1 fi rst, and then, 1.46 ms later, it reaches microphone 2. Find the distances L1 and L2.
L1
D L2
+x
+y
Sound source
Microphone 2
Microphone 1
PROBLEM 46
47. M SSM When an earthquake occurs, two types of sound waves are gen- erated and travel through the earth. The primary, or P, wave has a speed of about 8.0 km/s and the secondary, or S, wave has a speed of about 4.5 km/s. A seismograph, located some distance away, records the arrival of the P wave and then, 78 s later, records the arrival of the S wave. Assuming that the waves travel in a straight line, how far is the seismograph from the earthquake?
48. M V-HINT Consult Multiple-Concept Example 4 in order to review a model for solving this type of problem. Suppose that you are standing by the side of a road in the Sahara desert where the temperature has reached a hot 56 °C (130 °F). A truck, traveling at a constant speed, passes by. After 4.00 s have elapsed, you use the ultrasonic ruler discussed in Example 4 to measure the distance to the truck. A sound pulse leaves the ultrasonic ruler and returns 0.120 s later. Assume that the average molecular mass of air is 28.9 u, air is an ideal diatomic gas (γ = 75 ), and the truck moves a negligible distance in the time it takes for the sound pulse to reach it. Determine how fast the truck is moving.
49. H Available in WileyPLUS. 50. H Available in WileyPLUS. 51. H SSM Available in WileyPLUS.
Section 16.7 Sound Intensity 52. E BIO A typical adult ear has a surface area of 2.1 × 10−3 m2. The sound intensity during a normal conversation is about 3.2 × 10−6 W/m2 at the
listener’s ear. Assume that the sound strikes the surface of the ear perpendic- ularly. How much power is intercepted by the ear?
53. E SSM At a distance of 3.8 m from a siren, the sound intensity is 3.6 × 10−2 W/m2. Assuming that the siren radiates sound uniformly in all direc- tions, fi nd the total power radiated.
54. E GO A source of sound is located at the center of two concentric spheres, parts of which are shown in the drawing. The source emits sound uniformly in all directions. On the spheres are drawn three small patches that may or may not have equal areas. However, the same sound power passes through each patch. The source produces 2.3 W of sound power, and the radii of the concentric spheres are rA = 0.60 m and rB = 0.80 m. (a) Determine the sound intensity at each of the three patches. (b) The sound power that passes through each of the patches is 1.8 × 10−3 W. Find the area of each patch.
PROBLEM 54
Patch 3 Patch 2
Patch 1
Source of sound
rA
rB
55. E Available in WileyPLUS. 56. E Suppose that a public address system emits sound uniformly in all directions and that there are no refl ections. The intensity at a location 22 m away from the sound source is 3.0 × 10−4 W/m2. What is the intensity at a spot that is 78 m away?
57. E SSM A loudspeaker has a circular opening with a radius of 0.0950 m. The electrical power needed to operate the speaker is 25.0 W. The average sound intensity at the opening is 17.5 W/m2. What percentage of the elec- trical power is converted by the speaker into sound power?
58. E GO A man stands at the midpoint between two speakers that are broadcasting an amplifi ed static hiss uniformly in all directions. The speakers are 30.0 m apart and the total power of the sound coming from each speaker is 0.500 W. Find the total sound intensity that the man hears (a) when he is at his initial position halfway between the speakers, and (b) after he has walked 4.0 m directly toward one of the speakers.
59. M SSM MMH A dish of lasagna is being heated in a microwave oven. The eff ective area of the lasagna that is exposed to the microwaves is 2.2 × 10−2 m2. The mass of the lasagna is 0.35 kg, and its specifi c heat capacity is 3200 J/(kg · C°). The temperature rises by 72 °C in 8.0 minutes. What is the intensity of the microwaves in the oven?
60. M GO Two sources of sound are located on the x axis, and each emits power uniformly in all directions. There are no refl ections. One source is positioned at the origin and the other at x = +123 m. The source at the origin emits four times as much power as the other source. Where on the x axis are the two sounds equal in intensity? Note that there are two answers.
61. M BIO V-HINT Deep ultrasonic heating is used to promote healing of torn tendons. It is produced by applying ultrasonic sound over the aff ected area of the body. The sound transducer (generator) is circular with a radius of 1.8 cm, and it produces a sound intensity of 5.9 × 103 W/m2. How much time is required for the transducer to emit 4800 J of sound energy?
62. H Available in WileyPLUS.
462 CHAPTER 16 Waves and Sound
Section 16.8 Decibels 63. E A woman stands a distance d from a loud motor that emits sound uniformly in all directions. The sound intensity at her position is an uncom- fortable 3.2 × 10−3 W/m2. There are no refl ections. At a position twice as far from the motor, what are (a) the sound intensity and (b) the sound intensity level relative to the threshold of hearing?
64. E The volume control on a surround-sound amplifi er is adjusted so the sound intensity level at the listening position increases from 23 to 61 dB. What is the ratio of the fi nal sound intensity to the original sound intensity?
65. E BIO SSM A middle-aged man typically has poorer hearing than a middle-aged woman. In one case a woman can just begin to hear a musical tone, while a man can just begin to hear the tone only when its intensity level is increased by 7.8 dB relative to the just-audible intensity level for the woman. What is the ratio of the sound intensity just detected by the man to the sound intensity just detected by the woman?
66. E GO Using an intensity of 1 × 10−12 W/m2 as a reference, the threshold of hearing for an average young person is 0 dB. Person 1 and person 2, who are not average, have thresholds of hearing that are 𝛽1 = −8.00 dB and 𝛽2 = +12.0 dB. What is the ratio I1/I2 of the sound intensity I1 when person 1 hears the sound at his own threshold of hearing compared to the sound intensity I2 when person 2 hears the sound at his own threshold of hearing?
67. E A listener doubles his distance from a source that emits sound uni- formly in all directions. There are no refl ections. By how many decibels does the sound intensity level change?
68. E Sound is passing perpendicularly through an open window whose dimensions are 1.1 m × 0.75 m. The sound intensity level is 95 dB above the threshold of hearing. How much sound energy comes through the window in one hour?
69. E The bellow of a territorial bull hippopotamus has been measured at 115 dB above the threshold of hearing. What is the sound intensity?
70. E BIO V-HINT Hearing damage may occur when a person is exposed to a sound intensity level of 90.0 dB (relative to the threshold of hearing) for a period of 9.0 hours. One particular eardrum has an area of 2.0 × 10−4 m2. How much sound energy is incident on this eardrum during this time?
71. M CHALK SSM When one person shouts at a football game, the sound intensity level at the center of the fi eld is 60.0 dB. When all the people shout together, the intensity level increases to 109 dB. Assuming that each per- son generates the same sound intensity at the center of the fi eld, how many people are at the game?
72. M GO Review Conceptual Example 8 as background for this problem. A loudspeaker is generating sound in a room. At a certain point, the sound waves coming directly from the speaker (without refl ecting from the walls) create an intensity level of 75.0 dB. The waves refl ected from the walls create, by themselves, an intensity level of 72.0 dB at the same point. What is the total intensity level? (Hint: The answer is not 147.0 dB.) 73. M V-HINT A portable radio is sitting at the edge of a balcony 5.1 m above the ground. The unit is emitting sound uniformly in all directions. By acci- dent, it falls from rest off the balcony and continues to play on the way down. A gardener is working in a fl ower bed directly below the falling unit. From the instant the unit begins to fall, how much time is required for the sound intensity level heard by the gardener to increase by 10.0 dB?
74. H Available in WileyPLUS. 75. H SSM Available in WileyPLUS.
Section 16.9 The Doppler Eff ect 76. E A bird is fl ying directly toward a stationary bird-watcher and emits a frequency of 1250 Hz. The bird-watcher, however, hears a frequency of
1290 Hz. What is the speed of the bird, expressed as a percentage of the speed of sound?
77. E SSM From a vantage point very close to the track at a stock car race, you hear the sound emitted by a moving car. You detect a frequency that is 0.86 times as small as the frequency emitted by the car when it is stationary. The speed of sound is 343 m/s. What is the speed of the car?
78. E Dolphins emit clicks of sound for communication and echolocation. A marine biologist is monitoring a dolphin swimming in seawater where the speed of sound is 1522 m/s. When the dolphin is swimming directly away at 8.0 m/s, the marine biologist measures the number of clicks occurring per second to be at a frequency of 2500 Hz. What is the diff erence (in Hz) between this frequency and the number of clicks per second actually emitted by the dolphin?
79. E MMH A convertible moves toward you and then passes you; all the while, its loudspeakers are producing a sound. The speed of the car is a con- stant 9.00 m/s, and the speed of sound is 343 m/s. What is the ratio of the frequency you hear while the car is approaching to the frequency you hear while the car is moving away?
80. E The security alarm on a parked car goes off and produces a frequency of 960 Hz. The speed of sound is 343 m/s. As you drive toward this parked car, pass it, and drive away, you observe the frequency to change by 95 Hz. At what speed are you driving?
81. M V-HINT A car is parked 20.0 m directly south of a railroad crossing. A train is approaching the crossing from the west, headed directly east at a speed of 55.0 m/s. The train sounds a short blast of its 289-Hz horn when it reaches a point 20.0 m west of the crossing. What frequency does the car’s driver hear when the horn blast reaches the car? The speed of sound in air is 343 m/s. (Hint: Assume that only the component of the train’s velocity that is directed toward the car aff ects the frequency heard by the driver.) 82. M GO A loudspeaker in a parked car is producing sound whose frequency is 20 510 Hz. A healthy young person with normal hearing is standing nearby on the sidewalk but cannot hear the sound because the frequency is too high. When the car is moving, however, this person can hear the sound. (a) Is the car moving toward or away from the person? Why? (b) If the speed of sound is 343 m/s, what is the minimum speed of the moving car?
83. M SSM MMH Two trucks travel at the same speed. They are far apart on adjacent lanes and approach each other essentially head-on. One driver hears the horn of the other truck at a frequency that is 1.14 times the frequency he hears when the trucks are stationary. The speed of sound is 343 m/s. At what speed is each truck moving?
84. M GO A wireless transmitting microphone is mounted on a small plat- form that can roll down an incline, directly away from a loudspeaker that is mounted at the top of the incline. The loudspeaker broadcasts a tone that has a fi xed frequency of 1.000 × 104 Hz, and the speed of sound is 343 m/s. At a time of 1.5 s following the release of the platform, the microphone detects a frequency of 9939 Hz. At a time of 3.5 s following the release of the platform, the microphone detects a frequency of 9857 Hz. What is the acceleration (assumed constant) of the platform?
85. M V-HINT A car is accelerating while its horn is sounding. Just after the car passes a stationary person, the person hears a frequency of 966.0 Hz. Fourteen seconds later, the frequency heard by the person has decreased to 912.0 Hz. When the car is stationary, its horn emits a sound whose frequency is 1.00 × 103 Hz. The speed of sound is 343 m/s. What is the acceleration of the car?
86. M GO The siren on an ambulance is emitting a sound whose frequency is 2450 Hz. The speed of sound is 343 m/s. (a) If the ambulance is stationary and you (the “observer”) are sitting in a parked car, what are the wavelength and the frequency of the sound you hear? (b) Suppose that the ambulance is
Additional Problems 463
moving toward you at a speed of 26.8 m/s. Determine the wavelength and the frequency of the sound you hear. (c) If the ambulance is moving toward you at a speed of 26.8 m/s and you are moving toward it at a speed of 14.0 m/s, fi nd the wavelength and frequency of the sound you hear.
87. M SSM Two submarines are under water and approaching each other head-on. Sub A has a speed of 12 m/s and sub B has a speed of 8 m/s. Sub A
sends out a 1550-Hz sonar wave that travels at a speed of 1522 m/s. (a) What is the frequency detected by sub B? (b) Part of the sonar wave is refl ected from sub B and returns to sub A. What frequency does sub A detect for this refl ected wave?
88. H Available in WileyPLUS.
89. E A recording engineer works in a soundproofed room that is 44.0 dB quieter than the outside. If the sound intensity that leaks into the room is 1.20 × 10−10 W/m2, what is the intensity outside?
90. E Available in WileyPLUS. 91. E SSM Available in WileyPLUS. 92. E You are fl ying in an ultralight aircraft at a speed of 39 m/s. An eagle, whose speed is 18 m/s, is fl ying directly toward you. Each of the given speeds is relative to the ground. The eagle emits a shrill cry whose frequency is 3400 Hz. The speed of sound is 330 m/s. What frequency do you hear?
93. E SSM Suppose that the linear density of the A string on a violin is 7.8 × 10−4 kg/m. A wave on the string has a frequency of 440 Hz and a wavelength of 65 cm. What is the tension in the string?
94. E A car driving along a highway at a speed of 23 m/s strays onto the shoulder. Evenly spaced parallel grooves called “rumble strips” are carved into the pavement of the shoulder. Rolling over the rumble strips causes the car’s wheels to oscillate up and down at a frequency of 82 Hz. How far apart are the centers of adjacent rumble-strip grooves?
95. E SSM When Gloria wears her hearing aid, the sound intensity level increases by 30.0 dB. By what factor does the sound intensity increase?
96. E The average sound intensity inside a busy neighborhood restaurant is 3.2 × 10−5 W/m2. How much energy goes into each ear (area = 2.1 × 10−3 m2) during a one-hour meal?
97. E SSM Suppose that the amplitude and frequency of the transverse wave in Interactive Figure 16.2c are, respectively, 1.3 cm and 5.0 Hz. Find the total vertical distance (in cm) through which the colored dot moves in 3.0 s. 98. E A bat emits a sound whose frequency is 91 kHz. The speed of sound in air at 20.0 °C is 343 m/s. However, the air temperature is 35 °C, so the speed of sound is not 343 m/s. Assume that air behaves like an ideal gas, and fi nd the wavelength of the sound.
99. E SSM You are riding your bicycle directly away from a stationary source of sound and hear a frequency that is 1.0% lower than the emitted frequency. The speed of sound is 343 m/s. What is your speed?
100. E GO Argon (molecular mass = 39.9 u) is a monatomic gas. Assum- ing that it behaves like an ideal gas at 298 K (𝛾 = 1.67), fi nd (a) the rms speed of argon atoms and (b) the speed of sound in argon. 101. E SSM The sound intensity level at a rock concert is 115 dB, while that at a jazz fest is 95 dB. Determine the ratio of the sound intensity at the rock concert to the sound intensity at the jazz fest.
102. E An amplifi ed guitar has a sound intensity level that is 14 dB greater than the same unamplifi ed sound. What is the ratio of the amplifi ed intensity to the unamplifi ed intensity?
103. M In a discussion person A is talking 1.5 dB louder than person B, and person C is talking 2.7 dB louder than person A. What is the ratio of the sound intensity of person C to the sound intensity of person B?
104. M In Interactive Figure 16.3c the colored dot exhibits simple harmonic motion as the longitudinal wave passes. The wave has an amplitude of 5.4 × 10−3 m and a frequency of 4.0 Hz. Find the maximum acceleration of the dot.
105. M GO (a) A uniform rope of mass m and length L is hanging straight down from the ceiling. A small-amplitude transverse wave is sent up the rope from the bottom end. Derive an expression that gives the speed 𝜐 of the wave on the rope in terms of the distance y above the bottom end of the rope and the magnitude g of the acceleration due to gravity. (b) Use the expression that you have derived to calculate the speeds at distances of 0.50 m and 2.0 m above the bottom end of the rope.
106. M V-HINT A spider hangs from a strand of silk whose radius is 4.0 × 10−6 m. The density of the silk is 1300 kg/m3. When the spider moves, waves travel along the strand of silk at a speed of 280 m/s. Ignore the mass of the silk strand, and determine the mass of the spider.
107. M SSM Available in WileyPLUS. 108. M V-HINT A member of an aircraft maintenance crew wears protective earplugs that reduce the sound intensity by a factor of 350. When a jet aircraft is taking off , the sound intensity level experienced by the crew member is 88 dB. What sound intensity level would the crew member experience if he removed the protective earplugs?
109. H Available in WileyPLUS. 110. H Available in WileyPLUS. 111. M GO SSM A speedboat, starting from rest, moves along a straight line away from a dock. The boat has a constant acceleration of +3.00 m/s2 (see the fi gure). Attached to the dock is a siren that is producing a 755-Hz tone. If the air temperature is 20 °C, what is the frequency of the sound heard by a person on the boat when the boat’s displacement from the dock is +45.0 m?
+3.00 m/s2
+x
+45.0 m
Siren
PROBLEM 111
Additional Problems
464 CHAPTER 16 Waves and Sound
114. M Setting Safety Parameters. You and your team are asked to de- termine the hearing safety parameters for a loud experiment. Since the sound will persist for only a short time, the allowed intensity level that will not result in permanent hearing damage is 135 dB. The experiment consists of a single source with a power output of 550 W that projects sound isotropically (i.e., uniformly in all directions). (a) At what distance should you set the safety perimeter (i.e., the radius of a sphere in meters) centered at the source? (b) Where should you set the perimeter if the power of the source doubles? 115. M A Mysterious Underwater Object. You and your team are on a reconnaissance mission in a submarine exploring a mysterious object in the cold waters of the Weddell Sea, off the coast of Antarctica. The sonar
indicates that the object, which had otherwise been moving erratically, has changed course and is now on a direct collision course with your sub. The captain issues an “all stop” order, bringing the sub to a halt relative to the water. The sonar operator “pings” the object, which amounts to sending a short blast of sound in the direction of the object. The emitted sound wave has a frequency of 1550 Hz and a speed of 1552 m/s (the speed of sound in seawater). The sound refl ects from the object and returns 2.582 s after it was emitted from your sub, and its frequency has shifted to 1598 Hz. (a) How far from the sub was the object when the sound refl ected from it? (b) What is the object’s speed? (c) How long after you receive the return signal will it take the object to reach your submarine?
Team Problems
One of the most important concepts we encountered in this chapter is the transverse wave. For instance, transverse waves travel along a guitar string when it is plucked or along a violin string when it is bowed. Problem 112 reviews how the travel speed depends on the properties of the string and on the tension in it. Problem 113 illustrates how the Doppler eff ect arises when an observer is moving away from or toward a stationary source of sound. In fact, we will see that it’s possible for both situations to occur at the same time.
112. M CHALK The fi gure shows waves traveling on two strings. Each string is attached to a wall at one end and to a box that has a weight of 28.0 N at the other end. String 1 has a mass of 8.00 g and a length of 4.00 cm, and string 2 has a mass of 12.0 g and a length of 8.00 cm. Concepts: (i) Is the tension the same in each string? (ii) Is the speed of each wave the same? (iii) String 1 has a smaller mass and, hence, less inertia than string 2. Does this mean that the speed of the wave on string 1 is greater than the speed on string 2? Calculations: Determine the speed of the wave on each string.
PROBLEM 112 28.0 N String 1 String 2
113. M CHALK SSM A siren, mounted on a tower, emits a sound whose frequency is 2140 Hz. A person is driving a car away from the tower at a speed of 27.0 m/s. As the fi gure illustrates, the sound reaches the person by two paths: the sound refl ected from the building in front of the car, and the sound coming directly from the siren. The speed of sound is 343 m/s. Concepts: (i) One way that the Doppler eff ect can arise is that the wavelength of the sound changes. For either the direct or refl ected sound, does the wavelength change? (ii) Why does the driver hear a frequency for the refl ected sound that is diff erent from 2140 Hz, and is it greater or smaller than 2140 Hz? (iii) Why does the driver hear a frequency for the direct sound that is diff erent from 2140 Hz, and is it greater or smaller than 2140 Hz? Calculations: What frequency does the person hear for the (a) refl ected and (b) direct sound?
Direct Reflected
PROBLEM 113
Concepts and Calculations Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
17.1 Express the principle of linear superposition.
17.2 Solve spatial interference problems for sound waves.
17.3 Apply wave interference concepts to the diff raction of sound waves.
17.4 Explain beats as a wave interference phenomenon.
17.5 Analyze transverse standing waves.
17.6 Analyze longitudinal standing waves.
17.7 Define the harmonic content of complex sound waves.
Ja m
ie S
q u ir
e/ A
L L
S P
O R
T /G
et ty
I m
ag es
CHAPTER 17
The Principle of Linear Superposition and Interference Phenomena
This performer is playing a wind instrument known as a didgeridoo, which is thought to have originated
in northern Australia at least 1500 years ago and has been likened to a natural wooden trumpet. The
didgeridoo and virtually all musical instruments produce sound in a way that involves the principle of
linear superposition. All of the topics in this chapter are related to this principle.
17.1 The Principle of Linear Superposition Often, two or more sound waves are present at the same place at the same time, as is
the case with sound waves when everyone is talking at a party or when music plays
from the speakers of a stereo system. To illustrate what happens when several waves
pass simultaneously through the same region, let’s consider Animated Figures 17.1 and 17.2, which show two transverse pulses of equal heights moving toward each other along a Slinky. In Animated Figure 17.1 both pulses are “up,” whereas in Animated Figure 17.2 one is “up” and the other is “down.” Part a of each fi gure shows the two pulses beginning to overlap. The pulses merge, and the Slinky assumes a shape that is
the sum of the shapes of the individual pulses. Thus, when the two “up” pulses overlap 465
466 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
completely, as in Animated Figure 17.1b, the Slinky has a pulse height that is twice the height of an individual pulse. Likewise, when the “up” pulse and the “down” pulse overlap exactly, as
in Animated Figure 17.2b, they momentarily cancel, and the Slinky becomes straight. In either case, the two pulses move apart after overlapping, and the Slinky once again conforms to the
shapes of the individual pulses, as in part c of both fi gures. The adding together of individual pulses to form a resultant pulse is an example of a more
general concept called the principle of linear superposition.
THE PRINCIPLE OF LINEAR SUPERPOSITION When two or more waves are present simultaneously at the same place, the resultant disturbance is the sum of the disturbances from the individual waves.
This principle can be applied to all types of waves, including sound waves, water waves, and
electromagnetic waves such as light, radio waves, and microwaves. It embodies one of the most
important concepts in physics, and the remainder of this chapter deals with examples related to it.
Check Your Understanding
(The answer is given at the end of the book.) 1. CYU Figure 17.1 shows a graph of two pulses traveling toward each other at t = 0 s. Each pulse has
a constant speed of 1 cm/s. When t = 2 s, what is the height of the resultant pulse at (a) x = 3 cm and (b) x = 4 cm?
+2 cm
+1 cm
0
–1 cm
–2 cm
–3 cm
–4 cm 1 2 3
Distance x, cm
4 5 6 7 8 9
1 cm/s
1 cm/s
CYU FIGURE 17.1
17.2 Constructive and Destructive Interference of Sound Waves Suppose that the sounds from two speakers overlap in the middle of a listening area, as in
Interactive Figure 17.3, and that each speaker produces a sound wave of the same amplitude and frequency. For convenience, the wavelength of the sound is chosen to be 𝜆 = 1 m. In addition, assume that the diaphragms of the speakers vibrate in phase; that is, they move outward together and inward
together. If the distance of each speaker from the overlap point is the same (3 m in the drawing), the
condensations (C) of one wave always meet the condensations of the other when the waves come
together; similarly, rarefactions (R) always meet rarefactions. According to the principle of linear
superposition, the combined pattern is the sum of the individual patterns. As a result, the pressure
fl uctuations at the overlap point have twice the amplitude A that the individual waves have, and a listener at this spot hears a louder sound than the sound coming from either speaker alone. When two
waves always meet condensation-to-condensation and rarefaction-to-rarefaction (or crest-to-crest
and trough-to-trough), they are said to be exactly in phase and to exhibit constructive interference.
(a) Overlap begins
(b) Total overlap; the Slinky has twice the height of either pulse
(c) The receding pulses
ANIMATED FIGURE 17.1 Two transverse “up” pulses passing through each other.
(a) Overlap begins
(b) Total overlap
(c) The receding pulses
ANIMATED FIGURE 17.2 Two transverse pulses, one “up” and one “down,” passing
through each other.
17.2 Constructive and Destructive Interference of Sound Waves 467
Now consider what happens if one of the speakers is moved. The result is surprising. In
Interactive Figure 17.4, the left speaker is moved away* from the overlap point by a distance equal to one-half of the wavelength, or 0.5 m. Therefore, at the overlap point, a condensation
arriving from the left meets a rarefaction arriving from the right. Likewise, a rarefaction arriving
from the left meets a condensation arriving from the right. According to the principle of linear
superposition, the net eff ect is a mutual cancellation of the two waves. The condensations from
one wave off set the rarefactions from the other, leaving only a constant air pressure. A constant air pressure, devoid of condensations and rarefactions, means that a listener detects no sound.
When two waves always meet condensation-to-rarefaction (or crest-to-trough), they are said to
be exactly out of phase and to exhibit destructive interference. When two waves meet, they interfere constructively if they always meet exactly in phase and
destructively if they always meet exactly out of phase. In either case, this means that the wave
patterns do not shift relative to one another as time passes. Sources that produce waves in this
fashion are called coherent sources. THE PHYSICS OF . . . noise-canceling headphones. Destructive interference is the
basis of a useful technique for reducing the loudness of undesirable sounds. For instance,
Figure 17.5 shows a pair of noise-canceling headphones. Small microphones are mounted inside the headphones and detect noise such as the engine noise that an airplane pilot would hear. The
headphones also contain circuitry to process the electronic signals from the microphones and
reproduce the noise in a form that is exactly out of phase compared to the original. This out-of-
phase version is played back through the headphone speakers and, because of destructive interfer-
ence, combines with the original noise to produce a quieter background.
If the left speaker in Interactive Figure 17.4 were moved away from the overlap point by another one-half wavelength (312 m +
1
2 m = 4 m), the two waves would again be in phase, and
constructive interference would occur. The listener would hear a loud sound because the left wave
travels one whole wavelength (𝜆 = 1 m) farther than the right wave and, at the overlap point, con-
densation meets condensation and rarefaction meets rarefaction. In general, the important issue is
the diff erence in the path lengths traveled by each wave in reaching the overlap point:
3 m
3 m
C R
C R
Receiver
Constructive interference
A Pressure
Time
Pressure
Time
A
2A
+ =
INTERACTIVE FIGURE 17.3 The speakers in this drawing vibrate in phase. As a result
of constructive interference between the two
sound waves (amplitude = A), a loud sound (amplitude = 2A) is heard at an overlap point located equally distant from two in-phase
speakers (C, condensation; R, rarefaction).
*When the left speaker is moved back, its sound intensity and, hence, its pressure amplitude decrease at the overlap
point. In this chapter assume that the power delivered to the left speaker by the receiver is increased slightly to keep the
amplitudes equal at the overlap point.
Destructive interference
A Pressure
Time
A
+ =3 m
3 m C
C R
C R
Receiver
1–2
INTERACTIVE FIGURE 17.4 The speakers in this drawing vibrate in phase. However,
the left speaker is one-half of a wavelength
( 1
2 m) farther from the overlap point than
the right speaker. Because of destructive
interference, no sound is heard at the overlap
point (C, condensation; R, rarefaction).
468 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
Problem-Solving Insight For two wave sources vibrating in phase, a diff erence in path lengths that is zero or an integer number (1, 2, 3, . . .) of wavelengths leads to constructive
interference; a diff erence in path lengths that is a half-integer number ( 1
2, 1 1
2 , 2 1
2 , . . .) of
wavelengths leads to destructive interference.
Problem-Solving Insight For two wave sources vibrating out of phase, a diff erence in path lengths that is a half-integer number (
1
2, 1 1
2 , 2 1
2 , . . .) of wavelengths leads to constructive
interference; a diff erence in path lengths that is zero or an integer number (1, 2, 3, . . .) of
wavelengths leads to destructive interference.
Interference eff ects can also be detected if the two speakers are fi xed in position and the
listener moves about the room. Consider Figure 17.6, where the sound waves spread outward from each of two in-phase speakers, as indicated by the concentric circular arcs. Each solid arc
represents the middle of a condensation, and each dashed arc represents the middle of a rarefac-
tion. Where the two waves overlap, there are places of constructive interference and places of
destructive interference. Constructive interference occurs wherever two condensations or two
rarefactions intersect, and the drawing shows four such places as solid dots. A listener stationed at
any one of these locations hears a loud sound. On the other hand, destructive interference occurs
wherever a condensation and a rarefaction intersect, such as the two open dots in the picture. A
listener situated at a point of destructive interference hears no sound. At locations where neither
constructive nor destructive interference occurs, the two waves partially reinforce or partially
cancel, depending on the position relative to the speakers. Thus, it is possible for a listener to
walk about the overlap region and hear marked variations in loudness.
The individual sound waves from the speakers in Figure 17.6 carry energy, and the energy delivered to the overlap region is the sum of the energies of the individual waves. This
fact is consistent with the principle of conservation of energy, which we fi rst encountered in
Section 6.8. This principle states that energy can neither be created nor destroyed, but can only
be converted from one form to another. One of the interesting consequences of interference is
that the energy is redistributed, so there are places within the overlap region where the sound
is loud and other places where there is no sound at all. Interference, so to speak, “robs Peter to
pay Paul,” but energy is always conserved in the process. Example 1 illustrates how to decide
what a listener hears.
FIGURE 17.5 Noise-canceling headphones utilize destructive interference.
Noise
Noise
Speaker
Microphone
Electronic circuitry
Out-of-phase noise
Reduced noise level
1 w avel
engt h
R
C
R
C
R
C
FIGURE 17.6 Two sound waves overlap in the shaded region. The solid lines denote
the middle of the condensations (C), and
the dashed lines denote the middle of the
rarefactions (R). Constructive interference
occurs at each solid dot (●) and destructive
interference at each open dot ( ).
EXAMPLE 1 What Does a Listener Hear?
In Figure 17.7 two in-phase loudspeakers, A and B, are separated by 3.20 m. A listener is stationed at point C, which is 2.40 m in front of speaker B.
The triangle ABC is a right triangle. Both speakers are playing identical 214-Hz tones, and the speed of sound is 343 m/s. Does the listener hear a
loud sound or no sound?
Reasoning The listener will hear either a loud sound or no sound, depending on whether the interference occurring at point C is construc-
tive or destructive. To determine which it is, we need to fi nd the diff er-
ence in the distances traveled by the two sound waves that reach point C
and see whether the diff erence is an integer or half-integer number of
17.2 Constructive and Destructive Interference of Sound Waves 469
Up to this point, we have been assuming that the speaker diaphragms vibrate synchronously,
or in phase; that is, they move outward together and inward together. This may not be the case,
however, and Conceptual Example 2 considers what happens then.
wavelengths. In either event, the wavelength can be found from the relation
𝜆 = 𝜐/f (Equation 16.1).
Problem-Solving Insight To decide whether two sources of sound produce constructive or destructive interference at a point, determine the diff erence in path lengths between each source and that point and compare it to the wavelength of the sound.
Solution Since the triangle ABC is a right triangle, the distance AC is given by the Pythagorean theorem as √(3.20 m)
2 + (2.40 m) 2 = 4.00 m.
The distance BC is given as 2.40 m. Thus, the diff erence in the travel dis-
tances for the waves is 4.00 m − 2.40 m = 1.60 m. The wavelength of
the sound is
λ = υ f
= 343 m /s
214 Hz = 1.60 m (16.1)
Since the diff erence in the distances is one wavelength, constructive inter-
ference occurs at point C, and the listener hears a loud sound.
3.20 m
2.40 m
C
90°
A B
FIGURE 17.7 Example 1 discusses whether this setup leads to constructive
or destructive interference at point C
for 214-Hz sound waves.
CONCEPTUAL EXAMPLE 2 Out-of-Phase Speakers
To make a speaker operate, two wires (one red and one black, for in-
stance) must be connected between the speaker and the receiver (am-
plifi er), as in Figure 17.8. Consider one of the speakers in Interactive Figure 17.4, where the red wire connects the red terminal of the speaker to the red terminal of the receiver. Similarly, the black wire connects the
black terminal of the speaker to the black terminal of the receiver. For
the other speaker, however, the wires connect a terminal of one color on
the speaker to a terminal of a diff erent color on the receiver. Since the two
speakers are not connected to the receiver in exactly the same way, the
two diaphragms will vibrate out of phase, one moving outward every time
the other moves inward, and vice versa. A listener at the overlap point in
Interactive Figure 17.4 would now hear (a) no sound because destructive interference occurs (b) a loud sound because constructive interference occurs.
Reasoning Since the speaker diaphragms in Interactive Figure 17.4 are now vibrating out of phase, one of them is moving exactly opposite to
the way it was moving originally; let us assume that it is the left speaker.
The eff ect of this change is that every condensation originating from
the left speaker becomes a rarefaction, and every rarefaction becomes a
condensation.
Answer (a) is incorrect. When the two speakers in Interactive Fig- ure 17.4 are wired in phase, a condensation from one speaker always meets a rarefaction from the other at the overlap point, and destructive
interference occurs. However, if one of the speakers were wired out of
phase relative to the other, a condensation from one speaker would meet
a condensation from the other, and destructive interference would not occur.
Answer (b) is correct. If the left speaker in Interactive Figure 17.4 were connected out of phase with respect to the right speaker, a condensa-
tion from the right speaker would meet a condensation (not a rarefaction)
from the left speaker at the overlap point. Similarly, a rarefaction from the
right speaker would meet a rarefaction from the left speaker. The result is
constructive interference, and a loud sound would be heard.
FIGURE 17.8 A loudspeaker is connected to a receiver (amplifi er) by two wires.
A n d y W
as h n ik
470 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
THE PHYSICS OF . . . wiring the speakers in an audio system. Instructions for con- necting stereo or surround-sound systems specifi cally warn owners to avoid out-of-phase vibra-
tion of speaker diaphragms. If the wires and the terminals of the speakers and the receiver are
not color-coded, you can check for problems in the following way. Play music with a lot of
low-frequency bass tones. Set the receiver to its monaural mode, so the same sound comes out
of both speakers being tested. If the diaphragms are in phase, the bass sound will either remain
the same or become slightly louder as you slide the speakers together. If the diaphragms are out
of phase, the bass sound will fade noticeably (due to destructive interference) when the speakers
are right next to each other. In this event, simply interchange the wires to the terminals on one
(not both) of the speakers.
The phenomena of constructive and destructive interference are exhibited by all types of
waves, not just sound waves. We will encounter interference eff ects again in Chapter 27, in con-
nection with light waves.
Check Your Understanding
(The answers are given at the end of the book.) 2. Does the principle of linear superposition imply that two sound waves, passing through the same place
at the same time, always create a louder sound than is created by either wave alone?
3. Suppose that you are sitting at the overlap point between the two speakers in Interactive Figure 17.4. Because of destructive interference, you hear no sound, even though both speakers are emitting identi-
cal sound waves. One of the speakers is suddenly shut off . Will you now hear a sound? (a) No. (b) Yes. (c) Yes, but only if you move a distance of one wavelength closer to the speaker that is still producing sound.
4. Starting at the overlap point in Interactive Figure 17.3, you walk along a straight path that is perpen- dicular to the line between the speakers and passes through the midpoint of that line. As you walk, the loudness of the sound (a) changes from loud to faint to loud (b) changes from faint to loud to faint (c) does not change.
5. Starting at the overlap point in Interactive Figure 17.3, you walk along a path that is parallel to the line between the speakers. As you walk, the loudness of the sound (a) changes from loud to faint to loud (b) changes from faint to loud to faint (c) does not change.
17.3 Diff raction Section 16.5 discusses the fact that sound is a pressure wave created by a vibrating object, such as
a loudspeaker. The previous two sections of this chapter have examined what happens when two
sound waves are present simultaneously at the same place; according to the principle of linear
superposition, a resultant disturbance is formed from the sum of the individual waves. This prin-
ciple reveals that overlapping sound waves exhibit interference eff ects, whereby the sound energy
is redistributed within the overlap region. We will now use the principle of linear superposition
to explore another interference eff ect, that of diff raction.
When a wave encounters an obstacle or the edges of an opening, it bends around them. For
instance, a sound wave produced by a stereo system bends around the edges of an open doorway,
as Figure 17.9a illustrates. If such bending did not occur, sound could be heard outside the room only at locations directly in front of the doorway, as part b of the drawing suggests. (It is assumed that no sound is transmitted directly through the walls.) The bending of a wave around an obstacle
or the edges of an opening is called diff raction. All kinds of waves exhibit diff raction. To demonstrate how the bending of waves arises, Figure 17.10 shows an expanded view
of Figure 17.9a. When the sound wave reaches the doorway, the air in the doorway is set into longitudinal vibration. In eff ect, each molecule of the air in the doorway becomes a source of a
sound wave in its own right, and, for purposes of illustration, the drawing shows two of the mol-
ecules. Each produces a sound wave that expands outward in three dimensions, much like a water
wave does in two dimensions when a stone is dropped into a pond. The sound waves generated
by all the molecules in the doorway must be added together to obtain the total sound wave at any
location outside the room, in accord with the principle of linear superposition. However, even
(a) With diffraction
(b) Without diffraction
FIGURE 17.9 (a) The bending of a sound wave around the edges of the doorway is an
example of diff raction. The source of the sound
within the room is not shown. (b) If diff raction did not occur, the sound wave would not bend
as it passed through the doorway.
17.3 Diff raction 471
considering only the waves from the two molecules in the picture, it is clear that the expanding
wave patterns reach locations off to either side of the doorway. The net eff ect is a “bending,” or
diff raction, of the sound around the edges of the opening. Further insight into the origin of dif-
fraction can be obtained with the aid of Huygens’ principle (see Section 27.5).
When the sound waves generated by every molecule in the doorway are added together, it
is found that there are places where the intensity is a maximum and places where it is zero, in a
fashion similar to that discussed in the previous section. Analysis shows that at a great distance
from the doorway the intensity is a maximum directly opposite the center of the opening. As the
distance to either side of the center increases, the intensity decreases and reaches zero, then rises
again to a maximum, falls again to zero, rises back to a maximum, and so on. Only the maximum
at the center is a strong one. The other maxima are weak and become progressively weaker at
greater distances from the center. In Figure 17.10 the angle 𝜃 defi nes the location of the fi rst minimum intensity point on either side of the center. Equation 17.1 gives 𝜃 in terms of the wave- length 𝜆 and the width D of the doorway and assumes that the doorway can be treated like a slit whose height is very large compared to its width:
Single slit—fi rst minimum sin θ = λ D
(17.1)
Waves also bend around the edges of openings other than single slits. Particularly important
is the diff raction of sound by a circular opening, such as that in a loudspeaker. In this case, the
angle 𝜃 is related to the wavelength 𝜆 and the diameter D of the opening by
Circular opening— fi rst minimum sin θ = 1.22
λ D
(17.2)
An important point to remember about Equations 17.1 and 17.2 is that the extent of the dif-
fraction depends on the ratio of the wavelength to the size of the opening. If the ratio 𝜆/D is small, then 𝜃 is small and little diff raction occurs. The waves are beamed in the forward direction as they leave an opening, much like the light from a fl ashlight. Such sound waves are said to have “nar-
row dispersion.” Since high-frequency sound has a relatively small wavelength, it tends to have a
narrow dispersion. On the other hand, for larger values of the ratio 𝜆/D, the angle 𝜃 is larger. The waves spread out over a larger region and are said to have a “wide dispersion.” Low-frequency
sound, with its relatively large wavelength, typically has a wide dispersion.
In a stereo loudspeaker, a wide dispersion of the sound is desirable. Example 3 illustrates,
however, that there are limitations to the dispersion that can be achieved, depending on the loud-
speaker design.
Room
D
Vibrating air molecule located in the doorway
θ
θ
FIGURE 17.10 Each vibrating molecule of the air in the doorway generates a sound wave
that expands outward and bends, or diff racts,
around the edges of the doorway. Because of
interference eff ects among the sound waves
produced by all the molecules, the sound
intensity is mostly confi ned to the region defi ned
by the angle 𝜃 on either side of the doorway.
Analyzing Multiple-Concept Problems
EXAMPLE 3 The Physics of Loudspeakers
A 1500-Hz sound and a 8500-Hz sound emerge from a loudspeaker
through a circular opening that has a diameter of 0.30 m (see Figure 17.11). Assuming that the speed of sound in air is 343 m/s, fi nd the diff raction
angle 𝜃 for each sound.
Reasoning The diff raction angle 𝜃 depends on the ratio of the wave- length 𝜆 of the sound to the diameter D of the opening, according to sin 𝜃 = 1.22(𝜆/D) (Equation 17.2). The wavelength for each sound can be obtained from the given frequencies and the speed of sound.
The high frequencies are beamed forward inside this cone
This person hears primarily the low frequencies
9.4° 68°
This person hears the high and low frequencies
FIGURE 17.11 Because the dispersion of high
frequencies is less than
the dispersion of low
frequencies, you should
be directly in front of the
speaker to hear both the
high and low frequencies
equally well.
472 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
As we have seen, diff raction is an interference eff ect, one in which some of the wave’s energy
is directed into regions that would otherwise not be accessible. Energy, of course, is conserved
during this process, because energy is only redistributed during diff raction; no energy is created
or destroyed.
Check Your Understanding
(The answers are given at the end of the book.) 6. At an open-air rock concert you are standing directly in front of a speaker. You hear the high-frequency
sounds of a female vocalist as well as the low-frequency sounds of the rhythmic bass. As you walk
Description Symbol Value Sound frequency f 1500 Hz or 8500 Hz
Diameter of speaker opening D 0.30 m
Speed of sound 𝜐 343 m/s
Unknown Variable Diffraction angle 𝜃 ?
Knowns and Unknowns The following data are available:
Modeling the Problem
STEP 1 The Diff raction Angle Equation 17.2 indicates that the diff raction angle is related to the ratio of the wavelength 𝜆 of the sound to the diameter D of the opening by sin 𝜃 = 1.22(𝜆/D). Solving this expression for 𝜃 gives Equation 1 at the right. A value for D is given. To determine the value for 𝜆, we turn to Step 2.
STEP 2 Wavelength The wavelength 𝜆 is related to the frequency f and the speed 𝜐 of the sound according to 𝜐 = f𝜆 (Equation 16.1). Solving for 𝜆 gives
λ = υ f
which can be substituted into Equation 1 as shown at the right.
Problem-Solving Insight When a wave passes through an opening, the extent of diff raction is greater when the ratio 𝝀/D is greater, where 𝜆 is the wavelength of the wave and D is the width or diameter of the opening.
Solution Combining the results of each step algebraically, we fi nd that
θ = sin−1 ( 1.22 λD) = sin−1 (1.22 υ/ f D )
Applying the above result to each of the sound frequencies shows that
1500-Hz sound θ = sin−1(1.22 υf D) = sin−1[1.22 (343 m /s)
(1500 Hz)(0.30 m) ] = 68°
8500-Hz sound θ = sin−1(1.22 υf D) = sin−1[1.22 (343 m /s)
(8500 Hz)(0.30 m) ] = 9.4° Figure 17.11 illustrates these results. With a 0.30-m opening, the dispersion of the higher- frequency sound is limited to only 9.4°. To increase the dispersion, a smaller opening is needed.
It is for this reason that loudspeaker designers use a small-diameter speaker called a tweeter to generate the high-frequency sound (see Figure 17.12). Related Homework: Problems 12, 14, 15
STEP 1 STEP 2
θ = sin−1 ( 1.22 λD) (1)
?
θ = sin−1 ( 1.22 λD) (1)
λ = υ f
FIGURE 17.12 Small-diameter speakers (called tweeters) are used to produce high-
frequency sound. The small diameter helps to
promote a wider dispersion of the sound.
Tweeter
© J
P ag
et R
F p h o to
s/ A
la m
y
17.4 Beats 473
to one side of the speaker, the sounds of the vocalist _________, and those of the rhythmic bass
_________. (a) drop off noticeably; also drop off noticeably (b) drop off only slightly; drop off notice- ably (c) drop off only slightly; also drop off only slightly (d) drop off noticeably; drop off only slightly
7. Refer to Example 1 in Section 16.2. Which type of radio wave, AM or FM, diff racts more readily around a given obstacle? (a) AM, because it has a greater wavelength (b) FM, because it has a greater wavelength (c) AM, because it has a greater frequency (d) FM, because it has a greater frequency
17.4 Beats In situations where waves with the same frequency overlap, we have seen how the principle of linear superposition leads to constructive and destructive interference and how it explains dif-
fraction. We will see in this section that two overlapping waves with slightly diff erent frequen- cies give rise to the phenomenon of beats. However, the principle of linear superposition again provides an explanation of what happens when the waves overlap.
A tuning fork has the property of producing a single-frequency sound wave when struck
with a sharp blow. Figure 17.13 shows sound waves coming from two tuning forks placed side by side. The tuning forks in the drawing are identical, and each is designed to produce a 440-Hz
tone. However, a small piece of putty has been attached to one fork, whose frequency is lowered
to 438 Hz because of the added mass. When the forks are sounded simultaneously, the loudness
of the resulting sound rises and falls periodically—faint, then loud, then faint, then loud, and so
on. The periodic variations in loudness are called beats and result from the interference between two sound waves with slightly diff erent frequencies.
For clarity, Figure 17.13 shows the condensations and rarefactions of the sound waves sepa- rately. In reality, however, the waves spread out and overlap. In accord with the principle of linear
superposition, the ear detects the combined total of the two. Notice that there are places where
the waves interfere constructively and places where they interfere destructively. When a region
of constructive interference reaches the ear, a loud sound is heard. When a region of destruc-
tive interference arrives, the sound intensity drops to zero (assuming each of the waves has the
same amplitude). The number of times per second that the loudness rises and falls is the beat frequency and is the diff erence between the two sound frequencies. Thus, in the situation illus- trated in Figure 17.13, an observer hears the sound loudness rise and fall at the rate of 2 times per second (440 Hz – 438 Hz).
Figure 17.14 helps to explain why the beat frequency is the diff erence between the two frequencies. The drawing displays graphical representations of the pressure patterns of a 10-Hz
Destructive
Small piece of putty
440 Hz
438 Hz
DestructiveConstructive Constructive
FIGURE 17.13 Two tuning forks have slightly diff erent frequencies of 440 and 438 Hz. The phenomenon of beats occurs when the forks
are sounded simultaneously. The sound waves are not drawn to scale.
Time
Time
Time
FaintFaint
1
1 2 3 4 5 6 7 8 9 10 11 12
2 3 4 5 6 7 8 9 10
Loud Loud
FIGURE 17.14 A 10-Hz and a 12-Hz sound wave, when added together, produce a wave with a beat
frequency of 2 Hz. The drawings show the pressure
patterns (in blue) of the individual waves and the
pressure pattern (in red) that results when the two
overlap. The time interval shown is one second.
474 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
wave and a 12-Hz wave, along with the pressure pattern that results when the two overlap. These
frequencies have been chosen for convenience, even though they lie below the audio range and
are inaudible. Audible sound waves behave in exactly the same way. The top two drawings, in
blue, show the pressure variations in a one-second interval of each wave. The third drawing, in
red, shows the result of adding together the blue patterns according to the principle of linear
superposition. Notice that the amplitude in the red drawing is not constant, as it is in the individ-
ual waves. Instead, the amplitude changes from a minimum to a maximum, back to a minimum,
and so on. When such pressure variations reach the ear and occur in the audible frequency range,
they produce a loud sound when the amplitude is a maximum and a faint sound when the ampli-
tude is a minimum. Two loud–faint cycles, or beats, occur in the one-second interval shown in
the drawing, corresponding to a beat frequency of 2 Hz. Thus, the beat frequency is the diff erence
between the frequencies of the individual waves, or 12 Hz – 10 Hz = 2 Hz.
THE PHYSICS OF . . . tuning a musical instrument. Musicians often tune their instruments by listening to a beat frequency. For instance, a guitar player plucks an out-of-tune
string along with a tone that has the correct frequency. He then adjusts the string tension until the
beats vanish, ensuring that the string is vibrating at the correct frequency.
Check Your Understanding
(The answers are given at the end of the book.) 8. Tuning fork A (frequency unknown) and tuning fork B (frequency = 384 Hz) together produce 6 beats
in 2 seconds. When a small piece of putty is attached to tuning fork A, as in Figure 17.13, the beat frequency decreases. What is the frequency of tuning fork A before the putty is attached? (a) 378 Hz (b) 381 Hz (c) 387 Hz (d) 390 Hz
9. A tuning fork has a frequency of 440 Hz. The string of a violin and this tuning fork, when sounded together, produce a beat frequency of 1 Hz. From these two pieces of information alone, is it possible to
determine the exact frequency of the violin string? (a) Yes; the frequency of the violin string is 441 Hz. (b) No, because the frequency of the violin string could be either 439 or 441 Hz. (c) Yes; the frequency of the violin string is 439 Hz.
10. When the regions of constructive and destructive interference in Figure 17.13 move past a listener’s ear, a beat frequency of 2 Hz is heard. Suppose that the tuning forks in the drawing are sounded under
water and that the listener is also under water. The forks vibrate at 438 and 440 Hz, just as they do
in air. However, sound travels four times faster in water than in air. The beat frequency heard by the
underwater listener is (a) 16 Hz (b) 8 Hz (c) 4 Hz (d) 2 Hz.
17.5 Transverse Standing Waves A standing wave is another interference eff ect that can occur when two waves overlap. Standing
waves can arise with transverse waves, such as those on a guitar string, and also with longitudinal
sound waves, such as those in a fl ute. In any case, the principle of linear superposition provides
an explanation of the eff ect, just as it does for diff raction and beats.
Interactive Figure 17.15 shows some of the essential features of transverse standing waves. In this fi gure the left end of each string is vibrated back and forth, while the right end is attached
to a wall. Regions of the string move so fast that they appear only as a blur in the photographs.
Each of the patterns shown is called a transverse standing wave pattern. Notice that the pat- terns include special places called nodes and antinodes. The nodes are places that do not vibrate at all, and the antinodes are places where maximum vibration occurs. To the right of each pho- tograph is a drawing that helps us to visualize the motion of the string as it vibrates in a standing
wave pattern. These drawings freeze the shape of the string at various times and emphasize the
maximum vibration that occurs at an antinode with the aid of a red dot attached to the string.
Each standing wave pattern is produced at a unique frequency of vibration. These frequen-
cies form a series, the smallest frequency f1 corresponding to the one-loop pattern and the larger frequencies being integer multiples of f1, as Interactive Figure 17.15 indicates. Thus, if f1 is 10 Hz, the frequency needed to establish the 2-loop pattern is 2f1 or 20 Hz, whereas the frequency needed to create the 3-loop pattern is 3f1 or 30 Hz, and so on. The frequencies in this series (f1, 2f1, 3f1, etc.) are called harmonics. The lowest frequency f1 is called the fi rst harmonic, and
17.5 Transverse Standing Waves 475
the higher frequencies are designated as the second harmonic (2f1), the third harmonic (3f1), and so forth. The harmonic number (1st, 2nd, 3rd, etc.) corresponds to the number of loops in
the standing wave pattern. The frequencies in this series are also referred to as the fundamental
frequency, the fi rst overtone, the second overtone, and so on. Thus, frequencies above the funda-
mental are overtones (see Interactive Figure 17.15). Standing waves arise because identical waves travel on the string in opposite directions and
combine in accord with the principle of linear superposition. A standing wave is said to be standing because it does not travel in one direction or the other, as do the individual waves that produce
it. Figure 17.16 shows why there are waves traveling in both directions on the string. At the top of the picture, one-half of a wave cycle (the remainder of the wave is omitted for clarity) is
moving toward the wall on the right. When the half-cycle reaches the wall, it causes the string to
pull upward on the wall. Consistent with Newton’s action-reaction law, the wall pulls downward
on the string, and a downward-pointing half-cycle is sent back toward the left. Thus, the wave
refl ects from the wall. Upon arriving back at the point of origin, the wave refl ects again, this time
from the hand vibrating the string. For small vibration amplitudes, the hand is essentially fi xed
and behaves as the wall does in causing refl ections. Repeated refl ections at both ends of the string
create a multitude of wave cycles traveling in both directions.
As each new cycle is formed by the vibrating hand, previous cycles that have refl ected from
the wall arrive and refl ect again from the hand. Unless the timing is right, however, the new and
the refl ected cycles tend to off set one another, and a standing wave is not formed. Think about
pushing someone on a swing and timing your pushes so that they reinforce one another. Such
reinforcement in the case of the wave cycles leads to a large-amplitude standing wave. Suppose
that the string has a length L and its left end is being vibrated at a frequency f1. The time required to create a new wave cycle is the period T of the wave, where T = 1/f1 (Equation 10.5). On the other hand, the time needed for a cycle to travel from the hand to the wall and back, a distance of
2L, is 2L/𝜐, where 𝜐 is the wave speed. Reinforcement between new and refl ected cycles occurs if these two times are equal; that is, if 1/f1 = 2L/𝜐. Thus, a standing wave is formed when the string is vibrated with a frequency of f1 = 𝜐/(2L).
Repeated reinforcement between newly created and refl ected cycles causes a large- amplitude
standing wave to develop on the string, even when the hand itself vibrates with only a small
FIGURE 17.16 In refl ecting from the wall, a forward-traveling half-cycle becomes a
backward-traveling half-cycle that is inverted.
1st harmonic (fundamental)
Frequency = f1
(a)
© Richard Megna/Fundamental Photographs, NYC
2nd harmonic (1st overtone)
Frequency = 2f1
(b)
Antinodes © Richard Megna/Fundamental Photographs, NYC
INTERACTIVE FIGURE 17.15 Vibrating a string at certain unique frequencies sets up transverse standing wave patterns, such as the three shown in the photographs on the left. Each drawing on the right shows the
various shapes that the string assumes at various times as it vibrates. The red dots attached to the strings
focus attention on the maximum vibration that occurs at an antinode. In each of the drawings, one-half of
a wave cycle is outlined in red. (Richard Megna/Fundamental Photographs)
3rd harmonic (2nd overtone)
Frequency = 3f1
(c)
Nodes
© Richard Megna/Fundamental Photographs, NYC
476 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
amplitude. Thus, the motion of the string is a resonance eff ect, analogous to that discussed in Section 10.6 for an object attached to a spring. The frequency f1 at which resonance occurs is sometimes called a natural frequency of the string, similar to the frequency at which an object oscillates on a spring.
There is a diff erence between the resonance of the string and the resonance of a spring
system, however. An object on a spring has only a single natural frequency, whereas the string has
a series of natural frequencies. The series arises because a refl ected wave cycle need not return to its point of origin in time to reinforce every newly created cycle. Reinforcement can occur, for instance, on every other new cycle, as it does if the string is vibrated at twice the frequency f1, or f2 = 2 f1. Likewise, if the vibration frequency is f3 = 3f1, reinforcement occurs on every third new cycle. Similar arguments apply for any frequency fn = nf1, where n is an integer. As a result, the series of natural frequencies that lead to standing waves on a string fi xed at both ends is
String fi xed at both ends fn = n ( υ2L) n = 1, 2, 3, 4, . . . (17.3) It is also possible to obtain Equation 17.3 in another way. In Interactive Figure 17.15,
one-half of a wave cycle is outlined in red for each of the harmonics, to show that each loop in
a standing wave pattern corresponds to one-half a wavelength. Since the two fi xed ends of the
string are nodes, the length L of the string must contain an integer number n of half-wavelengths: L = n ( 12λn ) or 𝜆n = 2L/n. Using this result for the wavelength in the relation fn𝜆n = 𝜐 shows that fn(2L/n) = 𝜐, which can be rearranged to give Equation 17.3.
Problem-Solving Insight The distance between two successive nodes (or between two successive antinodes) of a standing wave is equal to one-half of a wavelength.
Standing waves on a string are important in the way many musical instruments produce
sound. For instance, a guitar string is stretched between two supports and, when plucked, vibrates
according to the series of natural frequencies given by Equation 17.3. The next two examples
show how this series of frequencies governs the design of a guitar.
Analyzing Multiple-Concept Problems
EXAMPLE 4 Playing a Guitar
The heaviest string on an electric guitar has a linear density of
5.28 × 10–3 kg/m and is stretched with a tension of 226 N. This string
produces the musical note E when vibrating along its entire length in a
standing wave at the fundamental frequency of 164.8 Hz. (a) Find the length L of the string between its two fi xed ends (see Figure 17.17a). (b) A guitar player wants the string to vibrate at a fundamental fre- quency of 2 × 164.8 Hz = 329.6 Hz, as it must if the musical note E
is to be sounded one octave higher in pitch. To accomplish this, he
presses the string against the proper fret before plucking the string.
Find the distance L between the fret and the bridge of the guitar (see Figure 17.17b).
Reasoning The series of natural frequencies (including the fundamen- tal) for a string fi xed at both ends is given by fn = n𝜐/(2L) (Equation 17.3), where n = 1, 2, 3, etc. This equation can be solved for the length L. The speed 𝜐 at which waves travel can be obtained from the tension and the linear density of the string. The fundamental frequencies that are given
correspond to n = 1.
FIGURE 17.17 These drawings show the standing waves (in blue) that exist on a guitar string under diff erent playing conditions.
L
L
(a) (b)
17.5 Transverse Standing Waves 477
Description Symbol Value Comment Explicit Data Linear density of string m/L 5.28 × 10–3 kg/m
Tension in string F 226 N
Natural frequency at which string vibrates fn 164.8 Hz or 329.6 Hz These are fundamental frequencies.
Implicit Data Integer variable in series of natural frequencies n 1 Fundamental frequencies are given.
Unknown Variable Length L ?
Knowns and Unknowns The given data are summarized as follows:
Modeling the Problem
STEP 1 Natural Frequencies According to Equation 17.3, the natural frequencies for a string fi xed at both ends are given by fn = n𝜐/(2L), where n takes on the integer values 1, 2, 3, etc., 𝜐 is the speed of the waves on the string, and L is the length between the two fi xed ends. Solving this expression for L gives Equation 1 at the right. In this equation, only the speed 𝜐 is unknown. We will obtain a value for it in Step 2.
STEP 2 Speed of the Waves on the String The speed 𝜐 of the waves traveling on the string is given by Equation 16.2 as
υ = √ Fm /L where F is the tension and m/L is the linear density, both of which are given. The substitution of this expression for the speed into Equation 1 is shown at the right.
Solution Combining the results of each step algebraically, we fi nd that
L = nυ 2 fn
= n
2 fn √ Fm /L
It is given that the two natural frequencies at which the string vibrates are fundamental frequen-
cies. Thus, n = 1 and fn = f1. We now determine the desired lengths in parts (a) and (b).
(a) L = n 2 fn
√ Fm /L = 1
2(164.8 Hz) √ 226 N5.28 × 10−3 kg /m = 0.628 m
(b) L = n 2 fn√
F m /L
= 1
2(329.6 Hz)√ 226 N
5.28 × 10−3 kg /m = 0.314 m
The length in part (b) is one-half the length in part (a) because the fundamental frequency in part (b)
is twice the fundamental frequency in part (a).
Related Homework: Problems 29, 32, 34
STEP 1 STEP 2
L = nυ 2 fn
(1)
?
L = nυ 2 fn
(1)
υ = √ Fm /L
CONCEPTUAL EXAMPLE 5 The Physics of the Frets on a Guitar
Figure 17.18 shows the frets on the neck of a guitar. They allow the player to produce a complete sequence of musical notes using a single string. Start-
ing with the fret at the top of the neck, each successive fret shows where the
player should press to get the next note in the sequence. Musicians call the
sequence the chromatic scale, and every thirteenth note in it corresponds
to one octave, or a doubling of the sound frequency. Which describes the
spacing between the frets? It is (a) the same everywhere along the neck (b) greatest at the top of the neck and decreases with each additional fret further on down toward the bridge (c) smallest at the top of the neck and increases with each additional fret further on down toward the bridge.
478 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
Check Your Understanding
(The answers are given at the end of the book.) 11. A standing wave that corresponds to the fourth harmonic is set up on a string that is fi xed at both ends.
(a) How many loops are in this standing wave? (b) How many nodes (excluding the nodes at the ends of the string) does this standing wave have? (c) Is there a node or an antinode at the midpoint of the string? (d) If the frequency of this standing wave is 440 Hz, what is the frequency of the lowest-frequency standing wave that could be set up on this string?
12. The tension in a guitar string is doubled. By what factor does the frequency of the vibrating string change? (a) It increases by a factor of 2. (b) It increases by a factor of √2. (c) It decreases by a factor of 2. (d) It decreases by a factor of √2.
13. A string is vibrating back and forth as in Interactive Figure 17.15a. The tension in the string is decreased by a factor of four, with the frequency and length of the string remaining the same. A new standing wave
pattern develops on the string. How many loops are in this new pattern? (a) 5 (b) 4 (c) 3 (d) 2 14. A rope is hanging vertically straight down. The top end is being vibrated back and forth, and a stand-
ing wave with many loops develops on the rope, analogous (but not identical) to a standing wave on
a horizontal rope. The rope has mass. The separation between successive nodes is (a) everywhere the same along the rope (b) greater near the top of the rope than near the bottom (c) greater near the bottom of the rope than near the top.
17.6 Longitudinal Standing Waves Standing wave patterns can also be formed from longitudinal waves. For example, when sound
refl ects from a wall, the forward- and backward-going waves can produce a standing wave.
Figure 17.19 illustrates the vibrational motion in a longitudinal standing wave on a Slinky. As in a transverse standing wave, there are nodes and antinodes. At the nodes the Slinky coils do not vibrate
at all; that is, they have no displacement. At the antinodes the coils vibrate with maximum amplitude
Reasoning Our reasoning is based on the relation f1 = 𝜐/(2 L) (Equa- tion 17.3, with n = 1). The value of n is 1 because a string vibrates mainly at its fundamental frequency when plucked, as mentioned in
Example 4. This equation shows that L, which is the length between a given fret and the bridge of the guitar, is inversely proportional to the
fundamental frequency f1, or L = 𝜐/(2 f1). In Example 4 we found that the E string has a length of L = 0.628 m, corresponding to a fundamen- tal frequency of f1 = 164.8 Hz. We also found that the length between the bridge and the fret that must be pressed to double this frequency
to 2 × 164.8 Hz = 329.6 Hz is one-half of 0.628 m, or L = 0.314 m. To understand the spacing between frets as one moves down the neck,
consider the fret that must be pressed to double the frequency again,
from 329.6 Hz to 659.2 Hz. The length between the bridge and this fret
would be one-half of 0.314 m, or L = 0.157 m. Thus, the distances of
the three frets that we have been discussing are 0.628 m, 0.314 m, and
0.157 m, as indicated in Figure 17.18. The distance D1 between the fi rst two of these frets is D1 = 0.628 m – 0.314 m = 0.314 m. Similarly, the distance between the second and third of these frets is D2 = 0.314 m – 0.157 m = 0.157 m.
Answers (a) and (c) are incorrect. The distances between the frets are shown in Figure 17.18. Clearly, the distances D1 and D2 are not equal, nor are they smaller at the top of the neck and greater further on down.
Answer (b) is correct. Figure 17.18 shows that D1 is greater than D2. Thus, the spacing between the frets is greatest at the top of the neck and
decreases with each additional fret further on down.
Related Homework: Problem 40
D2
D1
0.15 7 m
0.31 4 m 0.62
8 m
Second doubling
First doubling
Start
Bridge
Fret s co
ntin ue d
own tow
ard t he b
ridge
Frets
FIGURE 17.18 The spacing between the frets on the neck of a guitar changes going
down the neck toward the bridge.
17.6 Longitudinal Standing Waves 479
and, thus, have a maximum displacement. The red dots in Figure 17.19 indicate the lack of vibration at a node and the maximum vibration at an antinode. The vibration occurs along the line of travel of
the individual waves, as is to be expected for longitudinal waves. In a standing wave of sound, at the
nodes and antinodes, the molecules or atoms of the medium behave as the red dots do.
Musical instruments in the wind family depend on longitudinal standing waves in produc-
ing sound. Since wind instruments (trumpet, fl ute, clarinet, pipe organ, etc.) are modifi ed tubes
or columns of air, it is useful to examine the standing waves that can be set up in such tubes.
Interactive Figure 17.20 shows two cylindrical columns of air that are open at both ends. Sound waves, originating from a tuning fork, travel up and down within each tube, since they refl ect
from the ends of the tubes, even though the ends are open. If the frequency f of the tuning fork matches one of the natural frequencies of the air column, the downward- and upward-traveling
waves combine to form a standing wave, and the sound of the tuning fork becomes markedly
louder. To emphasize the longitudinal nature of the standing wave patterns, the left side of each
pair of drawings in Interactive Figure 17.20 replaces the air in the tubes with Slinkies, on which the nodes and antinodes are indicated with red dots. As an additional aid in visualizing the
standing waves, the right side of each pair of drawings shows blurred blue patterns within each
tube. These patterns symbolize the amplitude of the vibrating air molecules at various locations.
Wherever the pattern is widest, the amplitude of vibration is greatest (a displacement antinode),
and wherever the pattern is narrowest there is no vibration (a displacement node).
To determine the natural frequencies of the air columns in Interactive Figure 17.20, notice that there is a displacement antinode at each end of the open tube because the air molecules
there are free to move.* As in a transverse standing wave, the distance between two successive
antinodes is one-half of a wavelength, so the length L of the tube must be an integer number n of half-wavelengths: L = n ( 12λ n ) or λ n = 2L / n. Using this wavelength in the relation fn = 𝜐/λn shows that the natural frequencies fn of the tube are
Tube open at both ends fn = n ( υ2L) n = 1, 2, 3, 4, . . . (17.4) At these frequencies, large-amplitude standing waves develop within the tube due to resonance.
Example 6 illustrates how Equation 17.4 is involved when a fl ute is played.
N N N NA A A A
FIGURE 17.19 A longitudinal standing wave on a Slinky showing the displacement nodes
(N) and antinodes (A).
A Frequency = f
A
N
A
A
A
N
N
Frequency = 2f
INTERACTIVE FIGURE 17.20 A pictorial representation of longitudinal standing waves
on a Slinky (left side of each pair) and in a
tube of air (right side of each pair) that is
open at both ends (A, antinode; N, node).
*In reality, the antinode does not occur exactly at the open end. However, if the tube’s diameter is small compared to its
length, little error is made in assuming that the antinode is located right at the end.
EXAMPLE 6 The Physics of a Flute
When all the holes are closed on one type of fl ute, the lowest note it can sound
is a middle C (fundamental frequency = 261.6 Hz). The air temperature is
293 K, and the speed of sound is 343 m/s. Assuming the fl ute is a cylindri-
cal tube open at both ends, determine the distance L in Figure 17.21—that is, the distance from the mouthpiece to the end of the tube. (This distance is
approximate, since the antinode does not occur exactly at the mouthpiece.)
Reasoning For a tube open at both ends, the series of natural frequen- cies (including the fundamental) is given by fn = n𝜐/(2L) (Equation 17.4), where n takes on the integer values 1, 2, 3, etc. To obtain a value for L, we can solve this equation, since the given fundamental frequency
corresponds to n = 1 and the speed 𝜐 of sound is known.
Solution Solving Equation 17.4 for the length L, we obtain
L = nυ 2 fn
= (1)(343 m /s)
2(261.6 Hz) = 0.656 m
Head joint
L
FIGURE 17.21 The length L of a fl ute between the mouthpiece and the end of the
instrument determines the fundamental
frequency of the lowest playable note.
480 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
Standing waves can also exist in a tube with only one end open, as the patterns in Figure 17.22 indicate. Note the diff erence between these patterns and those in Interactive Figure 17.20. Here the standing waves have a displacement antinode at the open end and a displacement node
at the closed end, where the air molecules are not free to move. Since the distance between a
node and an adjacent antinode is one-fourth of a wavelength, the length L of the tube must be an odd number of quarter-wavelengths: L = 1(14 λ) and L = 3(
1
4 λ) for the two standing wave patterns in Figure 17.22. In general, then, L = n(14 λn ), where n is any odd integer (n = 1, 3, 5, . . .). From this result it follows that 𝜆n = 4L /n, and the natural frequencies fn can be obtained from the relation fn = 𝜐/𝜆n:
Tube open at only one end fn = n ( υ4L) n = 1, 3, 5, . . . (17.5) A tube open at only one end can develop standing waves only at the odd harmonic frequencies
f1, f3, f5, etc. In contrast, a tube open at both ends can develop standing waves at all harmonic frequencies f1, f2, f3, etc. Moreover, the fundamental frequency f1 of a tube open at only one end (Equation 17.5) is one-half that of a tube open at both ends (Equation 17.4). In other words, a
tube open only at one end needs to be only one-half as long as a tube open at both ends in order
to produce the same fundamental frequency. Energy is also conserved when a standing wave is produced, either on a string or in a tube
of air. The energy of the standing wave is the sum of the energies of the individual waves that
comprise the standing wave. Once again, interference redistributes the energy of the individual
waves to create locations of greatest energy (displacement antinodes) and locations of no energy
(displacement nodes).
Check Your Understanding
(The answers are given at the end of the book.) 15. A cylindrical bottle, partially fi lled with water, is open at the top. When you blow across the top of the
bottle a standing wave is set up inside it. Is there a node or an antinode (a) at the top of the bottle and (b) at the surface of the water? (c) If the standing wave is vibrating at its fundamental frequency, what is the distance between the top of the bottle and the surface of the water? Express your answer in terms
of the wavelength 𝜆 of the standing wave. (d) If you take a sip from the bottle, is the fundamental frequency of the standing wave raised, lowered, or does it remain the same?
16. In Interactive Figure 17.20 both tubes are fi lled with air, in which the speed of sound is 𝜐air. Suppose, instead, that the tube near the tuning fork labeled “Frequency = 2 f ” is fi lled not with air, but with another gas in which the speed of sound is 𝜐gas. The frequency of each tuning fork remains unchanged. How should 𝜐gas compare with 𝜐air in order that the standing wave pattern in each tube has the same appearance? (a) υgas = 12 υair (b) υgas = 2υair (c) υgas =
1
4 υair (d) υgas = 4υair 17. Standing waves can ruin the acoustics of a concert hall if there is excessive refl ection of the sound
waves that the performers generate. For example, suppose that a performer generates a 2093-Hz tone.
If a large-amplitude standing wave is present, it is possible for a listener to move a distance of only
4.1 cm and hear the loudness of the tone change from loud to faint. What does the distance of 4.1 cm
represent? (a) One wavelength of the sound (b) One-half the wavelength of the sound (c) One-fourth the wavelength of the sound
18. A wind instrument is brought into a warm house from the cold outdoors. What happens to the natural frequencies of the instrument? Neglect any change in the length of the instrument. (a) They increase. (b) They decrease. (c) They remain the same.
FIGURE 17.22 A pictorial representation of the longitudinal standing waves on a Slinky
(left side of each pair) and in a tube of air
(right side of each pair) that is open only at
one end (A, antinode; N, node).
A Frequency = f
A
A
N
N
N
Frequency = 3f
17.7 Complex Sound Waves 481
17.7 *Complex Sound Waves Musical instruments produce sound in a way that depends on standing waves. Examples 4 and 5
illustrate the role of transverse standing waves on the string of an electric guitar, while Example 6
stresses the role of longitudinal standing waves in the air column within a fl ute. In each example,
sound is produced at the fundamental frequency of the instrument.
In general, however, a musical instrument does not produce just the fundamental frequency
when it plays a note, but simultaneously generates a number of harmonics as well. Diff erent
instruments, such as a violin and a trumpet, generate harmonics to diff erent extents, and the
harmonics give the instruments their characteristic sound qualities or timbres. Suppose, for
instance, that a violinist and a trumpet player both sound concert A, a note whose fundamental
frequency is 440 Hz. Even though both instruments are playing the same note, most people can
distinguish the sound of the violin from that of the trumpet. The instruments sound diff erent
because the relative amplitudes of the harmonics (880 Hz, 1320 Hz, etc.) that the instruments
create are diff erent.
The sound wave corresponding to a note produced by a musical instrument or a singer is
called a complex sound wave because it consists of a mixture of the fundamental and har- monic frequencies. The pattern of pressure fl uctuations in a complex wave can be obtained by
using the principle of linear superposition, as Figure 17.23 indicates. This drawing shows a bar graph in which the heights of the bars give the relative amplitudes of the harmonics contained
in a note such as a singer might produce. When the individual pressure patterns for each of the
three harmonics are added together, they yield the complex pressure pattern shown at the top
of the picture.*
THE PHYSICS OF . . . a spectrum analyzer. In practice, a bar graph such as that in Figure 17.23 is determined with the aid of an electronic instrument known as a spectrum analyzer. When the note is produced, the complex sound wave is detected by a microphone that
converts the wave into an electrical signal. The electrical signal, in turn, is fed into the spectrum
analyzer, as Figure 17.24 illustrates. The spectrum analyzer then determines the amplitude and frequency of each harmonic present in the complex wave and displays the results on its screen.
A ir
p re
ss ur
e
Time
Complex pressure pattern
+ +
2
Harmonic number
A m
pl it
ud e
31
FIGURE 17.23 The topmost graph shows the pattern of pressure fl uctuations such as a singer
might produce. The pattern is the sum of the
fi rst three harmonics. The relative amplitudes
of the harmonics correspond to the heights of
the vertical bars in the bar graph.
Pressure pattern
Spectrum analyzer
2
Harmonic number
A m
pl it
ud e
31
FIGURE 17.24 A microphone detects a complex sound wave produced by a singer’s voice, and a spectrum analyzer determines the amplitude and frequency of each harmonic present in the wave.
*In carrying out the addition, we assume that each individual pattern begins at zero at the origin when the time equals zero.
EXAMPLE 7 BIO The Physics of Hearing Loss—Standing Waves in the Ear
The human ear canal (Figure 17.25) essentially acts like a tube closed at one end. If the ear canal has a length of 2.3 cm, what are the fundamental
wavelength and frequency for standing waves in the ear? Take the speed
of sound to be 343 m/s. What is the signifi cance of this result? Consult
the graph in Figure 16.35.
Reasoning We treat the auditory canal as a tube closed at one end. We can use Equation 17.5 to calculate the standing wave frequencies.
Solution The fundamental frequency is calculated for n = 1. Using this value in Equation 17.5, we get the following:
𝑓1 = (1)( 343 m/s(4)(0.023 m)) = 3700 Hz The fundamental wavelength is related to the fundamental frequency by
λ = υ f
= 343 m/s
3700 Hz = 9.3 × 10−2 m = 9.3 cm
482 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
Looking at the graph in Figure 16.35, we see that the intensity curves dip in the range of 2000 – 5000 Hz, with the ear having the greatest sensitiv-
ity at the fundamental frequency just below 4000 Hz. In fact, the ear can
detect sound intensities below the threshold of hearing at 3700 Hz. Due
to the resonance, sounds at this frequency are amplifi ed. Damage to the
ear can occur if exposed to high-intensity sounds for prolonged periods of
time. People working in high-noise environments without ear protection
often show signs of 3700-Hz hearing loss.
FIGURE 17.25 Diagram of the human ear showing the auditory canal as a tube closed at one end.
Inner ear
Semicircular canals
Anvil
Hammer
Cochlea
Auditory nerve
Eustachian tubeOval
window Stirrup
Middle ear
Tympanic membrane
Outer ear
Auditory canal
Pinna
2.3 cm
20 40 60 100 200 400
Frequency, Hz 1000
0
4000 10 000
120
100
80
60
In te
ns it
y le
ve l,
dB
40
20 20
40
60
80
100
120
0
Threshold of hearing
FIGURE 16.35 (REPEATED) Each curve represents the intensity levels at
which sounds of various frequencies
have the same loudness. The curves are
labeled by their intensity levels at 1000 Hz
and are known as Fletcher-Munson
curves.
Concept Summary 17.1 The Principle of Linear Superposition The principle of linear superposition states that when two or more waves are present simultaneously
at the same place, the resultant disturbance is the sum of the disturbances
from the individual waves.
17.2 Constructive and Destructive Interference of Sound Waves Constructive interference occurs at a point when two waves meet there
crest-to-crest and trough-to-trough, thus reinforcing each other. Destruc-
tive interference occurs when the waves meet crest-to-trough and cancel
each other.
When waves meet crest-to-crest and trough-to-trough, they are exactly in phase. When they meet crest-to-trough, they are exactly out of phase.
For two wave sources vibrating in phase, a diff erence in path lengths that
is zero or an integer number (1, 2, 3, . . .) of wavelengths leads to construc-
tive interference; a diff erence in path lengths that is a half-integer number
( 1
2 , 1 1
2 , 2 1
2 , . . .) of wavelengths leads to destructive interference.
For two wave sources vibrating out of phase, a diff erence in path
lengths that is a half-integer number ( 1
2 , 1 1
2 , 2 1
2 , . . .) of wavelengths
leads to constructive interference; a diff erence in path lengths that is zero
or an integer number (1, 2, 3, . . .) of wavelengths leads to destructive
interference.
17.3 Diff raction Diff raction is the bending of a wave around an obstacle or the edges of an opening. The angle through which the wave bends depends
on the ratio of the wavelength 𝜆 of the wave to the width D of the opening; the greater the ratio 𝜆/D, the greater the angle.
When a sound wave of wavelength 𝜆 passes through an opening, the fi rst
place where the intensity of the sound is a minimum relative to that at the
center of the opening is specifi ed by the angle 𝜃. If the opening is a rectangular
slit of width D, such as a doorway, the angle is given by Equation 17.1. If the opening is a circular opening of diameter D, such as that in a loudspeaker, the angle is given by Equation 17.2.
sin θ = λ D
(17.1)
sin θ = 1.22 λ D
(17.2)
17.4 Beats Beats are the periodic variations in amplitude that arise from the linear superposition of two waves that have slightly diff erent frequen-
cies. When the waves are sound waves, the variations in amplitude cause the
loudness to vary at the beat frequency, which is the diff erence between the
frequencies of the waves.
17.5 Transverse Standing Waves A standing wave is the pattern of dis- turbance that results when oppositely traveling waves of the same frequency
and amplitude pass through each other. A standing wave has places of min-
imum and maximum vibration called, respectively, nodes and antinodes.
Under resonance conditions, standing waves can be established only at
certain natural frequencies. The frequencies in this series ( f1, 2 f1, 3 f1, etc.) are called harmonics. The lowest frequency f1 is called the fi rst harmonic, the next frequency 2 f1 is the second harmonic, and so on. For a string that is fi xed at both ends and has a length L, the natural frequencies are specifi ed by Equation 17.3, where 𝜐 is the speed of the wave on the string and n is a positive integer.
fn = n ( υ2L) n = 1, 2, 3, 4, . . . (17.3)
Focus on Concepts 483
17.6 Longitudinal Standing Waves For a gas in a cylindrical tube open at both ends, the natural frequencies of vibration are specifi ed by Equation
17.4, where 𝜐 is the speed of sound in the gas and L is the length of the tube. For a gas in a cylindrical tube open at only one end, the natural frequencies
of vibration are given by Equation 17.5.
fn = n ( υ2L) n = 1, 2, 3, 4, . . . (17.4)
fn = n ( υ4L) n = 1, 3, 5, 7, . . . (17.5) 17.7 Complex Sound Waves A complex sound wave consists of a mixture of a fundamental frequency and overtone frequencies.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 17.1 The Principle of Linear Superposition 2. The drawing shows four moving pulses. Although shown as separated, the four pulses exactly overlap each other at the instant shown. Which combin-
ation of these pulses would produce a resultant pulse with the highest peak
and the deepest valley at this instant? (a) 1 and 2 (b) 2, 3, and 4 (c) 2 and 3 (d) 1, 2, and 3 (e) 1 and 3
QUESTION 2
(1) (2)
(3) (4)
Section 17.2 Constructive and Destructive Interference of Sound Waves 3. Two cellists, one seated directly behind the other in an orchestra, play the same note for the conductor, who is directly in front of them. Because of the
separation between the cellists, destructive interference occurs at the con-
ductor. This separation is the smallest that produces destructive interference.
Would this separation increase, decrease, or remain the same if the cellists
produced a note with a higher frequency? (a) The separation between the cellists would remain the same. (b) The separation would decrease because the wavelength of the sound is greater. (c) The separation would decrease because the wavelength of the sound is smaller. (d) The separation would increase because the wavelength of the sound is greater. (e) The separation would increase because the wavelength of the sound is smaller.
Section 17.3 Diff raction 5. A loudspeaker is producing sound of a certain wavelength. Which combination of the wavelength 𝜆 (expressed as a multiple of 𝜆0) and
the speaker’s diameter D (expressed as a multiple of D0) would exhibit the greatest amount of diff raction when the sound leaves the speaker
and enters the room? (a) 𝜆 = 𝜆0, D = D0 (b) 𝜆 = 2𝜆0, D = D0 (c) 𝜆 = 𝜆0, D = 2D0 (d) 𝜆 = 2𝜆0, D = 2D0 (e) 𝜆 = 3𝜆0, D = 2D0
7. Sound of a given frequency leaves a loudspeaker and spreads out due to diff raction. The speaker is placed in a room that contains either air or helium.
The speed of sound in helium is about three times as great as the speed of
sound in air. In which room, if either, does the sound exhibit the greater
diff raction when leaving the speaker? (a) The greater diff raction occurs in the air-fi lled room, because the wavelength of the sound is smaller in that
room. (b) The greater diff raction occurs in the air-fi lled room, because the wavelength of the sound is greater in that room. (c) The diff raction is the same in both rooms. (d) The greater diff raction occurs in the helium-fi lled room, because the wavelength of the sound is smaller in that room. (e) The greater diff raction occurs in the helium-fi lled room, because the wavelength
of the sound is greater in that room.
Section 17.4 Beats 8. Two musicians are comparing their trombones. The fi rst produces a tone that is known to be 438 Hz. When the two trombones play together they
produce 6 beats every 2 seconds. Which statement is true about the second
trombone? (a) It is producing either a 432-Hz sound or a 444-Hz sound. (b) It is producing either a 436-Hz sound or a 440-Hz sound. (c) It is producing a 444-Hz sound, and could be producing no other sound frequency. (d) It is producing either a 435-Hz sound or a 441-Hz sound. (e) It is producing a 441-Hz sound and could be producing no other sound frequency.
Section 17.5 Transverse Standing Waves 11. Two transverse standing waves are shown in the drawing. The strings have the same tension
and length, but the bottom string is more massive.
Which standing wave, if either, is vibrating at the
higher frequency? (a) The top standing wave has the higher frequency, because the traveling waves
have a smaller speed due to the smaller mass of the
string. (b) The top standing wave has the higher fre- quency, because the traveling waves have a larger speed due to the smaller
mass of the string. (c) Both standing waves have the same frequency, because the frequency of vibration does not depend on the mass of the string. (d) The bottom standing wave has the higher frequency, because the traveling waves
have a smaller speed due to the larger mass of the string. (e) The bottom standing wave has the higher frequency, because the traveling waves have a
larger speed due to the larger mass of the string.
12. A standing wave on a string fi xed at both ends is vibrating at its fourth harmonic. If the length, tension, and linear density are kept constant, what
can be said about the wavelength and frequency of the fi fth harmonic
relative to the fourth harmonic? (a) The wavelength of the fi fth harmonic is longer, and its frequency is higher. (b) The wavelength of the fi fth harmonic is longer, and its frequency is lower. (c) The wavelength of the fi fth harmonic is shorter, and its frequency is higher. (d) The wavelength of the fi fth har- monic is shorter, and its frequency is lower.
Focus on Concepts
QUESTION 11
484 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
Section 17.6 Longitudinal Standing Waves 14. A longitudinal standing wave is established in a tube that is open at both ends (see the drawing). The length of the tube is 0.80 m. What is the
wavelength of the waves that make up the standing wave? (a) 0.20 m (b) 0.40 m (c) 0.80 m (d) 1.20 m (e) 1.60 m
QUESTION 14
0.80 m
16. A longitudinal standing wave is established in a tube open at only one end (see the drawing). The frequency of the standing wave is 660 Hz, and the
speed of sound in air is 343 m/s. What is the length of the tube? (a) 0.13 m (b) 0.26 m (c) 0.39 m (d) 0.52 m (e) 0.65 m
QUESTION 16
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 17.1 The Principle of Linear Superposition,
Section 17.2 Constructive and Destructive Interference of Sound Waves 1. E In Figure 17.7, suppose that the separation between speakers A and B is 5.00 m and the speakers are vibrating in phase. They are playing identical
125-Hz tones, and the speed of sound is 343 m/s. What is the largest possible
distance between speaker B and the observer at C, such that he observes
destructive interference?
2. E Two speakers, one directly behind the other, are each generating a 245-Hz sound wave. What is the smallest separation distance between the speakers
that will produce destructive interference at a listener standing in front of
them? The speed of sound is 343 m/s.
3. E SSM The drawing graphs a string on which two rectangular pulses are traveling at a constant speed of 1 cm/s at time t = 0 s. Using the principle of linear superposition, draw the shape of the string at t = 1 s, 2 s, 3 s, and 4 s.
PROBLEM 3
1 cm/s 1 cm/s
0 2 4 6 8 10 12
Distance, cm
4. E Loudspeakers A and B are vibrating in phase and are playing the same tone, which has a frequency of 250 Hz. They are set up as in Figure 17.7, and point C is located as shown there. However, the distance between the
speakers and the distance between speaker B and point C have the same value
d. The speed of sound is 343 m/s. What is the smallest value of d, such that constructive interference occurs at point C?
5. E SSM Two waves are traveling in opposite directions on the same string. The displacements caused by the individual waves are given by y1 = (24.0 mm)sin(9.00𝜋t – 1.25𝜋x) and y2 = (35.0 mm)sin(2.88𝜋t + 0.400𝜋x).
Note that the phase angles (9.00𝜋t – 1.25𝜋x) and (2.88𝜋t + 0.400𝜋x) are in radians, t is in seconds, and x is in meters. At t = 4.00 s, what is the net dis- placement (in mm) of the string at (a) x = 2.16 m and (b) x = 2.56 m? Be sure to include the algebraic sign (+ or –) with your answers.
6. E CHALK GO Both drawings show the same square, each of which has a side of length L = 0.75 m. An observer O is stationed at one corner of each square. Two loudspeakers are located at corners of the square, as in either
drawing 1 or drawing 2. The speakers produce the same single-frequency
tone in either drawing and are in phase. The speed of sound is 343 m/s. Find
the single smallest frequency that will produce both constructive interference
in drawing 1 and destructive interference in drawing 2.
PROBLEM 6
O
Drawing 1 Drawing 2
O
7. E SSM The drawing shows a loudspeaker A and point C, where a listener is positioned. A second loudspeaker B is located somewhere to the right of
loudspeaker A. Both speakers vibrate in phase and are playing a 68.6-Hz
tone. The speed of sound is 343 m/s. What is the closest to speaker A that
speaker B can be located, so that the listener hears no sound?
PROBLEM 7 B
60.0°
A
1. 00
m
C
8. E GO Suppose that the two speakers in Figure 17.7 are separated by 2.50 m and are vibrating exactly out of phase at a frequency of 429 Hz. The speed of sound is 343 m/s. Does the observer at C observe constructive or destructive
interference when his distance from speaker B is (a) 1.15 m and (b) 2.00 m? 9. M MMH Two loudspeakers on a concert stage are vibrating in phase. A listener is 50.5 m from the left speaker and 26.0 m from the right one. The
listener can respond to all frequencies from 20 to 20 000 Hz, and the speed
of sound is 343 m/s. What are the two lowest frequencies that can be heard
loudly due to constructive interference?
10. M GO A listener is standing in front of two speakers that are producing sound of the same frequency and amplitude, except that they are vibrating out
of phase. Initially, the distance between the listener and each speaker is the
same (see the drawing). As the listener moves sideways, the sound intensity
Problems
Problems 485
gradually changes. When the distance x in the drawing is 0.92 m, the change reaches the maximum amount (either loud to soft, or soft to loud). Using the
data shown in the drawing and 343 m/s for the speed of sound, determine the
frequency of the sound coming from the speakers.
PROBLEM 10
4.00 m
3.00 m
Out-of-phase speakers
x
11. H Speakers A and B are vibrating in phase. They are directly facing each other, are 7.80 m apart, and are each playing a 73.0-Hz tone. The speed
of sound is 343 m/s. On the line between the speakers there are three points where constructive interference occurs. What are the distances of these three
points from speaker A?
Section 17.3 Diff raction 12. E Consult Multiple-Concept Example 3 for background pertinent to this problem. A speaker has a diameter of 0.30 m. (a) Assuming that the speed of sound is 343 m/s, fi nd the diff raction angle 𝜃 for a 2.0-kHz tone. (b) What speaker diameter D should be used to generate a 6.0-kHz tone whose diff raction angle is as wide as that for the 2.0-kHz tone in part (a)?
13. E SSM Sound exits a diff raction horn loudspeaker through a rectangular opening like a small doorway. Such a loudspeaker is mounted outside on a
pole. In winter, when the temperature is 273 K, the diff raction angle 𝜃 has a value of 15.0°. What is the diff raction angle for the same sound on a summer
day when the temperature is 311 K?
14. E GO For one approach to problems such as this, see Multiple-Concept Example 3. Sound emerges through a doorway, as in Figure 17.10. The width of the doorway is 77 cm, and the speed of sound is 343 m/s. Find
the diff raction angle 𝜃 when the frequency of the sound is (a) 5.0 kHz and (b) 5.0 × 102 Hz. 15. E V-HINT Available in WileyPLUS. 16. E GO The following two lists give the diameters and sound frequencies for three loudspeakers. Pair each diameter with a frequency, so that the dif-
fraction angle is the same for each of the speakers, and then fi nd the common
diff raction angle. Take the speed of sound to be 343 m/s.
Diameter, D Frequency, f 0.050 m 6.0 kHz
0.10 m 4.0 kHz
0.15 m 12.0 kHz
17. M A 3.00-kHz tone is being produced by a speaker with a diameter of 0.175 m. The air temperature changes from 0 to 29 °C. Assuming air to be an
ideal gas, fi nd the change in the diff raction angle 𝜃. 18. M GO Sound (speed = 343 m/s) exits a diff raction horn loudspeaker through a rectangular opening like a small doorway. A person is sitting at an
angle 𝛼 off to the side of a diff raction horn that has a width D of 0.060 m. This individual does not hear a sound wave that has a frequency of 8100 Hz. When
she is sitting at an angle 𝛼/2, the frequency that she does not hear is diff erent. What is this frequency?
Section 17.4 Beats 19. E SSM Two pure tones are sounded together. The drawing shows the pressure variations of the two sound waves, measured with respect to atmo-
spheric pressure. What is the beat frequency?
0.020 sPressure
TimeTime
Pressure
0.024 s
0 0
PROBLEM 19
20. E GO Two pianos each sound the same note simultaneously, but they are both out of tune. On a day when the speed of sound is 343 m/s, piano A
produces a wavelength of 0.769 m, while piano B produces a wavelength of
0.776 m. How much time separates successive beats?
21. E V-HINT MMH A 440.0-Hz tuning fork is sounded together with an out- of-tune guitar string, and a beat frequency of 3 Hz is heard. When the string is
tightened, the frequency at which it vibrates increases, and the beat frequency
is heard to decrease. What was the original frequency of the guitar string?
22. E Two ultrasonic sound waves combine and form a beat frequency that is in the range of human hearing for a healthy young person. The frequency of
one of the ultrasonic waves is 70 kHz. What are (a) the smallest possible and (b) the largest possible value for the frequency of the other ultrasonic wave? 23. E SSM Two out-of-tune fl utes play the same note. One produces a tone that has a frequency of 262 Hz, while the other produces 266 Hz. When a tuning
fork is sounded together with the 262-Hz tone, a beat frequency of 1 Hz is pro-
duced. When the same tuning fork is sounded together with the 266-Hz tone, a
beat frequency of 3 Hz is produced. What is the frequency of the tuning fork?
24. M GO Two cars have identical horns, each emitting a frequency of fs = 395 Hz. One of the cars is moving with a speed of 12.0 m/s toward a bystander waiting at a corner, and the other car is parked. The speed of sound
is 343 m/s. What is the beat frequency heard by the bystander?
25. M GO A sound wave is traveling in seawater, where the adiabatic bulk modulus and density are 2.31 × 109 Pa and 1025 kg/m3, respectively. The
wavelength of the sound is 3.35 m. A tuning fork is struck under water and
vibrates at 440.0 Hz. What would be the beat frequency heard by an under-
water swimmer?
26. H Two loudspeakers are mounted on a merry-go-round whose radius is 9.01 m. When stationary, the speakers both play a tone whose frequency is
100.0 Hz. As the drawing illustrates, they are situated at opposite ends of a
diameter. The speed of sound is 343.00 m/s, and the merry-go-round revolves
once every 20.0 s. What is the beat frequency that is detected by the listener
when the merry-go-round is near the position shown?
PROBLEM 26 Listener
Merry-go-round (top view)
486 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
Section 17.5 Transverse Standing Waves 27. E The fundamental frequency of a string fi xed at both ends is 256 Hz. How long does it take for a wave to travel the length of this string?
28. E A string that is fi xed at both ends has a length of 2.50 m. When the string vibrates at a frequency of 85.0 Hz, a standing wave with fi ve loops is
formed. (a) What is the wavelength of the waves that travel on the string? (b) What is the speed of the waves? (c) What is the fundamental frequency of the string?
29. E SSM The approach to solving this problem is similar to that taken in Multiple-Concept Example 4. On a cello, the string with the largest linear
density (1.56 × 10–2 kg/m) is the C string. This string produces a fundamental
frequency of 65.4 Hz and has a length of 0.800 m between the two fi xed ends.
Find the tension in the string.
30. E GO Two wires, each of length 1.2 m, are stretched between two fi xed supports. On wire A there is a second-harmonic standing wave whose
frequency is 660 Hz. However, the same frequency of 660 Hz is the third
harmonic on wire B. Find the speed at which the individual waves travel on
each wire.
31. E SSM Suppose that the strings on a violin are stretched with the same tension and each has the same length between its two fi xed ends. The musical
notes and corresponding fundamental frequencies of two of these strings are
G (196.0 Hz) and E (659.3 Hz). The linear density of the E string is 3.47 ×
10–4 kg/m. What is the linear density of the G string?
32. E To review the concepts that play roles in this problem, consult Multiple-Concept Example 4. Sometimes, when the wind blows across a
long wire, a low-frequency “moaning” sound is produced. This sound arises
because a standing wave is set up on the wire, like a standing wave on a guitar
string. Assume that a wire (linear density = 0.0140 kg/m) sustains a tension
of 323 N because the wire is stretched between two poles that are 7.60 m
apart. The lowest frequency that an average, healthy human ear can detect is
20.0 Hz. What is the lowest harmonic number n that could be responsible for the “moaning” sound?
33. E A string has a linear density of 8.5 × 10–3 kg/m and is under a tension of 280 N. The string is 1.8 m long, is fi xed at both ends, and is vibrating in
the standing wave pattern shown in the drawing. Determine the (a) speed, (b) wavelength, and (c) frequency of the traveling waves that make up the standing wave.
PROBLEM 33
34. E GO Multiple-Concept Example 4 deals with the same concepts as this problem. A 41-cm length of wire has a mass of 6.0 g. It is stretched
between two fi xed supports and is under a
tension of 160 N. What is the fundamental
frequency of this wire?
35. M CHALK GO A copper block is sus- pended from a wire, as in part 1 of the
drawing. A container of mercury is then
raised up around the block, as in part 2,
so that 50.0% of the block’s volume is
submerged in the mercury. The density of
copper is 8890 kg/m3, and that of mercury
is 13 600 kg/m3. Find the ratio of the fun-
damental frequency of the wire in part 2
to the fundamental frequency of the wire
in part 1.
36. M V-HINT The drawing shows two strings that have the same length and linear density. The left end of each string is attached to a wall, while the right
end passes over a pulley and is connected to objects of diff erent weights (WA and WB). Diff erent standing waves are set up on each string, but their frequen- cies are the same. If WA = 44 N, what is WB?
WA WB
PROBLEM 36
37. M SSM The E string on an electric bass guitar has a length of 0.628 m and, when producing the note E, vibrates at a fundamental frequency of 41.2 Hz.
Players sometimes add to their instruments a device called a “D-tuner.” This
device allows the E string to be used to produce the note D, which has a fun-
damental frequency of 36.7 Hz. The D-tuner works by extending the length
of the string, keeping all other factors the same. By how much does a D-tuner
extend the length of the E string?
38. M GO Standing waves are set up on two strings fi xed at each end, as shown in the drawing. The two strings have the same tension and mass per
unit length, but they diff er in length by 0.57 cm. The waves on the shorter
string propagate with a speed of 41.8 m/s, and the fundamental frequency of
the shorter string is 225 Hz. Determine the beat frequency produced by the
two standing waves.
PROBLEM 38
39. H SSM Available in WileyPLUS. 40. H Review Conceptual Example 5 before attempting this problem. As the drawing shows, the length of a guitar string is 0.628 m. The frets are
numbered for convenience. A performer can play a musical scale on a single
string because the spacing between the frets is designed according to the fol- lowing rule: When the string is pushed against any fret j, the fundamental frequency of the shortened string is larger by a factor of the twelfth root of two
( 12 √ 2 ) than it is when the string is pushed against the fret j – 1. Assuming
that the tension in the string is the same for any note, fi nd the spacing
(a) between fret 1 and fret 0 and (b) between fret 7 and fret 6.
0234567 1
0.628 m
PROBLEM 40
Section 17.6 Longitudinal Standing Waves,
Section 17.7 Complex Sound Waves 41. E BIO SSM Sound enters the ear, travels through the auditory canal, and reaches the eardrum. The auditory canal is approximately a tube open
at only one end. The other end is closed by the eardrum. A typical length
for the auditory canal in an adult is about 2.9 cm. The speed of sound is
343 m/s. What is the fundamental frequency of the canal? (Interestingly,
Copper block
Part 1 Part 2
PROBLEM 35
Additional Problems 487
the fundamental frequency is in the frequency range where human hearing
is most sensitive.)
42. E GO A tube with a cap on one end, but open at the other end, has a fundamental frequency of 130.8 Hz. The speed of sound is 343 m/s (a) If the cap is removed, what is the new fundamental frequency of the tube? (b) How long is the tube?
43. E An organ pipe is open at both ends. It is producing sound at its third harmonic, the frequency of which is 262 Hz. The speed of sound is 343 m/s.
What is the length of the pipe?
44. E The range of human hearing is roughly from twenty hertz to twenty kilohertz. Based on these limits and a value of 343 m/s for the speed of
sound, what are the lengths of the longest and shortest pipes (open at both
ends and producing sound at their fundamental frequencies) that you expect
to fi nd in a pipe organ?
45. E MMH The fundamental frequencies of two air columns are the same. Column A is open at both ends, while column B is open at only one end. The
length of column A is 0.70 m. What is the length of column B?
46. E Available in WileyPLUS. 47. E SSM A tube is open only at one end. A certain harmonic produced by the tube has a frequency of 450 Hz. The next higher harmonic has a
frequency of 750 Hz. The speed of sound in air is 343 m/s. (a) What is the integer n that describes the harmonic whose frequency is 450 Hz? (b) What is the length of the tube?
48. M V-HINT A thin 1.2-m aluminum rod sustains a longitudinal standing wave with vibration antinodes at each end of the rod. There are no other
antinodes. The density and Young’s modulus of aluminum are, respect-
ively, 2700 kg/m3 and 6.9 × 1010 N/m2. What is the frequency of the rod’s
vibration?
49. M CHALK SSM A person hums into the top of a well and fi nds that stand- ing waves are established at frequencies of 42, 70.0, and 98 Hz. The fre-
quency of 42 Hz is not necessarily the fundamental frequency. The speed of
sound is 343 m/s. How deep is the well?
50. M GO A vertical tube is closed at one end and open to air at the other end. The air pressure is 1.01 × 105 Pa. The tube has a length of 0.75 m. Mercury
(mass density = 13 600 kg/m3) is poured into it to shorten the eff ective length
for standing waves. What is the absolute pressure at the bottom of the mer-
cury column, when the fundamental frequency of the shortened, air-fi lled
tube is equal to the third harmonic of the original tube?
51. M V-HINT Available in WileyPLUS. 52. H Available in WileyPLUS.
53. E A string is fi xed at both ends and is vibrating at 130 Hz, which is its third harmonic frequency. The linear density of the string is 5.6 × 10–3 kg/m,
and it is under a tension of 3.3 N. Determine the length of the string.
54. E GO One method for measuring the speed of sound uses standing waves. A cylindrical tube is open at both ends, and one end admits sound
from a tuning fork. A movable plunger is inserted into the other end at a
distance L from the end of the tube where the tuning fork is. For a fi xed fre- quency, the plunger is moved until the smallest value of L is measured that allows a standing wave to be formed. Suppose that the tuning fork produces
a 485-Hz tone, and that the smallest value observed for L is 0.264 m. What is the speed of sound in the gas in the tube?
55. E SSM Available in WileyPLUS. 56. E Available in WileyPLUS. 57. E BIO Divers working in underwater chambers at great depths must deal with the danger of nitrogen narcosis (the “bends”), in which nitrogen
dissolves into the blood at toxic levels. One way to avoid this danger
is for divers to breathe a mixture containing only helium and oxygen.
Helium, however, has the eff ect of giving the voice a high-pitched quality,
like that of Donald Duck’s voice. To see why this occurs, assume for
simplicity that the voice is generated by the vocal cords vibrating above
a gas-fi lled cylindrical tube that is open only at one end. The quality of
the voice depends on the harmonic frequencies generated by the tube;
larger frequencies lead to higher-pitched voices. Consider two such tubes at
20 °C. One is fi lled with air, in which the speed of sound is 343 m/s. The
other is fi lled with helium, in which the speed of sound is 1.00 × 103 m/s.
To see the eff ect of helium on voice quality, calculate the ratio of the nth natural frequency of the helium-fi lled tube to the nth natural frequency of the air-fi lled tube.
58. E MMH The drawing graphs a string on which two pulses (half up and half down) are traveling at a constant speed of 1 cm/s at t = 0 s. Using the principle of linear superposition, draw the shape of the string at t = 1 s, 2 s, 3 s, and 4 s.
PROBLEM 58
1 cm/s 1 cm/s
0 2 4 6 8 10 12
Distance, cm
59. E SSM The A string on a string bass vibrates at a fundamental fre- quency of 55.0 Hz. If the string’s tension were increased by a factor of four,
what would be the new fundamental frequency?
60. M V-HINT Available in WileyPLUS. 61. M V-HINT The two speakers in the drawing are vibrating in phase, and a listener is standing at point P. Does constructive or destructive interfer-
ence occur at P when the speakers produce sound waves whose frequency is
(a) 1466 Hz and (b) 977 Hz? Justify your answers with appropriate calcula- tions. Take the speed of sound to be 343 m/s.
PROBLEM 61 P
1.813 m 1.187 m
2.200 m
62. H Available in WileyPLUS. 63. H SSM The arrangement in the drawing shows a block (mass = 15.0 kg) that is held in position on a frictionless incline by a cord (length = 0.600 m).
Additional Problems
488 CHAPTER 17 The Principle of Linear Superposition and Interference Phenomena
The mass per unit length of the cord is 1.20 × 10–2 kg/m, so the mass of the
cord is negligible compared to the mass of the block. The cord is being vi-
brated at a frequency of 165 Hz (vibration source not shown in the drawing).
What are the values of the angle 𝜃 between 15.0° and 90.0° at which a stand- ing wave exists on the cord?
PROBLEM 63 θ
64. M GO A fl autist is playing a fl ute as discussed in Example 6, but now the temperature is 305 K instead of 293 K. As a result, the speed of sound
is no longer 343 m/s. Therefore, with the length calculated in Example 6,
the note middle C does not have the proper fundamental frequency of
261.6 Hz. In other words, the fl ute is out of tune. To adjust the tuning, the
fl autist can alter the fl ute’s length by changing the extent to which the head
joint (see Figure 17.21) is inserted into the main stem of the instrument. To what length must the fl ute be adjusted to play middle C at its proper
frequency?
67. M An Acoustic Remote Control. You and your team are exploring an antiquated research facility in the mountains of southern Argentina that had
been abandoned in the 1960s. You come to a giant locked door that has no
visible handles or actuators, but you fi nd a hand-held device nearby that has
two buttons, labeled “Open” and “Close.” It looks like some kind of crude re-
mote control, but when you push the buttons they just click and nothing hap-
pens. You open the device’s top cover and inspect it. The internal mechanism
resembles an old acoustic remote control called the “Space Command 600”
that your parents had for their ancient TV. Pushing a button on the remote ac-
tuated a small hammer on the inside that struck the end of an aluminum rod,
about 2 or 3 cm in length. The rod vibrated and emitted an ultrasonic sound
wave that actuated an electrical circuit in the TV that was sensitive to that
frequency. The TV remote had three buttons, and therefore three rods that
vibrated at diff erent frequencies. The fi rst frequency turned the TV on and off ,
the second made the tuning dial click to the next station, and the third made
the dial turn in the opposite direction. You pull off the cover of the device
and fi nd that it has places for two ¼-inch diameter rods, but both are missing.
However, written on the inside of the cover of the device is the following:
“Open = 95.50 kHz” and “Close = 102.50 kHz.” Your team members search
and eventually fi nd a long piece of ¼-inch diameter aluminum rod. (a) To what lengths must you cut the rod in order to get the remote to work properly
(i.e., so that the fundamental frequencies of the rods match those utilized by
the remote)? (b) Suppose you had instead found a titanium rod. What lengths would be required in that case? (Young’s moduli are YAl = 6.9 × 1010 N/m2 and YTi = 1.2 × 1011 N/m2; the mass densities are ρAl = 2700 kg/m3 and ρTi = 4500 kg/m3.) 68. M A Tunable Inclined Plane. You and your team are designing a tun- able, single-tone, acoustic emitter. One end of a string is connected to a post
on the top of a frictionless inclined plane. The string supports a mass at rest
below, on the surface of the plane. The angle of the incline relative to the
horizontal (θ) is adjustable. The length of the string is L = 35.0 cm, and the mass per unit length of the string is λ = 5.28 × 10–3 kg/m. (a) When θ = 17.0°, the plucked string is supposed to emit a fundamental frequency of f = 212 Hz. What value of the mass (M) is needed under these conditions? (b) What is the full frequency range of the device (i.e., by changing the angle)?
(c) With the mass calculated in part (a), to what value should you set θ so that the fundamental frequency is 330 Hz?
Team Problems
Diff raction is the bending of a traveling wave around an obstacle or around
the edges of an opening, and is one of the consequences of superposition.
Problem 65 compares diff raction in two diff erent media and reviews some
of the fundamental properties of sound waves. Problem 66 deals with stand-
ing waves of sound in a gas. One of the factors that aff ects the formation of
standing waves is the speed at which the individual waves travel. Problem 66
reviews how the speed of sound depends on the properties of the gas.
65. M CHALK SSM A sound wave with a frequency of 15 kHz emerges through a circular opening that has a diameter of 0.20 m. Concepts: (i) The diff raction angle for a wave emerging through a circular opening is given
by sin 𝜃 = 1.22 𝜆/D, where 𝜆 is the wavelength of the sound and D is the diameter of the opening. What is meant by the diff raction angle? (ii) How is
the wavelength related to the frequency of the sound? (iii) Is the wavelength
of the sound in air greater than, smaller than, or equal to the wavelength in
water? Why? (Note: The speed of sound in air is 343 m/s and the speed of
sound in water is 1482 m/s.) (iv) Is the diff raction angle of the sound in air
greater than, smaller than, or equal to the diff raction angle in water? Explain.
Calculations: Find the diff raction angle 𝜃 when the sound travels (a) in air and (b) in water. 66. M CHALK Two tubes of gas are identical and are open only at one end. One tube contains neon (Ne) and the other krypton (Kr). Both are monatomic
gases, have the same temperature, and may be assumed to be ideal gases. The
fundamental frequency of the tube containing neon is 481 Hz. Concepts: (i) For a gas-fi lled tube open only at one end, the fundamental frequency
(n = 1) is f1 = 𝜐/(4L), where 𝜐 is the speed of sound and L is the length of the tube. How is the speed related to the properties of the gas? (ii) All of the
factors that aff ect the speed of sound in this problem are the same except for
the atomic masses, which are given by 20.180 u for neon, and 83.80 u for
krypton. Is the speed of sound in krypton greater than, smaller than, or equal
to the speed of sound in neon? Why? (iii) Is the fundamental frequency of the
tube containing krypton greater than, less than, or equal to the fundamental
frequency of the tube containing neon? Explain. Calculations: What is the fundamental frequency of the tube containing krypton?
Concepts and Calculations Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
18.1 Define electric charge.
18.2 Describe the electric force between charged particles.
18.3 Distinguish between conductors and insulators.
18.4 Explain charging by contact and charging by induction.
18.5 Use Coulomb’s law to calculate the force on a point charge due to other point charges.
18.6 Calculate the net electric field due to a configuration of point charges.
18.7 Draw electric field lines.
18.8 Describe the electric field inside a conductor.
18.9 Use Gauss’ law to obtain the value of the electric field due to charge distributions.
18.10 Describe how copiers and printers operate.
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CHAPTER 18
Electric Forces and Electric Fields
The silvery globe in the photograph is part of a Van de Graaff generator, which is a device that can separate the
electric charges that are one of the fundamental building blocks of atoms. Since she is touching the globe, all
parts of the girl’s body, including her hair, acquire the same kind of electric charge. The charges do not simply
fl ow through her body into the earth, because she is standing on a platform that prevents that from happening.
As we will see in this chapter, like charges repel each other, which is why the girl’s hair is standing on end.
18.1 The Origin of Electricity The electrical nature of matter is inherent in atomic structure. An atom consists of a
small, relatively massive nucleus that contains particles called protons and neutrons.
A proton has a mass of 1.673 × 10‒27 kg, and a neutron has a slightly greater mass of
1.675 × 10‒27 kg. Surrounding the nucleus is a diff use cloud of orbiting particles called
electrons, as Figure 18.1 suggests. An electron has a mass of 9.11 × 10‒31 kg. Like mass, electric charge is an intrinsic property of protons and electrons, and only two types of charge have been discovered, positive and negative. A proton has a positive
charge, and an electron has a negative charge. A neutron has no net electric charge.
Experiment reveals that the magnitude of the charge on the proton exactly equals the magnitude of the charge on the electron; the proton carries a charge +e, and the electron carries a charge ‒e. The SI unit for measuring the magnitude of an electric charge is the coulomb* (C), and e has been determined experimentally to have the value
e = 1.60 × 10‒19 C
489 *The defi nition of the coulomb depends on electric currents and magnetic fi elds, concepts that will be
discussed later. Therefore, we postpone its defi nition until Section 21.7.
490 CHAPTER 18 Electric Forces and Electric Fields
The symbol e represents only the magnitude of the charge on a proton or an electron and does not include the algebraic sign that indicates whether the charge is positive or negative.
In nature, atoms are normally found with equal numbers of protons and electrons. Usu-
ally, then, an atom carries no net charge because the algebraic sum of the positive charge of the
nucleus and the negative charge of the electrons is zero. When an atom, or any object, carries no
net charge, the object is said to be electrically neutral. The neutrons in the nucleus are electrically neutral particles.
Charges of larger magnitude than the charge on an electron or on a proton are built up on an
object by adding or removing electrons. Thus, any charge of magnitude q is an integer multiple of e; that is, q = Ne, where N is an integer. Because any electric charge q occurs in integer mul- tiples of elementary, indivisible charges of magnitude e, electric charge is said to be quantized. Example 1 emphasizes the quantized nature of electric charge.
+
–
–
–
–
–
+ + + +
electron proton neutron
FIGURE 18.1 An atom contains a small, positively charged nucleus, about which
the negatively charged electrons move. The
closed-loop paths shown here are symbolic
only. In reality, the electrons do not follow
discrete paths, as Section 30.5 discusses.
EXAMPLE 1 A Lot of Electrons
How many electrons are there in one coulomb of negative charge?
Reasoning The negative charge is due to the presence of excess elec- trons, since they carry negative charge. Because each electron has a
charge whose magnitude is e = 1.60 × 10‒19 C, the number of electrons is equal to the charge magnitude of one coulomb (1.00 C) divided by e.
Solution The number N of electrons is
N = 1.00 C
e =
1.00 C
1.60 × 10−19 C = 6.25 × 1018
18.2 Charged Objects and the Electric Force Electricity has many useful applications that have come about because it is possible to transfer
electric charge from one object to another. Usually electrons are transferred, and the body that
gains electrons acquires an excess of negative charge. The body that loses electrons has an excess
of positive charge. Such separation of charge occurs often when two unlike materials are rubbed
together. For example, when an ebonite (hard, black rubber) rod is rubbed against animal fur,
some of the electrons from atoms of the fur are transferred to the rod. The ebonite becomes
negatively charged, and the fur becomes positively charged, as Figure 18.2 indicates. Similarly, if a glass rod is rubbed with a silk cloth, some of the electrons are removed from the atoms of
the glass and deposited on the silk, leaving the silk negatively charged and the glass positively
charged. There are many familiar examples of charge separation, as when you walk across a nylon
rug or run a comb through dry hair. In each case, objects become “electrifi ed” as surfaces rub
against one another.
When an ebonite rod is rubbed with animal fur, the rubbing process serves only to sepa-
rate electrons and protons already present in the materials. No electrons or protons are created
Ebonite rod
Animal fur
– – –– – – +
+ + +
+ +
FIGURE 18.2 When an ebonite rod is rubbed against animal fur, electrons from atoms of
the fur are transferred to the rod. This transfer
gives the rod a negative charge (‒) and leaves
a positive charge (+) on the fur.
18.2 Charged Objects and the Electric Force 491
or destroyed. Whenever an electron is transferred to the rod, a proton is left behind on the fur.
Since the charges on the electron and proton have identical magnitudes but opposite signs, the
algebraic sum of the two charges is zero, and the transfer does not change the net charge of the
fur/rod system. If each material contains an equal number of protons and electrons to begin
with, the net charge of the system is zero initially and remains zero at all times during the rub-
bing process.
Electric charges play a role in many situations other than rubbing two surfaces together. They
are involved, for instance, in chemical reactions, electric circuits, and radioactive decay. A great
number of experiments have verifi ed that in any situation, the law of conservation of electric charge is obeyed.
LAW OF CONSERVATION OF ELECTRIC CHARGE During any process, the net electric charge of an isolated system remains constant (is conserved).
It is easy to demonstrate that two electrically charged objects exert a force on one another.
Consider Interactive Figure 18.3a, which shows two small balls that have been oppositely charged and are light and free to move. The balls attract each other. On the other hand, balls with the same type of charge, either both positive or both negative, repel each other, as parts b and c of the drawing indicate. The behavior depicted in Interactive Figure 18.3 illustrates the following fundamental characteristic of electric charges:
Like charges repel and unlike charges attract each other.
Like other forces that we have encountered, the electric force (also sometimes called the electrostatic force) can alter the motion of an object. It can do so by contributing to the net external force ΣF→ that acts on the object. Newton’s second law, ΣF→ = m a→, specifi es the acceleration a→ that arises because of the net external force. Any external electric force that acts on an object must be included when determining the net external force to be used in the
second law.
THE PHYSICS OF . . . electronic ink. A new technology based on the electric force may revolutionize the way books and other printed matter are made. This technology, called
electronic ink, allows letters and graphics on a page to be changed instantly, much like the
symbols displayed on a computer monitor. Figure 18.4a illustrates the essential features of electronic ink. It consists of millions of clear microcapsules, each having the diameter of a
human hair and fi lled with a dark, inky liquid. Inside each microcapsule are several dozen
extremely tiny white beads that carry a slightly negative charge. The microcapsules are sand-
wiched between two sheets, an opaque base layer and a transparent top layer, at which the
reader looks. When a positive charge is applied to a small region of the base layer, as shown
in part b of the drawing, the negatively charged white beads are drawn to it, leaving dark ink at the top layer. Thus, a viewer sees only the dark liquid. When a negative charge is applied
to a region of the base layer, the negatively charged white beads are repelled from it and are
forced to the top of the microcapsules; now a viewer sees a white area due to the beads. Thus,
electronic ink is based on the principle that like charges repel and unlike charges attract each
other; a positive charge causes one color to appear, and a negative charge causes another color
to appear. Each small region, whether dark or light, is known as a pixel (short for “picture ele- ment”). Computer chips provide the instructions to produce the negative and positive charges
on the base layer of each pixel. Letters and graphics are produced by the patterns generated
with the two colors.
(a)
+ –
(b)
– – + +
(c)
INTERACTIVE FIGURE 18.3 (a) A positive charge (‒) and a negative charge (+) attract
each other. (b) Two negative charges repel each other. (c) Two positive charges repel each other.
492 CHAPTER 18 Electric Forces and Electric Fields
Check Your Understanding
(The answers are given at the end of the book.) 1. An electrically neutral object acquires a net electric charge. Which one of the following statements
concerning the mass of the object is true? (a) The mass does not change. (b) The mass increases if the charge is positive and decreases if it is negative. (c) The mass increases if the charge is negative and decreases if it is positive.
2. Object A and object B are each electrically neutral. Two million electrons are removed from object A and placed on object B. Expressed in coulombs, what is the resulting charge (algebraic sign and mag-
nitude) on object A and on object B?
3. Object A has a charge of ‒1.6 × 10‒13 C, and object B is electrically neutral. Two million electrons are removed from object A and placed on object B. Expressed in coulombs, what is the resulting charge
(algebraic sign and magnitude) on object A and on object B?
(b)
(a)
Base layer
Base layer
Microcapsules
Dark pixel
Light pixel
Dark liquid
Beads
FIGURE 18.4 (a) Electronic ink consists of microcapsules fi lled with a dark, inky liquid and dozens of white beads. (b) Dark and light pixels are formed when positive and negative charges are placed in the base layer by electronic circuitry.
18.4 Charging by Contact and by Induction 493
18.3 Conductors and Insulators Electric charge can not only exist on an object, but it can also move through an object. However, materials diff er vastly in their abilities to allow electric charge to move or be conducted through
them. To help illustrate such diff erences in conductivity, Figure 18.5a recalls the conduction of heat through a bar of material whose ends are maintained at diff erent temperatures. As Section 13.2
discusses, metals conduct heat readily and, therefore, are known as thermal conductors. On the
other hand, substances that conduct heat poorly are referred to as thermal insulators.
A situation analogous to the conduction of heat arises when a metal bar is placed between
two charged objects, as in Figure 18.5b. Electrons are conducted through the bar from the nega- tively charged object toward the positively charged object. Substances that readily conduct electric
charge are called electrical conductors. Although there are exceptions, good thermal conductors are generally good electrical conductors. Metals such as copper, aluminum, silver, and gold are
excellent electrical conductors and, therefore, are used in electrical wiring. Materials that con-
duct electric charge poorly are known as electrical insulators. In many cases, thermal insulators are also electrical insulators. Common electrical insulators are rubber, many plastics, and wood.
Insulators, such as the rubber or plastic that coats electrical wiring, prevent electric charge from
going where it is not wanted.
The diff erence between electrical conductors and insulators is related to atomic structure.
As electrons orbit the nucleus, those in the outer orbits experience a weaker force of attraction to
the nucleus than do those in the inner orbits. Consequently, the outermost electrons (also called
the valence electrons) can be dislodged more easily than the inner ones. In a good conductor,
some valence electrons become detached from a parent atom and wander more or less freely
throughout the material, belonging to no one atom in particular. The exact number of electrons
detached from each atom depends on the nature of the material, but is usually between one and
three. When one end of a conducting bar is placed in contact with a negatively charged object
and the other end in contact with a positively charged object, as in Figure 18.5b, the “free” electrons are able to move readily away from the negative end and toward the positive end. The
ready movement of electrons is the hallmark of a good conductor. In an insulator the situation is
diff erent, for there are very few electrons free to move throughout the material. Virtually every
electron remains bound to its parent atom. Without the “free” electrons, there is very little fl ow
of charge when the material is placed between two oppositely charged bodies, so the material is
an electrical insulator.
18.4 Charging by Contact and by Induction When a negatively charged ebonite rod is rubbed on a metal object, such as the sphere in Animated Figure 18.6a, some of the excess electrons from the rod are transferred to the object. Once the electrons are on the metal sphere (where they can move readily) and the rod is removed, they
repel one another and spread out over the sphere’s surface. The insulated stand prevents them
from fl owing to the earth, where they could spread out even more. As shown in part b of the picture, the sphere is left with a negative charge distributed over its surface. In a similar manner,
the sphere would be left with a positive charge after being rubbed with a positively charged rod.
In this case, electrons from the sphere would be transferred to the rod. The process of giving one
object a net electric charge by placing it in contact with another object that is already charged is
known as charging by contact. It is also possible to charge a conductor in a way that does not involve contact. In Animated
Figure 18.7, a negatively charged rod is brought close to, but does not touch, a metal sphere. In
– – – – – – – –
– – – – – – –
– – – –
– –
– ––
–
–
– – – –
Metal sphere
Insulated stand
Ebonite rod
(a) (b)
ANIMATED FIGURE 18.6 (a) Electrons are transferred by rubbing the negatively charged
rod on the metal sphere. (b) When the rod is removed, the electrons distribute themselves
over the surface of the sphere.
(a)
Heat Hotter object
Cooler object
(b)
–
–
–
–Negatively charged object
Positively charged object
+ + + + + +
– – – – – –
FIGURE 18.5 (a) Heat is conducted from the hotter end of the metal bar to the cooler
end. (b) Electrons are conducted from the negatively charged end of the metal bar to the
positively charged end.
494 CHAPTER 18 Electric Forces and Electric Fields
the sphere, the free electrons closest to the rod move to the other side, as part a of the drawing indicates. As a result, the part of the sphere nearest the rod becomes positively charged and the
part farthest away becomes negatively charged. These positively and negatively charged regions
have been “induced” or “persuaded” to form because of the repulsive force between the negative
rod and the free electrons in the sphere. If the rod were removed, the free electrons would return
to their original places, and the charged regions would disappear.
Under most conditions the earth is a good electrical conductor. So when a metal wire is
attached between the sphere and the ground, as in Animated Figure 18.7b, some of the free electrons leave the sphere and distribute themselves over the much larger earth. If the ground-
ing wire is then removed, followed by the ebonite rod, the sphere is left with a positive net
charge, as part c of the picture shows. The process of giving one object a net electric charge without touching the object to a second charged object is called charging by induction. The process could also be used to give the sphere a negative net charge, if a positively charged rod
were used. Then, electrons would be drawn up from the ground through the grounding wire
and onto the sphere.
If the sphere in Animated Figure 18.7 were made from an insulating material like plastic, instead of metal, the method of producing a net charge by induction would not work, because
very little charge would fl ow through the insulating material and down the grounding wire. How-
ever, the electric force of the charged rod would have some eff ect on the insulating material.
The electric force would cause the positive and negative charges in the molecules of the material
to separate slightly, with the negative charges being “pushed” away from the negative rod, as
Figure 18.8 illustrates. Although no net charge is created, the surface of the plastic does acquire a slight induced positive charge and is attracted to the negative rod. It is attracted in spite of the
repulsive force between the negative rod and the negative charges in the plastic. This is because
the negative charges in the plastic are further away from the rod than the positive charges are.
For a similar reason, one piece of cloth can stick to another in the phenomenon known as “static
cling,” which occurs when an article of clothing has acquired an electric charge while being
tumbled about in a clothes dryer.
Check Your Understanding
(The answers are given at the end of the book.) 4. Two metal spheres are identical. They are
electrically neutral and are touching. An
electrically charged ebonite rod is then
brought near the spheres without touching
them, as CYU Figure 18.1 shows. After a while, with the rod held in place, the
spheres are separated, and the rod is then
removed. The following statements refer
to the masses mA and mB of the spheres after they are separated and the rod is removed. Which one or more of the statements is true? (a) mA = mB (b) mA > mB if the rod is positive (c) mA < mB if the rod is positive (d) mA > mB if the rod is negative (e) mA < mB if the rod is negative
5. Blow up a balloon, tie it shut, and rub it against your shirt a number of times, so that the balloon acquires a net electric charge. Now touch the balloon to the ceiling. When released, will the balloon
remain stuck to the ceiling?
Ebonite rod
Positive surface charge
Plastic
– – – –
– – –
+ –
+ –
+ –
+ –
FIGURE 18.8 The negatively charged rod induces a slight positive surface charge on
the plastic.
– – – –
– – – –
– – – –
– – – –
– – – –
– – – –
– – – – – –
–+++
+ +
+
+
Ebonite rod
(a)
––
+++
+ +
+
+
(b)
++
++
+
(c)
Metal sphere Grounding
wire
Insulated stand
Connection to ground
ANIMATED FIGURE 18.7 (a) When a charged rod is brought near the metal sphere
without touching it, some of the positive and
negative charges in the sphere are separated.
(b) Some of the electrons leave the sphere through the grounding wire, with the result
(c) that the sphere acquires a positive net charge.
A B
CYU FIGURE 18.1
18.5 Coulomb’s Law 495
6. A rod made from insulating material carries a net charge (which may be positive or negative), whereas a copper sphere is electrically neutral. The rod is held close to the sphere but does not touch it. Which
one of the following statements concerning the forces that the rod and sphere exert on each other is
true? (a) The forces are always attractive. (b) The forces are always repulsive. (c) The forces are attrac- tive when the rod is negative and repulsive when it is positive. (d) The forces are repulsive when the rod is negative and attractive when it is positive. (e) There are no forces.
18.5 Coulomb’s Law The Force That Point Charges Exert on Each Other The electrostatic force that stationary charged objects exert on each other depends on the amount
of charge on the objects and the distance between them. Experiments reveal that the greater the
charge and the closer together they are, the greater is the force. To set the stage for explaining
these features in more detail, Figure 18.9 shows two charged bodies. These objects are so small, compared to the distance r between them, that they can be regarded as mathematical points. The “point charges” have magnitudes* |q1| and |q2|. If the charges have unlike signs, as in part a of the picture, each object is attracted to the other by a force that is directed along the line between them; +F→ is the electric force exerted on object 1 by object 2 and −F→ is the electric force exerted on object 2 by object 1. If, as in part b, the charges have the same sign (both positive or both negative), each object is repelled from the other. The repulsive forces, like the attractive forces, act along the line between the charges. Whether attractive or repulsive, the two forces are equal
in magnitude but opposite in direction. These forces always exist as a pair, each one acting on a
diff erent object, in accord with Newton’s action–reaction law.
The French physicist Charles Augustin de Coulomb (1736–1806) carried out a number
of experiments to determine how the electric force that one point charge applies to another
depends on the amount of each charge and the separation between them. His result, now known
as Coulomb’s law, is stated as follows:
COULOMB’S LAW The magnitude F of the electrostatic force exerted by one point charge q1 on another point charge q2 is directly proportional to the magnitudes |q1| and |q2| of the charges and inversely proportional to the square of the distance r between them:
F = k ∣q1∣∣q2∣
r 2 (18.1)
where k is a proportionality constant: k = 8.99 × 109 N · m2/C2 in SI units. Equation 18.1 gives only the magnitude of the electrostatic force that each point charge exerts on the other; it does not give the direction. The electrostatic force is directed along the line join- ing the charges, and it is attractive if the charges have unlike signs and repulsive if the charges have like signs.
It is common practice to express k in terms of another constant 𝜀0, by writing k = 1/(4𝜋𝜀0); 𝜀0 is called the permittivity of free space and has a value that is given according to 𝜀0 = 1/(4𝜋k) = 8.85 × 10‒12 C2/(N · m2). Example 2 illustrates the use of Coulomb’s law.
*The magnitude of a variable is sometimes called the absolute value and is symbolized by a vertical bar to the left and
to the right of the variable. Thus, |q| denotes the magnitude or absolute value of the variable q, which is the value of q without its algebraic plus or minus sign. For example, if q = −2.0 C, then |q| = 2.0 C.
(a)
r
(b)
q1 q2+ + –F +F
r
q1 q2+ – –F+F
FIGURE 18.9 Each point charge exerts a force on the other. Regardless of whether
the forces are (a) attractive or (b) repulsive, they are directed along the line between the
charges and have equal magnitudes.
Math Skills When using Equation 18.1, substitute only the charge magnitudes (without algebraic signs) for |q1| and |q2|. Do not substitute negative numbers for these symbols. This is because the equa- tion gives only the magnitude of the electrostatic force, and the magnitude of a force cannot be negative.
For example, suppose that q1 = −5.0 × 10−6 C and q2 = +7.0 × 10−6 C. Then, for use in Equation 18.1, we would have the following values:
∣q1 ∣ = ∣−5.0 × 10−6 C∣ = 5.0 × 10−6 C (not − 5.0 × 10−6 C) ∣q2 ∣ = ∣+7.0 × 10−6 C∣ = 7.0 × 10−6 C
496 CHAPTER 18 Electric Forces and Electric Fields
The force calculated in Example 2 corresponds to about 2000 pounds and is so large
because charges of ±1.0 C are enormous. Such large charges are rare and are encountered
only in the most severe conditions, as in a lightning bolt, where as much as 25 C can be
transferred between the cloud and the ground. The typical charges produced in the labora-
tory are much smaller and are measured conveniently in microcoulombs (1 microcoulomb =
1 𝜇C = 10‒6 C). Coulomb’s law has a form that is remarkably similar to Newton’s law of gravitation (F =
Gm1m2/r2). The force in both laws depends on the inverse square (1/r2) of the distance between the two objects and is directed along the line between them. In addition, the force is proportional
to the product of an intrinsic property of each of the objects, the magnitudes of the charges |q1| and |q2| in Coulomb’s law and the masses m1 and m2 in the gravitation law. However, there is a major diff erence between the two laws. The electrostatic force can be either repulsive or attrac-
tive, depending on whether or not the charges have the same sign; in contrast, the gravitational
force is always an attractive force. Section 5.5 discusses how the gravitational attraction between the earth and a satellite pro-
vides the centripetal force that keeps a satellite in orbit. Example 3 illustrates that the electrostatic
force of attraction plays a similar role in a famous model of the atom created by the Danish physi-
cist Niels Bohr (1885–1962).
EXAMPLE 2 A Large Attractive Force
Two objects, whose charges are +1.0 and ‒1.0 C, are separated by 1.0 km.
Compared to 1.0 km, the sizes of the objects are small. Find the magni-
tude of the attractive force that either charge exerts on the other.
Reasoning Considering that the sizes of the objects are small compared to the separation distance, we can treat the charges as point charges. Cou-
lomb’s law may then be used to fi nd the magnitude of the attractive force,
provided that only the magnitudes of the charges are used for the symbols |q1| and |q2| that appear in the law.
Solution The magnitude of the force is
F = k ∣q1 ⃒ ∣q2 ⃒
r 2 =
(8.99 × 10 9 N · m2 /C2 )(1.0 C)(1.0 C) (1.0 × 10 3 m) 2
(18.1)
= 9.0 × 10 3 N
Analyzing Multiple-Concept Problems
EXAMPLE 3 A Model of the Hydrogen Atom
In the Bohr model of the hydrogen atom, the electron (charge = ‒e) is in a circular orbit about the nuclear proton (charge = +e) at a radius of 5.29 × 10‒11 m, as Figure 18.10 shows. The mass of the electron is 9.11 × 10‒31 kg. Determine the speed of the electron.
Reasoning Recall from Section 5.3 that a net force is required to keep an object such as an electron moving on a circular path. This net force
is called the centripetal force and always points toward the center of the
circle. The centripetal force has a magnitude given by Fc = m𝜐2/r, where m and 𝜐 are, respectively, the mass and speed of the electron and r is the radius of the orbit. This equation can be solved for the speed of the
electron. Since the mass and orbital radius are known, we can calculate
the electron’s speed provided that a value for the centripetal force can be
found. For the electron in the hydrogen atom, the centripetal force is pro-
vided almost exclusively by the electrostatic force that the proton exerts
on the electron. This attractive force points toward the center of the circle,
and its magnitude is given by Coulomb’s law. The electron is also pulled
toward the proton by the gravitational force. However, the gravitational
force is negligible in comparison to the electrostatic force.
r
–e
+e v
FIGURE 18.10 In the Bohr model of the hydrogen atom, the electron (−e) orbits the proton (+e) at a distance that is r = 5.29 × 10−11 m. The velocity of the electron is v→.
18.5 Coulomb’s Law 497
Knowns and Unknowns The data for this problem are:
Description Symbol Value Electron charge ‒e ‒1.60 × 10‒19 C
Electron mass m 9.11 × 10‒31 kg
Proton charge +e +1.60 × 10‒19 C
Radius of orbit r 5.29 × 10‒11 m
Unknown Variable Orbital speed of electron 𝜐 ?
Modeling the Problem
STEP 1 Centripetal Force An electron of mass m that moves with a constant speed 𝜐 on a circular path of radius r experiences a net force, called the centripetal force. The magnitude Fc of this force is given by Fc = m𝜐2/r (Equation 5.3). By solving this equation for the speed, we obtain Equation 1 at the right. The mass and radius in this expression are known. However, the
magnitude of the centripetal force is not known, so we will evaluate it in Step 2.
STEP 2 Coulomb’s Law As the electron orbits the proton in the hydrogen atom, it is attracted to the proton by the electrostatic force. The magnitude F of the electrostatic force is given by Coulomb’s law as F = k|q1||q2|/r2 (Equation 18.1), where |q1| and |q2| are the magnitudes of the charges, r is the orbital radius, and k = 8.99 × 109 N · m2/C2. Since the centripetal force is provided almost entirely by the electrostatic force, it follows that Fc = F. Furthermore, |q1| = |‒e| and |q2| = |+e|. With these substitutions, Equation 18.1 becomes
Fc = k ∣−e∣ ∣+e∣
r 2
All the variables on the right side of this expression are known, so we substitute it into Equation 1,
as indicated in the right column.
Solution Algebraically combining the results of the modeling steps, we have
υ = √rFc m = √r(k ∣−e∣∣+e∣
r2 )
m = √k ∣−e∣∣+e∣ mr
The speed of the orbiting electron is
υ = √k ∣−e∣ ∣+e∣mr = √(8.99 × 10
9 N · m2/C 2 ) ∣ −1.60 × 10−19 C ∣ ∣ +1.60 × 10−19 C ∣ (9.11 × 10−31 kg)(5.29 × 10−11 m)
= 2.19 × 10 6 m /s
Related Homework: Problems 19, 23
STEP 1 STEP 2
υ = √rFc m (1) ?
υ = √rFc m (1)
Fc = k ∣−e∣∣+e∣
r 2
THE PHYSICS OF . . . adhesion. Since the electrostatic force depends on the inverse square of the distance between the charges, it becomes larger for smaller distances, such as those
involved when a strip of adhesive tape is stuck to a smooth surface. Electrons shift over the small
distances between the tape and the surface. As a result, the materials become oppositely charged.
Since the distance between the charges is relatively small, the electrostatic force of attraction is
large enough to contribute to the adhesive bond. Figure 18.11 shows an image of the sticky sur- face of a piece of tape after it has been pulled off a metal surface. The image was obtained using
an atomic-force microscope and reveals the tiny pits left behind when microscopic portions of the
adhesive remain stuck to the metal because of the strong adhesive bonding forces.
498 CHAPTER 18 Electric Forces and Electric Fields
The Force on a Point Charge Due to Two or More Other Point Charges Up to now, we have been discussing the electrostatic force on a point charge (magnitude |q1|) due to another point charge (magnitude |q2|). Suppose that a third point charge (magnitude |q3|) is also present. What would be the net force on q1 due to both q2 and q3? It is convenient to deal with such a problem in parts. First, fi nd the magnitude and direction of the force exerted on q1 by q2 (ignoring q3). Then, determine the force exerted on q1 by q3 (ignoring q2). The net force on q1 is the vector sum of these forces. Examples 4 and 5 illustrate this approach when the charges lie along a straight line and on a plane, respectively.
FIGURE 18.11 After a strip of tape has been pulled off a metal surface, there are tiny pits
in the sticky surface of the tape, as this image
shows. It was obtained using an atomic-
force microscope. (Courtesy Louis Scudiero
and J.Thomas Dickinson, Washington State
University)
m
1.5
1.0
0.5
EXAMPLE 4 Three Charges on a Line
Figure 18.12a shows three point charges that lie along the x axis in a vacuum. Determine the magnitude and direction of the net electrostatic
force on q1.
Reasoning Part b of the drawing shows a free-body diagram of the forces that act on q1. Since q1 and q2 have opposite signs, they attract one another. Thus, the force exerted on q1 by q2 is F12
→ , and it points to the
left. Similarly, the force exerted on q1 by q3 is F13 →
and is also an attractive force. It points to the right in Figure 18.12b. The magnitudes of these forces can be obtained from Coulomb’s law. The net force is the vector
sum of F12 →
and F13 →
.
Solution In calculating the magnitudes of the individual forces with the aid of Equation 18.1, we use only the magnitudes of the charges (without
algebraic signs):
F12 = k ∣q1∣ ∣q2∣
r 12
2 =
(8.99 × 10 9 N · m2/C2 )(3.0 × 10−6 C)(4.0 × 10−6 C) (0.20 m)2
= 2.7 N
F13 = k ∣q1∣ ∣q3∣
r 13
2 =
(8.99 × 10 9 N · m2/C2 )(3.0 × 10−6 C)(7.0 × 10−6 C) (0.15 m)2
= 8.4 N
Since F12 →
points in the negative x direction, and F13 →
points in the positive
x direction, the net force F→ is
F →
= F12 →
+ F13 →
= (−2.7 N) + (8.4 N) = +5.7 N
The plus sign in the answer indicates that the net force points to the right
in the drawing.
q2
−4.0 μC +3.0 μC −7.0 μC
0.20 m 0.15 m q1 q3
(a)
F12 F13 +x
(b) Free-body diagram for q1
q1
FIGURE 18.12 (a) Three charges lying along the x axis. (b) The force exerted on q1 by q2 is F12
→ , while the force exerted on q1 by
q3 is F13 →
.
EXAMPLE 5 Three Charges in a Plane
Figure 18.13a shows three point charges that lie in the x, y plane in a vacuum. Find the magnitude and direction of the net electrostatic force
on q1.
Reasoning The force exerted on q1 by q2 is F12 →
and is an attractive force because the two charges have opposite signs. It points along the line
between the charges. The force exerted on q1 by q3 is F13 →
and is also an
18.5 Coulomb’s Law 499
Math Skills As discussed in Section 1.7, the vector components of the force F→ (magnitude = F) are two perpendicular vectors Fx
→
and Fy →
that are parallel to the x and y axes, respectively, and add vectorially so that F→ = Fx
→ + Fy
→ . The scalar component Fx has a
magnitude equal to that of the vector component Fx →
and is given a
positive sign if Fx →
points along the +x axis and a negative sign if Fx →
points along the −x axis. The scalar component Fy is defi ned simi- larly. Figure 18.14 shows the vector F→ and its components. Since the components are perpendicular, the shaded triangle is a right
triangle, and we can use the Pythagorean theorem (Equation 1.7).
This theorem states that the square of the length of the hypotenuse
of a right triangle is equal to the sum of the squares of the lengths
of the other two sides. The hypotenuse of the shaded triangle is F, and the other two sides are Fx and Fy. Thus, we have that
F 2 = F 2x + F 2y or F = √F 2x + F 2y To determine the angle 𝜃 we apply the tangent function (tan 𝜃).
According to Equation 1.3, tan 𝜃 is the length of the side of the
triangle opposite the angle 𝜃 divided by the length of the side ad-
jacent to the angle 𝜃. Thus, referring to Figure 18.14 to identify
these lengths, we see that tan θ = Fy Fx
. This equation means that 𝜃
is the angle whose tangent is Fy Fx
, a result that can be expressed by
using the inverse tangent function (tan−1):
θ = tan−1 ( Fy Fx)
F
Fx
Fy
+x
+y
θ
FIGURE 18.14 Math Skills drawing.
attractive force. It points along the line between q1 and q3. Coulomb’s law specifi es the magnitudes of these forces. Since the forces point in diff er-
ent directions (see Figure 18.13b), we will use vector components to fi nd the net force.
Solution The magnitudes of the forces are
F12 = k ∣q1∣ ∣q2∣
r 12
2 =
(8.99 × 10 9 N · m2 /C2 )(4.0 × 10−6 C)(6.0 × 10−6 C) (0.15 m) 2
= 9.6 N
F13 = k ∣q1∣ ∣q3∣
r 13
2 =
(8.99 × 10 9 N · m2 /C 2 ) (4.0 × 10−6 C)(5.0 × 10−6 C) (0.10 m) 2
= 18 N
The net force F→ is the vector sum of F12 →
and F13 →
, as part b of the draw- ing shows. The components of F→ that lie in the x and y directions are Fx →
and Fy →
, respectively. Our approach to fi nding F→ is the same as that used in Chapters 1 and 4. The forces F12
→ and F13
→ are resolved into x
and y components. Then, the x components are combined to give Fx →
,
and the y components are combined to give Fy →
. Once Fx →
and Fy →
, are known, the magnitude and direction of F→ can be determined using trigonometry.
Force x component y component
F12 → +(9.6 N) cos 73° = +2.8 N +(9.6 N) sin 73° = +9.2 N
F13 → +18 N 0 N
F→ Fx →
= +21 N Fy →
= +9.2 N
The magnitude F and the angle 𝜃 of the net force are
F = √Fx2 + Fy 2 = √(21 N) 2 + (9.2 N) 2 = 23 N
θ = tan−1 ( Fy Fx
) = tan−1 (9.2 N 21 N ) = 24°
q1 F13
F12
+x
+y
F
(a)
q1 q3 r13 = 0.10 m
q2 –6.0 μC
r 1 2
= 0.
15 m
73°
73° F12 sin 73°
F12 cos 73°
F12
(b) Free-body diagram for q1
+4.0 μC –5.0 μC
θ
FIGURE 18.13 (a) Three charges lying in a plane. (b) The net force acting on q1 is F→ = F12
→ + F13
→ . The angle that F→ makes with the +x axis is 𝜃.
500 CHAPTER 18 Electric Forces and Electric Fields
Check Your Understanding
(The answers are given at the end of the book.) 7. Identical point charges are fi xed to diagonally opposite corners of a square. Where does a third point
charge experience the greater force? (a) At the center of the square (b) At one of the empty corners (c) The question is unanswerable because the polarities of the charges are not given.
8. CYU Figure 18.2 shows three point charges arranged in three diff erent ways. The charges are +q, ‒q, and ‒q; each has the same magnitude, with one positive and the other two negative. In each of the arrangements the distance d is the same. Rank the arrangements in descending order (largest fi rst) according to the magnitude of the net electrostatic force that acts on the positive charge.
–q +q d d
–q
B
–q
+q 90°
d
d –q
C
+q –q d d
–q
A
CYU FIGURE 18.2
9. A proton and an electron are held in place on the x axis. The proton is at x = ‒d, while the electron is at x = +d. They are released simultaneously, and the only force that aff ects their motions signifi - cantly is the electrostatic force of attraction that each applies to the other. Which particle reaches
the origin fi rst?
10. A particle is attached to one end of a horizontal spring, and the other end of the spring is attached to a wall. When the particle is pushed so that the spring is compressed more and more, the particle experi-
ences a greater and greater force from the spring. Similarly, a charged particle experiences a greater and
greater force when pushed closer and closer to another particle that is fi xed in position and has a charge
of the same polarity. Considering this similarity, will the charged particle exhibit simple harmonic
motion on being released, as will the particle on the spring?
18.6 The Electric Field
Definition As we know, a charge can experience an electrostatic force due to the presence of other charges.
For instance, the positive charge q0 in Figure 18.15 experiences a force F →
, which is the vector
sum of the forces exerted by the charges on the rod and the two spheres. It is useful to think of
q0 as a test charge for determining the extent to which the surrounding charges generate a force. However, in using a test charge, we must be careful to select one with a very small magnitude,
so that it does not alter the locations of the other charges. The next example illustrates how the
concept of a test charge is applied.
– – – – –
– – – – –
Ebonite rod
+ + +
+ + +
+
+
––– – – – – –
– ––
–
F
q0
FIGURE 18.15 A positive charge q0 experiences an electrostatic force F→ due to the surrounding charges on the ebonite rod
and the two spheres.
EXAMPLE 6 A Test Charge
The positive test charge shown in Figure 18.15 is q0 = +3.0 × 10‒8 C and experiences a force F = 6.0 × 10‒8 N in the direction shown in the drawing. (a) Find the force per coulomb that the test charge experiences. (b) Using the result of part (a), predict the force that a charge of +12 × 10‒8 C would experience if it replaced q0.
Reasoning The charges in the environment apply a force F→ to the test charge q0. The force per coulomb experienced by the test charge is F
→ /q0.
If q0 is replaced by a new charge q, then the force on this new charge is the force per coulomb times q.
18.6 The Electric Field 501
– – – – –
– – – – –
Ebonite rod
+ + +
+ + +
+
+
––– – – – – –
– ––
–
F
q0
FIGURE 18.15 (REPEATED) A positive charge q0 experi- ences an electrostatic force
F→ due to the surrounding charges on the ebonite rod
and the two spheres.
Solution (a) The force per coulomb of charge is
F→
q0 =
6.0 × 10−8 N
3.0 × 10−8 C = 2.0 N/C
The direction of the force per coulomb is the same as the direction of F→ in Figure 18.15.
(b) The result from part (a) indicates that the surrounding charges can exert 2.0 newtons of force per coulomb of charge. Thus, a charge of +12 ×
10‒8 C would experience a force whose magnitude is
F = (2.0 N/C)(12 × 10‒8 C) = 24 × 10−8 N
The direction of this force would be the same as the direction of the force
experienced by the test charge, since both have the same positive sign.
The electric force per coulomb, F →
/q0, calculated in Example 6(a) is one illustration of an idea that is very important in the study of electricity. The idea is called the electric fi eld. Equation 18.2 presents the defi nition of the electric fi eld.
DEFINITION OF THE ELECTRIC FIELD The electric fi eld E→ that exists at a point is the electrostatic force F→ experienced by a small test charge* q0 placed at that point divided by the charge itself:
E→ = F →
q0 (18.2)
The electric fi eld is a vector, and its direction is the same as the direction of the force F→ on a positive test charge. SI Unit of Electric Field: newton per coulomb (N/C)
Equation 18.2 indicates that the unit for the electric fi eld is that of force divided by charge, which
is a newton/coulomb (N/C) in SI units.
It is the surrounding charges that create an electric fi eld at a given point. Any positive or negative charge placed at the point interacts with the fi eld and, as a result, experiences a force, as
the next example indicates.
EXAMPLE 7 An Electric Field Leads to a Force
In Figure 18.16 the charges on the two metal spheres and the ebonite rod create an electric fi eld E→ at the spot indicated. This fi eld has a magnitude of 2.0 N/C and is directed as in the drawing. Determine the force on a
charge placed at that spot, if the charge has a value of (a) q0 = +18 × 10‒8 C and (b) q0 = ‒24 × 10‒8 C.
Reasoning The electric fi eld at a given spot can exert a variety of forces, depending on the magnitude and sign of the charge placed there.
The charge is assumed to be small enough that it does not alter the loca-
tions of the surrounding charges that create the fi eld.
Solution (a) The magnitude of the force is the product of the magnitudes of q0 and E
→ :
F = |q0| E = (18 × 10−8 C)(2.0 N/C) = 36 × 10−8 N (18.2)
Since q0 is positive, the force points in the same direction as the electric fi eld, as part a of the drawing indicates.
(b) In this case, the magnitude of the force is
F = |q0| E = (24 × 10−8 C)(2.0 N/C) = 48 × 10−8 N (18.2)
The force on the negative charge points in the direction opposite to the force on the positive charge—that is, opposite to the electric fi eld (see
part b of the drawing).
*As long as the test charge is small enough that it does not disturb the surrounding charges, it may be either positive or
negative. Compared to a positive test charge, a negative test charge of the same magnitude experiences a force of the same
magnitude that points in the opposite direction. However, the same electric fi eld is given by Equation 18.2, in which F→ is replaced by −F→ and q0 is replaced by −q0.
502 CHAPTER 18 Electric Forces and Electric Fields
At a particular point in space, each of the surrounding charges contributes to the net elec-
tric fi eld that exists there. To determine the net fi eld, it is necessary to obtain the various
contributions separately and then fi nd the vector sum of them all. Such an approach is an illus-
tration of the principle of linear superposition, as applied to electric fi elds. (This principle is
introduced in Section 17.1, in connection with waves.) Example 8 emphasizes the vector nature
of the electric fi eld.
– – – – –
– – – – – – – – – –
– – – – –
+ ++ + +
+
+
+
–– – – –
– – – – – ––
F
E
(a)
+ ++ + +
+
+
+
–– – – –
– – – – – ––
(b)
+18 × 10–8 C –24 × 10–8 C
F
E
FIGURE 18.16 The electric fi eld E→ that exists at a given spot can exert a variety of
forces. The force exerted depends on the
magnitude and sign of the charge placed at
that spot. (a) The force on a positive charge points in the same direction as E→, while (b) the force on a negative charge points opposite to E→.
EXAMPLE 8 Electric Fields Add as Vectors Do
Animated Figure 18.17 shows two charged objects, A and B. Each contributes as follows to the net electric fi eld at point P: E→A = 3.00 N/C directed to the right, and E→B = 2.00 N/C directed downward. Thus, E
→
A and E→B are perpendicular. What is the net electric fi eld at P?
Reasoning The net electric fi eld E→ is the vector sum of E→A and E →
B: E→ = E
→
A + E →
B. As illustrated in Animated Figure 18.17, E →
A and E →
B are perpendicular, so E→ is the diagonal of the rectangle shown in the drawing. Thus, we can use the Pythagorean theorem to fi nd the magnitude of E→ and trigonometry to fi nd the directional angle 𝜃.
Solution The magnitude of the net electric fi eld is
E = √EA2 + EB2 = √(3.00 N/C) 2 + (2.00 N/C) 2 = 3.61 N/C
The direction of E→ is given by the angle 𝜃 in the drawing:
θ = tan−1 ( E B EA
) = tan−1 ( 2.00 N/C 3.00 N/C ) = 33.7°
P A
E
EA
EB
+ + +
+ + +
B + +
+ +
θ
ANIMATED FIGURE 18.17 The electric fi eld contributions E→A and E
→
B, which come from
the two charge distributions, are added
vectorially to obtain the net fi eld E→ at point P.
Point Charges A more complete understanding of the electric fi eld concept can be gained by considering the
fi eld created by a point charge, as in the following example.
EXAMPLE 9 The Electric Field of a Point Charge
There is an isolated point charge of q = +15 𝜇C in a vacuum at the left in Figure 18.18a. Using a test charge of q0 = +0.80 𝜇C, determine the electric fi eld at point P, which is 0.20 m away.
Reasoning Following the defi nition of the electric fi eld, we place the test charge q0 at point P, determine the force acting on the test charge, and then divide the force by the test charge.
18.6 The Electric Field 503
Problem-Solving Insight Equation 18.3 gives only the magnitude of the electric fi eld produced by a point charge. Therefore, do not use negative numbers for the symbol |q| in this equation.
The electric fi eld produced by a point charge q can be obtained in general terms from Coulomb’s law. First, note that the magnitude of the force exerted by the charge q on a test charge q0 is F = k|q||q0|/r2. Then, divide this value by |q0| to obtain the magnitude of the fi eld. Since |q0| is eliminated algebraically from the result, the electric fi eld does not depend on the test charge:
Point charge q E = k ∣q∣ r2
(18.3)
As in Coulomb’s law, the symbol |q| denotes the magnitude of q in Equation 18.3, without regard to whether q is positive or negative. If q is positive, then E→ is directed away from q, as in Figure 18.18b. On the other hand, if q is negative, then E→ is directed toward q, since a negative charge attracts a positive test charge. For instance, Figure 18.18c shows the electric fi eld that would exist at P if there were a charge of ‒q instead of +q at the left of the drawing. Example 10 reemphasizes the fact that all the surrounding charges make a contribution to the electric fi eld
that exists at a given place.
Solution Coulomb’s law (Equation 18.1) gives the magnitude of the force:
F = k ∣q0∣ ∣q∣
r 2 =
(8.99 × 10 9 N · m2/C 2 )(0.80 × 10−6 C)(15 × 10−6 C) (0.20 m) 2
= 2.7 N
Equation 18.2 gives the magnitude of the electric fi eld:
E = F
∣q0∣ =
2.7 N
0.80 × 10−6 C = 3.4 × 10 6 N/C
The electric fi eld E→ points in the same direction as the force F→ on the positive test charge. Since the test charge experiences a force of repulsion
directed to the right, the electric fi eld vector also points to the right, as
Figure 18.18b shows.
(a)
r
P
q0q
F
(b)
q
E
(c)
q
E
+
+
–
FIGURE 18.18 (a) At location P, a positive test charge q0 experiences a repulsive force F→ due to the positive point charge q. (b) At P, the electric fi eld E→ is directed to the right. (c) If the charge q were negative rather than positive, the
electric fi eld would have the same
magnitude as in (b) but would point to the left.
EXAMPLE 10 The Electric Fields from Separate Charges May Cancel
Two positive point charges, q1 = +16 𝜇C and q2 = +4.0 𝜇C, are separated in a vacuum by a distance of 3.0 m, as Figure 18.19 illustrates. Find the spot on the line between the charges where the net electric fi eld is zero.
Reasoning Between the charges the two fi eld contributions have oppo- site directions, and the net electric fi eld is zero at the place where the
magnitude of E→1 equals the magnitude of E →
2. However, since q2 is smaller than q1, this location must be closer to q2, in order that the fi eld of the smaller charge can balance the fi eld of the larger charge. In the drawing,
the cancellation spot is labeled P, and its distance from q1 is d.
Solution At P, E1 = E2, and using the expression E = k|q|/r 2 (Equation 18.3), we have
k (16 × 10−6 C) d2
= k (4.0 × 10−6 C)
(3.0 m − d)2
Rearranging this expression shows that 4.0(3.0 m ‒ d)2 = d2. Taking the square root of each side of this equation reveals that
2.0(3.0 m − d) = ± d
d
P q1 q2 + +
E2 E1
3.0 m
FIGURE 18.19 The two point charges q1 and q2 create electric fi elds E
→
1 and E →
2 that
cancel at a location P on the line between the charges.
The plus and minus signs on the right occur because either the positive or
negative root can be taken. Therefore, there are two possible values for d: +2.0 m and +6.0 m. The value +6.0 m corresponds to a location off to
the right of both charges, where the magnitudes of E→1 and E →
2 are equal,
but where the directions are the same. Thus, E→1 and E →
2 do not cancel at
this spot. The other value for d corresponds to the location shown in the drawing and is the zero-fi eld location: d = +2.0 m .
504 CHAPTER 18 Electric Forces and Electric Fields
When point charges are arranged in a symmetrical fashion, it is often possible to deduce use-
ful information about the magnitude and direction of the electric fi eld by taking advantage of the
symmetry. Conceptual Example 11 illustrates the use of this technique.
CONCEPTUAL EXAMPLE 11 Symmetry and the Electric Field
Four point charges all have the same magnitude, but they do not all have
the same sign. These charges are fi xed to the corners of a rectangle in two
diff erent ways, as Figure 18.20 shows. Consider the net electric fi eld at the center C of the rectangle in each case. In which case, if either, is the net electric fi eld greater? (a) It is greater in Figure 18.20a. (b) It is greater in Figure 18.20b. (c) The fi eld has the same magnitude in both cases. Reasoning The net electric fi eld at C is the vector sum of the individual fi elds created there by the charges at each corner. Each of the individual fi elds
has the same magnitude, since the charges all have the same magnitude and
are equidistant from C. The directions of the individual fi elds are diff erent, however. The fi eld created by a positive charge points away from the charge,
and the fi eld created by a negative charge points toward the charge.
Answers (a) and (c) are incorrect. To see why these answers are incor- rect, note that the charges on corners 2 and 4 are identical in both parts of
Figure 18.20. Moreover, in Figure 18.20a the charges at corners 1 and 3 are both +q, so they contribute individual fi elds of the same magnitude at C that have opposite directions and, therefore, cancel. However, in Figure 18.20b the charges at corners 1 and 3 are ‒q and +q, respectively. They contribute individual fi elds of the same magnitude at C that have the same directions and do not cancel, but combine to produce the fi eld E→13 shown in Figure 18.20b. The fact that this contribution to the net fi eld at C is present in Figure 18.20b but not in Figure 18.20a means that the net fi elds in the two cases are diff erent and that the net fi eld in Figure 18.20a is less than (not greater than) the net fi eld in Figure 18.20b. Answer (b) is correct. To assess the net fi eld at C, we need to consider the contribution from the charges at corners 2 and 4, which are ‒q and +q, respectively, in both cases. This is just like the arrangement on corners 1
and 3, which was discussed previously. It leads to a contribution to the net
fi eld at C that is shown as E→24 in both parts of the fi gure. In Figure 18.20a the net fi eld at C is just E→24, but in Figure 18.20b it is the vector sum of E→13 and E
→
24, which is clearly greater than either of these two values alone.
Related Homework: Problem 41
C
1 2
4 3
(a)
E24
C
(b)
E24E13
E
+q −q
+q +q
−q −q
+q +q
FIGURE 18.20 Charges of identical magnitude are placed at
the corners of a rectangle. However,
the charges do not all have the same
sign and give rise to diff erent
electric fi elds at the center C of the rectangle, depending on the
signs that they have.
The Parallel Plate Capacitor Equation 18.3, which gives the electric fi eld of a point charge, is a very useful result. With the
aid of integral calculus, this equation can be applied in a variety of situations where point charges
are distributed over one or more surfaces. One such example that has considerable practical
importance is the parallel plate capacitor. As Figure 18.21 shows, this device consists of two parallel metal plates, each with area A. A charge +q is spread uniformly over one plate, while a charge ‒q is spread uniformly over the other plate. In the region between the plates and away from the edges, the electric fi eld points from the positive plate toward the negative plate and is
perpendicular to both. It can be shown (see Example 15 in Section 18.9) that this electric fi eld
has a magnitude of
Parallel plate capacitor E = q
ε0 A =
σ ε0
(18.4)
where 𝜀0 is the permittivity of free space. In this expression the Greek symbol sigma (𝜎) denotes the charge per unit area (𝜎 = q/A) and is sometimes called the charge density. Except in the
+q
–q
Area = A
E
E
+ +
+ +
+
+ +
+ +
+
+ +
+ +
+
+ +
+ +
+
– –
– –
–
– –
– –
–
– –
– –
–
– –
– –
–
E
FIGURE 18.21 A parallel plate capacitor.
18.7 Electric Field Lines 505
region near the edges, the fi eld has the same value at all places between the plates. The fi eld does
not depend on the distance from the charges, in distinct contrast to the fi eld created by an isolated point charge.
Check Your Understanding
(The answers are given at the end of the book.) 11. There is an electric fi eld at point P. A very small positive charge is placed at this point and experiences
a force. Then the positive charge is replaced by a very small negative charge that has a magnitude dif-
ferent from that of the positive charge. Which one of the following statements is true concerning the
forces that these charges experience at P? (a) They are identical. (b) They have the same magnitude but diff erent directions. (c) They have diff erent magnitudes but the same direction. (d) They have diff erent magnitudes and diff erent directions.
12. Suppose that in Figure 18.20a point charges ‒q are fi xed in place at corners 1 and 3 and point charges +q are fi xed in place at corners 2 and 4. What then would be the net electric fi eld at the center C of the rectangle?
13. A positive point charge +q is fi xed in position at the center of a square, as CYU Figure 18.3 shows. A second point charge is fi xed to corner B, C, or D. The net electric fi eld that results at corner A is zero. (a) At which corner is the second charge located? (b) Is the second charge posi- tive or negative? (c) Does the second charge have a greater, a smaller, or the same magnitude as the charge at the center?
14. A positive point charge is located to the left of a negative point charge. When both charges have the same magnitude, there is no place on the
line passing through both charges where the net electric fi eld due to the
two charges is zero. Suppose, however, that the negative charge has a
greater magnitude than the positive charge. On which part of the line, if
any, is a place of zero net electric fi eld now located? (a) To the left of the positive charge (b) Between the two charges (c) To the right of the negative charge (d) There is no zero place.
15. Three point charges are fi xed to the corners of a square, one to a corner, in such a way that the net electric fi eld at the empty corner is zero. Do these charges all have (a) the same sign and (b) the same magnitude (but, possibly, diff erent signs)?
16. Consider two identical, thin, and nonconducting rods, A and B. On rod A, positive charge is spread evenly, so that there is the same amount of charge per unit length at every point. On rod B, positive
charge is spread evenly over only the left half, and the same amount of negative charge is spread evenly
over the right half. For each rod deduce the direction of the electric fi eld at a point that is located directly above the midpoint of the rod.
18.7 Electric Field Lines As we have seen, electric charges create an electric fi eld in the space around them. It is useful to
have a kind of “map” that gives the direction and strength of the fi eld at various places. The great
English physicist Michael Faraday (1791–1867) proposed an idea that provides such a “map”—
the idea of electric fi eld lines. Since the electric fi eld is the electric force per unit charge, fi eld lines are also called lines of force.
To introduce the electric fi eld line concept, Figure 18.22a shows a positive point charge +q. At the locations numbered 1–8, a positive test charge would experience a repulsive force, as the
arrows in the drawing indicate. Therefore, the electric fi eld created by the charge +q is directed radially outward. The electric fi eld lines are lines drawn to show this direction, as Figure 18.22b illustrates. They begin on the charge +q and point radially outward. Figure 18.23 shows the fi eld lines in the vicinity of a negative charge ‒q. In this case they are directed radially inward because the force on a positive test charge is one of attraction, indicating that the electric fi eld
points inward. In general, electric fi eld lines are always directed away from positive charges and toward negative charges.
The electric fi eld lines in Figures 18.22 and 18.23 are drawn in only two dimensions, as a matter of convenience. Field lines radiate from the charges in three dimensions, and an infi nite
CYU FIGURE 18.3
+q
A B
D C
506 CHAPTER 18 Electric Forces and Electric Fields
number of lines could be drawn. However, for clarity only a small number are ever included in
pictures. The number is chosen to be proportional to the magnitude of the charge; thus, fi ve times
as many lines would emerge from a +5q charge as from a +q charge. The pattern of electric fi eld lines also provides information about the magnitude or strength
of the fi eld. Notice that in Figures 18.22 and 18.23, the lines are closer together near the charges, where the electric fi eld is stronger. At distances far from the charges, where the electric fi eld is
weaker, the lines are more spread out. It is true in general that the electric fi eld is stronger in
regions where the fi eld lines are closer together. In fact, no matter how many charges are present,
the number of lines per unit area passing perpendicularly through a surface is proportional to the
magnitude of the electric fi eld.
In regions where the electric fi eld lines are equally spaced, there is the same number of lines
per unit area everywhere, and the electric fi eld has the same strength at all points. For example,
Figure 18.24 shows that the fi eld lines between the plates of a parallel plate capacitor are parallel and equally spaced, except near the edges where they bulge outward. The equally spaced, paral-
lel lines indicate that the electric fi eld has the same magnitude and direction at all points in the
central region of the capacitor.
Often, electric fi eld lines are curved, as in the case of an electric dipole. An electric dipole consists of two separated point charges that have the same magnitude but opposite signs. The
electric fi eld of a dipole is proportional to the product of the magnitude of one of the charges and
the distance between the charges. This product is called the dipole moment. Many molecules, such as H2O and HCl, have dipole moments. Figure 18.25 depicts the fi eld lines in the vicinity of a dipole. For a curved fi eld line, the electric fi eld vector at a point is tangent to the line at that point (see points 1, 2, and 3 in the drawing). The pattern of the lines for the dipole indicates that
the electric fi eld is greatest in the region between and immediately surrounding the two charges,
since the lines are closest together there.
Notice in Figure 18.25 that any given fi eld line starts on the positive charge and ends on the negative charge. This is a fundamental characteristic of electric fi eld lines:
Problem-Solving Insight Electric fi eld lines always begin on a positive charge and end on a negative charge and do not start or stop in midspace. Furthermore, the number of lines leaving
a positive charge or entering a negative charge is proportional to the magnitude of the charge.
This means, for example, that if 100 lines are drawn leaving a +4 𝜇C charge, then 75 lines would have to end on a ‒3 𝜇C charge and 25 lines on a ‒1 𝜇C charge. Thus, 100 lines leave the charge of +4 𝜇C and end on a total charge of ‒4 𝜇C, so the lines begin and end on equal amounts of total charge.
The electric fi eld lines are also curved in the vicinity of two identical charges. Figure 18.26 shows the pattern associated with two positive point charges and reveals that there is an absence
of lines in the region between the charges. The absence of lines indicates that the electric fi eld is
relatively weak between the charges.
Some of the important properties of electric fi eld lines are considered in Conceptual
Example 12.
+q –q
Edge view
+ + + + + + ++
+ + + + + ++
– – – – – – ––
– – – – – ––
FIGURE 18.24 In the central region of a parallel plate capacitor, the electric fi eld lines
are parallel and evenly spaced, indicating that
the electric fi eld there has the same magnitude
and direction at all points.
–q
FIGURE 18.23 The electric fi eld lines are directed radially inward toward a negative
point charge −q.
(a) (b)
8 2
7 3
6
5
1
4
+q +q
FIGURE 18.22 (a) At any of the eight marked spots around a positive point charge
+q, a positive test charge would experience a repulsive force directed radially outward.
(b) The electric fi eld lines are directed radially outward from a positive point
charge +q.
18.7 Electric Field Lines 507
–q
1
3
2
E1
E2
E3
+q
FIGURE 18.25 The electric fi eld lines of an electric dipole are curved and extend from the positive to the negative
charge. At any point, such as 1, 2, or 3, the fi eld created by
the dipole is tangent to the line through the point.
+q +q
FIGURE 18.26 The electric fi eld lines for two identical positive point charges. If the charges were both negative,
the directions of the lines would be reversed.
CONCEPTUAL EXAMPLE 12 Drawing Electric Field Lines
Figure 18.27 shows four choices for the electric fi eld lines between three negative point charges (‒q, ‒q, and ‒2q) and one positive point charge (+4q). Which of these choices is the only one of the four that could pos- sibly show a correct representation of the fi eld lines? (a) Figure 18.27a (b) Figure 18.27b (c) Figure 18.27c (d) Figure 18.27d
Reasoning Electric fi eld lines begin on positive charges and end on negative charges. The tangent to a fi eld line at a point gives the direction
of the electric fi eld at that point. Equally spaced parallel fi eld lines indi-
cate that the fi eld has a constant value (magnitude and direction) in the
corresponding region of space.
Answer (a) is incorrect. Field lines can never cross, as they do at point P in Figure 18.27a. If two fi eld lines were to intersect, there would be two electric fi elds at the point of intersection, one associated with each line.
However, there can only be one value of the electric fi eld at a given point.
−q
−q
(c) (d)
P
+4q+4q
−2q
−q
−q
(a)
+4q
−2q
−q
−q
(b)
+4q
−2q
−q
−q
−2q
FIGURE 18.27 Only one of these drawings shows a representation of the electric fi eld
lines between the charges that could be correct.
(See Conceptual Example 12.)
508 CHAPTER 18 Electric Forces and Electric Fields
Check Your Understanding
(The answers are given at the end of the book.) 17. Drawings A and B in CYU Figure 18.4 show two examples
of electric fi eld lines. Which (one or more) of the follow-
ing statements are true, and which (one or more) are false?
(a) In both A and B the electric fi eld is the same everywhere. (b) As you move from left to right in each case, the electric fi eld becomes stronger. (c) The electric fi eld in A is the same everywhere, but it becomes stronger in B as you move from
left to right. (d) The electric fi elds in both A and B could be created by negative charges located somewhere on the left and positive
charges somewhere on the right. (e) Both A and B arise from a single positive point charge located somewhere on the left.
18. A positively charged particle is moving horizontally when it enters the region between the plates of a parallel plate capacitor, as CYU Figure 18.5 illustrates. When the particle is within the capacitor, which of the following
vectors, if any, are parallel to the electric fi eld lines inside the capacitor? (a) The particle’s displacement (b) Its velocity (c) Its linear momentum (d) Its acceleration
18.8 The Electric Field Inside a Conductor: Shielding In conducting materials such as copper, electric charges move readily in response to the forces
that electric fi elds exert. This property of conducting materials has a major eff ect on the electric
fi eld that can exist within and around them. Suppose that a piece of copper carries a number of
excess electrons somewhere within it, as in Figure 18.28a. Each electron would experience a force of repulsion because of the electric fi eld of its neighbors. And, since copper is a conductor,
the excess electrons move readily in response to that force. In fact, as a consequence of the 1/r2 dependence on distance in Coulomb’s law, they rush to the surface of the copper. Once static
equilibrium is established with all of the excess charge on the surface, no further movement of
charge occurs, as part b of the drawing indicates. Similarly, excess positive charge also moves to the surface of a conductor. In general, at equilibrium under electrostatic conditions, any excess charge resides on the surface of a conductor.
Now consider the interior of the copper in Figure 18.28b. The interior is electrically neutral, although there are still free electrons that can move under the infl uence of an electric fi eld. The
absence of a net movement of these free electrons indicates that there is no net electric fi eld pres-
ent within the conductor. In fact, the excess charges arrange themselves on the conductor surface
precisely in the manner needed to make the electric fi eld zero within the material. Thus, at equi- librium under electrostatic conditions, the electric fi eld is zero at any point within a conducting material. This fact has some fascinating implications.
a constant magnitude and direction. However, the fi eld between the +4q charge and the ‒2q charge certainly is stronger in places close to either of the charges. The fi eld lines should, therefore, have a curved nature,
similar (but not identical) to the fi eld lines that surround a dipole.
Answer (c) is correct. Figure 18.27c contains none of the errors discussed previously and, therefore, is the only drawing that could be
correct.
Related Homework: Problems 32, 63
Answer (b) is incorrect. The number of fi eld lines that leave a positive charge or end on a negative charge is proportional to the magnitude of the
charge. Since 8 lines leave the +4q charge, one-half of them (or 4) must end on the ‒2q charge, and one-fourth of them (or 2) must end on each of the ‒q charges. Figure 18.27b incorrectly shows 5 lines ending on the ‒2q charge and 1 line ending on one of the ‒q charges.
Answer (d) is incorrect. Figure 18.27d is incorrect because the fi eld lines between the +4q charge and the ‒2q charge are parallel and evenly spaced, which would indicate that the fi eld everywhere in this region has
+ v
– – – – –
+ + + + +
CYU FIGURE 18.5
CYU FIGURE 18.4
A B
(a)
(b)
– – – –– –––– –––––
–
––
– –
––
–
–
–
–
– – – –
–
–
–
–
–
–
–– –– – ––
FIGURE 18.28 (a) Excess charge within a conductor (copper) moves quickly (b) to the surface.
18.8 The Electric Field Inside a Conductor: Shielding 509
Figure 18.29a shows an uncharged, solid, cylindrical conductor at equilibrium in the cen- tral region of a parallel plate capacitor. Induced charges on the surface of the cylinder alter the
electric fi eld lines of the capacitor. Since an electric fi eld cannot exist within the conductor under
these conditions, the electric fi eld lines do not penetrate the cylinder. Instead, they end or begin
on the induced charges. Consequently, a test charge placed inside the conductor would feel no force due to the presence of the charges on the capacitor. In other words, the conductor shields any charge within it from electric fi elds created outside the conductor. The shielding results from the induced charges on the conductor surface.
THE PHYSICS OF . . . shielding electronic circuits. Since the electric fi eld is zero inside the conductor, nothing is disturbed if a cavity is cut from the interior of the material, as
in Figure 18.29b. Thus, the interior of the cavity is also shielded from external electric fi elds, a fact that has important applications, particularly for shielding electronic circuits. “Stray” elec-
tric fi elds are produced by various electrical appliances (e.g., hair dryers, blenders, and vacuum
cleaners), and these fi elds can interfere with the operation of sensitive electronic circuits, such as
those in stereo amplifi ers, televisions, and computers. To eliminate such interference, circuits are
often enclosed within metal boxes that provide shielding from external fi elds.
The blowup in Figure 18.29a shows another aspect of how conductors alter the electric fi eld lines created by external charges. The lines are altered because the electric fi eld just outside the surface of a conductor is perpendicular to the surface at equilibrium under electrostatic con- ditions. If the fi eld were not perpendicular, there would be a component of the fi eld parallel to the surface. Since the free electrons on the surface of the conductor can move, they would do so
under the force exerted by that parallel component. In reality, however, no electron fl ow occurs at
equilibrium. Therefore, there can be no parallel component, and the electric fi eld is perpendicular
to the surface.
The preceding discussion deals with features of the electric fi eld within and around a con-
ductor at equilibrium under electrostatic conditions. These features are related to the fact that
conductors contain mobile free electrons and do not apply to insulators, which contain very few free electrons. Conceptual Example 13 further explores the behavior of a conducting material in
the presence of an electric fi eld.
(a)
(b)
– – – – – – – – –
+ + + + + + + + +
Cylindrical conductor (end view)
90°
–
– –
– – – ––
+ + + + +
+ + –
– – – – ––
+ + + + +
+ +
E = 0 N/C inside cavity
FIGURE 18.29 (a) A cylindrical conductor (shown as an end view) is placed between
the oppositely charged plates of a capacitor.
The electric fi eld lines do not penetrate the
conductor. The blowup shows that, just outside
the conductor, the electric fi eld lines are
perpendicular to its surface. (b) The electric fi eld is zero in a cavity within the conductor.
CONCEPTUAL EXAMPLE 13 A Conductor in an Electric Field
A charge +q is suspended at the center of a hollow, electrically neutral, spherical, metallic conductor, as Figure 18.30 illustrates. The table shows a number of possibilities for the charges that this suspended charge in-
duces on the interior and exterior surfaces of the conductor. Which one of
the possibilities is correct?
Interior Surface Exterior Surface (a) −q 0 (b) −1 2q −
1
2q
(c) +q −q (d) −q +q
+q
+
+ +
+ +
+
+
+
–
– –
– –
– –
–
FIGURE 18.30 A positive charge +q is suspended at the center of a hollow spherical
conductor that is electrically
neutral. Induced charges appear
on the inner and outer surfaces
of the conductor. The electric
fi eld within the conductor itself
is zero.
510 CHAPTER 18 Electric Forces and Electric Fields
18.9 Gauss’ Law Section 18.6 discusses how a point charge creates an electric fi eld in the space around the
charge. There are also many situations in which an electric fi eld is produced by charges that are
spread out over a region, rather than by a single point charge. Such an extended collection of
charges is called a charge distribution. For example, the electric fi eld within the parallel plate capacitor in Figure 18.21 is produced by positive charges spread uniformly over one plate and an equal number of negative charges spread over the other plate. As we will see, Gauss’
law describes the relationship between a charge distribution and the electric fi eld it produces.
This law was formulated by the German mathematician and physicist Carl Friedrich Gauss
(1777–1855).
In presenting Gauss’ law, it will be necessary to introduce a new idea called electric fl ux. The idea of fl ux involves both the electric fi eld and the surface through which it passes. By bring-
ing together the electric fi eld and the surface through which it passes, we will be able to defi ne
electric fl ux and then present Gauss’ law.
We begin by developing a version of Gauss’ law that applies only to a point charge, which
we assume to be positive. The electric fi eld lines for a positive point charge radiate outward in all
directions from the charge, as Figure 18.22b indicates. The magnitude E of the electric fi eld at a distance r from the charge is E = kq/r2, according to Equation 18.3, in which we have replaced the symbol |q| with the symbol q since we are assuming that the charge is positive. As mentioned in Section 18.5, the constant k can be expressed as k = 1/(4𝜋𝜀0), where 𝜀0 is the permittivity of free space. With this substitution, the magnitude of the electric fi eld becomes E = q/(4𝜋𝜀0r2). We now place this point charge at the center of an imaginary spherical surface of radius r, as Figure 18.31 shows. Such a hypothetical closed surface is called a Gaussian surface, although in general it need not be spherical. The surface area A of a sphere is A = 4𝜋r2, and the magnitude of the electric fi eld can be written in terms of this area as E = q/(A𝜀0), or
Gauss’ law for a point charge
EA = q ε0
(18.5)
The left side of Equation 18.5 is the product of the magnitude E of the electric fi eld at any point on the Gaussian surface and the area A of the surface. In Gauss’ law this product is especially important and is called the electric fl ux, ΦE: ΦE = EA. (It will be necessary to modify this defi nition of fl ux when we consider the general case of a Gaussian surface with
an arbitrary shape.)
Equation 18.5 is the result we have been seeking, for it is the form of Gauss’ law that applies
to a point charge. This result indicates that, aside from the constant 𝜀0, the electric fl ux ΦE depends only on the charge q within the Gaussian surface and is independent of the radius r of the surface. We will now see how to generalize Equation 18.5 to account for distributions of charges and
Gaussian surfaces with arbitrary shapes.
Electric
fl ux ΦE
{
Answer (d) is correct. Since the fi eld lines emanating from the sus- pended positive charge +q terminate only on negative charges and do not penetrate the metal, there must be an induced negative charge on the interior surface. Furthermore, the lines begin and end on equal amounts
of charge, so the magnitude of the total charge induced on the interior
surface is the same as the magnitude of the suspended charge. Thus, the
charge induced on the interior surface is ‒q. We know that the total net charge on the metallic conductor must remain at zero. Therefore, if a
charge ‒q is induced on the interior surface, there must also be a charge of +q induced on the exterior surface, because excess charge cannot remain inside of the solid metal at equilibrium.
Related Homework: Problem 65
Reasoning Three facts will guide our analysis. First: Since the suspended charge does not touch the conductor, the net charge on the conductor must
remain zero, because it is electrically neutral to begin with. Second: Elec-
tric fi eld lines begin on positive charges and end on negative charges. Third:
At equilibrium under electrostatic conditions, there is no electric fi eld and,
hence, no fi eld lines inside the solid material of the metallic conductor.
Answers (a) and (b) are incorrect. The net charge on the conductor in each of these answers is ‒q, which cannot be, since the conductor’s net charge must remain zero.
Answer (c) is incorrect. Electric fi eld lines emanate from the sus- pended positive charge +q and must end on the interior surface of the metallic conductor, since they do not penetrate the metal. However, the
charge on the interior surface in this answer is positive, and fi eld lines
must end on negative charges. Thus, this answer is incorrect.
r
Spherical Gaussian surface
Electric field lines
+q
FIGURE 18.31 A positive point charge is located at the center of an imaginary spherical
surface of radius r. Such a surface is one example of a Gaussian surface. Here the
electric fi eld is perpendicular to the surface
and has the same magnitude everywhere on it.
18.9 Gauss’ Law 511
Interactive Figure 18.32 shows a charge distribution whose net charge is labeled Q. The charge distribution is surrounded by a Gaussian surface—that is, an imaginary closed surface.
The surface can have any arbitrary shape (it need not be spherical), but it must be closed (an open surface would be like that of half an eggshell). The direction of the electric fi eld is not necessarily
perpendicular to the Gaussian surface. Furthermore, the magnitude of the electric fi eld need not
be constant on the surface but can vary from point to point.
To determine the electric fl ux through such a surface, we divide the surface into many tiny
sections with areas ΔA1, ΔA2, and so on. Each section is so small that it is essentially fl at and the electric fi eld E
→ is a constant (both in magnitude and direction) over it. For reference, a dashed
line called the “normal” is drawn perpendicular to each section on the outside of the surface.
To determine the electric fl ux for each of the sections, we use only the component of E →
that is
perpendicular to the surface—that is, the component of the electric fi eld that passes through the
surface. From Interactive Figure 18.32 it can be seen that this component has a magnitude of E cos ϕ, where ϕ is the angle between the electric fi eld and the normal. The electric fl ux through any one section is then (E cos ϕ)ΔA. The electric fl ux ΦE that passes through the entire Gaussian surface is the sum of all of these individual fl uxes: ΦE = (E1 cos ϕ1)ΔA1 + (E2 cos ϕ2)ΔA2 + . . ., or
ΦE = Σ (E cos ϕ)∆A (18.6)
where, as usual, the symbol Σ means “the sum of.” Gauss’ law relates the electric fl ux ΦE to the
net charge Q enclosed by the arbitrarily shaped Gaussian surface.
GAUSS’ LAW The electric fl ux ΦE through a Gaussian surface is equal to the net charge Q enclosed by the surface divided by 𝜺0, the permittivity of free space:
Σ (E cos ϕ)∆A = Q ε0
(18.7)
SI Unit of Electric Flux: N · m2/C
Although we arrived at Gauss’ law by assuming the net charge Q was positive, Equation 18.7 also applies when Q is negative. In this case, the electric fl ux ΦE is also negative. Gauss’ law is often used to fi nd the magnitude of the electric fi eld produced by a distribution of charges. The law is
most useful when the distribution is uniform and symmetrical. In the next two examples we will
see how to apply Gauss’ law in such situations.
⏟⎵⎵⏟⎵⎵⏟ Electric fl ux, ΦE
Gaussian surface
Δ A
Normal
Charge distribution
EE cos
Q
ϕ
ϕ
INTERACTIVE FIGURE 18.32 The charge distribution Q is surrounded by an arbitrarily shaped Gaussian surface. The electric fl ux
Φ through any tiny segment of the surface
is the product of E cos ϕ and the area ΔA of the segment: Φ = (E cos ϕ)ΔA. The angle ϕ is the angle between the electric fi eld and the
normal to the surface.
EXAMPLE 14 The Electric Field of a Charged Thin Spherical Shell
Figures 18.33a and b show a thin spherical shell of radius R (for clarity, only half of the shell is shown). A positive charge q is spread uniformly over the shell. Find the magnitude of the electric fi eld at any point (a) outside the shell and (b) inside the shell.
Reasoning Because the charge is distributed uniformly over the spheri- cal shell, the electric fi eld is symmetrical. This means that the electric
fi eld is directed radially outward in all directions, and its magnitude is the
same at all points that are equidistant from the shell. All such points lie on
a sphere, so the symmetry is called spherical symmetry. With this sym- metry in mind, we will use a spherical Gaussian surface to evaluate the
electric fl ux ΦE. We will then use Gauss’ law to determine the magnitude
of the electric fi eld.
Solution (a) To fi nd the magnitude of the electric fi eld outside the charged shell, we evaluate the electric fl ux ΦE = Σ (E cos ϕ)ΔA by using a spherical Gaussian surface of radius r (r > R) that is concentric with the shell. See the blue surface labeled S in Figure 18.33a. Since the electric fi eld E→ is everywhere perpendicular to the Gaussian surface, ϕ = 0° and cos ϕ = 1. In addition, E has the same value at all points on the surface, since they are equidistant from the charged shell. Being
constant over the surface, E can be factored outside the summation, with the result that
ΦE = Σ (E cos 0°)∆A = E( Σ ∆A) = E(4πr2)
The term Σ ΔA is just the sum of the tiny areas that make up the Gaussian surface. Since the area of a spherical surface is 4𝜋r2, we have Σ ΔA = 4𝜋r2. Setting the electric fl ux equal to Q/𝜀0, as specifi ed by Gauss’ law, yields E(4𝜋r2) = Q/𝜀0. Since the only charge within the Gaussian sur- face is the charge q on the shell, it follows that the net charge within the Gaussian surface is Q = q. Thus, we can solve for E and fi nd that
E = q
4π𝜀0r 2 (for r > R)
This is a surprising result, for it is the same as that for a point charge (see
Equation 18.3 with |q| = q). Thus, the electric fi eld outside a uniformly charged spherical shell is the same as if all the charge q were concentrated as a point charge at the center of the shell.
{
Area of
Gaussian
surface
{ Surface area
of sphere
512 CHAPTER 18 Electric Forces and Electric Fields
is the net charge inside the Gaussian surface. But now Q = 0 C, since all the charge lies on the shell that is outside the surface S1. Consequently, we have E(4𝜋r12) = Q/𝜀0 = 0, or
E = 0 N/C (for r < R)
Gauss’ law allows us to deduce that there is no electric fi eld inside a uni-
form spherical shell of charge. An electric fi eld exists only on the outside.
(b) To fi nd the magnitude of the electric fi eld inside the charged shell, we select a spherical Gaussian surface that lies inside the shell and is con-
centric with it. See the blue surface labeled S1 in Figure 18.33b. Inside the charged shell, the electric fi eld (if it exists) must also have spherical
symmetry. Therefore, using reasoning like that in part (a), the electric
fl ux through the Gaussian surface is ΦE = Σ (E cos ϕ)ΔA = E(4𝜋r12). In accord with Gauss’ law, the electric fl ux must be equal to Q/𝜀0, where Q
Gaussian surface, S
Gaussian surface, S1
(a)
+
+
+
+
+
+
+
+
(b)
+
+
+
+
+
+
+
+
R R
r
r1
FIGURE 18.33 A uniform distribution of positive charge resides on a thin spherical shell of radius R. The spherical Gaussian surfaces S and S1 are used in Example 14 to evaluate the electric fl ux (a) outside and (b) inside the shell, respectively. For clarity, only half the shell and the Gaussian surfaces are shown.
Gaussian surface, S
Gaussian surface, S1
(a)
+
+
+
+
+
+
+
+
(b)
+
+
+
+
+
+
+
+
R R
r
r1
FIGURE 18.33 (REPEATED) A uniform distribution of positive charge resides on a thin spherical shell of radius R. The spherical Gaussian surfaces S and S1 are used in Example 14 to evaluate the electric fl ux
(a) outside and (b) inside the shell, respectively. For clarity, only half the shell and the Gaussian surfaces are shown.
EXAMPLE 15 The Electric Field Inside a Parallel Plate Capacitor
According to Equation 18.4, the electric fi eld inside a parallel plate
capacitor, and away from the edges, is constant and has a magnitude of
E = σ/ε0, where 𝜎 is the charge density (the charge per unit area) on a plate. Use Gauss’ law to obtain this result.
Reasoning Figure 18.34a shows the electric fi eld inside a parallel plate capacitor. Because the positive and negative charges are distributed uni-
formly over the surfaces of the plates, symmetry requires that the electric
fi eld be perpendicular to the plates. We will take advantage of this sym-
metry by choosing our Gaussian surface to be a small cylinder whose axis
is perpendicular to the plates (see part b of the fi gure). With this choice, we will be able to evaluate the electric fl ux and then, with the aid of
Gauss’ law, determine E.
Solution Figure 18.34b shows that we have placed our Gaussian cylin- der so that its left end is inside the positive metal plate, and the right end is
in the space between the plates. To determine the electric fl ux through this
Gaussian surface, we evaluate the fl ux through each of the three parts—
labeled 1, 2, and 3 in the drawing—that make up the total surface of the
cylinder and then add up the fl uxes.
Surface 1—the fl at left end of the cylinder—is embedded inside the
positive metal plate. As discussed in Section 18.8, the electric fi eld is
zero everywhere inside a conductor that is in equilibrium under electro-
static conditions. Since E = 0 N/C, the electric fl ux through this surface is also zero:
Φ1 = Σ (E cos ϕ)∆A = Σ [(0 N/C) cos ϕ]∆A = 0
E
(a)
+
+
+
Gaussian surface
3 1 2
–
–
–
–
–
+
+
+
+
+
(b)
E
FIGURE 18.34 (a) A side view of a parallel plate capacitor, showing some of the electric fi eld lines. (b) The Gaussian surface is a cylinder oriented so its axis is perpendicular to the positive plate and its left end
is inside the plate.
18.10 Copiers and Computer Printers 513
Check Your Understanding
(The answers are given at the end of the book.) 19. A Gaussian surface contains a single charge within it, and as a result an electric fl ux passes through the
surface. Suppose that the charge is then moved to another spot within the Gaussian surface. Does the
fl ux through the surface change?
20. CYU Figure 18.6 shows an arrangement of three charges. In parts a and b diff erent Gaussian surfaces (both in blue) are shown. Through which surface, if either, does the greater electric fl ux pass?
CYU FIGURE 18.6
−1 μC
+1 μC
(a) (b)
+2 μC−1 μC
+1 μC
+2 μC
21. CYU Figure 18.7 shows three charges, labeled q1, q2, and q3. A Gaussian surface (in blue) is drawn around q1 and q2. (a) Which charges determine the electric fl ux through the Gaussian surface? (b) Which charges produce the electric fi eld that exists at the point P?
q1
q2
q3
P
Gaussian surface
CYU FIGURE 18.7
18.10 *Copiers and Computer Printers THE PHYSICS OF . . . xerography. The electrostatic force that charged particles exert on one another plays the central role in an offi ce copier. The copying process is called xerogra- phy, from the Greek xeros and graphos, meaning “dry writing.” The heart of a copier is the xerographic drum, an aluminum cylinder coated with a layer of selenium (see Figure 18.35a).
The electric fl ux through the entire Gaussian cylinder is the sum of
the three fl uxes determined above:
ΦE = Φ1 + Φ2 + Φ3 = 0 + 0 + EA = EA
According to Gauss’ law, we set the electric fl ux equal to Q/𝜀0, where Q is the net charge inside the Gaussian cylinder: EA = Q/ε0. But Q/A is the charge per unit area, 𝜎, on the plate. Therefore, we arrive at the value of the electric fi eld inside a parallel plate capacitor: E = σ /𝜀0 . The distance of the right end of the Gaussian cylinder from the positive plate does not
appear in this result, indicating that the electric fi eld is the same every-
where between the plates.
Surface 2—the curved wall of the cylinder—is everywhere parallel
to the electric fi eld between the plates, so that cos ϕ = cos 90° = 0. There- fore, the electric fl ux through this surface is also zero:
Φ2 = Σ (E cos ϕ)∆A = Σ (E cos 90°)∆A = 0
Surface 3—the fl at right end of the cylinder—is perpendicular to the
electric fi eld between the plates, so cos ϕ = cos 0° = 1. The electric fi eld is constant over this surface, so E can be taken outside the summation in Equation 18.6. Noting that Σ ΔA = A is the area of surface 3, we fi nd that the electric fl ux through this surface is
Φ3 = Σ (E cos ϕ)∆A = Σ (E cos 0°)∆A = E( Σ ∆A) = EA
514 CHAPTER 18 Electric Forces and Electric Fields
Aluminum is an excellent electrical conductor. Selenium, on the other hand, is a photoconduc-
tor: it is an insulator in the dark but becomes a conductor when exposed to light. Consequently,
a positive charge deposited on the selenium surface will remain there, provided the selenium is
kept in the dark. When the drum is exposed to light, however, electrons from the aluminum pass
through the conducting selenium and neutralize the positive charge.
The photoconductive property of selenium is critical to the xerographic process, as
Figure 18.35b illustrates. First, an electrode called a corotron gives the entire selenium sur- face a positive charge in the dark. Second, a series of lenses and mirrors focuses an image of
a document onto the revolving drum. The dark and light areas of the document produce cor-
responding areas on the drum. The dark areas retain their positive charge, but the light areas
become conducting and lose their positive charge, ending up neutralized. Thus, a positive-
charge image of the document remains on the selenium surface. In the third step, a special
dry black powder, called the toner, is given a negative charge and then spread onto the drum, where it adheres selectively to the positively charged areas. The fourth step involves trans-
ferring the toner onto a blank piece of paper. However, the attraction of the positive-charge
image holds the toner to the drum. To transfer the toner, the paper is given a greater positive charge than that of the image, with the aid of another corotron. Last, the paper and adhering toner pass through heated pressure rollers, which melt the toner into the fi bers of the paper
and produce the fi nished copy.
THE PHYSICS OF . . . a laser printer. A laser printer is used with computers to provide high-quality copies of text and graphics. It is similar in operation to the xerographic machine,
except that the information to be reproduced is not on paper. Instead, the information is trans-
ferred from the computer’s memory to the printer, and laser light is used to copy it onto the
selenium–aluminum drum. A laser beam, focused to a fi ne point, is scanned rapidly from side to
side across the rotating drum, as Figure 18.36 indicates. While the light remains on, the positive
Original document Selenium-coated drum
Heated pressure rollers
Corotron for drum
Corotron for drum
Corotron for paper
Finished copy
Heated pressure rollers
Lens
(b)
(a)
Corotron for paper
Copy output
Copy paper
Lamps
Selenium-coated drum
1. Charging the drum
2. Imaging the document on the drum
3. Fixing the toner to the drum
4. Transferring the toner to the paper
5. Melting the toner into the paper
Negatively charged toner
FIGURE 18.35 (a) This cutaway view shows the essential elements of a copying machine. (b) The fi ve steps in the xerographic process.
++ +
+ ++ +
+
+ +
+
+
+ +
+ +
+ +
Paths of scanning laser beam
Xerographic drum
FIGURE 18.36 As the laser beam scans back and forth across the surface of the xerographic
drum, a positive-charge image of the letter “A”
is created.
18.10 Copiers and Computer Printers 515
charge on the drum is neutralized. As the laser beam moves, the computer turns the beam off at
the right moments during each scan to produce the desired positive-charge image, which is the
letter “A” in the picture.
THE PHYSICS OF . . . an inkjet printer. An inkjet printer is another type of printer that uses electric charges in its operation. While shuttling back and forth across the paper, the
inkjet printhead ejects a thin stream of ink. Figure 18.37 illustrates the elements of one type of printhead. The ink is forced out of a small nozzle and breaks up into extremely small droplets,
with diameters that can be as small as 9 × 10‒6 m. About 150 000 droplets leave the nozzle each
second and travel with a speed of approximately 18 m/s toward the paper. During their fl ight, the
droplets pass through two electrical components, an electrode and the defl ection plates (a parallel plate capacitor). When the printhead moves over regions of the paper that are not to be inked,
the charging control is turned on and an electric fi eld is established between the printhead and
the electrode. As the drops pass through the electric fi eld, they acquire a net charge by the pro-
cess of induction. The defl ection plates divert the charged droplets into a gutter and thus prevent
them from reaching the paper. Whenever ink is to be placed on the paper, the charging control,
responding to instructions from the computer, turns off the electric fi eld. The uncharged droplets
fl y straight through the defl ection plates and strike the paper.
Ink
supply
Pump Char ging
control
Instructions from computer
Nozzle of printhead
Paper
Electrode Deflection plates
Gutter
FIGURE 18.37 An inkjet printhead ejects a steady fl ow of ink droplets. Charged droplets are defl ected into a gutter by the defl ection plates, while uncharged droplets fl y straight onto the paper. Letters formed
by an inkjet printer look normal, except when greatly enlarged and the patterns from the drops become
apparent.
EXAMPLE 16 BIO The Physics of Electroreception
Electroreception is an animal’s ability to detect electrical stimuli (i.e.,
electric fi elds in its environment). Certain species of fi sh, sharks, and dol-
phins use this ability to locate prey and other objects around them. Studies
suggest that sharks are the most electrically sensitive animals known,
being able to detect electric fi elds as low as 5.0 × 10−7 N/C. If a small fi sh
carrying a charge of −0.1 nC is creating this electric fi eld (like a point
charge), what is the maximum distance the shark could be away from the
fi sh and still detect it?
Reasoning We can simply use Equation 18.3, which is the electric fi eld created by a point charge.
Solution The expression for the electric fi eld of a point charge is given by the following:
E = k ∣q ∣ r 2
.
Rearranging this expression we solve for r:
r = √kqE = √(8.99 × 10 9 N
m2
C2 )(0.1 × 10−9 C) 5.0 × 10−7 N/C
= 1340 m .
This is an amazingly far distance. However, we have neglected the eff ect
of the water, which can reduce this value by over a factor of 100 or more
(see Section 19.5). Even so, having the ability to detect small electric
fi elds even a few meters away allows the shark to locate food that might
be hiding beneath sand, for example.
516 CHAPTER 18 Electric Forces and Electric Fields
Concept Summary 18.1 The Origin of Electricity There are two kinds of electric charge: positive and negative. The SI unit of electric charge is the coulomb (C).
The magnitude of the charge on an electron or a proton is e = 1.60 × 10‒19 C. Since the symbol e denotes a magnitude, it has no algebraic sign. Thus, the electron carries a charge of ‒e, and the proton carries a charge of +e. The charge on any object, whether positive or negative, is quantized, in the sense that the charge consists of an integer number of protons or
electrons.
18.2 Charged Objects and the Electric Force The law of conservation of electric charge states that the net electric charge of an isolated system
remains constant during any process.
Like charges repel and unlike charges attract each other.
18.3 Conductors and Insulators An electrical conductor is a material, such as copper, that conducts electric charge readily. An electrical insulator
is a material, such as rubber, that conducts electric charge poorly.
18.4 Charging by Contact and by Induction Charging by contact is the process of giving one object a net electric charge by placing it in contact
with an object that is already charged. Charging by induction is the process
of giving an object a net electric charge without touching it to a charged
object.
18.5 Coulomb’s Law A point charge is a charge that occupies so little space that it can be regarded as a mathematical point. Coulomb’s law gives
the magnitude F of the electric force that two point charges q1 and q2 exert on each other, according to Equation 18.1, where |q1| and |q2| are the mag- nitudes of the charges and have no algebraic sign. The term k is a constant and has the value k = 8.99 × 109 N · m2/C2. The force specifi ed by Equation 18.1 acts along the line between the two charges.
F = k ∣q1∣ ∣q 2∣
r2 (18.1)
The permittivity of free space 𝜀0 is defi ned by the relation
k = 1
4πε0 18.6 The Electric Field The electric fi eld E→ at a given spot is a vector and is the electrostatic force F→ experienced by a very small test charge q0 placed at that spot divided by the charge itself, as given by Equation 18.2. The direc-
tion of the electric fi eld is the same as the direction of the force on a positive
test charge. The SI unit for the electric fi eld is the newton per coulomb (N/C).
The source of the electric fi eld at any spot is the collection of charged objects
surrounding that spot.
E→ = F →
q0 (18.2)
The magnitude of the electric fi eld created by a point charge q is given by Equation 18.3, where |q| is the magnitude of the charge and has no algebraic sign and r is the distance from the charge. The electric fi eld E→ points away from a positive charge and toward a negative charge.
E = k ∣q∣ r2
(18.3)
For a parallel plate capacitor that has a charge per unit area of 𝜎 on each plate, the magnitude of the electric fi eld between the plates is given by Equation 18.4.
E = σ
ε0 (18.4)
18.7 Electric Field Lines Electric fi eld lines are lines that can be thought of as a “map,” insofar as the lines provide information about the
direction and strength of the electric fi eld. The lines are directed away
from positive charges and toward negative charges. The direction of the
lines gives the direction of the electric fi eld, since the electric fi eld vector
at a point is tangent to the line at that point. The electric fi eld is strongest
in regions where the number of lines per unit area passing perpendicularly
through a surface is the greatest—that is, where the lines are packed to-
gether most tightly.
18.8 The Electric Field Inside a Conductor: Shielding Excess negative or positive charge resides on the surface of a conductor at equilibrium under
electrostatic conditions. In such a situation, the electric fi eld at any point
within the conducting material is zero, and the electric fi eld just outside the
surface of the conductor is perpendicular to the surface.
18.9 Gauss’ Law The electric fl ux ΦE through a surface is related to the magnitude E of the electric fi eld, the area A of the surface, and the angle ϕ that specifi es the direction of the fi eld relative to the normal to the surface,
as shown in Equation 18.6. Gauss’ law states that the electric fl ux through a
closed surface (a Gaussian surface) is equal to the net charge Q enclosed by the surface divided by 𝜀0, the permittivity of free space (see Equation 18.7).
ΦE = Σ (E cos ϕ)∆A (18.6)
ΦE = Σ (E cos ϕ)ΔA = Q ε0
(18.7)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 18.1 The Origin of Electricity 1. An object carries a charge of ‒8.0 𝜇C, while another carries a charge of ‒2.0 𝜇C. How many electrons must be transferred from the fi rst object to the second so that both objects have the same charge?
Section 18.2 Charged Objects and the Electric Force 2. Each of three objects carries a charge. As the draw- ing shows, objects A and B attract each other, and ob-
jects C and A also attract each other. Which one of the
following statements concerning objects B and C is
true? (a) They attract each other. (b) They repel each other. (c) They neither attract nor repel each other. (d) This question cannot be answered without addi- tional information.
Focus on Concepts
A
B
C
A
QUESTION 2
Problems 517
Section 18.4 Charging by Contact and by Induction 4. Each of two identical objects carries a net charge. The objects are made from conducting material. One object is attracted to a positively charged ebonite rod,
and the other is repelled by the rod. After the objects are touched together, it is
found that they are each repelled by the rod. What can be concluded about the
initial charges on the objects? (a) Initially both objects are positive, with both charges having the same magnitude. (b) Initially both objects are negative, with both charges having the same magnitude. (c) Initially one object is positive and one is negative, with the negative charge having a greater magnitude than the
positive charge. (d) Initially one object is positive and one is negative, with the positive charge having a greater magnitude than the negative charge.
5. Only one of three balls A, B, and C carries a net charge q. The balls are made from conducting material and are identical. One of the uncharged balls
can become charged by touching it to the charged ball and then separating the
two. This process of touching one ball to another and then separating the two
balls can be repeated over and over again, with the result that the three balls
can take on a variety of charges. Which one of the following distributions of
charges could not possibly be achieved in this fashion, even if the process
were repeated a large number of times?
(a) qA = 1 3 q, qB = 1
3 q, qC = 1
3 q (c) qA = 1
2 q, qB = 3
8 q, qC = 1
4 q (b) qA = 1 2 q, qB =
1
4 q, qC = 1
4 q (d) qA = 3
8 q, qB = 3
8 q, qC = 1
4 q
Section 18.5 Coulomb’s Law 8. Three point charges have equal magnitudes and are located on the same line. The separation d between A and B is the same as the separation between B and C. One of the charges is positive and two are negative, as the drawing shows.
Consider the net electrostatic force that each charge experiences due to the other
two charges. Rank the net forces in descending order (greatest fi rst) according to
magnitude. (a) A, B, C (b) B, C, A (c) A, C, B (d) C, A, B (e) B, A, C
QUESTION 8 +
d d
A B C
– –
9. Three point charges have equal magnitudes and are fi xed to the corners of an equilateral triangle. Two of the charges are positive and one is negative, as
the drawing shows. At which one of the corners is the net force acting on the
charge directed parallel to the x axis? (a) A (b) B (c) C
QUESTION 9
+
+
A
B
C
+x
+y
–
Section 18.6 The Electric Field 12. A positive point charge q1 creates an electric fi eld of magnitude E1 at a spot located at a distance r1 from the charge. The charge is replaced by another positive point charge q2, which creates a fi eld of magnitude E2 = E1 at a distance of r2 = 2r1. How is q2 related to q1? (a) q 2 = 2q1 (b) q 2 = 1 2 q1 (c) q 2 = 4q1 (d) q 2 =
1
4 q1 (e) q 2 = √2q1 13. The drawing shows a positive and a negative point charge. The negative
charge has the greater magnitude. Where
on the line that passes through the charges
is the one spot where the total electric
fi eld is zero? (a) To the right of the negat- ive charge (b) To the left of the positive charge (c) Between the charges, to the left of the midpoint (d) Between the charges, to the right of the midpoint
Section 18.7 Electric Field Lines 17. The drawing shows some electric fi eld lines. For the points
indicated, rank the magnitudes
of the electric fi eld in descending
order (largest fi rst). (a) B, C, A (b) B, A, C (c) A, B, C (d) A, C, B (e) C, A, B
Section 18.8 The Electric Field Inside a Conductor: Shielding 18. The drawings show (in cross section) two solid spheres and two spher- ical shells. Each object is made from copper and has a net charge, as the plus
and minus signs indicate. Which drawing correctly shows where the charges
reside when they are in equilibrium? (a) A (b) B (c) C (d) D
+
+ +
+ +
+ +
+
++ + ++
++ +
– – – – –
––
–
–– – – –
– – –
DCBA
QUESTION 18
Section 18.9 Gauss’ Law 20. A cubical Gaussian surface surrounds two charges, q1 = +6.0 × 10‒12 C and q2 = ‒2.0 × 10‒12 C, as the draw- ing shows. What is the electric fl ux passing through the
surface?
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 18.1 The Origin of Electricity
Section 18.2 Charged Objects and the Electric Force
Section 18.3 Conductors and Insulators
Section 18.4 Charging by Contact and by Induction 1. E SSM Iron atoms have been detected in the sun’s outer atmosphere, some with many of their electrons stripped away. What is the net electric
Problems
A B C
QUESTION 17
+
–
QUESTION 20
+
Midpoint
–
QUESTION 13
518 CHAPTER 18 Electric Forces and Electric Fields
charge (in coulombs) of an iron atom with 26 protons and 7 electrons? Be
sure to include the algebraic sign (+ or ‒) in your answer.
2. E An object has a charge of ‒2.0 𝜇C. How many electrons must be removed so that the charge becomes +3.0 𝜇C? 3. E Four identical metallic objects carry the following charges: +1.6, +6.2, ‒4.8, and ‒9.4 𝜇C. The objects are brought simultaneously into con- tact, so that each touches the others. Then they are separated. (a) What is the fi nal charge on each object? (b) How many electrons (or protons) make up the fi nal charge on each object?
4. E GO Four identical metal spheres have charges of qA = ‒8.0 𝜇C, qB = ‒2.0 𝜇C, qC = +5.0 𝜇C, and qD = +12.0 𝜇C. (a) Two of the spheres are brought together so they touch, and then they are separated. Which spheres
are they, if the fi nal charge on each one is +5.0 𝜇C? (b) In a similar man- ner, which three spheres are brought together and then separated, if the fi nal
charge on each of the three is +3.0 𝜇C? (c) The fi nal charge on each of the three separated spheres in part (b) is +3.0 𝜇C. How many electrons would have to be added to one of these spheres to make it electrically neutral?
5. E SSM Consider three identical metal spheres, A, B, and C. Sphere A carries a charge of +5q. Sphere B carries a charge of ‒q. Sphere C carries no net charge. Spheres A and B are touched together and then separated. Sphere
C is then touched to sphere A and separated from it. Last, sphere C is touched
to sphere B and separated from it. (a) How much charge ends up on sphere C? What is the total charge on the three spheres (b) before they are allowed to touch each other and (c) after they have touched? 6. E GO A plate carries a charge of ‒3.0 𝜇C, while a rod carries a charge of +2.0 𝜇C. How many electrons must be transferred from the plate to the rod, so that both objects have the same charge?
7. M V-HINT Water has a mass per mole of 18.0 g/mol, and each water mo- lecule (H2O) has 10 electrons. (a) How many electrons are there in one liter (1.00 × 10‒3 m3) of water? (b) What is the net charge of all these electrons?
Section 18.5 Coulomb’s Law 8. E In a vacuum, two particles have charges of q1 and q2, where q1 = +3.5 𝜇C. They are separated by a distance of 0.26 m, and particle 1 experi- ences an attractive force of 3.4 N. What is q2 (magnitude and sign)? 9. E SSM Two spherical objects are separated by a distance that is 1.80 × 10‒3 m. The objects are initially electrically neutral and are very small
compared to the distance between them. Each object acquires the same neg-
ative charge due to the addition of electrons. As a result, each object exper-
iences an electrostatic force that has a magnitude of 4.55 × 10‒21 N. How
many electrons did it take to produce the charge on one of the objects?
10. E Two tiny conducting spheres are identical and carry charges of ‒20.0 𝜇C and +50.0 𝜇C. They are separated by a distance of 2.50 cm. (a) What is the magnitude of the force that each sphere experiences, and is the force attractive or repulsive? (b) The spheres are brought into contact and then separated to a distance of 2.50 cm. Determine the magnitude of the force
that each sphere now experiences, and state whether the force is attractive or
repulsive.
11. E SSM Two very small spheres are initially neutral and separated by a distance of 0.50 m. Suppose that 3.0 × 1013 electrons are removed from one
sphere and placed on the other. (a) What is the magnitude of the electrostatic force that acts on each sphere? (b) Is the force attractive or repulsive? Why? 12. E Two charges attract each other with a force of 1.5 N. What will be the force if the distance between them is reduced to one-ninth of its original value?
13. E Two point charges are fi xed on the y axis: a negative point charge q1 = ‒25 𝜇C at y1 = +0.22 m and a positive point charge q2 at y2 = +0.34 m. A third point charge q = +8.4 𝜇C is fi xed at the origin. The net electrostatic force exerted on the charge q by the other two charges has a magnitude of 27 N and points in the +y direction. Determine the magnitude of q2.
14. E GO The drawings show three charges that have the same magnitude but may have diff erent signs. In all cases the distance d between the charges is the same. The magnitude of the charges is |q| = 8.6 𝜇C, and the distance between them is d = 3.8 mm. Determine the magnitude of the net force on charge 2 for each of the three drawings.
1 2 3
(a) (c)(b)
d d−q +q +q 1 2 3
d d+q +q +q 1 2
3
d
d
+q −q
+q
PROBLEM 14
15. E SSM MMH Two tiny spheres have the same mass and carry charges of the same magnitude. The mass of each sphere is 2.0 × 10‒6 kg. The grav-
itational force that each sphere exerts on the other is balanced by the elec-
tric force. (a) What algebraic signs can the charges have? (b) Determine the charge magnitude.
16. E GO A charge +q is located at the origin, while an identical charge is located on the x axis at x = +0.50 m. A third charge of +2q is located on the x axis at such a place that the net electrostatic force on the charge at the origin doubles, its direction remaining unchanged. Where should the third
charge be located?
17. E SSM Two particles, with identical positive charges and a separation of 2.60 × 10‒2 m, are released from rest. Immediately after the release, particle 1
has an acceleration a→1 whose magnitude is 4.60 × 103 m/s2, while particle 2 has an acceleration a→2 whose magnitude is 8.50 × 103 m/s2. Particle 1 has a mass of 6.00 × 10‒6 kg. Find (a) the charge on each particle and (b) the mass of particle 2.
18. E A charge of ‒3.00 𝜇C is fi xed at the center of a compass. Two addi- tional charges are fi xed on the circle of the compass, which has a radius of
0.100 m. The charges on the circle are ‒4.00 𝜇C at the position due north and +5.00 𝜇C at the position due east. What are the magnitude and direction of the net electrostatic force acting on the charge at the center? Specify the
direction relative to due east.
19. M Multiple-Concept Example 3 provides some pertinent background for this problem. Suppose a single electron orbits about a nucleus contain-
ing two protons (+2e), as would be the case for a helium atom from which one of the two naturally occurring electrons is removed. The radius of the
orbit is 2.65 × 10‒11 m. Determine the magnitude of the electron’s centripetal
acceleration.
20. M V-HINT The drawing shows an equilateral triangle, each side of which has a length of 2.00 cm. Point charges are fi xed to each corner, as shown. The
4.00 𝜇C charge experiences a net force due to the charges qA and qB. This net force points vertically downward and has a magnitude of 405 N. Determine
the magnitudes and algebraic signs of the charges qA and qB.
PROBLEM 20 qA qB
+4.00 μC
21. M V-HINT MMH The drawing shows three point charges fi xed in place. The charge at the coordinate origin has a value of q1 = +8.00 𝜇C; the other two charges have identical magnitudes, but opposite signs: q2 = ‒5.00 𝜇C and q3 = +5.00 𝜇C. (a) Determine the net force (magnitude and direction) exerted
Problems 519
on q1 by the other two charges. (b) If q1 had a mass of 1.50 g and it were free to move, what would be its acceleration?
PROBLEM 21
+x
+y
q1
q2
q3
23.0° 23.0°
1.30 m
1.30 m
22. M GO An electrically neutral model airplane is fl ying in a horizontal circle on a 3.0-m guideline, which is nearly parallel to the ground. The line
breaks when the kinetic energy of the plane is 50.0 J. Reconsider the same
situation, except that now there is a point charge of +q on the plane and a point charge of ‒q at the other end of the guideline. In this case, the line breaks when the kinetic energy of the plane is 51.8 J. Find the magnitude of the charges.
23. M V-HINT Multiple-Concept Example 3 illustrates several of the con- cepts that come into play in this problem. A single electron orbits a lithium
nucleus that contains three protons (+3e). The radius of the orbit is 1.76 × 10‒11 m. Determine the kinetic energy of the electron.
24. M GO An unstrained horizontal spring has a length of 0.32 m and a spring constant of 220 N/m. Two small charged objects are attached to this spring,
one at each end. The charges on the objects have equal magnitudes. Because of
these charges, the spring stretches by 0.020 m relative to its unstrained length.
Determine (a) the possible algebraic signs and (b) the magnitude of the charges. 25. M SSM In the rectangle in the drawing, a charge is to be placed at the empty corner to make the net force on the charge at corner A point along the vertical direction. What charge (magnitude and algebraic sign) must be
placed at the empty corner?
PROBLEM 25
A
d
4d
+3.0 μC
+3.0 μC
+3.0 μC
26. H Available in WileyPLUS. 27. H CHALK SSM A small spherical insulator of mass 8.00 × 10‒2 kg and charge +0.600 𝜇C is hung by a thread of negligible mass. A charge of ‒0.900 𝜇C is held 0.150 m away from the sphere and directly to the right of it, so the thread makes an angle 𝜃 with the vertical (see the drawing). Find (a) the angle 𝜃 and (b) the tension in the thread.
PROBLEM 27
0.150 m
+0.600 μC –0.900 μC
θ
28. H Available in WileyPLUS.
Section 18.6 The Electric Field
Section 18.7 Electric Field Lines
Section 18.8 The Electric Field Inside a Conductor: Shielding 29. E SSM At a distance r1 from a point charge, the magnitude of the elec- tric fi eld created by the charge is 248 N/C. At a distance r2 from the charge, the fi eld has a magnitude of 132 N/C. Find the ratio r2/r1.
30. E GO Suppose you want to determine the electric fi eld in a certain region of space. You have a small object of known charge and an instru-
ment that measures the magnitude and direction of the force exerted on the
object by the electric fi eld. (a) The object has a charge of +20.0 𝜇C and the instrument indicates that the electric force exerted on it is 40.0 𝜇N, due east. What are the magnitude and direction of the electric fi eld? (b) What are the magnitude and direction of the electric fi eld if the object has a charge of ‒10.0 𝜇C and the instrument indicates that the force is 20.0 𝜇N, due west?
31. E An electric fi eld of 260 000 N/C points due west at a certain spot. What are the magnitude and direction of the force that acts on a charge of
‒7.0 𝜇C at this spot?
32. E MMH Review the important features of electric fi eld lines discussed in Conceptual Example 12. Three point charges (+q, +2q, and ‒3q) are at the corners of an equilateral triangle. Sketch in six electric fi eld lines between
the three charges.
33. E Four point charges have the same magnitude of 2.4 × 10‒12 C and are fi xed to the corners of a square that is 4.0 cm on a side. Three of the charges
are positive and one is negative. Determine the magnitude of the net electric
fi eld that exists at the center of the square.
34. E GO The drawing shows two situations in which charges are placed on the x and y axes. They are all located at the same distance of 6.1 cm from the origin O. For each of the situations in the drawing, determine the magnitude
of the net electric fi eld at the origin.
+2.0 μC –3.0 μC
–5.0 μC
(a)
+4.0 μC –1.0 μC
+1.0 μC
OO
+6.0 μC
(b)
PROBLEM 34
35. E MMH A uniform electric fi eld exists everywhere in the x, y plane. This electric fi eld has a magnitude of 4500 N/C and is directed in the positive
x direction. A point charge ‒8.0 × 10‒9 C is placed at the origin. Determine the magnitude of the net electric fi eld at (a) x = ‒0.15 m, (b) x = +0.15 m, and (c) y = +0.15 m. 36. E BIO GO The membrane surrounding a living cell consists of an inner and an outer wall that are separated by a small space. Assume that the mem-
brane acts like a parallel plate capacitor in which the eff ective charge density
on the inner and outer walls has a magnitude of 7.1 × 10‒6 C/m2. (a) What is the magnitude of the electric fi eld within the cell membrane? (b) Find the magnitude of the electric force that would be exerted on a potassium ion (K+;
charge = +e) placed inside the membrane.
37. E SSM Available in WileyPLUS. 38. E MMH A 3.0 𝜇C point charge is placed in an external uniform electric fi eld that has a magnitude of 1.6 × 104 N/C. At what distance from the charge
is the net electric fi eld zero?
39. E SSM A tiny ball (mass = 0.012 kg) carries a charge of ‒18 𝜇C. What electric fi eld (magnitude and direction) is needed to cause the ball to fl oat
above the ground?
40. E GO A proton and an electron are moving due east in a constant electric fi eld that also points due east. The electric fi eld has a magnitude of
520 CHAPTER 18 Electric Forces and Electric Fields
8.0 × 104 N/C. Determine the magnitude of the acceleration of the proton
and the electron.
41. E Review Conceptual Example 11 before attempting to work this problem. The magnitude of each of the charges in Figure 18.20 is 8.60 × 10‒12 C. The lengths of the sides of the rectangles are 3.00 cm and 5.00 cm.
Find the magnitude of the electric fi eld at the center of the rectangle in
Figures 18.20a and b. 42. E Two charges are placed between the plates of a parallel plate capa- citor. One charge is +q1 and the other is q2 = +5.00 𝜇C. The charge per unit area on each of the plates has a magnitude of 𝜎 = 1.30 × 10‒4 C/m2. The magnitude of the force on q1 due to q2 equals the magnitude of the force on q1 due to the electric fi eld of the parallel plate capacitor. What is the distance r between the two charges? 43. M MMH A small object has a mass of 3.0 × 10‒3 kg and a charge of ‒34 𝜇C. It is placed at a certain spot where there is an electric fi eld. When released, the object experiences an acceleration of 2.5 × 103 m/s2 in the dir-
ection of the +x axis. Determine the magnitude and direction of the electric fi eld.
44. M V-HINT Available in WileyPLUS. 45. M SSM Two point charges are located along the x axis: q1 = +6.0 𝜇C at x1 = +4.0 cm, and q2 = +6.0 𝜇C at x2 = ‒4.0 cm. Two other charges are located on the y axis: q3 = +3.0 𝜇C at y3 = +5.0 cm, and q4 = ‒8.0 𝜇C at y4 = +7.0 cm. Find the net electric fi eld (magnitude and direction) at the origin.
46. M GO The total electric fi eld E→ consists of the vector sum of two parts. One part has a magnitude of E1 = 1200 N/C and points at an angle 𝜃1 = 35° above the +x axis. The other part has a magnitude of E2 = 1700 N/C and points at an angle 𝜃2 = 55° above the +x axis. Find the magnitude and direction of the total fi eld. Specify the directional angle relative to the
+x axis. 47. M V-HINT A particle of charge +12 𝜇C and mass 3.8 × 10‒5 kg is re- leased from rest in a region where there is a constant electric fi eld of +480
N/C. What is the displacement of the particle after a time of 1.6 × 10‒2 s?
48. M GO The drawing shows a positive point charge +q1, a second point charge q2 that may be positive or negative, and a spot labeled P, all on the same straight line. The distance d between the two charges is the same as the distance between q1 and the spot P. With q2 present, the magnitude of the net electric fi eld at P is twice what it is when q1 is present alone. Given that q1 = +0.50 𝜇C, determine q2 when it is (a) positive and (b) negative.
d d q2 +q1
P
PROBLEM 48
49. M CHALK An electron is released from rest at the negative plate of a parallel plate capacitor. The charge per unit area on each plate is 𝜎 = 1.8 × 10‒7 C/m2, and the plate separation is 1.5 × 10‒2 m. How fast is the electron
moving just before it reaches the positive plate?
50. H Two particles are in a uniform electric fi eld that points in the +x dir- ection and has a magnitude of 2500 N/C. The mass and charge of particle 1
are m1 = 1.4 × 10‒5 kg and q1 = ‒7.0 𝜇C, while the corresponding values for particle 2 are m2 = 2.6 × 10‒5 kg and q2 = +18 𝜇C. Initially the particles are at rest. The particles are both located on the same electric fi eld line but are
separated from each other by a distance d. Particle 1 is located to the left of particle 2. When released, they accelerate but always remain at this same
distance from each other. Find d. 51. H SSM Available in WileyPLUS. 52. H The drawing shows an electron entering the lower left side of a par- allel plate capacitor and exiting at the upper right side. The initial speed of
the electron is 7.00 × 106 m/s. The capacitor is 2.00 cm long, and its plates
are separated by 0.150 cm. Assume that the electric fi eld between the plates
is uniform everywhere and fi nd its magnitude.
PROBLEM 52 –e
– – – – –
+ + + + + 2.00 cm
0.150 cm
53. H A small plastic ball with a mass of 6.50 × 10‒3 kg and with a charge of +0.150 𝜇C is suspended from an insulating thread and hangs between the plates of a capacitor (see the drawing). The ball is in equilibrium, with the
thread making an angle of 30.0° with respect to the vertical. The area of each
plate is 0.0150 m2. What is the magnitude of the charge on each plate?
PROBLEM 53
+ + + + + +
– – – – – –
+
30.0°
Section 18.9 Gauss’ Law 54. E A spherical surface completely surrounds a collection of charges. Find the electric fl ux through the surface if the collection consists of (a) a single +3.5 × 10‒6 C charge, (b) a single ‒2.3 × 10‒6 C charge, and (c) both of the charges in (a) and (b).
55. E SSM The drawing shows an edge-on view of two planar surfaces that intersect and are mutually perpendicular. Surface 1 has an area of 1.7 m2,
while surface 2 has an area of 3.2 m2. The electric fi eld E→ in the drawing is uniform and has a magnitude of 250 N/C. Find the magnitude of the electric
fl ux through (a) surface 1 and (b) surface 2.
PROBLEM 55
E
35°
Surface 2
Surface 1
56. E A surface completely surrounds a +2.0 × 10‒6 C charge. Find the electric fl ux through this surface when the surface is (a) a sphere with a radius of 0.50 m, (b) a sphere with a radius of 0.25 m, and (c) a cube with edges that are 0.25 m long.
57. E A circular surface with a radius of 0.057 m is exposed to a uniform external electric fi eld of magnitude 1.44 × 104 N/C. The magnitude of the
electric fl ux through the surface is 78 N · m2/C. What is the angle (less than 90°) between the direction of the electric fi eld and the normal to the surface?
58. E V-HINT A charge Q is located inside a rectangular box. The electric fl ux through each of the six surfaces of the box is: Φ1 = +1500 N · m2/C, Φ2 = +2200 N · m2/C, Φ3 = +4600 N · m2/C, Φ4 = ‒1800 N · m2/C, Φ5 = ‒3500 N · m2/C, and Φ6 = ‒5400 N · m2/C. What is Q? 59. M MMH Available in WileyPLUS. 60. M GO MMH Two spherical shells have a common center. A ‒1.6 × 10‒6 C charge is spread uniformly over the inner shell, which has a radius of 0.050 m. A
+5.1 × 10‒6 C charge is spread uniformly over the outer shell, which has a radius
of 0.15 m. Find the magnitude and direction of the electric fi eld at a distance
(measured from the common center) of (a) 0.20 m, (b) 0.10 m, and (c) 0.025 m. 61. M SSM Available in WileyPLUS. 62. H Available in WileyPLUS.
Concepts and Calculations Problems 521
63. E Available in WileyPLUS. 64. E GO The masses of the earth and moon are 5.98 × 1024 and 7.35 × 1022 kg, respectively. Identical amounts of charge are placed on each body,
such that the net force (gravitational plus electrical) on each is zero. What is
the magnitude of the charge placed on each body?
65. E Available in WileyPLUS. 66. E A small drop of water is suspended motionless in air by a uniform electric fi eld that is directed upward and has a magnitude of 8480 N/C. The
mass of the water drop is 3.50 × 10‒9 kg. (a) Is the excess charge on the water drop positive or negative? Why? (b) How many excess electrons or protons reside on the drop?
67. E SSM Two charges are placed on the x axis. One of the charges (q1 = +8.5 𝜇C) is at x1 = +3.0 cm and the other (q2 = ‒21 𝜇C) is at x1 = +9.0 cm. Find the net electric fi eld (magnitude and direction) at (a) x = 0 cm and (b) x = +6.0 cm. 68. E When point charges q1 = +8.4 𝜇C and q2 = +5.6 𝜇C are brought near each other, each experiences a repulsive force of magnitude 0.66 N.
Determine the distance between the charges.
69. E SSM MMH Available in WileyPLUS. 70. M CHALK MMH The drawing shows two positive charges q1 and q2 fi xed to a circle. At the center of the circle they produce a net electric fi eld that is
directed upward along the vertical axis. Determine the ratio |q2|/|q1| of the charge magnitudes.
PROBLEM 70 q1
q230.0° 60.0°
71. M SSM Available in WileyPLUS. 72. M GO Three point charges have equal magnitudes, two being positive and one negative. These charges are fi xed to the corners of an equilateral
triangle, as the drawing shows. The magnitude of each of the charges is
5.0 𝜇C, and the lengths of the sides of the triangle are 3.0 cm. Calculate the magnitude of the net force that each charge experiences.
PROBLEM 72 A
B
C
+
+–
73. M V-HINT Available in WileyPLUS. 74. M GO Four point charges have equal magnitudes. Three are positive, and one is negative, as the drawing shows. They are fi xed in place on the
same straight line, and adjacent charges are equally separated by a distance d. Consider the net electrostatic force acting on each charge. Calculate the ratio
of the largest to the smallest net force.
A
+ B
+ C
+ D
– d d d
PROBLEM 74
75. M V-HINT Available in WileyPLUS. 76. H Two identical small insulating balls are suspended by separate 0.25-m threads that are attached to a common point on the ceiling. Each ball has
a mass of 8.0 × 10‒4 kg. Initially the balls are uncharged and hang straight
down. They are then given identical positive charges and, as a result, spread
apart with an angle of 36° between the threads. Determine (a) the charge on each ball and (b) the tension in the threads. 77. (animated) M GO In a vacuum, a proton (charge = +e, mass = 1.67 × 10‒27 kg) is moving parallel to a uniform electric fi eld that is directed along
the +x axis (see the fi gure below). The proton starts with a velocity of +2.5 × 104 m/s and accelerates in the same direction as the electric fi eld, which has
a value of +2.3 × 103 N/C. Find the velocity of the proton when its displace-
ment is +2.0 mm from the starting point.
ANIMATED PROBLEM 77
+x Ex
ax
+2.0 mm
+ +
Additional Problems
In this chapter we have studied electric forces and electric fi elds. The format
of the following problems stresses the role of conceptual understanding in
problem solving. The purpose of the conceptual question section is to review
the important concepts and to build intuition to help in anticipating some of
the characteristics of the numerical answers.
78. M CHALK The charges on three identical metal spheres are ‒12 𝜇C, +4.0 𝜇C, and +2.0 𝜇C. The spheres are brought together so they simultan- eously touch each other. They are then separated and placed on the x and
y axes, as shown in the fi gure. Treat the spheres as if they were particles. Concepts: (i) Is the net charge on the system comprising the three spheres the same before and after touching? Why? (ii) After the spheres touch and are
separated, how is the charge distributed, and what is the value of the charge
on each sphere? (iii) Do q2 and q3 exert forces of equal magnitude on q1? (iv) Is the magnitude of the net force exerted on q1 equal to 2F, where F is the magnitude of the force that either q2 or q3 exerts on q1? Calculations: What is the net force (magnitude and direction) exerted on the sphere at the origin?
Concepts and Calculations Problems
522 CHAPTER 18 Electric Forces and Electric Fields
PROBLEM 78
(a) Three equal charges lie on the x and y axes. (b) The net force exerted by the two charges is F→.
F13 +x
+y
q1 q3
q2
+x
+y
q1 q3
q2
F F12
3.5 mm
3.5 mm
(a)
(b)
θ
79. M CHALK Two point charges are lying on the y axis as in the fi gure: q1 = ‒4.00 𝜇C and q2 = +4.00 𝜇C. They are equidistant from the point P, which lies on the x axis. Concepts: (i) There is no charge at P in part a of the fi gure. Is there an electric fi eld at P? (ii) What is the direction of the electric fi eld at point P due to charge q2? (iii) Is the magnitude of the electric fi eld at P equal
to E1 + E2, where E1 and E2 are the magnitudes of the electric fi elds produced by q1 and q2? Explain. Calculations: (a) What is the net electric fi eld at P? (b) A small object of charge q0 = +8.00 𝜇C and mass m = 1.2 g is placed at P. When it is released, what is its acceleration?
PROBLEM 79
(a) Charges q1 and q2 lie on the y axis, and point P lies on the x axis. (b) The net electric fi eld at point P is E→.
q1
q2
(a)
+x
+x
+y
+y
(b)
31.0° 31.0°
E2
E
P
E1
q1
q2
31.0° 31.0°
0.700 m
0.700 m
P
+
–
+
–
80. M An Electron Gun. You and your team are tasked with designing an “electron gun” that operates in a vacuum chamber, the purpose of which is to
direct a beam of electrons toward a tiny metallic plate in order to heat it. The
electrons in the beam have a speed of 3.50 × 107 m/s and travel in the positive
x direction through the center of a set of defl ecting plates (a parallel-plate capacitor) that sets up a uniform electric fi eld in the region between the plates.
The target is located 22.0 cm along the x-axis from the trailing edge of plates (i.e., the edge closest to the target), and 11.5 cm above the horizontal (i.e.,
in the +y direction). The length of the plates (in the x direction) is 2.50 cm. (a) In which direction should the electric fi eld between the plates point in order to defl ect the electrons towards the target? (b) To what magnitude should you set the electric fi eld so that the electron beam hits the target?
(c) After successfully striking the target using your results from (a) and (b), you realized that the target is not heating up to the required temperat-
ure. Since the degree of heating depends on the speed of the electrons, you
increase the electron speed to 5.20 × 107 m/s. With the electric fi eld setting
from (b), will the electrons still be on target? If not, to what value should you
set the electric fi eld?
81. M An Electrostatic Positioner. You and your team are designing a device that can be used to position a small, plastic object in the region
between the plates of a parallel-plate capacitor. A small plastic sphere of
mass m = 1.20 × 10−2 kg carries a charge q = +0.200 μC and hangs vertically (along the y direction) from a massless, insulating thread (length l = 10.0 cm) between two vertical capacitor plates. When there is no electric fi eld, the
object resides at the midpoint between the plates (at x = 0). However, when there is a fi eld between plates (in the ±x direction) the object moves to a new equilibrium position. (a) To what value should you set the fi eld if you want the object to be located at x = 2.10 cm? (b) To what value should you set the fi eld if you want the object to be located at x = −3.30 cm?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
19.1 Define electrical potential energy.
19.2 Solve problems involving electric potential and electric potential energy.
19.3 Calculate electric potential created by point charges.
19.4 Relate equipotential surfaces to the electric field.
19.5 Solve problems involving capacitors.
19.6 Describe biomedical applications of electric potential.
D A
N IE
L M
IH A
IL E
S C
U /A
F P
/G et
ty I
m ag
es /N
ew sC
o m
CHAPTER 19
Electric Potential Energy and the Electric Potential
In the medical diagnostic technique of electroencephalography, electrodes placed at various points on the head
detect the small voltages that exist between the points. The cap worn by the young man in this photograph
facilitates the placement of a number of electrodes, so that the voltages created by diff erent regions of the brain as
he plays a fl ipper pinball game can be measured simultaneously. The voltage between two points is another name
for the diff erence in electric potential between the points, which is related to the concept of electric potential
energy. Electric potential energy and electric potential are the central ideas in this chapter.
19.1 Potential Energy In Chapter 18 we discussed the electrostatic force that two point charges exert on each
other, the magnitude of which is F = k|q1||q2|/r2. The form of this equation is similar to the form for the gravitational force that two particles exert on each other, which is F = Gm1m2/r2, according to Newton’s law of universal gravitation (see Section 4.7). Both of these forces are conservative and, as Section 6.4 explains, a potential energy can be asso-
ciated with a conservative force. Thus, an electric potential energy exists that is analogous
to the gravitational potential energy. To set the stage for a discussion of the electric poten-
tial energy, let’s review some of the important aspects of the gravitational counterpart.
Figure 19.1, which is essentially Figure 6.10, shows a basketball of mass m fall- ing from point A to point B. The gravitational force, mg→, is the only force acting on
523 *The gravitational potential energy is now being denoted by GPE to distinguish it from the electric potential
energy EPE.
524 CHAPTER 19 Electric Potential Energy and the Electric Potential
the ball, where g is the magnitude of the acceleration due to gravity. As Section 6.3 discusses, the work WAB done by the gravitational force when the ball falls from a height of hA to a height of hB is
WAB = mghA − mghB = GPEA − GPEB (6.4)
Recall that the quantity mgh is the gravitational potential energy* of the ball, GPE = mgh (Equation 6.5), and represents the energy that the ball has by virtue of its position relative to the
surface of the earth. Thus, the work done by the gravitational force equals the initial gravitational
potential energy minus the fi nal gravitational potential energy.
Interactive Figure 19.2 clarifi es the analogy between electric and gravitational potential energies. In this drawing a positive test charge +q0 is situated at point A between two oppositely charged plates. Because of the charges on the plates, an electric fi eld E→ exists in the region between the plates. Consequently, the test charge experiences an electric force, F→ = q0E
→ (Equa-
tion 18.2), that is directed downward, toward the lower plate. (The gravitational force is being
neglected here.) As the charge moves from A to B, work is done by this force, in a fashion analogous to the work done by the gravitational force in Figure 19.1. The work WAB done by the electric force equals the diff erence between the electric potential energy EPE at A and the electric potential energy at B:
WAB = EPEA − EPEB (19.1)
This expression is similar to Equation 6.4. The path along which the test charge moves from A to B is of no consequence because the electric force, like the gravitational force, is conservative. For such forces, the work WAB is the same for all paths (see Section 6.4).
19.2 The Electric Potential Diff erence Since the electric force is F→ = q0E
→ , the work that it does as the charge moves from A to B in
Interactive Figure 19.2 depends on the charge q0. It is useful, therefore, to express this work on a per-unit-charge basis, by dividing both sides of Equation 19.1 by the charge:
WAB q 0
= EPEA
q 0 −
EPEB
q 0 (19.2)
Notice that the right-hand side of this equation is the diff erence between two terms, each of
which is an electric potential energy divided by the test charge, EPE/q0. The quantity EPE/q0 is the electric potential energy per unit charge and is an important concept in electricity. It is
called the electric potential or, simply, the potential and is referred to with the symbol V, as in Equation 19.3.
DEFINITION OF ELECTRIC POTENTIAL The electric potential V at a given point is the electric potential energy EPE of a small test charge q0 situated at that point divided by the charge itself:
V = EPE
q 0 (19.3)
SI Unit of Electric Potential: joule/coulomb = volt (V)
The SI unit of electric potential is a joule per coulomb, a quantity known as a volt. The name honors Alessandro Volta (1745–1827), who invented the voltaic pile, the forerunner of the battery.
In spite of the similarity in names, the electric potential energy EPE and the electric potential V are not the same. The electric potential energy, as its name implies, is an energy and, therefore, is measured in joules. In contrast, the electric potential is an energy per unit charge and is measured in joules per coulomb, or volts.
Initial
gravitational,
potential energy,
GPEA
{
Final
gravitational
potential energy,
GPEB
{
hA
F = mg
F = mg hB
A
B
FIGURE 19.1 Gravity exerts a force, F→ = mg→, on the basketball of mass m. Work is done by the gravitational force as the ball
falls from A to B.
q0
F = q0E
q0
F = q0E
A
B
− − − − − − − − − − − − − −
+ + + + + + + + + + + + + +
INTERACTIVE FIGURE 19.2 Because of the electric fi eld E→, an electric force, F→ = q0E
→ , is exerted on a positive test charge
+q0. Work is done by the force as the charge moves from A to B.
19.2 The Electric Potential Diff erence 525
We can now relate the work WAB done by the electric force when a charge q0 moves from A to B to the potential diff erence VB − VA between the points. Combining Equations 19.2 and 19.3, we have:
VB − VA = EPEB
q0 −
EPEA
q0 =
−WAB q0
(19.4)
Often, the “delta” notation is used to express the diff erence (fi nal value minus initial value) in
potentials and in potential energies: ΔV = VB − VA and Δ(EPE) = EPEB − EPEA. In terms of this notation, Equation 19.4 takes the following more compact form:
∆V = ∆(EPE)
q0 =
−WAB q0
(19.4)
Neither the potential V nor the potential energy EPE can be determined in an absolute sense, because only the diff erences ΔV and Δ(EPE) are measurable in terms of the work WAB. The gravi- tational potential energy has this same characteristic, since only the value at one height relative
to the value at some reference height has any signifi cance. Example 1 emphasizes the relative
nature of the electric potential.
EXAMPLE 1 Work, Electric Potential Energy, and Electric Potential
In Interactive Figure 19.2, the work done by the electric force as the test charge (q0 = +2.0 × 10−6 C) moves from A to B is WAB = +5.0 × 10−5 J. (a) Find the value of the diff erence, Δ(EPE) = EPEB − EPEA, in the elec- tric potential energies of the charge between these points. (b) Determine the potential diff erence, ΔV = VB − VA, between the points.
Reasoning The work done by the electric force when the charge travels from A to B is WAB = EPEA − EPEB, according to Equation 19.1. There- fore, the diff erence in the electric potential energies (fi nal value minus
initial value) is Δ(EPE) = EPEB − EPEA = −WAB. The potential diff erence, ΔV = VB − VA, is the diff erence in the electric potential energies divided by the charge q0, according to Equation 19.4.
Solution (a) The diff erence in the electric potential energies of the charge between the points A and B is
EPE B − EPE A = −WAB = −5.0 × 10−5 J (19.1)
=∆(EPE)
⏟⎵⎵⏟⎵⎵⏟
The fact that EPEB − EPEA is negative means that the charge has a higher
electric potential energy at A than at B.
(b) The potential diff erence ΔV between A and B is
VB − VA = EPE B − EPE A
q0 =
−5.0 × 10−5 J
2.0 × 10−6 C = −25 V (19.4)
The fact that VB − VA is negative means that the electric potential is higher at A than at B.
= ∆V
⏟⏟⏟
The potential diff erence between two points is measured in volts and, therefore, is often
referred to as a “voltage.” Everyone has heard of “voltage” because, as we will see in Chapter 20,
it is frequently used in connection with everyday devices. For example, your TV requires a
“voltage” of 120 V (which is applied between the two prongs of the plug on the power cord
when it is inserted into an electrical wall outlet), and your cell phone and laptop computer use
batteries that provide, for example, “voltages” of 1.5 V or 9 V (which exist between the two
battery terminals).
In Figure 19.1 the speed of the basketball increases as it falls from A to B. Since point A has a greater gravitational potential energy than point B, we see that an object of mass m accelerates when it moves from a region of higher potential energy toward a region of lower
potential energy. Likewise, the positive charge in Interactive Figure 19.2 accelerates as it moves from A to B because of the electric repulsion from the upper plate and the attraction to the lower plate. Since point A has a higher electric potential than point B, we conclude the following:
Problem-Solving Insight A positive charge accelerates from a region of higher electric potential toward a region of lower electric potential.
526 CHAPTER 19 Electric Potential Energy and the Electric Potential
On the other hand, a negative charge placed between the plates in Interactive Figure 19.2 behaves in the opposite fashion, since the electric force acting on the negative charge is directed
opposite to the electric force acting on the positive charge.
Problem-Solving Insight A negative charge accelerates from a region of lower potential toward a region of higher potential.
The next example illustrates the way positive and negative charges behave.
CONCEPTUAL EXAMPLE 2 How Positive and Negative Charges Accelerate
Three points, A, B, and C, are located along a horizontal line, as Figure 19.3 illustrates. A positive test charge is released from rest at A and acceler- ates toward B. Upon reaching B, the test charge continues to accelerate toward C. Assuming that only motion along the line is possible, what will a negative test charge do when it is released from rest at B? A negative test charge will (a) accelerate toward C, (b) remain stationary, (c) accelerate toward A.
Reasoning A positive charge accelerates from a region of higher poten- tial toward a region of lower potential. A negative charge behaves in an
opposite manner, because it accelerates from a region of lower potential
toward a region of higher potential.
Answers (a) and (b) are incorrect. The positive charge accelerates from A to B and then from B to C. A negative charge placed at B also accelerates, but in a direction opposite to that of the positive charge.
Therefore, a negative charge placed at B will not remain stationary, nor will it accelerate toward C.
Answer (c) is correct. Since the positive charge accelerates from A to B, the potential at A must exceed the potential at B. And since the posi- tive test charge accelerates from B to C, the potential at B must exceed the potential at C. The potential at point B, then, must lie between the potential at points A and C, as Figure 19.3 illustrates. When the negative test charge is released from rest at B, it will accelerate toward the region of higher potential, so it will begin moving toward A.
Higher potential
Lower potential
A B C
FIGURE 19.3 The electric potentials at points A, B, and C are diff erent. Under the infl uence of these potentials,
positive and negative charges
accelerate in opposite
directions.
As a familiar application of electric potential energy and electric potential, Figure 19.4 shows a 12-V automobile battery with a headlight connected between its terminals. The positive
terminal, point A, has a potential that is 12 V higher than the potential at the negative terminal, point B; in other words, VA − VB = 12 V. Positive charges would be repelled from the positive terminal and would travel through the wires and headlight toward the negative terminal.* As
the charges pass through the headlight, virtually all their potential energy is converted into heat,
which causes the fi lament to glow “white hot” and emit light. When the charges reach the nega-
tive terminal, they no longer have any potential energy. The battery then gives the charges an
additional “shot” of potential energy by moving them to the higher-potential positive terminal,
and the cycle is repeated. In raising the potential energy of the charges, the battery does work on
them and draws from its reserve of chemical energy to do so. Example 3 illustrates the concepts
of electric potential energy and electric potential as applied to a battery.
A
B
12-V battery
+ −
Filament
FIGURE 19.4 A headlight connected to a 12-V battery.
*Historically, it was believed that positive charges fl ow in the wires of an electric circuit. Today, it is known that negative
charges fl ow in wires from the negative toward the positive terminal. Here, however, we follow the customary practice
of describing the fl ow of negative charges by specifying the opposite but equivalent fl ow of positive charges. This
hypothetical fl ow of positive charges is called the “conventional electric current,” as we will see in Section 20.1.
Analyzing Multiple-Concept Problems
EXAMPLE 3 Operating a Headlight
The wattage of the headlight in Figure 19.4 is 60.0 W. Determine the number of particles, each carrying a charge of 1.60 × 10−19 C (the magni-
tude of the charge on an electron), that pass between the terminals of the
12-V car battery when the headlight burns for one hour.
Reasoning The number of particles is the total charge that passes between the battery terminals in one hour divided by the magnitude of the
charge on each particle. The total charge is the amount of charge needed
to convey the energy used by the headlight in one hour. This energy is
19.2 The Electric Potential Diff erence 527
As used in connection with batteries, the volt is a familiar unit for measuring electric poten-
tial diff erence. The word “volt” also appears in another context, as part of a unit that is used to
measure energy, particularly the energy of an atomic particle, such as an electron or a proton.
This energy unit is called the electron volt (eV).
Problem-Solving Insight One electron volt is the magnitude of the amount by which the potential energy of an electron changes when the electron moves through a potential diff erence
of one volt.
Description Symbol Value Comment Wattage of headlight P 60.0 W
Charge magnitude per particle e 1.60 × 10−19 C
Electric potential difference between battery terminals VA − VB 12 V See Figure 19.4.
Time headlight is on t 3600 s One hour.
Unknown Variable Number of particles n ?
Modeling the Problem
STEP 1 The Number of Particles The number n of particles is the total charge q0 that passes between the battery terminals in one hour divided by the magnitude e of the charge on each particle, as expressed by Equation 1 at the right. The value of e is given. To evaluate q0, we proceed to Step 2.
STEP 2 The Total Charge Provided by the Battery The battery must supply the total energy used by the headlight in one hour. The battery does this by supplying the charge q0 to convey this energy. The energy is the diff erence between the electric potential energy EPEA at terminal A and the electric potential energy EPEB at terminal B of the battery (see Figure 19.4). According to Equation 19.4, this total energy is EPEA − EPEB = q0(VA − VB), where VA − VB is the electric potential diff erence between the battery terminals. Solving this expression for q0 gives
q 0 = EPE A − EPE B
VA − VB which can be substituted into Equation 1, as shown at the right. As the data table shows, a value
is given for VA − VB. In Step 3, we determine a value for EPEA − EPEB.
STEP 3 The Energy Used by the Headlight The rate at which the headlight uses energy is the power P or wattage of the headlight. According to Equation 6.10b, the power is the total energy EPEA − EPEB divided by the time t, so that P = (EPEA − EPEB)/t. Solving for the total energy gives
EPE A − EPE B = Pt
Since P and t are given, we substitute this result into Equation 2, as indicated at the right.
Solution Combining the results of each step algebraically, we fi nd that
n = q 0 e =
(EPE A − EPE B) / (VA − VB) e
= Pt/ (VA − VB)
e The number of particles that pass between the battery terminals in one hour is
n = Pt
e(VA − VB) =
(60.0 W)(3600 s)
(1.60 × 10−19 C)(12 V) = 1.1 × 10 23
Related Homework: Problems 5, 58
STEP 1 STEP 2 STEP 2
n = q 0 e
(1)
?
related to the wattage of the headlight, which specifi es the power or rate
at which energy is used, and the time the light is on.
Knowns and Unknowns The following table summarizes the data provided:
n = q 0 e
(1)
q 0 = EPE A − EPE B
VA − VB (2)
?
n = q 0 e
(1)
q 0 = EPE A − EPE B
VA − VB (2)
EPE A − EPE B = Pt
528 CHAPTER 19 Electric Potential Energy and the Electric Potential
Since the magnitude of the change in potential energy is |q0ΔV| = |(−1.60 × 10−19 C) × (1.00 V)| = 1.60 × 10−19 J, it follows that
1 eV = 1.60 × 10−19 J
One million (10+6) electron volts of energy is referred to as one MeV, and one billion (10+9) elec-
tron volts of energy is one GeV, where the “G” stands for the prefi x “giga” (pronounced “jigʹa”).
In Equation 19.3, we have seen that the electric potential is the electric potential energy per
unit charge. In previous chapters, we have seen that the total energy of an object, which is the
sum of its kinetic and potential energies, is an important concept. Its signifi cance lies in the fact
that the total energy remains the same (is conserved) during the object’s motion, provided that
nonconservative forces, such as friction, are either absent or do no net work. While the sum of
the energies at each instant remains constant, energy may be converted from one form to another;
for example, gravitational potential energy is converted into kinetic energy as a ball falls. We
now include the electric potential energy EPE as part of the total energy that an object can have:
E = 12mυ2 + 1
2Iω2 + mgh + 1
2 kx 2 + EPE
If the total energy is conserved as the object moves, then its fi nal energy Ef is equal to its initial energy E0, or Ef = E0. Example 4 illustrates how the conservation of energy is applied to a charge moving in an electric fi eld.
Total
energy
Translational
kinetic energy
Rotational
kinetic energy
Gravitational
potential
energy
Elastic
potential
energy
Electric
potential
energy { { { { { {
Analyzing Multiple-Concept Problems
EXAMPLE 4 The Conservation of Energy
A particle has a mass of 1.8 × 10−5 kg and a charge of +3.0 × 10−5 C. It
is released from rest at point A and accelerates until it reaches point B, as Figure 19.5a shows. The particle moves on a horizontal straight line and does not rotate. The only forces acting on the particle are the gravi-
tational force and an electrostatic force (neither is shown in the drawing).
The electric potential at A is 25 V greater than that at B; in other words, VA − VB = 25 V. What is the translational speed of the particle at point B?
Reasoning The translational speed of the particle is related to the parti- cle’s translational kinetic energy, which forms one part of the total energy
that the particle has. The total energy is conserved, because only the grav-
itational force and an electrostatic force, both of which are conservative
forces, act on the particle (see Section 6.5). Thus, we will determine the
speed at point B by utilizing the principle of conservation of energy.
Knowns and Unknowns We have the following data:
+
BA B
A = 0 m/s
(a)
BA A
–
B = 0 m/s
(b)
υ
υ
υ
υ
FIGURE 19.5 (a) A positive charge starts
from rest at point A and accelerates toward point B. (b) A negative charge starts from rest at B and accelerates toward A.
Description Symbol Value Comment Explicit Data Mass of particle m 1.8 × 10−5 kg
Electric charge of particle q0 +3.0 × 10−5 C
Electric potential difference between points A and B VA − VB 25 V See Figure 19.5a. Implicit Data Speed at point A 𝜐A 0 m/s Particle released from rest.
Vertical height above ground h Remains constant Particle travels horizontally.
Angular speed 𝜔 0 rad/s Particle does not rotate during motion.
Elastic force Felastic 0 N No elastic force acts on particle.
Unknown Variable Speed at point B 𝜐B ?
19.2 The Electric Potential Diff erence 529
Modeling the Problem
STEP 1 Conservation of Total Energy The particle’s total energy E is
E = 12mυ2 + 1
2Iω2 + mgh + 1
2 kx 2 + EPE
Since the particle does not rotate, the angular speed 𝜔 is always zero (see the data table) and since there is no elastic force (see the data table), we may omit the terms
1
2lω2 and 1
2 kx 2 from this expression. With this in mind, we express the fact that EB = EA (energy is conserved) as follows:
1
2 mυ 2B + mgh B + EPE B = 1
2 mυ 2A + mgh A + EPE A
This equation can be simplifi ed further, since the particle travels horizontally, so that hB = hA (see the data table), with the result that
1
2 mυB2 + EPE B = 1
2 mυA2 + EPE A
Solving for 𝜐B gives Equation 1 at the right. Values for 𝜐A and m are available, and we turn to Step 2 in order to evaluate EPEA − EPEB.
STEP 2 The Electric Potential Diff erence According to Equation 19.4, the diff erence in electric potential energies EPEA − EPEB is related to the electric potential diff erence VA − VB:
EPEA − EPEB = q0(VA − VB)
The terms q0 and VA − VB are known, so we substitute this expression into Equation 1, as shown at the right.
Problem-Solving Insight A positive charge accelerates from a region of higher potential toward a region of lower potential. In contrast, a negative charge accel- erates from a region of lower potential toward a region of higher potential.
Solution Combining the results of each step algebraically, we fi nd that
υB = √υ 2A + 2(EPE A − EPE B)m = √υ 2A + 2q 0 (VA − VB)
m
The speed of the particle at point B is
υB = √υ 2A + 2q 0 (VA − VB)m = √(0 m /s)2 + 2(+3.0 × 10−5 C)(25 V)
1.8 × 10−5 kg = 9.1 m /s
Note that if the particle had a negative charge of −3.0 × 10−5 C and were released from rest at
point B, it would arrive at point A with the same speed of 9.1 m/s (see Figure 19.5b). This result can be obtained by returning to Modeling Step 1 and solving for 𝜐A instead of 𝜐B.
Related Homework: Problems 6, 7
{
Translational
kinetic energy
{
Rotational
kinetic energy
{
Gravitational
potential
energy
{
Elastic
potential
energy
{
Electric
potential
energy
STEP 1 STEP 2
υB = √υ 2A + 2(EPE A − EPE B)m (1) ?
υB = √υ 2A + 2(EPE A − EPE B)m (1) EPEA − EPEB = q0(VA − VB)
Check Your Understanding
(The answers are given at the end of the book.) 1. An ion, starting from rest, accelerates from point A to point B due to a potential diff erence between the
two points. Does the electric potential energy of the ion at point B depend on (a) the magnitude of its charge and (b) its mass? Does the speed of the ion at B depend on (c) the magnitude of its charge and (d) its mass?
(Continued)
530 CHAPTER 19 Electric Potential Energy and the Electric Potential
2. CYU Figure 19.1 shows three possibilities for the potentials at two points, A and B. In each case, the same positive charge is moved from A to B. In which case, if any, is the most work done on the positive charge by the electric force?
A B A B A B • • • • • •
150 V 100 V 25 V −25 V −10 V −60 V
Case 1 Case 2 Case 3
CYU FIGURE 19.1
3. A proton and an electron are released from rest at the midpoint between the plates of a charged parallel plate capacitor (see Section 18.6). Except for these particles, nothing else is between the
plates. Ignore the attraction between the proton and the electron, and decide which particle strikes
a capacitor plate fi rst.
19.3 The Electric Potential Diff erence Created by Point Charges A positive point charge +q creates an electric potential in a way that Figure 19.6 helps explain. This picture shows two locations A and B, at distances rA and rB from the charge. At any position between A and B an electrostatic force of repulsion F→ acts on a positive test charge +q0. The mag- nitude of the force is given by Coulomb’s law as F = kq0q/r2, where we assume for convenience that q0 and q are positive, so that |q0| = q0 and |q| = q. When the test charge moves from A to B, work is done by this force. Since r varies between rA and rB, the force F also varies, and the work is not the product of the force and the distance between the points. (Recall from Section 6.1 that
work is force times distance only if the force is constant.) However, the work WAB can be found with the methods of integral calculus. The result is
WAB = kqq 0
rA −
kqq 0 rB
This result is valid whether q is positive or negative, and whether q0 is positive or negative. The potential diff erence, VB − VA, between A and B can now be determined by substituting this expres- sion for WAB into Equation 19.4:
VB − VA = −WAB
q 0 =
kq rB
− kq rA
(19.5)
As point B is located farther and farther from the charge q, rB becomes larger and larger. In the limit that rB is infi nitely large, the term kq/rB becomes zero, and it is customary to set VB equal to zero also. In this limit, Equation 19.5 becomes VA = kq/rA, and it is standard convention to omit the subscripts and write the potential in the following form:
Potential of a point charge V = kq r (19.6)
The symbol V in this equation does not refer to the potential in any absolute sense. Rather, V = kq/r stands for the amount by which the potential at a distance r from a point charge diff ers from the potential at an infi nite distance away. In other words, V refers to a potential diff erence with the arbitrary assumption that the potential at infi nity is zero.
With the aid of Equation 19.6, we can describe the eff ect that a point charge q has on the surrounding space. When q is positive, the value of V = kq/r is also positive, indicating that the positive charge has everywhere raised the potential above the zero reference value. Conversely,
when q is negative, the potential V is also negative, indicating that the negative charge has every- where decreased the potential below the zero reference value. The next example deals with these
eff ects quantitatively.
Lower (downhill) potential
Higher (uphill) potential
A F B
rA rB
+q0+q
FIGURE 19.6 The positive test charge +q0 experiences a repulsive force F→ due to the positive point charge +q. As a result, work is done by this force when the test charge
moves from A to B. Consequently, the electric potential is higher (uphill) at A and lower (downhill) at B.
Math Skills In Equation 19.6 the symbol q denotes the value of the point charge, including both the mag- nitude of and the algebraic sign of the charge. Note especially that the symbol q does not have the same meaning as the symbol |q|, which denotes only the magnitude of the charge. When you use
Equation 19.6 to solve problems deal-
ing with the potential of a point charge,
both the magnitude and the algebraic
sign of the charge must be taken into
account, and the presence of q (rather than |q|) in the equation ensures that this will be so. Using only the magni-
tude of a point charge in Equation 19.6
would ignore the important fact that
positive and negative point charges
create diff erent potentials, even when
the charge magnitudes are the same.
19.3 The Electric Potential Diff erence Created by Point Charges 531
A single point charge raises or lowers the potential at a given location, depending on whether
the charge is positive or negative.
Problem-Solving Insight When two or more charges are present, the potential due to all the charges is obtained by adding together the individual potentials.
The next two examples will demonstrate this point.
EXAMPLE 5 The Potential of a Point Charge
Using a zero reference potential at infi nity, determine the amount by
which a point charge of 4.0 × 10−8 C alters the electric potential at a spot
1.2 m away when the charge is (a) positive and (b) negative.
Reasoning A point charge q alters the potential at every location in the surrounding space. In the expression V = kq/r, the eff ect of the charge in increasing or decreasing the potential is conveyed by the algebraic sign
for the value of q.
Solution (a) Figure 19.7a shows the potential when the charge is positive:
V = kq r
= (8.99 × 10 9 N · m2 / C 2 )(+4.0 × 10−8 C)
1.2 m = +300 V (19.6)
(b) Part b of the drawing illustrates the results when the charge is nega- tive. A calculation similar to the one in part (a) shows that the potential is
now negative: −300 V .
1.2 m
−300 V
+300 V
V = 0 at r = ∞
−4.0 × 10–8 C
+4.0 × 10–8 C
1.2 m(a)
(b)
V = 0 at r = ∞
FIGURE 19.7 A point charge of 4.0 × 10−8 C alters
the potential at a spot 1.2 m
away. The potential is
(a) increased by 300 V when the charge is positive
and (b) decreased by 300 V when the charge is negative,
relative to a zero reference
potential at infi nity.
CONCEPTUAL EXAMPLE 7 Where Is the Potential Zero?
Two point charges are fi xed in place, as in Figure 19.9. The positive charge is +2q and has twice the magnitude of the negative charge, which is −q. On the line that passes through the charges, three spots are identi- fi ed, P1, P2, and P3. At which of these spots could the potential be equal to zero? (a) P2 and P3 (b) P1 and P3 (c) P1 and P2
Reasoning The total potential is the algebraic sum of the individual potentials created by each charge. It will be zero if the potential due to
the positive charge is exactly off set by the potential due to the negative
charge. The potential of a point charge is directly proportional to the
charge and inversely proportional to the distance from the charge.
EXAMPLE 6 The Total Electric Potential
At locations A and B in Figure 19.8, fi nd the total electric potential due to the two point charges.
Reasoning At each location, each charge contributes to the total elec- tric potential. We obtain the individual contributions by using V = kq/r and fi nd the total potential by adding the individual contributions alge-
braically. The two charges have the same magnitude, but diff erent signs.
Thus, at A the total potential is positive because this spot is closer to the positive charge, whose eff ect dominates over that of the more distant
negative charge. At B, midway between the charges, the total potential is zero, since the potential of one charge exactly off sets that of the other.
Solution
+8.0 × 10–9 C −8.0 × 10–9 C
0.20 m 0.20 m 0.40 m
A B
FIGURE 19.8 Both the positive and negative charges aff ect the electric potential at locations
A and B.
Location Contribution from + Charge Contribution from − Charge Total Potential
A (8.99 × 10 9 N · m2 /C2 )(+8.0 × 10−9 C)
0.20 m +
(8.99 × 10 9 N · m2/C 2)(−8.0 × 10−9 C) 0.60 m
= +240 V
B (8.99 × 10 9 N · m2/C 2 )(+8.0 × 10−9 C)
0.40 m −
(8.99 × 10 9 N · m2/C 2 )(−8.0 × 10−9 C) 0.40 m
= 0 V
532 CHAPTER 19 Electric Potential Energy and the Electric Potential
In Example 6 we determined the total potential at a spot due to two point charges. In
Example 8 we now extend this technique to fi nd the total potential energy of three charges.
Answers (b) and (c) are incorrect. The total potential at P1 cannot be zero. The positive charge has the larger magnitude and is closer to P1 than is the negative charge. As a result, the potential of the positive charge at P1 dominates over the potential of the negative charge, so the total potential
cannot be zero.
Answer (a) is correct. Between the charges there is a location at which the individual potentials cancel each other. We saw a similar situation in
Example 6, where the canceling occurred at the midpoint between the two
charges that had equal magnitudes. Now the charges have unequal mag-
nitudes, so the cancellation point does not occur at the midpoint. Instead,
it occurs at the location P2, which is closer to the charge with the smaller magnitude—namely, the negative charge. At P2, since the potential of a point charge is inversely proportional to the distance from the charge, the
eff ect of the smaller charge will be able to off set the eff ect of the more
distant larger charge.
To the right of the negative charge there is also a location at which
the individual potentials exactly cancel each other. All places on this
section of the line are closer to the negative charge than to the positive
charge. Therefore, there is a location P3 in this region at which the po- tential of the smaller negative charge exactly cancels the potential of the
more distant and larger positive charge.
Related Homework: Problem 30
−q+2q P1 P2 P3
FIGURE 19.9 Two point charges, one positive and one negative. The positive charge,
+2q, has twice the magnitude of the negative charge, −q.
EXAMPLE 8 The Potential Energy of a Group of Charges
Three point charges initially are infi nitely far apart. Then, as Figure 19.10 shows, they are brought together and placed at the corners of an equilat-
eral triangle. Each side of the triangle has a length of 0.50 m. Determine
the electric potential energy of the triangular group. In other words, de-
termine the amount by which the electric potential energy of the group
diff ers from that of the three charges in their initial, infi nitely separated,
locations.
Reasoning We will proceed in steps by adding charges to the triangle one at a time, and then determining the electric potential energy at each
step. According to Equation 19.3, EPE = q0V, the electric potential energy is the product of the charge and the electric potential at the spot where the
charge is placed. The total electric potential energy of the triangular group
is the sum of the energies of each step in assembling the group.
Solution The order in which the charges are put on the triangle does not matter; we begin with the charge q1 = +5.0 𝜇C. When this charge is placed at a corner of the triangle, it has no electric potential energy,
according to EPE1 = q1(V2 + V3) = 0 J (Equation 19.3). This is because the total potential V2 + V3 produced by the other two charges is zero at this
Math Skills To illustrate that the order in which the charges are put on the triangle does not matter, let us obtain the total potential
energy of the group when the order begins with q2, continues with q3, and concludes with q1. When q2 is placed at a corner of the tri- angle, it has no electric potential energy EPE2, since it experiences
no electric potential due to the other charges, which are infi nitely
far away. Thus, we have
EPE 2 = 0 J
Once q2 is in place, it creates a potential V2 = kq 2 r
(Equation 19.6)
at either empty corner located a distance r away. When the charge q3 is placed at an empty corner, it experiences this potential and has an electric potential energy EPE3, as specifi ed by Equation 19.3:
EPE 3 = q 3V2 = q 3 kq 2
r Each of the charges in place creates a potential at the remaining empty
corner. Using Equation 19.6 for each charge, we see that the total
potential at the remaining empty corner is V2 + V3 = kq 2
r +
kq 3 r
.
When charge q1 is placed on this corner, therefore, it experiences this potential and has an electric potential energy EPE1, as given
by Equation 19.3:
EPE 1 = q 1(V2 + V3 ) = q1 kq 2
r +
q1 kq 3 r
Thus, we obtain the following total electric potential energy of
the group:
Total potential energy = 0 J + q 3 kq 2
r +
q1 kq 2 r
+ q1 kq 3
r This result is exactly the same as that determined in Example 8,
where a diff erent order of adding the charges is used: fi rst q1, second q2, and third q3.
q2 = +6.0 C q3 = –2.0 C
q1 = +5.0 Cμ
μμ
FIGURE 19.10 Three point charges are placed on the corners of an equilateral triangle.
Example 8 illustrates how to determine the
total electric potential energy of this group
of charges.
19.3 The Electric Potential Diff erence Created by Point Charges 533
Check Your Understanding
(The answers are given at the end of the book.) 4. CYU Figure 19.2 shows four arrangements (A–D) of two point charges. In each arrangement consider
the total electric potential that the charges produce at location P. Rank the arrangements (largest to smallest) according to the total potential. (a) B, C, A and D (a tie) (b) D, C, A, B (c) A and C (a tie), B, D (d) C, D, A, B
CYU FIGURE 19.2
+2q +2q +2q +2q
2r0 2r0 2r0 r0
2r0 2r0
r0 r0
−q
−q −q
−q
A
P P P P
B C D
5. A positive point charge and a negative point charge have equal magnitudes. One charge is fi xed to one corner of a square, and the other is fi xed to another corner. On which corners should the charges
be placed, so that the same potential exists at the empty corners? The charges should be placed at
(a) adjacent corners, (b) diagonally opposite corners. 6. Three point charges have identical magnitudes, but two of the charges are positive and one is negative.
These charges are fi xed to the corners of a square, one to a corner. No matter how the charges are ar-
ranged, the potential at the empty corner is always (a) zero, (b) negative, (c) positive. 7. Consider a spot that is located midway between two identical point charges. Which one of the following
statements concerning the electric fi eld and the electric potential at this spot is true? (a) The electric fi eld is zero, but the electric potential is not zero. (b) The electric fi eld is not zero, but the electric po- tential is zero. (c) Both the electric fi eld and the electric potential are zero. (d) Neither the electric fi eld nor the electric potential is zero.
8. Four point charges have the same magnitude (but they may have diff erent signs) and are placed at the corners of a square, as CYU Figure 19.3 shows. What must be the sign (+ or −) of each charge so that
corner, since they are infi nitely far away. Once the charge q1 is in place, the potential it creates at either empty corner (r = 0.50 m) is
V1 = kq1 r
= (8.99 × 10 9 N · m2 / C2 )(+5.0 × 10−6 C)
0.50 m
= +9.0 × 10 4 V (19.6)
Therefore, when the charge q2 = +6.0 𝜇C is placed at the second corner of the triangle, its electric potential energy is
EPE 2 = q 2V1 = q 2 kq 1
r = (+6.0 × 10−6 C)(+9.0 × 10 4 V)
= +0.54 J (19.3)
The electric potential at the remaining empty corner is the sum of the
potentials due to the two charges that are already in place:
V1 + V2 = kq1 r
+ kq 2 r
= (8.99 × 10 9 N · m2 /C2 )(+5.0 × 10−6 C)
0.50 m
+ (8.99 × 10 9 N · m2 / C2 )(+6.0 × 10−6 C)
0.50 m
= +2.0 × 10 5 V
When the third charge q3 = −2.0 𝜇C is placed at the remaining empty corner, its electric potential energy is
EPE 3 = q 3 (V1 + V2 ) = q 3 kq1
r +
q 3 kq 2 r
= (−2.0 × 10−6 C)(+2.0 × 10 5 V) = −0.40 J (19.3)
Problem-Solving Insight Be careful to distinguish between the concepts of potential V and electric potential energy EPE. Potential is electric potential energy per unit charge: V = EPE/q.
The total potential energy of the triangular group diff ers from that of
the widely separated charges by an amount that is the sum of the potential
energies calculated previously:
Total potential energy = 0 J + q2kq1
r +
q3kq1 r
+ q3kq 2
r
= 0 J + 0.54 J − 0.40 J = +0.14 J
This energy originates in the work done to bring the charges together.
{
EPE2
{
EPE1 EPE3
⏟⎵⎵⏟⎵⎵⏟
(Continued)
534 CHAPTER 19 Electric Potential Energy and the Electric Potential
both the electric fi eld and the electric potential are zero at the center of the square? Assume that the potential has a zero value at infi nity.
q1 q2
q4 q3
q1 q2 q3 q4 (a) − − − −
(b) + + − −
(c) + + + +
(d) + − + −
CYU FIGURE 19.3
9. An electric potential energy exists when two protons are separated by a certain distance. Does the electric potential energy increase, decrease, or remain the same (a) when both protons are replaced by electrons, and (b) when only one of the protons is replaced by an electron?
10. A proton is fi xed in place. An electron is released from rest and allowed to collide with the proton. Then the roles of the proton and electron are reversed, and the same experiment is repeated. Which, if either,
is traveling faster when the collision occurs, the proton or the electron?
19.4 Equipotential Surfaces and Their Relation to the Electric Field An equipotential surface is a surface on which the electric potential is the same everywhere. The easiest equipotential surfaces to visualize are those that surround an isolated point charge.
According to Equation 19.6, the potential at a distance r from a point charge q is V = kq/r. Thus, wherever r is the same, the potential is the same, and the equipotential surfaces are spherical sur- faces centered on the charge. There are an infi nite number of such surfaces, one for every value of
r, and Figure 19.11 illustrates two of them. The larger the distance r, the smaller is the potential of the equipotential surface.
The net electric force does no work as a charge moves on an equipotential surface. This important characteristic arises because when an electric force does work WAB as a charge moves from A to B, the potential changes according to VB − VA = −WAB/q0 (Equation 19.4). Since the potential remains the same everywhere on an equipotential surface, VA = VB, and we see that WAB = 0 J. In Figure 19.11, for instance, the electric force does no work as a test charge moves along the circular arc ABC, which lies on an equipotential surface. In contrast, the electric force does work when a charge moves between equipotential surfaces, as from A to D in the picture.
The spherical equipotential surfaces that surround an isolated point charge illustrate another
characteristic of all equipotential surfaces. Figure 19.12 shows two of the surfaces around a posi- tive point charge, along with some electric fi eld lines. The electric fi eld lines give the direction
of the electric fi eld, and for a positive point charge the electric fi eld is directed radially outward.
Therefore, at each location on an equipotential sphere the electric fi eld is perpendicular to the
surface and points outward in the direction of decreasing potential, as the drawing emphasizes.
This perpendicular relation is valid whether or not the equipotential surfaces result from a posi-
tive charge or have a spherical shape.
Problem-Solving Insight The electric fi eld created by any charge or group of charges is everywhere perpendicular to the associated equipotential surfaces and points in the direction
of decreasing potential.
For example, Animated Figure 19.13 shows the electric fi eld lines (in red) around an electric dipole, along with some equipotential surfaces (in blue), shown in cross section. Since the fi eld
lines are not simply radial, the equipotential surfaces are no longer spherical but, instead, have
the shape necessary to be everywhere perpendicular to the fi eld lines.
To see why an equipotential surface must be perpendicular to the electric fi eld, consider
Figure 19.14, which shows a hypothetical situation in which the perpendicular relation does not hold. If E→ were not perpendicular to the equipotential surface, there would be a component of E→
+q D B
A
C
Equipotential surfaces
FIGURE 19.11 The equipotential surfaces that surround the point charge +q are spherical. The electric force does no work
as a charge moves on a path that lies on
an equipotential surface, such as the path
ABC. However, work is done by the electric force when a charge moves between two
equipotential surfaces, as along the path AD.
+q
Higher potential
Lower potential 90°
90° 90° Electric field line
FIGURE 19.12 The radially directed electric fi eld of a point charge is perpendicular to the
spherical equipotential surfaces that surround
the charge. The electric fi eld points in the
direction of decreasing potential.
19.4 Equipotential Surfaces and Their Relation to the Electric Field 535
parallel to the surface. This fi eld component would exert an electric force on a test charge placed
on the surface. As the charge moved along the surface, work would be done by this component
of the electric force. The work, according to Equation 19.4, would cause the potential to change,
and, thus, the surface could not be an equipotential surface as assumed. The only way out of the
dilemma is for the electric fi eld to be perpendicular to the surface, so there is no component of
the fi eld parallel to the surface.
We have already encountered one equipotential surface. In Section 18.8, we found that the
direction of the electric fi eld just outside an electrical conductor is perpendicular to the conduc-
tor’s surface, when the conductor is at equilibrium under electrostatic conditions. Thus, the sur-
face of any conductor is an equipotential surface under such conditions. In fact, since the electric
fi eld is zero everywhere inside a conductor whose charges are in equilibrium, the entire conduc-
tor can be regarded as an equipotential volume.
There is a quantitative relation between the electric fi eld and the equipotential surfaces. One
example that illustrates this relation is the parallel plate capacitor in Figure 19.15. As Section 18.6 discusses, the electric fi eld E→ between the metal plates is perpendicular to them and is the same everywhere, ignoring fringe fi elds at the edges. To be perpendicular to the electric fi eld, the equi-
potential surfaces must be planes that are parallel to the capacitor plates, which themselves are
equipotential surfaces. The potential diff erence between the plates is given by Equation 19.4 as
ΔV = VB − VA = −WAB/q0, where A is a point on the positive plate and B is a point on the negative plate. The work done by the electric force as a positive test charge q0 moves from A to B is WAB = FΔs, where F refers to the electric force and Δs to the displacement along a line perpendicular to the plates. The force equals the product of the charge and the electric fi eld E (F = q0E), so the work becomes WAB = FΔs = q0EΔs. Therefore, the potential diff erence between the capacitor plates can be written in terms of the electric fi eld as ΔV = −WAB/q0 = −q0EΔs/q0, or
E = − ∆V ∆s
(19.7a)
The quantity ΔV/Δs is referred to as the potential gradient and has units of volts per meter. In general, the relation E = −ΔV/Δs gives only the component of the electric fi eld along the dis- placement Δs; it does not give the perpendicular component. The next example deals further with the equipotential surfaces between the plates of a capacitor.
+ −
ANIMATED FIGURE 19.13 A cross-sectional view of the equipotential surfaces (in blue) of an electric dipole. The surfaces are drawn to show that at every point they are perpendicular to the electric fi eld lines
(in red) of the dipole.
Equipotential surface
E
Component of E parallel to the
equipotential surface
FIGURE 19.14 In this hypothetical situation, the electric fi eld E→ is not perpendicular to the equipotential surface. As a result, there is a
component of E→ parallel to the surface.
Equipotential surfaces
Δs
A B
E
a b
FIGURE 19.15 The metal plates of a parallel plate capacitor are equipotential surfaces. Two
additional equipotential surfaces are shown
between the plates. These two equipotential
surfaces are parallel to the plates and are
perpendicular to the electric fi eld E→ between the plates.
EXAMPLE 9 The Electric Field and Potential Are Related
The plates of the capacitor in Figure 19.15 are separated by a distance 0.032 m, and the potential diff erence between them is (ΔV)plates = VB − VA = −64 V. Between the two blue equipotential surfaces there is a poten- tial diff erence of (ΔV)blue = Vb − Va = −3.0 V. Find the spacing between the two blue surfaces.
Reasoning To fi nd the spacing between the blue surfaces, we will solve Equation 19.7a for (Δs)blue with (ΔV)blue = −3.0 V and E equal to the electric fi eld between the plates of the capacitor. The electric fi eld E is the same everywhere between the plates (ignoring the fringe fi elds). A value
for E can be obtained by using Equation 19.7a with the data given for the
536 CHAPTER 19 Electric Potential Energy and the Electric Potential
Equation 19.7a gives the relationship between the electric fi eld and the electric potential.
It gives the component of the electric fi eld along the displacement Δs in a region of space where the electric potential changes from place to place and applies to a wide variety of situ-
ations. When applied strictly to a parallel plate capacitor, however, this expression is often
used in a slightly diff erent form. In Figure 19.15, the metal plates of the capacitor are marked A (higher potential) and B (lower potential). Traditionally, in discussions of such a capacitor, the potential diff erence between the plates is referred to by using the symbol V to denote the amount by which the higher potential exceeds the lower potential (V = VA − VB). In this tradi- tion, the symbol V is often referred to as simply the “voltage.” For example, if the potential diff erence between the plates of a capacitor is 5 volts, it is common to say that the “voltage”
of the capacitor is 5 volts. In addition, the displacement from plate A to plate B is expressed in terms of the separation d between the plates (d = sB − sA). With this nomenclature, Equation 19.7a becomes
E = − ∆V ∆s
= − VB − VA sB − sA
= VA − VB sB − sA
= V d (parallel plate capacitor) (19.7b)
Check Your Understanding
(The answers are given at the end of the book.) 11. CYU Figure 19.4 shows a cross-sectional view of two spherical equi-
potential surfaces and two electric fi eld lines that are perpendicular
to these surfaces. When an electron moves from point A to point B (against the electric fi eld), the electric force does +3.2 × 10−19 J
of work. What are the electric potential diff erences (a) VB − VA, (b) VC − VB, and (c) VC − VA?
12. The electric potential is constant throughout a given region of space. Is the electric fi eld zero or nonzero in this region?
13. In a region of space where the electric fi eld is constant everywhere, as it is inside a parallel plate capacitor, is the potential constant
everywhere? (a) Yes. (b) No, the potential is greatest at the posi- tive plate. (c) No, the potential is greatest at the negative plate.
14. A positive test charge is placed in an electric fi eld. In what direction should the charge be moved relative to the fi eld, so that the charge experiences a constant electric potential? The charge should be
moved (a) perpendicular to the electric fi eld, (b) in the same direction as the electric fi eld, (c) opposite to the direction of the electric fi eld.
distance between the plates and the potential diff erence between them
[(Δs)plates = 0.032 m and (ΔV)plates = −64 V].
Solution Solving Equation 19.7a for the spacing between the blue equi- potential surfaces gives
(∆s) blue = − (∆V ) blue
E
Using Equation 19.7a to determine the electric fi eld between the plates,
we fi nd that
E = − (∆V ) plates (∆s) plates
= − −64 V
0.032 m = 2.0 × 10 3 V/m
Substituting this result into the equation for (Δs)blue gives
(∆s) blue = − (∆V ) blue
E = −
−3.0 V
2.0 × 10 3 V/m = 1.5 × 10−3 m
Equipotential surfaces
Δs
A B
E
a b
FIGURE 19.15 (REPEATED) The metal plates of a parallel plate capacitor are equipotential surfaces. Two additional equipotential
surfaces are shown between the plates. These two equipotential surfaces
are parallel to the plates and are perpendicular to the electric fi eld E→ between the plates.
CYU FIGURE 19.4
A
B
C
Equipotential surfaces (Cross-sectional view)
Electric field lines
19.5 Capacitors and Dielectrics 537
15. The location marked P in CYU Figure 19.5 lies midway between the point charges +q and −q. The blue lines labeled A, B, and C are edge-on views of three planes. Which of the planes is an equipoten-
tial surface? (a) A and C (b) A, B, and C (c) Only B (d) None of the planes is an equipotential surface.
16. Imagine that you are moving a positive test charge along the line between two identical point charges. With regard to the electric po-
tential, is the midpoint on the line analogous to the top of a mountain
or the bottom of a valley when the two point charges are (a) positive and (b) negative?
19.5 Capacitors and Dielectrics
The Capacitance of a Capacitor In Section 18.6 we saw that a parallel plate capacitor consists of two parallel metal plates placed
near one another but not touching. This type of capacitor is only one among many. In general,
a capacitor consists of two conductors of any shape placed near one another without touching. For a reason that will become clear later on, it is common practice to fi ll the region between the
conductors or plates with an electrically insulating material called a dielectric, as Figure 19.16 illustrates.
A capacitor stores electric charge. Each capacitor plate carries a charge of the same mag- nitude, one positive and the other negative. Because of the charges, the electric potential of the positive plate exceeds that of the negative plate by an amount V, as Figure 19.16 indicates. Experiment shows that when the magnitude q of the charge on each plate is doubled, the magni- tude V of the electric potential diff erence is also doubled, so q is proportional to V: q ∝ V. Equa- tion 19.8 expresses this proportionality with the aid of a proportionality constant C, which is the capacitance of the capacitor.
THE RELATION BETWEEN CHARGE AND POTENTIAL DIFFERENCE FOR A CAPACITOR The magnitude q of the charge on each plate of a capacitor is directly proportional to the magnitude V of the potential diff erence between the plates:
q = CV (19.8)
where C is the capacitance.
SI Unit of Capacitance: coulomb/volt = farad (F)
Equation 19.8 shows that the SI unit of capacitance is the coulomb per volt (C/V). This unit is
called the farad (F), named after the English scientist Michael Faraday (1791–1867). One farad is an enormous capacitance. Usually smaller amounts, such as a microfarad (1 𝜇F = 10−6 F) or a
picofarad (1 pF = 10−12 F), are used in electric circuits. The capacitance refl ects the ability of the
capacitor to store charge, in the sense that a larger capacitance C allows more charge q to be put onto the plates for a given value of the potential diff erence V.
THE PHYSICS OF . . . random-access memory (RAM) chips. The ability of a capacitor to store charge lies at the heart of the random-access memory (RAM) chips used in computers,
where information is stored in the form of the “ones” and “zeros” that comprise binary numbers.
Figure 19.17 illustrates the role of a capacitor in a RAM chip. The capacitor is connected to a transistor switch, to which two lines are connected, an address line and a data line. A single
RAM chip often contains millions of such transistor–capacitor units. The address line is used by
the computer to locate a particular transistor–capacitor combination, and the data line carries
the data to be stored. A pulse on the address line turns on the transistor switch. With the switch
turned on, a pulse coming in on the data line can cause the capacitor to charge. A charged capaci-
tor means that a “one” has been stored, whereas an uncharged capacitor means that a “zero” has
been stored.
CYU FIGURE 19.5
+q –qP
CA
B
Voltmeter
Dielectric
Metal plate (area = A)
Plate separation
= d
Electric potential difference = V
FIGURE 19.16 A parallel plate capacitor consists of two metal plates, one carrying a
charge +q and the other a charge −q. The potential of the positive plate exceeds that of
the negative plate by an amount V. The region between the plates is fi lled with a dielectric.
Data line
Capacitor
Address line
Transistor switch
FIGURE 19.17 A transistor–capacitor combination is part of a RAM chip used in
computer memories.
538 CHAPTER 19 Electric Potential Energy and the Electric Potential
The Dielectric Constant If a dielectric is inserted between the plates of a capacitor, the capacitance can increase mark-
edly because of the way in which the dielectric alters the electric fi eld between the plates.
Interactive Figure 19.18 shows how this eff ect comes about. In part a, the region between the charged plates is empty. The fi eld lines point from the positive toward the negative plate. In
part b, a dielectric has been inserted between the plates. Since the capacitor is not connected to anything, the charge on the plates remains constant as the dielectric is inserted. In many
materials (e.g., water) the molecules possess permanent dipole moments, even though the mol-
ecules are electrically neutral. The dipole moment exists because one end of a molecule has
a slight excess of negative charge while the other end has a slight excess of positive charge.
When such molecules are placed between the charged plates of the capacitor, the negative ends
are attracted to the positive plate and the positive ends are attracted to the negative plate. As a
result, the dipolar molecules tend to orient themselves end to end, as in part b. Whether or not a molecule has a permanent dipole moment, the electric fi eld can cause the electrons to shift
position within a molecule, making one end slightly negative and the opposite end slightly
positive. Because of the end-to-end orientation, the left surface of the dielectric becomes posi-
tively charged, and the right surface becomes negatively charged. The surface charges are
shown in red in the picture.
Because of the surface charges on the dielectric, not all the electric fi eld lines generated by
the charges on the plates pass through the dielectric. As Interactive Figure 19.18c shows, some of the fi eld lines end on the negative surface charges and begin again on the positive surface
charges. Thus, the electric fi eld inside the dielectric is less strong than the electric fi eld inside
the empty capacitor, assuming the charge on the plates remains constant. This reduction in the
electric fi eld is described by the dielectric constant κ, which is the ratio of the fi eld magnitude E0 without the dielectric to the fi eld magnitude E inside the dielectric:
κ = E 0 E
(19.9)
Being a ratio of two fi eld strengths, the dielectric constant is a number without units. Moreover, since the fi eld E→0 without the dielectric is greater than the fi eld E
→ inside the dielectric, the dielec-
tric constant is greater than unity. The value of 𝜅 depends on the nature of the dielectric material, as Table 19.1 indicates.
The Capacitance of a Parallel Plate Capacitor The capacitance of a capacitor is aff ected by the geometry of the plates and the dielectric con-
stant of the material between them. For example, Figure 19.16 shows a parallel plate capacitor in which the area of each plate is A and the separation between the plates is d. The magnitude of the electric fi eld inside the dielectric is given by Equation 19.7b as E = V/d, where V is the magnitude of the potential diff erence between the plates. If the charge on each plate is kept fi xed,
the electric fi eld inside the dielectric is related to the electric fi eld in the absence of the dielectric
via Equation 19.9. Therefore,
E = E 0 κ =
V d
Since the electric fi eld within an empty capacitor is E0 = q/(𝜀0A) (see Equation 18.4), it follows that q/(𝜅𝜀0A) = V/d, which can be solved for q to give
q = ( κε0 A
d )V A comparison of this expression with q = CV (Equation 19.8) reveals that the capacitance C is
Parallel plate capacitor fi lled with a dielectric C =
κε0 A d
(19.10)
Only the geometry of the plates (A and d) and the dielectric constant 𝜅 aff ect the capacitance. With C0 representing the capacitance of the empty capacitor (κ = 1), Equation 19.10 shows that
–q +q
(a)
Positive surface charge on dielectric
Negative surface charge on dielectric
Molecule (b)
(c)
–q +q
–q +q
INTERACTIVE FIGURE 19.18 (a) The electric fi eld lines inside an empty capacitor.
(b) The electric fi eld produced by the charges on the plates aligns the molecular dipoles
within the dielectric end to end. The space
between the dielectric and the plates is added
for clarity. In reality, the dielectric fi lls the
region between the plates. (c) The surface charges on the dielectric reduce the electric
fi eld inside the dielectric.
TABLE 19.1 Dielectric Constants of Some Common Substancesa
Substance Dielectric
Constant, κ Vacuum 1
Air 1.000 54
Teflon 2.1
Benzene 2.28
Paper (royal gray) 3.3
Ruby mica 5.4
Neoprene rubber 6.7
Methyl alcohol 33.6
Water 80.4
aNear room temperature.
19.5 Capacitors and Dielectrics 539
C = 𝜅C0. In other words, the capacitance with the dielectric present is increased by a factor of 𝜅 over the capacitance without the dielectric. It can be shown that the relation C = 𝜅C0 applies to any capacitor, not just to a parallel plate capacitor. One reason, then, that capacitors are fi lled with
dielectric materials is to increase the capacitance.
CONCEPTUAL EXAMPLE 10 The Eff ect of a Dielectric When a Capacitor Has a Constant Charge
An empty capacitor is connected to a battery and charged up. The capaci-
tor is then disconnected from the battery, and a slab of dielectric material
is inserted between the plates. Does the potential diff erence across the
plates (a) increase, (b) remain the same, or (c) decrease?
Reasoning Our reasoning is guided by the following fact: Once the capacitor is disconnected from the battery, the charge on its plates remains
constant, for there is no longer any way for charge to be added or removed.
According to Equation 19.8, the magnitude q of the charge stored by the capacitor is q = CV, where C is its capacitance and V is the magnitude of the potential diff erence between the plates.
Answers (a) and (b) are incorrect. Placing a dielectric between the plates of a capacitor reduces the electric fi eld in that region (see Interactive
Figure 19.18c). The magnitude V of the potential diff erence is related to the magnitude E of the electric fi eld by V = Ed, where d is the distance between the capacitor plates. Since E decreases when the dielectric is inserted and d is unchanged, the potential diff erence does not increase or remain the same.
Answer (c) is correct. Inserting the dielectric causes the capacitance C to increase. Since q = CV and q is fi xed, the potential diff erence V across the plates must decrease in order for q to remain unchanged. The amount by which the potential diff erence decreases from the value
initially established by the battery depends on the dielectric constant of
the slab.
Related Homework: Problem 53
Capacitors are used often in electronic devices, and Example 11 deals with one familiar
application.
EXAMPLE 11 The Physics of a Computer Keyboard
One kind of computer keyboard is based on the idea of capacitance. Each
key is mounted on one end of a plunger, and the other end is attached to
a movable metal plate (see Figure 19.19). The movable plate is separated from a fi xed plate, the two plates forming a capacitor. When the key is
pressed, the movable plate is pushed closer to the fi xed plate, and the ca-
pacitance increases. Electronic circuitry enables the computer to detect the
change in capacitance, thereby recognizing which key has been pressed. The separation of the plates is normally 5.00 × 10−3 m but decreases to
0.150 × 10−3 m when a key is pressed. The plate area is 9.50 × 10−5 m2,
and the capacitor is fi lled with a material whose dielectric constant is 3.50.
Determine the change in capacitance that is detected by the computer.
Reasoning We can use Equation 19.10 directly to fi nd the capacitance of the key, since the dielectric constant 𝜅, the plate area A, and the plate separation d are known. We will use this relation twice, once to fi nd the capacitance when the key is pressed and once when it is not pressed. The
change in capacitance will be the diff erence between these two values.
Solution When the key is pressed, the capacitance is
C = κε0 A
d =
(3.50)[8.85 × 10−12 C2/(N · m2)](9.50 × 10−5 m2) 0.150 × 10−3 m
= 19.6 × 10−12 F (19.6 pF) (19.10)
A calculation similar to the one above reveals that when the key is not pressed, the capacitance has a value of 0.589 × 10−12 F (0.589 pF).
The change in capacitance is an increase of 19.0 × 10−12 F (19.0 pF ) . The change in the capacitance is greater with the dielectric present, which makes it easier for the circuitry within the computer to detect it.
`
esc
1 2 3 4 5
F1 F2 F3 F4 F5 F6
6 7 ~ ! @ # $ % ^ &
Q
control option
alt
W E R T Y U
A S D F G H J
Zshift X C V B N
tab
caps lock
option
alt
Key
Plunger
Dielectric Fixed metal plate
Movable metal plate
FIGURE 19.19 In one kind of computer keyboard, each key, when pressed, changes the
separation between the plates of a capacitor.
540 CHAPTER 19 Electric Potential Energy and the Electric Potential
Energy Storage in a Capacitor When a capacitor stores charge, it also stores energy. In charging up a capacitor, for example, a
battery does work in transferring an increment of charge from one plate of the capacitor to the
other plate. The work done is equal to the product of the charge increment and the potential diff er-
ence between the plates. However, as each increment of charge is moved, the potential diff erence
increases slightly, and a larger amount of work is needed to move the next increment. The total
work W done in completely charging the capacitor is the product of the total charge q transferred and the average potential diff erence V; W = qV. Since the average potential diff erence is one-half the fi nal potential V, or V = 12V, the total work done by the battery is W =
1
2 qV. This work does not disappear but is stored as electric potential energy in the capacitor, so that Energy =
1
2 qV. Equation 19.8 indicates that q = CV or, equivalently, that V = q/C. We can see, then, that our expression for the energy can be cast into two additional equivalent forms by substituting for q or for V. Equations 19.11a–c summarize these results:
Energy = 1
2 qV (19.11a)
Energy = 1
2 (CV )V = 1
2 CV 2 (19.11b)
Energy = 1
2 q ( q C) =
q 2
2C (19.11c)
It is also possible to regard the energy as being stored in the electric fi eld between the plates.
The relation between energy and fi eld strength can be obtained for a parallel plate capacitor by
substituting V = Ed (Equation 19.7b) and C = 𝜅𝜺0A/d (Equation 19.10) into Equation 19.11b:
Energy = 1
2 CV 2 = 1
2 ( κε0 A
d )(Ed )2 Since the area A times the separation d is the volume between the plates, the energy per unit volume or energy density is
Energy density = Energy
Volume =
1
2 κε0 E 2 (19.12)
It can be shown that this expression is valid for any electric fi eld strength, not just that between
the plates of a capacitor.
THE PHYSICS OF . . . an electronic fl ash attachment for a camera. The energy-storing capability of a capacitor is often put to good use in electronic circuits. For example, in an electronic
fl ash attachment for a camera, energy from the battery pack is stored in a capacitor. The capacitor is
then discharged between the electrodes of the fl ash tube, which converts the energy into light. Flash
duration times range from 1/200 to 1/1 000 000 second or less, with the shortest fl ashes being used
in high-speed photography (see Figure 19.20). Some fl ash attachments automatically control the fl ash duration by monitoring the light refl ected from the photographic subject and quickly stopping
or quenching the capacitor discharge when the refl ected light reaches a predetermined level.
BIO THE PHYSICS OF . . . a defi brillator. During a heart attack, the heart produces a rapid, unregulated pattern of beats, a condition known as cardiac fi brillation. Cardiac fi brilla-
tion can often be stopped by sending a very fast discharge of electrical energy through the heart.
For this purpose, emergency medical personnel use defi brillators, such as the one being used in
Figure 19.21. A paddle is connected to each plate of a large capacitor, and the paddles are placed on the chest near the heart. The capacitor is charged to a potential diff erence of about a thousand
volts. The capacitor is then discharged in a few thousandths of a second; the discharge current
passes through a paddle, the heart, and the other paddle. Within a few seconds, the heart often
returns to its normal beating pattern.
Check Your Understanding
(The answers are given at the end of the book.) 17. An empty parallel plate capacitor is connected to a battery that maintains a constant potential diff erence
between the plates. With the battery connected, a dielectric is then inserted between the plates. Do the
following quantities decrease, remain the same, or increase when the dielectric is inserted? (a) The
FIGURE 19.20 This time-lapse photo of a fi gure skater was obtained using a camera
with an electronic fl ash attachment. The
energy for each fl ash of light comes from the
electrical energy stored in a capacitor.
Robert Decelis Ltd/Image Bank/Getty Images
Adam Davis/Science Source
FIGURE 19.21 A paramedic is using a portable defi brillator in an attempt to revive
a heart attack victim. A defi brillator uses
the electrical energy stored in a capacitor to
deliver a controlled electric current that can
restore normal heart rhythm.
19.6 Biomedical Applications of Electric Potential Diff erences 541
electric fi eld between the plates (b) The capacitance (c) The charge on the plates (d) The energy stored by the capacitor
18. A parallel plate capacitor is charged up by a battery. The battery is then disconnected, but the charge remains on the plates. The plates are then pulled apart. Do the following quantities decrease, remain
the same, or increase as the distance between the plates increases? (a) The capacitance of the capacitor (b) The potential diff erence between the plates (c) The electric fi eld between the plates (d) The electric potential energy stored by the capacitor
19.6 *Biomedical Applications of Electric Potential Diff erences
Conduction of Electrical Signals in Neurons The human nervous system is remarkable for its ability to transmit information in the form of
electrical signals. These signals are carried by the nerves, and the concept of electric potential
diff erence plays an important role in the process. For example, sensory information from our eyes
and ears is carried to the brain by the optic nerves and auditory nerves, respectively. Other nerves
transmit signals from the brain or spinal column to muscles, causing them to contract. Still other
nerves carry signals within the brain.
A nerve consists of a bundle of axons, and each axon is one part of a nerve cell, or neuron. As Interactive Figure 19.22 illustrates, a typical neuron consists of a cell body with numerous exten- sions, called dendrites, and a single axon. The dendrites convert stimuli, such as pressure or heat, into electrical signals that travel through the neuron. The axon sends the signal to the nerve end-
ings, which transmit the signal across a gap (called a synapse) to the next neuron or to a muscle. The fl uid inside a cell, the intracellular fl uid, is quite diff erent from that outside the cell, the
extracellular fl uid. Both fl uids contain concentrations of positive and negative ions. However, the
extracellular fl uid is rich in sodium (Na+) and chlorine (Cl−) ions, whereas the intracellular fl uid
is rich in potassium (K+) ions and negatively charged proteins. These concentration diff erences
between the fl uids are extremely important to the life of the cell. If the cell membrane were freely
permeable, the ions would diff use across it until the concentrations on both sides were equal. (See
Section 14.4 for a review of diff usion.) This does not happen, because a living cell has a selec-
tively permeable membrane. Ions can enter or leave the cell only through membrane channels,
and the permeability of the channels varies markedly from one ion to another. For example, it is
much easier for K+ ions to diff use out of the cell than it is for Na+ to enter the cell. As a result of
selective membrane permeability, there is a small buildup of negative charges just on the inner
side of the membrane and an equal amount of positive charges on the outer side (see Figure 19.23). The buildup of charge occurs very close to the membrane, so the membrane acts like a capaci-
tor (see Problems 49 and 57). Elsewhere in the intracellular and extracellular fl uids, there are
equal numbers of positive and negative ions, so the fl uids are overall electrically neutral. Such a
separation of positive and negative charges gives rise to an electric potential diff erence across the
membrane, called the resting membrane potential. In neurons, the resting membrane potential
Dendrites
Cell body
Axon
Synapse
Another neuron or a muscle
Nerve endings
INTERACTIVE FIGURE 19.22 The anatomy of a typical neuron.
–
–
–
–
+
+
– – – –
–
– –
–
+ +
+ +
+
+
+ +
+
+
Positive charge layer
Extracellular fluid
(outside)
Intracellular fluid
(inside)
Cell membrane
Negative charge layer
FIGURE 19.23 Positive and negative charge layers form on the outside and
inside surfaces of a membrane during its
resting state.
542 CHAPTER 19 Electric Potential Energy and the Electric Potential
ranges from −40 to −90 mV, with a typical value of −70 mV. The minus sign indicates that the
inner side of the membrane is negative relative to the outer side.
BIO THE PHYSICS OF . . . an action potential. A “resting” neuron is one that is not conducting an electrical signal. The change in the resting membrane potential is the key factor in the initiation and conduction of a signal. When a suffi ciently strong stimulus is applied to a given point
on the neuron, “gates” in the membrane open and sodium ions fl ood into the cell, as Figure 19.24 illustrates. The sodium ions are driven into the cell by attraction to the negative ions on the inner
side of the membrane as well as by the relatively high concentration of sodium ions outside the
cell. The large infl ux of Na+ ions fi rst neutralizes the negative ions on the interior of the mem-
brane and then causes it to become positively charged. As a result, the membrane potential in this
localized region goes from −70 mV, the resting potential, to about +30 mV in a very short time
(see Figure 19.25). The sodium gates then close, and the cell membrane quickly returns to its normal resting potential. This change in potential, from −70 mV to +30 mV and back to −70 mV,
is known as the action potential. The action potential lasts for a few milliseconds, and it is the electrical signal that propagates down the axon, typically at a speed of about 50 m/s, to the next
neuron or to a muscle cell.
Medical Diagnostic Techniques Several important medical diagnostic techniques depend on the fact that the surface of the human
body is not an equipotential surface. Between various points on the body there are small potential diff erences (approximately 30–500 𝜇V), which provide the basis for electrocardiography, electro-
encephalography, and electroretinography. The potential diff erences can be traced to the electrical
characteristics of muscle cells and nerve cells. In carrying out their biological functions, these cells
utilize positively charged sodium and potassium ions and negatively charged chlorine ions that exist
within the cells and in the extracellular fl uid. As a result of such charged particles, electric fi elds are
generated that extend to the surface of the body and lead to the small potential diff erences.
BIO THE PHYSICS OF . . . electrocardiography. Figure 19.26 shows electrodes placed on the body to measure potential diff erences in electrocardiography. The potential
– – – –Intracellular fluid
(inside)
+
+
+
++
Na+
FIGURE 19.24 When a stimulus is applied to the cell, positive sodium ions (Na+) rush into the cell,
causing the interior surface of the membrane to
become momentarily positive.
Action potential
Na+ influx
0 1 2 3 4
+30
Time, ms
M em
br an
e po
te nt
ia l,
m V
0
–70
Membrane resting potential
FIGURE 19.25 The action potential is caused by the rush of positive sodium ions
into the cell and a subsequent return of the
cell to its resting potential.
Strip-chart recorder
Electrodes ED
C
A B EKG (Normal) EKG (Abnormal)
Time
Potential difference
Time
Potential difference
P P
Q
R
S TQ
R
S
T FIGURE 19.26 The potential diff erences
generated by heart muscle activity provide
the basis for electrocardiography. The normal
and abnormal EKG patterns correspond to
one heartbeat.
19.6 Biomedical Applications of Electric Potential Diff erences 543
diff erence between two locations changes as the heart beats and forms a repetitive pattern. The
recorded pattern of potential diff erence versus time is called an electrocardiogram (ECG or
EKG), and its shape depends on which pair of points in the picture (A and B, B and C, etc.) is used to locate the electrodes. The fi gure also shows some EKGs and indicates the regions (P, Q, R, S, and T) associated with specifi c parts of the heart’s beating cycle. The diff erences between the EKGs of normal and abnormal hearts provide physicians with a valuable diagnostic tool.
BIO THE PHYSICS OF . . . electroencephalography. In electroencephalography the electrodes are placed at specifi c locations on the head, as Figure 19.27 indicates, and they record the potential diff erences that characterize brain behavior. The graph of potential diff erence versus
time is known as an electroencephalogram (EEG). The various parts of the patterns in an EEG
are often referred to as “waves” or “rhythms.” The drawing shows an example of the main rest-
ing rhythm of the brain, the so-called alpha rhythm, and also illustrates the distinct diff erences
that are found between the EEGs generated by healthy (normal) and diseased (abnormal) tissue.
BIO THE PHYSICS OF . . . electroretinography. The electrical characteristics of the retina of the eye lead to the potential diff erences measured in electroretinography. Figure 19.28 shows a typical electrode placement used to record the pattern of potential diff erence versus time
that occurs when the eye is stimulated by a fl ash of light. One electrode is mounted on a contact
lens, while the other is often placed on the forehead. The recorded pattern is called an electroret-
inogram (ERG), and parts of the pattern are referred to as the “A wave” and the “B wave.” As the graphs show, the ERGs of normal and diseased (abnormal) eyes can diff er markedly.
Electrodes connected to detection and recording device
Time Time
Potential difference
Potential difference
EEG (Abnormal)EEG (Normal alpha rhythm)
FIGURE 19.27 In electroencephalography the potential diff erences created by the
electrical activity of the brain are used for
diagnosing abnormal behavior.
Electrodes connected to detection and recording device
Electronic flash Time Time
Potential difference
Potential difference
ERG (Normal) ERG (Abnormal) B
A
B
A FIGURE 19.28 The electrical activity of
the retina of the eye generates the potential
diff erences used in electroretinography.
EXAMPLE 12 BIO Energy Stored in a Defibrillator
A cardiac defi brillator, such as the one shown in Figure 19.21, stores energy in a large capacitor connected to its paddles. This energy is deliv-
ered to the heart by discharging the capacitor through the chest wall of the
patient. If the capacitor connected to the paddles has a value of 22.5 μF, and it is charged to a potential of 1250 V, what is (a) the energy delivered
by the capacitor, and (b) the charge on its plates?
Reasoning (a) To fi nd the energy stored in the capacitor, we can simply apply Equation 19.11b. (b) The defi nition of capacitance (Equation 19.8)
can be used to fi nd the charge on each plate.
Solution (a) Applying Equation 19.11b with the data given in the problem, we have Energy =
1
2CV 2 = 1
2 (22.5 × 10 −6 F)(1250 V)2 =
17.6 J (b) The charge on the capacitor is given by Q = CV = (22.5 × 10−6 F)(1250 V) = 0.028 C
544 CHAPTER 19 Electric Potential Energy and the Electric Potential
Concept Summary 19.1 Potential Energy When a positive test charge +q0 moves from point A to point B in the presence of an electric fi eld, work WAB is done by the elec- tric force. The work equals the electric potential energy (EPE) at A minus that at B, as given by Equation 19.1. The electric force is a conservative force, so the path along which the test charge moves from A to B is of no consequence, for the work WAB is the same for all paths.
WAB = EPEA − EPEB (19.1)
19.2 The Electric Potential Diff erence The electric potential V at a given point is the electric potential energy of a small test charge q0 situated at that point divided by the charge itself, as shown in Equation 19.3. The SI unit
of electric potential is the joule per coulomb (J/C), or volt (V). The electric
potential diff erence between two points A and B is given by Equation 19.4. The potential diff erence between two points (or between two equipotential
surfaces) is often called the “voltage.”
V = EPE
q0 (19.3)
VB − VA = EPEB
q 0 −
EPEA
q 0 =
−WAB q 0
(19.4)
A positive charge accelerates from a region of higher potential toward a
region of lower potential. Conversely, a negative charge accelerates from a
region of lower potential toward a region of higher potential.
An electron volt (eV) is a unit of energy. The relationship between elec-
tron volts and joules is 1 eV = 1.60 × 10−19 J.
The total energy E of a system is the sum of its translational (12 mυ2 ) and rotational (
1
2 Iω 2 ) kinetic energies, gravitational potential energy (mgh), elas- tic potential energy (
1
2 kx2), and electric potential energy (EPE), as indicated by Equation 1. If external nonconservative forces like friction do no net work,
the total energy of the system is conserved. That is, the fi nal total energy Ef is equal to the initial total energy E0; Ef = E0.
E = 12 mυ 2 + 1
2 Iω 2 + mgh + 1
2 kx 2 + EPE (1)
19.3 The Electric Potential Diff erence Created by Point Charges The electric potential V at a distance r from a point charge q is given by Equation 19.6, where k = 8.99 × 109 N · m2/C2. This expression for V assumes that the electric potential is zero at an infi nite distance away from the charge. The
total electric potential at a given location due to two or more charges is the
algebraic sum of the potentials due to each charge.
V = kq r
(19.6)
The total potential energy of a group of charges is the amount by which
the electric potential energy of the group diff ers from its initial value when
the charges are infi nitely far apart and far away. It is also equal to the work
required to assemble the group, one charge at a time, starting with the charges
infi nitely far apart and far away.
19.4 Equipotential Surfaces and Their Relation to the Electric Field An equipotential surface is a surface on which the electric potential is the
same everywhere. The electric force does no work as a charge moves on an
equipotential surface, because the force is always perpendicular to the dis-
placement of the charge.
The electric fi eld created by any group of charges is everywhere perpen-
dicular to the associated equipotential surfaces and points in the direction of
decreasing potential. The electric fi eld is related to two equipotential surfaces
by Equation 19.7a, where ΔV is the potential diff erence between the surfaces and Δs is the displacement. The term ΔV/Δs is called the potential gradient.
E = − ∆V ∆s
(19.7a)
19.5 Capacitors and Dielectrics A capacitor is a device that stores charge and energy. It consists of two conductors or plates that are near one
another, but not touching. The magnitude q of the charge on each plate is given by Equation 19.8, where V is the magnitude of the potential diff erence between the plates and C is the capacitance. The SI unit for capacitance is the coulomb per volt (C/V), or farad (F).
q = CV (19.8)
The insulating material included between the plates of a capacitor is
called a dielectric. The dielectric constant 𝜅 of the material is defi ned as shown in Equation 19.9, where E0 and E are, respectively, the magnitudes of the electric fi elds between the plates without and with a dielectric, assuming
the charge on the plates is kept fi xed.
κ = E0 E
(19.9)
The capacitance of a parallel plate capacitor fi lled with a dielectric is given
by Equation 19.10, where ε0 = 8.85 × 10−12 C2/(N · m 2 ) is the permittivity of free space, A is the area of each plate, and d is the distance between the plates.
C = κε0 A
d (19.10)
The electric potential energy stored in a capacitor is given by Equations
19.11a–c. The energy density is the energy stored per unit volume and is re-
lated to the magnitude E of the electric fi eld, as indicated in Equation 19.12.
Energy = 1
2qV = 1
2 CV 2 = q2/ (2C ) (19.11a–c)
Energy density = 1
2κε0E2 (19.12)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 19.2 The Electric Potential Diff erence 2. Two diff erent charges, q1 and q2, are placed at two diff erent locations, one charge at each location. The locations have the same electric potential V.
Do the charges have the same electric potential energy? (a) Yes. If the elec- tric potentials at the two locations are the same, the electric potential en-
ergies are also the same, regardless of the type (+ or −) and magnitude
of the charges placed at these locations. (b) Yes, because electric potential and electric potential energy are just diff erent names for the same concept.
(c) No, because the electric potential V at a given location depends on the charge placed at that location, whereas the electric potential energy EPE
does not. (d) No, because the electric potential energy EPE at a given
Focus on Concepts
Focus on Concepts 545
location depends on the charge placed at that location as well as the electric
potential V. 4. A proton is released from rest at point A in a constant electric fi eld and accelerates to point B (see part a of the drawing). An electron is released from rest at point B and accelerates to point A (see part b of the drawing). How does the change in the proton’s electric potential energy compare with
the change in the electron’s electric potential energy? (a) The change in the proton’s electric potential energy is the same as the change in the electron’s
electric potential energy. (b) The proton experiences a greater change in elec- tric potential energy, since it has a greater charge magnitude. (c) The proton experiences a smaller change in electric potential energy, since it has a smal-
ler charge magnitude. (d) The proton experiences a smaller change in electric potential energy, since it has a smaller speed at B than the electron has at A. This is due to the larger mass of the proton. (e) One cannot compare the change in electric potential energies because the proton and electron move in
opposite directions.
+
Proton
E
A B
(a) E
E
−
Electron
B
(b) E
A
QUESTION 4
Section 19.3 The Electric Potential Diff erence Created by Point Charges 6. The drawing shows three arrangements of charged particles, all the same distance from the origin. Rank the arrangements, largest to smallest, accord-
ing to the total electric potential V at the origin. (a) A, B, C (b) B, A, C (c) B, C, A (d) A, B and C (a tie) (e) A and C (a tie), B
A
−2q +6q
B
+4q
−2q +7q
−5q
C
+5q −3q
QUESTION 6
9. Four pairs of charged particles with identical separations are shown in the drawing. Rank the pairs according to their electric potential energy EPE,
greatest (most positive) fi rst.
(a) A and C (a tie), B and D (a tie) (b) A, B, C, D (c) C, B, D, A (d) B, A, C and D (a tie) (e) A and B (a tie), C, D
A
+4q +3q
B
−2q +6q
C
−12q −q
D
−4q +3q
QUESTION 9
Section 19.4 Equipotential Surfaces and Their Relation to the Electric Field 11. The drawing shows edge-on views of three parallel plate capacitors with the same separation between the plates. The potential of each plate is indic-
ated above it. Rank the capacitors as to the magnitude of the electric fi eld inside them, largest to smallest.
(a) A, B, C (b) A, C, B (c) C, B, A (d) C, A, B (e) B, C, A
A
+50 V +250 V
B
−100 V +150 V
C
−250 V +50 V
QUESTION 11
12. The drawing shows a plot of the electric potential V versus the displace- ment s. The plot consists of four segments. Rank the magnitude of the electric fi elds for the four segments, largest to smallest.
(a) D, C, B, A (b) A and C (a tie), B and D (a tie) (c) A, B, D, C (d) B, D, C, A (e) D, B, A and C (a tie)
A
B C
D
E le
ct ri
c po
te nt
ia l,
V
Displacement, s
QUESTION 12
Section 19.5 Capacitors and Dielectrics 17. Which two or more of the following actions would increase the energy stored in a parallel plate capacitor when a constant potential diff erence is
applied across the plates?
1. Increasing the area of the plates
2. Decreasing the area of the plates
3. Increasing the separation between the plates
4. Decreasing the separation between the plates
5. Inserting a dielectric between the plates
(a) 2, 4 (b) 2, 3, 5 (c) 1, 4, 5 (d) 1, 3
546 CHAPTER 19 Electric Potential Energy and the Electric Potential
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 19.1 Potential Energy
Section 19.2 The Electric Potential Diff erence 1. E During a particular thunderstorm, the electric potential diff erence between a cloud and the ground is Vcloud − Vground = 1.3 × 108 V, with the cloud being at the higher potential. What is the change in an electron’s
electric potential energy when the electron moves from the ground to the
cloud?
2. E A particle with a charge of −1.5 𝜇C and a mass of 2.5 × 10−6 kg is re- leased from rest at point A and accelerates toward point B, arriving there with
a speed of 42 m/s. The only force acting on the particle is the electric force.
(a) Which point is at the higher potential? Give your reasoning. (b) What is the potential diff erence VB − VA between A and B? 3. E BIO SSM Suppose that the electric potential outside a living cell is higher than that inside the cell by 0.070 V. How much work is done by the
electric force when a sodium ion (charge = +e) moves from the outside to the inside?
4. E GO A particle has a charge of +1.5 𝜇C and moves from point A to point B, a distance of 0.20 m. The particle experiences a constant electric force, and its motion is along the line of action of the force. The diff erence
between the particle’s electric potential energy at A and at B is EPEA − EPEB = +9.0 × 10−4 J. (a) Find the magnitude and direction of the electric force that acts on the particle. (b) Find the magnitude and direction of the electric fi eld that the particle experiences.
5. E MMH Available in WileyPLUS. 6. E GO Review Multiple-Concept Example 4 to see the concepts that are pertinent here. In a television picture tube, electrons strike the screen
after being accelerated from rest through a potential diff erence of 25 000 V.
The speeds of the electrons are quite large, and for accurate calculations
of the speeds, the eff ects of special relativity must be taken into account.
Ignoring such eff ects, fi nd the electron speed just before the electron strikes
the screen.
7. E SSM Multiple-Concept Example 4 deals with the concepts that are im- portant in this problem. As illustrated in Figure 19.5b, a negatively charged particle is released from rest at point B and accelerates until it reaches point A. The mass and charge of the particle are 4.0 × 10−6 kg and −2.0 × 10−5 C,
respectively. Only the gravitational force and the electrostatic force act on
the particle, which moves on a horizontal straight line without rotating. The
electric potential at A is 36 V greater than that at B; in other words, VA − VB = 36 V. What is the translational speed of the particle at point A? 8. E GO An electron and a proton, starting from rest, are accelerated through an electric potential diff erence of the same magnitude. In the pro-
cess, the electron acquires a speed 𝜐e, while the proton acquires a speed 𝜐p. Find the ratio 𝜐e/𝜐p. 9. M SSM Available in WileyPLUS.
10. M V-HINT A moving particle encounters an external electric fi eld that decreases its kinetic energy from 9520 eV to 7060 eV as the particle moves
from position A to position B. The electric potential at A is −55.0 V, and the electric potential at B is +27.0 V. Determine the charge of the particle. Include the algebraic sign (+ or −) with your answer.
11. M GO During a lightning fl ash, there exists a potential diff erence of Vcloud − Vground = 1.2 × 109 V between a cloud and the ground. As a result, a charge of −25 C is transferred from the ground to the cloud. (a) How much work Wground–cloud is done on the charge by the electric force? (b) If the work done by the electric force were used to accelerate a 1100-kg automobile from
rest, what would be its fi nal speed? (c) If the work done by the electric force were converted into heat, how many kilograms of water at 0 °C could be
heated to 100 °C?
12. H Available in WileyPLUS.
Section 19.3 The Electric Potential Diff erence Created by Point Charges 13. E Two point charges, +3.40 𝜇C and −6.10 𝜇C, are separated by 1.20 m. What is the electric potential midway between them?
14. E An electron and a proton are initially very far apart (eff ectively an infi nite distance apart). They are then brought together to form a hydrogen
atom, in which the electron orbits the proton at an average distance of 5.29 ×
10−11 m. What is EPEfi nal − EPEinitial, which is the change in the electric
potential energy?
15. E SSM Two charges A and B are fi xed in place, at diff erent distances from a certain spot. At this spot the potentials due to the two charges are
equal. Charge A is 0.18 m from the spot, while charge B is 0.43 m from it.
Find the ratio qB/qA of the charges. 16. E GO The drawing shows a square, each side of which has a length of L = 0.25 m. On two corners of the square are fi xed diff erent positive charges, q1 and q2. Find the electric potential energy of a third charge q3 = −6.0 × 10−9 C placed at corner A and then at corner B.
PROBLEM 16 q1 = +1.5 × 10 –9 C q2 = +4.0 × 10
–9 C
B A
17. E SSM The drawing shows four point charges. The value of q is 2.0 𝜇C, and the distance d is 0.96 m. Find the total potential at the location P. Assume that the potential of a point charge is zero at infi nity.
PROBLEM 17
q
q
d
d
d
d
−q
−q
P
Problems
Problems 547
18. E A charge of +125 𝜇C is fi xed at the center of a square that is 0.64 m on a side. How much work is done by the electric force as a charge of
+7.0 𝜇C is moved from one corner of the square to any other empty corner?
Explain.
19. E CHALK The drawing shows six point charges arranged in a rectangle. The value of q is 9.0 𝜇C, and the distance d is 0.13 m. Find the total electric potential at location P, which is at the center of the rectangle.
PROBLEM 19 −5q −3q +7q
+7q +3q +5q
d d
d
d d
d
P
20. E Location A is 3.00 m to the right of a point charge q. Location B lies on the same line and is 4.00 m to the right of the charge. The potential diff er-
ence between the two locations is VB − VA = 45.0 V. What are the magnitude and sign of the charge?
21. E Identical +1.8 𝜇C charges are fi xed to adjacent corners of a square. What charge (magnitude and algebraic sign) should be fi xed to one of the
empty corners, so that the total electric potential at the remaining empty
corner is 0 V?
22. E GO Charges of −q and +2q are fi xed in place, with a distance of 2.00 m between them. A dashed line is drawn through the negative charge,
perpendicular to the line between the charges. On the dashed line, at a dis-
tance L from the negative charge, there is at least one spot where the total potential is zero. Find L. 23. M CHALK SSM Determine the electric potential energy for the array of three charges in the drawing, relative to its value when the charges are
infi nitely far away and infi nitely far apart.
PROBLEM 23
+8.00 Cμ
+20.0 Cμ−15.0 Cμ
4.00 m
3.00 m
90.0°
24. M V-HINT Two identical point charges (q = +7.20 × 10−6 C) are fi xed at diagonally opposite corners of a square with sides of length 0.480 m. A test
charge (q0 = −2.40 × 10−8 C), with a mass of 6.60 × 10−8 kg, is released from rest at one of the empty corners of the square. Determine the speed of the test
charge when it reaches the center of the square.
25. M MMH Two protons are moving directly toward one another. When they are very far apart, their initial speeds are 3.00 × 106 m/s. What is the
distance of closest approach?
26. M V-HINT Four identical charges (+2.0 𝜇C each) are brought from infi n- ity and fi xed to a straight line. The charges are located 0.40 m apart. Determ-
ine the electric potential energy of this group.
27. M SSM A charge of −3.00 𝜇C is fi xed in place. From a horizontal dis- tance of 0.0450 m, a particle of mass 7.20 × 10−3 kg and charge −8.00 𝜇C is
fi red with an initial speed of 65.0 m/s directly toward the fi xed charge. How
far does the particle travel before its speed is zero?
28. M GO Identical point charges of +1.7 𝜇C are fi xed to diagonally op- posite corners of a square. A third charge is then fi xed at the center of the
square, such that it causes the potentials at the empty corners to change
signs without changing magnitudes. Find the sign and magnitude of the
third charge.
29. H One particle has a mass of 3.00 × 10−3 kg and a charge of +8.00 𝜇C. A second particle has a mass of 6.00 × 10−3 kg and the same charge. The
two particles are initially held in place and then released. The particles
fl y apart, and when the separation between them is 0.100 m, the speed of
the 3.00 × 10−3 kg particle is 125 m/s. Find the initial separation between
the particles.
30. H Available in WileyPLUS.
Section 19.4 Equipotential Surfaces and Their Relation to the Electric Field 31. E Two equipotential surfaces surround a +1.50 × 10−8 C point charge. How far is the 190-V surface from the 75.0-V surface?
32. E An equipotential surface that surrounds a point charge q has a poten- tial of 490 V and an area of 1.1 m2. Determine q. 33. E BIO SSM The inner and outer surfaces of a cell membrane carry a negative and a positive charge, respectively. Because of these charges, a po-
tential diff erence of about 0.070 V exists across the membrane. The thickness
of the cell membrane is 8.0 × 10−9 m. What is the magnitude of the electric
fi eld in the membrane?
34. E GO A positive point charge (q = +7.2 × 10−8 C) is surrounded by an equipotential surface A, which has a radius of rA = 1.8 m. A positive test charge (q0 = +4.5 × 10−11 C) moves from surface A to another equipotential surface B, which has a radius rB. The work done as the test charge moves from surface A to surface B is WAB = −8.1 × 10−9 J. Find rB. 35. E SSM A spark plug in an automobile engine consists of two metal conductors that are separated by a distance of 0.75 mm. When an electric
spark jumps between them, the magnitude of the electric fi eld is 4.7 ×
107 V/m. What is the magnitude of the potential diff erence ΔV between the conductors?
36. E The drawing that accompanies Problem 60 shows a graph of a set of equipotential surfaces in cross section. The grid lines are 2.0 cm apart.
Determine the magnitude and direction of the electric fi eld at position D. Specify whether the electric fi eld points toward the top or the bottom of the
drawing.
37. M SSM MMH An electric fi eld has a constant value of 4.0 × 103 V/m and is directed downward. The fi eld is the same everywhere. The potential
at a point P within this region is 155 V. Find the potential at the following points: (a) 6.0 × 10−3 m directly above P, (b) 3.0 × 10−3 m directly below P, (c) 8.0 × 10−3 m directly to the right of P. 38. M CHALK GO An electron is released from rest at the negative plate of a parallel plate capacitor and accelerates to the positive plate (see the drawing).
The plates are separated by a distance of 1.2 cm, and the electric fi eld within
the capacitor has a magnitude of 2.1 × 106 V/m. What is the kinetic energy of
the electron just as it reaches the positive plate?
PROBLEM 38
+ + + + + + + + + +
−
Electric field
Electron
F
− − − − − − − − − −
39. M V-HINT The drawing shows the electric potential as a function of dis- tance along the x axis. Determine the magnitude of the electric fi eld in the region (a) A to B, (b) B to C, and (c) C to D.
548 CHAPTER 19 Electric Potential Energy and the Electric Potential
PROBLEM 39
A B
C
D
0
5.0
4.0
3.0
2.0
1.0
0 0.20
P ot
en ti
al ,
V
0.40
x, m
0.60 0.80
40. M GO At a distance of 1.60 m from a point charge of +2.00 𝜇C, there is an equipotential surface. At greater distances there are additional equipoten-
tial surfaces. The potential diff erence between any two successive surfaces is
1.00 × 103 V. Starting at a distance of 1.60 m and moving radially outward,
how many of the additional equipotential surfaces are crossed by the time the
electric fi eld has shrunk to one-half of its initial value? Do not include the
starting surface.
41. M V-HINT The drawing shows a uniform electric fi eld that points in the negative y direction; the magnitude of the fi eld is 3600 N/C. Determine the electric potential diff erence (a) VB − VA between points A and B, (b) VC − VB between points B and C, and (c) VA − VC between points C and A.
PROBLEM 41
8.0 cm 10.0 cm
6.0 cm A
E E
B
C
+y
+x
Section 19.5 Capacitors and Dielectrics 42. E What is the capacitance of a capacitor that stores 4.3 𝜇C of charge on its plates when a voltage of 1.5 V is applied between them?
43. E BIO SSM The electric potential energy stored in the capacitor of a defi brillator is 73 J, and the capacitance is 120 𝜇F. What is the potential dif-
ference that exists across the capacitor plates?
44. E Two identical capacitors store diff erent amounts of energy: capacitor A stores 3.1 × 10−3 J, and capacitor B stores 3.4 × 10−4 J. The voltage across the
plates of capacitor B is 12 V. Find the voltage across the plates of capacitor A.
45. E MMH The electronic fl ash attachment for a camera contains a ca- pacitor for storing the energy used to produce the fl ash. In one such unit,
the potential diff erence between the plates of an 850-𝜇F capacitor is 280 V.
(a) Determine the energy that is used to produce the fl ash in this unit. (b) Assuming that the fl ash lasts for 3.9 × 10−3 s, fi nd the eff ective power or “wattage” of the fl ash.
46. E GO The same voltage is applied between the plates of two diff erent capacitors. When used with capacitor A, this voltage causes the capacitor to
store 11 𝜇C of charge and 5.0 × 10−5 J of energy. When used with capacitor B,
which has a capacitance of 6.7 𝜇F, this voltage causes the capacitor to store a
charge that has a magnitude of qB. Determine qB. 47. E SSM A parallel plate capacitor has a capacitance of 7.0 𝜇F when fi lled with a dielectric. The area of each plate is 1.5 m2 and the separation
between the plates is 1.0 × 10−5 m. What is the dielectric constant of the
dielectric?
48. E GO Two capacitors are identical, except that one is empty and the other is fi lled with a dielectric (𝜅 = 4.50). The empty capacitor is connected to a 12.0-V battery. What must be the potential diff erence across the plates
of the capacitor fi lled with a dielectric so that it stores the same amount of
electrical energy as the empty capacitor?
49. E BIO The membrane that surrounds a certain type of living cell has a surface area of 5.0 × 10−9 m2 and a thickness of 1.0 × 10−8 m. Assume that the
membrane behaves like a parallel plate capacitor and has a dielectric constant
of 5.0. (a) The potential on the outer surface of the membrane is +60.0 mV greater than that on the inside surface. How much charge resides on the outer
surface? (b) If the charge in part (a) is due to positive ions (charge +e), how many such ions are present on the outer surface?
50. M GO Capacitor A and capacitor B both have the same voltage across their plates. However, the energy of capacitor A can melt m kilograms of ice at 0 °C, while the energy of capacitor B can boil away the same amount of
water at 100 °C. The capacitance of capacitor A is 9.3 𝜇F. What is the capa-
citance of capacitor B?
51. M SSM MMH What is the potential diff erence between the plates of a 3.3-F capacitor that stores suffi cient energy to operate a 75-W light bulb for
one minute?
52. M V-HINT Available in WileyPLUS. 53. M Review Conceptual Example 10 before attempting this problem. An empty capacitor is connected to a 12.0-V battery and charged up. The capa-
citor is then disconnected from the battery, and a slab of dielectric material
(𝜅 = 2.8) is inserted between the plates. Find the amount by which the po- tential diff erence across the plates changes. Specify whether the change is an
increase or a decrease.
54. M V-HINT An empty parallel plate capacitor is connected between the terminals of a 9.0-V battery and charged up. The capacitor is then disconnec-
ted from the battery, and the spacing between the capacitor plates is doubled.
As a result of this change, what is the new voltage between the plates of the
capacitor?
55. H SSM Available in WileyPLUS. 56. H Available in WileyPLUS.
57. E BIO SSM An axon is the relatively long tail-like part of a neuron, or nerve cell. The outer surface of the axon membrane (dielectric constant = 5,
thickness = 1 × 10−8 m) is charged positively, and the inner portion is charged
negatively. Thus, the membrane is a kind of capacitor. Assuming that the
membrane acts like a parallel plate capacitor with a plate area of 5 × 10−6 m2,
what is its capacitance?
Additional Problems
Concepts and Calculations Problems 549
58. E GO Refer to Multiple-Concept Example 3 to review the concepts that are needed here. A cordless electric shaver uses energy at a rate of
4.0 W from a rechargeable 1.5-V battery. Each of the charged particles that
the battery delivers to the shaver carries a charge that has a magnitude of 1.6 ×
10−19 C. A fully charged battery allows the shaver to be used for its maximum
operation time, during which 3.0 × 1022 of the charged particles pass between
the terminals of the battery as the shaver operates. What is the shaver’s
maximum operation time?
59. E Available in WileyPLUS. 60. E V-HINT The drawing shows a graph of a set of equipotential surfaces seen in cross section. Each is labeled according to its electric potential. A
+2.8 × 10−7 C point charge is placed at position A. Find the work that is done on the point charge by the electric force when it is moved (a) from A to B, and (b) from A to C.
PROBLEM 60
A
B
C
D+150.0 V
+250.0 V
+350.0 V
+650.0 V
+550.0 V
+450.0 V
2.0 cm
61. E SSM The work done by an electric force in moving a charge from point A to point B is 2.70 × 10−3 J. The electric potential diff erence between the two points is VA − VB = 50.0 V. What is the charge?
62. E GO Two capacitors have the same plate separation, but one has square plates and the other has circular plates. The square plates are a length L on each side, and the diameter of the circular plate is L. The capacitors have the same capacitance because they contain diff erent dielectric materials. The dielectric
constant of the material between the square plates has a value of 𝜅square = 3.00. What is the dielectric constant 𝜅circle of the material between the circular plates? 63. E Three point charges, −5.8 × 10−9 C, −9.0 × 10−9 C, and +7.3 × 10−9 C, are fi xed at diff erent positions on a circle. The total electric potential
at the center of the circle is −2100 V. What is the radius of the circle?
64. M GO Equipotential surface A has a potential of 5650 V, while equipo- tential surface B has a potential of 7850 V. A particle has a mass of 5.00 × 10−2 kg and a charge of +4.00 × 10−5 C. The particle has a speed of 2.00 m/s
on surface A. A nonconservative outside force is applied to the particle, and it moves to surface B, arriving there with a speed of 3.00 m/s. How much work is done by the outside force in moving the particle from A to B? 65. M MMH Available in WileyPLUS. 66. H Available in WileyPLUS. 67. H SSM Available in WileyPLUS. 68. H Available in WileyPLUS. 69. M GO SSM The capacitance of an empty capacitor is 1.2 𝜇F. The capacitor is connected to a 12-V battery and charged up. With the capacitor
connected to the battery, a slab of dielectric material is inserted between the
plates. As a result, 2.6 × 10−5 C of additional charge fl ows from one plate, through the battery, and onto the other plate. What is the dielectric constant
of the material?
The conservation of energy (Chapter 6) and the conservation of linear mo-
mentum (Chapter 7) are two of the most broadly applicable principles in all
of science. In this chapter, we have seen that electrically charged particles
obey the conservation-of-energy principle, provided that the electric poten-
tial is taken into account. The behavior of electrically charged particles, how-
ever, must also be consistent with the conservation-of-momentum principle,
as Problem 70 emphasizes. Chapter 18 introduces the electric fi eld, and the
present chapter introduces the electric potential. These two concepts are cent-
ral to the study of electricity, and it is important to distinguish between them,
as Problem 71 illustrates.
70. M CHALK Particle 1 has a mass of m1 = 3.6 × 10−6 kg, while particle 2 has a mass of m2 = 6.2 × 10−6 kg. Each has the same electric charge. These particles are initially held at rest, and the two-particle system has an initial
electric potential energy of 0.150 J. Suddenly, the particles are released and
fl y apart because of the repulsive electric force that acts on each one (see
the fi gure). The eff ects of the gravitational force are negligible, and no other
forces act on the particles. Concepts: (i) What types of energy does the two- particle system have initially? (ii) What types of energy does the two-particle
system have at the instant illustrated in part b of the drawing? (iii) Does the principle of conservation of energy apply to this problem? Explain. (iv) Does
the conservation of linear momentum apply to the two particles as they fl y
apart? Explain. Calculations: At one instant following the release, the speed of particle 1 is measured to be 𝜐1 = 170 m/s. What is the electric potential energy at this instant?
71. M CHALK SSM Two identical point charges (+2.4 × 10−9 C) are fi xed in place, separated by 0.50 m (see the fi gure). Concepts: (i) The electric fi eld is a vector and has a direction. At the midpoint, what are the directions of the
individual electric-fi eld contributions from qA and qB? (ii) Is the magnitude of the net electric fi eld at the midpoint greater than, less than, or equal to
zero? (iii) Is the total electric potential at the midpoint positive, negative,
or zero? (iv) Does the electric potential have a direction associated with it?
Explain. Calculations: Find the electric fi eld and the electric potential at the midpoint of the line between the charges qA and qB..
Concepts and Calculations Problems
q
m1
q
m2
q
m1
q
m2
1f 2f
(b) Final
(a) Initial (at rest)
υ υ
(a) Two particles have diff erent masses, but the
same electrical charge q. They are initially at rest.
(b) At the instant following the release of the particles,
they are fl ying apart due to
the mutual force of electric
repulsion.
PROBLEM 70
qA qB rA rB
Midpoint
Problem 71 determines the electric fi eld and
the electric potential at the midpoint (rA = rB) between the identical charges (qA = qB). PROBLEM 71
550 CHAPTER 19 Electric Potential Energy and the Electric Potential
72. M A Proton Gun. You and your team are designing a device that creates a beam of high-velocity protons. The device consists of a parallel-plate
capacitor in which protons start at rest at the positive plate. The protons
accelerate toward the negative plate, which has a hole through which some
of the protons pass. The plates are separated by 6.0 cm, and the potential
diff erence between the plates is 5.0 kV. What are (a) the kinetic energies and (b) the speeds of the protons when they pass through the hole? (c) What is the acceleration of the protons between the plates?
73. M Storing Wind Energy. A certain windmill produces an average of 0.50 MW of electrical power during the late evening hours when energy con-
sumption is at a low (a four-hour span). An industrial capacitor (the “BC125”)
has a capacitance of C = 63.0 F and operates with a maximum voltage of 125 V between its plates. (a) You and your team are asked to determine how many of these capacitors will be needed to store the energy produced during the
four off -peak hours in the late evening so that it can be used during the peak
hours of the early afternoon. (b) The same company that makes the BC125 storage capacitor has discovered a breakthrough dielectric material that they
use in their new model of storage capacitor, the SBC240. The new dielectric
does two things: (1) Its dielectric constant is 2.5 times that of the dielectric
in the BC125, and (2) it can operate at 240 V. How many SBC240 capacitors
are needed to store the off -peak windmill energy?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
20.1 Define electromotive force and current. 20.2 Solve problems using Ohm’s law for a
simple series circuit.
20.3 Relate resistance and resistivity. 20.4 Solve problems involving electric power. 20.5 Solve ac circuit problems for current
and power.
20.6 Analyze resistor circuits with series connections.
20.7 Analyze resistor circuits with parallel connections.
20.8 Analyze resistor circuits with both series and parallel connections.
20.9 Solve circuit problems that include internal resistances of batteries.
20.10 Solve complex circuit problems by applying Kirchhoff ’s rules.
20.11 Describe how ammeters and voltmeters operate.
20.12 Analyze capacitor circuits. 20.13 Analyze RC circuits. 20.14 Explain why electrical grounding is
important.
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CHAPTER 20
Electric Circuits
Without electric circuits this exuberant display of colorful lights in Sydney, Australia, would not be
possible. Virtually every aspect of life in modern industrialized society utilizes or depends upon electric
circuits in some way.
20.1 Electromotive Force and Current Look around you. Chances are that there is an electrical device nearby—a radio,
a hair dryer, a computer—something that uses electrical energy to operate.
The energy needed to run an MP3 player, for instance, comes from batteries, as
Figure 20.1 illustrates. The transfer of energy takes place via an electric circuit, in which the energy source (the battery pack) and the energy-consuming device
(the MP3 player) are connected by conducting wires, through which electric
charges move.
Within a battery, a chemical reaction occurs that transfers electrons from one
terminal (leaving it positively charged) to another terminal (leaving it negatively
charged). Figure 20.2 shows the two terminals of a car battery and a fl ashlight battery. The drawing also illustrates the symbol used to represent a battery in circuit
drawings. Because of the positive and negative charges on the battery terminals, an
electric potential diff erence exists between them. The maximum potential diff erence is
called the electromotive force* (emf) of the battery, for which the symbol ℰ is used. In a typical car battery, the chemical reaction maintains the potential of the positive
terminal at a maximum of 12 volts (12 joules/coulomb) higher than the potential of the
negative terminal, so the emf is ℰ = 12 V. Thus, one coulomb of charge emerging from
the battery and entering a circuit has at most 12 joules of energy. In a typical fl ashlight
551 *The word “force” appears in this context for historical reasons, even though it is incorrect. As we have seen
in Section 19.2, electric potential is energy per unit charge, which is not force.
552 CHAPTER 20 Electric Circuits
battery the emf is 1.5 V. In reality, the potential diff erence between the terminals of a battery
is somewhat less than the maximum value indicated by the emf, for reasons that Section 20.9
discusses.
In a circuit such as the one shown in Figure 20.1, the battery creates an electric fi eld within and parallel to the wire, directed from the positive toward the negative terminal. The electric fi eld
exerts a force on the free electrons in the wire, and they respond by moving. Figure 20.3 shows charges moving inside a wire and crossing an imaginary surface that is perpendicular to their
motion. This fl ow of charge is known as an electric current. The electric current I is defi ned as the amount of charge per unit time that crosses the imaginary surface, as in Figure 20.3, in much the same sense that a river current is the amount of water per unit time that is fl owing past
a certain point. If the rate is constant, the current is
I = ∆q ∆t
(20.1)
If the rate of fl ow is not constant, then Equation 20.1 gives the average current. Since the units for
charge and time are the coulomb (C) and the second (s), the SI unit for current is a coulomb per
second (C/s). One coulomb per second is referred to as an ampere (A), after the French math- ematician André-Marie Ampère (1775–1836).
If the charges move around a circuit in the same direction at all times, the current is said
to be direct current (dc), which is the kind produced by batteries. In contrast, the current is said to be alternating current (ac) when the charges move fi rst one way and then the opposite way, changing direction from moment to moment. Many energy sources produce alternating
current—for example, generators at power companies and microphones. Example 1 deals with
direct current.
Battery pack
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Moving charge
Conducting wire
To MP3 player mechanism
+
–
FIGURE 20.1 In an electric circuit, energy is transferred from a source (the battery pack) to a device (the MP3 player) by charges that move through a conducting wire.
Positive (+) terminal Negative (–)
terminal
+ –
Positive (+) terminal (raised button)
Negative (–) terminal (metallic bottom surface)
+ –
FIGURE 20.2 Typical batteries and the symbol used to represent them in electric circuits.
Surface
FIGURE 20.3 The electric current is the amount of charge per unit time that passes
through an imaginary surface that is perpen-
dicular to the motion of the charges.
EXAMPLE 1 A Pocket Calculator
The battery pack of a pocket calculator has a voltage* of 3.0 V and deliv-
ers a current of 0.17 mA. In one hour of operation, (a) how much charge fl ows in the circuit and (b) how much energy does the battery deliver to the calculator circuit?
Reasoning Since current is defi ned as charge per unit time, the charge that fl ows in one hour is the product of the current and the time (3600 s).
The charge that leaves the 3.0-V battery pack has 3.0 joules of energy
per coulomb of charge. Thus, the total energy delivered to the calculator
circuit is the charge (in coulombs) times the energy per unit charge (in
volts or joules/coulomb).
Solution (a) The charge that fl ows in one hour can be determined from Equation 20.1:
∆q = I(∆t) = (0.17 × 10−3 A)(3600 s) = 0.61 C
(b) The energy delivered to the calculator circuit is
Energy = Charge × Energy
Charge = (0.61 C)(3.0 V) = 1.8 J⏟⏟⏟
Battery voltage
*The potential diff erence between two points, such as the terminals of a battery, is commonly called the voltage between
the points.
20.2 Ohm’s Law 553
Today, it is known that electrons fl ow in metal wires. Figure 20.4 shows the negative elec- trons emerging from the negative terminal of the battery and moving counterclockwise around
the circuit toward the positive terminal. It is customary, however, not to use the fl ow of electrons when discussing circuits. Instead, a so-called conventional current is used, for reasons that date to the time when it was believed that positive charges moved through metal wires. Conventional
current is the hypothetical fl ow of positive charges that would have the same eff ect in the circuit
as the movement of negative charges that actually does occur. In Figure 20.4, negative electrons leave the negative terminal of the battery, pass through the device, and arrive at the positive
terminal. The same eff ect would have been achieved if an equivalent amount of positive charge
had left the positive terminal, passed through the device, and arrived at the negative terminal.
Therefore, the drawing shows the conventional current originating from the positive terminal and
moving clockwise around the circuit. A conventional current of hypothetical positive charges is
consistent with our earlier use of a positive test charge for defi ning electric fi elds and potentials.
The direction of conventional current is always from a point of higher potential toward a point of
lower potential—that is, from the positive toward the negative terminal. In this text, the symbol
I stands for conventional current.
20.2 Ohm’s Law The current that a battery can push through a wire is analogous to the water fl ow that a pump
can push through a pipe. Greater pump pressures lead to larger water fl ow rates, and, similarly,
greater battery voltages lead to larger electric currents. In the simplest case, the current I is directly proportional to the voltage V; that is, I ∝ V. Thus, a voltage of 12 V leads to twice as much current as a voltage of 6 V, when each is connected to the same circuit.
In a water pipe, the fl ow rate is not only determined by the pump pressure but is also
aff ected by the length and diameter of the pipe. Longer and narrower pipes off er higher resis-
tance to the moving water and lead to smaller fl ow rates for a given pump pressure. A similar
situation exists in electric circuits, and to deal with it we introduce the concept of electri-
cal resistance. Electrical resistance is defi ned in terms of two ideas that have already been
discussed—the electric potential diff erence, or voltage (see Section 19.2), and the electric cur-
rent (see Section 20.1).
The resistance R is defi ned as the ratio of the voltage V applied across a piece of material to the current I through the material, or R = V/I. When only a small current results from a large voltage, there is a high resistance to the moving charge. For many materials (e.g., metals), the
ratio V/I is the same for a given piece of material over a wide range of voltages and currents. In such a case, the resistance is a constant. Then, the relation R = V/I is referred to as Ohm’s law, after the German physicist Georg Simon Ohm (1789–1854), who discovered it.
OHM’S LAW The ratio V/I is a constant, where V is the voltage applied across a piece of material (such as a wire) and I is the current through the material:
V I
= R = constant or V = IR (20.2)
R is the resistance of the piece of material. SI Unit of Resistance: volt/ampere (V/A) = ohm (Ω)
The SI unit for resistance is a volt per ampere, which is called an ohm and is represented by the Greek capital letter omega (Ω). Ohm’s law is not a fundamental law of nature like Newton’s laws
of motion. It is only a statement of the way certain materials behave in electric circuits.
To the extent that a wire or an electrical device off ers resistance to the fl ow of charges, it is
called a resistor. The resistance can have a wide range of values. The copper wires in a television set, for instance, have a very small resistance. On the other hand, commercial resistors can have
resistances up to many kilohms (1 kΩ = 103 Ω) or megohms (1 MΩ = 106 Ω). Such resistors play
an important role in electric circuits, where they are typically used to limit the amount of current
and establish the desired voltage levels.
Conventional current, I
Electron flow
Device
+ –
FIGURE 20.4 In a circuit, electrons actually fl ow through the metal wires. However, it is
customary to use a conventional current I to describe the fl ow of charges.
554 CHAPTER 20 Electric Circuits
In drawing electric circuits we follow the usual conventions: (1) a zigzag line rep-
resents a resistor and (2) a straight line (———) represents an ideal conducting wire, or one
with a negligible resistance. Example 2 illustrates an application of Ohm’s law to the circuit in
a fl ashlight.
EXAMPLE 2 A Flashlight
The fi lament in a light bulb is a resistor in the form of a thin piece
of wire. The wire becomes hot enough to emit light because of the
current in it. Interactive Figure 20.5 shows a fl ashlight that uses two 1.5-V batteries (eff ectively a single 3.0-V battery) to provide a current
of 0.40 A in the fi lament. Determine the resistance of the glowing
fi lament.
Reasoning The fi lament resistance is assumed to be the only resistance in the circuit. The potential diff erence applied across the fi lament is that
of the 3.0-V battery. The resistance, given by Equation 20.2, is equal to
this potential diff erence divided by the current.
Solution The resistance of the fi lament is
R = V I
= 3.0 V
0.40 A = 7.5 Ω (20.2)
On
Off
Bulb filament
Insulator
Metal
Metal tip
+ –
I
R
V Switch
Resistance of bulb filament
INTERACTIVE FIGURE 20.5 The circuit in this fl ashlight consists of a resistor (the fi lament of the light bulb) connected to a 3.0-V battery (two
1.5-V batteries).
Check Your Understanding
(The answers are given at the end of the book.) 1. In circuit A the battery that supplies energy has twice as much voltage as the battery in circuit B.
However, the current in circuit A is only one-half the current in circuit B. Circuit A presents _____
the resistance to the current that circuit B does. (a) twice (b) one-half (c) the same (d) four times (e) one-fourth
2. Two circuits present the same resistance to the current. In one circuit the battery causing the fl ow of current has a voltage of 9.0 V, and the current is 3.0 A. In the other circuit the battery has a voltage of
1.5 V. What is the current in this other circuit?
20.3 Resistance and Resistivity In a water pipe, the length and cross-sectional area of the pipe determine the resistance that the
pipe off ers to the fl ow of water. Longer pipes with smaller cross-sectional areas off er greater
resistance. Analogous eff ects are found in the electrical case. For a wide range of materials, the
resistance of a piece of material of length L and cross-sectional area A is
R = ρ L A
(20.3)
where 𝜌 is a proportionality constant known as the resistivity of the material. It can be seen from Equation 20.3 that the unit for resistivity is the ohm · meter (Ω · m), and Table 20.1 lists values for various materials. All the conductors in the table are metals and have small resistivities. Insulators
such as rubber have large resistivities. Materials like germanium and silicon have intermediate
resistivity values and are, accordingly, called semiconductors. Resistivity is an inherent property of a material, inherent in the same sense that density is
an inherent property. Resistance, on the other hand, depends on both the resistivity and the geometry
20.3 Resistance and Resistivity 555
of the material. Thus, two wires can be made from copper, which has a resistivity of 1.72 ×
10−8 Ω · m, but Equation 20.3 indicates that a short wire with a large cross-sectional area has a smaller resistance than does a long, thin wire. Wires that carry large currents, such as main power
cables, are thick rather than thin so that the resistance of the wires is kept as small as possible.
Similarly, electric tools that are to be used far away from wall sockets require thicker extension
cords, as Example 3 illustrates.
TABLE 20.1 Resistivitiesa of Various Materials
Material Resistivity 𝞺
(Ω · m) Material Resistivity 𝞺
(Ω · m) Conductors Semiconductors Aluminum 2.82 × 10−8 Carbon 3.5 × 10−5
Copper 1.72 × 10−8 Germanium 0.5b
Gold 2.44 × 10−8 Silicon 20–2300b
Iron 9.7 × 10−8 Insulators Mercury 95.8 × 10−8 Mica 1011–1015
Nichrome (alloy) 100 × 10−8 Rubber (hard) 1013–1016
Silver 1.59 × 10−8 Teflon 1016
Tungsten 5.6 × 10−8 Wood (maple) 3 × 1010
aThe values pertain to temperatures near 20 °C. bDepending on purity.
EXAMPLE 3 The Physics of Electrical Extension Cords
The instructions for an electric lawn mower suggest that a 20-gauge
extension cord can be used for distances up to 35 m, but a thicker 16-gauge
cord should be used for longer distances, to keep the resistance of the wire
as small as possible. The cross-sectional area of 20-gauge wire is 5.2 ×
10−7 m2, while that of 16-gauge wire is 13 × 10−7 m2. Determine the re-
sistance of (a) 35 m of 20-gauge copper wire and (b) 75 m of 16-gauge copper wire.
Reasoning According to Equation 20.3, the resistance of a copper wire depends on the resistivity of copper and the length and cross-
sectional area of the wire. The resistivity can be obtained from
Table 20.1, while the length and cross-sectional area are given in the problem statement.
Solution According to Table 20.1 the resistivity of copper is 1.72 × 10−8 Ω · m. The resistance of the wires can be found using Equation 20.3:
20-gauge wire R = ρL A
= (1.72 × 10−8 Ω · m)(35 m)
5.2 × 10−7 m2 = 1.2 Ω
16-gauge wire R = ρL A
= (1.72 × 10−8 Ω · m)(75 m)
13 × 10−7 m2 = 0.99 Ω
Even though it is more than twice as long, the thicker 16-gauge wire has
less resistance than the thinner 20-gauge wire. It is necessary to keep the
resistance as low as possible to minimize heating of the wire, thereby
reducing the possibility of a fi re, as Conceptual Example 7 in Section 20.5
emphasizes.
BIO THE PHYSICS OF . . . impedance plethysmography. Equation 20.3 provides the basis for an important medical diagnostic technique known as impedance (or resistance)
plethysmography. Figure 20.6 shows how the technique is applied to diagnose blood clotting in the veins (deep venous thrombosis) near the knee. A pressure cuff , like that used in blood pres-
sure measurements, is placed around the midthigh, while electrodes are attached around the calf.
The two outer electrodes are connected to a source that supplies a small amount of ac current.
The two inner electrodes are separated by a distance L, and the voltage between them is mea- sured. The voltage divided by the current gives the resistance. The key to this technique is the
fact that resistance can be related to the volume Vcalf of the calf between the inner electrodes. The volume is the product of the length L and the calf’s cross-sectional area A, or Vcalf = LA. Solving for A and substituting in Equation 20.3 shows that
R = ρ L A
= ρ L
Vcalf /L = ρ
L2
Vcalf
556 CHAPTER 20 Electric Circuits
Thus, resistance is inversely proportional to volume, a fact that is exploited in diagnosing deep
venous thrombosis. Blood fl ows from the heart into the calf through arteries in the leg and returns
through the system of veins. The pressure cuff in Figure 20.6 is infl ated to the point where it cuts off the venous fl ow but does not alter the arterial fl ow. As a result, more blood enters than leaves
the calf. Therefore, the volume of the calf increases, and the electrical resistance decreases. When
the cuff pressure is removed suddenly, the volume returns to a normal value, and so does the elec-
trical resistance. With healthy (unclotted) veins, there is a rapid return to normal values. A slow
return, however, reveals the presence of clotting.
The resistivity of a material depends on temperature. In metals, the resistivity increases with
increasing temperature, whereas in semiconductors the reverse is true. For many materials and
limited temperature ranges, it is possible to express the temperature dependence of the resistivity
as follows:
ρ = ρ 0 [1 + α (T − T0) ] (20.4)
In this expression 𝜌 and 𝜌0 are the resistivities at temperatures T and T0, respectively. The term 𝛼 has the unit of reciprocal temperature and is the temperature coeffi cient of resistivity. When the resistivity increases with increasing temperature, 𝛼 is positive, as it is for metals. When the resis-
tivity decreases with increasing temperature, 𝛼 is negative, as it is for the semiconductors carbon,
germanium, and silicon. Since resistance is given by R =𝜌L/A, both sides of Equation 20.4 can be multiplied by L/A to show that resistance depends on temperature according to
R = R 0 [1 + α (T − T0) ] (20.5)
The next example illustrates the role of the resistivity and its temperature coeffi cient in deter-
mining the electrical resistance of a piece of material.
L
Pressure cuff inflation system
Voltage measurement device
Electrode
Ac current source
FIGURE 20.6 Using the technique of impedance plethysmography, the electrical
resistance of the calf can be measured to
diagnose deep venous thrombosis (blood
clotting in the veins).
EXAMPLE 4 The Physics of a Heating Element on an Electric Stove
Figure 20.7a shows a cherry-red heating element on an electric stove. The element contains a wire (length = 1.1 m, cross-sectional area = 3.1 ×
10−6 m2) through which electric charge fl ows. As Figure 20.7b shows, this wire is embedded within an electrically insulating material that is
contained within a metal casing. The wire becomes hot in response to
the fl owing charge and heats the casing. The material of the wire has a
resistivity of 𝜌0 = 6.8 × 10 −5 Ω · m at T0 = 320 °C and a temperature coef-
fi cient of resistivity of 𝛼 = 2.0 × 10−3 (C°)−1. Determine the resistance of
the heater wire at an operating temperature of 420 °C.
Reasoning The expression R = 𝜌L/A (Equation 20.3) can be used to fi nd the resistance of the wire at 420 °C, once the resistivity 𝜌 is
determined at this temperature. Since the resistivity at 320 °C is given,
Equation 20.4 can be employed to fi nd the resistivity at 420 °C.
Solution At the operating temperature of 420 °C, the material of the wire has a resistivity of
ρ = ρ 0 [1 + α (T − T0) ]
ρ = (6.8 × 10−5 Ω · m){1 + [2.0 × 10−3 (C° )−1](420 °C − 320 °C)} = 8.2 × 10−5 Ω · m
This value of the resistivity can be used along with the given length and
cross-sectional area to fi nd the resistance of the heater wire:
R = ρL A
= (8.2 × 10−5 Ω · m)(1.1 m)
3.1 × 10−6 m2 = 29 Ω (20.3)
(a)
Metal casing
Heater wire (A = 3.1 × 10–6 m2)
L = 1.1 m
(b)
FIGURE 20.7 A heating element on an electric stove.
S p en
ce r
G ra
n t/
P h o to
E d it
20.4 Electric Power 557
There is an important class of materials whose resistivity suddenly goes to zero below a
certain temperature Tc, which is called the critical temperature and is commonly a few degrees above absolute zero. Below this temperature, such materials are called superconductors. The name derives from the fact that with zero resistivity, these materials off er no resistance to electric
current and are, therefore, perfect conductors. Once a current is established in a superconducting
ring, the current continues indefi nitely without the need for an emf. Currents have persisted in
superconductors for many years without measurable decay. In contrast, the current in a nonsuper-
conducting material drops to zero almost immediately after the emf is removed.
Many metals become superconductors only at very low temperatures, such as aluminum
(Tc = 1.18 K), tin (Tc = 3.72 K), lead (Tc = 7.20 K), and niobium (Tc = 9.25 K). Materials involv- ing copper oxide complexes have been made that undergo the transition to the superconducting
state at 175 K. Superconductors have many technological applications, including magnetic reso-
nance imaging (Section 21.7), magnetic levitation of trains (Section 21.9), cheaper transmission
of electric power, powerful (yet small) electric motors, and faster computer chips.
Check Your Understanding
(The answers are given at the end of the book.) 3. Two materials have diff erent resistivities. Two wires of the same length are made, one from each of
the materials. Is it possible for each wire to have the same resistance? (a) Yes, if the material with the greater resistivity is used for a thinner wire. (b) Yes, if the material with the greater resistivity is used for a thicker wire. (c) It is not possible.
4. How does the resistance of a copper wire change when both the length and diameter of the wire are doubled? (a) It decreases by a factor of two. (b) It increases by a factor of two. (c) It increases by a factor of four. (d) It decreases by a factor of four. (e) It does not change.
5. A resistor is connected between the terminals of a battery. This resistor is a wire, and the following fi ve choices give possibilities for its length and radius in multiples of L0 and r0, respectively. For which one or more of the possibilities is the current in the resistor a minimum? (a) L0 and r0 (b) 12 L 0 and
1
2 r 0 (c) 2L0 and 2r0 (d) 2L0 and r0 (e) 8L0 and 2r0
20.4 Electric Power One of the most important functions of current in an electric circuit is to transfer energy from a
source (a battery or a generator) to an electrical device (MP3 player, cell phone, etc.), as Figure 20.8 illustrates. Note that the positive (+) terminal of the battery is connected by a wire to the terminal
labeled A on the device; likewise, the negative terminal (−) of the battery is connected to the B terminal. Thus, the battery maintains a constant potential diff erence between the terminals A and B, with A being at the higher potential. When an amount of positive charge Δq moves from the
Electric deviceBattery Voltage, V
+
–
I
I
A
B
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FIGURE 20.8 The current I in the circuit delivers energy to the electric
device. The voltage between the
terminals of the device is V.
558 CHAPTER 20 Electric Circuits
higher potential (A) to the lower potential (B), its electric potential energy decreases. In accor- dance with Equation 19.4, this decrease is (Δq)V, where V is the amount by which the electric potential at A exceeds that at B or, in other words, the voltage between the two points. Since the change in energy per unit time is the power P (Equation 6.10b), the electric power associated with this change in energy is
P = Change in energy
Time interval =
(∆q)V ∆t
= ∆q ∆t
V
The term Δq/Δt is the charge per unit time, or the current I in the device, according to Equation 20.1. It follows, then, that the electric power is the product of the current and the voltage.
ELECTRIC POWER When electric charge fl ows from point A to point B in a circuit, leading to a current I, and the voltage between the points is V, the electric power associated with this current and voltage is
P = IV (20.6)
SI Unit of Power: watt (W)
Power is measured in watts, and Equation 20.6 indicates that the product of an ampere and a volt
is equal to a watt.
When the charge moves through the device in Figure 20.8, the charge loses electric potential energy. The principle of conservation of energy tells us that the decrease in potential energy must
be accompanied by a transfer of energy to some other form (or forms). In a cell phone, for exam-
ple, the energy transferred appears as light energy (coming from the display screen), sound energy
(emanating from the speaker), thermal energy (due to heating of the internal circuitry), and so on.
The charge in a circuit can also gain electrical energy. For example, when it moves through
the battery in Figure 20.8, the charge goes from a lower to a higher potential, just the opposite of what happens in the electrical device. In this case, the charge gains electric potential energy. Consistent with the conservation of energy, this increase in potential energy must come from
somewhere; in this case it comes from the chemical energy stored in the battery. Thus, the charge
regains the energy it lost to the device, at the expense of the chemical energy of the battery.
Many electrical devices are essentially resistors that become hot when provided with suffi -
cient electric power: toasters, irons, space heaters, heating elements on electric stoves, and incan-
descent light bulbs, to name a few. In such cases, it is convenient to have additional expressions
that are equivalent to the power P = IV but which include the resistance R explicitly. We can obtain two such equations by substituting V = IR, or equivalently I = V/R, into the relation P = IV:
P = IV (20.6a)
P = I(IR) = I 2R (20.6b)
P = (VR) V = V 2
R (20.6c)
Example 5 deals with the electric power delivered to the bulb of a fl ashlight.
{
Current I
EXAMPLE 5 The Power and Energy Used in a Flashlight
In the flashlight in Interactive Figure 20.5, the current is 0.40 A, and the voltage is 3.0 V. Find (a) the power delivered to the bulb and (b) the electrical energy dissipated in the bulb in 5.5 minutes of operation.
Reasoning The electric power delivered to the bulb is the product of the current and voltage. Since power is energy per unit time, the energy
delivered to the bulb is the product of the power and time.
Solution (a) The power is P = IV = (0.40 A)(3.0 V) = 1.2 W (20.6a)
The “wattage” rating of this bulb would, therefore, be 1.2 W.
(b) The energy consumed in 5.5 minutes (330 s) follows from the defi ni- tion of power as energy per unit time:
Energy = P ∆t = (1.2 W)(330 s) = 4.0 × 10 2 J
20.5 Alternating Current 559
Monthly electric bills specify the cost for the energy consumed during the month. Energy
is the product of power and time, and electric companies compute your energy consumption by
expressing power in kilowatts and time in hours. Therefore, a commonly used unit for energy is
the kilowatt · hour (kWh). For instance, if you used an average power of 1440 watts (1.44 kW) for 30 days (720 h), your energy consumption would be (1.44 kW) (720 h) = 1040 kWh. At a
cost of $0.12 per kWh, your monthly bill would be $125. As shown in Example 10 in Chapter 12,
1 kWh = 3.60 × 106 J of energy.
Check Your Understanding
(The answers are given at the end of the book.) 6. A toaster is designed to operate with a voltage of 120 V, and a clothes dryer is designed to operate with
a voltage of 240 V. Based solely on this information, which appliance uses more power? (a) The toaster (b) The dryer (c) Insuffi cient information is given for an answer.
7. When an incandescent light bulb is turned on, a constant voltage is applied across the tungsten fi la- ment, which then becomes white hot. The temperature coeffi cient of resistivity for tungsten is a positive
number. What happens to the power delivered to the bulb as the fi lament heats up? (a) It decreases. (b) It increases. (c) It remains constant.
8. CYU Figure 20.1 shows a circuit that includes a bime- tallic strip (made from brass and steel; see Section 12.4)
with a resistance heater wire wrapped around it. When
the switch is initially closed, a current appears in the
circuit because charges fl ow through the heater wire
(which becomes hot), the strip itself, the contact point,
and the light bulb. The bulb glows in response. As long
as the switch remains closed, does the bulb (a) continue to glow, (b) eventually turn off permanently, or (c) fl ash on and off ?
20.5 Alternating Current Many electric circuits use batteries and involve direct current (dc). However, there are consider-
ably more circuits that operate with alternating current (ac), in which the charge fl ow reverses
direction periodically. The common generators that create ac electricity depend on magnetic
forces for their operation and are discussed in Chapter 22. In an ac circuit, these generators serve
the same purpose as a battery serves in a dc circuit; that is, they give energy to the moving electric
charges. This section deals with ac circuits that contain only resistance.
Since the electrical outlets in a house provide alternating current, we all use ac circuits rou-
tinely. For example, the heating element of a toaster is essentially a thin wire of resistance R and becomes red hot when electrical energy is dissipated in it. Figure 20.9 shows the ac circuit that
Switch
Brass
Resistance heater wire
Contact point
Steel
CYU FIGURE 20.1
Ac generator
Ac generator
Heating element (thin wire of resistance R)
R
FIGURE 20.9 This circuit consists of a toaster (resistance = R) and an ac generator at the electric power company.
560 CHAPTER 20 Electric Circuits
is formed when a toaster is plugged into a wall socket. The circuit schematic in the picture intro-
duces the symbol � that is used to represent the generator. In this case, the generator is located at the electric power company.
Figure 20.10 shows a graph that records the voltage V produced between the terminals of the ac generator in Figure 20.9 at each moment of time t. This is the most common type of ac voltage. It fl uctuates sinusoidally between positive and negative values:
V = V0 sin 2πft (20.7)
where V0 is the maximum or peak value of the voltage, and f is the frequency (in cycles/s or Hz) at which the voltage oscillates. The angle 2πft in Equation 20.7 is expressed in radians, so a calcu- lator must be set to its radian mode before the sine of this angle is evaluated. In the United States,
the voltage at most home wall outlets has a peak value of approximately V0 = 170 volts and oscil- lates with a frequency of f = 60 Hz. Thus, the period of each cycle is 160 s, and the polarity of the generator terminals reverses twice during each cycle, as Figure 20.10 indicates.
The current in an ac circuit also oscillates. In circuits that contain only resistance, the current
reverses direction each time the polarity of the generator terminals reverses. Thus, the current in
a circuit like that in Figure 20.9 would have a frequency of 60 Hz and would change direction twice during each cycle. Substituting V = V0 sin 2πft into V = IR shows that the current can be represented as
I = V0 R
sin 2πft = I0 sin 2πft (20.8)
The peak current is given by I0 = V0/R, so it can be determined if the peak voltage and the resis- tance are known.
The power delivered to an ac circuit by the generator is given by P = IV, just as it is in a dc circuit. However, since both I and V depend on time, the power fl uctuates as time passes. Substi- tuting Equations 20.7 and 20.8 for V and I into P = IV gives
P = I0 V0 sin2 2πft (20.9)
This expression is plotted in Figure 20.11. Since the power fl uctuates in an ac circuit, it is customary to consider the average power P,
which is one-half the peak power, as Figure 20.11 indicates: P = 12 I0V0 (20.10)
On the basis of this expression, a kind of average current and average voltage can be introduced
that are very useful when discussing ac circuits. A rearrangement of Equation 20.10 reveals that
P = ( I0
√2 ) (
V0 √2
) = IrmsVrms (20.11) Irms and Vrms are called the root-mean-square (rms) current and voltage, respectively, and may be calculated from the peak values by dividing them by √ 2:*
Irms = I0
√2 (20.12)
Vrms = V0 √2
(20.13)
Problem-Solving Insight The rms values of the ac current and the ac voltage, Irms and Vrms, respectively, are not the same as the peak values I0 and V0. The rms values are always smaller than the peak values by a factor of √ 2.
Since the normal maximum ac voltage at a home wall socket in the United States is V0 = 170 volts, the corresponding rms voltage is Vrms = (170 volts)/ √ 2 = 120 volts. Instructions for electrical devices usually specify this rms value. Similarly, when we specify an ac voltage or current in this
text, it is an rms value, unless indicated otherwise. When we specify ac power, it is an average
power, unless stated otherwise.
+
+V0
0 t
–V0
–
– + – +
+ –
FIGURE 20.10 In the most common case, the ac voltage is a sinusoidal function of
time. The relative polarity of the generator
terminals during the positive and negative
parts of the sine wave is indicated.
I0V0
I0V0 1– 2
Average power
t
P
FIGURE 20.11 In an ac circuit, the power P delivered to a resistor oscillates between zero and a peak value of I0V0, where I0 and V0 are the peak current and voltage, respectively.
*This applies only for sinusoidal current and voltage.
20.5 Alternating Current 561
Except for dealing with average quantities, the relation P = IrmsVrms has the same form as Equation 20.6a (P = IV). Moreover, Ohm’s law can be written conveniently in terms of rms quantities:
Vrms = Irms R (20.14)
Substituting Equation 20.14 into P = IrmsVrms shows that the average power can be expressed in the following ways:
P = IrmsVrms (20.15a)
P = I 2rms R (20.15b)
P = V 2rms R
(20.15c)
These expressions are completely analogous to P = IV = I2R = V2/R (Equations 20.6a–c) for dc circuits. Example 6 deals with the average power in one familiar ac circuit.
EXAMPLE 6 Electric Power Sent to a Loudspeaker
A stereo receiver applies a peak ac voltage of 34 V to a speaker. The
speaker behaves approximately* as if it had a resistance of 8.0 Ω, as the
circuit in Figure 20.12 indicates. Determine (a) the rms voltage, (b) the rms current, and (c) the average power for this circuit.
Reasoning The rms voltage is, by defi nition, equal to the peak voltage divided by √ 2 . Furthermore, we are assuming that the circuit contains
only a resistor. Therefore, we can use Ohm’s law (Equation 20.14) to cal-
culate the rms current as the rms voltage divided by the resistance, and
we can then determine the average power as the rms current times the rms
voltage (Equation 20.15a).
Solution (a) The peak value of the voltage is V0 = 34 V, so the corre- sponding rms value is
Vrms = V0 √2
= 34 V
√2 = 24 V (20.13)
(b) The rms current can be obtained from Ohm’s law:
Irms = Vrms R
= 24 V
8.0 Ω = 3.0 A (20.14)
(c) The average power is
P = IrmsVrms = (3.0 A)(24 V) = 72 W (20.15a)
Receiver
8.0-Ω speaker
V0 = 34 V R = 8.0 Ω
FIGURE 20.12 A receiver applies an ac voltage (peak value = 34 V) to an 8.0-Ω
speaker.
The electric power dissipated in a resistor causes the resistor to heat up. Excessive power can
lead to a potential fi re hazard, as Conceptual Example 7 discusses.
*Other factors besides resistance can aff ect the current and voltage in ac circuits; they are discussed in Chapter 23.
CONCEPTUAL EXAMPLE 7 Extension Cords and a Potential Fire Hazard
During the winter, many people use portable electric space heaters to
keep warm. When the heater is located far from a 120-V wall receptacle,
an extension cord is necessary (see Figure 20.13). To prevent fi res, how- ever, manufacturers sometimes caution about using extension cords. To
minimize the risk of a fi re, should a long extension cord used with a space
heater be made from (a) larger-gauge or (b) smaller-gauge wire?
Reasoning An electric space heater contains a heater element that is a piece of wire of resistance R, which is heated to a high temperature because of the power I2rmsR dissipated in it. A typical heater uses a relatively large current Irms of about 12 A. On its way to the heater, this current passes through the wires of the extension cord. Since these additional wires off er
resistance to the current, the extension cord can also heat up, just as the
562 CHAPTER 20 Electric Circuits
Check Your Understanding
(The answers are given at the end of the book.) 9. CYU Figure 20.2 shows a circuit in which a light bulb is
connected to the household ac voltage via two switches,
S1 and S2. This is the kind of wiring, for example, that allows you to turn on a carport light from either inside the house or
out in the carport. Which one or more of the combinations of
the switch positions will turn on the light? (a) S1 set to A and S2 set to B (b) S1 set to B and S2 set to B (c) S1 set to B and S2 set to A (d) S1 set to A and S2 set to A
10. Two light bulbs are designed for use with an ac voltage of 120 V and are rated at 75 W and 150 W. Which bulb, if
either, has the greater fi lament resistance?
11. An ac circuit contains only a generator and a resistor. Which one of the following changes leads to the greatest average
power being delivered to the circuit? (a) Double the peak voltage of the generator and double the resistance. (b) Double the resistance. (c) Double the peak voltage of the generator. (d) Double the peak voltage of the generator and reduce the resistance by a factor of two.
20.6 Series Wiring Thus far, we have dealt with circuits that include only a single device, such as a light bulb or a
loudspeaker. There are, however, many circuits in which more than one device is connected to a
voltage source. This section introduces one method by which such connections may be made—
namely, series wiring. Series wiring means that the devices are connected in such a way that there is the same electric current through each device. Figure 20.14 shows a circuit in which two diff erent devices, represented by resistors R1 and R2, are connected in series with a battery. Note that if the current in one resistor is interrupted, the current in the other is too. This could
occur, for example, if two light bulbs were connected in series and the fi lament of one bulb
broke. Because of the series wiring, the voltage V supplied by the battery is divided between the two resistors. The drawing indicates that the portion of the voltage across R1 is V1, while the portion across R2 is V2, so V = V1 + V2. For the individual resistances, the defi nition of resistance indicates that R1 = V1/I and R2 = V2/I, so that V1 = IR1 and V2 = IR2. Therefore, we have
V = V1 + V2 = IR1 + IR2 = I(R1 + R2) = IRS where RS is called the equivalent resistance of the series circuit. Thus, two resistors in series are equivalent to a single resistor whose resistance is RS = R1 + R2, in the sense that there is the same current through RS as there is through the series combination of R1 and R2. This line of reasoning can be extended to any number of resistors in series if we note the following:
heater element does. This unwanted heating depends on the resistance of
the wire in the extension cord and could lead to a fi re. As Example 3 dis-
cusses, the larger-gauge wire is the one that has the smaller cross-sectional
area. The cross-sectional area is important because it is one of the factors
that determine the resistance of the wire in the extension cord.
Answer (a) is incorrect. To keep the heating of the extension cord to a safe level, the resistance of the wire must be kept small. Recall from
Section 20.3 that the resistance of a wire depends inversely on its cross-
sectional area. A larger-gauge wire has a smaller cross-sectional area
and, therefore, has a greater resistance Rextension cord. This greater resistance would lead to more (not less) heating of the extension cord, because of the
power I2rms Rextension cord dissipated in it.
Answer (b) is correct. Since the wire’s resistance depends inversely on its cross-sectional area, a smaller-gauge wire, with its larger cross-sectional
area, has a smaller resistance Rextension cord. This smaller resistance would lead to less heating of the extension cord due to the power I2rmsRextension cord dissipated in it, thus minimizing the risk of a fi re.
Related Homework: Problem 36
FIGURE 20.13 When an extension cord is used with a
space heater, the cord must
have a resistance that is
suffi ciently small to prevent
overheating of the cord.
S1
A
B
A
B
Switch inside house
Switch in carport
S2
CYU FIGURE 20.2
+ –
R1
V1
I
V
V2
R2
FIGURE 20.14 When two resistors are connected in series, the same current I is in both of them.
20.6 Series Wiring 563
Problem-Solving Insight The voltage across all the resistors in series is the sum of the individual voltages across each resistor.
The result for the equivalent resistance is
Series resistors RS = R1 + R2 + R3 + ⋅ ⋅ ⋅ (20.16)
Examples 8 and 9 illustrate the concept of equivalent resistance in series circuits.
EXAMPLE 8 A Series Circuit
Suppose that the resistances in Figure 20.14 are R1 = 47 Ω and R2 = 86 Ω, and the battery voltage is 24 V. Determine the equivalent resistance of the
two resistors and the current in the circuit.
Reasoning The two resistors are wired in series, since there is the same current through each one. The equivalent resistance RS of a series circuit is the sum of the individual resistances, so RS = R1 + R2. The current I can be obtained from Ohm’s law as the voltage V divided by the equivalent resistance: I = V/RS.
Solution The equivalent resistance is
RS = R1 + R2 = 47 Ω + 86 Ω = 133 Ω (20.16)
The current in the circuit is
I = V RS
= 24 V
133 Ω = 0.18 A (20.2)
Analyzing Multiple-Concept Problems
EXAMPLE 9 Power Delivered to a Series Circuit
A 6.00-Ω resistor and a 3.00-Ω resistor are connected in series with a 12.0-V
battery, as Figure 20.15 indicates. Assuming that the battery contributes no resistance to the circuit, fi nd the power delivered to each of the resistors.
Reasoning The power P delivered to each resistor is the product of the current squared (I2) and the corresponding resistance R, or P = I2R. The
resistances are known, and Ohm’s law can be used to fi nd the current.
Ohm’s law states that the current in the circuit (which is also the current
through each of the resistors) equals the voltage V of the battery divided by the equivalent resistance RS of the two resistors: I = V/RS. Since the resistors are connected in series, we can obtain the equivalent resistance
by adding the two resistances (see Figure 20.15).
+ –
6.00 Ω 3.00 Ω
Is equivalent to
I
12.0 V
+ –
Rs = 9.00 Ω
I
12.0 V
FIGURE 20.15 A 6.00-Ω and a 3.00-Ω resistor connected in series are equivalent to a single 9.00-Ω resistor.
Knowns and Unknowns The data for this problem are:
Description Symbol Value Resistance of 6.00-Ω resistor R1 6.00 Ω
Resistance of 3.00-Ω resistor R2 3.00 Ω
Battery voltage V 12.0 V
Unknown Variables Power delivered to 6.00-Ω resistor P1 ?
Power delivered to 3.00-Ω resistor P2 ?
564 CHAPTER 20 Electric Circuits
Modeling the Problem
STEP 1 Power The power P1 delivered to the 6.00-Ω resistor is given by P1=I2R1 (Equation 20.6b), where I is the current through the resistor and R1 is the resistance. In this expression R1 is a known quantity, and the current I will be determined in Step 2.
STEP 2 Ohm’s Law The current I in the circuit depends on the voltage V of the battery and the equivalent resistance RS of the two resistors in series (see Figure 20.15). This dependence is given by Ohm’s law (Equation 20.2) as
I = V RS
This result for the current can be substituted into Equation 20.6b, as indicated at the right. Note
from the data table that the voltage is given. In Step 3 we will evaluate the equivalent resistance
from the individual resistances R1 and R2.
STEP 3 Equivalent Resistance Since the two resistors are wired in series, the equivalent resistance RS is the sum of the two resistances (Equation 20.16):
RS = R1 + R2
The resistances R1 and R2 are known. We substitute this expression for RS into Equation 1, as shown in the right column.
Solution Algebraically combining the results of the three steps, we have
P1 = I 2R1 = ( VRS) 2
R1 = ( VR1 + R2) 2
R1
The power delivered to the 6.00-Ω resistor is
P1 = ( VR1 + R2) 2
R1 = ( 12.0 V6.00 Ω + 3.00 Ω) 2
(6.00 Ω) = 10.7 W
In a similar fashion, it can be shown that the power delivered to the 3.00-Ω resistor is
P2 = ( VR1 + R2) 2
R2 = ( 12.0 V6.00 Ω + 3.00 Ω) 2
(3.00 Ω) = 5.3 W
Related Homework: Problems 44, 46
STEP 1 STEP 2 STEP 2
P1 = I 2R1 (20.6b)
?
P1 = I 2R1 (20.6b)
I = V RS
(1)
?
P1 = I 2R1 (20.6b)
I = V RS
(1)
RS = R1 + R2 (20.16)
In Example 9 the total power sent to the two resistors is P = 10.7 W + 5.3 W = 16.0 W. Alternatively, the total power could have been obtained by using the voltage across the two resis-
tors (the battery voltage) and the equivalent resistance RS:
P = V 2
RS =
(12.0 V)2
6.00 Ω + 3.00 Ω = 16.0 W (20.6c)
Problem-Solving Insight The total power delivered to any number of resistors in series is equal to the power delivered to the equivalent resistance.
THE PHYSICS OF . . . personal digital assistants. Pressure-sensitive pads form the heart of computer input devices that function as personal digital assistants, or PDAs, and they
off er an interesting application of series resistors. These devices are simple to use. You write
directly on the pad with a plastic stylus that itself contains no electronics (see Figure 20.16). The writing appears as the stylus is moved, and recognition software interprets it as input for the
built-in computer. The pad utilizes two transparent conductive layers that are separated by a small
distance, except where pressure from the stylus brings them into contact (see point P in the draw- ing). Current I enters the positive side of the top layer, fl ows into the bottom layer through point P, and exits that layer through its negative side. Each layer provides resistance to the current, the
20.7 Parallel Wiring 565
amounts depending on where the point P is located. As the right side of the drawing indicates, the resistances from the layers are in series, since the same current exists in both of them. The
voltage across the top-layer resistance is VT, and the voltage across the bottom-layer resistance is VB. In each case, the voltage is the current times the resistance. These two voltages are used to locate the point P and to activate (darken) one of the elements or pixels in a liquid crystal display matrix that lies beneath the transparent layers (see Section 24.6 for a discussion of liquid crystal
displays). As the stylus is moved, the writing becomes visible as one element after another in the
display matrix is activated.
THE PHYSICS OF . . . a joystick. The joystick, found in computer games, also takes advantage of resistors connected in series. A joystick contains two straight coils of resistance
wire that are oriented at 90° to each other (see Figure 20.17a). When the joystick is moved, it repositions the metallic slider on each of the coils. As part b of the drawing illustrates, each coil is connected across a 1.5-V battery.* Because one end of a coil is at 1.5 V and the other at 0 V,
the voltage at the location of the slider is somewhere between these values; the voltage of the
left slider in the drawing is labeled V1 and the voltage of the right slider is V2. The slider voltages are sent via wires to a computer, which translates them into positional data. In eff ect, the slider
divides each resistance coil into two smaller resistance coils wired in series, and allows the volt-
age at the point where they are joined together to be detected.
Check Your Understanding
(The answer is given at the end of the book.) 12. The power rating of a 1000-W heater specifi es the power that the heater uses when it is connected to an
ac voltage of 120 V. What is the total power used by two of these heaters when they are connected in
series with a single ac voltage of 120 V? (a) 4000 W (b) 3000 W (c) 2000 W (d) 1000 W (e) 500 W
20.7 Parallel Wiring Parallel wiring is another method of connecting electrical devices. Parallel wiring means that the devices are connected in such a way that the same voltage is applied across each device. Figure 20.18 shows two resistors connected in parallel between the terminals of a battery. Part a of the picture is drawn so as to emphasize that the entire voltage of the battery is applied across
each resistor. Actually, parallel connections are rarely drawn in this manner; instead they are
drawn as in part b, where the dots indicate the points where the wires for the two branches are joined together. Figures 20.18a and b are equivalent representations of the same circuit.
Point of contact P
Current I I
VT
VB
Transparent conductive layers
Liquid crystal display matrix
Point of contact P
Stylus
FIGURE 20.16 The pressure pad on which the user writes in a personal digital assistant is based on the use of resistances that are connected in series.
Joystick
Sliders
Coil resistors
Slider
+1.5 V
+1.5 V
0 V
0 V
To computer
To computer
Slider
(a)
(b)
V 1
V 2
FIGURE 20.17 (a) A joystick uses two perpendicular movable sliders, and each
makes contact with a coil resistor. (b) The sliders allow detection of the voltages V1 and V2, which a computer translates into positional data.
*For clarity, two batteries are shown in Figure 20.17b, one associated with each resistance coil. In reality, both coils are connected across a single battery.
+ –
R2
R1
V (a)
+ –
R2
I2
I1
R1
I V (b)
FIGURE 20.18 (a) When two resistors are connected in parallel, the same voltage V is applied across each resistor. (b) This drawing is equivalent to part a. I1 and I2 are the currents in R1 and R2.
566 CHAPTER 20 Electric Circuits
Parallel wiring is very common. For example, when an electrical appliance is plugged into
a wall socket, the appliance is connected in parallel with other appliances, as in Figure 20.19, where the entire voltage of 120 V is applied across each one of the devices: the television, the
stereo, and the light bulb (when the switch is turned on). The presence of the unused socket or
other devices that are turned off does not aff ect the operation of those devices that are turned on.
Moreover, if the current in one device is interrupted (perhaps by an opened switch or a broken
wire), the current in the other devices is not interrupted. In contrast, if household appliances were
connected in series, there would be no current through any appliance if the current in the circuit
were halted at any point.
When two resistors R1 and R2 are connected as in Figure 20.18, each receives current from the battery as if the other were not present. Therefore, R1 and R2 together draw more current from the battery than does either resistor alone. According to the defi nition of resistance, R = V/I, a larger current implies a smaller resistance. Thus, the two parallel resistors behave as a single
equivalent resistance that is smaller than either R1 or R2. Figure 20.20 returns to the water-fl ow analogy to provide additional insight into this important feature of parallel wiring. In part a, two sections of pipe that have the same length are connected in parallel with a pump. In part b these two sections have been replaced with a single pipe of the same length, whose cross-sectional area
equals the combined cross-sectional areas of section 1 and section 2. The pump (analogous to a
voltage source) can push more water per second (analogous to current) through the wider pipe in
part b (analogous to a wider wire) than it can through either of the narrower pipes (analogous to narrower wires) in part a. In eff ect, the wider pipe off ers less resistance to the fl ow of water than either of the narrower pipes off ers individually.
As in a series circuit, it is possible to replace a parallel combination of resistors with an
equivalent resistor that results in the same total current and power for a given voltage as the origi-
nal combination. To determine the equivalent resistance for the two resistors in Figure 20.18b, note that the total current I from the battery is the sum of I1 and I2, where I1 is the current in resis- tor R1 and I2 is the current in resistor R2: I = I1 + I2. Since the same voltage V is applied across each resistor, the defi nition of resistance indicates that I1 = V/R1 and I2 = V/R2. Therefore,
I = I1 + I2 = V R1
+ V R2
= V ( 1R1 + 1
R2) = V ( 1
RP) where RP is the equivalent resistance. Hence, when two resistors are connected in parallel, they are equivalent to a single resistor whose resistance RP can be obtained from 1/RP = 1/R1 + 1/R2.
Problem-Solving Insight For any number of resistors wired in parallel, the total current from the voltage source is the sum of the currents in the individual resistors.
Thus, a similar line of reasoning reveals that the equivalent resistance is
Parallel resistors 1
RP =
1
R1 +
1
R2 +
1
R3 + ⋅ ⋅ ⋅ (20.17)
The next example deals with a parallel combination of resistors that occurs in a stereo
system.
120 V Switch
Light bulb
StereoTV
FIGURE 20.19 This drawing shows some of the parallel connections found in a typical
home. Each wall socket provides 120 V to the
appliance connected to it. In addition, 120 V
is applied to the light bulb when the switch is
turned on.
FIGURE 20.20 (a) Two equally long pipe sections, with cross-sectional areas A1 and A2, are connected in parallel to a water pump. (b) The two parallel pipe sections in part a are equivalent to a single pipe of the same
length whose cross-sectional area is A1 + A2.
Pump
(a) (b)
Pump
Cross-sectional area = A1
Cross-sectional area = A2
Cross-sectional area = A1 + A2
20.7 Parallel Wiring 567
In Example 10, the total power delivered by the receiver is the sum of the individual values
that were found in part (d), P = 4.50 W + 9.00 W = 13.5 W. Alternatively, the total power can be obtained from the equivalent resistance RP = 2.67 Ω and the total current in part (b):
P = I 2rmsRP = (2.25 A)2 (2.67 Ω) = 13.5 W (20.15b)
Problem-Solving Insight The total power delivered to any number of resistors in parallel is equal to the power delivered to the equivalent resistor.
*In reality, frequency-dependent characteristics (see Chapter 23) play a role in the operation of a loudspeaker. We
assume here, however, that the frequency of the sound is low enough that the speakers behave as pure resistances.
EXAMPLE 10 The Physics of Main and Remote Stereo Speakers
Most receivers allow the user to connect “remote” speakers (to play music in
another room, for instance) in addition to the main speakers. Figure 20.21 shows that the remote speaker and the main speaker for the right stereo
channel are connected to the receiver in parallel (for clarity, the speakers
for the left channel are not shown). At the instant represented in the picture,
the ac voltage across the speakers is 6.00 V. The main-speaker resistance
is 8.00 Ω, and the remote-speaker resistance is 4.00 Ω.* Determine (a) the equivalent resistance of the two speakers, (b) the total current supplied by the receiver, (c) the current in each speaker, and (d) the power dissipated in each speaker.
Reasoning The total current supplied to the two speakers by the receiver can be calculated as Irms = Vrms/RP, where RP is the equivalent resistance of the two speakers in parallel and can be obtained from 1/RP = 1/R1 + 1/R2. The current in each speaker is diff erent, however, since the speakers have
diff erent resistances. The average power delivered to a given speaker is
the product of its current and voltage. In the parallel connection the same
voltage is applied to each speaker.
Problem-Solving Insight The equivalent resistance RP of a number of resistors in parallel has a reciprocal given by RP−1 = R1−1 + R2−1 + R3−1 +. . ., where R1, R2, and R3 are the individual resistances. After adding together the reciprocals R1−1, R2−1, and R3−1, do not forget to take the reciprocal of the result to fi nd RP.
Solution (a) According to Equation 20.17, the equivalent resistance of the two speakers is given by
1
RP =
1
8.00 Ω +
1
4.00 Ω =
3
8.00 Ω or RP =
8.00 Ω
3 = 2.67 Ω
This result is illustrated in part b of the drawing. (b) Using the equivalent resistance in Ohm’s law shows that the total current is
Irms = Vrms RP
= 6.00 V
2.67 Ω = 2.25 A (20.14)
(c) Applying Ohm’s law to each speaker gives the individual speaker currents:
8.00-Ω speaker Irms = Vrms R
= 6.00 V
8.00 Ω = 0.750 A
4.00-Ω speaker Irms = Vrms R
= 6.00 V
4.00 Ω = 1.50 A
The sum of these currents is equal to the total current obtained in part (b).
(d) The average power dissipated in each speaker can be calculated using P = IrmsVrms with the individual currents obtained in part (c):
8.00-Ω speaker P = (0.750 A)(6.00 V) = 4.50 W (20.15a)
4.00-Ω speaker P = (1.50 A)(6.00 V) = 9.00 W (20.15a)
Is equivalent to
R2 = 4.00 Ω
Main speaker R1 = 8.00 Ω
Remote speaker R2 = 4.00 Ω
RP = 2.67 Ω
R1 = 8.00 Ω
6.00 V
6.00 V
(a) (b)
FIGURE 20.21 (a) The main and remote speakers in a stereo system are connected in parallel to the receiver. (b) The circuit schematic shows the situation when the ac voltage across the speakers is 6.00 V.
568 CHAPTER 20 Electric Circuits
In a parallel combination of resistances, it is the smallest resistance that has the largest impact in determining the equivalent resistance. In fact, if one resistance approaches zero, then
according to Equation 20.17, the equivalent resistance also approaches zero. In such a case, the
near-zero resistance is said to short out the other resistances by providing a near-zero resistance path for the current to follow as a shortcut around the other resistances.
An interesting application of parallel wiring occurs in a three-way light bulb, as Conceptual
Example 11 discusses.
50-W filament
100-W filament
Simplified version of 3-way switch in lamp socket
B
A
INTERACTIVE FIGURE 20.22 A three-way light bulb uses two connected fi laments. The
fi laments can be turned on one at a time or
both together in parallel.
CONCEPTUAL EXAMPLE 11 The Physics of a Three-Way Light Bulb
Three-way light bulbs are popular because they can provide three levels
of illumination (e.g., 50 W, 100 W, and 150 W) using a 120-V socket. The
socket, however, must be equipped with a special three-way switch that
enables one to select the illumination level. This switch does not select
diff erent voltages, because a three-way bulb uses a single voltage of 120 V.
Within the bulb are two separate fi laments. When the bulb is producing
its highest illumination level and one of the fi laments burns out (i.e., vapor-
izes), the bulb shines at one of the other illumination levels (either the
lowest or the intermediate one). When the bulb is set to its highest level
of illumination, how are the two fi laments connected, (a) in parallel or (b) in series?
Reasoning In a series connection, the fi laments would be connected in such a way that there is the same current through each one. The current
would enter one fi lament and then leave that fi lament and enter into the
other one. In a parallel connection, the same voltage would be applied
across each fi lament, but the current through each would, in general, be
diff erent, the two currents existing independently of one another.
Answer (b) is incorrect. If the fi laments were wired in series and one of them burned out, no current would pass through the bulb and none of
the illumination levels would be available, contrary to what is observed.
Therefore, the fi laments are not wired in series.
Answer (a) is correct. Since the fi laments are not in series, they must be in parallel, as Interactive Figure 20.22 helps to explain. The power dissipated in a resistance R is P = V2rms/R, according to Equation 20.15c. With a single value of 120 V for the voltage Vrms, three diff erent power ratings for the bulb can be obtained only if three diff erent values for the
resistance R are available. In a 50-W/100-W/150-W bulb, for example, one resistance R50 is provided by the 50-W fi lament, and the second resis- tance R100 comes from the 100-W fi lament. The third resistance R150 is the parallel combination of the other two and can be obtained from 1/R150 = 1/R50+1/R100. Interactive Figure 20.22 illustrates a simplifi ed version of
how the three-way switch operates in such a bulb. The fi rst position of the
switch closes contact A and leaves contact B open, energizing only the 50-W fi lament. The second position closes contact B and leaves contact A open, energizing only the 100-W fi lament. The third position closes both
contacts A and B, so that both fi laments light up to give the highest level of illumination.
Related Homework: Problem 51
Check Your Understanding
(The answers are given at the end of the book.) 13. A car has two headlights, and their power is derived from the car’s battery. The fi lament in one burns
out, but the other headlight stays on. Are the headlights connected in series or in parallel?
14. Two identical light bulbs are connected to identical batteries in two diff erent ways. In method A the bulbs are connected in parallel, and the parallel combination is connected between the one battery’s
terminals. In method B the bulbs are connected in series, and the series combination is connected be-
tween the other battery’s terminals. What is the ratio of the power supplied by the battery in method A
to the power supplied in method B? (a) 14 (b) 4 (c) 1
2 (d) 2 (e) 1
20.8 Circuits Wired Partially in Series and Partially in Parallel 569
20.8 Circuits Wired Partially in Series and Partially in Parallel Often an electric circuit is wired partially in series and partially in parallel. The key to determin-
ing the current, voltage, and power in such a case is to deal with the circuit in parts, with the
resistances in each part being either in series or in parallel with each other. Example 12 shows
how such an analysis is carried out.
110 Ω
180 Ω
220 Ω 24 V
A
B
250 Ω
110 Ω
180 Ω 470 Ω 24 V
A
B
110 Ω
180 Ω 470 Ω 24 V
A
B
110 Ω
130 Ω 24 V
A
B
110 Ω
130 Ω 24 V
A
B
240 Ω 24 V
(a)
(b)
(c)
+
–
+
–
+
–
+
–
+
–
+
–
FIGURE 20.23 The circuits shown in this picture are equivalent.
EXAMPLE 12 A Four-Resistor Circuit
Figure 20.23a shows a circuit composed of a 24-V battery and four resis- tors, whose resistances are 110, 180, 220, and 250 Ω. Find (a) the total current supplied by the battery and (b) the voltage between points A and B in the circuit.
Reasoning The total current that is supplied by the battery can be obtained from Ohm’s law, I = V/R, where R is the equivalent resistance of the four resistors. The equivalent resistance can be calculated by dealing
with the circuit in parts. The voltage VAB between the two points A and B is also given by Ohm’s law, VAB = IRAB, where I is the current and RAB is the equivalent resistance between the two points.
Solution (a) The 220-Ω resistor and the 250-Ω resistor are in series, so they are equivalent to a single resistor whose resistance is 220 Ω +
250 Ω = 470 Ω (see Figure 20.23a). The 470-Ω resistor is in parallel with the 180-Ω resistor. Their equivalent resistance can be obtained from
Equation 20.17:
1
RAB =
1
470 Ω +
1
180 Ω = 0.0077 Ω−1
RAB = 1
0.0077 Ω−1 = 130 Ω
The circuit is now equivalent to a circuit containing a 110-Ω resistor in
series with a 130-Ω resistor (see Figure 20.23b). This combination be- haves like a single resistor whose resistance is R = 110 Ω + 130 Ω = 240 Ω (see Figure 20.23c). The total current from the battery is, then,
I = V R
= 24 V
240 Ω = 0.10 A
(b) The current I = 0.10 A passes through the resistance between points A and B. Therefore, Ohm’s law indicates that the voltage across the 130-Ω resistor between points A and B is
VAB = IRAB = (0.10 A)(130 Ω) = 13 V
570 CHAPTER 20 Electric Circuits
Check Your Understanding
(The answers are given at the end of the book.) 15. In one of the circuits in CYU Figure 20.3 none of the resistors is in series or in parallel with any of the
other resistors. Which circuit is it?
(a) (b) (c)
CYU FIGURE 20.3
16. You have three resistors, each of which has a resistance R. By connecting all three together in various ways, which one or more of the following resistance values can you obtain? (a) 3R (b) 32 R (c) R (d)
2
3 R (e) 13 R
17. You have four resistors, each of which has a resistance R. It is possible to connect these four together so that the equivalent resistance of the combination is also R. How many ways can you do it? There is more than one way.
20.9 Internal Resistance So far, the circuits we have considered include batteries or generators that contribute only
their emfs to a circuit. In reality, however, such devices also add some resistance. This resis-
tance is called the internal resistance of the battery or generator because it is located inside the device. In a battery, the internal resistance is due to the chemicals within the battery. In a
generator, the internal resistance is the resistance of wires and other components within the
generator.
Figure 20.24 presents a schematic representation of the internal resistance r of a battery. The drawing emphasizes that when an external resistance R is connected to the battery, the resistance is connected in series with the internal resistance. The internal resistance of a functioning battery is typically small (several thousandths of an ohm for a new car battery). Nevertheless, the eff ect
of the internal resistance may not be negligible. Example 13 illustrates that when current is drawn
from a battery, the internal resistance causes the voltage between the terminals to drop below the
maximum value specifi ed by the battery’s emf. The actual voltage between the terminals of a
battery is known as the terminal voltage.
VInternal resistance
r
R R
+ –
Positive terminal of
battery
Negative terminal of
battery
+ –
FIGURE 20.24 When an external resistance R is connected between the terminals of a battery, the resis- tance is connected in series with the internal resistance r of the battery.
20.10 Kirchhoff ’s Rules 571
Example 13 indicates that the terminal voltage of a battery is smaller when the current drawn
from the battery is larger, an eff ect that any car owner can demonstrate. Turn the headlights on
before starting your car, so that the current through the battery is about 10 A, as in part (a) of
Example 13. Then start the car. The starter motor draws a large amount of additional current from
the battery, momentarily increasing the total current by an appreciable amount. Consequently, the
terminal voltage of the battery decreases, causing the headlights to become dimmer.
20.10 Kirchhoff ’s Rules Electric circuits that contain a number of resistors can often be analyzed by combining individual
groups of resistors in series and parallel, as Section 20.8 discusses. However, there are many cir-
cuits in which no two resistors are in series or in parallel. To deal with such circuits it is necessary
to employ methods other than the series–parallel method. One alternative is to take advantage
of Kirchhoff ’s rules, named after their developer Gustav Kirchhoff (1824–1887). There are two
rules, the junction rule and the loop rule, and both arise from principles and ideas that we have encountered earlier. The junction rule is an application of the law of conservation of electric
charge (see Section 18.2) to the electric current in a circuit. The loop rule is an application of the
principle of conservation of energy (see Section 6.8) to the electric potential (see Section 19.2)
that exists at various places in a circuit.
Figure 20.26 illustrates in greater detail the basic idea behind Kirchhoff ’s junction rule. The picture shows a junction where several wires are connected together. As Section 18.2 discusses,
electric charge is conserved. Therefore, since there is no accumulation of charges at the junction
itself, the total charge per second fl owing into the junction must equal the total charge per second
fl owing out of it. In other words, the junction rule states that the total current directed into a junction must equal the total current directed out of the junction, or 7 A = 5 A + 2 A for the specifi c case shown in the picture.
To car's electrical system (ignition, lights, radio, etc.)
12 Vr = 0.010 Ω
++
+ –
––
I
I
+
–
Positive terminal
Negative terminal
FIGURE 20.25 A car battery whose emf is 12 V and whose internal
resistance is r.
EXAMPLE 13 The Physics of Automobile Batteries
Figure 20.25 shows a car battery whose emf is 12.0 V and whose in- ternal resistance is 0.010 Ω. This resistance is relatively large because
the battery is old and the terminals are corroded. What is the terminal
voltage when the current I drawn from the battery is (a) 10.0 A and (b) 100.0 A?
Reasoning The voltage between the terminals is not the entire 12.0-V emf, because part of the emf is needed to make the current go through
the internal resistance. The amount of voltage needed can be determined
from Ohm’s law as the current I through the battery times the internal resistance r. For larger currents, a larger amount of voltage is needed, leaving less of the emf between the terminals.
Solution (a) The voltage needed to make a current of I = 10.0 A go through an internal resistance of r = 0.010 Ω is
V = Ir = (10.0 A)(0.010 Ω) = 0.10 V
To fi nd the terminal voltage, remember that the direction of convention-
al current is always from a higher toward a lower potential. To empha-
size this fact in the drawing, plus and minus signs have been included
at the right and left ends, respectively, of the resistance r. The terminal voltage can be calculated by starting at the negative terminal and keep-
ing track of how the voltage increases and decreases as we move toward
the positive terminal. The voltage rises by 12.0 V due to the battery’s
emf. However, the voltage drops by 0.10 V because of the potential dif-
ference across the internal resistance. Therefore, the terminal voltage is
12.0 V − 0.10 V = 11.9 V .
(b) When the current through the battery is 100.0 A, the voltage needed to make the current go through the internal resistance is
V = Ir = (100.0 A)(0.010 Ω) = 1.0 V
The terminal voltage now decreases to 12.0 V − 1.0 V = 11.0 V .
Junction
5 A
2 A
7 A
FIGURE 20.26 A junction is a point in a circuit where a number of wires are connected
together. If 7 A of current is directed into the
junction, then a total of 7 A (5 A + 2 A) of
current must be directed out of the junction.
572 CHAPTER 20 Electric Circuits
To help explain Kirchhoff ’s loop rule, Figure 20.27 shows a circuit in which a 12-V battery is connected to a series combination of a 5-Ω and a 1-Ω resistor. The plus and minus signs associ-
ated with each resistor remind us that, outside a battery, conventional current is directed from a
higher toward a lower potential. From left to right, there is a potential drop of 10 V across the fi rst
resistor and another drop of 2 V across the second resistor. Keeping in mind that potential is the
electric potential energy per unit charge, let us follow a positive test charge clockwise* around the
circuit. Starting at the negative terminal of the battery, we see that the test charge gains potential
energy because of the 12-V rise in potential due to the battery. The test charge then loses potential
energy because of the 10-V and 2-V drops in potential across the resistors, ultimately arriving
back at the negative terminal. In traversing the closed-circuit loop, the test charge is like a skier
gaining gravitational potential energy in going up a hill on a chair lift and then losing it to friction
in coming down and stopping. When the skier returns to the starting point, the gain equals the
loss, so there is no net change in potential energy. Similarly, when the test charge arrives back at
its starting point, there is no net change in electric potential energy, the gains matching the losses.
The loop rule expresses this example of energy conservation in terms of the electric potential and states that for a closed-circuit loop, the total of all the potential drops is the same as the total of all the potential rises, or 10 V + 2 V = 12 V for the specifi c case in Figure 20.27.
Kirchhoff ’s rules can be applied to any circuit, even when the resistors are not in series
or in parallel. The two rules are summarized below, and Examples 14 and 15 illustrate how to
use them.
KIRCHHOFF’S RULES Junction rule. The sum of the magnitudes of the currents directed into a junction equals the sum of the magnitudes of the currents directed out of the junction. Loop rule. Around any closed-circuit loop, the sum of the potential drops equals the sum of the potential rises.
+ 5 Ω
10 V
1 Ω – + –
+ –
2 V
12 V
2 A
FIGURE 20.27 Following a positive test charge clockwise around the circuit, we see
that the total voltage drop of 10 V + 2 V
across the two resistors equals the voltage
rise of 12 V due to the battery. The plus and
minus signs on the resistors emphasize that,
outside a battery, conventional current is
directed from a higher potential (+) toward a
lower potential (−).
*The choice of the clockwise direction is arbitrary.
EXAMPLE 14 Using Kirchhoff ’s Loop Rule
Figure 20.28 shows a circuit that contains two batteries and two resistors. Determine the current I in the circuit.
Reasoning The fi rst step is to draw the current, which we have chosen to be clockwise around the circuit. The choice of direction is arbitrary, and if it is incorrect, I will turn out to be negative.
The second step is to mark the resistors with plus and minus signs,
which serve as an aid in identifying the potential drops and rises for
Kirchhoff ’s loop rule.
Problem-Solving Insight Remember that, outside a battery, conventional current is always directed from a higher poten- tial (+) toward a lower potential (−).
Thus, we must mark the resistors as indicated in Figure 20.28, to be con- sistent with the clockwise direction chosen for the current.
We may now apply Kirchhoff ’s loop rule to the circuit, starting at
corner A, proceeding clockwise around the loop, and identifying the po- tential drops and rises as we go. The potential across each resistor is given
by Ohm’s law as V = IR. The clockwise direction is arbitrary, and the same result is obtained with a counterclockwise path.
Solution Starting at corner A and moving clockwise around the loop, there is
1. A potential drop (+ to −) of IR = I(12 Ω) across the 12-Ω resistor 2. A potential drop (+ to −) of 6.0 V across the 6.0-V battery
3. A potential drop (+ to −) of IR = I(8.0 Ω) across the 8.0-Ω resistor 4. A potential rise (− to +) of 24 V across the 24-V battery
Setting the sum of the potential drops equal to the sum of the potential
rises, as required by Kirchhoff ’s loop rule, gives
I (12 Ω) + 6.0 V + I (8.0 Ω) = 24 V
Solving this equation for the current yields I = 0.90 A . The current is a positive number, indicating that our initial choice for the direction (clock-
wise) of the current was correct.
Potential drops
⏟⎵⎵⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⎵⎵⏟ {
Potential rises
+
12 Ω
I
I
A –
– ++ –
24 V
+ –
6.0 V
8.0 Ω
FIGURE 20.28 A single-loop circuit that contains two batteries and two resistors.
20.10 Kirchhoff ’s Rules 573
EXAMPLE 15 The Physics of an Automobile Electrical System
In a car, the headlights are connected to the battery and would discharge
the battery if it were not for the alternator, which is run by the engine.
Interactive Figure 20.29 indicates how the car battery, headlights, and alternator are connected. The circuit includes an internal resistance of
0.0100 Ω for the car battery and its leads and a resistance of 1.20 Ω for
the headlights. For the sake of simplicity, the alternator is approximated
as an additional 14.00-V battery with an internal resistance of 0.100 Ω.
Determine the currents through the car battery (IB), the headlights (IH), and the alternator (IA).
Reasoning The drawing shows the directions chosen arbitrarily for the currents IB, IH, and IA. If any direction is incorrect, the analysis will reveal a negative value for the corresponding current.
Next, we mark the resistors with the plus and minus signs that serve
as an aid in identifying the potential drops and rises for the loop rule,
recalling that, outside a battery, conventional current is always directed
from a higher potential (+) toward a lower potential (−). Thus, given the
directions selected for IB, IH, and IA, the plus and minus signs must be those indicated in Interactive Figure 20.29.
Kirchhoff ’s junction and loop rules can now be used.
Problem-Solving Insight In problems involving Kirchhoff ’s rules, it is always helpful to mark the resistors with plus and minus signs to keep track of the potential rises and drops in the circuit.
Solution The junction rule can be applied to junction B or junction E to give the same result:
Junction rule applied at B
IA + IB = IH
In applying the loop rule to the lower loop BEFA, we start at point B, move clockwise around the loop, and identify the potential drops and rises.
There is a potential rise (− to +) of IB (0.0100 Ω) across the 0.0100-Ω resistor and then a drop (+ to −) of 12.00 V due to the car battery. Con-
tinuing around the loop, we fi nd a 14.00-V rise (− to +) across the alter-
nator, followed by a potential drop (+ to −) of IA (0.100 Ω) across the 0.100-Ω resistor. Setting the sum of the potential drops equal to the sum
of the potential rises gives the following result:
Loop rule: BEFA IA(0.100 Ω) + 12.00 V = IB(0.0100 Ω) + 14.00 V
Since there are three unknown variables in this problem, IB, IH, and IA, a third equation is needed for a solution. To obtain the third equation, we apply the loop rule to the upper loop CDEB, choosing a clockwise path for convenience. The result is
Loop rule: CDEB IB(0.0100 Ω) + IH(1.20 Ω) = 12.00 V
These three equations can be solved simultaneously to show that
IA = 19.1 A, IB = −9.0 A, IH = 10.1 A
The negative answer for IB indicates that the current through the battery is not directed from right to left, as drawn in Interactive Figure 20.29. Instead, the 9.0-A current is directed from left to right, opposite to the
way current would be directed if the alternator were not connected. It is
Into
junction
{ {
Out of
junction
⏟⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⏟ Potential drops
⏟⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⏟ Potential rises
⏟⎵⎵⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⎵⎵⏟ Potential drops Potential rises
{
+ –
Alternator 14.00 V 0.100 Ω
Headlights 1.20 Ω
Battery 12.00 V, 0.0100 Ω
+ –
–
0.100 Ω A F
+ + –
14.00 V
– 0.0100 Ω
B E + + –
12.00 V
+ 1.20 Ω
C D –
IA
IH
IB
INTERACTIVE FIGURE 20.29 A circuit showing the headlight(s), battery, and alternator of a car.
Math Skills The three equations that must be solved simultane- ously for IA, IB, and IH are
IA + IB = IH (1)
IA(0.100) + 12.00 = IB (0.0100) + 14.00 (2)
IB (0.0100) + IH (1.20) = 12.00 (3)
For clarity, units have been omitted. Substituting Equation 1 for IH into Equation 3 gives
IB(0.0100) + (IA + IB)(1.20) = 12.00 or
IB (1.21) + IA(1.20) = 12.00 (4)
Solving Equation 4 for IB shows that
IB = 12.00 − IA(1.20)
1.21 = 9.92 − IA(0.992) (5)
Substituting Equation 5 for IB into Equation 2, we fi nd that
IA(0.100) + 12.00 = [ 9.92 − IA(0.992)](0.0100) + 14.00
This result contains only the unknown variable IA and can be solved to show that IA = 19.1 A . Using this value for IA in Equation 5 reveals that
IB = 9.92 − (19.1)(0.992) = −9.0 A
Finally, substituting the values for both IA and IB into Equation 1 yields
IH = 19.1 + (−9.0) = 10.1 A
{ IH
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟ IB
{
IA
{
IB
{
IA
the left-to-right current created by the alternator that keeps the battery
charged.
Note that we can check our results by applying Kirchhoff ’s loop rule
to the outer loop ABCDEF. If our results are correct, then the sum of the potential drops around this loop will be equal to the sum of the potential
rises.
574 CHAPTER 20 Electric Circuits
REASONING STRATEGY Applying Kirchhoff ’s Rules 1. Draw the current in each branch of the circuit. Choose any direction. If your choice is
incorrect, the value obtained for the current will turn out to be a negative number. 2. Mark each resistor with a plus sign at one end and a minus sign at the other end, in a way
that is consistent with your choice for the current direction in Step 1. Outside a battery, conventional current is always directed from a higher potential (the end marked +) toward a lower potential (the end marked −).
3. Apply the junction rule and the loop rule to the circuit, obtaining in the process as many independent equations as there are unknown variables.
4. Solve the equations obtained in Step 3 simultaneously for the unknown variables. (See Appendix C.3.)
Check Your Understanding
(The answer is given at the end of the book.) 18. CYU Figure 20.4 shows a circuit containing three resistors and three
batteries. In preparation for applying Kirchhoff ’s rules, the currents
in each resistor have been drawn. For these currents, write down the
equations that result from applying Kirchhoff ’s junction rule and loop
rule. Apply the loop rule to loops ABCD and BEFC.
20.11 The Measurement of Current and Voltage Current and voltage can be measured with devices known, respectively, as ammeters and voltme-
ters. There are two types of such devices: those that use digital electronics and those that do not.
The essential feature of nondigital devices is the dc galvanometer. As Figure 20.30a illustrates, a galvanometer consists of a magnet, a coil of wire, a spring, a pointer, and a calibrated scale. The
coil is mounted so that it can rotate, which causes the pointer to move in relation to the scale. The
coil rotates in response to the torque applied by the magnet when there is a current in the coil
(see Section 21.6). The coil stops rotating when this torque is balanced by the torque of the spring.
Two characteristics of a galvanometer are important when it is used as part of a measurement
device. First, the amount of dc current that causes full-scale defl ection of the pointer indicates the
sensitivity of the galvanometer. For instance, Figure 20.30a shows an instrument that defl ects full scale when the current in the coil is 0.10 mA. The second important characteristic is the resis-
tance RC of the wire in the coil. Figure 20.30b shows how a galvanometer with a coil resistance of RC is represented in a circuit diagram.
THE PHYSICS OF . . . an ammeter. Since an ammeter is an instrument that measures cur- rent, it must be inserted in the circuit so the current passes directly through it, as Figure 20.31 shows. (This is true for both digital and nondigital ammeters; Figure 20.31 shows a digital instrument.)
A nondigital ammeter includes a galvanometer and one or more shunt resistors, which are connected in parallel with the galvanometer and provide a bypass for current in excess of the
galvanometer’s full-scale limit. The bypass allows the ammeter to be used to measure a current
exceeding the full-scale limit. In Figure 20.32, for instance, a current of 60.0 mA enters terminal A of an ammeter (nondigital), which uses a galvanometer with a full-scale current of 0.100 mA. The shunt resistor R can be selected so that 0.100 mA of current enters the galvanometer, while 59.9 mA bypasses it. In such a case, the measurement scale on the ammeter would be labeled 0
to 60.0 mA. To determine the shunt resistance, it is necessary to know the coil resistance RC (see Problem 115).
3.0 V
B
C
A
D
E
F
+
–
+ –
5.0 V
7.0 V
+ –
R1
I1
I3
R2
R3
I2
CYU FIGURE 20.4
North pole of magnet
Calibrated scale
0 mA
Spring
Coil
0.10 mA
I = 0.10 mA
N South pole of magnet
S
(a)
(b)
RC
I I
G
FIGURE 20.30 (a) A dc galvanometer. The coil of wire and pointer rotate when there
is a current in the wire. (b) A galvanometer with a coil resistance of RC is represented in a circuit diagram as shown here.
20.12 Capacitors in Series and in Parallel 575
When an ammeter is inserted into a circuit, the equivalent resistance of the ammeter adds to
the circuit resistance. Any increase in circuit resistance causes a reduction in current, and this is a
problem, because an ammeter should only measure the current, not change it. Therefore, an ideal ammeter would have zero resistance. In practice, a good ammeter is designed with an equivalent
resistance small enough so there is only a negligible reduction of the current in the circuit when
the ammeter is inserted.
THE PHYSICS OF . . . a voltmeter. A voltmeter is an instrument that measures the voltage between two points, A and B, in a circuit. Figure 20.33 shows that the voltmeter must be connected between the points and is not inserted into the circuit as an ammeter is. (This is true for both digital and nondigital voltmeters; Figure 20.33 shows a digital instrument.)
A nondigital voltmeter includes a galvanometer whose scale is calibrated in volts. Suppose,
for instance, that the galvanometer in Figure 20.34 has a full-scale current of 0.1 mA and a coil resistance of 50 Ω. Under full-scale conditions, the voltage across the coil would, therefore, be
V = IRC = (0.1 × 10−3 A)(50 Ω) = 0.005 V. Thus, this galvanometer could be used to register volt- ages in the range 0−0.005 V. A nondigital voltmeter, then, is a galvanometer used in this fashion,
along with some provision for adjusting the range of voltages to be measured. To adjust the range,
an additional resistance R is connected in series with the coil resistance RC (see Problem 88). Ideally, the voltage registered by a voltmeter should be the same as the voltage that exists
when the voltmeter is not connected. However, a voltmeter takes some current from a circuit and,
thus, alters the circuit voltage to some extent. An ideal voltmeter would have infi nite resistance and would draw away only an infi nitesimal amount of current. In reality, a good voltmeter is
designed with a resistance that is large enough so the unit does not appreciably alter the voltage
in the circuit to which it is connected.
Check Your Understanding
(The answers are given at the end of the book.) 19. An ideal ammeter has _________ resistance, whereas an ideal voltmeter has ________ resistance.
(a) zero, zero (b) infi nite, infi nite (c) zero, infi nite (d) infi nite, zero 20. What would happen to the current in a circuit if a voltmeter, inadvertently mistaken for an ammeter,
were inserted into the circuit? The current would (a) increase markedly (b) decrease markedly (c) remain the same.
20.12 Capacitors in Series and in Parallel Figure 20.35 shows two diff erent capacitors connected in parallel to a battery. Since the capaci- tors are in parallel, they have the same voltage V across their plates. However, the capacitors contain diff erent amounts of charge. The charge stored by a capacitor is q = CV (Equation 19.8), so q1 = C1V and q2 = C2V.
Digital ammeter
ICurrent I
+ –
FIGURE 20.31 An ammeter must be inserted into a circuit so that the current passes directly
through it.
+ –
Digital voltmeter
A
Voltage between points
A and B
B
FIGURE 20.33 To measure the voltage between two points A and B in a circuit, a voltmeter is connected between the points.
Nondigital ammeter
A
A
B
B
RC
0.100 mA
60.0 mA
60.0 mA
59.9 mA
Shunt resistor
R
G
FIGURE 20.32 If a galvanometer with a full- scale limit of 0.100 mA is to be used to measure
a current of 60.0 mA, a shunt resistance R must be used, so the excess current of 59.9 mA
can detour around the galvanometer coil.
RC = 50 Ω
0.1 mA
0.005 V
G
FIGURE 20.34 The galvanometer shown has a full-scale defl ection of 0.1 mA and a
coil resistance of 50 Ω.
576 CHAPTER 20 Electric Circuits
As with resistors, it is always possible to replace a parallel combination of capacitors with an
equivalent capacitor that stores the same charge and energy for a given voltage as the combina- tion does. To determine the equivalent capacitance CP, note that the total charge q stored by the two capacitors is
q = q1 + q2 = C1V + C2V = (C1 + C2 )V = CPV
This result indicates that two capacitors in parallel can be replaced by an equivalent capacitor
whose capacitance is CP = C1 + C2. For any number of capacitors in parallel, the equivalent capacitance is
Parallel capacitors CP = C1 + C 2 + C3 + ⋅ ⋅ ⋅ (20.18)
Capacitances in parallel simply add together to give an equivalent capacitance. This behavior
contrasts with that of resistors in parallel, which combine as reciprocals, according to Equation
20.17. The reason for this diff erence is that the charge q on a capacitor is directly proportional to the capacitance C (q = CV), whereas the current I in a resistor is inversely proportional to the resistance R (I = V/R).
The equivalent capacitor not only stores the same amount of charge as the parallel combination
of capacitors, but also stores the same amount of energy. For instance, the energy stored in a single
capacitor is 1
2 CV 2 (Equation 19.11b), so the total energy stored by two capacitors in parallel is
Total energy = 1
2 C1V 2 + 1
2 C 2V 2 = 1
2 (C1 + C 2)V 2 = 1
2 CPV 2
which is equal to the energy stored in the equivalent capacitor CP. When capacitors are connected in series, the equivalent capacitance is diff erent from when
they are in parallel. As an example, Figure 20.36 shows two capacitors in series and reveals the following important fact.
Problem-Solving Insight All capacitors in series, regardless of their capacitances, contain charges of the same magnitude, +q and −q, on their plates.
The battery places a charge of +q on plate a of capacitor C1, and this charge induces a charge of +q to depart from the opposite plate aʹ, leaving behind a charge −q. The +q charge that leaves plate aʹ is deposited on plate b of capacitor C2 (since these two plates are connected by a wire),
+ –
V
C1
C2
+ q2 – q2
+ q1 – q1
+ –
V
CP
+ q1 + q2
Is equivalent to
– q1 – q2
FIGURE 20.35 In a parallel combination of capacitances C1 and C2, the voltage V across each capacitor is the same, but the charges q1 and q2 on each capacitor are diff erent.
+ –
V
C1
V1
a a′ b b′
+ q – q
C2
+ q – q
CS
+ q – q
+ –
V
Is equivalent to
V2
FIGURE 20.36 In a series combination of capacitances C1 and C2, the same amount of charge q is on the plates of each capacitor, but the voltages V1 and V2 across each capacitor are diff erent.
20.13 RC Circuits 577
where it induces a +q charge to move away from the opposite plate bʹ, leaving behind a charge of −q. Thus, all capacitors in series contain charges of the same magnitude on their plates. Note the diff erence between charging capacitors in parallel and in series. When charging parallel capaci-
tors, the battery moves a charge q that is the sum of the charges moved for each of the capacitors: q = q1 + q2 + q3 + . . . . In contrast, when charging a series combination of n capacitors, the bat- tery only moves a charge q, not nq, because the charge q passes by induction from one capacitor directly to the next one in line.
The equivalent capacitance CS for the series connection in Figure 20.36 can be determined by observing that the battery voltage V is shared by the two capacitors. The drawing indicates that the voltages across C1 and C2 are V1 and V2, so that V = V1 + V2. Since the voltages across the capacitors are V1 = q/C1 and V2 = q/C2, we fi nd that
V = V1 + V2 = q C1
+ q
C2 = q( 1C1 +
1
C2) = q( 1
CS) Thus, two capacitors in series can be replaced by an equivalent capacitor, which has a capacitance
CS that can be obtained from 1/CS = 1/C1 + 1/C2. For any number of capacitors connected in series the equivalent capacitance is given by
Series capacitors 1
CS =
1
C1 +
1
C2 +
1
C3 + ⋅ ⋅ ⋅ (20.19)
Equation 20.19 indicates that capacitances in series combine as reciprocals and do not simply add
together as resistors in series do. It is left as an exercise (Problem 99) to show that the equivalent
series capacitance stores the same electrostatic energy as the sum of the energies of the individual
capacitors.
It is possible to simplify circuits containing a number of capacitors in the same general
fashion as that outlined for resistors in Example 12 and Figure 20.23. The capacitors in a parallel grouping can be combined according to Equation 20.18, and those in a series grouping can be
combined according to Equation 20.19.
20.13 RC Circuits Many electric circuits contain both resistors and capacitors. Figure 20.37 illustrates an example of a resistor–capacitor circuit, or RC circuit. Part a of the drawing shows the circuit at a time t after the switch has been closed and the battery has begun to charge up the capacitor plates. The
charge on the plates builds up gradually to its equilibrium value of q0 = CV0, where V0 is the volt- age of the battery. Assuming that the capacitor is uncharged at time t = 0 s when the switch is closed, it can be shown that the magnitude q of the charge on the plates at time t is
Capacitor charging q = q 0 [1 − e−t /(RC )] (20.20)
FIGURE 20.37 Charging a capacitor.
q0 = CV0 q
t
(a)
V0
(b)
C
Switch
I
R
+ q – q
+ –
Math Skills If the need arises, you can solve Equation 20.20 for the time t with the aid of natural logarithms. The fi rst step is to rearrange the equation so as to isolate the exponential e on one side of the equals sign:
q = q 0[1 − e−t/(RC ) ] or q
q 0 = 1 − e−t / (RC ) or 1 −
q q 0
= e−t /(RC )
According to Equation D-9 in Appendix D, the natural logarithm of eZ is ln eZ = Z. Therefore, we can take the natural logarithm of both sides of the rearranged equation and obtain
ln (1 − q q 0) = ln e−t/(RC ) = −
t RC or t = −RC [ ln (1 −
q q 0)]
To illustrate this result, suppose that RC = 5.00 s and that the capacitor has acquired a charge q that is one-fourth of its fi nal equilibrium value q0, so that q = 0.250 q0. The time required for the capacitor to acquire the charge is
t = −(5.00 s) [ ln (1 − 0.250 q 0
q 0 )] = −(5.00 s) ln 0.750 = −(5.00 s)(−0.288) = 1.44 s
578 CHAPTER 20 Electric Circuits
where the exponential e has the value of 2.718. . . . Part b of the drawing shows a graph of this expression, which indicates that the charge is q = 0 C when t = 0 s and increases gradually toward the equilibrium value of q0 = CV0. The voltage V across the capacitor at any time can be obtained from Equation 20.20 by dividing the charges q and q0 by the capacitance C, since V = q/C and V0 = q0/C.
The term RC in the exponent in Equation 20.20 is called the time constant 𝜏 of the circuit:
τ = RC (20.21)
The time constant is measured in seconds; verifi cation of the fact that an ohm times a farad is
equivalent to a second is left as an exercise (see Check Your Understanding Question 21). The
time constant is the amount of time required for the capacitor to accumulate 63.2% of its equilib-
rium charge, as can be seen by substituting t = 𝜏 = RC in Equation 20.20; q0(1 − e−1) = q0(0.632). The charge approaches its equilibrium value rapidly when the time constant is small and slowly
when the time constant is large.
Figure 20.38a shows a circuit at a time t after a switch is closed to allow a charged capaci- tor to begin discharging. There is no battery in this circuit, so the charge +q on the left plate of the capacitor can fl ow counterclockwise through the resistor and neutralize the charge −q on the right plate. Assuming that the capacitor has a charge q0 at time t = 0 s when the switch is closed, it can be shown that
Capacitor discharging q = q 0 e−t /(RC ) (20.22)
where q is the amount of charge remaining on either plate at time t. The graph of this expression in part b of the drawing shows that the charge begins at q0 when t = 0 s and decreases gradually toward zero. Smaller values of the time constant RC lead to a more rapid discharge. Equation 20.22 indicates that when t = 𝜏 = RC, the magnitude of the charge remaining on each plate is q0e−1 = q0(0.368). Therefore, the time constant is also the amount of time required for a charged capacitor to lose 63.2% of its charge.
BIO THE PHYSICS OF . . . heart pacemakers. The charging/discharging of a capacitor has many applications. Heart pacemakers, for instance, incorporate RC circuits to control the tim- ing of voltage pulses that are delivered to a malfunctioning heart to regulate its beating cycle. The
pulses are delivered by electrodes attached externally to the chest or located internally near the
heart when the pacemaker is implanted surgically (see Figure 20.39). A voltage pulse is deliv- ered when the capacitor discharges to a preset level, following which the capacitor is recharged
rapidly and the cycle repeats. The value of the time constant RC controls the pulsing rate, which is about once per second.
THE PHYSICS OF . . . windshield wipers. The charging/discharging of a capacitor is also used in automobiles that have windshield wipers equipped for intermittent operation dur-
ing a light drizzle. In this mode of operation, the wipers remain off for a while and then turn on
briefl y. The timing of the on–off cycle is determined by the time constant of a resistor–capacitor
combination.
Check Your Understanding
(The answers are given at the end of the book.) 21. The time constant 𝜏 of a series RC circuit is measured in seconds (s)
and is given by 𝜏 = RC, where the resistance R is measured in ohms (Ω) and the capacitance C is measured in farads (F). Verify that an ohm times a farad is equivalent to a second.
22. CYU Figure 20.5 shows two diff erent resistor–capacitor arrange- ments. The time constant for arrangement A is 0.20 s. What is the time
constant for arrangement B? (a) 0.050 s (b) 0.10 s (c) 0.20 s (d) 0.40 s (e) 0.80 s
q0 q
t
(a)
(b)
C
Switch
I
R
+ q – q
FIGURE 20.38 Discharging a capacitor.
FIGURE 20.39 This color-enhanced frontal X-ray photograph of a human chest shows an
enlarged heart and a heart pacemaker that has
been implanted surgically.
PacemakerHeartElectrical wire
L iv
in g A
rt E
n te
rp ri
se s,
L L
C /S
ci en
ce S
o u rc
e
B
C
C
R
A
C CR
CYU FIGURE 20.5
20.14 Safety and the Physiological Eff ects of Current 579
20.14 Safety and the Physiological Eff ects of Current Electric circuits, although very useful, can also be hazardous. To reduce the danger inherent in using circuits, proper electrical grounding is necessary. The next two fi gures help to illustrate what electrical grounding means and how it is achieved.
Figure 20.40a shows a clothes dryer connected to a wall socket via a two-prong plug. The dryer is operating normally; that is, the wires inside are insulated from the metal casing of the
dryer, so no charge fl ows through the casing itself. Notice that one terminal of the ac generator
is customarily connected to ground by the electric power company. Part b of the drawing shows the hazardous result that occurs if a wire comes loose and contacts the metal casing. A
person touching it receives a shock, since electric charge fl ows through the casing, the person’s
body, and the ground on the way back to the generator.
THE PHYSICS OF . . . safe electrical grounding. Figure 20.41 shows the same appli- ance connected to a wall socket via a three-prong plug that provides safe electrical grounding.
The third prong connects the metal casing directly to a copper rod driven into the ground or to a
copper water pipe that is in the ground. This arrangement protects against electrical shock in the
event that a broken wire touches the metal casing. In this event, charge would fl ow through the
casing, through the third prong, and into the ground, returning eventually to the generator. No
charge would fl ow through the person’s body, because the copper rod provides much less electri-
cal resistance than does the body.
BIO THE PHYSICS OF . . . the physiological eff ects of current. Serious and some- times fatal injuries can result from electrical shock. The severity of the injury depends on the
magnitude of the current and the parts of the body through which the moving charges pass. The
amount of current that causes a mild tingling sensation is about 0.001 A. Currents on the order of
0.01–0.02 A can lead to muscle spasms, in which a person “can’t let go” of the object causing the
shock. Currents of approximately 0.2 A are potentially fatal because they can make the heart fi bril-
late, or beat in an uncontrolled manner. Substantially larger currents stop the heart completely.
However, since the heart often begins beating normally again after the current ceases, the larger
currents can be less dangerous than the smaller currents that cause fi brillation.
Two-prong plug
Ground
(a)
Heater
(b)
Wire touches metal
casing
FIGURE 20.40 (a) A normally operating clothes dryer that is connected to a wall socket via a two-prong plug. (b) An internal wire accidentally touches the metal casing, and a person who touches the casing receives an electrical shock.
Wire touches metal
casing
Three-prong plug
Ground Copper rod Third prong connected to casing
FIGURE 20.41 A safely connected dryer. If the dryer malfunctions, a
person touching it receives no shock,
since electric charge fl ows through
the third prong and into the ground
via a copper rod, rather than through
the person’s body.
580 CHAPTER 20 Electric Circuits
EXAMPLE 16 BIO The Physics of Pacemakers
As mentioned previously in this chapter, a pacemaker sends an electrical
pulse to a patient’s heart each time a capacitor in the pacemaker discharges,
thereby regulating the beating cycle. One particular pacemaker uses an RC circuit that discharges when the charge on the capacitor reaches 75% of
its equilibrium charge value. If this occurs every 1.2 seconds, and the ca-
pacitance of the RC circuit is 110 μF, what is the resistance of the resistor?
Reasoning To calculate the resistance of the RC circuit we can use Equation 20.20, which is the charging equation for the capacitor in the
circuit.
Solution Beginning with Equation 20.20, we have: Q = Q0[1 − e−t /(RC )]. We rearrange this equation to solve for the resistance:
⇒ e−t /(RC ) = 1 − Q Q0
⇒ −t RC
= in(1 − Q Q0) ⇒ R =
−t
C in(1 − Q Q0)
.
We can now substitute in the values given in the problem:
R = −1.2 s
(110 × 10−6 F) in(1 − 0.75) = 7870 Ω
Concept Summary 20.1 Electromotive Force and Current There must be at least one source or generator of electrical energy in an electric circuit. The electro-
motive force (emf) of a generator, such as a battery, is the maximum potential
diff erence (in volts) that exists between the terminals of the generator.
The rate of fl ow of charge is called the electric current. If the rate is con-
stant, the current I is given by Equation 20.1, where ∆q is the magnitude of the charge crossing a surface in a time Δt, the surface being perpendicular to the motion of the charge. The SI unit for current is the coulomb per second
(C/s), which is referred to as an ampere (A). When the charges fl ow only in
one direction around a circuit, the current is called direct current (dc). When
the direction of charge fl ow changes from moment to moment, the current is
known as alternating current (ac). Conventional current is the hypothetical
fl ow of positive charges that would have the same eff ect in a circuit as the
movement of negative charges that actually does occur.
I = ∆q ∆t
(20.1)
20.2 Ohm’s Law The defi nition of electrical resistance R is R = V/I, where V (in volts) is the voltage applied across a piece of material and I (in amperes) is the current through the material. Resistance is measured in volts
per ampere, a unit called an ohm (Ω). If the ratio of the voltage to the current
is constant for all values of voltage and current, the resistance is constant. In
this event, the defi nition of resistance becomes Ohm’s law, Equation 20.2.
V I
= R = constant or V = IR (20.2)
20.3 Resistance and Resistivity The resistance of a piece of material of length L and cross-sectional area A is given by Equation 20.3, where 𝜌 is the resistivity of the material. The resistivity of a material depends on the tem-
perature. For many materials and limited temperature ranges, the temperature
dependence is given by Equation 20.4, where 𝜌 and 𝜌0 are the resistivities at
the temperatures T and T0, respectively, and 𝛼 is the temperature coeffi cient of resistivity. The temperature dependence of the resistance R is given by Equation 20.5, where R and R0 are the resistances at the temperatures T and T0, respectively.
R = ρ L A
(20.3)
ρ = ρ0[1 + α(T − T0) ] (20.4)
R = R0[1 + α(T − T0) ] (20.5)
20.4 Electric Power When electric charge fl ows from point A to point B in a circuit, leading to a current I, and the voltage between the points is V, the
electric power associated with this current and voltage is given by Equation
20.6a. For a resistor, Ohm’s law applies, and it follows that the power
delivered to the resistor is also given by either Equation 20.6b or 20.6c.
P = IV (20.6a)
P = I 2R (20.6b)
P = V 2
R (20.6c)
20.5 Alternating Current The alternating voltage between the terminals of an ac generator can be represented by Equation 20.7, where V0 is the peak value of the voltage, t is the time, and f is the frequency (in hertz) at which the voltage oscillates. Correspondingly, in a circuit containing only resistance,
the ac current is given by Equation 20.8, where I0 is the peak value of the current and is related to the peak voltage via I0 = V0/R.
V = V0 sin 2πft (20.7)
I = I0 sin 2πft (20.8)
For sinusoidal current and voltage, the root mean square (rms) current and
voltage are related to the peak values according to Equations 20.12 and 20.13.
Irms = I0
√2 (20.12)
Vrms = V0 √2
(20.13)
The power in an ac circuit is the product of the current and the voltage
and oscillates in time. The average power is given by Equation 20.15a. For a
resistor, Ohm’s law applies, so that Vrms = IrmsR, and the average power deliv- ered to the resistor is also given by Equations 20.15b and 20.15c.
P = IrmsVrms (20.15a)
P = I rms 2 R (20.15b)
P = V rms 2
R (20.15c)
20.6 Series Wiring When devices are connected in series, there is the same current through each device. The equivalent resistance RS of a series combination of resistances (R1, R2, R3, etc.) is given by Equation 20.16. The power delivered to the equivalent resistance is equal to the total power de-
livered to any number of resistors in series.
RS = R1 + R2 + R3 + . . . (20.16)
Focus on Concepts 581
20.7 Parallel Wiring When devices are connected in parallel, the same voltage is applied across each device. In general, devices wired in parallel
carry diff erent currents. The reciprocal of the equivalent resistance RP of a parallel combination of resistances (R1, R2, R3, etc.) is given by Equation 20.17. The power delivered to the equivalent resistance is equal to the total
power delivered to any number of resistors in parallel.
1
RP =
1
R1 +
1
R2 +
1
R3 + ⋅ ⋅ ⋅ (20.17)
20.8 Circuits Wired Partially in Series and Partially in Parallel Sometimes, one section of a circuit is wired in series, while another is wired
in parallel. In such cases the circuit can be analyzed in parts, according to the
respective series and parallel equivalent resistances of the various sections.
20.9 Internal Resistance The internal resistance of a battery or gener- ator is the resistance within the battery or generator. The terminal voltage
is the voltage between the terminals of a battery or generator and is equal to
the emf only when there is no current through the device. When there is a
current I, the internal resistance r causes the terminal voltage to be less than the emf by an amount Ir.
20.10 Kirchhoff ’s Rules Kirchhoff ’s junction rule states that the sum of the magnitudes of the currents directed into a junction equals the sum of the
magnitudes of the currents directed out of the junction. Kirchhoff ’s loop rule
states that, around any closed-circuit loop, the sum of the potential drops
equals the sum of the potential rises. The Reasoning Strategy given at the
end of Section 20.10 explains how these two rules are applied to analyze any
circuit.
20.11 The Measurement of Current and Voltage A galvanometer is a device that responds to electric current and is used in nondigital ammeters
and voltmeters. An ammeter is an instrument that measures current and must
be inserted into a circuit in such a way that the current passes directly through
the ammeter. A voltmeter is an instrument for measuring the voltage between
two points in a circuit. A voltmeter must be connected between the two points
and is not inserted into a circuit as an ammeter is.
20.12 Capacitors in Series and in Parallel The equivalent capacitance CP for a parallel combination of capacitances (C1, C2, C3, etc.) is given by Equation 20.18. In general, each capacitor in a parallel combination carries
a diff erent amount of charge. The equivalent capacitor carries the same total
charge and stores the same total energy as the parallel combination.
CP = C1 + C2 + C3 + ⋅ ⋅ ⋅ (20.18)
The reciprocal of the equivalent capacitance CS for a series combination (C1, C2, C3, etc.) of capacitances is given by Equation 20.19. The equivalent capacitor carries the same amount of charge as any one of the capacitors in the combination and stores the same total energy as the series combination.
1
CS =
1
C1 +
1
C2 +
1
C3 + ⋅ ⋅ ⋅ (20.19)
20.13 RC Circuits The charging or discharging of a capacitor in a dc series circuit (resistance R, capacitance C) does not occur instantaneously. The charge on a capacitor builds up gradually, as described by Equation
20.20, where q is the charge on the capacitor at time t and q0 is the equi- librium value of the charge. The time constant 𝜏 of the circuit is given by
Equation 20.21. The discharging of a capacitor through a resistor is described
by Equation 20.22, where q0 is the charge on the capacitor at time t = 0 s.
q = q 0 [1 − e−t /(RC )] (20.20)
τ = RC (20.21)
q = q 0e−t /(RC ) (20.22)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 20.1 Electromotive Force and Current 1. In 2.0 s, 1.9 × 1019 electrons pass a certain point in a wire. What is the current I in the wire?
Section 20.2 Ohm’s Law 2. Which one of the following graphs correctly represents Ohm’s law, where V is the voltage and I is the current? (a) A (b) B (c) C (d) D
QUESTION 2
I
V
A
I
V
C
I
V
B
I
V
D
Section 20.3 Resistance and Resistivity 3. Two wires are made from the same material. One wire has a resistance of 0.10 Ω. The other wire is twice as long as the fi rst wire and has a radius
that is half as much. What is the resistance of the second wire? (a) 0.40 Ω (b) 0.20 Ω (c) 0.10 Ω (d) 0.050 Ω (e) 0.80 Ω
Section 20.4 Electric Power 5. A single resistor is connected across the terminals of a battery. Which one or more of the following changes in voltage and current leaves unchanged the
electric power dissipated in the resistor?
(A) Doubling the voltage and reducing the current by a factor of two
(B) Doubling the voltage and increasing the resistance by a factor of
four
(C) Doubling the current and reducing the resistance by a factor of
four
(a) A, B, C (b) A, B (c) B, C (d) A (e) B
Section 20.5 Alternating Current 7. The average power dissipated in a 47-Ω resistor is 2.0 W. What is the peak value I0 of the ac current in the resistor?
Focus on Concepts
582 CHAPTER 20 Electric Circuits
Section 20.6 Series Wiring 8. For the circuit shown in the drawing, what is the voltage V1 across resist- ance R1?
(a) V1 = ( R1 R2)V (d) V1 = (
R1 R1 + R2)V
(b) V1 = ( R2 R1)V (e) V1 = (
R1 + R2 R1 )V
(c) V1 = V
Section 20.7 Parallel Wiring 10. For the circuit shown in the drawing, what is the ratio of the current I1 in resistance R1 to the current I2 in resistance R2?
(a) I1 I2
= R1 R2
(d) I1 I2
= 1
(b) I1 I2
= R2
R1 + R2 (e)
I1 I2
= R2 R1
(c) I1 I2
= R1
R1 + R2
Section 20.8 Circuits Wired Partially in Series and Partially in Parallel 12. In the following three arrangements each resistor has the same resistance R. Rank the equivalent resistances of the arrangements in descending order (largest fi rst). (a) A, B, C (b) B, A, C (c) B, C, A (d) A, C, B (e) C, B, A
QUESTION 12
R
R R
R
R R
R R
R R R
R
A B
C
Section 20.9 Internal Resistance 13. A battery has an emf of V and an internal resistance of r. What resis- tance R, when connected across the terminals of this battery, will cause the terminal voltage of the battery to be
1
2 V? (a) R = 1
2 r (b) R = 2r (c) R = 4r (d) R = r (e) R = 14 r
Section 20.10 Kirchhoff ’s Rules 15. When applying Kirchhoff ’s rules, one of the essential steps is to mark each resistor with plus and minus signs to label how the potential changes
from one end of the resistor to the other. The circuit in the drawing contains
four resistors, each marked with the associated plus and minus signs. How-
ever, one resistor is marked incorrectly. Which one is it? (a) R1 (b) R2 (c) R3 (d) R4
QUESTION 15
+ –
+ –
+ –
+ – + –
+ –
+
–
+ –
5.0 V
7.0 V
3.0 V
2.0 V
R4
I4
R1
I1
I3
I5 I6
R2
R3
I2
Section 20.12 Capacitors in Series and in Parallel 18. Three capacitors are identical, each having a capacitance C. Two of them are connected in series. Then, this series combination is connected in parallel
with the third capacitor. What is the equivalent capacitance of the entire con-
nection? (a) 12 C (b) 1
3 C (c) 3C (d) 2
3 C (e) 3
2 C
Section 20.13 RC Circuits 20. The time constant of an RC circuit is 2.6 s. How much time t is required for the capacitor (uncharged initially) to gain one-half of its full equilibrium
charge?
R1 R2
+ –
VQUESTION 8
R1
+ –
V
R2
QUESTION 10
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
Note: For problems that involve ac conditions, the current and voltage are rms values and the power is an average value, unless indicated otherwise.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 20.1 Electromotive Force and Current
Section 20.2 Ohm’s Law
1. E BIO A defi brillator is used during a heart attack to restore the heart to its normal beating pattern (see Section 19.5). A defi brillator passes 18 A of
current through the torso of a person in 2.0 ms. (a) How much charge moves during this time? (b) How many electrons pass through the wires connected to the patient?
2. E An especially violent lightning bolt has an average current of 1.26 × 103 A lasting 0.138 s. How much charge is delivered to the ground by the
lightning bolt?
Problems
Problems 583
3. E SSM A battery charger is connected to a dead battery and delivers a current of 6.0 A for 5.0 hours, keeping the voltage across the battery ter-
minals at 12 V in the process. How much energy is delivered to the battery?
4. E A coff ee-maker contains a heating element that has a resistance of 14 Ω. This heating element is energized by a 120-V outlet. What is the current in
the heating element?
5. E BIO GO Suppose that the resistance between the walls of a biological cell is 5.0 × 109 Ω. (a) What is the current when the potential diff erence between the walls is 75 mV? (b) If the current is composed of Na+ ions (q =+e), how many such ions fl ow in 0.50 s? 6. M A car battery has a rating of 220 ampere · hours (A · h). This rating is one indication of the total charge that the battery can provide to a circuit before failing. (a) What is the total charge (in coulombs) that this battery can provide? (b) Determine the maximum current that the battery can provide for 38 minutes.
7. M BIO A resistor is connected across the terminals of a 9.0-V battery, which delivers 1.1 × 105 J of energy to the resistor in six hours. What is the
resistance of the resistor?
8. M GO The resistance of a bagel toaster is 14 Ω. To prepare a bagel, the toaster is operated for one minute from a 120-V outlet. How much energy is
delivered to the toaster?
9. H SSM Available in WileyPLUS.
Section 20.3 Resistance and Resistivity 10. E GO The resistance and the magnitude of the current depend on the path that the current takes. The drawing shows three situations in which the
current takes diff erent paths through a piece of material. Each of the rectangu-
lar pieces is made from a material whose resistivity is 𝜌 = 1.50 × 10−2 Ω · m, and the unit of length in the drawing is L0 = 5.00 cm. Each piece of material is connected to a 3.00-V battery. Find (a) the resistance and (b) the current in each case.
V
+ –
+ – – V+
V
2L0 L0 4L0
2L0 L0 4L0
2L0 L0
4L0
(a) (c)(b)
PROBLEM 10
11. E Two wires are identical, except that one is aluminum and one is copper. The aluminum wire has a resistance of 0.20 Ω. What is the resistance of the
copper wire?
12. E A cylindrical wire has a length of 2.80 m and a radius of 1.03 mm. It carries a current of 1.35 A, when a voltage of 0.0320 V is applied across the
ends of the wire. From what material in Table 20.1 is the wire made? 13. E A coil of wire has a resistance of 38.0 Ω at 25 °C and 43.7 Ω at 55 °C. What is the temperature coeffi cient of resistivity?
14. E A large spool in an electrician’s workshop has 75 m of insulation- coated wire coiled around it. When the electrician connects a battery to the
ends of the spooled wire, the resulting current is 2.4 A. Some weeks later,
after cutting off various lengths of wire for use in repairs, the electrician fi nds
that the spooled wire carries a 3.1-A current when the same battery is con-
nected to it. What is the length of wire remaining on the spool?
15. E SSM Available in WileyPLUS. 16. E High-voltage power lines are a familiar sight throughout the country. The aluminum wire used for some of these lines has a cross-sectional area of
4.9 × 10−4 m2. What is the resistance of ten kilometers of this wire?
17. M The temperature coeffi cient of resistivity for the metal gold is 0.0034 (C°)−1, and for tungsten it is 0.0045 (C°)−1. The resistance of a gold wire
increases by 7.0% due to an increase in temperature. For the same increase
in temperature, what is the percentage increase in the resistance of a tungsten
wire?
18. M GO A tungsten wire has a radius of 0.075 mm and is heated from 20.0 to 1320 °C. The temperature coeffi cient of resistivity is 𝛼 = 4.5 ×
10−3 (C°)−1. When 120 V is applied across the ends of the hot wire, a cur-
rent of 1.5 A is produced. How long is the wire? Neglect any eff ects due to
thermal expansion of the wire.
19. M SSM Available in WileyPLUS. 20. M V-HINT Two cylindrical rods, one copper and the other iron, are identical in lengths and cross-sectional areas. They are joined end to end to
form one long rod. A 12-V battery is connected across the free ends of the
copper–iron rod. What is the voltage between the ends of the copper rod?
21. H BIO A digital thermometer employs a thermistor as the temperature- sensing element. A thermistor is a kind of semiconductor and has a large neg-
ative temperature coeffi cient of resistivity 𝛼. Suppose that 𝛼 = −0.060 (C°)−1
for the thermistor in a digital thermometer used to measure the temperature of
a patient. The resistance of the thermistor decreases to 85% of its value at the
normal body temperature of 37.0 °C. What is the patient’s temperature?
Section 20.4 Electric Power 22. E An electric blanket is connected to a 120-V outlet and consumes 140 W of power. What is the resistance of the heater wire in the blanket?
23. E The heating element in an iron has a resistance of 24 Ω. The iron is plugged into a 120-V outlet. What is the power delivered to the iron?
24. E A blow-dryer and a vacuum cleaner each operate with a voltage of 120 V. The current rating of the blow-dryer is 11 A, and that of the vacuum
cleaner is 4.0 A. Determine the power consumed by (a) the blow-dryer and (b) the vacuum cleaner. (c) Determine the ratio of the energy used by the blow-dryer in 15 minutes to the energy used by the vacuum cleaner in one-
half hour.
25. E There are approximately 110 million households that use TVs in the United States. Each TV uses, on average, 75 W of power and is turned on for
6.0 hours a day. If electrical energy costs $0.12 per kWh, how much money
is spent every day in keeping 110 million TVs turned on?
26. E An MP3 player operates with a voltage of 3.7 V, and is using 0.095 W of power. Find the current being supplied by the player’s battery.
27. E SSM In doing a load of clothes, a clothes dryer uses 16 A of current at 240 V for 45 min. A personal computer, in contrast, uses 2.7 A of current at
120 V. With the energy used by the clothes dryer, how long (in hours) could
you use this computer to “surf” the Internet?
28. M V-HINT An electric heater used to boil small amounts of water con- sists of a 15-Ω coil that is immersed directly in the water. It operates from a
120-V socket. How much time is required for this heater to raise the temper-
ature of 0.50 kg of water from 13 °C to the normal boiling point?
29. M The rear window of a van is coated with a layer of ice at 0 °C. The density of ice is 917 kg/m3. The driver of the van turns on the rear-window
defroster, which operates at 12 V and 23 A. The defroster directly heats an
area of 0.52 m2 of the rear window. What is the maximum thickness of ice
coating this area that the defroster can melt in 3.0 minutes?
30. M GO A piece of Nichrome wire has a radius of 6.5 × 10−4 m. It is used in a laboratory to make a heater that uses 4.00 × 102 W of power when
connected to a voltage source of 120 V. Ignoring the eff ect of temperature on
resistance, estimate the necessary length of wire.
31. M SSM Tungsten has a temperature coeffi cient of resistivity of 0.0045 (C°)−1. A tungsten wire is connected to a source of constant voltage
via a switch. At the instant the switch is closed, the temperature of the wire is
28 °C, and the initial power delivered to the wire is P0. At what wire temper- ature will the power that is delivered to the wire be decreased to
1
2 P0?
584 CHAPTER 20 Electric Circuits
Section 20.5 Alternating Current 32. E According to Equation 20.7, an ac voltage V is given as a function of time t by V = V0 sin 2𝜋ft, where V0 is the peak voltage and f is the frequency (in hertz). For a frequency of 60.0 Hz, what is the smallest value of the time
at which the voltage equals one-half of the peak value?
33. E The rms current in a copy machine is 6.50 A, and the resistance of the machine is 18.6 Ω. What are (a) the average power and (b) the peak power delivered to the machine?
34. E GO The rms current in a 47-Ω resistor is 0.50 A. What is the peak value of the voltage across this resistor?
35. E A 550-W space heater is designed for operation in Germany, where household electrical outlets supply 230 V (rms) service. What is the power
output of the heater when plugged into a 120-V (rms) electrical outlet in a
house in the United States? Ignore the eff ects of temperature on the heater’s
resistance.
36. E V-HINT Review Conceptual Example 7 as an aid in solving this prob- lem. A portable electric heater uses 18 A of current. The manufacturer re-
commends that an extension cord attached to the heater receive no more than
2.0 W of power per meter of length. What is the smallest radius of copper
wire that can be used in the extension cord? (Note: An extension cord con- tains two wires.)
37. E SSM The average power used by a stereo speaker is 55 W. Assuming that the speaker can be treated as a 4.0-Ω resistance, fi nd the peak value of
the ac voltage applied to the speaker.
38. M GO The recovery time of a hot water heater is the time required to heat all the water in the unit to the desired temperature. Suppose that a 52-gal
(1.00 gal = 3.79 × 10−3 m3) unit starts with cold water at 11 °C and delivers hot
water at 53 °C. The unit is electric and utilizes a resistance heater (120 V ac,
3.0 Ω) to heat the water. Assuming that no heat is lost to the environment,
determine the recovery time (in hours) of the unit.
39. M SSM A light bulb is connected to a 120.0-V wall socket. The current in the bulb depends on the time t according to the relation I = (0.707 A) sin [(314 Hz)t]. (a) What is the frequency f of the alternating current? (b) Determine the resistance of the bulb’s fi lament. (c) What is the average power delivered to the light bulb?
40. H Available in WileyPLUS.
Section 20.6 Series Wiring 41. E SSM Three resistors, 25, 45, and 75 Ω, are connected in series, and a 0.51-A current passes through them. What are (a) the equivalent resistance and (b) the potential diff erence across the three resistors? 42. E GO A 60.0-W lamp is placed in series with a resistor and a 120.0-V source. If the voltage across the lamp is 25 V, what is the resistance R of the resistor?
43. E SSM The current in a series circuit is 15.0 A. When an additional 8.00-Ω resistor is inserted in series, the current drops to 12.0 A. What is the
resistance in the original circuit?
44. E V-HINT Multiple-Concept Example 9 discusses the physics principles used in this problem. Three resistors, 2.0, 4.0, and 6.0 Ω, are connected in
series across a 24-V battery. Find the power delivered to each resistor.
45. E The current in a 47-Ω resistor is 0.12 A. This resistor is in series with a 28-Ω resistor, and the series combination is connected across a battery.
What is the battery voltage?
46. M V-HINT Multiple-Concept Example 9 reviews the concepts that are important to this problem. A light bulb is wired in series with a 144-Ω
resistor, and they are connected across a 120.0-V source. The power delivered
to the light bulb is 23.4 W. What is the resistance of the light bulb? Note that
there are two possible answers.
47. M SSM MMH Three resistors are connected in series across a battery. The value of each resistance and its maximum power rating are as follows:
2.0 Ω and 4.0 W, 12.0 Ω and 10.0 W, and 3.0 Ω and 5.0 W. (a) What is the greatest voltage that the battery can have without one of the resistors burning
up? (b) How much power does the battery deliver to the circuit in (a)? 48. M V-HINT One heater uses 340 W of power when connected by itself to a battery. Another heater uses 240 W of power when connected by itself to the
same battery. How much total power do the heaters use when they are both
connected in series across the battery?
49. H Two resistances, R1 and R2, are connected in series across a 12-V battery. The current increases by 0.20 A when R2 is removed, leaving R1 con- nected across the battery. However, the current increases by just 0.10 A when
R1 is removed, leaving R2 connected across the battery. Find (a) R1 and (b) R2.
Section 20.7 Parallel Wiring 50. E A coff ee-maker (14 Ω) and a toaster (19 Ω) are connected in parallel to the same 120-V outlet in a kitchen. How much total power is supplied to
the two appliances when both are turned on?
51. E For the three-way bulb (50 W, 100 W, 150 W) discussed in Concep- tual Example 11, fi nd the resistance of each of the two fi laments. Assume
that the wattage ratings are not limited by signifi cant fi gures, and ignore any
heating eff ects on the resistances.
52. E GO The drawing shows three diff erent resistors in two diff erent cir- cuits. The battery has a voltage of V = 24.0 V, and the resistors have values of R1 = 50.0 Ω, R2 = 25.0 Ω, and R3 = 10.0 Ω. (a) For the circuit on the left, determine the current through and the voltage across each resistor. (b) Repeat part (a) for the circuit on the right.
PROBLEM 52
R1
R3
R2 + –
+ – VV
R1 R2 R3
(a) (b)
53. E SSM The drawing shows a circuit that contains a battery, two resis- tors, and a switch. What is the equivalent resistance of the circuit when the
switch is (a) open and (b) closed? What is the total power delivered to the resistors when the switch is (c) open and (d) closed?
PROBLEM 53
9.00 V
Switch
R1 = 65.0 Ω R2 = 96.0 Ω
54. E A 16-Ω loudspeaker, an 8.0-Ω loudspeaker, and a 4.0-Ω loudspeaker are connected in parallel across the terminals of an amplifi er. Determine the
equivalent resistance of the three speakers, assuming that they all behave as
resistors.
55. E SSM Two resistors, 42.0 and 64.0 Ω, are connected in parallel. The current through the 64.0-Ω resistor is 3.00 A. (a) Determine the current in the other resistor. (b) What is the total power supplied to the two resistors? 56. E V-HINT Two identical resistors are connected in parallel across a 25-V battery, which supplies them with a total power of 9.6 W. While the battery
is still connected, one of the resistors is heated so that its resistance doubles.
The resistance of the other resistor remains unchanged. Find (a) the initial resistance of each resistor and (b) the total power delivered to the resistors after one resistor has been heated.
Problems 585
57. E MMH A coff ee cup heater and a lamp are connected in parallel to the same 120-V outlet. Together, they use a total of 111 W of power. The resist-
ance of the heater is 4.0 × 102 Ω. Find the resistance of the lamp.
58. M Two resistors have resistances R1 and R2. When the resistors are con- nected in series to a 12.0-V battery, the current from the battery is 2.00 A.
When the resistors are connected in parallel to the battery, the total current
from the battery is 9.00 A. Determine R1 and R2. 59. M GO SSM A cylindrical aluminum pipe of length 1.50 m has an inner radius of 2.00 × 10−3 m and an outer radius of 3.00 × 10−3 m. The interior of
the pipe is completely fi lled with copper. What is the resistance of this unit?
(Hint: Imagine that the pipe is connected between the terminals of a battery and decide whether the aluminum and copper parts of the pipe are in series
or in parallel.)
60. M GO The drawing shows two circuits, and the same battery is used in each. The two resistances RA in circuit A are the same, and the two resis- tances RB in circuit B are the same. Knowing that the same total power is delivered in each circuit, fi nd the ratio RB/RA for the circuits.
PROBLEM 60
RA RA
V
+ –
Circuit A
RB
RB
V
+ –
Circuit B
61. H Available in WileyPLUS.
Section 20.8 Circuits Wired Partially in Series and Partially in Parallel 62. E A 60.0-Ω resistor is connected in parallel with a 120.0-Ω resistor. This parallel group is connected in series with a 20.0-Ω resistor. The total
combination is connected across a 15.0-V battery. Find (a) the current and (b) the power delivered to the 120.0-Ω resistor. 63. E SSM A 14-Ω coff ee maker and a 16-Ω frying pan are connected in series across a 120-V source of voltage. A 23-Ω bread maker is also connec-
ted across the 120-V source and is in parallel with the series combination.
Find the total current supplied by the source of voltage.
64. E GO Find the equivalent resistance between points A and B in the drawing.
PROBLEM 64
A
B
4.00 Ω 3.00 Ω 2.00 Ω
1.00 Ω
3.00 Ω
6.00 Ω2.00 Ω
65. E CHALK SSM Determine the equivalent resistance between the points A and B for the group of resistors in the drawing.
PROBLEM 65
A
B
20.0 Ω 9.0 Ω 8.0 Ω
4.0 Ω
6.0 Ω
3.0 Ω
66. E GO The circuit in the drawing contains three identical resistors. Each resistor has a value of 10.0 Ω. Determine the equivalent resistance between
the points a and b, b and c, and a and c.
PROBLEM 66
R c
RR
a b
67. E GO Find the equivalent resistance between the points A and B in the drawing.
PROBLEM 67
R1 = 16 Ω R2 = 8 Ω
R3 = 48 Ω
A B R4 = 26 Ω
68. M GO Each resistor in the three circuits in the drawing has the same resistance R, and the batteries have the same voltage V. The values for R and V are 9.0 Ω and 6.0 V, respectively. Determine the total power delivered by the battery in each of the three circuits.
PROBLEM 68
R R
R R
V
+ –
Circuit A
R
R R
V
+ –
Circuit B
R R
R
R
V
+ –
Circuit C
R
R R
69. M Eight diff erent values of resistance can be obtained by connecting together three resistors (1.00, 2.00, and 3.00 Ω) in all possible ways. What
are the values?
70. M V-HINT MMH Determine the power supplied to each of the resistors in the drawing.
PROBLEM 70 120 V
R2 = 576 Ω
R3 = 576 Ω
R1 = 576 Ω
+ –
A
586 CHAPTER 20 Electric Circuits
71. M SSM The circuit in the drawing contains fi ve identical resistors. The 45-V battery delivers 58 W of power to the circuit. What is the resistance R of each resistor?
PROBLEM 71
+ –
45 V
R1
R2
R3
R4
R5
72. H Available in WileyPLUS.
Section 20.9 Internal Resistance 73. E SSM Available in WileyPLUS. 74. E A 1.40-Ω resistor is connected across a 9.00-V battery. The voltage between the terminals of the battery is observed to be only 8.30 V. Find the
internal resistance of the battery.
75. E When a light bulb is connected across the terminals of a battery, the battery delivers 24 W of power to the bulb. A voltage of 11.8 V exists
between the terminals of the battery, which has an internal resistance of 0.10 Ω.
What is the emf of the battery?
76. E A battery has an internal resistance of 0.012 Ω and an emf of 9.00 V. What is the maximum current that can be drawn from the battery without the
terminal voltage dropping below 8.90 V?
77. M GO A battery delivering a current of 55.0 A to a circuit has a terminal voltage of 23.4 V. The electric power being dissipated by the internal resist-
ance of the battery is 34.0 W. Find the emf of the battery.
78. M V-HINT Available in WileyPLUS.
Section 20.10 Kirchhoff ’s Rules 79. E SSM Consider the circuit in the drawing. Determine (a) the mag- nitude of the current in the circuit and (b) the magnitude of the voltage between the points labeled A and B. (c) State which point, A or B, is at the higher potential.
PROBLEM 79
5.0 Ω
30.0 V
A 27 Ω
12 Ω
8.0 Ω
10.0 V
B
80. E GO The drawing shows a portion of a larger circuit. Current fl ows left to right in each resistor. What is the current in the resistor R?
PROBLEM 80
I1 = 3.00 A
R1 = 2.70 Ω
I2
R2 = 4.40 Ω
R
81. E MMH Find the magnitude and the direction of the current in the 2.0-Ω resistor in the drawing.
PROBLEM 81
1.0 Ω
3.0 Ω 4.0 V
2.0 Ω 1.0 V + –
– +
82. E GO Using Kirchhoff ’s loop rule, fi nd the value of the current I in part c of the drawing, where R = 5.0 Ω. (Note: Parts a and b of the drawing are used in the online tutorial help that is provided for this problem in the
WileyPLUS homework management program.)
R
R
A A BB
RV V +–
I
I I
+ –
+ – 3.0 Ω 4.0 Ω36 V 12 V
– +
(a) (b)
(c)
PROBLEM 82
83. E Determine the current (both magnitude and direction) in the 8.0- and 2.0-Ω resistors in the drawing.
PROBLEM 83
R1 = 8.0 Ω
V2 = 12 V
+
–
+ –
R2 = 2.0 Ω
V1 = 4.0 V
84. M V-HINT Determine the voltage across the 5.0-Ω resistor in the drawing. Which end of the resistor is at the higher potential?
PROBLEM 84
5.0 Ω
10.0 Ω
2.0 V
10.0 Ω
+ – 10.0 V 15.0 V
+ –
+ –
85. M CHALK SSM MMH Find the current in the 4.00-Ω resistor in the drawing. Specify the direction of the current.
PROBLEM 85
+
– 6.00 V
9.00 V3.00 V + –
+ –
2.00 Ω 8.00 Ω
4.00 Ω
Problems 587
86. H None of the resistors in the circuit shown in the drawing is connected in series or in parallel with one another. Find (a) the current I5 and the resist- ances (b) R2 and (c) R3.
PROBLEM 86
6.0 A
R2
9.0 A 75.0 V
12.0 A
R1 = 4.0 Ω
I5
+ –
R4 = 2.0 Ω R5 = 2.2 Ω
R3
Section 20.11 The Measurement of Current and Voltage 87. E SSM The coil of a galvanometer has a resistance of 20.0 Ω, and its meter defl ects full scale when a current of 6.20 mA passes through it.
To make the galvanometer into a nondigital ammeter, a 24.8-mΩ shunt
resistor is added to it. What is the maximum current that this ammeter
can read?
88. E The coil of wire in a galvanometer has a resistance of RC = 60.0 Ω. The galvanometer exhibits a full-scale defl ection when the current through it
is 0.400 mA. A resistor is connected in series with this combination so as to
produce a nondigital voltmeter. The voltmeter is to have a full-scale defl ec-
tion when it measures a potential diff erence of 10.0 V. What is the resistance
of this resistor?
89. E Available in WileyPLUS. 90. E A galvanometer with a coil resistance of 9.00 Ω is used with a shunt resistor to make a nondigital ammeter that has an equivalent resistance of
0.40 Ω. The current in the shunt resistor is 3.00 mA when the galvanometer
reads full scale. Find the full-scale current of the galvanometer.
91. M SSM Two scales on a nondigital voltmeter measure voltages up to 20.0 and 30.0 V, respectively. The resistance connected in series with the
galvanometer is 1680 Ω for the 20.0-V scale and 2930 Ω for the 30.0-V scale.
Determine the coil resistance and the full-scale current of the galvanometer
that is used in the voltmeter.
92. H In measuring a voltage, a voltmeter uses some current from the circuit. Consequently, the voltage measured is only an approximation to the voltage
present when the voltmeter is not connected. Consider a circuit consisting of
two 1550-Ω resistors connected in series across a 60.0-V battery. (a) Find the voltage across one of the resistors. (b) A nondigital voltmeter has a full-scale voltage of 60.0 V and uses a galvanometer with a full-scale defl ection of
5.00 mA. Determine the voltage that this voltmeter registers when it is con-
nected across the resistor used in part (a).
Section 20.12 Capacitors in Series and in Parallel 93. E Two capacitors are connected in parallel across the terminals of a battery. One has a capacitance of 2.0 𝜇F and the other a capacitance of
4.0 𝜇F. These two capacitors together store 5.4 × 10−5 C of charge. What is
the voltage of the battery?
94. E Three parallel plate capacitors are connected in series. These capa- citors have identical geometries. However, they are fi lled with three diff erent
materials. The dielectric constants of these materials are 3.30, 5.40, and 6.70.
It is desired to replace this series combination with a single parallel plate
capacitor. Assuming that this single capacitor has the same geometry as each
of the other three capacitors, determine the dielectric constant of the material
with which it is fi lled.
95. E SSM Three capacitors are connected in series. The equivalent capa- citance of this combination is 3.00 𝜇F. Two of the individual capacitances are
6.00 𝜇F and 9.00 𝜇F. What is the third capacitance (in 𝜇F)?
96. E GO Two capacitors are connected to a battery. The battery voltage is V = 60.0 V, and the capacitances are C1 = 2.00 𝜇F and C2 = 4.00 𝜇F. Determine the total energy stored by the two capacitors when they are wired
(a) in parallel and (b) in series. 97. E Determine the equivalent capacitance between A and B for the group of capacitors in the drawing.
PROBLEM 97
A
B
5.0 Fμ 24 Fμ
4.0 Fμ 12 Fμ
6.0 Fμ 8.0 Fμ
98. E V-HINT A 2.00-𝜇F and a 4.00-𝜇F capacitor are connected to a 60.0-V battery. What is the total charge supplied to the capacitors when they are
wired (a) in parallel and (b) in series with each other? 99. E Suppose that two capacitors (C1 and C2) are connected in series. Show that the sum of the energies stored in these capacitors is equal to the
energy stored in the equivalent capacitor. [Hint: The energy stored in a capa- citor can be expressed as q2/(2C).]
100. M A 3.00-𝜇F and a 5.00-𝜇F capacitor are connected in series across a 30.0-V battery. A 7.00-𝜇F capacitor is then connected in parallel across the
3.00-𝜇F capacitor. Determine the voltage across the 7.00-𝜇F capacitor.
101. M CHALK SSM A 7.0-𝜇F and a 3.0-𝜇F capacitor are connected in series across a 24-V battery. What voltage is required to charge a parallel combina-
tion of the two capacitors to the same total energy?
102. H The drawing shows two capacitors that are fully charged (C1 = 2.00 𝜇F, q1 = 6.00 𝜇C; C2 = 8.00 𝜇F, q2 = 12.0 𝜇C). The switch is closed, and charge fl ows until equilibrium is reestablished (i.e., until both capacitors
have the same voltage across their plates). Find the resulting voltage across
either capacitor.
PROBLEM 102
C2 ++ +
Switch
+ –– ––
+ + – – C1
Section 20.13 RC Circuits 103. E BIO SSM In a heart pacemaker, a pulse is delivered to the heart 81 times per minute. The capacitor that controls this pulsing rate discharges
through a resistance of 1.8 × 106 Ω. One pulse is delivered every time the
fully charged capacitor loses 63.2% of its original charge. What is the capa-
citance of the capacitor?
104. E A circuit contains a resistor in series with a capacitor, the series combination being connected across the terminals of a battery, as in Figure 20.37a. The time constant for charging the capacitor is 1.5 s when the res- istor has a resistance of 2.0 × 104 Ω. What would the time constant be if the
resistance had a value of 5.2 × 104 Ω?
105. E V-HINT The circuit in the drawing contains two resistors and two capacitors that are connected to a battery via a switch. When the switch is
closed, the capacitors begin to charge up. What is the time constant for the
charging process?
588 CHAPTER 20 Electric Circuits
PROBLEM 105 + –
Ω4.0 k
Ω2.0 k
Switch
3.0 Fμ
6.0 Fμ
106. M MMH How many time constants must elapse before a capacitor in a series RC circuit is charged to 80.0% of its equilibrium charge? 107. M MMH Four identical capacitors are connected with a resistor in two diff erent ways. When they are connected as in part a of the drawing, the time
constant to charge up this circuit is 0.72 s. What is the time constant when
they are connected with the same resistor, as in part b?
R
C C
C C
+ –
R
C
C
C
+ –
C
(b)(a)
PROBLEM 107
108. E GO Each of the four circuits in the drawing consists of a single res- istor whose resistance is either R or 2R, and a single battery whose voltage is either V or 2V. The unit of voltage in each circuit is V = 12.0 V and the unit of resistance is R = 6.00 Ω. Determine (a) the power supplied to each resistor and (b) the current delivered to each resistor.
PROBLEM 108
+ –
V
(a)
R
+ –
V
(b)
2R 2R
+ –
2V 2V (c)
R
+ –
(d)
109. E SSM Available in WileyPLUS. 110. E Available in WileyPLUS. 111. E SSM In the Arctic, electric socks are useful. A pair of socks uses a 9.0-V battery pack for each sock. A current of 0.11 A is drawn from each
battery pack by wire woven into the socks. Find the resistance of the wire in
one sock.
112. (animated) E Available in WileyPLUS. 113. E In Section 12.3 it was mentioned that temperatures are often mea- sured with electrical resistance thermometers made of platinum wire. Suppose
that the resistance of a platinum resistance thermometer is 125 Ω when its
temperature is 20.0 °C. The wire is then immersed in boiling chlorine, and the
resistance drops to 99.6 Ω. The temperature coeffi cient of resistivity of plat-
inum is 𝛼 = 3.72 × 10−3 (C°)−1. What is the temperature of the boiling chlorine? 114. E The circuit in the drawing shows two resistors, a capacitor, and a battery. When the capacitor is fully charged, what is the magnitude q of the charge on one of its plates?
PROBLEM 114
+ –V = 12 V
ΩR2 = 2.0
ΩR1 = 4.0 C = 9.0 Fμ
115. E Available in WileyPLUS. 116. E An 86-Ω resistor and a 67-Ω resistor are connected in series across a battery. The voltage across the 86-Ω resistor is 27 V. What is the voltage
across the 67-Ω resistor?
117. M SSM The current in the 8.00-Ω resistor in the drawing is
0.500 A. Find the current in (a) the 20.0-Ω resistor and in (b) the 9.00-Ω resistor.
118. M Available in WileyPLUS. 119. M SSM An extension cord is used with an electric weed trimmer
that has a resistance of 15.0 Ω. The
extension cord is made of copper
wire that has a cross-sectional area
of 1.3 × 10−6 m2. The combined
length of the two wires in the ex-
tension cord is 92 m. (a) Determine the resistance of the extension cord.
(b) The extension cord is plugged into a 120-V socket. What voltage is applied to the trimmer itself?
120. M GO The total current delivered to a number of devices connected in parallel
is the sum of the individual currents in each
device. Circuit breakers are resettable auto-
matic switches that protect against a dan-
gerously large total current by “opening” to
stop the current at a specifi ed safe value.
A 1650-W toaster, a 1090-W iron, and a
1250-W microwave oven are turned on in a
kitchen. As the drawing shows, they are all
connected through a 20-A circuit breaker
(which has negligible resistance) to an ac
voltage of 120 V. (a) Find the equivalent resistance of the three devices. (b) Obtain the total current delivered by the source and determine whether the breaker will
“open” to prevent an accident.
121. M SSM Available in WileyPLUS. 122. M V-HINT The fi lament in an incandescent light bulb is made from tung- sten. The light bulb is plugged into a 120-V outlet and draws a current of 1.24 A.
If the radius of the tungsten wire is 0.0030 mm, how long must the wire be?
123. M SSM Available in WileyPLUS. 124. H Available in WileyPLUS.
Additional Problems
120 V
20 A
Circuit breaker
PROBLEM 120
20.0 Ω
8.00 Ω
16.0 Ω
9.00 Ω
18.0 Ω
+ –
PROBLEM 117
Team Problems 589
Series and parallel wiring are two common ways in which devices, such as
light bulbs, can be connected in a circuit. Problem 125 reviews the concepts
of voltage, resistance, and power in the context of these two types of circuits.
Kirchhoff ’s junction rule and loop rule are important tools for analyzing the
currents and voltages in complex circuits. The rules are easy to use, once
some of the subtleties are understood. Problem 126 explores these subtleties
in a two-loop circuit.
125. M CHALK SSM A circuit contains a 48-V battery and a single light bulb whose resistance is 240 Ω. A second, identical, light bulb can be wired either
in series or in parallel with the fi rst one (see the fi gure). Concepts: (i) How is the power P that is delivered to a light bulb related to the bulb’s resistance R and the voltage V across it? (ii) When there is only one bulb in the circuit, what is the voltage across it? (iii) The more power delivered to a bulb, the brighter it is. When two bulbs are wired in series, does the brightness of each
bulb increase, decrease, or remain the same relative to the brightness of the
bulb in the single-bulb circuit? (iv) When two bulbs are wired in parallel,
does the brightness of each bulb increase, decrease, or remain the same re-
lative to the brightness of the bulb in the single-bulb circuit? Calculations: Determine the power delivered to a single bulb when the circuit contains
(a) only one bulb, (b) two bulbs in series and (c) two bulbs in parallel. Assume that the battery has no internal resistance.
126. M CHALK For this problem concerning Kirchhoff ’s junction rule and loop rule, refer to the fi gure. Concepts: (i) Notice that there are two loops, labeled 1 and 2 in this circuit. Does it matter that there is no battery in loop 1,
but only two resistors? Explain. (ii) The currents through the three resistors
are labeled as I1, I2, and I3. Does it matter which direction, left-to-right or right-to-left, has been chosen for each circuit? (iii) When we place + and −
signs on the ends of each resistor, does it matter which side is + and which is
−? (iv) When we evaluate the potential drops and rises around a closed loop,
does it matter which direction, clockwise or counterclockwise, is chosen for
the evaluation? Calculations: Use Kirchhoff ’s junction and loop rules to de- termine the currents through the three resistors.
Concepts and Calculations Problems
+ – + –
48 V
Series wiring Parallel wiring
48 V
Ω240 Ω240
Ω240
Ω240
+ –
48 V
Ω240
PROBLEM 125
+
+ +–
+ –
–
–
Ω4.0
Ω6.0
6.0 V
F
C
G
HA
B
E
D
I1
I3
I2
Ω3.0 2
1
PROBLEM 126
127. M Fixing a Radio. You and your team are stranded on a tropical island that hosts a deserted military base. In your eff orts to get rescued, you fi nd
a radio. However, when you power it up some lights turn on, but the radio
does not transmit or receive. You open up the back cover and quickly identify
the problem: There is a burnt resistor on the circuit board. You have located
some basic electronics tools and supplies, but the charred resistor is uniden-
tifi able, so you do not know what to use for its replacement. There is a crude
schematic on the inside of the cover of the radio, but it only gives the value of
the current through the part of the circuit with the burnt resistor. You sketch
the circuit with all the elements you can identify (see drawing). (a) Determine the value of the damaged resistor. (b) The next problem is that the resistors that you have found are all 47.0 Ω. The available space will only allow for six
or fewer resistors. Find a confi guration of six or fewer 47.0-Ω resistors that
has an equivalent resistance within 10% of that calculated in part (a).
128. M A Resistive Heater. You and your team are designing a small tube heater that consists of a small ceramic tube wrapped with a special heater
wire composed of Nichrome. When you run an electrical current through
the wire, the wire (and therefore the tube) heats up through resistive heating.
Nichrome is an alloy composed of 80% nickel and 20% chromium, and has a
resistivity of ρ = 1.25 × 10−6 Ω · m. (a) What is the resistance per centimeter of 28-gauge Nichrome wire? (“28 gauge” means the wire has a diameter
D = 0.320 mm) (b) You wrap the tube with 45.0 cm of the Nichrome wire, and you want the power output of your heater to be 120 W. What current is
needed? (c) What voltage will provide the current calculated in (b)?
Team Problems
(Burnt)
1/18 AR = ???
+ –
+–
2.0 Ω4.0 Ω
8.0 Ω 2.0 V
3.0 V
PROBLEM 127
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
21.1 Define magnetic field.
21.2 Calculate the magnetic force on a moving charge in a magnetic field.
21.3 Analyze the motion of a charged particle in a magnetic field.
21.4 Describe how the masses of ions are determined using a mass spectrometer.
21.5 Calculate the magnetic force on a current in a magnetic field.
21.6 Calculate the torque on a current- carrying coil.
21.7 Calculate magnetic fields produced by currents.
21.8 Apply Ampère’s law to calculate the magnetic field due to a steady current.
21.9 Describe magnetic materials.
S u ra
n g a
W ee
ra tu
n g a/
1 2 3 R
F . co
m
CHAPTER 21
Magnetic Forces and Magnetic Fields
This beautiful display of light in the sky is known as the northern lights (aurora borealis). It occurs when
charged particles, streaming from the sun, become trapped by the earth’s magnetic fi eld. The particles
collide with molecules in the upper atmosphere, and the result is the production of light. Magnetic forces
and magnetic fi elds are the subjects of this chapter.
21.1 Magnetic Fields Permanent magnets have long been used in navigational compasses. As Figure 21.1 illustrates, the compass needle is a permanent magnet supported so it can rotate freely
in a plane. When the compass is placed on a horizontal surface, the needle rotates until
one end points approximately to the north. The end of the needle that points north is
labeled the north magnetic pole; the opposite end is the south magnetic pole. Magnets can exert forces on each other. Figure 21.2 shows that the magnetic
forces between north and south poles have the property that
like poles repel each other, and unlike poles attract.
This behavior is similar to that of like and unlike electric charges. However, there is
a signifi cant diff erence between magnetic poles and electric charges. It is possible
to separate positive from negative electric charges and produce isolated charges of
either kind. In contrast, no one has found a magnetic monopole (an isolated north or
south pole). Any attempt to separate north and south poles by cutting a bar magnet
in half fails, because each piece becomes a smaller magnet with its own north and
south poles.
590
21.1 Magnetic Fields 591
S
N
FIGURE 21.1 The needle of a compass is a permanent magnet that has a north magnetic
pole (N) at one end and a south magnetic
pole (S) at the other.
Like poles repel (a)
Unlike poles attract (b)
FIGURE 21.2 Bar magnets have a north magnetic pole at one end and a south magnetic pole at the other end. (a) Like poles repel each other, and (b) unlike poles attract.
Magnetic field lines
(a)
SN
(c)
SN
FIGURE 21.4 (a) The magnetic fi eld lines and (b) the pattern of iron fi lings (black, curved regions) in the vicinity of a bar magnet. (c) The magnetic fi eld lines in the gap of a horseshoe magnet.
(b)
SN
C o rd
el ia
M o ll
o y /S
ci en
ce S
o u rc
e
Surrounding a magnet, there is a magnetic fi eld. The magnetic fi eld is analogous to the electric fi eld that exists in the space around electric charges. Like the electric fi eld, the magnetic
fi eld has both a magnitude and a direction. We postpone a discussion of the magnitude until
Section 21.2, concentrating our attention here on the direction. The direction of the magnetic fi eld at any point in space is the direction indicated by the north pole of a small compass needle placed at that point. In Figure 21.3 the compass needle is symbolized by an arrow, with the head of the arrow representing the north pole. The drawing shows how compasses can be used to map
out the magnetic fi eld in the space around a bar magnet. Since like poles repel and unlike poles
attract, the needle of each compass becomes aligned relative to the magnet in the manner shown
in the picture. The compass needles provide a visual picture of the magnetic fi eld that the bar
magnet creates.
To help visualize the electric fi eld, we introduced electric fi eld lines in Section 18.7. In a
similar fashion, it is possible to draw magnetic fi eld lines, and Figure 21.4a illustrates some of the lines around a bar magnet. The lines appear to originate from the north pole and end on the
south pole; they do not start or stop in midspace. A visual image of the magnetic fi eld lines can
be created by sprinkling fi nely ground iron fi lings on a piece of paper that covers the magnet. Iron
fi lings in a magnetic fi eld behave like tiny compasses and align themselves along the fi eld lines,
as the photograph in Figure 21.4b shows. As is the case with electric fi eld lines, the magnetic fi eld at any point is tangent to the mag-
netic fi eld line at that point. Furthermore, the strength of the fi eld is proportional to the number
of lines per unit area that passes through a surface oriented perpendicular to the lines. Thus, the
magnetic fi eld is stronger in regions where the fi eld lines are relatively close together and weaker
where they are relatively far apart. For instance, in Figure 21.4a the lines are closest together near the north and south poles, refl ecting the fact that the strength of the fi eld is greatest in these
regions. Away from the poles, the magnetic fi eld becomes weaker. Notice in part c of the drawing that the fi eld lines in the gap between the poles of the horseshoe magnet are nearly parallel and
equally spaced, indicating that the magnetic fi eld there is approximately constant.
Although the north pole of a compass needle points northward, it does not point exactly
at the north geographic pole. The north geographic pole is that point where the earth’s axis of
rotation crosses the surface in the northern hemisphere (see Figure 21.5). Measurements of the magnetic fi eld surrounding the earth show that the earth behaves magnetically almost as if it were
SN
Compass
FIGURE 21.3 At any location in the vicinity of a magnet, the north pole (the arrowhead
in this drawing) of a small compass needle
points in the direction of the magnetic fi eld at
that location.
North magnetic pole
Magnetic axis
Rotational axis
North geographic pole
S
N
FIGURE 21.5 The earth behaves magnet- ically almost as if a bar magnet were located
near its center. The axis of this fi ctitious bar
magnet does not coincide with the earth’s
rotational axis; the two axes are currently
about 11.5° apart.
592 CHAPTER 21 Magnetic Forces and Magnetic Fields
a bar magnet.* As the drawing illustrates, the orientation of this fi ctitious bar magnet defi nes a
magnetic axis for the earth. The location at which the magnetic axis crosses the surface in the
northern hemisphere is known as the north magnetic pole. It is so named because it is the location
toward which the north end of a compass needle points. Since unlike poles attract, the south pole
of the earth’s fi ctitious bar magnet lies beneath the north magnetic pole, as Figure 21.5 indicates. The north magnetic pole does not coincide with the north geographic pole but, instead, lies
at a latitude of nearly 80°, just northwest of Ellef Ringnes Island in extreme northern Canada. It
is interesting to note that the position of the north magnetic pole is not fi xed, but moves over the
years. Pointing as it does at the north magnetic pole, a compass needle deviates from the north
geographic pole. The angle that a compass needle deviates is called the angle of declination. For New York City, the present angle of declination is about 13° west, meaning that a compass needle
points 13° west of geographic north.
Figure 21.5 shows that the earth’s magnetic fi eld lines are not parallel to the surface at all points. For instance, near the north magnetic pole the fi eld lines are almost perpendicular to the
surface of the earth. The angle that the magnetic fi eld makes with respect to the surface at any
point is known as the angle of dip. BIO THE PHYSICS OF . . . navigation in animals. Some animals can sense the earth’s
magnetic fi eld and use it for navigational purposes. Until recently (2004), the only examples of this
ability were in vertebrates, or animals that have a backbone, such as migratory birds. Now, however,
researchers have found that the spiny lobster (see Figure 21.6), which is an invertebrate, can also use the earth’s magnetic fi eld to navigate and can determine its geographic location in a way similar to
that of a person using the Global Positioning System (see Section 5.5). This ability may be related to
the presence in the lobsters of the mineral magnetite, a magnetic material used for compass needles.
21.2 The Force That a Magnetic Field Exerts on a Moving Charge When a charge is placed in an electric fi eld, it experiences an electric force, as Section 18.6 dis-
cusses. When a charge is placed in a magnetic fi eld, it also experiences a force, provided that certain
conditions are met, as we will see. The magnetic force, like all the forces we have studied (e.g., the gravitational, elastic, and electric forces), may contribute to the net force that causes an object
to accelerate. Thus, when present, the magnetic force must be included in Newton’s second law.
The following two conditions must be met for a charge to experience a magnetic force when
placed in a magnetic fi eld:
1. The charge must be moving, because no magnetic force acts on a stationary charge. 2. The velocity of the moving charge must have a component that is perpendicular to the
direction of the magnetic fi eld.
To examine the second condition, consider Figure 21.7, which shows a positive test charge +q0 moving with a velocity v→ through a magnetic fi eld B→. The fi eld is produced by magnets not shown in the drawing and is assumed to be constant in both magnitude and direction. If the
charge moves parallel or antiparallel to the fi eld, as in Figure 21.7a, the charge experiences no magnetic force. If, however, the charge moves perpendicular to the fi eld, as in Figure 21.7b, the charge experiences the maximum possible force F→max. In general, if a charge moves at an angle 𝜃* with respect to the fi eld (see Figure 21.7c), only the velocity component 𝜐 sin 𝜃, which is per- pendicular to the fi eld, gives rise to a magnetic force. This force F→ is smaller than the maximum possible force. The component of the velocity that is parallel to the magnetic fi eld yields no force.
Figure 21.7 shows that the direction of the magnetic force F→ is perpendicular to both the velocity v→ and the magnetic fi eld B→; in other words, F→ is perpendicular to the plane defi ned by
*At present it is not known with certainty what causes the earth’s magnetic fi eld. The magnetic fi eld seems to originate
from electric currents that in turn arise from electric charges circulating within the liquid outer region of the earth’s core.
Section 21.7 discusses how a current produces a magnetic fi eld.
*The angle 𝜃 between the velocity of the charge and the magnetic fi eld is chosen so that it lies in the range 0 ≤ 𝜃 ≤ 180°.
FIGURE 21.6 Spiny lobsters use the earth’s magnetic fi eld to navigate and determine their
geographic position.
D.P. Wilson/FLPA/Science Source
21.2 The Force That a Magnetic Field Exerts on a Moving Charge 593
v→ and B→. As an aid in remembering the direction of the force, it is convenient to use Right-Hand Rule No. 1 (RHR-1), as Animated Figure 21.8 illustrates:
Right-Hand Rule No. 1. Extend the right hand so the fi ngers point along the direction of the magnetic fi eld B→ and the thumb points along the velocity v→ of the charge. The palm of the hand then faces in the direction of the magnetic force F→ that acts on a positive charge.
It is as if the open palm of the right hand pushes on the positive charge in the direction of the
magnetic force.
Problem-Solving Insight If the moving charge is negative instead of positive, the direction of the magnetic force is opposite to that predicted by RHR-1.
Thus, there is an easy method for fi nding the force on a moving negative charge. First, assume
that the charge is positive and use RHR-1 to fi nd the direction of the force. Then, reverse this
direction to fi nd the direction of the force acting on the negative charge.
We will now use what we know about the magnetic force to defi ne the magnetic fi eld, in a
procedure that is analogous to that used in Section 18.6 to defi ne the electric fi eld. Recall that the
electric fi eld at any point in space is the force per unit charge that acts on a test charge q0 placed at that point. In other words, to determine the electric fi eld E→, we divide the electrostatic force F→ by the charge q0: E
→ = F→/q0. In the magnetic case, however, the test charge is moving, and the force
depends not only on the charge q0, but also on the velocity component 𝜐 sin 𝜃 that is perpendicu- lar to the magnetic fi eld. Therefore, to determine the magnitude of the magnetic fi eld, we divide
the magnitude of the magnetic force by the magnitude |q0| of the charge and also by 𝜐 sin 𝜃, according to the following defi nition:
DEFINITION OF THE MAGNETIC FIELD The magnitude B of the magnetic fi eld at any point in space is defi ned as
B = F
∣q0∣(υ sin θ) (21.1)
where F is the magnitude of the magnetic force on a test charge, |q0| is the magnitude of the test charge, and 𝞾 is the magnitude of the charge’s velocity, which makes an angle 𝞱 (0 ≤ 𝞱 ≤ 180°) with the direction of the magnetic fi eld. The magnetic fi eld B→ is a vector, and its direction can be determined by using a small compass needle.
SI Unit of Magnetic Field: newton · second coulomb · meter = 1 tesla (T)
B
–v
v
v+q0
+q0 +q0
(a) (b)
Fmax
90°
+q0
(c)
F
θ
θ
v
sin
B
B
B
B
B
B
B
B
FIGURE 21.7 (a) No magnetic force acts on a charge moving with a velocity v→ that is parallel or antiparallel to a magnetic fi eld B→. (b) The charge experiences a maximum force F→ max when the charge moves perpendicular to the fi eld. (c) If the charge travels at an angle 𝜃 with respect to B→, only the velocity component perpendicular to B→ gives rise to a magnetic force F→, which is smaller than F→ max. This component is 𝜐 sin 𝜃.
B
Right hand
RHR–1
v
F
ANIMATED FIGURE 21.8 Right-Hand Rule No. 1 is illustrated. When the right
hand is oriented so the fi ngers point along
the magnetic fi eld B→ and the thumb points along the velocity v→ of a positively charged particle, the palm faces in the direction of the
magnetic force F→ applied to the particle.
594 CHAPTER 21 Magnetic Forces and Magnetic Fields
The unit of magnetic fi eld strength that follows from Equation 21.1 is the N · s/(C · m). This unit is called the tesla (T), a tribute to the Croatian-born American engineer Nikola Tesla (1856– 1943). Thus, one tesla is the strength of the magnetic fi eld in which a unit test charge, traveling
perpendicular to the magnetic fi eld at a speed of one meter per second, experiences a force of one
newton. Because a coulomb per second is an ampere (1 C/s = 1 A, see Section 20.1), the tesla is
often written as 1 T = 1 N/(A · m). In many situations the magnetic fi eld has a value that is considerably less than one tesla. For
example, the strength of the magnetic fi eld near the earth’s surface is approximately 10−4 T. In
such circumstances, a magnetic fi eld unit called the gauss (G) is sometimes used. Although not an SI unit, the gauss is a convenient size for many applications involving magnetic fi elds. The
relation between the gauss and the tesla is
1 gauss = 10−4 tesla
Example 1 deals with the magnetic force exerted on a moving proton and on a moving
electron.
EXAMPLE 1 Magnetic Forces on Charged Particles
A proton in a particle accelerator has a speed of 5.0 × 106 m/s. The proton
encounters a magnetic fi eld whose magnitude is 0.40 T and whose direc-
tion makes an angle of 𝜃 = 30.0° with respect to the proton’s velocity (see
Figure 21.7c). Find the magnitude and direction of (a) the magnetic force on the proton and (b) the acceleration of the proton. (c) What would be the force and acceleration if the particle were an electron instead of a proton?
Reasoning For both the proton and the electron, the magnitude of the magnetic force is given by Equation 21.1. The magnetic forces that act
on these particles have opposite directions, however, because the charges
have opposite signs. In either case, the acceleration is given by Newton’s
second law, which applies to the magnetic force just as it does to any
force. In using the second law, we must take into account the fact that the
masses of the proton and the electron are diff erent.
Solution (a) The positive charge on a proton is 1.60 × 10−19 C, and according to Equation 21.1, the magnitude of the magnetic force is F = |q0|𝜐B sin 𝜃. Therefore,
F = (1.60 × 10−19 C)(5.0 × 106 m/s)(0.40 T)(sin 30.0°) = 1.6 × 10−13 N
The direction of the magnetic force is given by RHR-1 and is upward in Figure 21.7c, with the magnetic fi eld pointing to the right.
(b) The magnitude a of the proton’s acceleration follows directly from Newton’s second law as the magnitude of the net force divided by the
mass mp of the proton. Since the only force acting on the proton is the magnetic force F, it is the net force. Thus,
a = F mp
= 1.6 × 10−13 N
1.67 × 10−27 kg = 9.6 × 1013 m /s2 (4.1)
The direction of the acceleration is the same as the direction of the net
force (the magnetic force).
(c) The magnitude of the magnetic force on the electron is the same as that on the proton, since both have the same velocity and charge magnitude.
However, the direction of the force on the electron is opposite to that on
the proton, or downward in Figure 21.7c, since the electron charge is negative. Furthermore, the electron has a smaller mass me and, therefore, experiences a signifi cantly greater acceleration:
a = F m e
= 1.6 × 10−13 N
9.11 × 10−31 kg = 1.8 × 1017 m /s2
The direction of this acceleration is downward in Figure 21.7c.
Check Your Understanding
(The answers are given at the end of the book.) 1. Suppose that you accidentally use your left hand, instead of your right hand, to determine the direction
of the magnetic force that acts on a positive charge moving in a magnetic fi eld. Do you get the correct
answer? (a) Yes, because either hand can be used (b) No, because the direction you get will be perpendicular to the
correct direction (c) No, because the direction you get will be opposite to the correct direction
2. Two particles, having the same charge but diff erent velo- cities, are moving in a constant magnetic fi eld (see CYU Figure 21.1, where the velocity vectors are drawn to scale). Which particle, if either, experiences the greater magnetic
force? (a) Particle 1 experiences the greater force, because it is moving perpendicular to the magnetic fi eld. (b) Particle 2 experiences the greater force, because it has the greater CYU FIGURE 21.1
B
B
B
v1 v2
1 2
21.3 The Motion of a Charged Particle in a Magnetic Field 595
speed. (c) Particle 2 experiences the greater force, because a component of its velocity is parallel to the magnetic fi eld. (d) Both particles experience the same magnetic force, because the component of each velocity that is perpendicular to the magnetic fi eld is the same.
3. A charged particle, passing through a certain region of space, has a velocity whose magnitude and direction remain constant. (a) If it is known that the external magnetic fi eld is zero everywhere in this region, can you conclude that the external electric fi eld is also zero? (b) If it is known that the external electric fi eld is zero everywhere, can you conclude that the external magnetic fi eld is
also zero?
21.3 The Motion of a Charged Particle in a Magnetic Field
Comparing Particle Motion in Electric and Magnetic Fields The motion of a charged particle in an electric fi eld is noticeably diff erent from the motion
in a magnetic fi eld. For example, Figure 21.9a shows a positive charge moving between the plates of a parallel plate capacitor. Initially, the charge is moving perpendicular to the direc-
tion of the electric fi eld. Since the direction of the electric force on a positive charge is in the
same direction as the electric fi eld, the particle is defl ected sideways. Part b of the drawing shows the same particle traveling initially at right angles to a magnetic fi eld. An application
of RHR-1 shows that when the charge enters the fi eld, the charge is defl ected upward (not
sideways) by the magnetic force. As the charge moves upward, the direction of the magnetic
force changes, always remaining perpendicular to both the magnetic fi eld and the velocity.
Conceptual Example 2 focuses on the diff erence in how electric and magnetic fi elds apply
forces to a moving charge.
– –
– –
E
B
v
v
F
+q
+q
(a)
(b)
–
+
+
+
+
+
+
+
+
+
+
+
+
F
FIGURE 21.9 (a) The electric force F→ that acts on a positive charge is parallel to the
electric fi eld E→. (b) The magnetic force F→ is perpendicular to both the magnetic fi eld B→ and the velocity v→.
*In many instances it is convenient to orient the magnetic fi eld B→ so its direction is perpendicular to the page. In these cases it is customary to use a dot to symbolize the magnetic fi eld pointing out of the page (toward the reader); this dot symbolizes the tip of the arrow representing the B→ vector. A region in which a magnetic fi eld is directed into the page is drawn as a series of crosses that indicate the tail feathers of the arrows representing the B→ vectors. Therefore, regions in which a magnetic fi eld is directed out of the page or into the page are drawn as shown below:
· · · · × × × × · · · · × × × × · · · · × × × ×
Out of page Into page
CONCEPTUAL EXAMPLE 2 The Physics of a Velocity Selector
A velocity selector is a device for measuring the velocity of a charged
particle. The device operates by applying electric and magnetic forces to
the particle in such a way that these forces balance. Figure 21.10a shows a particle with a positive charge +q and a velocity v→ that is perpendicular to a constant magnetic fi eld* B→. Figure 21.10b illustrates a velocity se- lector, which is a cylindrical tube that is located within the magnetic fi eld.
Inside the tube there is a parallel plate capacitor that produces an elec-
tric fi eld E→ (not shown) perpendicular to the magnetic fi eld. The charged particle enters the left end of the tube, moving perpendicular to the mag-
netic fi eld. If the strengths of E→ and B→ are adjusted properly, the electric and magnetic forces acting on the particle will cancel each other. With no
net force acting on the particle, the velocity remains unchanged, accord-
ing to Newton’s fi rst law. As a result, the particle moves in a straight line
at a constant speed and exits at the right end of the tube. The magnitude
of the velocity that is “selected” can be determined from a knowledge of
the strengths of the electric and magnetic fi elds. Particles with velocities
diff erent from the one “selected” are defl ected and do not exit at the right
end of the tube.
How should the electric fi eld E→ be directed so that the force it applies to the particle can balance the magnetic force produced by B→? The electric fi eld should be directed: (a) in the same direction as the magnetic fi eld; (b) in a direction opposite to that of the magnetic fi eld; (c) from the upper plate of the parallel plate capacitor toward the lower plate; (d) from the lower plate of the parallel plate capacitor toward the upper plate.
Reasoning If the electric and magnetic forces are to cancel each other, they must have opposite directions. The direction of the magnetic force
596 CHAPTER 21 Magnetic Forces and Magnetic Fields
We have seen that a charged particle traveling in a magnetic fi eld experiences a magnetic
force that is always perpendicular to the fi eld. In contrast, the force applied by an electric fi eld
is always parallel (or antiparallel) to the fi eld direction. Because of the diff erence in the way that
electric and magnetic fi elds exert forces, the work done on a charged particle by each fi eld is
diff erent, as we now discuss.
The Work Done on a Charged Particle Moving Through Electric and Magnetic Fields In Figure 21.9a an electric fi eld applies a force to a positively charged particle, and, consequently, the path of the particle bends in the direction of the force. Because there is a component of the
particle’s displacement in the direction of the electric force, the force does work on the particle,
according to Equation 6.1. This work increases the kinetic energy and, hence, the speed of the
particle, in accord with the work–energy theorem (see Section 6.2). In contrast, the magnetic
force in Figure 21.9b always acts in a direction that is perpendicular to the motion of the charge. Consequently, the displacement of the moving charge never has a component in the direction of
the magnetic force. As a result, the magnetic force cannot do work and change the kinetic energy of the charged particle in Figure 21.9b. Thus, the speed of the particle does not change, although the force does alter the direction of the motion.
The Circular Trajectory To describe the motion of a charged particle in a constant magnetic fi eld more completely, let’s
discuss the special case in which the velocity of the particle is perpendicular to a uniform mag-
netic fi eld. As Interactive Figure 21.11 illustrates, the magnetic force serves to move the particle in a circular path. To understand why, consider two points on the circumference labeled 1 and 2.
When the positively charged particle is at point 1, the magnetic force F→ is perpendicular to the velocity v→ and points directly upward in the drawing. This force causes the trajectory to bend upward. When the particle reaches point 2, the magnetic force still remains perpendicular to the
velocity but is now directed to the left in the drawing.
Problem-Solving Insight The magnetic force always remains perpendicular to the velocity and is directed toward the center of the circular path.
can be found by applying Right-Hand Rule No. 1 (RHR-1) to the moving
charged particle. This rule reveals that the magnetic force acting on the
positively charged particle in Figure 21.10a is directed upward, toward the top of the page when the particle enters the fi eld region. Since the
particle is positively charged, the direction of the electric force is the
same as the direction of the electric fi eld produced by the capacitor
plates.
Answers (a), (b), and (d) are incorrect. The electric force on the pos- itively charged particle is in the direction of the electric fi eld. Thus, the
electric force would point perpendicularly into the page in answer (a),
perpendicularly out of the page in answer (b), and upward toward the
top of the page in answer (d). Since the magnetic force points upward
toward the top of the page when the particle enters the fi eld region, these
electric forces do not have the proper direction to cancel the magnetic
force.
Answer (c) is correct. Since the magnetic force is directed upward when the particle enters the fi eld region, the electric force must be direc-
ted downward. The force applied to a positive charge by an electric fi eld
has the same direction as the fi eld itself, so the electric fi eld must point
downward, from the upper plate of the capacitor toward the lower plate.
As a result, the upper plate must be positively charged.
Related Homework: Problems 24, 28
(b)
v
Tube (cutaway
view)
Capacitor plates
+q
(a)
B (into paper)
v +q
FIGURE 21.10 (a) A particle with a positive charge q and velocity v→ moves perpendicularly into a magnetic fi eld B→. (b) A velocity selector is a tube in which an electric fi eld (not shown) is perpendicular to a
magnetic fi eld, and the fi eld magnitudes are adjusted so that the electric
and magnetic forces acting on the particle cancel each other.
F
v
R. H.
F
v
F
r
F
B (into paper)
2
1
+q
INTERACTIVE FIGURE 21.11 A positively charged particle is moving perpendicular to a
constant magnetic fi eld. The magnetic force
F→ causes the particle to move on a circular path (R.H. = right hand).
21.3 The Motion of a Charged Particle in a Magnetic Field 597
To fi nd the radius of the path in Interactive Figure 21.11, we use the concept of centripetal force from Section 5.3. The centripetal force is the net force, directed toward the center of the
circle, that is needed to keep a particle moving along a circular path. The magnitude Fc of this force depends on the speed 𝜐 and mass m of the particle, as well as the radius r of the circle:
Fc = mυ2
r (5.3)
In the present situation, the magnetic force furnishes the centripetal force. Being perpendicular
to the velocity, the magnetic force does no work in keeping the charge +q on the circular path. According to Equation 21.1, the magnitude of the magnetic force is given by |q|𝜐B sin 90°, so |q|𝜐B = m𝜐2/r or
r = mυ ∣q∣B
(21.2)
This result shows that the radius of the circle is inversely proportional to the magnitude of the
magnetic fi eld, with stronger fi elds producing “tighter” circular paths. Example 3 illustrates an
application of Equation 21.2.
EXAMPLE 3 The Motion of a Proton
A proton is released from rest at point A, which is located next to the positive plate of a parallel plate capacitor (see Figure 21.12). The proton then accelerates toward the negative plate, leaving the capacitor at point B through a small hole in the plate. The electric potential of the positive plate
is 2100 V greater than that of the negative plate, so VA − VB = 2100 V. Once outside the capacitor, the proton travels at a constant velocity until
it enters a region of constant magnetic fi eld of magnitude 0.10 T. The ve-
locity is perpendicular to the magnetic fi eld, which is directed out of the
page in Figure 21.12. Find (a) the speed 𝜐B of the proton when it leaves the negative plate of the capacitor, and (b) the radius r of the circular path on which the proton moves in the magnetic fi eld.
Reasoning The only force that acts on the proton (charge = +e) while it is between the capacitor plates is the conservative electric force. Thus, we
can use the conservation of energy to fi nd the speed of the proton when
it leaves the negative plate. The total energy of the proton is the sum of
its kinetic energy, 1
2 mυ2, and its electric potential energy, EPE. Following Example 4 in Chapter 19, we set the total energy at point B equal to the total energy at point A:
1
2 mυB2 + EPEB = 1
2 mυA2 + EPEA
We note that 𝜐A = 0 m/s, since the proton starts from rest, and use Equa-
tion 19.4 to set EPEA − EPEB = e(VA − VB). Then the conservation of energy reduces to
1
2 mυB 2 = e(VA − VB). Solving for 𝜐B gives 𝜐B = √2e(VA − VB) /m. The proton enters the magnetic fi eld with this speed and moves on a circular path with a radius that is given by Equation 21.2.
⏟⎵⎵⎵⏟⎵⎵⎵⏟
Total energy at B ⏟⎵⎵⎵⏟⎵⎵⎵⏟
Total energy at A
Solution (a) The speed of the proton is
υB = √2e(VA − VB)m = √ 2(1.60 × 10−19 C)(2100 V)
1.67 × 10−27 kg = 6.3 × 105 m/s
(b) When the proton moves in the magnetic fi eld, the radius of the circular path is
r = mυB eB
= (1.67 × 10−27 kg)(6.3 × 105 m /s)
(1.60 × 10−19 C)(0.10 T) = 6.6 × 10−2 m (21.2)
Parallel plate capacitor
B (out of paper)
r
B
A = 0 m/s
– – – –
+e
+ + + +
FIGURE 21.12 A proton, starting from rest at the positive plate of the capacitor, accelerates toward the negative plate. After leaving the capa-
citor, the proton enters a magnetic fi eld, where it moves on a circular
path of radius r.
One of the important and exciting areas in physics today is the study of elementary particles,
which are the basic building blocks from which all matter is constructed. Important information
about an elementary particle can be obtained from its motion in a magnetic fi eld, with the aid of
a device known as a bubble chamber. A bubble chamber contains a superheated liquid such as
hydrogen, which will boil and form bubbles readily. When an electrically charged particle passes
through the chamber, a thin track of bubbles is left in its wake. This track can be photographed
to show how a magnetic fi eld aff ects the particle motion. Conceptual Example 4 illustrates how
physicists deduce information from such photographs.
598 CHAPTER 21 Magnetic Forces and Magnetic Fields
CONCEPTUAL EXAMPLE 4 Particle Tracks in a Bubble Chamber
Figure 21.13a shows the bubble-chamber tracks resulting from an event that begins at point A. At this point a gamma ray (emitted by certain radioactive substances), traveling in from the left, spontaneously trans-
forms into two charged particles. There is no track from the gamma ray
itself. These particles move away from point A, producing the two spiral tracks. A third charged particle is knocked out of a hydrogen atom and
moves forward, producing the long track with the slight upward curvature.
Each of the three particles has the same mass and carries a charge of the
same magnitude. A uniform magnetic fi eld is directed out of the paper to-
ward you. What is the sign (+ or −) of the charge carried by each particle?
Particle 1 Particle 2 Particle 3 (a) − − +
(b) − + −
(c) + − −
(d) + − +
Reasoning Figure 21.13b shows a positively charged particle traveling with a velocity v→ that is perpendicular to a magnetic fi eld. The fi eld is directed out of the paper, just like it is in part a of the drawing. RHR-1 indicates that the magnetic force points downward. This magnetic force
provides the centripetal force that causes a particle to move on a circular
path (see Section 5.3). The centripetal force is directed toward the center
of the circular path. Thus, in Figure 21.13a a positive charge would move on a downward-curving track, and a negative charge would move on an
upward-curving track.
Answers (a), (c), and (d) are incorrect. Since particles 1 and 3 move on upward-curving tracks, they are negatively charged, not positively charged.
Answer (b) is correct. A downward-curving track in the photograph indicates a positive charge, while an upward-curving track indicates a
negative charge. Thus, particles 1 and 3 carry a negative charge. They are,
in fact, electrons (e−). In contrast, particle 2 carries a positive charge. It is
called a positron (e+), an elementary particle that has the same mass as an
electron but an opposite charge.
Related Homework: Check Your Understanding 5, 6, Problem 26
FIGURE 21.13 (a) A photograph of tracks in a
bubble chamber. A magnetic
fi eld is directed perpen-
dicularly out of the paper.
At point A, a gamma ray (not visible) spontaneously
transforms into two charged
particles, and a third charged
particle is knocked out of
a hydrogen atom in the
chamber. (b) In accord with RHR-1, the magnetic fi eld
applies a downward force to
a positive charged particle
that moves to the right.(b)
(a)
Particle 1
A
Particle 3
Particle 2
R. H. v
B (out of paper)
+q
F
Lawrence Berkeley Laboratory/Science Source
Check Your Understanding
(The answers are given at the end of the book.) 4. Suppose that the positive charge in Figure 21.9a were launched from the negative plate toward the pos-
itive plate, in a direction opposite to the electric fi eld E→. A suffi ciently strong electric fi eld would pre- vent the charge from striking the positive plate. Suppose that the positive charge in Figure 21.9b were launched from the south pole toward the north pole, in a direction opposite to the magnetic fi eld B→. Would a suffi ciently strong magnetic fi eld prevent the charge from reaching the north pole? (a) Yes (b) No, because a magnetic fi eld cannot exert a force on a charged particle that is moving antiparallel to the fi eld (c) No, because the magnetic force would cause the charge to move faster as it moved toward the north pole
5. Review Conceptual Example 4 and Concept Simulation 21.1 at www.wiley.com/college/cutnell as background for this question. Three particles move through a constant magnetic fi eld and follow the paths
shown in CYU Figure 21.2. Determine whether each particle is positively (+) charged, negatively (−) charged, or neutral.
Particle 1 Particle 2 Particle 3 (a) neutral + neutral
(b) − neutral +
(c) − − −
(d) + neutral −
(e) + + +
B (into paper)
1
2 3
CYU FIGURE 21.2
21.4 The Mass Spectrometer 599
6. Suppose that the three particles in Figure 21.13a have identical charge magnitudes and masses. Which particle has the greatest speed? Refer to Conceptual Example 4 as needed.
7. A positive charge moves along a circular path under the infl uence of a magnetic fi eld. The magnetic fi eld is perpendicular to the plane of the circle, as in Interactive Figure 21.11. If the velocity of the particle is reversed at some point along the path, will the particle retrace its path? (a) Yes (b) No, because it will move around a diff erent circle in a counterclockwise direction
8. Refer to Interactive Figure 21.11. Assume that the particle in the picture is a proton. If an electron is projected at point 1 with the same velocity v→, it will not follow exactly the same path as the proton, unless the magnetic fi eld is adjusted in the following manner: the magnitude of the magnetic fi eld must
be ___________, and the direction of the magnetic fi eld must be ___________. (a) the same, reversed (b) increased, the same (c) reduced, reversed
9. CYU Figure 21.3 shows a top view of four interconnected chambers. A negative charge is fi red into chamber 1. By turning on separate mag- netic fi elds in each chamber, the charge can be made to exit from cham-
ber 4, as shown. How should the magnetic fi eld in each chamber be
directed: out of the page or into the page?
Chamber 1 Chamber 2 Chamber 3 Chamber 4 (a) out of into out of into
(b) into out of out of into
(c) out of into into out of
(d) into out of into out of
1
v –q
4 3
2
CYU FIGURE 21.3
B (into paper)
Target
+x+q
+y
–x
–y
CYU FIGURE 21.4
10. CYU Figure 21.4 shows a particle carrying a positive charge +q at the coordinate origin, as well as a target located in the third
quadrant. A uniform magnetic fi eld is directed perpendicularly
into the plane of the paper. The charge can be projected in the
plane of the paper only, along the positive or negative x or y axis. There are four possible directions (+x, −x, +y, −y) for the initial velocity of the particle. The particle can be made to hit the target
for only two of the four directions. Which two directions are they?
(a) +y, −y (b) −y, +x (c) −x, +y (d) +x, −x
21.4 The Mass Spectrometer Physicists use mass spectrometers for determining the relative masses and abundances of
isotopes.* Chemists use these instruments to help identify unknown molecules produced in
chemical reactions. Mass spectrometers are also used during surgery, where they give the
anesthesiologist information on the gases, including the anesthetic, in the patient’s lungs.
THE PHYSICS OF . . . a mass spectrometer. In the type of mass spectrometer illustrated in Figure 21.14, the atoms or molecules are fi rst vaporized and then ionized by the ion source. The ionization process removes one electron from the particle, leaving it with a net positive
charge of +e. The positive ions are then accelerated through the potential diff erence V, which is applied between the ion source and the metal plate. With a speed 𝜐, the ions pass through a hole in
the plate and enter a region of constant magnetic fi eld B→, where they are defl ected in semicircular paths. Only those ions following a path with the proper radius r strike the detector, which records the number of ions arriving per second.
*Isotopes are atoms that have the same atomic number but diff erent atomic masses due to the presence of diff erent
numbers of neutrons in the nucleus. They are discussed in Section 31.1.
–
Ion source
Detector
Metal plate
V
B (out of paper)
m
r
m1
+
FIGURE 21.14 In this mass spectrometer the dashed lines are the paths traveled by ions
of diff erent masses. Ions with mass m follow the path of radius r and enter the detector. Ions with the larger mass m1 follow the outer path and miss the detector.
600 CHAPTER 21 Magnetic Forces and Magnetic Fields
The mass m of the detected ions can be expressed in terms of r, B, and υ by recalling that the radius of the path followed by a particle of charge +e is r = m𝜐/(eB) (Equation 21.2). In addition, the Reasoning section in Example 3 shows that the ion speed 𝜐 can be expressed in terms of the
potential diff erence V as υ = √2eV/m. This expression for the ion speed is the same as that used in Example 3, except that, for convenience, we have replaced the potential diff erence, VA − VB, by the symbol V. Eliminating 𝜐 from these two equations algebraically and solving for the mass gives
m = (er 2
2V)B2 This result shows that the mass of each ion reaching the detector is proportional to B2. Exper- imentally changing the value of B and keeping the term in the parentheses constant will allow ions of diff erent masses to enter the detector. A plot of the detector output as a function of B2 then gives an indication of what masses are present and the abundance of each mass.
Figure 21.15 shows a record obtained by a mass spectrometer for naturally occurring neon gas. The results show that the element neon has three isotopes whose atomic mass numbers are 20, 21,
and 22. These isotopes occur because neon atoms exist with diff erent numbers of neutrons in the
nucleus. Notice that the isotopes have diff erent abundances, with neon-20 being the most abundant.
21.5 The Force on a Current in a Magnetic Field As we have seen, a charge moving through a magnetic fi eld can experience a magnetic force. Since
an electric current is a collection of moving charges, a current in the presence of a magnetic fi eld
can also experience a magnetic force. In Interactive Figure 21.16, for instance, a current-carrying wire is placed between the poles of a magnet. When the direction of the current I is as shown, the moving charges experience a magnetic force that pushes the wire to the right in the drawing. The
direction of the force is determined in the usual manner by using RHR-1, with the minor modifi ca-
tion that the direction of the velocity of a positive charge is replaced by the direction of the conven-
tional current I. If the current in the drawing were reversed by switching the leads to the battery, the direction of the force would be reversed, and the wire would be pushed to the left.
When a charge moves through a magnetic fi eld, the magnitude of the force that acts on the
charge is F = |q|𝜐B sin 𝜃 (Equation 21.1). With the aid of Figure 21.17, this expression can be put into a form that is more suitable for use with an electric current. The drawing shows a wire
of length L that carries a current I. The wire is oriented at an angle 𝜃 with respect to a magnetic fi eld B→. This picture is similar to Figure 21.7c, except that now the charges move in a wire. The magnetic force exerted on this length of wire is the net force acting on the total amount of charge
moving in the wire. Suppose that an amount of conventional positive charge Δq travels the length of the wire in a time interval Δt. The magnitude of the magnetic force on this amount of charge is given by Equation 21.1 as F = (Δq)𝜐B sin 𝜃. Multiplying and dividing the right side of this equation by Δt, we fi nd that
F = ( ∆q ∆ t ) (υ ∆ t) B sin θ
The term Δq/Δt is the current I in the wire (see Equation 20.1), and the term 𝜐Δt is the length L of the wire. With these two substitutions, the expression for the magnetic force exerted on a current-carrying wire becomes
Magnetic force on a current-carrying wire of length L
F = ILB sin θ (21.3)
As in the case of a single charge traveling in a magnetic fi eld, the magnetic force on a current-
carrying wire is a maximum when the wire is oriented perpendicular to the fi eld (𝜃 = 90°) and
vanishes when the current is parallel or antiparallel to the fi eld (𝜃 = 0° or 180°). The direction
of the magnetic force is given by RHR-1, as Figure 21.17 indicates.
I
{
L
{
O ut
pu t
fr om
d et
ec to
r (A
bu nd
an ce
)
20 21 22
(Proportional to atomic mass) B2
FIGURE 21.15 The mass spectrum (not to scale) of naturally occurring neon, showing
three isotopes whose atomic mass numbers
are 20, 21, and 22. The larger the peak, the
more abundant the isotope.
F
B
B
I
I
I
R.H.
S
N +
–
INTERACTIVE FIGURE 21.16 The wire carries a current I, and the bottom segment of the wire is oriented perpendicular to a
magnetic fi eld B→. A magnetic force defl ects the wire to the right.
F
B
B
F
Wire of length L
I
I
θ
R.H.
B
B
FIGURE 21.17 The current I in the wire, oriented at an angle 𝜃 with respect to a magnetic fi eld B→, is acted upon by a magnetic force F→.
21.5 The Force on a Current in a Magnetic Field 601
THE PHYSICS OF . . . a loudspeaker. Most loudspeakers operate on the principle that a magnetic fi eld exerts a force on a current-carrying wire. Figure 21.18a shows a speaker design that consists of three basic parts: a cone, a voice coil, and a permanent magnet. The cone is moun-
ted so it can vibrate back and forth. When vibrating, it pushes and pulls on the air in front of it,
thereby creating sound waves. Attached to the apex of the cone is the voice coil, which is a hollow
cylinder around which coils of wire are wound. The voice coil is slipped over one of the poles of
the stationary permanent magnet (the north pole in the drawing) and can move freely. The two
ends of the voice-coil wire are connected to the speaker terminals on the back panel of a receiver.
The receiver acts as an ac generator, sending an alternating current to the voice coil. The alternat-
ing current interacts with the magnetic fi eld to generate an alternating force that pushes and pulls
on the voice coil and the attached cone. To see how the magnetic force arises, consider Figure 21.18b, which is a cross-sectional view of the voice coil and the magnet. In the cross-sectional view, the current is directed into the page in the upper half of the voice coil ( × × × ) and out of the
page in the lower half ( ). In both cases the magnetic fi eld is perpendicular to the current, so
the maximum possible force is exerted on the wire. An application of RHR-1 to both the upper
and lower halves of the voice coil shows that the magnetic force F→ in the drawing is directed to the right, causing the cone to accelerate in that direction. One-half of a cycle later when the cur-
rent is reversed, the direction of the magnetic force is also reversed, and the cone accelerates to
the left. If, for example, the alternating current from the receiver has a frequency of 1000 Hz, the
alternating magnetic force causes the cone to vibrate back and forth at the same frequency, and a
1000-Hz sound wave is produced. Thus, it is the magnetic force on a current-carrying wire that
is responsible for converting an electrical signal into a sound wave. In Example 5 a typical force
and acceleration in a loudspeaker are determined.
Problem-Solving Insight Whenever the current in a wire reverses direction, the force exerted on the wire by a given magnetic fi eld also reverses direction.
FIGURE 21.18 (a) An “exploded” view of one type of speaker design, which shows a
cone, a voice coil, and a permanent magnet.
(b) Because of the current in the voice coil (shown as × and ), the magnetic fi eld
causes a force F→ to be exerted on the voice coil and cone.
S
S
N
F
(a) (b)
F
Magnetic fieldCone
Voice coil
Permanent magnet
Back panel of receiver
Speaker terminals
S
S
N
EXAMPLE 5 The Force and Acceleration in a Loudspeaker
The voice coil of a speaker has a diameter of d = 0.025 m, contains 55 turns of wire, and is placed in a 0.10-T magnetic fi eld. The current in the
voice coil is 2.0 A. (a) Determine the magnetic force that acts on the coil and cone. (b) The voice coil and cone have a combined mass of 0.020 kg. Find their acceleration.
Reasoning The magnetic force that acts on the current-carrying voice coil is given by Equation 21.3 as F = ILB sin 𝜃. The eff ective length L of the wire in the voice coil is very nearly the number of turns N times the circumference (𝜋d) of one turn: L = N𝜋d. The acceleration of the voice coil and cone is given by Newton’s second law as the magnetic force di-
vided by the combined mass.
Solution (a) Since the magnetic fi eld acts perpendicular to all parts of the wire, 𝜃 = 90° and the force on the voice coil is
F = ILB sin θ = I (Nπd ) B sin θ = (2.0 A)[55π (0.025 m)](0.10 T)sin 90° = 0.86 N (21.3)
(b) According to Newton’s second law, the acceleration of the voice coil and cone is
a = F m
= 0.86 N
0.020 kg = 43 m /s2 (4.1)
This acceleration is more than four times the acceleration due to gravity.
602 CHAPTER 21 Magnetic Forces and Magnetic Fields
Check Your Understanding
(The answers are given at the end of the book.) 11. Refer to Interactive Figure 21.16. (a) What happens to the direction of the magnetic force if the cur-
rent is reversed? (b) What happens to the direction of the force if both the current and the magnetic poles are reversed?
12. The same current-carrying wire is placed in the same magnetic fi eld B→ in four diff erent orientations (see CYU Figure 21.5). Rank the orientations according to the magnitude of the magnetic force exer- ted on the wire, largest to smallest.
B
I (into paper)
I
A
B
I
B
B
I
C
B
D
CYU FIGURE 21.5
21.6 The Torque on a Current-Carrying Coil We have seen that a current-carrying wire can experience a force when placed in a magnetic fi eld.
If a loop of wire is suspended properly in a magnetic fi eld, the magnetic force produces a torque
that tends to rotate the loop. This torque is responsible for the operation of a widely used type of
electric motor.
Figure 21.19a shows a rectangular loop of wire attached to a vertical shaft. The shaft is mounted so that it is free to rotate in a uniform magnetic fi eld. When there is a current in the loop,
the loop rotates because magnetic forces act on the vertical sides, labeled 1 and 2 in the drawing.
Part b shows a top view of the loop and the magnetic forces F→ and −F→ that act on the two sides. These two forces have the same magnitude, but an application of RHR-1 shows that they point
in opposite directions, so the loop experiences no net force. The loop does, however, experience
a net torque that tends to rotate it in a clockwise fashion about the vertical shaft. Figure 21.20a shows that the torque is maximum when the normal to the plane of the loop is perpendicular to
the fi eld. In contrast, part b shows that the torque is zero when the normal is parallel to the fi eld. When a current-carrying loop is placed in a magnetic fi eld, the loop tends to rotate such that its normal becomes aligned with the magnetic fi eld. In this respect, a current loop behaves like a magnet (e.g., a compass needle) suspended in a magnetic fi eld, since a magnet also rotates to
align itself with the magnetic fi eld.
1
2 B
B
(a)
I
I
Shaft
B
(b)
Side 1
Side 2
Line of
action
Normal
F
– F
ϕ
ϕ 2 w
FIGURE 21.19 (a) A current-carrying loop of wire, which can rotate about a vertical
shaft, is situated in a magnetic fi eld. (b) A top view of the loop. The current in side 1
is directed out of the page ( ), while the
current in side 2 is directed into the page
( × ). The current in side 1 experiences a
force F→ that is opposite to the force −F→ exerted on side 2. The two forces produce a
clockwise torque about the shaft.
B
(a) Maximum torque (b) Zero torque
F
F
– F
– F
Normal
Normal 90°
B
FIGURE 21.20 (a) Maximum torque occurs when the normal to the plane of the loop is perpendicular to the magnetic fi eld.
(b) The torque is zero when the normal is parallel to the fi eld.
21.6 The Torque on a Current-Carrying Coil 603
It is possible to determine the magnitude of the torque on the loop in Figure 21.19a. From Equation 21.3 the magnetic force on each vertical side has a magnitude of F = ILB sin 90°, where L is the length of side 1 or side 2, and 𝜃 = 90° because the current I always remains perpendicular to the magnetic fi eld as the loop rotates. As Section 9.1 discusses, the torque produced by a force
is the product of the magnitude of the force and the lever arm. In Figure 21.19b the lever arm 𝓁 is the perpendicular distance from the line of action of the force to the shaft. This distance is
given by 𝓁 = (w/2) sin 𝜙, where w is the width of the loop, and 𝜙 is the angle between the normal to the plane of the loop and the direction of the magnetic fi eld. The net torque is the sum of the
torques on the two sides, so
Net torque = τ = ILB ( 12 w sin ϕ) + ILB ( 1
2 w sin ϕ) = IAB sin ϕ
In this result the product Lw has been replaced by the area A of the loop. If the wire is wrapped so as to form a coil containing N loops, each of area A, the force on each side is N times larger, and the torque becomes proportionally greater:
τ = NIA (B sin ϕ) (21.4)
Equation 21.4 has been derived for a rectangular coil, but it is valid for any shape of fl at coil,
such as a circular coil. The torque depends on the geometric properties of the coil and the current
in it through the quantity NIA. This quantity is known as the magnetic moment of the coil, and its unit is ampere · meter2 (A · m2). The greater the magnetic moment of a current-carrying coil, the greater is the torque that the coil experiences when placed in a magnetic fi eld. Example 6
discusses the torque that a magnetic fi eld applies to such a coil.
Magnetic
moment
{
Math Skills To understand why the lever arm for the torque calculation is 𝓁 = (w/2)sin 𝜙, it is fi rst necessary to know why the two angles labeled 𝜙 in Figure 21.19b are equal. Referring to Figure 21.21a and noting that the normal is perpendicular to the plane of the loop, we can see that 𝛼 + 𝜙 = 90° or 𝛼 = 90° − 𝜙. Furthermore, the force −F→ is perpendicular to the magnetic fi eld B→, so the triangle including angles 𝛼 and 𝛽 is a right triangle. Therefore, it follows that 𝛼 + 𝛽 = 90°. Solving this equation gives 𝛽 = 90° − 𝛼, and substituting 𝛼 = 90° − 𝜙 reveals that
β = 90° − α = 90° − (90° − ϕ) = ϕ
Recognizing that the two angles labeled 𝜙 in Figure 21.19b are equal, we can now understand why the lever arm is 𝓁 = (w/2)sin 𝜙 for the force −F→. According to the defi nition given in Equation 1.1,
the sine function is sin ϕ = ho h
, where ho is the length of the side of a right triangle that is opposite
the angle 𝜙 and h is the length of the hypotenuse (see Figure 21.21b). By comparing Figure 21.21b with Figure 21.21c, we can see that
sin ϕ = ho h
= ℓ
w/2 or ℓ =
w 2
sin ϕ
𝛼 ⏟⎵⏟⎵⏟
B
(a)
Side 2
Normal
– F
ϕ
β α
Line of
action
2 w
(c)
Side 2
Normal
ϕ
ℓ
(b)
ϕh
ho
90°
FIGURE 21.21 Math Skills drawing.
604 CHAPTER 21 Magnetic Forces and Magnetic Fields
EXAMPLE 6 The Torque Exerted on a Current-Carrying Coil
A coil of wire has an area of 2.0 × 10−4 m2, consists of 100 loops or turns,
and contains a current of 0.045 A. The coil is placed in a uniform magnetic
fi eld of magnitude 0.15 T. (a) Determine the magnetic moment of the coil. (b) Find the maximum torque that the magnetic fi eld can exert on the coil.
Reasoning and Solution (a) The magnetic moment of the coil is
Magnetic moment = NIA = (100)(0.045 A)(2.0 × 10−4 m2 ) = 9.0 × 10−4 A · m2
(b) According to Equation 21.4, the torque is the product of the magnetic moment NIA and B sin 𝜙. However, the maximum torque occurs when 𝜙 = 90°, so
τ = (NIA) (B sin 90°) = (9.0 × 10−4 A · m2)(0.15 T) = 1.4 × 10−4 N · m Magnetic
moment
{
THE PHYSICS OF . . . a direct-current electric motor. The electric motor is found in many devices, such as CD players, automobiles, washing machines, and air conditioners.
Figure 21.22 shows that a direct-current (dc) motor consists of a coil of wire placed in a magnetic fi eld and free to rotate about a vertical shaft. The coil of wire contains many turns and is wrapped
around an iron cylinder that rotates with the coil, although these features have been omitted to
simplify the drawing. The coil and iron cylinder assembly is known as the armature. Each end
of the wire coil is attached to a metallic half-ring. Rubbing against each of the half-rings is a
graphite contact called a brush. While the half-rings rotate with the coil, the graphite brushes
remain stationary. The two half-rings and the associated brushes are referred to as a split-ring
commutator (see below).
The operation of a motor can be understood by considering Figure 21.23. In part a the cur- rent from the battery enters the coil through the left brush and half-ring, goes around the coil,
and then leaves through the right half-ring and brush. Consistent with RHR-1, the directions of
the magnetic forces F→ and −F→ on the two sides of the coil are as shown in the drawing. These forces produce the torque that turns the coil. Eventually, the coil reaches the position shown in
part b of the drawing. In this position the half-rings momentarily lose electrical contact with the brushes, so that there is no current in the coil and no applied torque. However, like any
moving object, the rotating coil does not stop immediately, for its inertia carries it onward.
When the half-rings reestablish contact with the brushes, there again is a current in the coil,
and a magnetic torque again rotates the coil in the same direction. The split-ring commutator
ensures that the current is always in the proper direction to yield a torque that produces a con-
tinuous rotation of the coil.
Shaft
Armature (iron core
not shown)
Brush
Half-rings
Brush
CD platter
FIGURE 21.22 The basic components of a dc motor. A CD platter is shown as it might
be attached to the motor.
+ – + –I
I
I
I
(a)
– F
B
F
(b)
B
FIGURE 21.23 (a) When a current exists in the coil, the coil experiences a torque. (b) Because of its inertia, the coil continues to rotate when there is no current.
21.7 Magnetic Fields Produced by Currents 605
21.7 Magnetic Fields Produced by Currents We have seen that a current-carrying wire can experience a magnetic force when placed in a mag-
netic fi eld that is produced by an external source, such as a permanent magnet. A current-carrying wire also produces a magnetic fi eld of its own, as we will see in this section. Hans Christian Oersted (1777–1851) fi rst discovered this eff ect in 1820 when he observed that a current-carrying
wire infl uences the orientation of a nearby compass needle. The compass needle aligns itself with
the net magnetic fi eld produced by the current and the magnetic fi eld of the earth. Oersted’s dis-
covery, which linked the motion of electric charges with the creation of a magnetic fi eld, marked
the beginning of an important discipline called electromagnetism.
A Long, Straight Wire Figure 21.24a illustrates Oersted’s discovery with a very long, straight wire. When a current is present, the compass needles point in a circular pattern about the wire. The pattern indicates that
the magnetic fi eld lines produced by the current are circles centered on the wire. If the direction
of the current is reversed, the needles also reverse their directions, indicating that the direction of
the magnetic fi eld has reversed. The direction of the fi eld can be obtained by using Right-Hand Rule No. 2 (RHR-2), as part b of the drawing indicates:
Right-Hand Rule No. 2. Curl the fi ngers of the right hand into the shape of a half-circle. Point the thumb in the direction of the conventional current I, and the tips of the fi ngers will point in the direction of the magnetic fi eld B→. Experimentally, it is found that the magnitude B of the magnetic fi eld produced by an in-
fi nitely long, straight wire is directly proportional to the current I and inversely proportional to the radial distance r from the wire: B ∝ I/r. As usual, this proportionality is converted into an equation by introducing a proportionality constant, which, in this instance, is written as 𝜇0/(2𝜋). Thus, the magnitude of the magnetic fi eld is
Infi nitely long, straight wire B = μ 0 I 2πr
(21.5)
The constant 𝜇0 is referred to as the permeability of free space, and its value is 𝜇0 = 4𝜋 × 10−7 T · m/A. The magnetic fi eld becomes stronger nearer the wire, where r is smaller. Therefore, the fi eld lines near the wire are closer together than those located farther away, where the fi eld is
weaker. Figure 21.25 shows the pattern of fi eld lines. The magnetic fi eld that surrounds a current-carrying wire can exert a force on a moving
charge, as the next example illustrates.
(a)
(b)
I
R.H. RHR–2
I
B
FIGURE 21.24 (a) A very long, straight, current-carrying wire produces magnetic
fi eld lines that are circular about the wire, as
indicated by the compass needles. (b) With the thumb of the right hand (R.H.) along
the current I, the curled fi ngers point in the direction of the magnetic fi eld, according to
RHR-2.
r
I
FIGURE 21.25 The magnetic fi eld becomes stronger as the radial distance r decreases, so the fi eld lines are closer together near the wire.
Analyzing Multiple-Concept Problems
EXAMPLE 7 A Current Exerts a Magnetic Force on a Moving Charge
Figure 21.26 shows a very long, straight wire carrying a current of 3.0 A. A particle has a charge of +6.5 × 10−6 C and is moving parallel to the wire
at a distance of 0.050 m. The speed of the particle is 280 m/s. Determine
the magnitude and direction of the magnetic force exerted on the charged
particle by the current in the wire.
Reasoning The current generates a magnetic fi eld in the space around the wire. The charged particle moves in the presence of this fi eld and,
therefore, can experience a magnetic force. The magnitude of this force is
given by Equation 21.1, and the direction can be determined by applying
RHR-1 (see Section 21.2). Note in Figure 21.26 that the magnetic fi eld B→ produced by the current lies in a plane that is perpendicular to both the wire and the velocity v→ of the particle. Thus, the angle between B→ and v→ is θ = 90.0°.
F
v
B
q0
B
F
v
R.H.
I
FIGURE 21.26 The positive charge q0 moves with a velocity v→ and experiences a magnetic force
F→ because of the magnetic fi eld B→ produced by the current in the wire.
606 CHAPTER 21 Magnetic Forces and Magnetic Fields
We have now seen that an electric current can create a magnetic fi eld of its own. Ear-
lier, we have also seen that an electric current can experience a force created by another
magnetic fi eld. Therefore, the magnetic fi eld that one current creates can exert a force on
another nearby current. Conceptual Example 8 deals with this magnetic interaction between
currents.
Modeling the Problem
STEP 1 Magnetic Force on the Particle The magnitude F of the magnetic force acting on the charged particle is given at the right by Equation 21.1, where ∣q0∣ is the magnitude of the charge, 𝜐 is the particle speed, B is the magnitude of the magnetic fi eld produced by the wire, and 𝜃 is the angle between the particle velocity and the magnetic fi eld. Values for ∣q0∣, 𝜐, and 𝜃 are given. The value of B, however, is unknown, and we determine it in Step 2.
STEP 2 Magnetic Field Produced by the Wire The magnitude B of the magnetic fi eld pro- duced by a current I in an infi nitely long, straight wire is given by Equation 21.5:
B = μ 0I 2πr
(21.5)
where 𝜇0 is the permeability of free space and r is the distance from the wire. This expression can be substituted into Equation 21.1, as shown at the right.
Solution Combining the results of each step algebraically, we fi nd that
F = |q0|𝜐B sin 𝜃 = |q0|𝜐 ( μ0 I 2πr) sin θ
The magnitude of the magnetic force on the charged particle is
F = ∣q0∣υ ( μ 0 I 2πr) sin θ
= (6.5 × 10−6 C)(280 m /s) (4π × 10−7 T · m/A)(3.0 A)
2π (0.050 m) sin 90.0° = 2.2 × 10−8 N
The direction of the magnetic force is predicted by RHR-1 and, as shown in Figure 21.26, is radially inward toward the wire.
Related Homework: Problem 76
STEP 1 STEP 2
F = |q0|𝜐B sin 𝜃 (21.1)
?
F = |q0|𝜐B sin 𝜃 (21.1)
B = μ 0I 2πr
(21.5)
Knowns and Unknowns The following list summarizes the data that are given:
Description Symbol Value Comment Explicit Data Current in wire I 3.0 A
Electric charge of particle q0 +6.5 × 10−6 C
Distance of particle from wire r 0.050 m Particle moves parallel to wire; see Figure 21.26.
Speed of particle 𝜐 280 m/s
Implicit Data Directional angle of particle velocity with respect
to magnetic field
𝜃 90.0° Particle moves parallel to wire; see Reasoning.
Unknown Variable Magnitude of magnetic force exerted on particle F ?
21.7 Magnetic Fields Produced by Currents 607
A Loop of Wire If a current-carrying wire is bent into a circular loop, the magnetic fi eld lines around the loop
have the pattern shown in Figure 21.28a. At the center of a loop of radius R, the magnetic fi eld is perpendicular to the plane of the loop and has the value B = 𝜇0I/(2R), where I is the current in the loop. Often, the loop consists of N turns of wire that are wound suffi ciently close together that they form a fl at coil with a single radius. In this case, the magnetic fi elds of the individual turns
add together to give a net fi eld that is N times greater than the fi eld of a single loop. For such a coil the magnetic fi eld at the center is
Center of a circular loop B = N μ 0 I 2R
(21.6)
CONCEPTUAL EXAMPLE 8 The Net Force That a Current-Carrying Wire Exerts on a Current-Carrying Coil
Figure 21.27 shows a very long, straight wire carrying a current I1 and a rectangular coil carrying a current I2. The wire and the coil lie in the same plane, with the wire parallel to the long sides of the rectangle. The coil is
(a) attracted to the wire, (b) repelled from the wire, (c) neither attracted to nor repelled from the wire.
Reasoning The current in the straight wire exerts a force on each of the four sides of the coil. The net force acting on the coil is the vector
sum of these four forces. To determine whether the net force is attractive,
repulsive, or neither, we need to consider the directions and magnitudes
of the individual forces. For each side of the rectangular coil we will fi rst
use RHR-2 to determine the direction of the magnetic fi eld produced by
the long, straight wire. Then, we will employ RHR-1 to fi nd the direction
of the magnetic force exerted on each side.
It should be noted that the magnetic forces that act on the two short
sides of the rectangular coil play no role. To see why, consider a small
segment of each of the short sides, located at the same distance from the
straight wire, as indicated by the dashed line in Figure 21.27. Each of these segments experiences the same magnetic fi eld from the current I1. RHR-2 shows that this fi eld is directed downward into the plane of
the paper, so that it is perpendicular to the current I2 in each segment. However, the directions of I2 in the segments are opposite. As a result, RHR-1 reveals that the magnetic fi eld from the straight wire applies a
magnetic force to one segment that is opposite to the magnetic force
applied to the other segment. Thus, the forces on the two short sides of
the coil cancel.
Answers (b) and (c) are incorrect. There is indeed a net magnetic force that acts on the rectangular coil, but it is not a force that repels the coil
from the straight wire. To see why, consider the following explanation.
Answer (a) is correct. In the long side of the coil near the wire, the cur- rent I2 has the same direction as the current I1, and two such currents attract each other. In the other long side of the coil the current I2 has a direction op- posite to that of I1, and they repel one another. However, the attractive force is stronger than the repulsive force because the magnetic fi eld produced by
the current I1 is stronger at shorter distances than at greater distances. Con- sequently, the rectangular coil is attracted to the long, straight wire.
I1
Segment Segment
I2
FIGURE 21.27 A very long, straight wire carries a current I1, and a rectangular coil carries a current I2. The dashed line is parallel to the wire and locates a small segment on
each short side of the coil.
+–
I
(a) (b)
B
R.H.
FIGURE 21.28 (a) The magnetic fi eld lines in the vicinity of a current-carrying circular
loop. (b) The direction of the magnetic fi eld at the center of the loop is given by RHR-2.
608 CHAPTER 21 Magnetic Forces and Magnetic Fields
The direction of the magnetic fi eld at the center of the loop can be determined with the help of
RHR-2. If the thumb of the right hand is pointed in the direction of the current and the curled
fi ngers are placed at the center of the loop, as in Figure 21.28b, the fi ngers indicate that the mag- netic fi eld points from right to left.
Example 9 shows how the magnetic fi elds produced by the current in a loop of wire and the
current in a long, straight wire combine to form a net magnetic fi eld.
EXAMPLE 9 Finding the Net Magnetic Field
A long, straight wire carries a current of I1 = 8.0 A. As Figure 21.29a illustrates, a circular loop of wire lies immediately to the right of the
straight wire. The loop has a radius of R = 0.030 m and carries a current of I2 = 2.0 A. Assuming that the thickness of each wire is negligible, fi nd the magnitude and direction of the net magnetic fi eld at the center C of the loop.
Reasoning The net magnetic fi eld at the point C is the sum of two contributions: (1) the fi eld B1
→ produced by the long, straight wire ac-
cording to Equation 21.5 [B1 = 𝜇0 I1/(2𝜋r)], and (2) the fi eld B2 →
pro-
duced by the circular loop according to Equation 21.6 with N = 1 [B2 = 𝜇0 I2/(2 R)]. An application of RHR-2 shows that at point C the fi eld B1
→
is directed upward, perpendicular to the plane containing the straight
wire and the loop (see part b of the drawing). Similarly, RHR-2 shows that the magnetic fi eld B2
→ is directed downward, opposite to the direc-
tion of B1 →
.
Problem-Solving Insight Do not confuse the formula for the magnetic fi eld produced at the center of a circular loop with that of a very long, straight wire. The formulas are similar, diff ering only by a factor of 𝞹 in the denominator.
Solution If we choose the upward direction in Figure 21.29b as positive, the net magnetic fi eld at point C is
B = μ0 I1 2πr −
μ0 I2 2R
= μ0 2
( I1 πr
− I2 R)
B = (4π × 10−7 T · m /A)
2 [ 8.0 Aπ (0.030 m) −
2.0 A
0.030 m ] = 1.1 × 10−5 T The net fi eld is positive, so it is directed upward, perpendicular to the plane.
Long,
straight wire {
Center of a
circular loop
{
I1
C C
(a) (b)
I2
B1
B2
FIGURE 21.29 (a) A long, straight wire carrying a cur-
rent I1 lies next to a circular loop that carries a current I2. (b) The magnetic fi elds at the center C of the loop produced by the straight wire
(B1 →
) and the loop (B2 →
).
A comparison of the magnetic fi eld lines around the current loop in Figure 21.28a with those in the vicinity of the short bar magnet in Figure 21.30a shows that the two patterns are similar. Not only are the patterns similar, but the loop itself behaves as a bar magnet with a “north pole”
on one side and a “south pole” on the other side. To emphasize that the loop may be imagined
to be a bar magnet, Figure 21.30b includes a “phantom” bar magnet at the center of the loop. The side of the loop that acts like a north pole can be determined with the aid of RHR-2: curl
the fi ngers of the right hand into the shape of a half-circle, point the thumb along the current I, and place the curled fi ngers at the center of the loop. The fi ngers not only point in the direction
of B→, but they also point toward the north pole of the loop.
(b)(a)
R.H.
Phantom bar magnet
SN
N S
North pole
I
FIGURE 21.30 (a) The fi eld lines around the bar magnet resemble those around the
loop in Figure 21.28a. (b) The current loop can be imagined to be a “phantom” bar
magnet with a north pole and a south pole.
21.7 Magnetic Fields Produced by Currents 609
Because a current-carrying loop acts like a bar magnet, two adjacent loops can be either
attracted to or repelled from each other, depending on the relative directions of the currents.
Figure 21.31 includes a “phantom” magnet for each loop and shows that the loops are attracted to each other when the currents are in the same direction and repelled from each other when the
currents are in opposite directions.
A Solenoid A solenoid is a long coil of wire in the shape of a helix (see Figure 21.32). If the wire is wound so the turns are packed close to each other and the solenoid is long compared to its diameter, the
magnetic fi eld lines have the appearance shown in the drawing. Notice that the fi eld inside the
solenoid and away from its ends is nearly constant in magnitude and directed parallel to the axis.
The direction of the fi eld inside the solenoid is given by RHR-2, just as it is for a circular current
loop. The magnitude of the magnetic fi eld in the interior of a long solenoid is
Interior of a long solenoid
B = μ 0 nI (21.7)
where n is the number of turns per unit length of the solenoid and I is the current. If, for example, the solenoid contains 100 turns and has a length of 0.05 m, the number of turns per unit length is
n = (100 turns)/(0.05 m) = 2000 turns/m. The magnetic fi eld outside the solenoid is not constant and is much weaker than the interior fi eld. In fact, the magnetic fi eld outside is nearly zero if the
length of the solenoid is much greater than its diameter.
As with a single loop of wire, a solenoid can also be imagined to be a bar magnet, for the
solenoid is just an array of connected current loops. And, as with a circular current loop, the
location of the north pole can be determined with RHR-2. Figure 21.32 shows that the left end of the solenoid acts as a north pole, and the right end behaves as a south pole. Solenoids are often
referred to as electromagnets, and they have several advantages over permanent magnets. For one thing, the strength of the magnetic fi eld can be altered by changing the current and/or the
number of turns per unit length. Furthermore, the north and south poles of an electromagnet can
be readily switched by reversing the current.
BIO THE PHYSICS OF . . . magnetic resonance imaging (MRI). Applications of the magnetic fi eld produced by a current-carrying solenoid are widespread. An important medical
application is in magnetic resonance imaging (MRI). With this technique, detailed pictures of the
internal parts of the body can be obtained in a noninvasive way that involves none of the risks
inherent in the use of X-rays. Figure 21.33 shows a magnetic resonance imaging machine being
SN
SN
NS
(a) Attraction
(b) Repulsion
Note current reversal
SN
FIGURE 21.31 (a) The two current loops attract each other if the directions of the currents
are the same and (b) repel each other if the directions are opposite. The “phantom” magnets
help explain the attraction and repulsion.
R.H.
North pole
Solenoid
+ – II
N S
FIGURE 21.32 A solenoid and a cross-sectional view of it, showing the magnetic fi eld lines and the north and south poles.
FIGURE 21.33 A magnetic resonance imaging (MRI) machine being used. The
circular opening in which the patient is
positioned provides access to the interior of
a solenoid. MRI scans of the knee are shown
on the monitor.
Pixtal/SuperStock
610 CHAPTER 21 Magnetic Forces and Magnetic Fields
used. The circular opening visible in the photograph provides access to the interior of a solenoid,
which is typically made from superconducting wire. The superconducting wire facilitates the
use of a large current to produce a strong magnetic fi eld. In the presence of this fi eld, the nuclei
of certain atoms can be made to behave as tiny radio transmitters and emit radio waves similar
to those used by FM stations. The hydrogen atom, which is so prevalent in the human body, can
be made to behave in this fashion. The strength of the magnetic fi eld determines where a given
collection of hydrogen atoms will “broadcast” on an imaginary FM dial. With a magnetic fi eld
that has a slightly diff erent strength at diff erent places, it is possible to associate the location on
this imaginary FM dial with a physical location within the body. Computer processing of these
locations produces the magnetic resonance image. When hydrogen atoms are used in this way,
the image is essentially a map showing their distribution within the body. Remarkably detailed
images can now be obtained, such as the one in Figure 21.34. They provide doctors with a powerful diagnostic tool that complements those from X-ray and other techniques. Surgeons can
now perform operations more accurately by stepping inside specially designed MRI scanners
along with the patient and seeing live images of the area into which they are cutting.
THE PHYSICS OF . . . television screens and computer display monitors. Some televi- sion sets and some computer display monitors use electromagnets (solenoids) to produce images
by exerting magnetic forces on moving electrons. An evacuated glass tube, called a cathode-ray
tube (CRT), contains an electron gun that sends a narrow beam of high-speed electrons toward
the screen of the tube, as Figure 21.35a illustrates. The inner surface of the screen is covered with a phosphor coating, and when the electrons strike it, they generate a spot of visible light.
This spot is called a pixel (a contraction of “picture element”).
To create a black-and-white picture, the electron beam is scanned rapidly from left to right
across the screen. As the beam makes each horizontal scan, the number of electrons per second
striking the screen is changed by electronics controlling the electron gun, making the scan line
brighter in some places and darker in others. When the beam reaches the right side of the screen,
it is turned off and returned to the left side slightly below where it started (see Figure 21.35b). The beam is then scanned across the next line, and so on. In current TV sets, a complete picture
consists of 525 scan lines (or 625 in Europe) and is formed in 1
30 of a second. High-defi nition TV
sets have about 1100 scan lines, giving a much sharper, more detailed picture.
The electron beam is defl ected by a pair of electromagnets placed around the neck of the
tube, between the electron gun and the screen. One electromagnet is responsible for producing
the horizontal defl ection of the beam and the other for the vertical defl ection. For clarity, Figure 21.35a shows the net magnetic fi eld generated by the electromagnets at one instant, and not the electromagnets themselves. The electric current in the electromagnets produces a net magnetic
fi eld that exerts a force on the moving electrons, causing their trajectories to bend and reach
diff erent points on the screen. Changing the current changes the fi eld, so the electrons can be
defl ected to any point on the screen.
FIGURE 21.34 Magnetic resonance imaging provides one way to diagnose brain disorders.
This color-enhanced MRI scan shows the
brain of a patient with a large pineal region
meningioma (see the red circular region),
which is a usually benign, slow-growing tumor.
Living Art Enterprises/Science Source
(c)
Cathode-ray tube
Deflection magnetic
field
Electron gun
(a) (b)
Electron beam
Pixel
Phosphor-coated screen
FIGURE 21.35 (a) A cathode-ray tube contains an electron gun, a magnetic fi eld for defl ecting the electron beam, and a phosphor-coated screen. A CRT color TV actually uses three guns, although only one is shown
here for clarity. (b) The image is formed by scanning the electron beam across the screen. (c) The red, green, and blue phosphors of a color TV.
21.7 Magnetic Fields Produced by Currents 611
A color TV operates with three electron guns instead of one. Furthermore, the single phos-
phor of a black-and-white TV is replaced by a large number of three-dot clusters of phosphors
that glow red, green, and blue when struck by an electron beam, as indicated in Figure 21.35c. Each red, green, and blue color in a cluster is produced when electrons from one of the three
guns strike the corresponding phosphor dot. The three dots are so close together that, from a nor-
mal viewing distance, they cannot be separately distinguished. Red, green, and blue are primary
colors, so virtually all other colors can be created by varying the intensities of the three beams
focused on a cluster.
Check Your Understanding
(The answers are given at the end of the book.) 13. CYU Figure 21.6 shows a conducting wire wound into a helical
shape. The helix acts like a spring and expands back toward its
original shape after the coils are squeezed together and released.
The bottom end of the wire just barely touches the mercury
(a good electrical conductor) in the cup. After the switch is
closed, current in the circuit causes the light bulb to glow. Does
the bulb (a) repeatedly turn on and off like a turn signal on a car, (b) glow continually, or (c) glow briefl y and then go out?
14. For each electromagnet at the left in CYU Figure 21.7, will it be attracted to or repelled from the permanent magnet immedi-
ately to its right?
15. For each electromagnet at the left in CYU Figure 21.8, will it be attracted to or repelled from the electromagnet immediately to
its right?
16. Refer to Figure 21.5. If the earth’s magnetism is assumed to ori- ginate from a large circular loop of current within the earth, then
the plane of the current loop must be oriented ___________ to the
earth’s magnetic axis, and the direction of the current around the
loop (when looking down on the loop from the north magnetic
pole) is __________. (a) parallel, clockwise (b) parallel, counter- clockwise (c) perpendicular, clockwise (d) perpendicular, coun- terclockwise
17. CYU Figure 21.9 shows an end-on view of three parallel wires that are perpendicular to the plane of the paper. In two of the wires the cur-
rent is directed into the paper, while in the remaining wire the current
is directed out of the paper. The two outermost wires are held rigidly
in place. Which way will the middle wire move? (a) To the left (b) To the right (c) It will not move at all.
18. In CYU Figure 21.10, assume that the current I1 is larger than the current I2. In parts a and b, decide whether there are places at which the total magnetic fi eld is zero. State whether these places are located to the left of both wires, between
the wires, or to the right of both wires.
Attraction
(b)
F
B
–F
I1 I2
Repulsion
(a)
F
B
–F I1 I2
Wire 1 Wire 2
CYU FIGURE 21.10
19. Each of the four drawings CYU Figure 21.11 shows the same three concentric loops of wire. The cur- rents in the loops have the same magnitude I and have the directions shown. Rank the magnitude of the net magnetic fi eld produced at the center of each of the four drawings, largest to smallest.
+ –Mercury Switch
CYU FIGURE 21.6
(a)
(b)
CYU FIGURE 21.8
Current
CYU FIGURE 21.9
(a) N S
N S(b)
CYU FIGURE 21.7
612 CHAPTER 21 Magnetic Forces and Magnetic Fields
I
A
I
B
I
C
I
D
CYU FIGURE 21.11
20. There are four wires viewed end-on in CYU Figure 21.12. They are long, straight, and perpendicular to the plane of the paper. Their cross sections lie at the corners of a square. The magnitude of the current
in each wire is the same. What must be the direction of the current in each wire (into or out of the page),
so that when any single current is turned off , the total magnetic fi eld at P (the center of the square) is directed toward a corner of the square?
Wire 1 Wire 2 Wire 3 Wire 4 (a) out of out of into out of
(b) into out of into into
(c) out of into out of out of
(d) into into into into CYU FIGURE 21.12
Wire 1 Wire 2
Wire 4 Wire 3
P
21.8 Ampère’s Law We have seen that an electric current creates a magnetic fi eld. However, the magnitude and dir-
ection of the fi eld at any point in space depends on the specifi c geometry of the wire carrying
the current. For instance, distinctly diff erent magnetic fi elds surround a long, straight wire, a
circular loop of wire, and a solenoid. Although diff erent, each of these fi elds can be obtained
from a general law known as Ampère’s law, which is valid for a wire of any geometrical shape. Ampère’s law specifi es the relationship between an electric current and the magnetic fi eld that
it creates.
To see how Ampère’s law is stated, consider Figure 21.36, which shows two wires carrying currents I1 and I2. In general, there may be any number of currents. Around the wires we construct an arbitrarily shaped but closed path. This path encloses a surface and is constructed from a large
number of short segments, each of length Δ𝓁. Ampère’s law deals with the product of Δ𝓁 and
B‖ for each segment, where B‖ is the component of the magnetic fi eld that is parallel to Δ𝓁 (see the blow-up view in the drawing). For magnetic fi elds that do not change as time passes, the law
states that the sum of all the B‖ Δ𝓁 terms is proportional to the net current I passing through the surface enclosed by the path. For the specifi c example in Figure 21.36, we see that I = I1 + I2. Ampère’s law is stated in equation form as follows:
AMPÈRE’S LAW FOR STATIC MAGNETIC FIELDS For any current geometry that produces a magnetic fi eld that does not change in time,
ΣB‖∆ℓ = μ0 I (21.8)
where Δℓ is a small segment of length along a closed path of arbitrary shape around the current, B‖ is the component of the magnetic fi eld parallel to Δℓ, I is the net current passing through the surface bounded by the path, and 𝞵0 is the permeability of free space. The symbol Σ indicates that the sum of all B‖ Δℓ terms must be taken around the closed path.
To illustrate the use of Ampère’s law, we apply it in Example 10 to the special case of the
current in a long, straight wire and show that it leads to the proper expression for the magnetic
fi eld.
I1 I2
Δ
Closed path constructed from short segments
Surface enclosed by path
Δ B
B
FIGURE 21.36 This setup is used in the text to explain Ampère’s law.
21.9 Magnetic Materials 613
21.9 Magnetic Materials
Ferromagnetism The similarity between the magnetic fi eld lines in the neighborhood of a bar magnet and those
around a current loop suggests that the magnetism in each case arises from a common cause. The
fi eld that surrounds the loop is created by the charges moving in the wire. The magnetic fi eld
around a bar magnet is also due to the motion of charges, but the motion is not that of a bulk
current through the magnetic material. Instead, the motion responsible for the magnetism is that
of the electrons within the atoms of the material.
The magnetism produced by electrons within an atom can arise from two motions. First, each
electron orbiting the nucleus behaves like an atomic-sized loop of current that generates a small
magnetic fi eld, similar to the fi eld created by the current loop in Figure 21.28a. Second, each electron possesses a spin that also gives rise to a magnetic fi eld. The net magnetic fi eld created by
the electrons within an atom is due to the combined fi elds created by their orbital and spin motions.
In most substances the magnetism produced at the atomic level tends to cancel out, with the
result that the substance is nonmagnetic overall. However, there are some materials, known as
ferromagnetic materials, in which the cancellation does not occur for groups of approximately 1016–1019 neighboring atoms, because they have electron spins that are naturally aligned parallel
to each other. This alignment results from a special type of quantum mechanical* interaction
between the spins. The result of the interaction is a small but highly magnetized region of about
0.01 to 0.1 mm in size, depending on the nature of the material; this region is called a magnetic domain. Each domain behaves as a small magnet with its own north and south poles. Common ferromagnetic materials are iron, nickel, cobalt, chromium dioxide, and alnico (an aluminum– nickel–cobalt alloy).
Induced Magnetism Often magnetic domains in ferromagnetic material are arranged randomly, as Figure 21.38a illus- trates for a piece of iron. In such a situation, the magnetic fi elds of the domains cancel each other,
so the iron displays little, if any, overall magnetism. However, an unmagnetized piece of iron can
EXAMPLE 10 An Infinitely Long, Straight, Current-Carrying Wire
Use Ampère’s law to obtain the magnetic fi eld produced by the current in
an infi nitely long, straight wire.
Reasoning Figure 21.24a shows that compass needles point in a circu- lar pattern around the wire, so we know that the magnetic fi eld lines are
circular. Therefore, it is convenient to use a circular path of radius r when applying Ampère’s law, as Figure 21.37 indicates.
Solution Along the circular path in Figure 21.37, the magnetic fi eld is everywhere parallel to Δ𝓁 and has a constant magnitude, since each
point is at the same distance from the wire. Thus, B‖ = B and, accord- ing to Ampère’s law, we have
ΣB‖∆ℓ = B ( Σ ∆ℓ ) = μ 0 I
However, ΣΔ𝓁 is just the circumference 2𝜋r of the circle, so Ampère’s law reduces to
B ( Σ ∆ℓ ) = B (2πr ) = μ0 I Dividing both sides by 2𝜋r shows that B = μ0 I/ (2πr ) , as given earlier in Equation 21.5.
r
Circular path
Δ
I
B
FIGURE 21.37 Example 10 uses Ampère’s law to fi nd the magnetic fi eld in the vicinity
of this long, straight, current-carrying wire.
*The branch of physics called quantum mechanics is mentioned in Section 29.5. A detailed discussion of it is beyond
the scope of this book.
614 CHAPTER 21 Magnetic Forces and Magnetic Fields
be magnetized by placing it in an external magnetic fi eld provided by a permanent magnet or
an electromagnet. The external magnetic fi eld penetrates the unmagnetized iron and induces (or brings about) a state of magnetism in the iron by causing two eff ects. Those domains whose mag-
netism is parallel or nearly parallel to the external magnetic fi eld grow in size at the expense of
other domains that are not so oriented. In Figure 21.38b the growing domains are colored gold. In addition, the magnetic alignment of some domains may rotate and become more oriented in
the direction of the external fi eld. The resulting preferred alignment of the domains gives the iron
an overall magnetism, so the iron behaves like a magnet with associated north and south poles. In
some types of ferromagnetic materials, such as the chromium dioxide used in cassette tapes, the
domains remain aligned for the most part when the external magnetic fi eld is removed, and the
material thus becomes permanently magnetized.
The magnetism induced in a ferromagnetic material can be surprisingly large, even in the
presence of a weak external fi eld. For instance, it is not unusual for the induced magnetic fi eld
to be a hundred to a thousand times stronger than the external fi eld that causes the alignment.
For this reason, high-fi eld electromagnets are constructed by wrapping the current-carrying wire
around a solid core made from iron or other ferromagnetic material.
Induced magnetism explains why a permanent magnet sticks to a refrigerator door and why
an electromagnet can pick up scrap iron at a junkyard. Notice in Figure 21.38b that there is a north pole at the end of the iron that is closest to the south pole of the permanent magnet. The net
result is that the two opposite poles give rise to an attraction between the iron and the permanent
magnet. Conversely, the north pole of the permanent magnet would also attract the piece of iron
by inducing a south pole in the nearest side of the iron. In nonferromagnetic materials, such as
aluminum and copper, the formation of magnetic domains does not occur, so magnetism cannot
be induced into these substances. Consequently, magnets do not stick to aluminum cans.
THE PHYSICS OF . . . detecting fi ngerprints. The attraction that induced magnetism creates between a permanent magnet and a ferromagnetic material is used in crime-scene
investigations, where powder is dusted onto surfaces to make fi ngerprints visible. Magnetic
fi ngerprint powder allows investigators to recover evidence from surfaces like the neoprene
glove in Figure 21.39, which are very diffi cult to examine without damaging the prints in the process. Brushing excess conventional powder away ruins the delicate ridges of the pattern
that allow the print to be identifi ed reliably. Magnetic fi ngerprint powder, however, consists of
tiny iron fl akes coated with an organic material that allows them to stick to the greasy residue
in the print. A permanent magnet eliminates the need for brushing away excess powder by
creating induced magnetism in the iron and pulling away the powder not stuck directly to the
greasy residue.
Magnetic Tape Recording THE PHYSICS OF . . . magnetic tape recording. The process of magnetic tape recording uses induced magnetism, as Figure 21.40 illustrates. The weak electrical signal from a microphone is routed to an amplifi er where it is amplifi ed. The current from the output of the amplifi er is then
sent to the recording head, which is a coil of wire wrapped around an iron core. The iron core has
Magnetic domains
Permanent magnet
(a) Unmagnetized iron (b) Induced magnetism
FIGURE 21.38 (a) Each magnetic domain is a highly magnetized region that behaves like a small magnet (represented by an arrow whose head indicates a north pole). Unmagnetized iron consists of many
domains that are randomly aligned. The size of each domain is exaggerated for clarity. (b) The external magnetic fi eld of the permanent magnet causes those domains that are parallel or nearly parallel to the
fi eld to grow in size (shown in gold color).
FIGURE 21.39 Magnetic fi ngerprint powder has been used to reveal fi ngerprints on this
neoprene glove. The powder consists of tiny
iron fl akes coated with an organic material
that enables them to stick to the greasy residue
in the print. Because of induced magnetism, a
permanent magnet can be used to remove any
excess powder that would obscure the evidence.
This eliminates the need for brushing and
possible damage to the print.
James King-Holmes/SPL/Science Source
Tape travel
Recording head
Plastic backing
Amplifier
Magnetic coating
InputOutput
Induced magnetism
Fringe field penetrates magnetic coating
FIGURE 21.40 The magnetic fringe fi eld of the recording head penetrates the magnetic
coating on the tape and magnetizes it.
21.9 Magnetic Materials 615
the approximate shape of a horseshoe with a small gap between the two ends. The ferromagnetic
iron substantially enhances the magnetic fi eld produced by the current in the coil.
When there is a current in the coil, the recording head becomes an electromagnet with a
north pole at one end and a south pole at the other end. The magnetic fi eld lines pass through
the iron core and cross the gap. Within the gap, the lines are directed from the north pole toward
the south pole. Some of the fi eld lines in the gap “bow outward,” as Figure 21.40 indicates; the bowed region of the magnetic fi eld is called the fringe fi eld. The fringe fi eld penetrates the magnetic coating on the tape and induces magnetism in the coating. This induced magnetism is
retained when the tape leaves the vicinity of the recording head and, thus, provides a means for
storing audio information. Audio information is stored, because at any instant in time the way
in which the tape is magnetized depends on the amount and direction of current in the recording
head. The current, in turn, depends on the sound picked up by the microphone, so that changes
in the sound that occur from moment to moment are preserved as changes in the tape’s induced
magnetism.
Maglev Trains THE PHYSICS OF . . . a magnetically levitated train. A magnetically levitated train—maglev, for short—uses forces that arise from induced magnetism to levitate or fl oat above a guideway.
Since it rides a few centimeters above the guideway, a maglev does not need wheels. Freed from
friction due to the guideway, the train can achieve signifi cantly greater speeds than do conven-
tional trains. For example, the Transrapid maglev in Figure 21.41 has achieved speeds of 110 m/s (250 mph).
Figure 21.41a shows that the Transrapid maglev achieves levitation with electromagnets mounted on arms that extend around and under the guideway. When a current is sent to an
electromagnet, the resulting magnetic fi eld creates induced magnetism in a rail mounted in the
guideway. The upward attractive force from the induced magnetism is balanced by the weight of
the train, so the train moves without touching the rail or the guideway.
Magnetic levitation only lifts the train and does not move it forward. Figure 21.41b illustrates how magnetic propulsion is achieved. In addition to the levitation electromagnets, propulsion
electromagnets are also placed along the guideway. By controlling the direction of the currents
in the train and guideway electromagnets, it is possible to create an unlike pole in the guideway
just ahead of each electromagnet on the train and a like pole just behind. Each electromagnet on
the train is thus both pulled and pushed forward by electromagnets in the guideway. By adjusting
the timing of the like and unlike poles in the guideway, the speed of the train can be adjusted.
Reversing the poles in the guideway electromagnets serves to brake the train.
FIGURE 21.41 (a) The Transrapid maglev (a German train) has achieved speeds
of 110 m/s (250 mph). The levitation
electromagnets are drawn up toward the rail
in the guideway, levitating the train. (b) The magnetic propulsion system.
Guideway Rail
Arm
Guideway (b)(a)
Levitation electromagnet
S N S N N S N
© B
er n d M
el lm
an n /A
la m
y
616 CHAPTER 21 Magnetic Forces and Magnetic Fields
Check Your Understanding
(The answers are given at the end of the book.) 21. In a TV commercial that advertises a soda pop, a strong electromagnet picks up a delivery truck car-
rying cans of the soft drink. The picture switches to the interior of the truck, where cans are seen to fl y
upward and stick to the roof just beneath the electromagnet. Are these cans made entirely of aluminum?
22. Suppose that you have two bars. Bar 1 is a permanent magnet and bar 2 is not a magnet, but is made from a ferromagnetic material like iron. A third bar (bar 3), which is known to be a permanent magnet, is brought
close to one end of bar 1 and then to one end of bar 2. Which one of the following statements is true?
(a) Bars 1 and 3 will either be attracted to or repelled from each other, while bars 2 and 3 will always be repelled from each other. (b) Bars 1 and 3 will either be attracted to or repelled from each other, while bars 2 and 3 will always be attracted to each other. (c) Bars 1 and 3 will always be repelled from each other, while bars 2 and 3 will either be attracted to or repelled from each other. (d) Bars 1 and 3 will always be attracted to each other, while bars 2 and 3 will either be attracted to or repelled from each other.
EXAMPLE 11 BIO The Physics of MRI Machines—The Superconducting Magnet
As mentioned previously in this chapter, the medical diagnostic technique of
magnetic resonance imaging relies on a large solenoid electromagnet to pro-
duce strong magnetic fi elds. Assume the magnet is wound with a single layer
of 2.0-mm diameter wire that is insulated. If the highest magnetic fi eld pro-
duced by the magnet is 1.7 T, what is the maximum current in the magnet?
Reasoning Since the magnetic fi eld in the MRI machine is produced by a solenoid, we can apply Equation 21.7 to calculate the current in the
magnet. To do this, we will need the value of n (the number of turns per unit length). This can be determined from the length of the magnet and
the thickness of the wire.
Solution Beginning with Equation 21.7, we have: B = μ0nI = μ0(Nℓ)I, where n = (Nℓ) is the number of turns (N) in the solenoid divided by its length (𝓁). N is determined by how many turns of wire in a single layer can fi t side-by-side along the length of the solenoid. Therefore, N = 𝓁/d,
where we let d represent the diameter of the wire. Making this substitu- tion into Equation 21.7 above, we have the following:
B = μ0(ℓ/dℓ )I = μ0I d
.
We can now solve this for the current in the solenoid:
I = dB μ0
= (0.002 m)(1.7 T)
4π × 10−7 T · m/A = 2700 A .
This is an incredibly large current for a wire that is only 2.0 mm in dia-
meter! As we mentioned previously in the chapter, the niobium-based
wire in the MRI magnet can carry such large currents because of its super-
conducting properties (no loss due to electrical resistance). However, in
order to take advantage of the wire’s superconducting properties, it must
be cooled to temperatures close to absolute zero Kelvin by submersing it
in liquid helium.
Concept Summary 21.1 Magnetic Fields A magnet has a north pole and a south pole. The north pole is the end that points toward the north magnetic pole of the earth
when the magnet is freely suspended. Like magnetic poles repel each other,
and unlike poles attract each other.
A magnetic fi eld exists in the space around a magnet. The magnetic fi eld
is a vector whose direction at any point is the direction indicated by the north
pole of a small compass needle placed at that point. As an aid in visualizing
the magnetic fi eld, magnetic fi eld lines are drawn in the vicinity of a magnet.
The lines appear to originate from the north pole and end on the south pole.
The magnetic fi eld at any point in space is tangent to the magnetic fi eld line
at the point. Furthermore, the strength of the magnetic fi eld is proportional
to the number of lines per unit area that passes through a surface oriented
perpendicular to the lines.
21.2 The Force That a Magnetic Field Exerts on a Moving Charge The direction of the magnetic force acting on a charge moving with a velo-
city v→ in a magnetic fi eld B→ is perpendicular to both v→ and B→. For a positive charge the direction can be determined with the aid of Right-Hand Rule No. 1
(see below). The magnetic force on a moving negative charge is opposite to
the force on a moving positive charge.
Right-Hand Rule No. 1: Extend the right hand so the fi ngers point along
the direction of the magnetic fi eld B→ and the thumb points along the velocity v→ of the charge. The palm of the hand then faces in the direction of the mag- netic force F→ that acts on a positive charge.
The magnitude B of the magnetic fi eld at any point in space is defi ned according to Equation 21.1, where F is the magnitude of the magnetic force on a test charge, |q0| is the magnitude of the test charge, and 𝜐 is the magni- tude of the charge’s velocity, which makes an angle 𝜃 with the direction of
the magnetic fi eld. The SI unit for the magnetic fi eld is the tesla (T). Another,
smaller unit for the magnetic fi eld is the gauss; 1 gauss = 10−4 tesla. The
gauss is not an SI unit.
B = F
∣q0∣ υsin θ (21.1)
21.3 The Motion of a Charged Particle in a Magnetic Field When a charged particle moves in a region that contains both magnetic and electric
Focus on Concepts 617
fi elds, the net force on the particle is the vector sum of the magnetic and
electric forces.
A magnetic force does no work on a charged particle moving as in Fig- ure 21.9b, because the direction of the force is always perpendicular to the motion of the particle. Being unable to do work, the magnetic force cannot
change the kinetic energy, and hence the speed, of the particle; however, the
magnetic force does change the direction in which the particle moves.
When a particle of charge q (magnitude = |q|) and mass m moves with speed υ perpendicular to a uniform magnetic fi eld of magnitude B, the mag- netic force causes the particle to move on a circular path that has a radius
given by Equation 21.2.
r = mυ ∣q∣B
(21.2)
21.4 The Mass Spectrometer The mass spectrometer is an instrument for measuring the abundance of ionized atoms or molecules that have diff erent
masses. The atoms or molecules are ionized (charge = +e), accelerated to a speed 𝜐 by a potential diff erence V, and sent into a uniform magnetic fi eld of magnitude B. The magnetic fi eld causes the particles (each with a mass m) to move on a circular path of radius r. The relation between m and B is given by Equation 1.
m = (er 2
2V) B2 (1) 21.5 The Force on a Current in a Magnetic Field An electric current, being composed of moving charges, can experience a magnetic force when
placed in a magnetic fi eld of magnitude B. For a straight wire that has a length L and carries a current I, the magnetic force has a magnitude that is given by Equation 21.3, where 𝜃 is the angle between the directions of the current and
the magnetic fi eld. The direction of the force is perpendicular to both the cur-
rent and the magnetic fi eld and is given by Right-Hand Rule No. 1.
F = ILB sin θ (21.3)
21.6 The Torque on a Current-Carrying Coil Magnetic forces can exert a torque on a current-carrying loop of wire and thus cause the loop to
rotate. When a current I exists in a coil of wire with N turns, each of area A, in the presence of a magnetic fi eld of magnitude B, the coil experiences a net torque that has a magnitude given by Equation 21.4, where 𝜙 is the angle
between the direction of the magnetic fi eld and the normal to the plane of the
coil. The quantity NIA is known as the magnetic moment of the coil.
τ = NIAB sin ϕ (21.4)
21.7 Magnetic Fields Produced by Currents An electric current produces a magnetic fi eld, with diff erent current geometries giving rise to
diff erent fi eld patterns. For an infi nitely long, straight wire, the magnetic fi eld
lines are circles centered on the wire, and their direction is given by Right-
Hand Rule No. 2 (see below). The magnitude of the magnetic fi eld at a radial
distance r from the wire is given by Equation 21.5, where I is the current in the wire and 𝜇0 is a constant known as the permeability of free space
(μ0 = 4π × 10−7 T · m /A).
B = μ0I 2πr
(21.5)
Right-Hand Rule No. 2: Curl the fi ngers of the right hand into the shape
of a half-circle. Point the thumb in the direction of the conventional current I, and the tips of the fi ngers will point in the direction of the magnetic fi eld B→.
The magnitude of the magnetic fi eld at the center of a fl at circular loop
consisting of N turns, each of radius R and carrying a current I, is given by Equation 21.6. The loop has associated with it a north pole on one side and
a south pole on the other side. The side of the loop that behaves like a north
pole can be predicted by using Right-Hand Rule No. 2.
B = N μ0I 2R
(21.6)
A solenoid is a coil of wire wound in the shape of a helix. Inside a long
solenoid the magnetic fi eld is nearly constant and has a magnitude that is
given by Equation 21.7, where n is the number of turns per unit length of the solenoid and I is the current in the wire. One end of the solenoid behaves like a north pole, and the other end like a south pole. The end that is the north pole
can be predicted by using Right-Hand Rule No. 2.
B = μ0nI (21.7)
21.8 Ampère’s Law Ampère’s law specifi es the relationship between a current and its associated magnetic fi eld. For any current geometry that pro-
duces a magnetic fi eld that does not change in time, Ampère’s law is given by
Equation 21.8, where Δ𝓁 is a small segment of length along a closed path of
arbitrary shape around the current, B‖ is the component of the magnetic fi eld parallel to Δ𝓁, I is the net current passing through the surface bounded by the path, and 𝜇0 is the permeability of free space. The symbol Σ indicates that the
sum of all B‖ Δ𝓁 terms must be taken around the closed path.
ΣB‖∆ℓ = μ0 I (21.8)
21.9 Magnetic Materials Ferromagnetic materials, such as iron, are made up of tiny regions called magnetic domains, each of which behaves as
a small magnet. In an unmagnetized ferromagnetic material, the domains are
randomly aligned. In a permanent magnet, many of the domains are aligned,
and a high degree of magnetism results. An unmagnetized ferromagnetic
material can be induced into becoming magnetized by placing it in an external
magnetic fi eld.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 21.2 The Force That a Magnetic Field Exerts on a Moving Charge 2. At a location near the equator, the earth’s magnetic fi eld is horizontal and points north. An electron is moving vertically upward from the ground. What
is the direction of the magnetic force that acts on the electron? (a) North (b) East (c) South (d) West (e) The magnetic force is zero.
3. The drawing shows four situations in which a positively charged particle is moving with a velocity v→ through a magnetic fi eld B→. In each case, the magnetic fi eld is directed out of the page toward you, and the velocity is
directed to the right. In only one of these drawings is the magnetic force F→ physically reasonable. Which drawing is it? (a) 1 (b) 2 (c) 3 (d) 4
+ v
B (out of page)
1 2 3 4
F
+ v
B (out of page)
F
+ v
B (out of page)
F (into page)
+ v
B (out of page)
F
QUESTION 3
Focus on Concepts
618 CHAPTER 21 Magnetic Forces and Magnetic Fields
Section 21.3 The Motion of a Charged Particle in a Magnetic Field 6. Three particles are moving perpendicular to a uniform magnetic fi eld and travel on circular paths (see the drawing). The particles have the same mass
and speed. List the particles in order of their charge magnitude, largest to
smallest. (a) 3, 2, 1 (b) 3, 1, 2 (c) 2, 3, 1 (d) 1, 3, 2 (e) 1, 2, 3
QUESTION 6
1 2
3
B (out of page)
8. The drawing shows the circular paths of an electron and a proton. These particles have the same charge magnitudes, but the proton is more massive.
They travel at the same speed in a uniform magnetic fi eld B→, which is dir- ected into the page everywhere. Which particle follows the larger circle, and
does it travel clockwise or counterclockwise?
QUESTION 8
B (into page)
Particle Direction of Travel (a) electron clockwise
(b) electron counterclockwise
(c) proton clockwise
(d) proton counterclockwise
Section 21.5 The Force on a Current in a Magnetic Field 12. Four views of a horseshoe magnet and a current-carrying wire are shown in the drawing. The wire is perpendicular to the page, and the current is
directed out of the page toward you. In which one or more of these situations
does the magnetic force on the current point due north? (a) 1 and 2 (b) 3 and 4 (c) 2 (d) 3 (e) 1
S
N
NN SS
1 2 3 4
S
N
S
N
Current (out of page) Current (out of page)
QUESTION 12
Section 21.6 The Torque on a Current-Carrying Coil 13. A square, current-carrying loop is placed in a uniform magnetic fi eld B→ with the plane of the loop parallel to the magnetic fi eld (see the draw-
ing). The dashed line is the axis of rotation. The
magnetic fi eld exerts _______. (a) a net force and a net torque on the loop (b) a net force, but not a net torque, on the loop (c) a net torque, but not a net force, on the loop (d) neither a net force nor a net torque on the loop
Section 21.7 Magnetic Fields Produced by Currents 16. The drawing shows four situations in which two very long wires are car- rying the same current, although the directions of the currents may be dif-
ferent. The point P in the drawings is equidistant from each wire. Which one (or more) of these situations gives rise to a zero net magnetic fi eld at P? (a) 2 and 4 (b) Only 1 (c) Only 2 (d) 2 and 3 (e) 3 and 4
P
1
P P P
2 3 4
QUESTION 16
17. Three long, straight wires are carrying currents that have the same magnitude. In C the current is
opposite to the current in A and B. The wires are
equally spaced. Each wire experiences a net force
due to the other two wires. Which wire experiences
a net force with the greatest magnitude? (a) A (b) B (c) C (d) All three wires experience a net force that has the same magnitude.
II
Axis through center of loop
B
B
B
B
QUESTION 13
I A
I B
I C
QUESTION 17
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 21.1 Magnetic Fields
Section 21.2 The Force That a Magnetic Field Exerts on a Moving Charge 1. E SSM In New England, the horizontal component of the earth’s magnetic fi eld has a magnitude of 1.6 × 10−5 T. An electron is shot vertically straight
up from the ground with a speed of 2.1 × 106 m/s. What is the magnitude of
Problems
Problems 619
the acceleration caused by the magnetic force? Ignore the gravitational force
acting on the electron.
2. E (a) A proton, traveling with a velocity of 4.5 × 106 m/s due east, ex- periences a magnetic force that has a maximum magnitude of 8.0 × 10−14 N
and a direction of due south. What are the magnitude and direction of the
magnetic fi eld causing the force? (b) Repeat part (a) assuming the proton is replaced by an electron.
3. E SSM At a certain location, the horizontal component of the earth’s magnetic fi eld is 2.5 × 10−5 T, due north. A proton moves eastward with just
the right speed for the magnetic force on it to balance its weight. Find the
speed of the proton.
4. E A charge of −8.3 𝜇C is traveling at a speed of 7.4 × 106 m/s in a region of space where there is a magnetic fi eld. The angle between the velocity of
the charge and the fi eld is 52°. A force of magnitude 5.4 × 10−3 N acts on the
charge. What is the magnitude of the magnetic fi eld?
5. E When a charged particle moves at an angle of 25° with respect to a magnetic fi eld, it experiences a magnetic force of magnitude F. At what angle (less than 90°) with respect to this fi eld will this particle, moving at the same
speed, experience a magnetic force of magnitude 2F? 6. E GO A particle that has an 8.2 𝜇C charge moves with a velocity of mag- nitude 5.0 × 105 m/s along the +x axis. It experiences no magnetic force, although there is a magnetic fi eld present. The maximum possible magnetic
force that the charge could experience has a magnitude of 0.48 N. Find the
magnitude and direction of the magnetic fi eld. Note that there are two pos-
sible answers for the direction of the fi eld.
7. E A magnetic fi eld has a magnitude of 1.2 × 10−3 T, and an electric fi eld has a magnitude of 4.6 × 103 N/C. Both fi elds point in the same direction. A
positive 1.8 𝜇C charge moves at a speed of 3.1 × 106 m/s in a direction that
is perpendicular to both fi elds. Determine the magnitude of the net force that
acts on the charge.
8. E GO Two charged particles move in the same direction with respect to the same magnetic fi eld. Particle 1 travels three times faster than particle 2.
However, each particle experiences a magnetic force of the same magnitude.
Find the ratio |q1|/|q2| of the magnitudes of the charges. 9. M V-HINT The drawing shows a parallel plate capacitor that is moving with a speed of 32 m/s through a 3.6-T magnetic fi eld. The velocity v→ is perpendicular to the magnetic fi eld. The electric fi eld within the capacitor
has a value of 170 N/C, and each plate has an area of 7.5 × 10−4 m2. What is
the magnetic force (magnitude and direction) exerted on the positive plate of
the capacitor?
PROBLEM 9
+
+
+
+
–
–
–
–
E B
v
10. M V-HINT One component of a magnetic fi eld has a magnitude of 0.048 T and points along the +x axis, while the other component has a magnitude of 0.065 T and points along the −y axis. A particle carrying a charge of +2.0 × 10−5 C is moving along the +z axis at a speed of 4.2 × 103 m/s. (a) Find the magnitude of the net magnetic force that acts on the particle. (b) Determine the angle that the net force makes with respect to the +x axis. 11. M SSM The electrons in the beam of a television tube have a kinetic energy of 2.40 × 10−15 J. Initially, the electrons move horizontally from west
to east. The vertical component of the earth’s magnetic fi eld points down,
toward the surface of the earth, and has a magnitude of 2.00 × 10−5 T. (a) In what direction are the electrons defl ected by this fi eld component? (b) What is the acceleration of an electron in part (a)?
Section 21.3 The Motion of a Charged Particle in a Magnetic Field
Section 21.4 The Mass Spectrometer 12. E An ionized helium atom has a mass of 6.6 × 10−27 kg and a speed of 4.4 × 105 m/s. It moves perpendicular to a 0.75-T magnetic fi eld on a circular
path that has a 0.012-m radius. Determine whether the charge of the ionized
atom is +e or +2e. 13. E BIO SSM In the operating room, anesthesiologists use mass spectro- meters to monitor the respiratory gases of patients undergoing surgery. One
gas that is often monitored is the anesthetic isofl urane (molecular mass =
3.06 × 10−25 kg). In a spectrometer, a singly ionized molecule of isofl urane
(charge = +e) moves at a speed of 7.2 × 103 m/s on a circular path that has a radius of 0.10 m. What is the magnitude of the magnetic fi eld that the spec-
trometer uses?
14. E GO A charged particle with a charge-to-mass ratio of |q|/m = 5.7 × 108 C/kg travels on a circular path that is perpendicular to a magnetic fi eld
whose magnitude is 0.72 T. How much time does it take for the particle to
complete one revolution?
15. E A charged particle enters a uniform magnetic fi eld and follows the circular path shown in the drawing. (a) Is the particle positively or negatively charged? Why? (b) The particle’s speed is 140 m/s, the magnitude of the magnetic fi eld is 0.48 T, and the radius of the path is 960 m. Determine the
mass of the particle, given that its charge has a magnitude of 8.2 × 10−4 C.
PROBLEM 15
B (out of paper)
q
16. E GO A proton is projected perpendicularly into a magnetic fi eld that has a magnitude of 0.50 T. The fi eld is then adjusted so that an electron will
follow a circular path of the same radius when it is projected perpendicularly
into the fi eld with the same velocity that the proton had. What is the mag-
nitude of the fi eld used for the electron?
17. E SSM When beryllium-7 ions (m = 11.65 × 10−27 kg) pass through a mass spectrometer, a uniform magnetic fi eld of 0.283 T curves their path
directly to the center of the detector (see Figure 21.14). For the same acceler- ating potential diff erence, what magnetic fi eld should be used to send beryl-
lium-10 ions (m = 16.63 × 10−27 kg) to the same location in the detector? Both types of ions are singly ionized (q = +e). 18. E GO Suppose that an ion source in a mass spectrometer produces doubly ionized gold ions (Au2+), each with a mass of 3.27 × 10−25 kg. The ions are accelerated from rest through a potential diff erence of 1.00 kV. Then,
a 0.500-T magnetic fi eld causes the ions to follow a circular path. Determine
the radius of the path.
19. E An 𝛼-particle has a charge of +2e and a mass of 6.64 × 10−27 kg. It is accelerated from rest through a potential diff erence that has a value of 1.20 ×
106 V and then enters a uniform magnetic fi eld whose magnitude is 2.20 T.
The 𝛼-particle moves perpendicular to the magnetic fi eld at all times. What is
620 CHAPTER 21 Magnetic Forces and Magnetic Fields
(a) the speed of the 𝛼-particle, (b) the magnitude of the magnetic force on it, and (c) the radius of its circular path? 20. E GO Particle 1 and particle 2 have masses of m1 = 2.3 × 10−8 kg and m2 = 5.9 × 10−8 kg, but they carry the same charge q. The two particles ac- celerate from rest through the same electric potential diff erence V and enter the same magnetic fi eld, which has a magnitude B. The particles travel per- pendicular to the magnetic fi eld on circular paths. The radius of the circular
path for particle 1 is r1 = 12 cm. What is the radius (in cm) of the circular path for particle 2?
21. E Two of the isotopes of carbon, carbon-12 and carbon-13, have masses of 19.93 × 10−27 kg and 21.59 × 10−27 kg, respectively. These two isotopes
are singly ionized (+e), each given a speed of 6.667 × 105 m/s. The ions then enter the bending region of a mass spectrometer where the magnetic fi eld is
0.8500 T. Determine the spatial separation between the two isotopes after
they have traveled through a half-circle.
22. M V-HINT The ion source in a mass spectrometer produces both singly and doubly ionized species, X+ and X2+. The diff erence in mass between
these species is too small to be detected. Both species are accelerated through
the same electric potential diff erence, and both experience the same magnetic
fi eld, which causes them to move on circular paths. The radius of the path for
the species X+ is r1, while the radius for species X2+ is r2. Find the ratio r1/r2 of the radii.
23. M SSM MMH A proton with a speed of 3.5 × 106 m/s is shot into a region between two plates
that are separated by a distance of 0.23 m. As the
drawing shows, a magnetic fi eld exists between the
plates, and it is perpendicular to the velocity of the
proton. What must be the magnitude of the magnetic
fi eld so the proton just misses colliding with the op-
posite plate?
24. M V-HINT Review Conceptual Example 2 as an aid in understanding this problem. A velocity selector has an electric fi eld of magnitude 2470 N/C,
directed vertically upward, and a horizontal magnetic fi eld that is directed
south. Charged particles, traveling east at a speed of 6.50 × 103 m/s, enter
the velocity selector and are able to pass completely through without being
defl ected. When a diff erent particle with an electric charge of +4.00 × 10−12 C
enters the velocity selector traveling east, the net force (due to the electric and
magnetic fi elds) acting on it is 1.90 × 10−9 N, pointing directly upward. What
is the speed of this particle?
25. M SSM A particle of mass 6.0 × 10−8 kg and charge +7.2 𝜇C is traveling due east. It enters perpendicularly a magnetic fi eld whose magnitude is 3.0 T.
After entering the fi eld, the particle completes one-half of a circle and exits
the fi eld traveling due west. How much time does the particle spend traveling
in the magnetic fi eld?
26. M V-HINT Conceptual Example 4 provides background pertinent to this problem. An electron has a kinetic energy of 2.0 × 10−17 J. It moves on a
circular path that is perpendicular to a uniform magnetic fi eld of magnitude
5.3 × 10−5 T. Determine the radius of the path.
27. M CHALK A positively charged particle of mass 7.2 × 10−8 kg is traveling due east with a speed of 85 m/s and enters a 0.31-T uniform magnetic fi eld. The
particle moves through one-quarter of a circle in a time of 2.2 × 10−3 s, at which
time it leaves the fi eld heading due south. All during the motion the particle
moves perpendicular to the magnetic fi eld. (a) What is the magnitude of the mag- netic force acting on the particle? (b) Determine the magnitude of its charge. 28. M Review Conceptual Example 2 as background for this problem. A charged particle moves through a velocity selector at a constant speed in
a straight line. The electric fi eld of the velocity selector is 3.80 × 103 N/C,
while the magnetic fi eld is 0.360 T. When the electric fi eld is turned off , the
charged particle travels on a circular path whose radius is 4.30 cm. Find the
charge-to-mass ratio of the particle.
29. H Available in WileyPLUS.
Section 21.5 The Force on a Current in a Magnetic Field 30. E At New York City, the earth’s magnetic fi eld has a vertical compon- ent of 5.2 × 10−5 T that points downward (perpendicular to the ground) and
a horizontal component of 1.8 × 10−5 T that points toward geographic north
(parallel to the ground). What are the magnitude and direction of the mag-
netic force on a 6.0-m long, straight wire that carries a current of 28 A per-
pendicularly into the ground?
31. E SSM A 45-m length of wire is stretched horizontally between two vertical posts. The wire carries a current of 75 A and experiences a magnetic
force of 0.15 N. Find the magnitude of the earth’s magnetic fi eld at the location
of the wire, assuming the fi eld makes an angle of 60.0° with respect to the wire.
32. E A straight wire in a magnetic fi eld experiences a force of 0.030 N when the current in the wire is 2.7 A. The current in the wire is changed, and
the wire experiences a force of 0.047 N as a result. What is the new current?
33. E A horizontal wire of length 0.53 m, carrying a current of 7.5 A, is placed in a uniform external magnetic fi eld. When the wire is horizontal, it
experiences no magnetic force. When the wire is tilted upward at an angle
of 19°, it experiences a magnetic force of 4.4 × 10−3 N. Determine the mag-
nitude of the external magnetic fi eld.
34. E GO The drawing shows a wire composed of three segments, AB, BC, and CD. There is a
current of I = 2.8 A in the wire. There is also a magnetic fi eld B→ (magnitude = 0.26 T) that is the same everywhere and points in the dir-
ection of the +z axis. The lengths of the wire segments are LAB = 1.1 m, LBC = 0.55 m, and L CD = 0.55 m. Find the magnitude of the force that acts on each segment.
35. E SSM A wire carries a current of 0.66 A. This wire makes an angle of 58° with respect to
a magnetic fi eld of magnitude 4.7 × 10−5 T. The wire experiences a magnetic
force of magnitude 7.1 × 10−5 N. What is the length of the wire?
36. E Available in WileyPLUS. 37. E A loop of wire has the shape of a right triangle (see the drawing) and carries a current
of I = 4.70 A. A uniform magnetic fi eld is dir- ected parallel to side AB and has a magnitude of 1.80 T. (a) Find the magnitude and direction of the magnetic force exerted on each side of the
triangle. (b) Determine the magnitude of the net force exerted on the triangle.
38. M CHALK GO A copper rod of length 0.85 m is lying on a frictionless table (see the drawing).
Each end of the rod is attached to a fi xed wire by
an unstretched spring that has a spring constant
of k = 75 N/m. A magnetic fi eld with a strength of 0.16 T is oriented perpendicular to the surface of the table. (a) What must be the direction of the current in the copper rod that causes the springs to
stretch? (b) If the current is 12 A, by how much does each spring stretch?
PROBLEM 38
Copper rod
Fixed wires
Table (top view)
B (out of paper)
Proton
B
v
PROBLEM 23
A
C B
I
D
+y
+x
+z
B
PROBLEM 34
B
2.00 m
55.0° A B
C
I
PROBLEM 37
Problems 621
39. M SSM MMH The drawing shows a thin, uniform rod that has a length of 0.45 m and a mass of 0.094 kg. This rod lies in the plane of the paper and is
attached to the fl oor by a hinge at point P. A uniform magnetic fi eld of 0.36 T is directed perpendicularly into the plane of the paper. There is a current I = 4.1 A in the rod, which does not rotate clockwise or counterclockwise. Find the
angle 𝜃. (Hint: The magnetic force may be taken to act at the center of gravity.)
PROBLEM 39
I
P
B (into page)
θ
40. M CHALK GO A horizontal wire is hung from the ceiling of a room by two massless strings. The wire has a length of 0.20 m and a mass of 0.080 kg. A
uniform magnetic fi eld of magnitude 0.070 T is directed from the ceiling to the
fl oor. When a current of I = 42 A exists in the wire, the wire swings upward and, at equilibrium, makes an angle 𝜙 with respect to the vertical, as the draw-
ing shows. Find (a) the angle 𝜙 and (b) the tension in each of the two strings.
PROBLEM 40 S
N
I
B
ϕ
41. H The two conducting rails in the drawing are tilted upward so they each make an angle of 30.0° with respect to the ground. The vertical mag-
netic fi eld has a magnitude of 0.050 T. The 0.20-kg aluminum rod (length =
1.6 m) slides without friction down the rails at a constant velocity. How much current fl ows through the rod?
PROBLEM 41
Conducting rails
1.6 m 30°
B
B
B
B
Section 21.6 The Torque on a Current-Carrying Coil 42. E Two coils have the same number of circular turns and carry the same current. Each rotates in a magnetic fi eld as in Figure 21.19. Coil 1 has a radius of 5.0 cm and rotates in a 0.18-T fi eld. Coil 2 rotates in a 0.42-T fi eld.
Each coil experiences the same maximum torque. What is the radius (in cm)
of coil 2?
43. E The 1200-turn coil in a dc motor has an area per turn of 1.1 × 10−2 m2. The design for the motor specifi es that the magnitude of the maximum torque
is 5.8 N · m when the coil is placed in a 0.20-T magnetic fi eld. What is the current in the coil?
44. E Two circular coils of current-carrying wire have the same magnetic moment. The fi rst coil has a radius of 0.088 m, has 140 turns, and carries a
current of 4.2 A. The second coil has 170 turns and carries a current of 9.5 A.
What is the radius of the second coil?
45. E A wire has a length of 7.00 × 10−2 m and is used to make a circular coil of one turn. There is a current of 4.30 A in the wire. In the presence of a 2.50-T
magnetic fi eld, what is the maximum torque that this coil can experience?
46. E GO The coil of wire in the drawing is a right triangle and is free to rotate about an axis that is attached along side AC. The current in the loop is I = 4.70 A, and the magnetic fi eld (parallel to the plane of the loop and side AB) is B = 1.80 T. (a) What is the magnetic moment of the loop, and (b) what is the magnitude of the net torque exerted on the loop by the magnetic fi eld?
PROBLEM 46
B
2.00 m
55.0° A B
C
I
47. E V-HINT Available in WileyPLUS. 48. E GO You have a wire of length L = 1.00 m from which to make the square coil of a dc motor. The current in the coil is I = 1.7 A, and the mag- netic fi eld of the motor has a magnitude of B = 0.34 T. Find the maximum torque exerted on the coil when the wire is used to make a single-turn square
coil and a two-turn square coil.
49. E SSM The rectangular loop in the drawing consists of 75 turns and carries a current of I = 4.4 A. A 1.8-T magnetic fi eld is directed along the +y axis. The loop is free to rotate about the z axis. (a) Determine the magnitude of the net torque exerted on the loop and (b) state whether the 35° angle will increase or decrease.
PROBLEM 49
z
y
x
I 0.70 m
75 turns
35° 0.50 m
I
B
50. M A square coil and a rectangular coil are each made from the same length of wire. Each contains a single turn. The long sides of the rectangle are
twice as long as the short sides. Find the ratio 𝜏square/𝜏rectangle of the maximum torques that these coils experience in the same magnetic fi eld when they con-
tain the same current.
51. M MMH Available in WileyPLUS. 52. H Available in WileyPLUS.
Section 21.7 Magnetic Fields Produced by Currents 53. E SSM Suppose in the fi gure that I1 = I2 = 25 A and that the separa- tion between the wires is 0.016 m. By applying an external magnetic fi eld
(created by a source other than the wires) it is possible to cancel the mutual
repulsion of the wires. This external fi eld must point along the vertical
622 CHAPTER 21 Magnetic Forces and Magnetic Fields
direction. (a) Does the external fi eld point up or down? Explain. (b) What is the magnitude of the external fi eld?
Repulsion
(a)
F
B
–F I1 I2
Wire 1 Wire 2
PROBLEM 53 Attraction
(b)
F
B
–F
I1 I2
54. E A long solenoid has a length of 0.65 m and contains 1400 turns of wire. There is a current of 4.7 A in the wire. What is the magnitude of the
magnetic fi eld within the solenoid?
55. E BIO SSM The magnetic fi eld produced by the solenoid in a mag- netic resonance imaging (MRI) system designed for measurements on whole
human bodies has a fi eld strength of 7.0 T, and the current in the solenoid is
2.0 × 102 A. What is the number of turns per meter of length of the solenoid?
Note that the solenoid used to produce the magnetic fi eld in this type of system
has a length that is not very long compared to its diameter. Because of this
and other design considerations, your answer will be only an approximation.
56. E GO A long solenoid has 1400 turns per meter of length, and it carries a current of 3.5 A. A small circular coil of wire is placed inside the solenoid
with the normal to the coil oriented at an angle of 90.0° with respect to the
axis of the solenoid. The coil consists of 50 turns, has an area of 1.2 × 10−3 m2,
and carries a current of 0.50 A. Find the torque exerted on the coil.
57. E SSM Two circular loops of wire, each containing a single turn, have the same radius of 4.0 cm and a common center. The planes of the loops are
perpendicular. Each carries a current of 1.7 A. What is the magnitude of the
net magnetic fi eld at the common center?
58. E Two rigid rods are oriented parallel to each other and to the ground. The rods carry the same current in the same direction. The length of each rod
is 0.85 m, and the mass of each is 0.073 kg. One rod is held in place above
the ground, while the other fl oats beneath it at a distance of 8.2 × 10−3 m.
Determine the current in the rods.
59. E Two long, straight wires are separated by 0.120 m. The wires carry currents of 8.0 A in opposite directions, as the drawing indicates. Find the
magnitude of the net magnetic fi eld at the points labeled (a) A and (b) B.
PROBLEM 59
0.030 m
A
B
0.060 m
0.120 m
I
I
60. E GO A long, straight wire carrying a current of 305 A is placed in a uniform magnetic fi eld that has a magnitude of 7.00 × 10−3 T. The wire
is perpendicular to the fi eld. Find a point in space where the net magnetic
fi eld is zero. Locate this point by specifying its perpendicular distance from
the wire.
61. M MMH Two circular coils are concentric and lie in the same plane. The inner coil contains 140 turns of wire, has a radius of 0.015 m, and carries a
current of 7.2 A. The outer coil contains 180 turns and has a radius of 0.023 m.
What must be the magnitude and direction (relative to the current in the inner
coil) of the current in the outer coil, so that the net magnetic fi eld at the com-
mon center of the two coils is zero?
62. M Available in WileyPLUS. 63. M V-HINT Two infi nitely long, straight wires are parallel and separated by a distance of one meter. They carry currents in the same direction. Wire 1
carries four times the current that wire 2 carries. On a line drawn perpendic-
ular to both wires, locate the spot (relative to wire 1) where the net magnetic
fi eld is zero. Assume that wire 1 lies to the left of wire 2 and note that there
are three regions to consider on this line: to the left of wire 1, between wire 1
and wire 2, and to the right of wire 2.
64. M GO The drawing shows two perpendicular, long, straight wires, both of which lie in the plane of the paper. The current in each of the wires is
I = 5.6 A. Find the magnitudes of the net magnetic fi elds at points A and B.
PROBLEM 64
I
B
A
I
0.40 m
0.20 m
0.20 m
0.40 m
65. M SSM A piece of copper wire has a resistance per unit length of 5.90 × 10−3 Ω/m. The wire is wound into a thin, fl at coil of many turns that
has a radius of 0.140 m. The ends of the wire are connected to a 12.0-V bat-
tery. Find the magnetic fi eld strength at the center of the coil.
66. H The drawing shows two wires that both carry the same current of I = 85.0 A and are oriented perpendicular to the plane of the
paper. The current in one wire is directed out
of the paper, while the current in the other is
directed into the paper. Find the magnitude and
direction of the net magnetic fi eld at point P.
67. H The drawing shows two long, straight wires that are suspended from a ceiling. The
mass per unit length of each wire is 0.050 kg/m. Each of the four strings
suspending the wires has a length of 1.2 m. When the wires carry identical
currents in opposite directions, the angle between the strings holding the two
wires is 15°. What is the current in each wire?
PROBLEM 67
15°
1.2 m I
I
1.2 m
15°
Section 21.8 Ampère’s Law 68. E Suppose that a uniform magnetic fi eld is everywhere perpendicular to this page. The fi eld points directly upward toward you. A circular path is
0.150 m
0.150 m 0.150 m
P
I I
PROBLEM 66
Additional Problems 623
drawn on the page. Use Ampère’s law to show that there can be no net current
passing through the circular surface.
69. E V-HINT The wire in Figure 21.37 carries a current of 12 A. Suppose that a second long, straight wire is placed right next to this wire. The current
in the second wire is 28 A. Use Ampère’s law to fi nd the magnitude of the
magnetic fi eld at a distance of r = 0.72 m from the wires when the currents are (a) in the same direction and (b) in opposite directions. 70. M MMH Available in WileyPLUS. 71. H SSM Available in WileyPLUS.
72. E In a certain region, the earth’s magnetic fi eld has a magnitude of 5.4 × 10−5 T and is directed north at an angle of 58° below the horizontal. An
electrically charged bullet is fi red north and 11° above the horizontal, with a
speed of 670 m/s. The magnetic force on the bullet is 2.8 × 10−10 N, directed
due east. Determine the bullet’s electric charge, including its algebraic sign
(+ or −).
73. E SSM An electron is moving through a magnetic fi eld whose mag- nitude is 8.70 × 10−4 T. The electron experiences only a magnetic force and
has an acceleration of magnitude 3.50 × 1014 m/s2. At a certain instant, it has
a speed of 6.80 × 106 m/s. Determine the angle 𝜃 (less than 90°) between the
electron’s velocity and the magnetic fi eld.
74. E GO A very long, straight wire carries a current of 0.12 A. This wire is tangent to a single-turn, circular wire loop that also carries a current. The
directions of the currents are such that the net magnetic fi eld at the center
of the loop is zero. Both wires are insulated and have diameters that can be
neglected. How much current is there in the loop?
75. E SSM The maximum torque experienced by a coil in a 0.75-T mag- netic fi eld is 8.4 × 10−4 N · m. The coil is circular and consists of only one turn. The current in the coil is 3.7 A. What is the length of the wire from
which the coil is made?
76. E Multiple-Concept Example 7 discusses how problems like this one can be solved. A +6.00 𝜇C charge is moving with a speed of 7.50 × 104 m/s
parallel to a very long, straight wire. The wire is 5.00 cm from the charge
and carries a current of 67.0 A in a direction opposite to that of the moving
charge. Find the magnitude and direction of the force on the charge.
77. E V-HINT The x, y, and z components of a magnetic fi eld are Bx = 0.10 T, By = 0.15 T, and Bz = 0.17 T. A 25-cm wire is oriented along the z axis and carries a current of 4.3 A. What is the magnitude of the magnetic force that
acts on this wire?
78. E In a lightning bolt, a large amount of charge fl ows during a time of 1.8 × 10−3 s. Assume that the bolt can be treated as a long, straight line of
current. At a perpendicular distance of 27 m from the bolt, a magnetic fi eld of
8.0 × 10−5 T is measured. How much charge has fl owed during the lightning
bolt? Ignore the earth’s magnetic fi eld.
79. E A charge is moving perpendicular to a magnetic fi eld and experiences a force whose magnitude is 2.7 × 10−3 N.
If this same charge were to move at the
same speed and the angle between its
velocity and the same magnetic fi eld
were 38°, what would be the mag-
nitude of the magnetic force that the
charge would experience?
80. E GO The drawing shows four in- sulated wires overlapping one another,
forming a square with 0.050-m sides.
All four wires are much longer than
the sides of the square. The net mag-
netic fi eld at the center of the square is
61 μT. Calculate the current I.
81. M SSM Available in WileyPLUS. 82. M GO A particle has a charge of q = +5.60 μC and is located at the coordinate origin. As the drawing shows, an electric fi eld of Ex = +245 N/C exists along the +x axis. A magnetic fi eld also exists, and its x and y com- ponents are Bx = +1.80 T and By = +1.40 T. Calculate the force (magnitude and direction) exerted on the particle by each of the three fi elds when it
is (a) stationary, (b) moving along the +x axis at a speed of 375 m/s, and (c) moving along the +z axis at a speed of 375 m/s.
+y
+x
+z
q Bx
Ex
By
PROBLEM 82
83. M V-HINT Available in WileyPLUS. 84. H Available in WileyPLUS. 85. H SSM Available in WileyPLUS. 86. M GO The fi gure shows two parallel, straight wires that are very long. The wires are separated by a distance of 0.065 m and carry currents of I1 = 15 A and I2 = 7.0 A. Find the magnitude and direction of the force that the magnetic fi eld of wire 1 applies to a 1.5-m section of wire 2 when the cur-
rents have (a) opposite and (b) the same directions.
Repulsion
(a)
F
B
–F I1 I2
Wire 1 Wire 2
PROBLEM 86 Attraction
(b)
F
B
–F
I1 I2
F
Wire 2
Additional Problems
3.9 A
4.6 A
0.050 m
8.5 AI
PROBLEM 80
624 CHAPTER 21 Magnetic Forces and Magnetic Fields
Both magnetic and electric fi elds can apply forces to an electric charge. How-
ever, there are distinct diff erences in the way the two types of fi elds apply
their forces. Problem 87 serves to review how the two types of fi elds behave.
A number of forces can act on a rigid object, and some of them can produce
torques, as Chapter 9 discusses. If, as a result of the forces and torques, the
object has no acceleration of any kind, it is in equilibrium. Problem 88 illus-
trates how the magnetic force can be one of the forces keeping an object in
equilibrium.
87. M CHALK SSM The fi gure shows a particle that carries a charge of q0 = −2.80 × 10−6 C. It is moving along the +y axis at a speed of 𝜐 = 4.8 × 106 m/s. A magnetic fi eld B→ of magnitude 3.35 × 10−5 T is direc- ted along the +z axis, and an electric fi eld E→ of magnitude 123 N/C points along the −x axis. Concepts: (i) What forces make up the net force acting on the particle? (ii) How do you determine the direction of the magnetic force
acting on the negative charge? (iii) How do you determine the direction of
the electric force acting on the negative charge? (iv) Does the fact that the
charge is moving aff ect the values of the magnetic and electric forces? Cal- culations: Determine the magnitude and direction of the net force that acts on the particle.
88. M CHALK A 125-turn rectangular coil of wire is hung from one arm of a balance, as the fi gure shows. With the magnetic fi eld B→ turned off , an object of mass M is added to the pan on the other arm to balance the weight of the coil. Concepts: (i) In a balanced, or equilibrium, condition the device has no angular acceleration. What does this imply about the net torque acting
on the device? (ii) What is torque? (iii) In calculating the torques acting on
an object in equilibrium, where do you locate the axis of rotation? Calcu- lations: When a constant 0.200-T magnetic fi eld is turned on and there is a current of 8.50 A in the coil, how much additional mass m must be added to regain the balance?
PROBLEM 88
Axis
I
M m
125-turn coil
0.0150 m
B (into paper)
ℓ ℓ
Concepts and Calculations Problems
PROBLEM 87
B
E
v
+y
+x
+z
q0
89. M An Electron Evaporator. Electron beams are sometimes used to melt and evaporate
metals in order to deposit thin metallic fi lms on
surfaces (similar to gold plating). One method is
to put the material to be evaporated (called the
“target”) into a small tungsten cup (a crucible that
has a very high melting point) and direct a beam of
electrons at the target. Your team has been given
the task of designing an electron-beam evapor-
ator. The crucible is a cylinder, 2.0 cm in diameter
and 1.5 cm in height, and contains a small target
of pure nickel (Ni). The electrons are accelerated
through a potential diff erence of V = 1.20 kV, and form a beam that originates below the crucible, exactly 3.70 cm off its center,
in the +x direction (see the drawing). (a) What is the speed of the electrons in the beam? (b) You must steer the electron beam with a magnetic fi eld so that it curls over the lip of the cup and strikes the nickel target. Assuming that a
uniform fi eld exists above the cup (the fi eld is zero below), what must be the
radius of the beam’s circular path? (c) In what direction should the fi eld point
if the beam initially approaches the cup from the –y axis? (d) What must be the magnitude of the uniform magnetic fi eld?
90. M An Isotope Separator. Hydrogen has three isotopes 1H (m1 = mp), 2H (m2 ≌ 2mp), and 3H (ms ≌ 3mp), where mp is the mass of a proton (1.67 × 10–27 kg). You and your team are tasked with constructing an isotope separ-
ator that will separate a gas of mixed hydrogen isotopes. The gas fi rst passes
through a device that atomizes it (i.e., makes sure the atoms are separate, and
do not form H2 molecules), and then ionizes the atoms (strips off their only
electron) so that they have a net charge of +e. Next, the atoms (now positive ions) are accelerated between the plates of a parallel-plate capacitor with a
voltage of 2.5 kV across it, and emerge through a hole in one of the plates
as a beam. (a) What are the speeds of the three isotopes when they emerge from the capacitor plates? (b) The accelerated ions enter a region of uniform magnetic fi eld oriented perpendicular to the velocity vector of the ion beam.
What should be the magnitude of the magnetic fi eld if you want the largest
diameter of the three ion paths to be 20.0 cm? (c) If you are collecting the atoms after completing a half-circle, one collector should be located 20.0 cm
from the point where the beam enters the magnetic fi eld. Where should the
other two be located?
V
y
x
r
O
Electron beam
Field region
3.70 cm
PROBLEM 89
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
22.1 Predict when an induced current will flow.
22.2 Solve motional emf problems.
22.3 Calculate magnetic flux.
22.4 Solve problems using Faraday’s law of induction.
22.5 Predict the direction of an induced current using Lenz’s law.
22.6 Describe how sound is reproduced via induction.
22.7 Solve problems involving generators.
22.8 Define mutual induction and self- inductance.
22.9 Solve problems involving transformers.
© J
eff
G re
en b er
g /A
g e
F o to
st o ck
CHAPTER 22
Electromagnetic Induction
Electric guitars are famous for their amplifi ed and manipulatable sound. To produce this sound, virtually
all of them have one or more electromagnetic pickups located beneath the strings (see Section 22.6).
These pickups work because of electromagnetic induction, which is the process by which a magnet is
used to create or induce an emf in a coil of wire. In this photograph the pickup is indicated by the shiny
rectangle in the white area.
22.1 Induced Emf and Induced Current There are a number of ways a magnetic fi eld can be used to generate an electric cur-
rent, and Interactive Figure 22.1 illustrates one of them. This drawing shows a bar magnet and a helical coil of wire to which an ammeter is connected. When there
is no relative motion between the magnet and the coil, as in part a of the drawing, the ammeter reads zero, indicating that no current exists. However, when the magnet
moves toward the coil, as in part b, a current I appears. As the magnet approaches, the magnetic fi eld B
→ that it creates at the location of the coil becomes stronger and stron-
ger, and it is this changing fi eld that produces the current. When the magnet moves away from the coil, as in part c, a current is also produced, but with a reversed direc- tion. Now the magnetic fi eld at the coil becomes weaker as the magnet moves away.
Once again it is the changing fi eld that generates the current. A current would also be created in Interactive Figure 22.1 if the magnet were
held stationary and the coil were moved, because the magnetic fi eld at the coil would
be changing as the coil approached or receded from the magnet. Only relative motion
between the magnet and the coil is needed to generate a current; it does not matter
which one moves.
625
626 CHAPTER 22 Electromagnetic Induction
The current in the coil is called an induced current because it is brought about (or “induced”) by a changing magnetic fi eld. Since a source of emf (electromotive force) is always needed to
produce a current, the coil itself behaves as if it were a source of emf. This emf is known as an
induced emf. Thus, a changing magnetic fi eld induces an emf in the coil, and the emf leads to an induced current.
THE PHYSICS OF . . . an automobile cruise control. Induced emf and induced current are frequently used in the cruise controls found in many cars. Interactive Figure 22.2 illustrates how a cruise control operates. Usually two magnets are mounted on opposite sides of the vehi-
cle’s drive shaft, with a stationary sensing coil positioned nearby. As the shaft turns, the magnets
pass by the coil and cause an induced emf and current to appear in it. A microprocessor (the
“brain” of a computer) counts the pulses of current and, with the aid of its internal clock and a
knowledge of the shaft’s radius, determines the rotational speed of the drive shaft. The rotational
speed, in turn, is related to the car’s speed. Thus, once the driver sets the desired cruising speed
with the speed control switch (mounted near the steering wheel), the microprocessor can com-
pare it with the measured speed. To the extent that the selected cruising speed and the measured
speed diff er, a signal is sent to a servo, or control, mechanism, which causes the throttle/fuel
injector to send more or less fuel to the engine. The car speeds up or slows down accordingly,
until the desired cruising speed is reached.
Figure 22.3 shows another way to induce an emf and a current in a coil. An emf can be induced by changing the area of a coil in a constant magnetic fi eld. Here the shape of the coil is being distorted to reduce the area. As long as the area is changing, an induced emf and cur-
rent exist; they vanish when the area is no longer changing. If the distorted coil is returned to its
original shape, thereby increasing the area, an oppositely directed current is generated while the
area is changing.
S NS NS N
Ammeter
Current upward
Bar magnet Coil
I I
B
(a) (b)
I I
(c)
Current downward
B
INTERACTIVE FIGURE 22.1 (a) When there is no relative motion between the coil of wire and the bar magnet, there is no current in the coil. (b) A current is created in the coil when the magnet moves toward the coil. (c) A current also exists when the magnet moves away from the coil, but the direction of the current is opposite to that in (b).
Microprocessor Servo control mechanism
Throttle/Fuel injector
Magnet
Sensing coil Drive shaft
Speed control switch
INTERACTIVE FIGURE 22.2 Induced emf lies at the heart of an automobile cruise control,
in which an emf is induced in a sensing coil by
magnets attached to the rotating drive shaft.
22.2 Motional Emf 627
In each of the previous examples, both an emf and a current are induced in the coil because
the coil is part of a complete, or closed, circuit. If the circuit were open—perhaps because of an
open switch—there would be no induced current. However, an emf would still be induced in the
coil, whether the current exists or not.
Changing a magnetic fi eld and changing the area of a coil are methods that can be used to
create an induced emf. The phenomenon of producing an induced emf with the aid of a magnetic
fi eld is called electromagnetic induction. The next section discusses yet another method by which an induced emf can be created.
Check Your Understanding
(The answer is given at the end of the book.) 1. Suppose that the coil and the magnet in Interactive Figure 22.1a were each moving with the same
velocity relative to the earth. Would there be an induced current in the coil?
22.2 Motional Emf
The Emf Induced in a Moving Conductor When a conducting rod moves through a constant magnetic fi eld, an emf is induced in the rod.
This special case of electromagnetic induction arises as a result of the magnetic force that acts
on a moving charge (see Section 21.2). Consider the metal rod of length L moving to the right in Animated Figure 22.4a. The velocity v→ of the rod is constant and is perpendicular to a uniform magnetic fi eld B
→ . Each charge q within the rod also moves with a velocity v→ and experiences a
magnetic force of magnitude F = ∣q∣𝜐B, according to Equation 21.1. By using RHR-1, it can be seen that the mobile, free electrons are driven to the bottom of the rod, leaving behind an equal
amount of positive charge at the top. (Remember to reverse the direction of the force that RHR-1
predicts, since the electrons have a negative charge. See Section 21.2.) The positive and negative
charges accumulate until the attractive electric force that they exert on each other becomes equal
in magnitude to the magnetic force. When the two forces balance, equilibrium is reached and no
further charge separation occurs.
The separated charges on the ends of the moving conductor give rise to an induced emf,
called a motional emf because it originates from the motion of charges through a magnetic fi eld. The emf exists as long as the rod moves. If the rod is brought to a halt, the magnetic force van-
ishes, with the result that the attractive electric force reunites the positive and negative charges
and the emf disappears. The emf of the moving rod is analogous to the emf between the termi-
nals of a battery. However, the emf of a battery is produced by chemical reactions, whereas the
motional emf is created by the agent that moves the rod through the magnetic fi eld (like the hand
in Animated Figure 22.4b). The fact that the electric and magnetic forces balance at equilibrium in Animated Figure22.4a
can be used to determine the magnitude of the motional emf ℰ. Acccording to Equation 18.2,
the magnitude of the electric force acting on the positive charge q at the top of the rod is Eq, where E is the magnitude of the electric fi eld due to the separated charges. And according to Equation 19.7a (without the minus sign), the electric fi eld magnitude is given by the voltage
between the ends of the rod (the emf ℰ) divided by the length L of the rod. Thus, the electric force is Eq = (ℰ/L)q. Since we are dealing now with a positive charge, the magnetic force is B∣q∣(𝜐 sin 90°) = Bq𝜐, according to Equation 21.1, because the charge q moves perpendicular to the magnetic fi eld. Since these two forces balance, it follows that (ℰ/L)q = Bq𝜐. The emf, then, is
Motional emf when v→, B → ,
and L are mutually ℰ = 𝜐BL (22.1) perpendicular
As expected, ℰ = 0 V when 𝜐 = 0 m/s, because no motional emf is developed in a stationary
rod. Greater speeds and stronger magnetic fi elds lead to greater emfs for a given length L. As with
I I
Ammeter
FIGURE 22.3 While the area of the coil is changing, an induced emf and current are
generated.
Conducting rod
Conducting rail
+++
+
–
–
(a)
(b)
B
I
I
I L
L
– –
v
v
ANIMATED FIGURE 22.4 (a) When a conducting rod moves at right angles to a
constant magnetic fi eld, the magnetic force
causes opposite charges to appear at the ends
of the rod, giving rise to an induced emf.
(b) The induced emf causes an induced current I to appear in the circuit.
628 CHAPTER 22 Electromagnetic Induction
batteries, ℰ is expressed in volts. In Animated Figure 22.4b the rod is sliding on conducting rails that form part of a closed circuit, and L is the length of the rod between the rails. Due to the emf, electrons fl ow in a clockwise direction around the circuit. Positive charge would fl ow in the
direction opposite to the electron fl ow, so the conventional current I is drawn counterclockwise in the picture. Example 1 illustrates how to determine the electrical energy that the motional emf
delivers to a device such as the light bulb in the drawing.
EXAMPLE 1 Operating a Light Bulb with Motional Emf
Suppose that the rod in Animated Figure 22.4b is moving at a speed of 5.0 m/s in a direction perpendicular to a 0.80-T magnetic fi eld. The rod
has a length of 1.6 m and a negligible electrical resistance. The rails also
have negligible resistance. The light bulb, however, has a resistance of
96 Ω. Find (a) the emf produced by the rod, (b) the current induced in the circuit, (c) the electric power delivered to the bulb, and (d) the energy used by the bulb in 60.0 s.
Reasoning The moving rod acts like an imaginary battery and supplies a motional emf of 𝜐BL to the circuit. The induced current can be deter- mined from Ohm’s law as the motional emf divided by the resistance of
the bulb. The electric power delivered to the bulb is the product of the
induced current and the potential diff erence across the bulb (which, in this
case, is the motional emf). The energy used is the product of the power
and the time.
Solution (a) The motional emf is given by Equation 22.1 as ℰ = υBL = (5.0 m /s)(0.80 T)(1.6 m) = 6.4 V
(b) According to Ohm’s law, the induced current is equal to the motional emf divided by the resistance of the circuit:
I = ℰ
R =
6.4 V
96 Ω = 0.067 A (20.2)
(c) The electric power P delivered to the light bulb is the product of the current I and the potential diff erence across the bulb:
P = Iℰ = (0.067 A)(6.4 V) = 0.43 W (20.6a)
(d) Since power is energy per unit time, the energy E used in 60.0 s is the product of the power and the time:
E = Pt = (0.43 W)(60.0 s) = 26 J (6.10b)
Motional Emf and Electrical Energy Motional emf arises because a magnetic force acts on the charges in a conductor that is moving
through a magnetic fi eld. Whenever this emf causes a current, a second magnetic force enters the
picture. In Animated Figure 22.4b, for instance, the second force arises because the current I in the rod is perpendicular to the magnetic fi eld. The current, and hence the rod, experiences a mag-
netic force F→ whose magnitude is given by Equation 21.3 as F = ILB sin 90°. Using the values of I, L, and B given in Example 1, we see that F = (0.067 A)(1.6 m)(0.80 T) = 0.086 N. The direction of F→ is specifi ed by RHR-1 and is opposite to the velocity v→ of the rod, and thus points to the left (see Figure 22.5). By itself, F→ would slow down the rod, and here lies the crux of the matter. To keep the rod moving to the right with a constant velocity, a counterbalancing force
must be applied to the rod by an external agent, such as the hand in the picture. This force is
labeled F→hand in the drawing. The counterbalancing force must have a magnitude of 0.086 N and must be directed opposite to the magnetic force F→. If the counterbalancing force were removed, the rod would decelerate under the infl uence of F→ and eventually come to rest. During the decel- eration, the motional emf would decrease and the light bulb would eventually go out.
We can now answer an important question—Who or what provides the 26 J of electrical
energy that the light bulb in Example 1 uses in 60.0 seconds? The provider is the external agent
that applies the 0.086-N counterbalancing force needed to keep the rod moving. This agent does
work, and Example 2 shows that the work done is equal to the electrical energy used by the bulb.
+
–
I
I
I v F
Fhand
+
–
I v F
B
Fhand
x
FIGURE 22.5 A magnetic force F→ is exerted on the current I in the moving rod and is directed opposite
to the rod’s velocity v→. Since the force F→hand counterbalances the magnetic force F→, the rod moves to the right at a constant velocity.
22.2 Motional Emf 629
Analyzing Multiple-Concept Problems
EXAMPLE 2 The Work Needed to Keep the Light Bulb Burning
As we saw in Example 1, an induced current of 0.067 A exists in the
circuit due to the moving rod. As Figure 22.5 shows, the hand provides a force F→hand that keeps the rod moving to the right. Determine the work done by this force in a time of 60.0 s. Assume, as in Example 1, that the
magnetic fi eld has a magnitude of 0.80 T and that the rod has a length of
1.6 m and moves at a constant speed of 5.0 m/s.
Reasoning According to the discussion in Section 6.1, the work done by the hand is equal to the product of (1) the magnitude Fhand of the force exerted by the hand, (2) the magnitude x of the rod’s displacement, and (3) the cosine of the angle between the force and the displacement. Since
the rod moves to the right at a constant speed, it has no acceleration and
is, therefore, in equilibrium (see Section 4.11). Thus, the force exerted
by the hand must be equal in magnitude, but opposite in direction, to the
magnetic force F→ exerted on the rod, since they are the only two forces acting on the rod along the direction of the motion. We will determine
the magnitude F of the magnetic force by using Equation 21.3, and this will enable us to fi nd Fhand. Since the rod moves at a constant speed, the magnitude x of its displacement is the product of its speed and the time of travel.
Knowns and Unknowns The data for this problem are:
Description Symbol Value Current I 0.067 A
Length of rod L 1.6 m
Speed of rod 𝜐 5.0 m/s
Time during which rod moves t 60.0 s
Magnitude of magnetic field B 0.80 T
Unknown Variable Work done by hand W ?
Modeling the Problem
STEP 1 Work The work done by the hand in Figure 22.5 is given by W = Fhandx cos 𝜃ʹ (Equa- tion 6.1). In this equation, Fhand is the magnitude of the force that the hand exerts on the rod, x is the magnitude of the rod’s displacement, and 𝜃ʹ is the angle between the force and the displace-
ment. Since the force and displacement point in the same direction, 𝜃ʹ = 0°, so
W = Fhand x cos 0°
Two forces act on the rod; the force F→hand, which points to the right, and the magnetic force F →
,
which points to the left. Since the rod moves at a constant velocity, the magnitudes of these two
forces are equal, so that Fhand = F. Substituting this relation into the expression for the work gives Equation 1 at the right. At this point, neither F nor x is known, but they will be evaluated in Steps 2 and 3, respectively.
STEP 2 Magnetic Force Exerted on a Current-Carrying Rod We have seen in Section 21.5 that a rod of length L that carries a current I in a magnetic fi eld of magnitude B experiences a magnetic force of magnitude F. The magnitude of the force is given by F = ILB sin 𝜃 (Equation 21.3), where 𝜃 is the angle between the direction of the current and the magnetic fi eld. In this
case, the current and magnetic fi eld are perpendicular to each other (see Figure 22.5), so 𝜃 = 90°. Thus, the magnitude of the magnetic force is
F = ILB sin 90°
The quantities, I, L, and B are known, and we substitute this expression into Equation 1 at the right.
STEP 3 Kinematics Since the rod is moving at a constant speed, the distance x it travels is the product of its speed 𝜐 and the time t:
x = υt
The variables 𝜐 and t are known. We can also substitute this relation into Equation 1, as shown in the right column.
W = Fx cos 0° (1)
??
W = Fx cos 0° (1)
F = ILB sin 90° ?
W = Fx cos 0° (1)
F = ILB sin 90° x = υt
630 CHAPTER 22 Electromagnetic Induction
It is important to realize that the direction of the current in Figure 22.5 is consistent with the principle of conservation of energy. Consider what would happen if the direction of the cur-
rent were reversed, as in Figure 22.6. With the direction of the current reversed, the direction of the magnetic force F→ would also be reversed and would point in the direction of the velocity v→ of the rod. As a result, the force would cause the rod to accelerate rather than decelerate. The rod would accelerate without the need for an external force (like that provided by the hand in
Figure 22.5) and would create a motional emf that supplies energy to the light bulb. Thus, this hypothetical generator would produce energy out of nothing, since there is no external agent.
Such a device cannot exist because it violates the principle of conservation of energy, which
states that energy cannot be created or destroyed, but can only be converted from one form to
another. Therefore, the current cannot be directed clockwise around the circuit, as in Figure 22.6. In situations such as the one in Examples 1 and 2, when a motional emf leads to an induced cur-
rent, a magnetic force always appears that opposes the motion, in accord with the principle of
conservation of energy. Conceptual Example 3 deals further with the important issue of energy
conservation.
Solution Algebraically combining the results of the three steps, we have
W = Fx cos 0° = (ILB sin 90°)x cos 0° = (ILB sin 90°)(υt) cos 0°
The work done by the force of the hand is
W = (ILB sin 90°)(υt) cos 0° = (0.067 A)(1.6 m)(0.80 T)(sin 90°)(5.0 m/s)(60.0 s)(cos 0°) = 26 J
The 26 J of work done on the rod by the hand is mechanical energy and is the same as the 26 J
of energy consumed by the light bulb (see Example 1). Hence, the moving rod and the magnetic
force convert mechanical energy into electrical energy, much as a battery converts chemical
energy into electrical energy.
Related Homework: Problem 8
STEP 1 STEP 2 STEP 2
I
I
F v
–
+
I
FIGURE 22.6 The current cannot be directed clockwise in this circuit, because the
magnetic force F→ exerted on the rod would then be in the same direction as the velocity
v→. The rod would accelerate to the right and create energy on its own, violating the
principle of conservation of energy.
CONCEPTUAL EXAMPLE 3 Conservation of Energy
Figure 22.7a illustrates a conducting rod that is free to slide down be- tween two vertical copper tracks. There is no kinetic friction between
the rod and the tracks, although the rod maintains electrical contact with
the tracks during its fall. A constant magnetic fi eld B→ is directed perpen- dicular to the motion of the rod, as the drawing shows. Because there is
no friction, the only force that acts on the rod is its weight W→, so the rod falls with an acceleration equal to the acceleration due to gravity, which
has a magnitude of g = 9.8 m/s2. Suppose that a resistance R is connected between the tops of the tracks, as in part b of the drawing. Is the magnitude of the acceleration with which the rod now falls (a) equal to g, (b) greater than g, or (c) less than g?
Reasoning As the rod falls perpendicular to the magnetic fi eld, a motional emf is induced between its ends. This emf is induced whether or not the
resistance R is attached between the tracks. However, when R is present, a complete circuit is formed, and the emf produces an induced current I that is perpendicular to the fi eld. The direction of this current is such that the
rod experiences an upward magnetic force F→, opposite to the weight of the rod (see part b of the drawing and use RHR-1). The net force acting on the rod is W→ + F→, which is less than the weight, since F→ points upward and the weight W→ points downward. In accord with Newton’s second law of motion, the downward acceleration is proportional to the net force.
Answers (a) and (b) are incorrect. Since the net downward force on the rod in Figure 22.7b is less than the rod’s weight and since the down- ward acceleration is proportional to the net force, the rod cannot have an
acceleration whose magnitude is equal to or greater than g.
Answer (c) is correct. Since the net downward force on the rod when R is present is less than the rod’s weight and since the downward accel- eration is proportional to the net force, the downward acceleration has a
magnitude less than g. Thus, the rod gains speed as it falls but does so less rapidly than if R were not present. As the speed of the rod in Figure 22.7b increases during the descent, the magnetic force increases, until the time comes when its magnitude equals the magnitude of the rod’s weight.
When this occurs, the net force and the rod’s acceleration will be zero.
From this moment on, the rod will fall at a constant velocity. In any event,
the rod always has a smaller speed than does a freely falling rod (i.e., R is absent) at the same place. The speed is smaller because only part of
the gravitational potential energy (GPE) is being converted into kinetic
energy (KE) as the rod falls, with part also being dissipated as heat in the
resistance R. In fact, when the rod eventually attains a constant velocity, none of the GPE is converted into KE and all of it is dissipated as heat.
Related Homework: Problem 10
22.3 Magnetic Flux 631
Check Your Understanding
(The answers are given at the end of the book.) 2. Consider the induced emf being generated in Animated Figure 22.4. Suppose that the length of the rod
is reduced by a factor of four. For the induced emf to be the same, what should be done? (a) Without changing the speed of the rod, increase the strength of the magnetic fi eld by a factor of four. (b) With- out changing the magnetic fi eld, increase the speed of the rod by a factor of four. (c) Increase both the speed of the rod and the strength of the magnetic fi eld by a factor of two. (d) All of the previous three methods may be used.
3. In the discussion concerning Figure 22.5, we saw that a force of 0.086 N from an external agent was required to keep the rod moving at a constant velocity. Suppose that friction is absent and that the light
bulb is suddenly removed from its socket while the rod is moving. How much force does the external
agent then need to apply to the rod to keep it moving at a constant velocity? (a) 0 N (b) Greater than 0 N but less than 0.086 N (c) More than 0.086 N (d) 0.086 N
4. Eddy currents are electric currents that can arise in a piece of metal when it moves through a region where the magnetic fi eld is not the same everywhere. CYU Figure 22.1 shows, for example, a metal sheet moving to the right at a velocity v→ and a magnetic fi eld B→ that is directed perpendicular to the sheet. At the instant represented, the fi eld only extends over the left half of the sheet. An emf is induced
that leads to the eddy current indicated. Such eddy currents cause the velocity of the moving sheet to
decrease and are used in various devices as a brake to damp out unwanted motion. Does the eddy cur-
rent in the drawing circulate (a) counterclockwise or (b) clockwise?
CYU FIGURE 22.1
v
B (into paper)
Eddy current
Metal sheet
22.3 Magnetic Flux
Motional Emf and Magnetic Flux Motional emf, as well as any other type of induced emf, can be described in terms of a concept
called magnetic fl ux. Magnetic fl ux is analogous to electric fl ux, which deals with the electric fi eld and the surface through which it passes (see Section 18.9 and Figure 18.33). Magnetic fl ux
FIGURE 22.7 (a) There is no kinetic friction between the falling rod and the tracks, so the
only force acting on the rod is its weight W→. (b) When an induced current I exists in the circuit, a magnetic force F→ also acts on the rod.
Vertical tracks
Conducting rod
W
B
(a) (b)
W
B
F
I
R
I
632 CHAPTER 22 Electromagnetic Induction
is defi ned in a similar way by bringing together the magnetic fi eld and the surface through which
it passes.
We can see how the motional emf is related to the magnetic fl ux with the aid of Figure 22.8, which shows the rod used to derive Equation 22.1 (ℰ = 𝜐BL). In this drawing the rod moves through a magnetic fi eld beginning at time t = 0 s. In part a the rod has moved a distance x0 to the right at time t0, whereas in part b it has moved a greater distance x at a later time t. The speed 𝜐 of the rod is the distance traveled divided by the elapsed time: 𝜐 = (x − x0)/(t − t0). Substituting this expression for 𝜐 into ℰ = 𝜐BL gives
ℰ = ( x − x 0 t − t 0 )BL = (
xL − x 0 L t − t0 )B
As the drawing indicates, the term x0L is the area A0 swept out by the rod in moving a distance x0, and xL is the area A swept out in moving a distance x. Thus, the emf becomes
ℰ = ( A − A0 t − t0 )B =
(BA) − (BA) 0 t − t0
The product BA of the magnetic fi eld strength and the area appears in the numerator of this expression. This product is called magnetic fl ux and is represented by the symbol Φ (Greek capital letter phi); thus Φ = BA. The magnitude of the induced emf is the change in fl ux ΔΦ = Φ − Φ0 divided by the time interval Δt = t − t0 during which the change occurs:
ℰ = Φ − Φ0
t − t0 =
∆Φ
∆t
In other words, the induced emf equals the time rate of change of the magnetic fl ux.
You will almost always see the previous equation written with a minus sign—namely,
ℰ = −ΔΦ/Δt. The minus sign is introduced for the following reason: The direction of the current induced in the circuit is such that the magnetic force F→ acts on the rod to oppose its motion, thereby tending to slow down the rod (see Figure 22.5). The minus sign ensures that the polarity of the induced emf sends the induced current in the proper direction so as to give rise to this opposing mag-
netic force.* This issue of the polarity of the induced emf will be discussed further in Section 22.5.
The advantage of writing the induced emf as ℰ = −ΔΦ/Δt is that this relation is far more general than our present discussion suggests. In Section 22.4 we will see that ℰ = −ΔΦ/Δt can be applied to all possible ways of generating induced emfs.
A General Expression for Magnetic Flux In Figure 22.8 the direction of the magnetic fi eld B→ is perpendicular to the surface swept out by the moving rod. In general, however, B→ may not be perpendicular to the surface. For instance, in Figure 22.9 the direction perpendicular to the surface is indicated by the normal to the surface,
Area = A0
t = 0 s t = 0 s
t
(a) (b)
t0
L
B
v
x0
Area = A
x
v
FIGURE 22.8 (a) In a time t0, the moving rod sweeps out an area A0 = x0L. (b) The area swept out in a time t is A = xL. In both parts of the fi gure the areas are shaded in color.
*A detailed mathematical discussion of why the minus sign arises is beyond the scope of this book.
Normal
Surface (area = A)
B
B cos
ϕ
ϕ
FIGURE 22.9 When computing the magnetic fl ux, the component of the magnetic fi eld that
is perpendicular to the surface must be used;
this component is B cos 𝜙.
22.3 Magnetic Flux 633
but the magnetic fi eld is inclined at an angle 𝜙 with respect to this direction. In such a case the
fl ux is computed using only the component of the fi eld perpendicular to the surface, B cos 𝜙. The general expression for magnetic fl ux is
Φ = (B cos ϕ) A = BA cos ϕ (22.2)
If either the magnitude B of the magnetic fi eld or the angle 𝜙 is not constant over the surface (i.e., they are not the same at each point on the surface), an average value for the product B cos 𝜙 must be used to compute the fl ux. Equation 22.2 shows that the unit of magnetic fl ux is the tesla · meter2 (T · m2). This unit is called a weber (Wb), after the German physicist Wilhelm Weber (1804 – 1891): 1 Wb = 1 T · m2. Example 4 illustrates how to determine the magnetic fl ux for three diff erent orientations of the surface of a coil relative to the magnetic fi eld.
Math Skills Equation 22.2 uses the component of the magnetic fi eld perpendicular to the surface in defi ning the magnetic fl ux Φ. In order to determine this component of the fi eld, we use the cosine
function. According to the defi nition given in Equation 1.1, the cosine function is cos ϕ = ha h
, where
ha is the length of the side of a right triangle that is adjacent to the angle 𝜙 and h is the length of the hypot- enuse (see Figure 22.10a). Figure 22.10b shows the fi eld B→ (magnitude B) and its components Bx and By. The fi eld B→ is oriented at an angle 𝜙 with respect to the normal, and the component that we seek is By, the one that points along the direction of the normal. By comparing Figures 22.10a and b, we can see that
cos ϕ = h a h
= By B or By = B cos ϕ
FIGURE 22.10 Math Skills drawing.
hha
Normal
Surface
(a)
90° By
Bx
Normal
Surface
(b)
B ϕ ϕ
EXAMPLE 4 Magnetic Flux
A rectangular coil of wire is situated in a constant magnetic fi eld whose
magnitude is 0.50 T. The coil has an area of 2.0 m2. Determine the mag-
netic fl ux for the following three orientations, 𝜙 = 0°, 60.0°, and 90.0°,
shown in Figure 22.11.
Reasoning The magnetic fl ux Φ is defi ned as Φ = BA cos 𝜙, where B is the magnitude of the magnetic fi eld, A is the area of the surface through which the magnetic fi eld passes, and 𝜙 is the angle between the magnetic
fi eld and the normal to the surface.
Problem-Solving Insight The magnetic fl ux Φ is determined by more than just the magnitude B of the magnetic fi eld and the area A. It also depends on the angle 𝟇 (see Figure 22.9 and Equation 22.2).
Solution The magnetic fl ux for the three cases is: 𝜙 = 0º Φ = (0.50 T)(2.0 m2) cos 0° = 1.0 Wb 𝜙 = 60.0º Φ = (0.50 T)(2.0 m2) cos 60.0° = 0.50 Wb 𝜙 = 90.0º Φ = (0.50 T)(2.0 m2) cos 90.0° = 0 Wb
Magnetic field lines
Coil
Normal ϕ = 0° ϕ = 60° ϕ = 90°
60° 90°
FIGURE 22.11 Three orientations of a rectangular coil (drawn as an edge view) relative to the magnetic fi eld lines. The magnetic fi eld lines
that pass through the coil are those in the regions shaded in blue.
634 CHAPTER 22 Electromagnetic Induction
Graphical Interpretation of Magnetic Flux It is possible to interpret the magnetic fl ux graphically because the magnitude of the mag-
netic fi eld B→ is proportional to the number of fi eld lines per unit area that pass through a surface perpendicular to the lines (see Section 21.1). For instance, the magnitude of B→ in Figure 22.12a is three times larger than it is in part b of the drawing, since the number of fi eld lines drawn through the identical surfaces is in the ratio of 3:1. Because Φ is directly
proportional to B for a given area, the fl ux in part a is also three times larger than the fl ux in part b. Therefore, the magnetic fl ux is proportional to the number of fi eld lines that pass through a surface.
The graphical interpretation of fl ux also applies when the surface is oriented at an angle
with respect to B→. For example, as the coil in Figure 22.11 is rotated from 𝜙 = 0° to 60° to 90°, the number of magnetic fi eld lines passing through the surface (see the fi eld lines in the regions
shaded in blue) changes in the ratio of 8 : 4 : 0 or 2 : 1 : 0. The results of Example 4 show that the
fl ux in the three orientations changes by the same ratio. Because the magnetic fl ux is proportional
to the number of fi eld lines passing through a surface, we often use phrases such as “the fl ux that
passes through a surface bounded by a loop of wire.”
Check Your Understanding
(The answers are given at the end of the book.) 5. A magnetic fi eld has the same direction and the same magnitude B everywhere. A circular area A is
bounded by a loop of wire. Which of the following statements is true concerning the magnitude of the
magnetic fl ux that passes through this area? (a) It is zero. (b) It is BA. (c) Its maximum possible value is BA. (d) Its minimum possible value is BA.
6. Suppose that a magnetic fi eld is constant everywhere on a fl at 1.0-m2 surface and that the magnetic fl ux through this surface is 2.0 Wb. From these data, which one of the following pieces of information
can be determined about the magnetic fi eld? (a) The magnitude of the fi eld (b) The magnitude of the component of the fi eld that is perpendicular to the surface (c) The magnitude of the component of the fi eld that is parallel to the surface
22.4 Faraday’s Law of Electromagnetic Induction Two scientists are given credit for the discovery of electromagnetic induction: the Englishman
Michael Faraday (1791–1867) and the American Joseph Henry (1797–1878). Since Faraday
investigated electromagnetic induction in more detail and published his fi ndings fi rst, the law
that describes the phenomenon bears his name.
Faraday discovered that whenever there is a change in fl ux through a loop of wire, an emf is induced in the loop. In this context, the word “change” refers to a change as time passes. A fl ux
that is constant in time creates no emf. Faraday’s law of electromagnetic induction is expressed
by bringing together the idea of magnetic fl ux and the time interval during which it changes. In
fact, Faraday found that the magnitude of the induced emf is equal to the time rate of change of
the magnetic fl ux. This is consistent with the relation we obtained in Section 22.3 for the specifi c
case of motional emf: ℰ = −ΔΦ/Δt. Often the magnetic fl ux passes through a coil of wire containing more than one loop
(or turn). If the coil consists of N loops, and if the same fl ux passes through each loop, it is found experimentally that the total induced emf is N times that induced in a single loop. An analogous situation occurs in a fl ashlight when two 1.5-V batteries are stacked in series on
top of one another to give a total emf of 3.0 volts. For the general case of N loops, the total induced emf is described by Faraday’s law of electromagnetic induction in the following
manner:
Magnetic field lines
Surface (perpendicular to
magnetic field lines) (a)
(b)
FIGURE 22.12 The magnitude of the magnetic fi eld in (a) is three times as great as that in (b) because the number of magnetic fi eld lines crossing the surfaces is in the
ratio of 3 : 1.
22.4 Faraday’s Law of Electromagnetic Induction 635
FARADAY’S LAW OF ELECTROMAGNETIC INDUCTION The average emf ℰ induced in a coil of N loops is
ℰ = −N ( Φ − Φ0
t − t0 ) = −N ∆Φ
∆ t (22.3)
where ΔΦ is the change in magnetic fl ux through one loop and Δt is the time interval during which the change occurs. The term ΔΦ/Δt is the average time rate of change of the fl ux that passes through one loop. SI Unit of Induced Emf: volt (V)
Faraday’s law states that an emf is generated if the magnetic fl ux changes for any reason.
Since the fl ux is given by Equation 22.2 as Φ = BA cos 𝜙, it depends on the three factors, B, A, and 𝜙, any of which may change. Example 5 considers a change in B.
EXAMPLE 5 The Emf Induced by a Changing Magnetic Field
A coil of wire consists of 20 turns, or loops, each with an area of 1.5 ×
10−3 m2. A magnetic fi eld is perpendicular to the surface of each loop at
all times, so that 𝜙 = 𝜙0 = 0°. At time t0 = 0 s, the magnitude of the fi eld at the location of the coil is B0 = 0.050 T. At a later time t = 0.10 s, the magnitude of the fi eld at the coil has increased to B = 0.060 T. (a) Find the average emf induced in the coil during this time. (b) What would be the value of the average induced emf if the magnitude of the magnetic
fi eld decreased from 0.060 T to 0.050 T in 0.10 s?
Reasoning To fi nd the induced emf, we use Faraday’s law of electro- magnetic induction (Equation 22.3), combining it with the defi nition of
magnetic fl ux from Equation 22.2. We note that only the magnitude of the
magnetic fi eld changes in time. All other factors remain constant.
Problem-Solving Insight The change in any quantity is the fi nal value minus the initial value: e.g., the change in fl ux is ΔΦ = Φ − Φ0 and the change in time is Δt = t − t0.
Solution (a) Since 𝜙 = 𝜙0, the induced emf is
ℰ = −N ( Φ − Φ 0
t − t0 ) = −N ( BA cos ϕ − B0 A cos ϕ
t − t0 ) = −NA cos ϕ (
B − B0 t − t0 )
ℰ = −(20)(1.5 × 10−3 m2)(cos 0°) (0.060 T − 0.050 T0.10 s − 0 s ) = −3.0 × 10−3 V
(b) The calculation here is similar to that in part (a), except the initial and fi nal values of B are interchanged. This interchange reverses the sign of the emf, so ℰ = +3.0 × 10−3 V . Because the algebraic sign or polarity
of the emf is reversed, the direction of the induced current would be
opposite to that in part (a).
EXAMPLE 6 The Emf Induced in a Rotating Coil
A fl at coil of wire has an area of 0.020 m2 and consists of 50 turns. At t0 = 0 s the coil is oriented so the normal to its surface has the same direction
(𝜙0 = 0°) as a constant magnetic fi eld of magnitude 0.18 T. The coil is
then rotated through an angle of 𝜙 = 30.0° in a time of 0.10 s (see Figure 22.11). (a) Determine the average induced emf. (b) What would be the induced emf if the coil were returned to its initial orientation in the same
time of 0.10 s?
Reasoning As in Example 5 we can determine the induced emf by using Faraday’s law of electromagnetic induction, along with the defi nition of
magnetic fl ux. In the present case, however, only 𝜙 (the angle between
the normal to the surface of the coil and the magnetic fi eld) changes in
time. All other factors remain constant.
Solution (a) Faraday’s law yields
ℰ = −N( Φ − Φ0
t − t0 ) = −N( BA cos ϕ − BA cos ϕ0
t − t0 ) = −NBA(
cos ϕ − cos ϕ0 t − t0 )
ℰ = −(50)(0.18 T)(0.020 m2 )(cos 30.0° − cos 0°0.10 s − 0 s ) = +0.24 V (b) When the coil is rotated back to its initial orientation in a time of 0.10 s, the initial and fi nal values of 𝜙 are interchanged. As a result, the induced
emf has the same magnitude but opposite polarity, so ℰ = −0.24 V .
The next example demonstrates that an emf can be created when a coil is rotated in a
magnetic fi eld.
636 CHAPTER 22 Electromagnetic Induction
THE PHYSICS OF . . . a ground fault interrupter. One application of Faraday’s law that is found in the home is a safety device called a ground fault interrupter. This device protects
against electrical shock from an appliance, such as a clothes dryer. It plugs directly into a wall
socket, as in Figure 22.13 or, in new home construction, replaces the socket entirely. The inter- rupter consists of a circuit breaker that can be triggered to stop the current to the dryer, depend-
ing on whether an induced voltage appears across a sensing coil. This coil is wrapped around an
iron ring, through which the current-carrying wires pass. In the drawing, the current going to the
dryer is shown in red, and the returning current is shown in green. Each of the currents creates
a magnetic fi eld that encircles the corresponding wire, according to RHR-2 (see Section 21.7).
However, the fi eld lines have opposite directions since the currents have opposite directions. As
the drawing shows, the iron ring guides the fi eld lines through the sensing coil. Since the current
is ac, the fi elds from the red and green current are changing, but the red and green fi eld lines
always have opposite directions and the opposing fi elds cancel at all times. As a result, the net
fl ux through the coil remains zero, and no induced emf appears in the coil. Thus, when the dryer
operates normally, the circuit breaker is not triggered and does not shut down the current. The
picture changes if the dryer malfunctions, as when a wire inside the unit breaks and accidentally
contacts the metal case. When someone touches the case, some of the current begins to pass
through the person’s body and into the ground, returning to the ac generator without using the return wire that passes through the ground fault interrupter. Under this condition, the net mag- netic fi eld through the sensing coil is no longer zero and changes with time, since the current is
ac. The changing fl ux causes an induced voltage to appear in the sensing coil, which triggers the
circuit breaker to stop the current. Ground fault interrupters work very fast (in less than a mil-
lisecond) and turn off the current before it reaches a dangerous level.
Conceptual Example 7 discusses another application of electromagnetic induction—namely,
how a stove can cook food without getting hot.
Ac generator
Iron ring
Ground fault interrupter
Heater element
Magnetic field lines
Sensing coil
Circuit breaker
FIGURE 22.13 The clothes dryer is connected to the wall socket through a ground
fault interrupter. The dryer is operating
normally.
CONCEPTUAL EXAMPLE 7 The Physics of an Induction Stove
Figure 22.14 shows two pots of water that were placed on an induction stove at the same time. There are two interesting features in this draw-
ing. First, the stove itself is cool to the touch. Second, the water in the
ferromagnetic metal pot is boiling while the water in the glass pot is not.
How can such a “cool” stove boil water, and why isn’t the water in the
glass pot boiling?
Reasoning and Solution The key to this puzzle is related to the fact that one pot is made from a ferromagnetic metal and one from glass. We
know that metals are good conductors, while glass is an insulator. Per-
haps the stove causes electricity to fl ow directly in the metal pot. This
Glass pot
Ferromagnetic metal pot
FIGURE 22.14 The water in the ferromagnetic metal pot is
boiling—yet the water in the
glass pot is not boiling, and
the stove top is cool to the
touch. The stove operates in
this way by using electromag-
netic induction.
22.5 Lenz’s Law 637
Check Your Understanding
(The answers are given at the end of the book.) 7. In the most common form of lightning, electric charges fl ow between the ground and a cloud. The fl ow
changes dramatically over short periods of time. Even without directly striking an electrical appliance
in your house, a bolt of lightning that strikes nearby can produce a current in the circuits of the appli-
ance. Note that such circuits typically contain coils or loops of wire. Why can the lightning cause the
current to appear?
8. A solenoid is connected to an ac source. A copper ring and a rubber ring are placed inside the solenoid, with the normal to the plane of each ring parallel to the axis of the solenoid. An induced emf appears
_________. (a) in the copper ring but not in the rubber ring (b) in the rubber ring but not in the copper ring (c) in both rings
9. A magnetic fi eld of magnitude B = 0.20 T is reduced to zero in a time interval of Δt = 0.10 s, thereby creating an induced current in a loop of wire. Which one or more of the following choices would cause
the same induced current to appear in the same loop of wire? (a) B = 0.40 T and Δt = 0.20 s (b) B = 0.30 T and Δt = 0.10 s (c) B = 0.30 T and Δt = 0.30 s (d) B = 0.10 T and Δt = 0.050 s (e) B = 0.50 T and Δt = 0.40 s
10. A coil is placed in a magnetic fi eld, and the normal to the plane of the coil remains parallel to the fi eld. Which one of the following options causes the magnitude of the average emf induced in the coil to be
as large as possible? (a) The magnitude of the fi eld is small, and its rate of change is large. (b) The magnitude of the fi eld is large, and its rate of change is small. (c) The magnitude of the fi eld is large, and it does not change.
22.5 Lenz’s Law An induced emf drives current around a circuit just as the emf of a battery does. With a battery,
conventional current is directed out of the positive terminal, through the attached device, and
into the negative terminal. The same is true for an induced emf, although the locations of the
positive and negative terminals are generally not as obvious. Therefore, a method is needed for
determining the polarity or algebraic sign of the induced emf, so the terminals can be identifi ed.
As we discuss this method, it will be helpful to keep in mind that the net magnetic fi eld penetrat-
ing a coil of wire results from two contributions. One is the original magnetic fi eld that produces
the changing fl ux that leads to the induced emf. The other arises because of the induced current,
which, like any current, creates its own magnetic fi eld. The fi eld created by the induced current
is called the induced magnetic fi eld. To determine the polarity of the induced emf, we will use a method based on a discov-
ery made by the Russian physicist Heinrich Lenz (1804–1865). This discovery is known as
Lenz’s law.
LENZ’S LAW The induced emf resulting from a changing magnetic fl ux has a polarity that leads to an induced current whose direction is such that the induced magnetic fi eld opposes the original fl ux change.
is exactly what happens. The stove is called an induction stove because it operates by using electromagnetic induction. Just beneath the cook-
ing surface is a metal coil that carries an ac current (frequency about
25 kHz). This current produces an alternating magnetic fi eld that extends
outward to the location of the metal pot. As the changing fi eld crosses the
pot’s bottom surface, an emf is induced in it. Because the pot is metal-
lic, an induced current is generated by the induced emf. The metal has a
fi nite resistance to the induced current, however, and heats up as energy
is dissipated in this resistance. The fact that the metal is ferromagnetic
is important. Ferromagnetic materials contain magnetic domains (see
Section 21.9), and the boundaries between them move extremely rapidly
in response to the external magnetic fi eld, thus enhancing the induction
eff ect. A normal aluminum cooking pot, in contrast, is not ferromagnetic,
so this enhancement is absent and such cookware is not used with induc-
tion stoves. An emf is also induced in the glass pot and the cooking sur-
face of the stove. However, these materials are insulators, so very little
induced current exists within them. Thus, they do not heat up very much
and remain cool to the touch.
638 CHAPTER 22 Electromagnetic Induction
Lenz’s law is best illustrated with examples. Each will be worked out according to the
following reasoning strategy:
REASONING STRATEGY Determining the Polarity of the Induced Emf 1. Determine whether the magnetic fl ux that penetrates a coil is increasing or decreasing. 2. Find what the direction of the induced magnetic fi eld must be so that it can oppose the
change in fl ux by adding to or subtracting from the original fi eld. 3. Having found the direction of the induced magnetic fi eld, use RHR-2 (see Section 21.7) to
determine the direction of the induced current. Then the polarity of the induced emf can be assigned because conventional current is directed out of the positive terminal, through the external circuit, and into the negative terminal.
CONCEPTUAL EXAMPLE 8 The Emf Produced by a Moving Magnet
Figure 22.15a shows a permanent magnet approaching a loop of wire. The external circuit attached to the loop consists of the resistance R, which could represent the fi lament in a light bulb, for instance. In Figure 22.15a, what is the polarity of the induced emf? In other words, (a) is point A posi- tive and point B negative or (b) is point A negative and point B positive?
Reasoning We will apply Lenz’s law, the essence of which is that the change in magnetic fl ux must be opposed by the induced magnetic fi eld.
The fl ux through the loop is increasing, since the magnitude of the mag-
netic fi eld at the loop is increasing as the magnet approaches. To oppose
the increase in the fl ux, the direction of the induced magnetic fi eld must
be opposite to the fi eld of the bar magnet. Thus, since the fi eld of the bar
magnet passes through the loop from left to right in part a of the drawing, the induced fi eld must pass through the loop from right to left. An induced
current creates this induced fi eld, and from the direction of this current we
will be able to decide the polarity of the induced emf.
Answer (b) is incorrect. If point A were negative and point B were positive, as in Figure 22.15b, the induced current in the loop would be as shown in that part of the drawing, because conventional current exits
from the positive terminal and returns through the external circuit (the
resistance R) to the negative terminal. Application of RHR-2 reveals that this induced current would lead to an induced fi eld that passes through
the loop from left to right, not right to left as needed to oppose the fl ux
change.
Answer (a) is correct. Figure 22.15c shows the situation with point A positive and point B negative and the induced current that results. An application of RHR-2 reveals that the induced fi eld produced by this
current indeed passes through the loop from right to left, as needed.
We conclude, therefore, that the polarity shown in Figure 22.15c is correct.
(a)
Magnetic field lines
A B
R
S N R.H.
(b)
A B
–
Induced current
Induced magnetic
field lines
+
(c)
R.H. A
B
+
Induced current
Induced magnetic
field lines
–
FIGURE 22.15 (a) As the magnet moves to the right, the magnetic fl ux through the loop increases. The external circuit attached to the loop has a resistance R. (b) One possibility and (c) another possibility for the direction of the induced current. See Conceptual Example 8.
In Conceptual Example 8 the direction of the induced magnetic fi eld is opposite to the direc-
tion of the external fi eld of the bar magnet.
Problem-Solving Insight The induced fi eld is not always opposite to the external fi eld, however, because Lenz’s law requires only that it must oppose the change in the fl ux that
generates the emf.
Conceptual Example 9 illustrates this point.
22.5 Lenz’s Law 639
Lenz’s law should not be thought of as an independent law, because it is a consequence of
the law of conservation of energy. The connection between energy conservation and induced
emf has already been discussed in Section 22.2 for the specifi c case of motional emf. However,
the connection is valid for any type of induced emf. In fact, the polarity of the induced emf, as
specifi ed by Lenz’s law, ensures that energy is conserved.
Check Your Understanding
(The answers are given at the end of the book.) 11. In Figure 22.3 a coil of wire is being stretched. What would be the direction of the induced current
if the direction of the external magnetic fi eld in the fi gure were reversed? (a) Clockwise (b) Counter- clockwise
12. A circular loop of wire is lying fl at on a horizontal table, and you are looking down at it. An external magnetic fi eld has a constant direction that is perpendicular to the table, and there is an induced clock-
wise current in the loop. Is the external fi eld directed upward toward you or downward away from you,
and is its magnitude increasing or decreasing? Note that there are two possible answers.
CONCEPTUAL EXAMPLE 9 The Emf Produced by a Moving Copper Ring
In Figure 22.16 there is a constant magnetic fi eld in a rectangular region of space. This fi eld is directed perpendicularly into the page. Outside this
region there is no magnetic fi eld. A copper ring slides through the region,
from position 1 to position 5. Since the fi eld is zero outside the rectan-
gular region, no fl ux passes through the ring in positions 1 and 5, there
is no change in the fl ux through the ring, and there is no induced emf or
current in the ring. Which one of the following options correctly describes
the induced current in the ring as it passes through positions 2, 3, and 4?
(a) I2 is clockwise, I3 is counterclockwise, I4 is counterclockwise. (b) I2 is counterclockwise, I3 is clockwise, I4 is clockwise. (c) I2 is clockwise, I3 = 0 A, I4 is counterclockwise. (d) I2 is counterclockwise, I3 = 0 A, I4 is clockwise.
Reasoning Lenz’s law will guide us. It requires that the induced mag- netic fi eld oppose the change in fl ux. Sometimes this means that the
induced fi eld is opposite to the external magnetic fi eld, as in Example 8.
However, we will see that the induced fi eld sometimes has the same
direction as the external fi eld in order to oppose the fl ux change.
Answers (a) and (b) are incorrect. Both of these answers specify that there is an induced current I3 in the ring as it passes through position 3, contrary to fact. The external fi eld within the rectangular region certainly
produces a fl ux through the ring. (See Figure 22.16.) However, the exter- nal fi eld is constant, so the fl ux through the ring does not change as the
ring moves. In order for an induced emf to exist and to cause an induced
current, the fl ux must change.
Answer (c) is incorrect. As the ring moves out of the fi eld region in position 4, the fl ux through the ring decreases, so there is an induced
emf and an induced current. Lenz’s law requires that the induced current
must lead to an induced magnetic fi eld that opposes this fl ux decrease. To
oppose the decrease, the induced fi eld must point in the same direction as
the external fi eld. To create an induced fi eld pointing into the page, the
induced current I4 must be clockwise (use RHR-2), not counterclockwise as this answer specifi es.
Answer (d) is correct. In position 2 the fl ux increases and, accord- ing to Lenz’s law, the induced current must create an induced magnetic
fi eld that opposes the increase. To oppose the increase the induced
fi eld must point opposite to the external fi eld and, therefore, must point
out of the page. RHR-2 indicates that the induced current must be
counterclockwise, as this answer states. In position 4 the fl ux through
the ring decreases, and the induced magnetic fi eld must oppose the
decrease by pointing in the same direction as the external fi eld—
namely, into the page. RHR-2 reveals that the induced current must be
clockwise, as this answer indicates. In position 3 the fl ux through the
loop is not changing, so there is no induced emf and current, as this
answer specifi es.
Related Homework: Problem 73
Position 1
Position 2
Position 3
Position 4
Position 5
FIGURE 22.16 A constant magnetic fi eld is directed
into the page in the shaded
rectangular region. Conceptual
Example 9 discusses what
happens to the induced emf and
current in a copper ring that
slides through the region from
position 1 to position 5.
(Continued)
640 CHAPTER 22 Electromagnetic Induction
13. When the switch in CYU Figure 22.2 is closed, the current in the coil increases to its equilibrium value. While the cur-
rent is increasing there is an induced current in the metal
ring. The ring is free to move. What happens to the ring?
(a) It does not move. (b) It jumps downward. (c) It jumps upward.
14. A conducting rod is free to slide along a pair of conduct- ing rails, in a region where a uniform and constant (in time)
magnetic fi eld is directed into the plane of the paper, as
CYU Figure 22.3 illustrates. Initially the rod is at rest. There is no friction between the rails and the rod. What
happens to the rod after the switch is closed? If any in-
duced emf develops, be sure to account for its eff ect.
(a) The rod accelerates to the right, its velocity increas- ing without limit. (b) The rod does not move. (c) The rod accelerates to the right for a while and then slows
down and comes to a halt. (d) The rod accelerates to the right and eventually reaches a constant velocity at which
it continues to move.
22.6 *Applications of Electromagnetic Induction to the Reproduction of Sound THE PHYSICS OF . . . the electric guitar pickup. Electromagnetic induction plays an important role in the technology used for the reproduction of sound. Virtually all electric gui-
tars, for example, use electromagnetic pickups in which an induced emf is generated in a coil of
wire by a vibrating string. Each pickup is located below the strings, as Figure 22.17 illustrates, and each is sensitive to diff erent harmonics that the strings produce. Each string is made from a
magnetizable metal, and the pickup consists of a coil of wire within which a permanent magnet is
located. The magnetic fi eld of the magnet penetrates the guitar string, causing it to become mag-
netized with north and south poles. When the magnetized string is plucked, it oscillates, thereby
changing the magnetic fl ux that passes through the coil. The changing fl ux induces an emf in
the coil, and the polarity of this emf alternates with the vibratory motion of the string. A string
vibrating at 440 Hz, for example, induces a 440-Hz ac emf in the coil. This signal, after being
amplifi ed, is sent to loudspeakers, which produce a 440-Hz sound wave (concert A).
THE PHYSICS OF . . . a tape-deck playback head. The playback head of a tape deck uses a moving tape to generate an emf in a coil of wire. Figure 22.18 shows a section of mag- netized tape in which a series of “tape magnets” have been created in the magnetic layer of the
tape during the recording process (see Section 21.9). The tape moves beneath the playback head,
which consists of a coil of wire wrapped around an iron core. The iron core has the approximate
shape of a horseshoe with a small gap between the two ends. Some of the fi eld lines of the tape
magnet under the gap are routed through the highly magnetizable iron core, and hence through
Iron core
Coil
Metal ring
Switch
Battery
+ –
CYU FIGURE 22.2
+ –
B (into paper)
Switch
Conducting rail
Rod
CYU FIGURE 22.3
Pickups N
N
S
Coil To amplifier
Side view
Permanent magnet
Guitar string (magnetizable)
S S N
FIGURE 22.17 When the string of an electric guitar vibrates, an emf is induced in the coil of the pickup. The two ends of the coil are connected to the input of an amplifi er.
22.7 The Electric Generator 641
the coil, as they proceed from the north pole to the south pole. Consequently, the fl ux through
the coil changes as the tape moves past the gap. The change in fl ux leads to an ac emf, which is
amplifi ed and sent to the speakers, which reproduce the original sound.
THE PHYSICS OF . . . microphones. There are a number of types of microphones, and Figure 22.19 illustrates the one known as a moving-coil microphone. When a sound wave strikes the diaphragm of the microphone, the diaphragm vibrates back and forth, and the attached
coil moves along with it. Nearby is a stationary magnet. As the coil alternately approaches and
recedes from the magnet, the fl ux through the coil changes. Consequently, an ac emf is induced in
the coil. This electrical signal is sent to an amplifi er and then to the speakers. In a moving-magnet
microphone, the magnet is attached to the diaphragm and moves relative to a stationary coil.
Check Your Understanding
(The answer is given at the end of the book.) 15. The string of an electric guitar vibrates in a standing wave pattern that consists of nodes and antinodes.
(Section 17.5 discusses standing waves.) Where should an electromagnetic pickup be located in the
standing wave pattern to produce a maximum emf? (a) At a node (b) At an antinode
22.7 The Electric Generator
How a Generator Produces an Emf Electric generators, such as those in Figure 22.20, produce virtually all of the world’s electrical energy. A generator produces electrical energy from mechanical work, which is just the opposite
of what a motor does. In a motor, an input electric current causes a coil to rotate, thereby doing mechanical work on any object attached to the shaft of the motor. In a generator, the shaft is
rotated by some mechanical means, such as an engine or a turbine, and an emf is induced in a
coil. If the generator is connected to an external circuit, an electric current is the output of the generator.
THE PHYSICS OF . . . an electric generator. In its simplest form, an ac generator con- sists of a coil of wire that is rotated in a uniform magnetic fi eld, as Figure 22.21a indicates. Although not shown in the picture, the wire is usually wound around an iron core. As in an
electric motor, the coil/core combination is called the armature. Each end of the wire forming the coil is connected to the external circuit by means of a metal ring that rotates with the coil.
NSound
Diaphragm
To amplifier To amplifier
Stationary bar magnet
Coil moves with diaphragm
FIGURE 22.19 A moving-coil microphone.
Coil
Gap
Tape magnet
S N
S N
S N
Iron core
To amplifier
Tape motion
Magnetic field line(s)
FIGURE 22.18 The playback head of a tape deck. As each tape magnet goes by the gap,
some magnetic fi eld lines pass through the
core and coil. The changing fl ux in the coil
creates an induced emf. The gap width has
been exaggerated.
FIGURE 22.20 Electric generators such as these supply electric power by producing an
induced emf according to Faraday’s law of
electromagnetic induction.
David Weintraub/Science Source
642 CHAPTER 22 Electromagnetic Induction
Each ring slides against a stationary carbon brush, to which the external circuit (the lamp in the
drawing) is connected.
To see how current is produced by the generator, consider the two vertical sides of the coil
in Figure 22.21b. Since each is moving in a magnetic fi eld B→, the magnetic force exerted on the charges in the wire causes them to fl ow, thus creating a current. With the aid of RHR-1 (fi ngers
of extended right hand point along B→, thumb along the velocity v→, palm pushes in the direction of the force on a positive charge), it can be seen that the direction of the current is from bottom
to top in the left side and from top to bottom in the right side. Thus, charge fl ows around the
loop. The upper and lower segments of the loop are also moving. However, these segments can
be ignored because the magnetic force on the charges within them points toward the sides of the
wire and not along the length.
The magnitude of the motional emf developed in a conductor moving through a magnetic
fi eld is given by Equation 22.1. To apply this expression to the left side of the coil, whose length
is L (see Figure 22.21c), we need to use the velocity component υ⊥ that is perpendicular to B →
.
Letting 𝜃 be the angle between v→ and B→ (see Figure 22.21b), it follows that υ⊥ = υ sin θ, and, with the aid of Equation 22.1, the emf can be written as
ℰ = BLυ⊥ = BLυ sin θ
The emf induced in the right side has the same magnitude as that in the left side. Since the emfs
from both sides drive current in the same direction around the loop, the emf for the complete
loop is ℰ = 2BL𝜐 sin 𝜃. If the coil consists of N loops, the net emf is N times as great as that of one loop, so
ℰ = N(2BLυ sin θ)
It is convenient to express the variables 𝜐 and 𝜃 in terms of the angular speed 𝜔 at which the coil rotates. Equation 8.2 shows that the angle 𝜃 is the product of the angular speed and the time,
𝜃 = 𝜔t, if it is assumed that 𝜃 = 0 rad when t = 0 s. Furthermore, any point on each vertical side moves on a circular path of radius r = W/2, where W is the width of the coil (see Figure 22.21c). Thus, the tangential speed 𝜐 of each side is related to the angular speed 𝜔 via Equation 8.9 as
𝜐 = r𝜔 = (W/2)𝜔. Substituting these expressions for 𝜃 and 𝜐 in the previous equation for ℰ, and recognizing that the product LW is the area A of the coil, we can write the induced emf as
Emf induced in a rotating ℰ = NABω sin ωt = ℰ0 sin ωt where ω = 2πf (22.4) planar coil
Carbon brush
Carbon brush
N S
Coil rotated by mechanical means
I I
I
I
I
I
B
B
v
Metal rings
L
W
(a) (b) (c)
θFIGURE 22.21 (a) This electric generator consists of a coil (only one loop is shown) of
wire that is rotated in a magnetic fi eld B→ by some mechanical means. (b) The current I arises because of the magnetic force exerted
on the charges in the moving wire. (c) The dimensions of the coil.
Scott Shaw/The Plain Dealer/Barcroft Media
This personal energy generator (PEG) is a
small device that can fi t into a backpack. It
uses Faraday’s law of electromagnetic induc-
tion to convert some of the kinetic energy
of your normal movements into electric
energy, which keeps a battery in the device
fully charged. The PEG serves as a back-up
power source for your mobile phone or other
handheld electronic equipment.
22.7 The Electric Generator 643
In this result, the angular speed 𝜔 is in radians per second and is related to the frequency f [in cycles per second or hertz (Hz)] according to 𝜔 = 2𝜋f (Equation 10.6).
Although Equation 22.4 was derived for a rectangular coil, the result is valid for any planar
shape of area A (e.g., circular) and shows that the emf varies sinusoidally with time. The peak, or maximum, emf ℰ0 occurs when sin 𝜔t = 1 and has the value ℰ0 = NAB𝜔. Figure 22.22 shows a plot of Equation 22.4 and reveals that the emf changes polarity as the coil rotates. This changing
polarity is exactly the same as that discussed for an ac voltage in Section 20.5 and illustrated in
Figure 20.10. If the external circuit connected to the generator is a closed circuit, an alternat- ing current results that changes direction at the same frequency f as the emf changes polarity. Therefore, this electric generator is also called an alternating current (ac) generator. The next two examples show how Equation 22.4 is applied.
Emf,
Time, t 0
+
–
ℰ
ℰ0
FIGURE 22.22 An ac generator produces this alternating emf ℰ according to ℰ =
ℰ0 sin 𝜔t.
EXAMPLE 10 An Ac Generator
In Figure 22.21 the coil of the ac generator rotates at a frequency of f = 60.0 Hz and develops an emf of 120 V (rms; see Section 20.5). The coil
has an area of A = 3.0 × 10−3 m2 and consists of N = 500 turns. Find the magnitude of the magnetic fi eld in which the coil rotates.
Reasoning The magnetic fi eld can be found from the relation ℰ0 = NAB𝜔. However, in using this equation we must remember that ℰ0 is the peak emf, whereas the given value of 120 V is not a peak value but an rms
value. The peak emf is related to the rms emf by ℰ0 = √2ℰrms, according
to Equation 20.13.
Problem-Solving Insight In the equation ℰ0 = NAB𝟂, remember that the angular frequency 𝟂 must be in rad/s and is related to the frequency f (in Hz) according to 𝟂 = 2𝞹f (Equation 10.6).
Solution Solving ℰ0 = NAB𝜔 for B and using the facts that ℰ0 = √2ℰrms (Equation 20.13) and 𝜔 = 2𝜋f (Equation 10.6), we fi nd that the magnitude of the magnetic fi eld is
B = ℰ0
NAω =
√2ℰrms
NA2π f =
√2 (120 V)
(500)(3.0 × 10−3 m2 )2π (60.0 Hz) = 0.30 T
Analyzing Multiple-Concept Problems
EXAMPLE 11 The Physics of a Bike Generator
A bicyclist is traveling at night, and a generator mounted on the bike pow-
ers a headlight. A small rubber wheel on the shaft of the generator presses
against the bike tire and turns the coil of the generator at an angular speed
that is 44 times as great as the angular speed of the tire itself. The tire
has a radius of 0.33 m. The coil consists of 75 turns, has an area of 2.6 ×
10−3 m2, and rotates in a 0.10-T magnetic fi eld. When the peak emf being
generated is 6.0 V, what is the linear speed of the bike?
Reasoning Since the tires are rolling, the linear speed 𝜐 of the bike is related to the angular speed 𝜔tire of its tires by 𝜐 = r𝜔tire (see Section 8.6),
where r is the radius of a tire. We are given that the angular speed 𝜔coil of the coil is 44 times as great as that of the tire. Thus, ω tire =
1
44 ωcoil and the linear speed of the bike can be related to the angular speed of
the coil. Furthermore, according to the discussion in this section on
electric generators, the angular speed of the coil is related (see Equa-
tion 22.4) to the peak emf developed by the rotating coil, the number
of turns in the coil, the area of the coil, and the magnetic fi eld, all of
which are known.
Knowns and Unknowns The data for this problem are:
Description Symbol Value Comment Radius of tire r 0.33 m
Number of turns in coil N 75
Angular speed of coil 𝜔coil 44𝜔tire Angular speed of coil is 44 times as great as that of tire.
Area of coil A 2.6 × 10−3 m2
Magnitude of magnetic field B 0.10 T
Peak emf produced by generator ℰ0 6.0 V
Unknown Variable Linear speed of bike 𝜐 ?
644 CHAPTER 22 Electromagnetic Induction
The Electrical Energy Delivered by a Generator and the Countertorque Some power-generating stations burn fossil fuel (coal, gas, or oil) to heat water and produce pres-
surized steam for turning the blades of a turbine whose shaft is linked to the generator. Others use
nuclear fuel or falling water as a source of energy. As the turbine rotates, the generator coil also
rotates and mechanical work is transformed into electrical energy.
The devices to which the generator supplies electricity are known collectively as the “load,”
because they place a burden or load on the generator by taking electrical energy from it. If all the
devices are switched off , the generator runs under a no-load condition, because there is no current
in the external circuit and the generator does not supply electrical energy. Then, work needs to be
done on the turbine only to overcome friction and other mechanical losses within the generator
itself, and fuel consumption is at a minimum.
Figure 22.23 illustrates a situation in which a load is connected to a generator. Because there is now a current I = I1 + I2 in the coil of the generator and the coil is situated in a magnetic fi eld, the current experiences a magnetic force F→. Figure 22.24 shows the magnetic force acting on the left side of the coil, with the direction of F→ given by RHR-1. A force of equal magnitude but opposite direction also acts on the right side of the coil, although this force is not shown in the drawing. The
magnetic force F→ gives rise to a countertorque that opposes the rotational motion. The greater the current drawn from the generator, the greater the countertorque, and the harder it is for the turbine
to turn the coil. To compensate for this countertorque and keep the coil rotating at a constant
Modeling the Problem
STEP 1 Rolling Motion When a tire rolls without slipping on the ground, the linear speed 𝜐 of the tire (the speed at which its axle is moving forward) is related to the angular speed 𝜔tire of
the tire about the axle. This relationship is given by
υ = rωtire (8.12)
where r is the radius of the tire. We are given that the angular speed 𝜔coil of the coil is 44 times as great as the angular speed of the tire, so 𝜔coil = 44𝜔tire. Solving this equation for 𝜔tire and substitut-
ing the result into 𝜐 = r𝜔tire, we obtain Equation 1 at the right. The radius of the tire is known, but the angular speed of the coil is not; we will evaluate it in Step 2.
STEP 2 Peak Emf Induced in a Rotating Planar Coil A generator produces an emf when a coil of wire rotates in a magnetic fi eld. According to Equation 22.4, the peak emf ℰ0 is given
by ℰ0 = NAB𝜔coil, where N is the number of turns in the coil, A is the area of the coil, B is the magnitude of the magnetic fi eld, and 𝜔coil is the angular speed of the rotating coil. Solving this
relation for 𝜔coil gives
ωcoil = ℰ0
NAB
Note from the data table that all the variables on the right side of this equation are known. We
substitute this result into Equation 1, as indicated at the right.
Solution Algebraically combining the results of the two steps, we have
υ = r( 144)ωcoil = r ( 1
44)( ℰNAB) The linear speed of the bicycle is
υ = r( 144)( ℰ0
NAB) = (0.33 m)( 144)[ 6.0 V
(75)(2.6 × 10−3 m2 )(0.10 T) ] = 2.3 m/s Related Homework: Problem 47
STEP 1 STEP 2
υ = r( 144)ωcoil (1)
?
υ = r( 144)ωcoil (1)
ωcoil = ℰ0
NAB
Turbine Electric
generator
Load
I1
I1
I2
I2
FIGURE 22.23 The generator supplies a total current of I = I1 + I2 to the load.
22.7 The Electric Generator 645
angular speed, work must be done by the turbine, which means that more fuel must be burned.
This is another example of the law of conservation of energy, since the electrical energy consumed
by the load must ultimately come from the energy source used to drive the turbine.
The Back Emf Generated by an Electric Motor A generator converts mechanical work into electrical energy; in contrast, an electric motor con-
verts electrical energy into mechanical work. Both devices are similar and consist of a coil of
wire that rotates in a magnetic fi eld. In fact, as the armature of a motor rotates, the magnetic fl ux
passing through the coil changes and an emf is induced in the coil. Thus, when a motor is operat-
ing, two sources of emf are present: (1) the applied emf V that provides current to drive the motor (e.g., from a 120-V outlet), and (2) the emf ℰ induced by the generator-like action of the rotating
coil. The circuit diagram in Figure 22.25 shows these two emfs. Consistent with Lenz’s law, the induced emf ℰ acts to oppose the applied emf V and is called
the back emf or the counter emf of the motor. The greater the speed of the motor, the greater is the fl ux change through the coil, and the greater is the back emf. Because V and ℰ have opposite polarities, the net emf in the circuit is V − ℰ. In Figure 22.25, R is the resistance of the wire in the coil, and the current I drawn by the motor is determined from Ohm’s law as the net emf divided by the resistance:
I = V − ℰ
R (22.5)
The next example uses this result to illustrate that the current in a motor depends on both the
applied emf V and the back emf ℰ.
(a)
(b)
Shaft
I
I
B
F
Shaft
Top view of coil
Current I (out of paper)
B
FIGURE 22.24 (a) A current I exists in the rotating coil of a generator. (b) A top view of the coil, showing the magnetic force F→ exerted on the left side of the coil.
I
V +
– I
I
R
Ac motor
V +
– I
ℰ +
–
Ac motor
FIGURE 22.25 The applied emf V supplies the current I to drive the motor. The circuit on the right shows V along with the electrical equivalent of the motor, including the resistance R of its coil and the back emf ℰ.
EXAMPLE 12 The Physics of Operating a Motor
The coil of an ac motor has a resistance of R = 4.1 Ω. The motor is plugged into an outlet where V = 120.0 volts (rms), and the coil develops a back emf of ℰ = 118.0 volts (rms) when rotating at normal constant speed. The
motor is turning a wheel. Find (a) the current when the motor fi rst starts up and (b) the current when the motor is operating at normal speed.
Reasoning Once normal operating speed is attained, the motor need only work to compensate for frictional losses. But in bringing the wheel
up to speed from rest, the motor must also do work to increase the wheel’s
rotational kinetic energy. Thus, bringing the wheel up to speed requires
more work, and hence more current, than maintaining the normal operat-
ing speed. We expect our answers to parts (a) and (b) to refl ect this fact.
Problem-Solving Insight The current in an electric motor depends on both the applied emf V and any back emf ℰ developed because the coil of the motor is rotating.
Solution (a) When the motor just starts up, the coil is not rotating, so there is no back emf induced in the coil and ℰ = 0 V. The start-up current
drawn by the motor is
I = V − ℰ
R =
120 V − 0 V
4.1 Ω = 29 A (22.5)
(b) At normal speed, the motor develops a back emf of ℰ = 118.0 volts, so the current is
I = V − ℰ
R =
120.0 V − 118.0 V
4.1 Ω = 0.49 A
646 CHAPTER 22 Electromagnetic Induction
Example 12 illustrates that when a motor is just starting, there is little back emf, and, consequently,
a relatively large current exists in the coil. As the motor speeds up, the back emf increases until
it reaches a maximum value when the motor is rotating at normal speed. The back emf becomes
almost equal to the applied emf, and the current is reduced to a relatively small value, which is
suffi cient to provide the torque on the coil needed to overcome frictional and other losses in the
motor and to drive the load (e.g., a fan).
Check Your Understanding
(The answers are given at the end of the book.) 16. In a car, the generator-like action of the alternator occurs while the engine is running and keeps the bat-
tery fully charged. The headlights would discharge an old and failing battery quickly if it were not for
the alternator. Why does the engine of a parked car run more quietly with the headlights off than with
them on when the battery is in bad shape?
17. You have a fi xed length of wire and need to design a generator that will produce the greatest peak emf for a given frequency and magnetic fi eld strength. You should use (a) a one-turn square coil, (b) a two- turn square coil, (c) either a one- or a two-turn square coil because both give the same peak emf for a given frequency and magnetic fi eld strength.
18. An electric motor in a hair dryer is running at its normal constant operating speed and, thus, is drawing a relatively small current, as in part (b) of Example 12. The wire in the coil of the motor has some re-
sistance. What happens to the temperature of the coil if the shaft of the motor is prevented from turning,
so that the back emf is suddenly reduced to zero? (a) Nothing. (b) The temperature decreases. (c) The temperature increases (the coil could even burn up).
22.8 Mutual Inductance and Self-Inductance
Mutual Inductance We have seen that an emf can be induced in a coil by keeping the coil stationary and moving a
magnet nearby, or by moving the coil near a stationary magnet. Figure 22.26 illustrates another important method of inducing an emf. Here, two coils of wire, the primary coil and the second- ary coil, are placed close to each other. The primary coil is the one connected to an ac generator, which sends an alternating current Ip through it. The secondary coil is not attached to a generator, although a voltmeter is connected across it to register any induced emf.
The current-carrying primary coil is an electromagnet and creates a magnetic fi eld in the
surrounding region. If the two coils are close to each other, a signifi cant fraction of this magnetic
fi eld penetrates the secondary coil and produces a magnetic fl ux. The fl ux is changing, since the
current in the primary coil and its associated magnetic fi eld are changing. Because of the change
in fl ux, an emf is induced in the secondary coil.
The eff ect in which a changing current in one circuit induces an emf in another circuit is
called mutual induction. According to Faraday’s law of electromagnetic induction, the average emf ℰs induced in the secondary coil is proportional to the change in fl ux ΔΦs passing through
it. However, ΔΦs is produced by the change in current ΔIp in the primary coil. Therefore, it is convenient to recast Faraday’s law into a form that relates ℰs to ΔIp. To see how this recasting is accomplished, note that the net magnetic fl ux passing through the secondary coil is NsΦs, where Ns is the number of loops in the secondary coil and Φs is the fl ux through one loop (assumed to be the same for all loops). The net fl ux is proportional to the magnetic fi eld, which, in turn, is pro-
portional to the current Ip in the primary coil. Thus, we can write NsΦs ∝ Ip. This proportionality can be converted into an equation in the usual manner by introducing a proportionality constant
M, known as the mutual inductance:
NsΦs = MIp or M = NsΦs
Ip (22.6)
Voltmeter
+ Ac generator
Changing magnetic field lines produced by primary coil
Primary coil
–
Ip
Secondary coil
FIGURE 22.26 An alternating current Ip in the primary coil creates an alternating
magnetic fi eld. This changing fi eld induces
an emf in the secondary coil.
22.8 Mutual Inductance and Self-Inductance 647
Substituting this equation into Faraday’s law, we fi nd that
ℰs = −Ns ∆Φs
∆t = −
∆(NsΦs) ∆t
= − ∆(MIp)
∆t = −M
∆Ip ∆t
Emf due to mutual induction
ℰs = −M ∆Ip ∆t
(22.7)
Writing Faraday’s law in this manner makes it clear that the average emf ℰs induced in the
secondary coil is due to the change in the current ΔIp in the primary coil. Equation 22.7 shows that the measurement unit for the mutual inductance M is V · s/A,
which is called a henry (H) in honor of Joseph Henry: 1 V · s/A = 1 H. The mutual inductance depends on the geometry of the coils and the nature of any ferromagnetic core material that is
present. Although M can be calculated for some highly symmetrical arrangements, it is usually measured experimentally. In most situations, values of M are less than 1 H and are often on the order of millihenries (1 mH = 1 × 10−3 H) or microhenries (1 𝜇H = 1 × 10−6 H).
BIO THE PHYSICS OF . . . transcranial magnetic stimulation (TMS). A new tech- nique that shows promise for the treatment of psychiatric disorders such as depression is based
on mutual induction. This technique is called transcranial magnetic stimulation (TMS) and is a
type of indirect and gentler electric shock therapy. In traditional electric shock therapy, electric
current is delivered directly through the skull and penetrates the brain, disrupting its electrical
circuitry and in the process alleviating the symptoms of the psychiatric disorder. The treatment
is not gentle and requires an anesthetic, because relatively large electric currents must be used to
penetrate the skull. In contrast, TMS produces its electric current by using a time-varying mag-
netic fi eld. A primary coil is positioned over the part of the brain to be treated (see Figure 22.27), and a time-varying current is applied to this coil. The arrangement is analogous to that in
Figure 22.26, except that the brain and the electrically conductive pathways within it take the place of the secondary coil. The magnetic fi eld produced by the primary coil penetrates the brain
and, since the fi eld is changing in time, it induces an emf in the brain. This induced emf causes
an electric current to fl ow in the conductive brain tissue, with therapeutic results similar to those
of conventional electric shock treatment. The current delivered to the brain, however, is much
smaller than the current in the conventional treatment, so that patients receive TMS treatments
without anesthetic and without severe after-eff ects such as headaches and memory loss. TMS
remains in the experimental stage, however, and the optimal protocol for applying the technique
has not yet been determined.
Self-Inductance In all the examples of induced emfs presented so far, the magnetic fi eld has been produced by an
external source, such as a permanent magnet or an electromagnet. However, the magnetic fi eld
need not arise from an external source. An emf can be induced in a current-carrying coil by a
change in the magnetic fi eld that the current itself produces. For instance, Figure 22.28 shows a coil connected to an ac generator. The alternating current creates an alternating magnetic fi eld
that, in turn, creates a changing fl ux through the coil. The change in fl ux induces an emf in the
coil, in accord with Faraday’s law. The eff ect in which a changing current in a circuit induces an
emf in the same circuit is referred to as self-induction. When dealing with self-induction, as with mutual induction, it is customary to recast Fara-
day’s law into a form in which the induced emf is proportional to the change in current in the
coil rather than to the change in fl ux. If Φ is the magnetic fl ux that passes through one turn of the
coil, then NΦ is the net fl ux through a coil of N turns. Since Φ is proportional to the magnetic fi eld, and the magnetic fi eld is proportional to the current I, it follows that NΦ ∝ I. By inserting a constant L, called the self-inductance, or simply the inductance, of the coil, we can convert this proportionality into Equation 22.8:
N Φ = LI or L = N Φ
I (22.8)
FIGURE 22.27 In the technique of transcranial magnetic stimulation (TMS),
a time-varying electric current is applied
to a primary coil, which is positioned over
a region of the brain, as this photograph
illustrates. The time-varying magnetic fi eld
produced by the coil penetrates the brain
and creates an induced emf within it. This
induced emf leads to an induced current that
disrupts the electric circuits of the brain,
thereby relieving some of the symptoms of
psychiatric disorders such as depression.
Richard T. Nowitz/Science Source
+ Ac generator
Magnetic field lines
produced by I
–
I I
FIGURE 22.28 The alternating current in the coil generates an alternating magnetic
fi eld that induces an emf in the coil.
648 CHAPTER 22 Electromagnetic Induction
Faraday’s law of induction now gives the average induced emf as
ℰ = −N ∆Φ
∆ t = −
∆(N Φ) ∆t
= − ∆(LI )
∆ t = −L
∆ I ∆ t
Emf due to self-induction
ℰ = −L ∆ I ∆ t
(22.9)
Like mutual inductance, L is measured in henries. The magnitude of L depends on the geometry of the coil and on the core material. Wrapping the coil around a ferromagnetic (iron)
core substantially increases the magnetic fl ux—and therefore the inductance—relative to that
for an air core. Because of their self-inductance, coils are known as inductors and are widely used in electronics. Inductors come in all sizes, typically in the range between millihenries and
microhenries.
The Energy Stored in an Inductor An inductor, like a capacitor, can store energy. This stored energy arises because a genera-
tor does work to establish a current in an inductor. Suppose that an inductor is connected to
a generator whose terminal voltage can be varied continuously from zero to some fi nal value.
As the voltage is increased, the current I in the circuit rises continuously from zero to its fi nal value. While the current is rising, an induced emf ℰ = −L(ΔI/Δt) appears across the inductor. Conforming to Lenz’s law, the polarity of the induced emf ℰ is opposite to the polarity of the
generator voltage, so as to oppose the increase in the current. Thus, the generator must do work
to push the charges through the inductor against this induced emf. The increment of work ΔW done by the generator in moving a small amount of charge ΔQ through the inductor is ΔW = −(ΔQ)ℰ = −(ΔQ)[−L(ΔI/Δt)], according to Equation 19.4. Since ΔQ/Δt is the current I, the work done is
∆W = LI(∆ I )
In this expression ΔW represents the work done by the generator to increase the current in the inductor by an amount ΔI. To determine the total work W done while the current is changed from zero to its fi nal value, all the small increments ΔW must be added together. This summation is left as an exercise (see Problem 80). The result is W = 12 LI 2, where I represents the fi nal current in the inductor. This work is stored as energy in the inductor, so that
Energy stored in an inductor Energy =
1
2 L I 2 (22.10)
It is possible to regard the energy in an inductor as being stored in its magnetic fi eld. For the
special case of a long solenoid (see Problem 83), the self-inductance is L = 𝜇0n2Aℓ, where n is the number of turns per unit length, A is the cross-sectional area, and ℓ is the length of the solenoid. As a result, the energy stored in a long solenoid is
Energy = 1
2 LI 2 = 1
2 μ0 n2AℓI 2
Since B = 𝜇0nI at the interior of a long solenoid (Equation 21.7), this energy can be expressed as
Energy = 1
2μ 0 B 2Aℓ
The term Aℓ is the volume inside the solenoid where the magnetic fi eld exists, so the energy per unit volume, or energy density, is
Energy density = Energy
Volume =
1
2μ0 B2 (22.11)
Although this result was obtained for the special case of a long solenoid, it is quite general and is
valid for any point where a magnetic fi eld exists in air or vacuum or in a nonmagnetic material.
Thus, energy can be stored in a magnetic fi eld, just as it can in an electric fi eld.
22.9 Transformers 649
22.9 Transformers One of the most important applications of mutual induction and self-induction takes place in a
transformer. A transformer is a device that is used to increase or decrease an ac voltage. For instance, whenever a cordless device (e.g., a cell phone) is plugged into a wall receptacle to
recharge the batteries, a transformer plays a role in reducing the 120-V ac voltage to a much
smaller value. Typically, between 3 and 9 V are needed to energize batteries. In another example,
a picture tube in a television set needs about 15 000 V to accelerate the electron beam, and a
transformer is used to obtain this high voltage from the 120 V at a wall socket.
THE PHYSICS OF . . . transformers. Figure 22.29 shows a drawing of a transformer. The transformer consists of an iron core on which two coils are wound: a primary coil with Np turns and a secondary coil with Ns turns. The primary coil is the one connected to the ac generator. For the moment, suppose that the switch in the secondary circuit is open, so there is no current
in this circuit. The alternating current in the primary coil establishes a changing magnetic fi eld in
the iron core. Because iron is easily magnetized, it greatly enhances the magnetic fi eld relative to
that in an air core and guides the fi eld lines to the secondary coil. In a well-designed core, nearly
all the magnetic fl ux Φ that passes through each turn of the primary also goes through each turn
of the secondary. Since the magnetic fi eld is changing, the fl ux through the primary and second-
ary coils is also changing, and consequently an emf is induced in both coils. In the secondary coil
the induced emf ℰs arises from mutual induction and is given by Faraday’s law as
ℰs = −Ns ∆Φ
∆ t
In the primary coil the induced emf ℰp is due to self-induction and is specifi ed by Faraday’s
law as
ℰp = −Np ∆Φ
∆ t
The term ΔΦ/Δt is the same in both of these equations, since the same fl ux penetrates each turn of both coils. Dividing the two equations shows that
ℰs
ℰp =
Ns Np
In a high-quality transformer the resistances of the coils are negligible, so the magnitudes of the
emfs, ℰs and ℰp, are nearly equal to the terminal voltages, Vs and Vp, across the coils (see Section 20.9 for a discussion of terminal voltage). The relation ℰs/ℰp = Ns/Np is called the transformer equation and is usually written in terms of the terminal voltages:
Vs Vp
= Ns Np
(22.12)
According to the transformer equation, if Ns is greater than Np, the secondary (output) volt- age is greater than the primary (input) voltage. In this case we have a step-up transformer. On the
Transformer equation
+
– Ac generator
Primary coil (Np turns)
Iron core
Magnetic field lines Transformer symbol
Secondary coil (Ns turns)
Switch
Ip
FIGURE 22.29 A transformer consists of a primary coil and a secondary coil, both wound on an iron core. The changing magnetic fl ux produced by the current in the primary coil induces an emf in the secondary
coil. At the far right is the symbol for a transformer.
650 CHAPTER 22 Electromagnetic Induction
other hand, if Ns is less than Np, the secondary voltage is less than the primary voltage, and we have a step-down transformer. The ratio Ns/Np is referred to as the turns ratio of the transformer. A turns ratio of 8/1 (often written as 8 : 1) means, for example, that the secondary coil has eight
times more turns than the primary coil. Conversely, a turns ratio of 1:8 implies that the secondary
has one-eighth as many turns as the primary.
A transformer operates with ac electricity and not with dc. A steady direct current in the
primary coil produces a fl ux that does not change in time, and thus no emf is induced in the sec-
ondary coil. The ease with which transformers can change voltages from one value to another is
a principal reason why ac is preferred over dc.
With the switch in the secondary circuit of Figure 22.29 closed, a current Is exists in the circuit and electrical energy is fed to the TV tube. This energy comes from the ac generator con-
nected to the primary coil. Although the secondary voltage Vs may be larger or smaller than the primary voltage Vp, energy is not being created or destroyed by the transformer. Energy conser- vation requires that the energy delivered to the secondary coil must be the same as the energy
delivered to the primary coil, provided no energy is dissipated in heating these coils or is other-
wise lost. In a well-designed transformer, less than 1% of the input energy is lost in the form of
heat. Noting that power is energy per unit time, and assuming 100% energy transfer, the average
power Pp delivered to the primary coil is equal to the average power Ps delivered to the secondary coil: Pp = Ps. However, P = IV (Equation 20.15a), so IpVp = IsVs, or
I
s
Ip =
Vp Vs
= Np Ns
(22.13)
Observe that Vs/Vp is equal to the turns ratio Ns/Np, while Is/Ip is equal to the inverse turns ratio Np/Ns.
Problem-Solving Insight Consequently, a transformer that steps up the voltage simultaneously steps down the current, and a transformer that steps down the voltage steps up the current.
However, the power is neither stepped up nor stepped down, since Pp = Ps. Example 13 emphasizes this fact.
Power distribution stations use high-voltage
transformers similar to this one to step up or
step down voltages.
Charles Thatcher/Getty Images
EXAMPLE 13 A Step-Down Transformer
A step-down transformer inside a stereo receiver has 330 turns in the
primary coil and 25 turns in the secondary coil. The plug connects the
primary coil to a 120-V wall socket, and there is a current of 0.83 A in the
primary coil while the receiver is turned on. Connected to the secondary
coil are the transistor circuits of the receiver. Find (a) the voltage across the secondary coil, (b) the current in the secondary coil, and (c) the aver- age electric power delivered to the transistor circuits.
Reasoning The transformer equation, Equation 22.12, states that the secondary voltage Vs is equal to the product of the primary voltage Vp and the turns ratio Ns/Np. On the other hand, Equation 22.13 indicates that the secondary current Is is equal to the product of the primary current Ip and the inverse turns ratio Np/Ns. The average power delivered to the transistor circuits is the product of the secondary current and the secondary voltage.
Solution (a) The voltage across the secondary coil can be found from the transformer equation:
Vs = Vp Ns Np
= (120 V) ( 25330) = 9.1 V (22.12)
(b) The current in the secondary coil is
Is = Ip Np Ns
= (0.83 A) (33025 ) = 11 A (22.13) (c) The average power Ps delivered to the secondary coil is the product of Is and Vs:
Ps = IsVs = (11 A)(9.1 V) = 1.0 × 10 2 W (20.15a)
As a check on our calculation, we verify that the power delivered to the
secondary coil is the same as that sent to the primary coil from the wall
receptacle:
Pp = IpVp = (0.83 A)(120 V) = 1.0 × 102 W
Transformers play an important role in the transmission of power between electrical generat-
ing plants and the communities they serve. Whenever electricity is transmitted, there is always
some loss of power in the transmission lines themselves due to resistive heating. Since the resis-
tance of the wires is proportional to their length, the longer the wires the greater is the power loss.
The resistance of the wires is also inversely proportional to their cross-sectional area, so thicker
22.9 Transformers 651
wires are used to help minimize the power loss. To reduce the loss further, power companies
use transformers that step up the voltage to high levels while reducing the current. A smaller
current means less power loss, since P = I2R, where R is the resistance of the transmission wires (see Problem 67). Interactive Figure 22.30 shows one possible way of transmitting power. The power plant produces a voltage of 12 000 V. This voltage is then raised to 240 000 V by a 20:1
step-up transformer. The high-voltage power is sent over the long-distance transmission line.
Upon arrival at the city, the voltage is reduced to about 8000 V at a substation using a 1:30 step-
down transformer. However, before any domestic use, the voltage is further reduced to 240 V (or
possibly 120 V) by another step-down transformer that is often mounted on a utility pole. The
power is then distributed to consumers.
Check Your Understanding
(The answers are given at the end of the book.) 19. A transformer changes the 120-V voltage at a wall socket to 12 000 V. The current delivered by the
wall socket is (a) stepped up by a factor of 100, (b) stepped down by a factor of 100, (c) neither stepped up nor stepped down.
20. A transformer that stepped up the voltage and the current simultaneously would (a) produce less power at the secondary coil than was supplied at the primary coil, (b) produce more power at the secondary coil than was supplied at the primary coil, (c) produce the same amount of power at the secondary coil that was supplied at the primary coil, (d) violate the law of conservation of energy. Choose one or more.
Power plant
Step-up transformer
High-voltage transmission line
12 000 V 8000 V
240 000 V 240 V
Step-down transformer (substation)
Step-down transformer
INTERACTIVE FIGURE 22.30 Transformers play a key role in the transmission of electric power.
EXAMPLE 14 BIO The Physics of Wireless Charging—Implantable Medical Devices
Because of electromagnetic induction, energy can be transferred between
two coils that are not in contact, as long as the changing magnetic fl ux
created by one coil passes through the second one. This arrangement can
be used to charge batteries connected to small medical devices that are
implanted inside the body for many diff erent applications (Figure 22.31). The implantable device is powered by a rechargeable battery that is con-
nected to a small, fl at coil (secondary) that is positioned just below the
skin. The primary coil from the external charging device is placed on the
skin directly above the secondary coil and transfers energy by induction
to charge the device’s internal battery. Consider the example of a wire-
less pacemaker, where a battery is connected to a coil that produces an
average power of 3.0 W. If the rms current in the charging (primary)
coil is 500 mA, what is the voltage across it? Assume an energy transfer
effi ciency of 70%.
Reasoning The problem tells us that the average power delivered to the secondary coil by the primary occurs with an effi ciency of 70%. This
means that Ps = (70%)Pp = (0.70)Pp. We can then use Equation 20.15a to solve for the voltage across the primary coil.
Solution Substituting Equation 20.15a into the expression above, we get the following: Ps = (0.70)IpVp. We can rearrange this expression and solve for the voltage:
Vp = Ps
(0.70)Ip =
3.0 W
(0.70)(0.50 mA) = 8.6 V .
Implantable devices off er the advantage of lower infection risk, since no
wires have to exit the body. However, they take longer to charge, and fur-
ther advances in their implementation, as well as other areas of concern,
like security, will have to be improved before they are widely used.
652 CHAPTER 22 Electromagnetic Induction
Deep brain neurostimulators
Cochlear implants
Wireless implantable medical devices
Cardiac defibrillators/ pacemakers
Insulin pumps
Gastric stimulators
Foot drop implants
I
FIGURE 22.31 Examples of medical devices that could be implanted inside the body and
charged inductively.
Concept Summary 22.1 Induced Emf and Induced Current Electromagnetic induction is the phenomenon in which an emf is induced in a piece of wire or a coil of
wire with the aid of a magnetic fi eld. The emf is called an induced emf, and
any current that results from the emf is called an induced current.
22.2 Motional Emf An emf ℰ is induced in a conducting rod of length L when the rod moves with a speed 𝜐 in a magnetic fi eld of magnitude B, according to Equation 22.1, which applies when the velocity of the rod, the
length of the rod, and the magnetic fi eld are mutually perpendicular. When
the motional emf is used to operate an electrical device, such as a light bulb,
the energy delivered to the device originates in the work done to move the
rod, and the law of conservation of energy applies.
ℰ = υBL (22.1)
22.3 Magnetic Flux The magnetic fl ux Φ that passes through a surface is given by Equation 22.2, where B is the magnitude of the magnetic fi eld, A is the area of the surface, and 𝜙 is the angle between the fi eld and the normal
to the surface. The magnetic fl ux is proportional to the number of magnetic
fi eld lines that pass through the surface.
Φ = BA cos ϕ (22.2)
22.4 Faraday’s Law of Electromagnetic Induction Faraday’s law of electromagnetic induction states that the average emf ℰ induced in a coil of
N loops is given by Equation 22.3, where ΔΦ is the change in magnetic fl ux through one loop and Δt is the time interval during which the change occurs. Motional emf is a special case of induced emf.
ℰ = −N ( Φ − Φ0
t − t0 ) = −N ∆Φ
∆t (22.3)
22.5 Lenz’s Law Lenz’s law provides a way to determine the polarity of an induced emf. Lenz’s law is stated as follows: The induced emf resulting from
a changing magnetic fl ux has a polarity that leads to an induced current whose
direction is such that the induced magnetic fi eld opposes the original fl ux
change. This statement is a consequence of the law of conservation of energy.
22.7 The Electric Generator In its simplest form, an electric generator consists of a coil of N loops that rotates in a uniform magnetic fi eld B→ . The
emf produced by this generator is given by Equation 22.4, where A is the area of the coil, 𝜔 is the angular speed (in rad/s) of the coil, and ℰ0 = NAB𝜔 is the peak emf. The angular speed in rad/s is related to the frequency f in cycles/s, or Hz, according to 𝜔 = 2𝜋f.
ℰ = NABω sin ωt = ℰ0 sin ωt (22.4)
When an electric motor is running, it exhibits a generator-like behavior by
producing an induced emf, called the back emf. The current I needed to keep the motor running at a constant speed is given by Equation 22.5, where V is the emf applied to the motor by an external source, ℰ is the back emf, and R is the resistance of the motor coil.
I = V − ℰ
R (22.5)
22.8 Mutual Inductance and Self-Inductance Mutual induction is the eff ect in which a changing current in the primary coil induces an emf
in the secondary coil. The average emf ℰs induced in the secondary coil
by a change in current ΔIp in the primary coil is given by Equation 22.7, where Δt is the time interval during which the change occurs. The con- stant M is the mutual inductance between the two coils and is measured in henries (H).
ℰs = −M ∆ Ip ∆ t
(22.7)
Self-induction is the eff ect in which a change in current ΔI in a coil in- duces an average emf ℰ in the same coil, according to Equation 22.9. The
constant L is the self-inductance, or inductance, of the coil and is measured in henries.
ℰ = −L ∆ I ∆ t
(22.9)
To establish a current I in an inductor, work must be done by an external agent. This work is stored as energy in the inductor, the amount
of energy being given by Equation 22.10. The energy stored in an induc-
tor can be regarded as being stored in its magnetic fi eld. At any point in
air or vacuum or in a nonmagnetic material where a magnetic fi eld B→
Focus on Concepts 653
exists, the energy density, or the energy stored per unit volume, is given
by Equation 22.11.
Energy = 1
2 LI 2 (22.10)
Energy density = 1
2μ0 B2 (22.11)
22.9 Transformers A transformer consists of a primary coil of Np turns and a secondary coil of Ns turns. If the resistances of the coils are negligible, the voltage Vp across the primary coil and the voltage Vs across the secondary coil are related according to the transformer equation, which is Equation 22.12,
where the ratio Ns/Np is called the turns ratio of the transformer. A trans- former functions with ac electricity, not with dc. If the transformer is 100%
effi cient in transferring power from the primary to the secondary coil,
the ratio of the secondary current Is to the primary current Ip is given by Equation 22.13.
Vs Vp
= Ns Np
(22.12)
I
s
Ip =
Np Ns
(22.13)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 22.2 Motional Emf 2. You have three light bulbs; bulb A has a resistance of 240 Ω, bulb B has a resistance of 192 Ω, and bulb C has a resistance of 144 Ω. Each of these
bulbs is used for the same amount of time in a setup like the one in the draw-
ing. In each case the speed of the rod and the magnetic fi eld strength are the
same. Rank the setups in descending order, according to how much work
the hand in the drawing must do (largest amount of work fi rst). (a) A, B, C (b) A, C, B (c) B, C, A (d) B, A, C (e) C, B, A
QUESTION 2
Conducting rail +
–
I
I
I L
v
Section 22.3 Magnetic Flux 4. The drawing shows a cube. The dashed lines in the drawing are perpen- dicular to faces 1, 2, and 3 of the cube. Magnetic fi elds are oriented with
respect to these faces as shown, and each of the three fi elds B1 →
, B2 →
, and B3 →
has the same magnitude. Note that B2 →
is parallel to face 2 of the cube. Rank
the magnetic fl uxes that pass through the faces 1, 2, and 3 of the cube in
decreasing order (largest fi rst). (a) Φ1, Φ2, Φ3 (b) Φ1, Φ3, Φ2 (c) Φ2, Φ1, Φ3 (d) Φ2, Φ3, Φ1 (e) Φ3, Φ2, Φ1
QUESTION 4
B120°
70° 90°
B3
B2
1
2
3
Section 22.4 Faraday’s Law of Electromagnetic Induction 7. The drawing shows three fl at coils, one square and two rectangular, that are each being pushed into a region where there is a uniform magnetic fi eld
directed into the page. Outside of this region the magnetic fi eld is zero. In
each case the magnetic fi eld within the region has the same magnitude, and
the coil is being pushed at the same velocity v→. Each coil begins with one side just at the edge of the fi eld region. Consider the magnitude of the aver-
age emf induced as each coil is pushed from the starting position shown in
the drawing until the coil is just completely within the fi eld region. Rank the
magnitudes of the average emfs in descending order (largest fi rst). (a) ℰA, ℰB, ℰC (b) ℰA, ℰC, ℰB (c) ℰB, ℰA and ℰC (a tie) (d) ℰC, ℰA and ℰB (a tie)
L
L
A
L
2L
B
L
2L
C
v vv
QUESTION 7
8. A long, vertical, straight wire carries a current I. The wire is perpendicular to the plane of a circular metal loop
and passes through the center of the loop (see the draw-
ing). The loop is allowed to fall and maintains its orient-
ation with respect to the straight wire while doing so. In
what direction does the current induced in the loop fl ow?
(a) There is no induced current. (b) It is fl owing around the loop from A to B to C to A. (c) It is fl owing around the loop from C to B to A to C.
Section 22.5 Lenz’s Law 9. The drawing shows a top view of two circular coils of conducting wire lying on a fl at surface. The centers of the coils coincide. In the larger coil
there are a switch and a battery. The smaller
coil contains no switch and no battery. De-
scribe the induced current that appears in the
smaller coil when the switch in the larger coil
is closed. (a) It fl ows counterclockwise forever after the switch is closed. (b) It fl ows clock- wise forever after the switch is closed. (c) It fl ows counterclockwise, but only for a short
period just after the switch is closed. (d) It fl ows clockwise, but only for a short period just
after the switch is closed.
Focus on Concepts
I
A
B
C
QUESTION 8
Switch
QUESTION 9
654 CHAPTER 22 Electromagnetic Induction
Section 22.7 The Electric Generator 10. You have a fi xed length of conducting wire. From it you can construct a single-turn fl at coil that has the shape of a square, a circle, or a rectangle
with the long side twice the length of the short side. Each can be used with
the same magnetic fi eld to produce a generator that operates at the same fre-
quency. Rank the peak emfs ℰ0 of the three generators in descending order
(largest fi rst). (a) ℰ0, square, ℰ0, circle, ℰ0, rectangle (b) ℰ0, circle, ℰ0, square, ℰ0, rectangle (c) ℰ0, square, ℰ0, rectangle, ℰ0, circle (d) ℰ0, rectangle, ℰ0, square, ℰ0, circle (e) ℰ0, rectangle, ℰ0, circle, ℰ0, square
12. An electric motor is plugged into a standard wall socket and is running at normal speed. Suddenly, some dirt prevents the shaft of the motor from
turning quite so rapidly. What happens to the back emf of the motor, and
what happens to the current that the motor draws from the wall socket?
(a) The back emf increases, and the current drawn from the socket decreases. (b) The back emf increases, and the current drawn from the socket increases. (c) The back emf decreases, and the current drawn from the socket decreases. (d) The back emf decreases, and the current drawn from the socket increases.
Section 22.8 Mutual Inductance and Self-Inductance 14. Inductor 1 stores the same amount of energy as inductor 2, although it has only one-half the inductance of inductor 2. What is the ratio I1/I2 of the currents in the two inductors? (a) 2.000 (b) 1.414 (c) 4.000 (d) 0.500 (e) 0.250
Section 22.9 Transformers 18. The primary coil of a step-up transformer is connected across the termin- als of a standard wall socket, and resistor 1 with a resistance R1 is connected across the secondary coil. The current in the resistor is then measured. Next,
resistor 2 with a resistance R2 is connected directly across the terminals of the wall socket (without the transformer). The current in this resistor is also
measured and found to be the same as the current in resistor 1. How does
the resistance R2 compare to the resistance R1? (a) The resistance R2 is less than the resistance R1. (b) The resistance R2 is greater than the resistance R1. (c) The resistance R2 is the same as the resistance R1.
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 22.2 Motional Emf 1. E A 0.80-m aluminum bar is held with its length parallel to the east–west direction and dropped from a bridge. Just before the bar hits the river below,
its speed is 22 m/s, and the emf induced across its length is 6.5 × 10−4 V. As-
suming the horizontal component of the earth’s magnetic fi eld at the location
of the bar points directly north, (a) determine the magnitude of the horizontal component of the earth’s magnetic fi eld, and (b) state whether the east end or the west end of the bar is positive.
2. E Near San Francisco, where the vertically downward component of the earth’s magnetic fi eld is 4.8 × 10−5 T, a car is traveling forward at 25 m/s.
The width of the car is 2.0 m. (a) Find the emf induced between the two sides of the car. (b) Which side of the car is positive—the driver’s side or the passenger’s side?
3. E In 1996, NASA performed an experiment called the Tethered Satellite experiment. In this experiment a 2.0 × 104-m length of wire was let out by the
space shuttle Atlantis to generate a motional emf. The shuttle had an orbital speed of 7.6 × 103 m/s, and the magnitude of the earth’s magnetic fi eld at the
location of the wire was 5.1 × 10−5 T. If the wire had moved perpendicular to
the earth’s magnetic fi eld, what would have been the motional emf generated
between the ends of the wire?
4. E BIO The drawing shows a type of fl ow meter that can be used to measure the speed of blood in situations when a blood vessel is suffi ciently
exposed (e.g., during surgery). Blood is conductive enough that it can be
treated as a moving conductor. When it fl ows perpendicularly with respect
to a magnetic fi eld, as in the drawing, electrodes can be used to measure
the small voltage that develops across the vessel. Suppose that the speed of
the blood is 0.30 m/s and the diameter of the vessel is 5.6 mm. In a 0.60-T
magnetic fi eld what is the magnitude of the voltage that is measured with the
electrodes in the drawing?
PROBLEM 4
Electrode
Blood
Electrode
5. E SSM The drawing shows three identical rods (A, B, and C) moving in diff erent planes. A constant magnetic fi eld of magnitude 0.45 T is dir-
ected along the +y axis. The length of each rod is L = 1.3 m, and the rods each have the same speed, 𝜐A = 𝜐B = 𝜐C = 2.7 m/s. For each rod, fi nd the
magnitude of the motional emf, and indicate which end (1 or 2) of the rod
is positive.
PROBLEM 5
y B
z
x
C
B
A
1 2
1
2
1
2
v
v
v
6. E GO Two circuits contain an emf produced by a moving metal rod, like that shown in Animated Figure 22.4b. The speed of the rod is the same in each circuit, but the bulb in circuit 1 has one-half the resistance of the bulb in
circuit 2. The circuits are otherwise identical. The resistance of the light bulb
in circuit 1 is 55 Ω, and that in circuit 2 is 110 Ω. Determine (a) the ratio ℰ1/ ℰ2 of the emfs and (b) the ratio I1/I2 of the currents in the circuits. (c) If the speed of the rod in circuit 1 were twice that in circuit 2, what would be the
ratio P1/P2 of the powers in the circuits?
Problems
Problems 655
7. M GO Refer to the drawing that accompanies Check Your Understanding Question 14. Suppose that the voltage of the battery in the circuit is 3.0 V,
the magnitude of the magnetic fi eld (directed perpendicularly into the plane
of the paper) is 0.60 T, and the length of the rod between the rails is 0.20 m.
Assuming that the rails are very long and have negligible resistance, fi nd the
maximum speed attained by the rod after the switch is closed.
8. M V-HINT Multiple-Concept Example 2 discusses the concepts that are used in this problem. Suppose that the magnetic fi eld in Figure 22.5 has a magnitude of 1.2 T, the rod has a length of 0.90 m, and the hand keeps the
rod moving to the right at a constant speed of 3.5 m/s. If the current in the
circuit is 0.040 A, what is the average power being delivered to the circuit
by the hand?
9. M CHALK SSM Suppose that the light bulb in Animated Figure 22.4b is a 60.0-W bulb with a resistance of 240 Ω. The magnetic fi eld has a magnitude
of 0.40 T, and the length of the rod is 0.60 m. The only resistance in the cir-
cuit is that due to the bulb. What is the shortest distance along the rails that
the rod would have to slide for the bulb to remain lit for one-half second?
10. H Review Conceptual Example 3 and Figure 22.7b. A conducting rod slides down between two frictionless vertical copper tracks at a constant
speed of 4.0 m/s perpendicular to a 0.50-T magnetic fi eld. The resistance of
the rod and tracks is negligible. The rod maintains electrical contact with the
tracks at all times and has a length of 1.3 m. A 0.75-Ω resistor is attached
between the tops of the tracks. (a) What is the mass of the rod? (b) Find the change in the gravitational potential energy that occurs in a time of 0.20 s.
(c) Find the electrical energy dissipated in the resistor in 0.20 s.
Section 22.3 Magnetic Flux For problems in this set, assume that the magnetic fl ux is a positive quantity. 11. E SSM The drawing shows two surfaces that have the same area. A uniform magnetic fi eld B→ fi lls the space occupied by these surfaces, and it is oriented parallel to the yz plane as shown. Find the ratio Φxz/Φxy of the mag- netic fl uxes that pass through the surfaces.
PROBLEM 11
y
z
x
B 35°
12. E Two fl at surfaces are exposed to a uniform, horizontal magnetic fi eld of magnitude 0.47 T. When viewed edge-on, the fi rst surface is tilted at an
angle of 12° from the horizontal, and a net magnetic fl ux of 8.4 × 10−3 Wb
passes through it. The same net magnetic fl ux passes through the second sur-
face. (a) Determine the area of the fi rst surface. (b) Find the smallest possible value for the area of the second surface.
13. E SSM A standard door into a house rotates about a vertical axis through one side, as defi ned by the door’s hinges. A uniform magnetic fi eld is parallel
to the ground and perpendicular to this axis. Through what angle must the
door rotate so that the magnetic fl ux that passes through it decreases from its
maximum value to one-third of its maximum value?
14. E GO A loop of wire has the shape shown in the drawing. The top part of the wire is bent into a semicircle of radius r = 0.20 m. The normal to the plane of the loop is parallel to a constant magnetic fi eld (𝜙 = 0°) of
magnitude 0.75 T. What is the change ∆Φ in the magnetic fl ux that passes
through the loop when, starting with the position shown in the drawing, the
semicircle is rotated through half a revolution?
PROBLEM 14
B (into paper)
r
15. E A magnetic fi eld has a magnitude of 0.078 T and is uniform over a circular surface whose radius is 0.10 m. The fi eld is oriented at an angle of
𝜙 = 25° with respect to the normal to the surface. What is the magnetic fl ux
through the surface?
16. M GO A square loop of wire consisting of a single turn is perpendic- ular to a uniform magnetic fi eld. The square loop is then re-formed into
a circular loop, which also consists of a single turn and is also perpen-
dicular to the same magnetic fi eld. The magnetic fl ux that passes through
the square loop is 7.0 × 10−3 Wb. What is the fl ux that passes through the
circular loop?
17. M V-HINT A fi ve-sided object, whose dimensions are shown in the draw- ing, is placed in a uniform magnetic fi eld. The magnetic fi eld has a mag-
nitude of 0.25 T and points along the positive y direction. Determine the magnetic fl ux through each of the fi ve sides.
PROBLEM 17
y
B
z
x 0.40 m
1. 2
m 0.50 m
0.30 m
Section 22.4 Faraday’s Law of Electromagnetic Induction 18. E GO A magnetic fi eld passes through a stationary wire loop, and its magnitude changes in time according to the graph in the drawing. The
direction of the fi eld remains constant, however. There are three equal time
intervals indicated in the graph: 0–3.0 s, 3.0–6.0 s, and 6.0–9.0 s. The loop
consists of 50 turns of wire and has an area of 0.15 m2. The magnetic fi eld
is oriented parallel to the normal to the loop. For purposes of this problem,
this means that ϕ = 0° in Equation 22.2. (a) For each interval, determine the induced emf. (b) The wire has a resistance of 0.50 Ω. Determine the induced current for the fi rst and third intervals.
PROBLEM 18 t (s)
3.00 0
0.40
0.20
6.0 9.0
B (T
)
19. E A rectangular loop of wire with sides 0.20 and 0.35 m lies in a plane perpendicular to a constant magnetic fi eld (see part a of the drawing). The magnetic fi eld has a magnitude of 0.65 T and is directed parallel to the nor-
mal of the loop’s surface. In a time of 0.18 s, one-half of the loop is then fol-
ded back onto the other half, as indicated in part b of the drawing. Determine the magnitude of the average emf induced in the loop.
656 CHAPTER 22 Electromagnetic Induction
(a) (b)
PROBLEM 19
20. E BIO Magnetic resonance imaging (MRI) is a medical technique for producing pictures of the interior of the body. The patient is placed within a
strong magnetic fi eld. One safety concern is what would happen to the posit-
ively and negatively charged particles in the body fl uids if an equipment fail-
ure caused the magnetic fi eld to be shut off suddenly. An induced emf could
cause these particles to fl ow, producing an electric current within the body.
Suppose the largest surface of the body through which fl ux passes has an area
of 0.032 m2 and a normal that is parallel to a magnetic fi eld of 1.5 T. Determ-
ine the smallest time period during which the fi eld can be allowed to vanish
if the magnitude of the average induced emf is to be kept less than 0.010 V.
21. E SSM A circular coil (950 turns, radius = 0.060 m) is rotating in a uni- form magnetic fi eld. At t = 0 s, the normal to the coil is perpendicular to the magnetic fi eld. At t = 0.010 s, the normal makes an angle of ϕ = 45° with the fi eld because the coil has made one-eighth of a revolution. An average emf of
magnitude 0.065 V is induced in the coil. Find the magnitude of the magnetic
fi eld at the location of the coil.
22. E The magnetic fl ux that passes through one turn of a 12-turn coil of wire changes to 4.0 from 9.0 Wb in a time of 0.050 s. The average induced
current in the coil is 230 A. What is the resistance of the wire?
23. E MMH A constant magnetic fi eld passes through a single rectangular loop whose dimensions are 0.35 m × 0.55 m. The magnetic fi eld has a mag-
nitude of 2.1 T and is inclined at an angle of 65° with respect to the normal
to the plane of the loop. (a) If the magnetic fi eld decreases to zero in a time of 0.45 s, what is the magnitude of the average emf induced in the loop?
(b) If the magnetic fi eld remains constant at its initial value of 2.1 T, what is the magnitude of the rate ∆A/∆t at which the area should change so that the average emf has the same magnitude as in part (a)?
24. E A uniform magnetic fi eld is perpendicular to the plane of a single- turn circular coil. The magnitude of the fi eld is changing, so that an emf
of 0.80 V and a current of 3.2 A are induced in the coil. The wire is then
re-formed into a single-turn square coil, which is used in the same magnetic
fi eld (again perpendicular to the plane of the coil and with a magnitude chan-
ging at the same rate). What emf and current are induced in the square coil?
25. M MMH A copper rod is sliding on two conducting rails that make an angle of 19° with respect to each other, as in the drawing. The rod is moving
to the right with a constant speed of 0.60 m/s. A 0.38-T uniform magnetic
fi eld is perpendicular to the plane of the paper. Determine the magnitude of
the average emf induced in the triangle ABC during the 6.0-s period after the rod has passed point A.
PROBLEM 25
B (into paper)
A C
B
19° 90° υ = 0.60 m/s
26. M CHALK GO A fl at coil of wire has an area A, N turns, and a resistance R. It is situated in a magnetic fi eld, such that the normal to the coil is parallel to the magnetic fi eld. The coil is then rotated through an angle of 90°, so that
the normal becomes perpendicular to the magnetic fi eld. The coil has an area
of 1.5 × 10−3 m2, 50 turns, and a resistance of 140 Ω. During the time while it
is rotating, a charge of 8.5 × 10−5 C fl ows in the coil. What is the magnitude
of the magnetic fi eld?
27. E SSM A magnetic fi eld is passing through a loop of wire whose area is 0.018 m2. The direction of the magnetic fi eld is parallel to the normal to
the loop, and the magnitude of the fi eld is increasing at the rate of 0.20 T/s.
(a) Determine the magnitude of the emf induced in the loop. (b) Suppose that the area of the loop can be enlarged or shrunk. If the magnetic fi eld is
increasing as in part (a), at what rate (in m2/s) should the area be changed at
the instant when B = 1.8 T if the induced emf is to be zero? Explain whether the area is to be enlarged or shrunk.
28. M V-HINT A fl at circular coil with 105 turns, a radius of 4.00 × 10−2 m, and a resistance of 0.480 Ω is exposed to an external magnetic fi eld that is
directed perpendicular to the plane of the coil. The magnitude of the external
magnetic fi eld is changing at a rate of ∆B/∆t = 0.783 T/s, thereby inducing a current in the coil. Find the magnitude of the magnetic fi eld at the center of
the coil that is produced by the induced current.
29. M GO The drawing shows a coil of copper wire that consists of two semicircles joined by straight sections of wire. In part a the coil is lying fl at on a horizontal surface. The dashed line also lies in the plane of the hori-
zontal surface. Starting from the orientation in part a, the smaller semicircle rotates at an angular frequency 𝜔 about the dashed line, until its plane be-
comes perpendicular to the horizontal surface, as shown in part b. A uniform magnetic fi eld is constant in time and is directed upward, perpendicular to the
horizontal surface. The fi eld completely fi lls the region occupied by the coil
in either part of the drawing. The magnitude of the magnetic fi eld is 0.35 T.
The resistance of the coil is 0.025 Ω, and the smaller semicircle has a radius
of 0.20 m. The angular frequency at which the small semicircle rotates is
1.5 rad/s. Determine the average current I, if any, induced in the coil as the coil changes shape from that in part a of the drawing to that in part b. Be sure to include an explicit plus or minus sign along with your answer.
(b)(a)
ω ω
PROBLEM 29
30. M GO A conducting coil of 1850 turns is connected to a galvanometer, and the total resistance of the circuit is 45.0 Ω. The area of each turn is 4.70 ×
10−4 m2. This coil is moved from a region where the magnetic fi eld is zero into
a region where it is nonzero, the normal to the coil being kept parallel to the
magnetic fi eld. The amount of charge that is induced to fl ow around the circuit
is measured to be 8.87 × 10−3 C. Find the magnitude of the magnetic fi eld.
31. H SSM Available in WileyPLUS.
Section 22.5 Lenz’s Law 32. E Starting from the position indicated in the drawing, the semicircu- lar piece of wire rotates through half a revolution in the direction shown.
Which end of the resistor is positive—the left or the right end? Explain your
reasoning.
PROBLEM 32
B (into paper)
r
Problems 657
33. E SSM The plane of a fl at, circular loop of wire is horizontal. An ex- ternal magnetic fi eld is directed perpendicular to the plane of the loop. The
magnitude of the external magnetic fi eld is increasing with time. Because of
this increasing magnetic fi eld, an induced current is fl owing clockwise in the
loop, as viewed from above. What is the direction of the external magnetic
fi eld? Justify your conclusion.
34. E GO The drawing shows a straight wire carrying a current I. Above the wire is a rectangular loop that contains a resistor R. If the current I is decreasing in time, what is the direction of the induced current through the
resistor R—left-to-right or right-to-left?
PROBLEM 34 I
R
35. E SSM The drawing depicts a copper loop lying fl at on a table (not shown) and connected to a battery via a closed switch. The current I in the loop generates the magnetic fi eld lines shown in the drawing. The switch is
then opened and the current goes to zero. There are also two smaller con-
ducting loops A and B lying fl at on the table, but not connected to batteries.
Determine the direction of the induced current in (a) loop A and (b) loop B. Specify the direction of each induced current to be clockwise or counter-
clockwise when viewed from above the table. Provide a reason for each
answer.
PROBLEM 35
+ –
Copper loop
Switch
Magnetic field lines
A B
I
I
36. E The drawing shows that a uniform magnetic fi eld is directed perpen- dicularly into the plane of the paper and fi lls the entire region to the left of
the y axis. There is no magnetic fi eld to the right of the y axis. A rigid right triangle ABC is made of copper wire. The triangle rotates counterclockwise about the origin at point C. What is the direction (clockwise or counterclock- wise) of the induced current when the triangle is crossing (a) the +y axis, (b) the −x axis, (c) the −y axis, and (d) the +x axis? For each case, justify your answer.
PROBLEM 36
y
x C B
A
B (into paper)
37. M MMH A circular loop of wire rests on a table. A long, straight wire lies on this loop, directly over its center, as the drawing illustrates. The
current I in the straight wire is decreasing. In what direction is the induced current, if any, in the loop? Give your reasoning.
PROBLEM 37
I
Table top
38. M V-HINT The drawing shows a bar magnet falling through a metal ring. In part a the ring is solid all the way around, but in part b it has been cut through. (a) Explain why the motion of the magnet in part a is retarded when the magnet is above the ring and below the ring as well. Draw any induced
currents that appear in the ring. (b) Explain why the motion of the magnet is unaff ected by the ring in part b.
PROBLEM 38
N
(a)
S
(b)
N
S
39. H Available in WileyPLUS.
Section 22.7 The Electric Generator 40. E A 120.0-V motor draws a current of 7.00 A when running at normal speed. The resistance of the armature wire is 0.720 Ω. (a) Determine the back emf generated by the motor. (b) What is the current at the instant when the motor is just turned on and has not begun to rotate? (c) What series resist- ance must be added to limit the starting current to 15.0 A?
41. E SSM A generator has a square coil consisting of 248 turns. The coil rotates at 79.1 rad/s in a 0.170-T magnetic fi eld. The peak output of the gen-
erator is 75.0 V. What is the length of one side of the coil?
42. E You need to design a 60.0-Hz ac generator that has a maximum emf of 5500 V. The generator is to contain a 150-turn coil that has an area per
turn of 0.85 m2. What should be the magnitude of the magnetic fi eld in which
the coil rotates?
43. E MMH The maximum strength of the earth’s magnetic fi eld is about 6.9 × 10−5 T near the south magnetic pole. In principle, this fi eld could be
used with a rotating coil to generate 60.0-Hz ac electricity. What is the min-
imum number of turns (area per turn = 0.022 m2) that the coil must have to
produce an rms voltage of 120 V?
44. E Available in WileyPLUS. 45. M V-HINT A generator uses a coil that has 100 turns and a 0.50-T mag- netic fi eld. The frequency of this generator is 60.0 Hz, and its emf has an rms
value of 120 V. Assuming that each turn of the coil is a square (an approxim-
ation), determine the length of the wire from which the coil is made.
46. M GO The coil of a generator has a radius of 0.14 m. When this coil is unwound, the wire from which it is made has a length of 5.7 m. The magnetic
fi eld of the generator is 0.20 T, and the coil rotates at an angular speed of
25 rad/s. What is the peak emf of this generator?
47. M SSM Consult Multiple-Concept Example 11 for background material relating to this problem. A small rubber wheel on the shaft of a bicycle gen-
erator presses against the bike tire and turns the coil of the generator at an
angular speed that is 38 times as great as the angular speed of the tire itself.
658 CHAPTER 22 Electromagnetic Induction
Each tire has a radius of 0.300 m. The coil consists of 125 turns, has an area
of 3.86 × 10−3 m2, and rotates in a 0.0900-T magnetic fi eld. The bicycle starts
from rest and has an acceleration of +0.550 m/s2. What is the peak emf pro-
duced by the generator at the end of 5.10 s?
48. H Available in WileyPLUS.
Section 22.8 Mutual Inductance and Self-Inductance 49. E SSM The earth’s magnetic fi eld, like any magnetic fi eld, stores energy. The maximum strength of the earth’s fi eld is about 7.0 × 10−5 T. Find
the maximum magnetic energy stored in the space above a city if the space
occupies an area of 5.0 × 108 m2 and has a height of 1500 m.
50. E The current through a 3.2-mH inductor varies with time according to the graph shown in the drawing. What is the average induced emf during the
time intervals (a) 0–2.0 ms, (b) 2.0–5.0 ms, and (c) 5.0–9.0 ms?
PROBLEM 50 t (ms) 2.00
0
4.0
5.0 9.0
I (A
)
51. E Two coils of wire are placed close together. Initially, a current of 2.5 A exists in one of the coils, but there is no current in the other. The current
is then switched off in a time of 3.7 × 10−2 s. During this time, the average
emf induced in the other coil is 1.7 V. What is the mutual inductance of the
two-coil system?
52. E GO During a 72-ms interval, a change in the current in a primary coil occurs. This change leads to the appearance of a 6.0-mA current in a nearby
secondary coil. The secondary coil is part of a circuit in which the resistance
is 12 Ω. The mutual inductance between the two coils is 3.2 mH. What is the
change in the primary current?
53. E Mutual induction can be used as the basis for a metal detector. A typical setup uses two large coils that are parallel to each other and have
a common axis. Because of mutual induction, the ac generator connected
to the primary coil causes an emf of 0.46 V to be induced in the secondary
coil. When someone without metal objects walks through the coils, the mu-
tual inductance and, thus, the induced emf do not change much. But when a
person carrying a handgun walks through, the mutual inductance increases.
The change in emf can be used to trigger an alarm. If the mutual inductance
increases by a factor of three, fi nd the new value of the induced emf.
54. E GO A constant current of I = 15 A exists in a solenoid whose induct- ance is L = 3.1 H. The current is then reduced to zero in a certain amount of time. (a) If the current goes from 15 to 0 A in a time of 75 ms, what is the emf induced in the solenoid? (b) How much electrical energy is stored in the solenoid? (c) At what rate must the electrical energy be removed from the solenoid when the current is reduced to 0 A in a time of 75 ms? Note that the
rate at which energy is removed is the power.
55. E SSM Suppose you wish to make a solenoid whose self-inductance is 1.4 mH. The inductor is to have a cross-sectional area of 1.2 × 10−3 m2 and a
length of 0.052 m. How many turns of wire are needed?
56. M GO A long, current-carrying solenoid with an air core has 1750 turns per meter of length and a radius of 0.0180 m. A coil of 125 turns is wrapped
tightly around the outside of the solenoid, so it has virtually the same radius
as the solenoid. What is the mutual inductance of this system?
57. M Available in WileyPLUS. 58. M V-HINT Available in WileyPLUS. 59. H Available in WileyPLUS.
Section 22.9 Transformers 60. E The battery charger for an MP3 player contains a step-down trans- former with a turns ratio of 1:32, so that the voltage of 120 V available at a
wall socket can be used to charge the battery pack or operate the player. What
voltage does the secondary coil of the transformer provide?
61. E MMH The secondary coil of a step-up transformer provides the voltage that operates an electrostatic air fi lter. The turns ratio of the trans-
former is 50:1. The primary coil is plugged into a standard 120-V outlet. The
current in the secondary coil is 1.7 × 10−3 A. Find the power consumed by
the air fi lter.
62. E GO The rechargeable batteries for a laptop computer need a much smaller voltage than what a wall socket provides. Therefore, a transformer is
plugged into the wall socket and produces the necessary voltage for charging
the batteries. The batteries are rated at 9.0 V, and a current of 225 mA is used
to charge them. The wall socket provides a voltage of 120 V. (a) Determine the turns ratio of the transformer. (b) What is the current coming from the wall socket? (c) Find the average power delivered by the wall socket and the average power sent to the batteries.
63. E The resistances of the primary and secondary coils of a transformer are 56 and 14 Ω, respectively. Both coils are made from lengths of the same
copper wire. The circular turns of each coil have the same diameter. Find the
turns ratio Ns/Np. 64. E A transformer consisting of two coils wrapped around an iron core is connected to a generator and a resistor, as shown in the drawing.
There are 11 turns in the primary coil and 18 turns in the secondary coil.
The peak voltage across the resistor is 67 V. What is the peak emf of the
generator?
PROBLEM 64
R
65. E SSM A step-down transformer (turns ratio = 1:8) is used with an electric train to reduce the voltage from the wall receptacle to a value needed
to operate the train. When the train is running, the current in the secondary
coil is 1.6 A. What is the current in the primary coil?
66. M GO In a television set the power needed to operate the picture tube comes from the secondary of a transformer. The primary of the transformer
is connected to a 120-V receptacle on a wall. The picture tube of the televi-
sion set uses 91 W, and there is 5.5 mA of current in the secondary coil of
the transformer to which the tube is connected. Find the turns ratio Ns/Np of the transformer.
67. M SSM A generating station is producing 1.2 × 106 W of power that is to be sent to a small town located 7.0 km away. Each of the two wires
that comprise the transmission line has a resistance per kilometer of 5.0 ×
10−2 Ω/km. (a) Find the power used to heat the wires if the power is trans- mitted at 1200 V. (b) A 100:1 step-up transformer is used to raise the voltage before the power is transmitted. How much power is now used to
heat the wires?
68. M V-HINT Available in WileyPLUS. 69. H A generator is connected across the primary coil (Np turns) of a transformer, while a resistance R2 is connected across the secondary coil (Ns turns). This circuit is equivalent to a circuit in which a single resist- ance R1 is connected directly across the generator, without the transformer. Show that R1 = (Np/Ns)2R2, by starting with Ohm’s law as applied to the secondary coil.
Concepts and Calculations Problems 659
70. E In each of two coils the rate of change of the magnetic fl ux in a single loop is the same. The emf induced in coil 1, which has 184 loops, is 2.82 V.
The emf induced in coil 2 is 4.23 V. How many loops does coil 2 have?
71. E SSM Available in WileyPLUS. 72. E GO A planar coil of wire has a single turn. The normal to this coil is parallel to a uniform and constant (in time) magnetic fi eld of 1.7 T. An emf
that has a magnitude of 2.6 V is induced in this coil because the coil’s area A is shrinking. What is the magnitude of ΔA/Δt, which is the rate (in m2/s) at which the area changes?
73. E CHALK SSM Review Conceptual Example 9 as an aid in understand- ing this problem. A long, straight wire lies on a table and carries a current I. As the drawing shows, a small circular loop of wire is pushed across the
top of the table from position 1 to position 2. Determine the direction of
the induced current, clockwise or counterclockwise, as the loop moves past
(a) position 1 and (b) position 2. Justify your answers.
PROBLEM 73
I
Table top
1
2
74. E In some places, insect “zappers,” with their blue lights, are a familiar sight on a summer’s night. These devices use a high voltage to electrocute
insects. One such device uses an ac voltage of 4320 V, which is obtained
from a standard 120.0-V outlet by means of a transformer. If the primary coil
has 21 turns, how many turns are in the secondary coil?
75. E SSM Available in WileyPLUS. 76. M GO At its normal operating speed, an electric fan motor draws only 15.0% of the current it draws when it just begins to turn the fan blade. The
fan is plugged into a 120.0-V socket. What back emf does the motor generate
at its normal operating speed?
77. M V-HINT Parts a and b of the drawing show the same uniform and con- stant (in time) magnetic fi eld B→ directed perpendicularly into the paper over a rectangular region. Outside this region, there is no fi eld. Also shown is a
rectangular coil (one turn), which lies in the plane of the paper. In part a the long side of the coil (length = L) is just at the edge of the fi eld region, while
in part b the short side (width = W) is just at the edge. It is known that L/W = 3.0. In both parts of the drawing the coil is pushed into the fi eld with the same
velocity v→ until it is completely within the fi eld region. The magnitude of the average emf induced in the coil in part a is 0.15 V. What is its magnitude in part b?
PROBLEM 77
B (into paper)
L
(a) (b)
W vv
78. M V-HINT Indicate the direction of the electric fi eld between the plates of the parallel plate capacitor shown in the drawing if the magnetic fi eld is
decreasing in time. Give your reasoning.
PROBLEM 78
B (out of paper)
Capacitor
79. M SSM A piece of copper wire is formed into a single circular loop of radius 12 cm. A magnetic fi eld is oriented parallel to the normal to the loop,
and it increases from 0 to 0.60 T in a time of 0.45 s. The wire has a resistance
per unit length of 3.3 × 10−2 Ω/m. What is the average electrical energy dis-
sipated in the resistance of the wire?
80. M Available in WileyPLUS. 81. H Available in WileyPLUS. 82. H Available in WileyPLUS. 83. M GO SSM A long solenoid of length 8.0 × 10−2 m and cross-sectional area 5.0 × 10−5 m2 contains 6500 turns per meter of length. Determine the
emf induced in the solenoid when the current in the solenoid changes from
0 to 1.5 A during the time interval from 0 to 0.20 s.
Additional Problems
In this chapter we have seen that there are three ways to create an induced
emf in a coil: by changing the magnitude of a magnetic fi eld, by changing
the direction of the fi eld relative to the coil, and by changing the area of the
coil. Problem 84 explores the third method and, in the process, provides a
review of Faraday’s law of electromagnetic induction. Problem 85 explores
the characteristics of the emf produced in a generator that utilizes a coil
rotating in a fi xed magnetic fi eld.
84. M CHALK A circular coil of radius 0.11 m contains a single turn and is located in a constant magnetic fi eld of magnitude 0.27 T. The magnetic
fi eld has the same direction as the normal to the plane of the coil. The radius
increases to 0.30 m in a time of 0.080 s. Concepts: (i) Why is there an emf induced in the coil? (ii) Does the magnitude of the induced emf depend on
whether the area is increasing or decreasing? Explain. (iii) What determines
the amount of current induced in the coil? (iv) If the coil is cut so it is no
longer one continuous piece, are there an induced emf and an induced cur-
rent? Explain. Calculations: (a) Determine the magnitude of the emf induced in the coil. (b) The coil has a resistance of 0.70 Ω. Find the magnitude of the induced current.
Concepts and Calculations Problems
660 CHAPTER 22 Electromagnetic Induction
85. M CHALK SSM The graph in the fi gure shows the emf produced by a generator as a function of time t. The coil for the generator has an area of A = 0.15 m2 and consists of N = 10 turns. The coil rotates in a fi eld of magnitude 0.27 T. Concepts: (i) Can the period of the rotating coil be determined from the graph? (ii) The emf produced by a generator depends on its angular frequency.
How is the angular frequency of the coil related to its period? (iii) Starting at
t = 0 s, how much time is required for the generator to produce its peak emf? Express the answer in terms of the period T of the motion (e.g., t = (0.1) T). (iv) How often does the polarity of the emf change in one cycle? Calcula- tions: (a) Determine the period of the motion. (b) What is the angular fre- quency of the rotating coil? (c) Find the value of the emf when t = 14 T , where T denotes the period of the coil motion. (d) What is the emf when t = 0.025 s?
t (s) 0 0.030 0.060
ℰ (V
)
PROBLEM 85
86. M Reconfi guring a Transformer. You and your team are exploring an abandoned science facility on the coast of western Antarctica when a large
storm hits, and it is clear that you will be stuck there for a few days. You and
the others search for supplies and fi nd a generator and a tank of fuel. Hav-
ing electrical power would allow you to keep your communication devices
operational and make your stay more comfortable. A team member gets the
generator running, but there is a complication: The output of the generator is
50 Hz at 440 VAC (RMS), and your devices require 60 Hz, 110 VAC (RMS).
The electrical power in many European countries runs on 240 V at 50 Hz, so
a few of your team members have converters. However, 440 V is still too high
to use them. You search and eventually fi nd a large transformer that, accord-
ing to a worn tag on its case, is designed to step down from 5000 V to 880 V.
The tag also indicates that its primary coil has 1500 turns, but you cannot
read the number of turns in the secondary coil. (a) How many turns should its secondary coil have? (b) It will be a diffi cult job, but you can change the number of primary turns by cutting some of them out. How many turns
should you leave on the primary coil so that, with the primary connected to
440 V, the secondary outputs 240 V (so that you can use the 240 V to 110 V
converters)? (c) You fi nd that the current at the source (i.e., that connected to the primary) is limited to a maximum of 20.0 A. What is the maximum
current limit through the secondary coil? (d) What is the maximum average power available at the secondary coil?
87. M A Generator Bike. You and your team are designing a generator using a stationary bike to rotate a coil in a uniform magnetic fi eld. The gear-
ing is set up so that the coil rotates 60 times for one complete rotation of the
bike pedals. Therefore, one revolution of the pedals per second results in a
60-Hz alternating current in the coil. The circular coil has 350 turns and a
diameter of 15.0 cm, and its axis of rotation is along its diameter. (a) If a uniform magnetic fi eld is oriented perpendicular to the coil’s axis of rotation
and has a magnitude of B = 0.225 T, what is the peak emf produced by the generator bike? (b) What is the rms emf? (c) To what magnitude should you reduce the fi eld if you want the rms emf to be 110 VAC? (d) Instead of reducing the fi eld, you could use a step-down transformer to reduce the rms
emf to 110 VAC. What should be the ratio of primary to secondary turns of
the transformer coils?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
23.1 Calculate capacitive reactance.
23.2 Calculate inductive reactance.
23.3 Calculate impedance in an RCL circuit.
23.4 Calculate the resonance frequency of an RCL circuit.
23.5 Describe how semiconductor devices operate.
L ar
ry F
re n ch
/S tr
in g er
/G et
ty I
m ag
es
CHAPTER 23
Alternating Current Circuits
This halftime performance by The Who was part of the festivities at Super Bowl XLIV. Without the aid
of alternating current (ac) circuits it would not be possible to stage such entertainment spectaculars. Ac
circuits lie at the heart of all the audio systems used in the performance.
23.1 Capacitors and Capacitive Reactance Our experience with capacitors so far has been in dc circuits. As we have seen in Sec-
tion 20.13, charge fl ows in a dc circuit only for the brief period after the battery voltage
is applied across the capacitor. In other words, charge fl ows only while the capacitor is
charging up. After the capacitor becomes fully charged, no more charge leaves the bat-
tery. However, suppose that the battery connections to the fully charged capacitor were
suddenly reversed. Then charge would fl ow again, but in the reverse direction, until
the battery recharges the capacitor according to the new connections. In an ac circuit
what happens is similar. The polarity of the voltage applied to the capacitor continu-
ally switches back and forth, and, in response, charges fl ow fi rst one way around the
circuit and then the other way. This fl ow of charge, surging back and forth, constitutes
an alternating current. Thus, charge fl ows continuously in an ac circuit containing a
capacitor.
To help set the stage for the present discussion, recall from Section 20.5 that
the rms voltage Vrms across the resistor in a purely resistive ac circuit is related to the rms current Irms by Vrms = IrmsR (Equation 20.14). The resistance R has the same value for any frequency of the ac voltage or current. Figure 23.1 emphasizes this fact by showing that a graph of resistance versus frequency is a horizontal
straight line. 661
R
Frequency, f (Hz)
R es
is ta
nc e,
R (o
hm s)
V0 sin 2 ftπ
FIGURE 23.1 The resistance in a purely resis- tive circuit has the same value at all frequencies.
The maximum emf of the generator is V0.
662 CHAPTER 23 Alternating Current Circuits
For the rms voltage across a capacitor the following expression applies, which is analogous
to Vrms = IrmsR:
Vrms = IrmsXC (23.1)
The term XC appears in place of the resistance R and is called the capacitive reactance. The capacitive reactance, like resistance, is measured in ohms and determines how much rms current exists in a capacitor in response to a given rms voltage across the capacitor. It is found experi-
mentally that the capacitive reactance XC is inversely proportional to both the frequency f and the capacitance C, according to the following equation:
X C = 1
2πfC (23.2)
For a fi xed value of the capacitance C, Figure 23.2 gives a plot of XC versus frequency, accord- ing to Equation 23.2. A comparison of this drawing with Figure 23.1 reveals that a capacitor and a resistor behave diff erently. As the frequency becomes very large, Figure 23.2 shows that XC approaches zero, signifying that a capacitor off ers only a negligibly small opposition to the alternat-
ing current. In contrast, in the limit of zero frequency (i.e., direct current), XC becomes infi nitely large, and a capacitor provides so much opposition to the motion of charges that there is no current.
Example 1 illustrates the use of Equation 23.2 and also demonstrates how frequency and
capacitance determine the amount of current in an ac circuit.
C
Frequency, f (Hz)
Capacitive reactance, XC (ohms)
V0 sin 2 ftπ
FIGURE 23.2 The capacitive reactance XC is inversely proportional to the frequency f according to XC = 1/(2𝜋fC).
EXAMPLE 1 A Capacitor in an Ac Circuit
For the circuit in Figure 23.2, the capacitance of the capacitor is 1.50 𝜇F, and the rms voltage of the generator is 25.0 V. What is the rms current in
the circuit when the frequency of the generator is (a) 1.00 × 102 Hz and (b) 5.00 × 103 Hz?
Reasoning The current can be found from Irms = Vrms/XC, once the capacitive reactance XC is determined. The values for the capacitive reac- tance will refl ect the fact that the capacitor provides more opposition to
the current when the frequency is smaller.
Problem-Solving Insight The capacitive reactance XC is inversely proportional to the frequency f of the voltage, so if the frequency increases by a factor of 50, as in this example, the capacitive reactance decreases by a factor of 50.
Solution (a) At a frequency of 1.00 × 102 Hz, we fi nd
XC = 1
2πfC =
1
2π (1.00 × 102 Hz)(1.50 × 10−6 F) = 1060 Ω (23.2)
Irms = Vrms XC
= 25.0 V
1060 Ω = 0.0236 A (23.1)
(b) When the frequency is 5.00 × 103 Hz, the calculations are similar:
XC = 1
2πfC =
1
2π (5.00 × 103 Hz)(1.50 × 10−6 F) = 21.2 Ω (23.2)
Irms = Vrms XC
= 25.0 V
21.2 Ω = 1.18 A (23.1)
We now consider the behavior of the instantaneous (not rms) voltage and current. For com-
parison, Figure 23.3 shows graphs of voltage and current versus time in a resistive circuit. These graphs indicate that when only resistance is present, the voltage and current are proportional to
each other at every moment. For example, when the voltage increases from A to B on the graph, the current follows along in step, increasing from Aʹ to Bʹ during the same time interval. Like- wise, when the voltage decreases from B to C, the current decreases from Bʹ to Cʹ. For this reason, the current in a resistance R is said to be in phase with the voltage across the resistance.
For a capacitor, this in-phase relation between instantaneous voltage and current does not exist. Interactive Figure 23.4 shows graphs of the ac voltage and current versus time for a circuit that contains only a capacitor. As the voltage increases from A to B, the charge on the capacitor increases and reaches its full value at B. The current, however, is not the same thing as the charge. The current is the rate of fl ow of charge and has a maximum positive value at the start of the
charging process at Aʹ. It is a maximum because there is no charge on the capacitor at the start and hence no capacitor voltage to oppose the generator voltage. When the capacitor is fully charged
at B, the capacitor voltage has a magnitude equal to that of the generator and completely opposes the generator voltage. The result is that the current decreases to zero at Bʹ. While the capacitor voltage decreases from B to C, the charges fl ow out of the capacitor in a direction opposite to that of the charging current, as indicated by the negative current from Bʹ to Cʹ. Thus, voltage and current are not in phase but are, in fact, one-quarter wave cycle out of step, or out of phase. More
R
t
V B
A
C
t
I B´
C ´ Á
V0 sin 2 ftπ
FIGURE 23.3 The instantaneous voltage V and current I in a purely resistive circuit are in phase, which means that they increase and decrease in step with one another.
23.1 Capacitors and Capacitive Reactance 663
specifi cally, assuming that the voltage fl uctuates as V0 sin 2𝜋ft, the current varies as I0 sin (2𝜋ft + 𝜋/2) = I0 cos 2𝜋ft. Since 𝜋/2 radians correspond to 90° and since the current reaches its maximum value before the voltage does, it is said that the current in a capacitor leads the voltage across the capacitor by a phase angle of 90°.
The fact that the current and voltage for a capacitor are 90° out of phase has an important
consequence from the point of view of electric power, since power is the product of current and
voltage. For the time interval between points A and B (or Aʹ and Bʹ) in Interactive Figure 23.4, both current and voltage are positive. Therefore, the instantaneous power is also positive, mean-
ing that the generator is delivering energy to the capacitor. However, during the period between
B and C (or Bʹ and Cʹ), the current is negative while the voltage remains positive, and the power, which is the product of the two, is negative. During this period, the capacitor is returning energy
to the generator. Thus, the power alternates between positive and negative values for equal periods
of time. In other words, the capacitor alternately absorbs and releases energy.
Problem-Solving Insight Consequently, the average power (and, hence, the average energy) used by a capacitor in an ac circuit is zero.
It will prove useful later on to use a model for the voltage and current when analyzing
ac circuits. In this model, voltage and current are represented by rotating arrows, often called
phasors, whose lengths correspond to the maximum voltage V0 and maximum current I0, as Figure 23.5 indicates. These phasors rotate counterclockwise at a frequency f. For a resistor, the phasors are co-linear as they rotate (see part a of the drawing) because voltage and current are in phase. For a capacitor (see part b), the phasors remain perpendicular while rotating because the phase angle between the current and the voltage is 90°. Since current leads voltage for a capaci-
tor, the current phasor is ahead of the voltage phasor in the direction of rotation.
Note from the two circuit drawings in Figure 23.5 that the instantaneous voltage across the resistor or the capacitor is V0 sin 2𝜋ft. We can fi nd this instantaneous value of the voltage directly from the phasor diagram. Imagine that the voltage phasor V0 in this diagram represents the hypotenuse of a right triangle. Then, the vertical component of the phasor would be V0 sin 2𝜋ft. In a similar manner, the instantaneous current can be found as the vertical component of the current phasor.
Check Your Understanding
(The answer is given at the end of the book.) 1. One circuit contains only an ac generator and a resistor, and the rms current in this circuit is IR. Another
circuit contains only an ac generator and a capacitor, and the rms current in this circuit is IC. The maxi- mum, or peak, voltage of the generator is the same in both circuits and does not change. If the frequency
of each generator is tripled, by what factor does the ratio IR/IC change? Specify whether the change is an increase or a decrease.
C
B
Voltage Current
A C
B´
C ´
Á
t
V0 sin 2 ftπ
INTERACTIVE FIGURE 23.4 In a circuit containing only a capacitor, the instantaneous
voltage and current are not in phase. Instead,
the current leads the voltage by one-quarter of a cycle or by a phase angle of 90°.
Math Skills Why does I0 sin (2πf t + π 2 ) = I0 cos 2π f t? To see why, consider the trigonometric identity sin (α + β) = sin α cos β + cos α sin β (see Appendix E.2, Other Trigonometric Identities,
Equation 6). Using 𝛼 = 2𝜋ft and β = π 2
in this identity, we fi nd that
I0 sin (2πf + π 2 ) = I0 sin 2πft cos π 2
+ I0 cos 2πft sin π 2
But π 2
radians corresponds to 90°, so that cos π 2
= 0 and sin π 2
= 1. With these two substitutions,
we have
I0 sin (2πf t + π 2 ) = I0 cos 2πf t
0
{
1
{
V0
I0
R
Voltage phasor
Current phasor
V0
I0
C
90°
(a)
(b)
2 ftπ
2 ft
V0 sin 2 ftπ
V0 sin 2 ftπ
π
FIGURE 23.5 These rotating-arrow models (or phasor models) represent the voltage and
the current in ac circuits that contain (a) only a resistor and (b) only a capacitor.
664 CHAPTER 23 Alternating Current Circuits
23.2 Inductors and Inductive Reactance As Section 22.8 discusses, an inductor is usually a coil of wire, and the basis of its operation is
Faraday’s law of electromagnetic induction. According to Faraday’s law, an inductor develops a
voltage that opposes a change in the current. This voltage V is given by V = −L(ΔI/Δt) (see Equa- tion 22.9*), where ΔI/Δt is the rate at which the current changes and L is the inductance of the inductor. In an ac circuit the current is always changing, and Faraday’s law can be used to show
that the rms voltage across an inductor is
Vrms = Irms XL (23.3)
Equation 23.3 is analogous to Vrms = IrmsR, with the term XL appearing in place of the resistance R and being called the inductive reactance. The inductive reactance is measured in ohms and determines how much rms current exists in an inductor for a given rms voltage across the induc-
tor. It is found experimentally that the inductive reactance XL is directly proportional to the fre- quency f and the inductance L, as indicated by the following equation:
XL = 2πfL (23.4)
This relation indicates that the larger the inductance, the larger is the inductive reactance. Note
that the inductive reactance is directly proportional to the frequency (XL ∝ f ), whereas the capaci- tive reactance is inversely proportional to the frequency (XC ∝ 1/f ).
Figure 23.6 shows a graph of the inductive reactance versus frequency for a fi xed value of the inductance, according to Equation 23.4. As the frequency becomes very large, XL also becomes very large. In such a situation, an inductor provides a large opposition to the alternating
current. In the limit of zero frequency (i.e., direct current), XL becomes zero, indicating that an inductor does not oppose direct current at all. The next example demonstrates the eff ect of induc-
tive reactance on the current in an ac circuit.
L
Frequency, f (Hz)
Inductive reactance, XL (ohms)
V0 sin 2 ftπ
FIGURE 23.6 In an ac circuit the inductive reactance XL is directly proportional to the frequency f, according to XL = 2𝜋fL.
*When an inductor is used in a circuit, the notation is simplifi ed if we designate the potential diff erence across the
inductor as the voltage V, rather than the emf ℰ.
EXAMPLE 2 An Inductor in an Ac Circuit
The circuit in Figure 23.6 contains a 3.60-mH inductor. The rms voltage of the generator is 25.0 V. Find the rms current in the circuit when the
generator frequency is (a) 1.00 × 102 Hz and (b) 5.00 × 103 Hz. Reasoning The current can be calculated from Irms = Vrms/XL, provided the inductive reactance is obtained fi rst. The inductor off ers more opposi-
tion to the changing current when the frequency is larger, and the values
for the inductive reactance will refl ect this fact.
Problem-Solving Insight The inductive reactance XL is directly proportional to the frequency f of the voltage. If the frequency increases by a factor of 50, as here, the inductive reactance also increases by a factor of 50.
Solution (a) At a frequency of 1.00 × 102 Hz, we fi nd
XL = 2πfL = 2π (1.00 × 102 Hz)(3.60 × 10−3 H) = 2.26 Ω (23.4)
Irms = Vrms XL
= 25.0 V
2.26 Ω = 11.1 A (23.3)
(b) The calculation is similar when the frequency is 5.00 × 103 Hz:
XL = 2πfL = 2π (5.00 × 103 Hz)(3.60 × 10−3 H) = 113 Ω (23.4)
Irms = Vrms XL
= 25.0 V
113 Ω = 0.221 A (23.3)
Due to its inductive reactance, an inductor aff ects the amount of current in an ac circuit. The
inductor also infl uences the current in another way, as Interactive Figure 23.7 shows. This fi gure displays graphs of voltage and current versus time for a circuit containing only an inductor. At a
maximum or minimum on the current graph, the current does not change much with time, so the
voltage generated by the inductor to oppose a change in the current is zero. At the points on the cur-
rent graph where the current is zero, the graph is at its steepest, and the current has the largest rate of
increase or decrease. Correspondingly, the voltage generated by the inductor to oppose a change in
the current has the largest positive or negative value. Thus, current and voltage are not in phase but are
one-quarter of a wave cycle out of phase. If the voltage varies as V0 sin 2𝜋ft, the current fl uctuates as I0 sin (2𝜋ft − 𝜋/2) = −I0 cos 2𝜋ft. The current reaches its maximum after the voltage does, and it is said
23.3 Circuits Containing Resistance, Capacitance, and Inductance 665
that the current in an inductor lags behind the voltage by a phase angle of 90° (𝜋/2 radians). In a purely capacitive circuit, in contrast, the current leads the voltage by 90° (see Interactive Figure 23.4).
In an inductor the 90° phase diff erence between current and voltage leads to the same result
for average power that it does in a capacitor. An inductor alternately absorbs and releases energy
for equal periods of time.
Problem-Solving Insight Thus, the average power (and, hence, the average energy) used by an inductor in an ac circuit is zero.
As an alternative to the graphs in Interactive Figure 23.7, Figure 23.8 uses phasors to describe the instantaneous voltage and current in a circuit containing only an inductor. The volt-
age and current phasors remain perpendicular as they rotate, because there is a 90° phase angle
between them. The current phasor lags behind the voltage phasor, relative to the direction of
rotation, in contrast to the equivalent picture in Figure 23.5b for a capacitor. Once again, the instantaneous values are given by the vertical components of the phasors.
Check Your Understanding
(The answer is given at the end of the book.) 2. CYU Figure 23.1 shows three ac circuits: one contains a resistor, one a capacitor, and one an inductor.
The frequency of each ac generator is reduced to one-half its initial value. Which circuit experiences
(a) the greatest increase in current and (b) the least change in current?
V0 sin 2 ftπ V0 sin 2 ftπ V0 sin 2 ftπ
R C L
CYU FIGURE 23.1
23.3 Circuits Containing Resistance, Capacitance, and Inductance Capacitors and inductors can be combined along with resistors in a single circuit. The simplest
combination contains a resistor, a capacitor, and an inductor in series, as Figure 23.9 shows. In a series RCL circuit the total opposition to the fl ow of charge is called the impedance of the circuit and comes partially from (1) the resistance R, (2) the capacitive reactance XC, and (3) the inductive reactance XL. It is tempting to follow the analogy of a series combination of resistors and calculate the impedance by simply adding together R, XC, and XL. However, such a procedure is not correct. Instead, the phasors shown in Figure 23.10 must be used. The lengths of the voltage phasors in this drawing represent the maximum voltages VR, VC, and VL across the resistor, the capacitor, and the inductor, respectively. The current is the same for each device, since the circuit is wired in
series. The length of the current phasor represents the maximum current I0. Notice that the draw- ing shows the current phasor to be (1) in phase with the voltage phasor for the resistor, (2) ahead
of the voltage phasor for the capacitor by 90°, and (3) behind the voltage phasor for the inductor by
90°. These three facts are consistent with our earlier discussion in Sections 23.1 and 23.2.
The basis for dealing with the voltage phasors in Figure 23.10 is Kirchhoff ’s loop rule. In an ac circuit this rule applies to the instantaneous voltages across each circuit component and the generator. Therefore, it is necessary to take into account the fact that these voltages do not have the same phase;
that is, the phasors VR, VC, and VL point in diff erent directions in the drawing. Kirchhoff ’s loop rule indicates that the phasors add together to give the total voltage V0 that is supplied to the circuit by the generator. The addition, however, must be like a vector addition, to take into account the diff erent
directions of the phasors. Since VL and VC point in opposite directions, they combine to give a resultant
Voltage Current
t
L
V0 sin 2 ftπ
INTERACTIVE FIGURE 23.7 The instan- taneous voltage and current in a circuit
containing only an inductor are not in phase.
The current lags behind the voltage by one- quarter of a cycle or by a phase angle of 90°.
V0
I0
2 ftπ
90°
L
V0 sin 2 ftπ
FIGURE 23.8 This phasor model represents the voltage and current in a circuit that contains
only an inductor.
LCR
V0 sin 2 ftπ
FIGURE 23.9 A series RCL circuit contains a resistor, a capacitor, and an inductor.
666 CHAPTER 23 Alternating Current Circuits
phasor of VL − VC, as Figure 23.11 shows. In this drawing the resultant VL − VC is perpendicular to VR and may be combined with it to give the total voltage V0. Using the Pythagorean theorem, we fi nd
V 20 = V 2R + (VL − VC)2
In this equation each of the symbols stands for a maximum voltage and when divided by √2
gives the corresponding rms voltage. Therefore, it is possible to divide both sides of the equation
by (√2 )2 and obtain a result for Vrms = V0/ √2. This result has exactly the same form as that above, but involves the rms voltages VR-rms, VC-rms, and VL-rms. However, to avoid such awkward symbols, we simply interpret VR, VC, and VL as rms quantities in the following expression:
V 2rms = VR2 + (VL − VC ) 2 (23.5)
The last step in determining the impedance of the circuit is to remember that
VR = IrmsR, VC = IrmsXC, and VL = IrmsXL. With these substitutions Equation 23.5 can be written as
Vrms = Irms √R2 + (XL − XC )2
Therefore, for the entire RCL circuit, it follows that
Vrms = IrmsZ (23.6)
where the impedance Z of the circuit is defi ned as
Series RCL combination Z = √R
2 + (XL − XC )2 (23.7)
The impedance of the circuit, like R, XC, and XL, is measured in ohms. In Equation 23.7, XL = 2𝜋fL and XC = 1/(2𝜋fC).
The phase angle between the current in and the voltage across a series RCL combination is
the angle 𝜙 between the current phasor I0 and the voltage phasor V0 in Figure 23.11. According to Figure 23.11, the tangent of this angle is
tan ϕ = VL − VC
VR =
IrmsXL − IrmsXC IrmsR
Series RCL combination tan ϕ =
XL − XC R
(23.8)
VR
VL
VC
I0
LCR
90°
90°
VR VC VL
V0 sin 2 ftπ
FIGURE 23.10 The three voltage phasors (VR, VC, and VL) and the current phasor (I0) for a series RCL circuit.
FIGURE 23.11 This simplifi ed version of Figure 23.10 results when the phasors VL and VC, which point in opposite directions, are combined to give a resultant of VL − VC.
VR
V0
VL – VC I0ϕ
Math Skills To see why tan ϕ = VL − VC
VR , remember that the tangent function is defi ned as
tan ϕ = ho ha
(Equation 1.3). As shown in Figure 23.12a, ho is the length of the side of a right triangle
opposite the angle 𝜙, and ha is the length of the side adjacent to the angle 𝜙. Figure 23.11 shows the angle 𝜙 as the phase angle between the current phasor I0 and the voltage phasor V0 and is reproduced in Figure 23.12b. The corresponding right triangles are shaded in Figure 23.12, and a comparison reveals that ho = VL − VC and ha = VR. It follows that
tan ϕ = ho ha
= VL − VC
VR
ϕ ha
ho
(a)
VR
V0
VL – VC I0ϕ
(b)
FIGURE 23.12 Math Skills drawing.
23.3 Circuits Containing Resistance, Capacitance, and Inductance 667
The phase angle 𝜙 is important because it has a major eff ect on the average power P deliv- ered to the circuit. Remember that, on the average, only the resistance consumes power; that is,
P = I 2 rms R (Equation 20.15b). According to Figure 23.11, cos 𝜙 = VR/V0 = (Irms R)/(IrmsZ) = R/Z, so that R = Z cos 𝜙. Therefore,
P = I 2rms Z cos ϕ = Irms (IrmsZ ) cos ϕ
P = IrmsVrms cos ϕ (23.9)
where Vrms = IrmsZ is the rms voltage of the generator, according to Equation 23.6. The term cos 𝜙 is called the power factor of the circuit. As a check on the validity of Equation 23.9, note that if no resistance is present, R = 0 Ω, and cos 𝜙 = R/Z = 0. Consequently, P = IrmsVrms cos 𝜙 = 0, a result that is expected since, on the average, neither a capacitor nor an inductor consumes energy.
Conversely, if only resistance is present, Z = √R2 + (XL − XC )2 = R, and cos 𝜙 = R/Z = 1. In this case, P = IrmsVrms cos 𝜙 = IrmsVrms, which is the expression for the average power delivered to a resistor. Examples 3 and 4 deal with the current, voltages, and power for a series RCL circuit.
Analyzing Multiple-Concept Problems
EXAMPLE 3 Current in a Series RCL Circuit
A series RCL circuit contains a 148-Ω resistor, a 1.50-𝜇F capacitor, and
a 35.7-mH inductor. The generator has a frequency of 512 Hz and an rms
voltage of 35.0 V. Determine the rms current in the circuit.
Reasoning The rms current in the circuit is equal to the rms voltage of the generator divided by the impedance of the circuit, according to Equa-
tion 23.6. The impedance of the circuit can be found from the resistance
of the resistor and the reactances of the capacitor and the inductor via
Equation 23.7. The reactances of the capacitor and the inductor can be
found with the aid of Equations 23.2 and 23.4.
Knowns and Unknowns The following table summarizes the data that we have:
Description Symbol Value Comment Resistance of resistor R 148 Ω
Capacitance of capacitor C 1.50 𝜇F 1 𝜇F = 10−6 F
Inductance of inductor L 35.7 mH 1 mH = 10−3 H
Frequency of generator f 512 Hz
Rms voltage of generator Vrms 35.0 V
Unknown Variable Rms current in circuit Irms ?
Modeling the Problem
STEP 1 Current According to Equation 23.6, the rms voltage Vrms of the generator, the rms current Irms, and the impedance Z of the circuit are related according to
Vrms = IrmsZ
Solving for the current gives Equation 1 at the right, in which Vrms is known. The impedance is unknown, but it can be dealt with as in Step 2.
STEP 2 Impedance For a series RCL circuit, the impedance Z is related to the resistance R, the inductive reactance XL, and the capacitive reactance XC, according to
Z = √R2 + (XL − XC)2 (23.7)
As indicated at the right, this expression can be substituted into Equation 1. The resistance is
given, and we turn to Step 3 to deal with the reactances.
Irms = Vrms Z
(1)
?
Irms = Vrms Z
(1)
Z = √R2 + (XL − XC)2 (23.7)
?
⏟⎵⏟⎵⏟
668 CHAPTER 23 Alternating Current Circuits
EXAMPLE 4 Voltages and Power in a Series RCL Circuit
For the series RCL circuit discussed in Example 3, the resistance, capaci-
tance, and inductance are R = 148 Ω, C = 1.50 𝜇F, and L = 35.7 mH, respectively. The generator has a frequency of 512 Hz and an rms voltage
of 35.0 V. In Example 3, it is found that the rms current in the circuit is
Irms = 0.201 A. Find (a) the rms voltage across each circuit element and (b) the average electric power delivered by the generator. Reasoning The rms voltages across each circuit element can be deter- mined from VR = IrmsR, VC = IrmsXC, and VL = IrmsXL. In these expressions, the rms current is known. The resistance R is given, and the capacitive reactance XC and inductive reactance XL can be determined from Equa- tions 23.2 and 23.4. The average power delivered to the circuit by the
generator is specifi ed by Equation 23.9.
Solution (a) The individual reactances are
XC = 1
2πfC =
1
2π (512 Hz)(1.50 × 10−6 F) = 207 Ω (23.2)
XL = 2πfL = 2π(512 Hz)(35.7 × 10−3 H) = 115 Ω (23.4)
The rms voltages across each circuit element are
VR = Irms R = (0.201 A)(148 Ω) = 29.7 V (20.14)
VC = Irms XC = (0.201 A)(207 Ω) = 41.6 V (23.1)
VL = Irms XL = (0.201 A)(115 Ω) = 23.1 V (23.3)
Observe that these three voltages do not add up to give the generator’s
rms voltage of 35.0 V. Instead, the rms voltages satisfy Equation 23.5. It
is the sum of the instantaneous voltages across R, C, and L that equals the generator’s instantaneous voltage, according to Kirchhoff ’s loop rule. The rms voltages do not satisfy the loop rule.
Math Skills The sum of the three voltages calculated in Example 4 is
VR + VC + VL = 29.7 V + 41.6 V + 23.1 V = 94.4 V
Since the rms voltage of the generator is 35.0 V in Example 4, the
voltages VR, VC, and VL (respectively across the resistor, the capaci- tor, and the inductor) in a series RCL circuit clearly do not add up
to give the rms voltage of the generator. However, they do satisfy
V 2rms = V 2R + (VL − VC) 2 (Equation 23.5). You can use this fact to check the correctness of your calculations in problems such as that
in the example. For instance, using VR = 29.7 V, VC = 41.6 V, and VL = 23.1 V in Equation 23.5, we fi nd
V 2 rms = V R2 + (VL − VC ) 2 = (29.7 V) 2 + (23.1 V − 41.6 V) 2
Vrms = √(29.7 V) 2 + (23.1 V − 41.6 V) 2 = 35.0 V
This result confi rms the correctness of the calculations in Example 4,
since the rms voltage of the generator is, in fact, 35.0 V.
STEP 3 Inductive and Capacitive Reactances The inductive reactance XL and the capacitive reactance XC are given, respectively, by Equation 23.4 and Equation 23.2 as
XL = 2πf L and XC = 1
2πf C
where L is the inductance, C is the capacitance, and f is the frequency. Using these two expres- sions, we fi nd that
XL − XC = 2πfL − 1
2πf C
This result can now be substituted into Equation 23.7, as shown at the right.
Solution Combining the results of each step algebraically, we fi nd that
Irms = Vrms Z
= Vrms
√R 2 + (XL − XC) 2 =
Vrms
√R2 + (2πfL − 1 2πf C ) 2
The rms current in the circuit is
Irms = Vrms
√R 2 + (2πf L − 1 2π f C ) 2
= 35.0 V
√(148 Ω)2 + [2π(512 Hz)(35.7 × 10−3 H) − 1 2π(512 Hz)(1.50 × 10−6 F) ] 2
= 0.201 A
Related Homework: Problem 19
STEP 1 STEP 2 STEP 2
Irms = Vrms Z
(1)
Z = √R2 + (XL − XC)2 (23.7)
XL − XC = 2πfL − 1
2πf C
⏟⎵⏟⎵⏟
23.3 Circuits Containing Resistance, Capacitance, and Inductance 669
In addition to the series RCL circuit, there are many diff erent ways to connect resistors,
capacitors, and inductors. In analyzing these additional possibilities, it helps to keep in mind the
behavior of capacitors and inductors at the extreme limits of the frequency. When the frequency
approaches zero (i.e., dc conditions), the reactance of a capacitor becomes so large that no charge
can fl ow through the capacitor. It is as if the capacitor were cut out of the circuit, leaving an open
gap in the connecting wire. In the limit of zero frequency the reactance of an inductor is vanish-
ingly small. The inductor off ers no opposition to a dc current and behaves as if it were replaced
with a wire of zero resistance. In the limit of very large frequency, the behaviors of a capacitor
and an inductor are reversed. The capacitor has a very small reactance and off ers little opposition
to the current, as if it were replaced by a wire with zero resistance. In contrast, the inductor has
a very large reactance when the frequency is very large. The inductor off ers so much opposition
to the current that it might as well be cut out of the circuit, leaving an open gap in the connecting
wire. Conceptual Example 5 illustrates how to gain insight into more complicated circuits using
the limiting behaviors of capacitors and inductors.
(b) The average power delivered by the generator is P = IrmsVrms cos ϕ (Equation 23.9). Therefore, a value for the phase angle 𝜙 is needed and can be obtained from Equation 23.8 as follows:
tan ϕ = XL − XC
R or ϕ = tan−1 (
XL − XC R )
= tan−1 (115 Ω − 207 Ω 148 Ω ) = −32°
The phase angle is negative since the circuit is more capacitive than in-
ductive (XC is greater than XL), and the current leads the voltage. The average power delivered by the generator is
P = IrmsVrms cos ϕ = (0.201 A)(35.0 V) cos (−32°) = 6.0 W
This amount of power is delivered only to the resistor, since neither the
capacitor nor the inductor uses power, on average.
CONCEPTUAL EXAMPLE 5 The Limiting Behavior of Capacitors and Inductors
Figure 23.13a shows two circuits. The rms voltage of the generator is the same in each case. The values of the resistance R, the capacitance C, and the inductance L in these circuits are the same. The frequency of the ac generator is very nearly zero. In which circuit does the generator supply
more rms current, (a) circuit I or (b) circuit II?
Reasoning According to Equation 23.6, the rms current is given by Irms = Vrms/Z. However, the impedance Z cannot be obtained from Equation 23.7, since the circuits in Figure 23.13a are not series RCL circuits. Since Vrms is the same in each case, the greater current is delivered to the circuit with
the smaller impedance Z. In the limit of very small frequencies, the capaci- tors have very large impedances and, thus, allow very little current to fl ow
through them. In essence, the capacitors behave as if they were cut out of the
circuit, leaving gaps in the connecting wires. On the other hand, in the limit
of very small frequencies, the inductors have very small impedances and
behave as if they were replaced by wires with zero resistance. Figure 23.13b shows the circuits as they would appear according to these changes.
Answer (a) is incorrect. According to Figure 23.13b, circuit I behaves as if it contained only two identical resistors wired in series, with a total
impedance of Z = R + R = 2R. In contrast, circuit II behaves as if it con- tained two identical resistors wired in parallel, in which case the total
impedance is given by 1/Z = 1/R + 1/R = 2/R, or Z = R/2. Circuit I contains the greater impedance, so the generator supplies less, not more,
rms current to that circuit.
Answer (b) is correct. The rms current Irms in a circuit is given by Irms = Vrms/Z. Since Vrms is the same for both circuits and circuit II has the smaller impedance [see the explanation for why Answer (a) is incorrect],
its generator supplies the greater rms current.
Related Homework: Check Your Understanding 7, 8, Problem 46
Circuit II
(a)
LR
L R
C
Circuit II (Low-frequency limit)
(b)
R
R
CR
C R L
Circuit I
(a)
R
R
Circuit I (Low-frequency limit)
(b)
FIGURE 23.13 (a) These circuits are discussed in the limit of very small or low frequency in
Conceptual Example 5. (b) For a frequency very near zero, the circuits in part a behave as if they were as shown here.
670 CHAPTER 23 Alternating Current Circuits
BIO THE PHYSICS OF . . . body-fat scales. The impedance of an ac circuit contains important information about the resistance, capacitance, and inductance in the circuit. As an
example of a very complex circuit, consider the human body. It contains muscle, which is a rela-
tively good conductor of electricity due to its high water content, and also fat, which is a relatively
poor conductor due to its low water content. The impedance that the body off ers to ac electricity
is referred to as bioelectrical impedance and is largely determined by resistance and capacitive
reactance. Capacitance enters the picture because cell membranes can act like tiny capacitors.
Bioelectric impedance analysis provides the basis for the determination of body-fat percentage
by the body-fat scales (see Figure 23.14) that are widely available for home use. When you stand barefoot on such a scale, electrodes beneath your feet send a weak ac current (approximately
800 𝜇A, 50 kHz) through your lower body in order to measure your body’s impedance. The scale
also measures your weight. A built-in computer combines the impedance and weight with infor-
mation you provide about height, age, and sex to determine the percentage of fat in your body to
an accuracy of about 5%. For men (age 20 to 39) a percentage of 8 to 19% is considered average,
whereas the corresponding range of values for women of similar ages is 21 to 33%.
BIO THE PHYSICS OF . . . transcutaneous electrical nerve stimulation (TENS). Weak ac electricity with a much lower frequency than that used to measure bioelectrical impedance is
used in a technique called transcutaneous electrical nerve stimulation (TENS). TENS is the most
commonly used form of electroanalgesia in pain-management situations and, in its conventional
form, uses an ac frequency between 40 and 150 Hz. Ac current is passed between two electrodes
attached to the body and inhibits the transmission of pain-related nerve impulses. The technique
is thought to work by aff ecting the “gates” in a nerve cell that control the passage of sodium
ions into and out of the cell (see Section 19.6). Figure 23.15 shows TENS being applied during assessment of pain control following suspected damage to the radial nerve in the forearm.
Check Your Understanding
(The answers are given at the end of the book.) 3. A long wire of fi nite resistance is connected to an ac generator. The wire is then wound into a coil of
many loops and reconnected to the generator. Is the current in the circuit with the coil greater than, less
than, or the same as the current in the circuit with the uncoiled wire?
4. A light bulb and a parallel plate capacitor (containing a dielectric material between the plates) are con- nected in series to the 60-Hz ac voltage present at a wall outlet. When the dielectric material is removed
from the space between the plates, does the brightness of the bulb increase, decrease, or remain the same?
5. An air-core inductor is connected in series with a light bulb, and this circuit is plugged into an ac electrical outlet. When a piece of iron is inserted inside the inductor, does the brightness of the bulb
increase, decrease, or remain the same?
6. Consider the circuit in Figure 23.9. With the capacitor and the inductor present, a certain amount of current is in the circuit. Then the capacitor and the inductor are removed, so that only the resistor
remains connected to the generator. Is it possible that, under a certain condition, the current in the sim-
plifi ed circuit has the same rms value as in the original circuit? (a) No (b) Yes, when XL = R (c) Yes, when XC = R (d) Yes, when XC = XL
7. Review Conceptual Example 5 as an aid in understanding this question. An inductor and a capacitor are connected in parallel across the terminals of an ac generator. Does the current from the generator
decrease, remain the same, or increase as the frequency becomes (a) very large and (b) very small? 8. Review Conceptual Example 5 as an aid in understanding this question. For which of the two circuits
discussed there does the generator deliver more current when the frequency is very large? (a) Circuit I (b) Circuit II
23.4 Resonance in Electric Circuits The behavior of the current and voltage in a series RCL circuit can give rise to a condition of reso- nance. Resonance occurs when the frequency of a vibrating force exactly matches a natural (reso- nant) frequency of the object to which the force is applied. When resonance occurs, the force can
Electrodes for heels
Electrodes for balls of feet
FIGURE 23.14 Bathroom scales are now widely available that can provide estimates
of your body-fat percentage. When you stand
barefoot on the scale, electrodes beneath your
feet send a small ac current through your
lower body that allows the body’s electrical
impedance to be measured. This impedance
is correlated with the percentage of fat in the
body.
Electrodes
FIGURE 23.15 Transcutaneous electrical nerve stimulation (TENS) is shown here being
applied to the forearm, in an assessment of
pain control following suspected damage to
the radial nerve.
Martin Dohrn/SPL/Science Source
23.4 Resonance in Electric Circuits 671
transmit a large amount of energy to the object, leading to a large- amplitude vibratory motion. We
have already encountered several instances of resonance. For example, resonance can occur when
a vibrating force acts on an object of mass m that is attached to a spring whose spring constant is k (Section 10.6). In this case there is one natural frequency f0, whose value is f 0 = [1/(2π)] √k /m. Resonance also occurs when standing waves are set up on a string (Section 17.5) or in a tube of
air (Section 17.6). The string and tube of air have many natural frequencies, one for each allowed
standing wave. As we will now see, a condition of resonance can also be established in a series
RCL circuit. In this case there is only one natural frequency, and the vibrating force is provided by
the oscillating electric fi eld that is related to the voltage of the generator.
Animated Figure 23.16 helps us understand why a resonant frequency exists for an ac cir- cuit. This drawing presents an analogy between the electrical case (ignoring resistance) and the
mechanical case of an object attached to a horizontal spring (ignoring friction). Part a shows a fully stretched spring that has just been released, and the initial speed 𝜐 of the object is zero. All the energy is stored in the form of elastic potential energy. When the object begins to move, it
gradually loses potential energy and gains kinetic energy. In part b, the object moves with speed 𝜐max and maximum kinetic energy through the position where the spring is unstretched (zero poten- tial energy). Because of its inertia, the moving object coasts through this position and eventually
comes to a halt in part c when the spring is fully compressed and all kinetic energy has been con- verted back into elastic potential energy. Part d of the picture is like part b, except that the direction of motion is reversed. The resonant frequency f0 of the object on the spring is the natural frequency at which the object vibrates and is given as f 0 = [1/(2π)] √k /m according to Equations 10.6 and 10.11. In this expression, m is the mass of the object, and k is the spring constant.
In the electrical case, Animated Figure 23.16a begins with a fully charged capacitor that has just been connected to an inductor. At this instant the energy is stored in the electric fi eld
between the capacitor plates. As the capacitor discharges, the electric fi eld E →
between the plates
decreases, while a magnetic fi eld B →
builds up around the inductor because of the increasing
current in the circuit. The maximum current and the maximum magnetic fi eld exist at the instant
when the capacitor is completely discharged, as in part b of the fi gure. Energy is now stored entirely in the magnetic fi eld of the inductor. The voltage induced in the inductor keeps the
charges fl owing until the capacitor again becomes fully charged, but now with reversed polar-
ity, as in part c. Once again, the energy is stored in the electric fi eld between the plates, and no energy resides in the magnetic fi eld of the inductor. Part d of the cycle repeats part b, but with reversed directions of current and magnetic fi eld. Thus, an ac circuit can have a resonant
frequency because there is a natural tendency for energy to shuttle back and forth between the
electric fi eld of the capacitor and the magnetic fi eld of the inductor.
To determine the resonant frequency at which energy shuttles back and forth between the
capacitor and the inductor, we note that the current in a series RCL circuit is Irms = Vrms/Z (Equation 23.6). In this expression Z is the impedance of the circuit and is given by Z = √R2 + (XL − XC)2 (Equation 23.7). As Figure 23.17 illustrates, the rms current is a maximum when the impedance
+ + + +
– – – –
E + + + +
– – – –
E
Imax B ImaxB max
= 0 m/s
maxυ
υ
υ
υ = 0 m/s
Position when spring is unstretched
Position when spring is unstretched
PE
(a)
PE
(c)
KE
(b)
KE
(d )
ANIMATED FIGURE 23.16 The oscillation of an object on a spring is analogous to the oscillation of the electric and magnetic fi elds that occur, respectively, in a capacitor and in an inductor. (PE, potential energy;
KE, kinetic energy.)
f
Impedance Z
rms current
f0
FIGURE 23.17 In a series RCL circuit the impedance is a minimum, and the current is
a maximum, when the frequency f equals the resonant frequency f0 of the circuit.
672 CHAPTER 23 Alternating Current Circuits
is a minimum, assuming a given generator voltage. The minimum impedance of Z = R occurs when the frequency is f0, such that XL = XC or 2𝜋f0L = 1/(2𝜋f0C). This result can be solved for f0, which is the resonant frequency:
f0 = 1
2π √LC (23.10)
The resonant frequency is determined by the inductance and the capacitance, but not the
resistance.
The eff ect of resistance on electrical resonance is to make the “sharpness” of the circuit
response less pronounced, as Figure 23.18 indicates. When the resistance is small, the current– frequency graph falls off suddenly on either side of the maximum current. When the resistance is
large, the falloff is more gradual, and there is less current at the maximum.
Check Your Understanding
(The answers are given at the end of the book.) 9. The resistance in a series RCL circuit is doubled. (a) Does the resonant frequency increase, decrease, or
remain the same? (b) Does the maximum current in the circuit increase, decrease, or remain the same? 10. In a series RCL circuit at resonance, does the current lead or lag behind the voltage across the generator,
or is the current in phase with the voltage?
11. Is it possible for two series RCL circuits to have the same resonant frequencies and yet have (a) diff er- ent R values and (b) diff erent C and L values?
12. Suppose the generator connected to a series RCL circuit has a frequency that is greater than the reso- nant frequency of the circuit. Suppose, in addition, that it is necessary to match the resonant frequency
of the circuit to the frequency of the generator. To accomplish this, should you add a second capacitor
(a) in series or (b) in parallel with the one already present?
23.5 Semiconductor Devices Semiconductor devices such as diodes and transistors are widely used in modern electronics, and
Figure 23.19 illustrates one application. The drawing shows an audio system in which small ac voltages (originating in a compact disc player, an FM tuner, or a cassette deck) are amplifi ed so
they can drive the speaker(s). The electric circuits that accomplish the amplifi cation do so with
the aid of a dc voltage provided by the power supply. In portable units the power supply is simply
a battery. In nonportable units, however, the power supply is a separate electric circuit containing
diodes, along with other elements. As we will see, the diodes convert the 60-Hz ac voltage pres-
ent at a wall outlet into the dc voltage needed by the amplifi er, which, in turn, performs its job of
amplifi cation with the aid of transistors.
f
Small resistance
Large resistance
Irms
f0
FIGURE 23.18 The eff ect of resistance on the current in a series RCL circuit.
Power supply
Diodes
60-Hz ac voltage from wall socket
Dc voltage
Cassette deck
FM tuner
Transistors
Amplifier
Speaker(s)
Compact disc player
FIGURE 23.19 In a typical audio system, diodes are used in the power supply to create
a dc voltage from the ac voltage present at
the wall socket. This dc voltage is necessary
so the transistors in the amplifi er can perform
their task of enlarging the small ac voltage
(in blue) originating in the compact disc
player, or other device.
23.5 Semiconductor Devices 673
n-Type and p-Type Semiconductors The materials used in diodes and transistors are semiconductors, such as silicon and germanium.
However, they are not pure materials because small amounts of “impurity” atoms (about one
part in a million) have been added to them to change their conductive properties. For instance,
Figure 23.20a shows an array of atoms that symbolizes the crystal structure in pure silicon. Each silicon atom has four outer-shell* electrons, and each electron participates with electrons from
neighboring atoms in forming the bonds that hold the crystal together. Since they participate in
forming bonds, these electrons generally do not move throughout the crystal. Consequently, pure
silicon and germanium are not good conductors of electricity. It is possible, however, to increase
their conductivities by adding tiny amounts of impurity atoms, such as phosphorus or arsenic,
whose atoms have fi ve outer-shell electrons. For example, when a phosphorus atom replaces a
silicon atom in the crystal, only four of the fi ve outer-shell electrons of phosphorus fi t into the
crystal structure. The extra fi fth electron does not fi t in and is relatively free to diff use through-
out the crystal, as part b of the drawing suggests. A semiconductor containing small amounts of phosphorus can therefore be envisioned as containing immobile, positively charged phosphorus
atoms and a pool of electrons that are free to wander throughout the material. These mobile elec-
trons allow the semiconductor to conduct electricity.
The process of adding impurity atoms is called doping. A semiconductor doped with an impurity that contributes mobile electrons is called an n-type semiconductor, since the mobile charge carriers have a negative charge. Note that an n-type semiconductor is overall electrically neutral, since it contains equal numbers of positive and negative charges.
It is also possible to dope a silicon crystal with an impurity whose atoms have only three
outer-shell electrons (e.g., boron or gallium). Because of the missing fourth electron, there is a
“hole” in the lattice structure at the boron atom, as Figure 23.20c illustrates. An electron from a neighboring silicon atom can move into this hole, in which event the region around the boron
atom, having acquired the electron, becomes negatively charged. Of course, when a nearby elec-
tron does move, it leaves behind a hole. This hole is positively charged, since it results from the
removal of an electron from the vicinity of a neutral silicon atom. The vast majority of atoms in
the lattice are silicon, so the hole is almost always next to another silicon atom. Consequently,
an electron from one of these adjacent atoms can move into the hole, with the result that the hole
moves to yet another location. In this fashion, a positively charged hole can wander through the
crystal. This type of semiconductor can, therefore, be viewed as containing immobile, negatively
charged boron atoms and an equal number of positively charged, mobile holes. Because of the
mobile holes, the semiconductor can conduct electricity. In this case the charge carriers are posi-
tive. A semiconductor doped with an impurity that introduces mobile positive holes is called a p-type semiconductor.
The Semiconductor Diode THE PHYSICS OF . . . a semiconductor diode. A p-n junction diode is a device that is formed from a p-type semiconductor and an n-type semiconductor. The p-n junction between the two materials is of fundamental importance to the operation of diodes and transistors. Figure 23.21
*Section 30.6 discusses the electronic structure of the atom in terms of “shells.”
(a) Pure material
Extra electron diffuses about
Silicon atom
(b) n-type material
(c) p-type material
Outer-shell electron
Immobile phosphorus (positively charged)
Positive hole diffuses about
Immobile boron (negatively charged)
FIGURE 23.20 A silicon crystal that is (a) undoped, or pure, (b) doped with phosphorus to produce an n-type material, and (c) doped with boron to produce a p-type material.
Mobile positively charged holes
Immobile negative charges
Mobile negative electrons
p-type n-type
Immobile positive charges
+
–
+
–
+
–
+
–
+
–
+
–
–
+
–
+
–
+
–
+
–
+
–
+
FIGURE 23.21 A p-type semiconductor and an n-type semiconductor.
674 CHAPTER 23 Alternating Current Circuits
shows separate p-type and n-type semiconductors, each electrically neutral. Figure 23.22a shows them joined together to form a diode. Mobile electrons from the n-type semiconductor and mobile holes from the p-type semiconductor fl ow across the junction and combine. This process leaves the n-type material with a positive charge layer and the p-type material with a negative charge layer, as part b of the drawing indicates. The positive and negative charge layers on the two sides of the junction set up an electric fi eld E
→ , much like the fi eld in a parallel plate capacitor. This
electric fi eld tends to prevent any further movement of charge across the junction, and all charge
fl ow quickly stops.
Suppose now that a battery is connected across the p-n junction, as in Figure 23.23a, where the negative terminal of the battery is attached to the n-material, and the positive terminal is attached to the p-material. In this situation the junction is said to be in a condition of forward bias, and, as a result, there is a current in the circuit. The negative terminal of the battery repels the mobile electrons in the n-type material, and they move toward the junction. Likewise, the positive terminal repels the positive holes in the p-type material, and they also move toward the junction. At the junction the electrons fi ll the holes. In the meantime, the negative terminal pro-
vides a fresh supply of electrons to the n-material, and the positive terminal pulls off electrons from the p-material, forming new holes in the process. Consequently, a continual fl ow of charge, and hence a current, is maintained.
In Figure 23.23b the battery polarity has been reversed, and the p-n junction is in a condition known as reverse bias. The battery forces electrons in the n-material and holes in the p-material away from the junction. As a result, the potential across the junction builds up until it opposes the
battery potential, and very little current can be sustained through the diode. The diode, then, is a
unidirectional device, for it allows current to pass in only one direction.
The graph in Figure 23.24 shows the dependence of the current on the magnitude and polar- ity of the voltage applied across a p-n junction diode. The exact values of the current depend on the nature of the semiconductor and the extent of the doping. Also shown in the drawing is
the symbol used for a diode ( ). The direction of the arrowhead in the symbol indicates the direction of the conventional current in the diode under a forward-bias condition. In a forward-
bias condition, the side of the symbol that contains the arrowhead has a positive potential relative
to the other side.
p-type n-type
(a)
+
–
+
–
+
–
+
–
+
–
+
–
–
+
–
+
–
+
–
+
–
+
–
+
p-type n-type
Charge layers
(b)
+
+
+
+
–
+
–
+
–
–
+
–
+
–
+
–
E
–
E
–
E
FIGURE 23.22 At the junction between n and p materials, (a) mobile electrons and holes combine and
(b) create positive and negative charge layers. The electric fi eld produced by
the charge layers is E→.
p-type n-type
I
I
(a) Forward bias
Conventional current
+
+ +
+
+
–
– –
– –
+ –
p-type n-type
(b) Reverse bias
+
+
+
+
+
–
–
–
– –
+
+ + + + +
– – – – –
–
FIGURE 23.23 There is an appreciable current through the diode when the diode is forward- biased. (b) Under a reverse-bias condition, there is almost no current through the diode.
V (volts)
I (mA)
Reverse bias
20
–1.0 –0.5 +0.5 +1.0
10
30
+–
Forward bias
+ –
FIGURE 23.24 The current–voltage characteristics of a typical p-n junction diode.
23.5 Semiconductor Devices 675
THE PHYSICS OF . . . light-emitting diodes (LEDs). A special kind of diode is called an LED, which stands for light-emitting diode. You can see LEDs in the form of small bright red, green, or yellow lights that appear on most electronic devices, such as computers, TV sets, and
audio systems. These diodes, like others, carry current in only one direction. Imagine a forward-
biased diode, like that shown in Figure 23.23a, in which a current exists. An LED emits light whenever electrons and holes combine, the light coming from the p-n junction. Commercial LEDs are often made from gallium, suitably doped with arsenic and phosphorus atoms.
BIO THE PHYSICS OF . . . a fetal oxygen monitor. A fetal oxygen monitor uses LEDs to measure the level of oxygen in a fetus’s blood. A sensor is inserted into the mother’s uterus
and positioned against the cheek of the fetus, as indicated in Figure 23.25. Two LEDs are located within the sensor, and each shines light of a diff erent wavelength (or color) into the fetal tissue.
The light is refl ected by the oxygen-carrying red blood cells and is detected by an adjacent pho-
todetector. Light from one of the LEDs is used to measure the level of oxyhemoglobin in the
blood, and light from the other LED is used to measure the level of deoxyhemoglobin. From a
comparison of these two levels, the oxygen saturation in the blood is determined.
THE PHYSICS OF . . . rectifi er circuits. Because diodes are unidirectional devices, they are commonly used in rectifi er circuits, which convert an ac voltage into a dc voltage. For
instance, Figure 23.26 shows a circuit in which charges fl ow through the resistance R only while the ac generator biases the diode in the forward direction. Since current occurs only during
one-half of every generator voltage cycle, the circuit is called a half-wave rectifi er. A plot of the output voltage across the resistor reveals that only the positive halves of each cycle are present.
If a capacitor is added in parallel with the resistor, as indicated in Figure 23.26, the capacitor charges up and keeps the voltage from dropping to zero between each positive half-cycle. It is
also possible to construct full-wave rectifi er circuits, in which both halves of every cycle of the generator voltage drive current through the load resistor in the same direction (see Check Your
Understanding Question 13).
When a circuit such as the one in Figure 23.26 includes a capacitor and also a transformer to establish the desired voltage level, the circuit is called a power supply. In the audio system in Figure 23.19, the power supply receives the 60-Hz ac voltage from a wall socket and produces a dc output voltage that is used for the transistors within the amplifi er. Power supplies using diodes
are also found in virtually all electronic appliances, such as televisions and microwave ovens.
Time
Diode
C R
Generator voltage
Output voltage
Without capacitor
With capacitor
Time
FIGURE 23.26 A half-wave rectifi er circuit, together with a capacitor and a transformer (not shown), constitutes a dc power supply because the rectifi er converts an ac voltage into a dc voltage.
Sensor
FIGURE 23.25 A fetal oxygen monitor uses a sensor that contains LEDs to measure the
level of oxygen in the blood of an unborn child. © 2
0 0 4 , 2 0 1 1 N
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676 CHAPTER 23 Alternating Current Circuits
Solar Cells THE PHYSICS OF . . . solar cells. Solar cells use p-n junctions to convert sunlight directly into electricity, as Figure 23.27 illustrates. The solar cell in this drawing consists of a p-type semi- conductor surrounding an n-type semiconductor. As discussed earlier, charge layers form at the junction between the two types of semiconductors, leading to an electric fi eld E
→ pointing from
the n-type toward the p-type layer. The outer covering of p-type material is so thin that sunlight penetrates into the charge layers and ionizes some of the atoms there. In the process of ionization,
the energy of the sunlight causes a negative electron to be ejected from the atom, leaving behind
a positive hole. As the drawing indicates, the electric fi eld in the charge layers causes the electron
and the hole to move away from the junction. The electron moves into the n-type material, and the hole moves into the p-type material. As a result, the sunlight causes the solar cell to develop negative and positive terminals, much like the terminals of a battery. The current that a single
solar cell can provide is small, so applications of solar cells often use many of them mounted to
form large panels, as Figure 23.28 illustrates.
Transistors THE PHYSICS OF . . . transistors. A number of diff erent kinds of transistors are in use today. One type is the bipolar-junction transistor, which consists of two p-n junctions formed by three layers of doped semiconductors. As Figure 23.29 indicates, there are pnp and npn transistors. In either case, the middle region is made very thin compared to the outer regions.
A transistor is useful because it can be used in circuits that amplify a smaller voltage into
a larger one. A transistor plays the same kind of role in an amplifi er circuit that a valve does
when it controls the fl ow of water through a pipe. A small change in the valve setting pro-
duces a large change in the amount of water per second that fl ows through the pipe. Similarly,
a small change in the voltage input to a transistor produces a large change in the output from
the transistor.
Figure 23.30 shows a pnp transistor connected to two batteries, labeled VE and VC. The voltages VE and VC are applied in such a way that the p-n junction on the left has a forward bias, while the p-n junction on the right has a reverse bias. Moreover, the voltage VC is usually much larger than VE for a reason to be discussed shortly. The drawing also shows the standard symbol and nomenclature for the three sections of the pnp transistor—namely, the emitter, the base, and the collector. The arrow in the symbol points in the direction of the conventional current through the emitter.
The positive terminal of VE pushes the mobile positive holes in the p-type material of the emitter toward the emitter/base junction. Since this junction has a forward bias, the holes enter
the base region readily. Once in the base region, the holes come under the strong infl uence of
–
–
+
+
p-type
n-type
Charge layers
E
+ terminal – terminal
= hole = electron
FIGURE 23.27 A solar cell formed from a p-n junction. When sunlight strikes it, the solar cell acts like a battery, with + and −
terminals.
FIGURE 23.28 This boat, the PlanetSolar, is powered by the electrical energy generated
by approximately 500 m2 of solar cells that
cover its top surface. It was built by the ship-
yard of Knierim Yachtbau in Kiel, Germany.
CHRISTIAN CHARISIUS/Reuters/Landov LLC
p-type p-type
pnp transistor
n-type
n-type n-type
npn transistor
p-type
FIGURE 23.29 There are two kinds of bipolar-junction transistors, pnp and npn.
FIGURE 23.30 A pnp transistor, along with its bias voltages VE and VC. On the symbol for the pnp transistor at the right, the emitter is marked with an arrow that denotes the direction of conventional current
through the emitter.
Forward-biased junction Reverse-biased junction
Symbol for a pnp transistor
Emitter Collector
Emitter Collector
Base
Base
p-type n-type p-type
IC
VCVE
IB IE
+ –+ –
23.5 Semiconductor Devices 677
VC and are attracted to its negative terminal. Since the base is so thin (about 10−6 m or so), approximately 98% of the holes are drawn through the base and into the collector. The remain-
ing 2% of the holes combine with free electrons in the base region, thereby giving rise to a small
base current IB. As the drawing shows, the moving holes in the emitter and collector constitute currents that are labeled IE and IC, respectively. From Kirchhoff ’s junction rule it follows that IC = IE − IB.
Because the base current IB is small, the collector current is determined primarily by current from the emitter (IC = IE − IB ≈ IE). This means that a change in IE will cause a change in IC of nearly the same amount. Furthermore, a substantial change in IE can be caused by only a small change in the forward-bias voltage VE. To see that this is the case, look at Figure 23.24 and notice how steep the current–voltage curve is for a p-n junction: small changes in the forward-bias volt- age give rise to large changes in the current.
With the help of Interactive Figure 23.31 we can now appreciate what was meant by the earlier statement that a small change in the voltage input to a transistor leads to a large change
in the output. This picture shows an ac generator connected in series with the battery VE and a resistance R connected in series with the collector. The generator voltage could originate from many sources, such as an electric guitar pickup or a compact disc player, while the resistance R could represent a loudspeaker. The generator introduces small voltage changes in the forward
bias across the emitter/base junction and, thus, causes large corresponding changes in the current
leaving the collector and passing through the resistance R. As a result, the output voltage across R is an enlarged or amplifi ed version of the input voltage of the generator. The operation of an npn transistor is similar to that of a pnp transistor. The main diff erence is that the bias voltages and current directions are reversed.
It is important to realize that the increased power available at the output of a transistor
amplifi er does not come from the transistor itself. Rather, it comes from the power provided by the voltage source VC. The transistor, acting like an automatic valve, merely allows the small signals from the input generator to control the power taken from the source VC and delivered to the resistance R.
Today it is possible to combine arrays of billions of transistors, diodes, resistors, and capaci-
tors on a tiny chip of silicon that usually measures less than a centimeter on a side. These arrays
are called integrated circuits (ICs) and can be designed to perform almost any desired electronic function. Integrated circuits, such as the type in Figure 23.32, have revolutionized the electronics industry and lie at the heart of computers, cellular phones, digital watches, and programmable
appliances.
Emitter Collector
Generator voltage
Output voltage
Time
Time
Base
p-type n-type p-type
VCVE
+ –+ –
R
INTERACTIVE FIGURE 23.31 The basic pnp transistor amplifi er in this drawing amplifi es a small generator voltage to produce an enlarged voltage across the resistance R.
FIGURE 23.32 Integrated circuit (IC) chips are manufactured on wafers of semiconductor
material. Shown here is one wafer containing
many chips.
Adam Hart-Davis/Science Source
678 CHAPTER 23 Alternating Current Circuits
Check Your Understanding
(The answer is given at the end of the book.) 13. CYU Figure 23.2 shows a full-wave rectifi er circuit, in which the
direction of the current through the load resistor R is the same for both positive and negative halves of the generator’s voltage cycle.
What is the direction of the current through the resistor (left to right,
or right to left) when (a) the top of the generator is positive and the bottom is negative and (b) the top of the generator is negative and the bottom is positive?
R
CYU FIGURE 23.2
EXAMPLE 6 BIO The Physics of Nuclear Magnetic Resonance—NMR
In Chapter 21 we described the medical diagnostic technique of magnetic
resonance imaging, or MRI. This technique is based on the more funda-
mental principle of nuclear magnetic resonance, or NMR. Here, nuclei
in the substance under study will absorb and re-emit radio waves when
placed in a strong magnetic fi eld. They do this by rotating at a frequency
that is typically hundreds of MHz. A pickup coil detects the AC voltage
created by the rotating nuclei, and diff erent nuclei will produce a dif-
ferent characteristic frequency. Consider an NMR spectrometer that is
confi gured with a pickup coil designed to detect one particular resonant
frequency. This occurs because the coil is part of an RLC circuit with a capacitance of 9.4 × 10−16 F. If the inductance of the pickup coil is
7.5 mH, what is the resonant frequency of the coil?
Reasoning In an RLC circuit, the resonance frequency depends on the value of the circuit’s capacitance and inductance, as given by Equation
23.10. We can use this relationship to calculate the frequency.
Solution Applying Equation 23.10, we have:
f0 = 1
2π√LC =
1
2π√(0.0075 H)(9.4 × 10−16 F) = 6.0 × 107 Hz
= 60 MHz
Concept Summary 23.1 Capacitors and Capacitive Reactance In an ac circuit the rms voltage Vrms across a capacitor is related to the rms current Irms by Equation 23.1, where XC is the capacitive reactance. The capacitive reactance is measured in ohms (Ω) and is given by Equation 23.2, where f is the frequency and C is the capacitance. The ac current in a capacitor leads the voltage across the
capacitor by a phase angle of 90° or 𝜋/2 radians. As a result, a capacitor con-
sumes no power, on average.
Vrms = Irms XC (23.1)
The phasor model is useful for analyzing the voltage and current in an
ac circuit. In this model, the voltage and current are represented by rotat-
ing arrows, called phasors. The length of the voltage phasor represents the
maximum voltage V0, and the length of the current phasor represents the maximum current I0. The phasors rotate in a counterclockwise direction at a frequency f. Since the current leads the voltage by 90° in a capacitor, the cur- rent phasor is ahead of the voltage phasor by 90° in the direction of rotation.
The instantaneous values of the voltage and current are equal to the vertical
components of the corresponding phasors.
XC = 1
2πfC (23.2)
23.2 Inductors and Inductive Reactance In an ac circuit the rms voltage Vrms across an inductor is related to the rms current Irms by Equation 23.3, where XL is the inductive reactance. The inductive reactance is measured in ohms (Ω) and is given by Equation 23.4, where f is the frequency and
L is the inductance. The ac current in an inductor lags behind the voltage across the inductor by a phase angle of 90° or 𝜋/2 radians. Consequently, an
inductor, like a capacitor, consumes no power, on average.
Vrms = Irms XL (23.3) XL = 2πfL (23.4)
The voltage and current phasors in a circuit containing only an inductor also
rotate in a counterclockwise direction at a frequency f. However, since the current lags the voltage by 90° in an inductor, the current phasor is behind the voltage
phasor by 90° in the direction of rotation. The instantaneous values of the voltage
and current are equal to the vertical components of the corresponding phasors.
23.3 Circuits Containing Resistance, Capacitance, and Inductance When a resistor, a capacitor, and an inductor are connected in series, the rms
voltage across the combination is related to the rms current according to Equa-
tion 23.6, where Z is the impedance of the combination. The impedance is measured in ohms (Ω) and is given by Equation 23.7, where R is the resistance, and XL and XC are, respectively, the inductive and capacitive reactances.
Vrms = IrmsZ (23.6)
Z = √R2 + (XL − XC )2 (23.7)
The tangent of the phase angle 𝜙 between current and voltage in a series
RCL circuit is given by Equation 23.8.
tan ϕ = XL − XC
R (23.8)
Focus on Concepts 679
Only the resistor in the RCL combination consumes power, on average.
The average power P consumed in the circuit is given by Equation 23.9, where cos 𝜙 is called the power factor of the circuit.
P = Irms Vrms cos ϕ (23.9)
23.4 Resonance in Electric Circuits A series RCL circuit has a reson- ant frequency f0 that is given by Equation 23.10, where L is the inductance and C is the capacitance. At resonance, the impedance of the circuit has a minimum value equal to the resistance R, and the rms current has a max- imum value.
f 0 = 1
2π√LC (23.10)
23.5 Semiconductor Devices In an n-type semiconductor, mobile negat- ive electrons carry the current. An n-type material is produced by doping a semiconductor such as silicon with a small amount of impurity atoms such
as phosphorus. In a p-type semiconductor, mobile positive “holes” in the crystal structure carry the current. A p-type material is produced by doping a semiconductor with a small amount of impurity atoms such as boron. These
two types of semiconductors are used in p-n junction diodes, light-emitting diodes, solar cells, and pnp and npn bipolar junction transistors.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 23.1 Capacitors and Capacitive Reactance 1. A circuit contains an ac generator and a resistor. What happens to the average power dissipated in the resistor when the frequency is doubled and
the rms voltage is tripled? (a) Nothing happens, because the average power does not depend on either the frequency or the rms voltage. (b) The average power doubles because it is proportional to the frequency. (c) The average power triples because it is proportional to the rms voltage. (d) The average power increases by a factor of 32 = 9 because it is proportional to the square
of the rms voltage. (e) The average power increases by a factor of 2 × 3 = 6 because it is proportional to the product of the frequency and the rms voltage.
Section 23.2 Inductors and Inductive Reactance 4. What happens to the capacitive reactance XC and the inductive reactance XL if the frequency of the ac voltage is doubled? (a) XC increases by a factor of 2, and XL decreases by a factor of 2. (b) XC and XL both increase by a factor of 2. (c) XC and XL do not change. (d) XC and XL both decrease by a factor of 2. (e) XC decreases by a factor of 2, and XL increases by a factor of 2. 8. Each of the four phasor diagrams represents a diff erent circuit. V0 and I0 represent, respectively, the maximum voltage of the generator and the current
in the circuit. Which circuit contains only a resistor? (a) A (b) B (c) C (d) D
V0 V0
I0
90°
A
I0
90°
B
QUESTION 8
V0 V0I0
C
I0
D
Section 23.3 Circuits Containing Resistance, Capacitance, and Inductance 11. The table shows the rms voltage VC across the capacitor and the rms voltage VL across the inductor for three series RCL circuits. In which circuit does the rms voltage across the entire RCL combination lead the current
through the combination? (a) Circuit 1 (b) Circuit 2 (c) Circuit 3 (d) The total rms voltage across the RCL combination does not lead the current in
any of the circuits.
Circuit VC VL 1 50 V 100 V
2 100 V 50 V
3 50 V 50 V
15. A capacitor and an inductor are connected to an ac generator in two ways: in series and in parallel (see the drawing). At low frequencies, which
circuit has the greater current? (a) The series circuit, because the impedance of the circuit is small due to the small reactances of both the inductor and
the capacitor. (b) The series circuit, because the impedance of the circuit is large due to the large reactances of both the inductor and the capacitor.
(c) The parallel circuit, because the impedance of the circuit is small due to the large reactance of the inductor. (d) The parallel circuit, because the impedance of the circuit is large due to the large reactance of the inductor.
(e) The parallel circuit, because the impedance of the circuit is small due to the small reactance of the inductor.
QUESTION 15
L C
Series
L
C
Parallel
Section 23.4 Resonance in Electric Circuits 18. In an RCL circuit a second capacitor is added in parallel to the capa- citor already present. Does the resonant frequency of the circuit increase,
decrease, or remain the same? (a) The resonant frequency increases, because it depends inversely on the square root of the capacitance, and the equivalent
capacitance decreases when a second capacitor is added in parallel. (b) The resonant frequency increases, because it is directly proportional to the capa-
citance, and the equivalent capacitance increases when a second capacitor is
Focus on Concepts
680 CHAPTER 23 Alternating Current Circuits
added in parallel. (c) The resonant frequency decreases, because it is directly proportional to the capacitance, and the equivalent capacitance decreases
when a second capacitor is added in parallel. (d) The resonant frequency
decreases, because it depends inversely on the square root of the capacitance,
and the equivalent capacitance increases when a second capacitor is added in
parallel. (e) The resonant frequency remains the same.
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
Note: For problems in this set, the ac current and voltage are rms values, and the power is an average value, unless indicated otherwise.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 23.1 Capacitors and Capacitive Reactance 1. E SSM A 63.0-𝜇F capacitor is connected to a generator operating at a low frequency. The rms voltage of the generator is 4.00 V and is constant.
A fuse in series with the capacitor has negligible resistance and will burn
out when the rms current reaches 15.0 A. As the generator frequency is in-
creased, at what frequency will the fuse burn out?
2. E GO Two identical capacitors are connected in parallel to an ac gen- erator that has a frequency of 610 Hz and produces a voltage of 24 V. The
current in the circuit is 0.16 A. What is the capacitance of each capacitor?
3. E The reactance of a capacitor is 68 Ω when the ac frequency is 460 Hz. What is the reactance when the frequency is 870 Hz?
4. E GO A capacitor is connected to an ac generator that has a frequency of 3.4 kHz and produces a voltage of 2.0 V. The current in the capacitor is
35 mA. When the same capacitor is connected to a second ac generator that
has a frequency of 5.0 kHz, the current in the capacitor is 85 mA. What
voltage does the second generator produce?
5. E SSM A capacitor is connected across the terminals of an ac generator that has a frequency of 440 Hz and supplies a voltage of 24 V. When a second
capacitor is connected in parallel with the fi rst one, the current from the gen-
erator increases by 0.18 A. Find the capacitance of the second capacitor.
6. M CHALK GO Two parallel plate capacitors are identical, except that one of them is empty and the other contains a material with a dielectric constant of
4.2 in the space between the plates. The empty capacitor is connected between
the terminals of an ac generator that has a fi xed frequency and rms voltage.
The generator delivers a current of 0.22 A. What current does the generator
deliver after the other capacitor is connected in parallel with the fi rst one?
7. M V-HINT A capacitor is connected across an ac generator whose fre- quency is 750 Hz and whose peak output voltage is 140 V. The rms current in the circuit is 3.0 A. (a) What is the capacitance of the capacitor? (b) What is the magnitude of the maximum charge on one plate of the capacitor? 8. H A capacitor (capacitance C1) is connected across the terminals of an ac generator. Without changing the voltage or frequency of the generator, a
second capacitor (capacitance C2) is added in series with the fi rst one. As a result, the current delivered by the generator decreases by a factor of three.
Suppose that the second capacitor had been added in parallel with the fi rst
one, instead of in series. By what factor would the current delivered by the
generator have increased?
Section 23.2 Inductors and Inductive Reactance 9. E SSM An 8.2-mH inductor is connected to an ac generator (10.0 V rms, 620 Hz). Determine the peak value of the current supplied by the generator. 10. E An inductor has an inductance of 0.080 H. The voltage across this inductor is 55 V and has a frequency of 650 Hz. What is the current in the
inductor?
11. E An inductor is to be connected to the terminals of a generator (rms voltage = 15.0 V) so that the resulting rms current will be 0.610 A. Determ-
ine the required inductive reactance.
12. E GO An ac generator has a frequency of 7.5 kHz and a voltage of 39 V. When an inductor is connected between the terminals of this generator, the
current in the inductor is 42 mA. What is the inductance of the inductor?
13. E V-HINT A 40.0-𝜇F capacitor is connected across a 60.0-Hz generator. An inductor is then connected in parallel with the capacitor. What is the value
of the inductance if the rms currents in the inductor and capacitor are equal?
14. E GO An ac generator has a frequency of 2.2 kHz and a voltage of 240 V. An inductance L1 = 6.0 mH is connected across its terminals. Then a second inductance L2 = 9.0 mH is connected in parallel with L1. Find the current that the generator delivers to L1 and to the parallel combination. 15. M SSM A 30.0-mH inductor has a reactance of 2.10 kΩ. (a) What is the frequency of the ac current that passes through the inductor? (b) What is the capacitance of a capacitor that has the same reactance at this frequency? The
frequency is tripled, so that the reactances of the inductor and capacitor are
no longer equal. What are the new reactances of (c) the inductor and (d) the capacitor?
16. H Available in WileyPLUS.
Section 23.3 Circuits Containing Resistance, Capacitance, and Inductance 17. E SSM A series RCL circuit includes a resistance of 275 Ω, an induct- ive reactance of 648 Ω, and a capacitive reactance of 415 Ω. The current in
the circuit is 0.233 A. What is the voltage of the generator?
18. E A series RCL circuit contains a 47.0-Ω resistor, a 2.00-𝜇F capacitor, and a 4.00-mH inductor. When the frequency is 2550 Hz, what is the power
factor of the circuit?
19. E SSM Multiple-Concept Example 3 reviews some of the basic ideas that are pertinent to this problem. A circuit consists of a 215-Ω resistor and a
0.200-H inductor. These two elements are connected in series across a gen-
erator that has a frequency of 106 Hz and a voltage of 234 V. (a) What is the current in the circuit? (b) Determine the phase angle between the current and the voltage of the generator.
20. E GO An ac series circuit has an impedance of 192 Ω, and the phase angle between the current and the voltage of the generator is 𝜙 = −75°. The
circuit contains a resistor and either a capacitor or an inductor. Find the
resistance R and the capacitive reactance XC or the inductive reactance XL, whichever is appropriate.
21. E When only a resistor is connected across the terminals of an ac generator (112 V) that has a fi xed frequency, there is a current of 0.500 A in
Problems
Additional Problems 681
the resistor. When only an inductor is connected across the terminals of this
same generator, there is a current of 0.400 A in the inductor. When both the
resistor and the inductor are connected in series between the terminals of this
generator, what are (a) the impedance of the series combination and (b) the phase angle between the current and the voltage of the generator?
22. E GO A 2700-Ω resistor and a 1.1-𝜇F capacitor are connected in series across a generator (60.0 Hz, 120 V). Determine the power delivered to the
circuit.
23. E Available in WileyPLUS. 24. M CHALK GO Part a of the drawing shows a resistor and a charged capacitor wired in series. When the switch is closed, the capacitor discharges
as charge moves from one plate to the other. Part b shows the amount q of charge remaining on each plate of the capacitor as a function of time. In part c of the drawing, the switch has been removed and an ac generator has been
inserted into the circuit. The circuit elements in the drawing have the follow-
ing values: R = 18 Ω, Vrms = 24 V for the generator, and f = 380 Hz for the generator. The time constant for the circuit in part a is 𝜏 = 3.0 × 10−4 s. What is the rms current in the circuit in part c?
R C
t
q R C
+ + –
–
Switch
(c)(b)(a)
PROBLEM 24
25. M SSM A circuit consists of an 85-Ω resistor in series with a 4.0-𝜇F ca- pacitor, and the two are connected between the terminals of an ac generator.
The voltage of the generator is fi xed. At what frequency is the current in the
circuit one-half the value that exists when the frequency is very large?
26. M BIO V-HINT In one measurement of the body’s bioelectric imped- ance, values of Z = 4.50 × 102 Ω and 𝜙 = −9.80° are obtained for the total impedance and the phase angle, respectively. These values assume that the
body’s resistance R is in series with its capacitance C and that there is no inductance L. Determine the body’s resistance and capacitive reactance. 27. M MMH Available in WileyPLUS. 28. M V-HINT An 84.0-mH inductor and a 5.80-𝜇F capacitor are connected in series with a generator whose frequency is 375 Hz. The rms voltage across
the capacitor is 2.20 V. Determine the rms voltage across the inductor.
29. H Available in WileyPLUS.
Section 23.4 Resonance in Electric Circuits 30. E A tank circuit in a radio transmitter is a series RCL circuit connected to an antenna. The antenna broadcasts radio signals at the resonant frequency
of the tank circuit. Suppose that a certain tank circuit in a shortwave radio
transmitter has a fi xed capacitance of 1.8 × 10−11 F and a variable inductance.
If the antenna is intended to broadcast radio signals ranging in frequency
from 4.0 MHz to 9.0 MHz, fi nd the (a) minimum and (b) maximum induct- ance of the tank circuit.
31. E SSM A series RCL circuit has a resonant frequency of 690 kHz. If the value of the capacitance is 2.0 × 10−9 F, what is the value of the inductance?
32. E The power dissipated in a series RCL circuit is 65.0 W, and the current is 0.530 A. The circuit is at resonance. Determine the voltage of the generator.
33. E SSM A 10.0-Ω resistor, a 12.0-𝜇F capacitor, and a 17.0-mH inductor are connected in series with a 155-V generator. (a) At what frequency is the current a maximum? (b) What is the maximum value of the rms current? 34. E GO The capacitance in a series RCL circuit is C1 = 2.60 𝜇F, and the corresponding resonant frequency is f01 = 7.30 kHz. The generator frequency is 5.60 kHz. What is the value of the capacitance C2 that should be added to the circuit so that the circuit will have a resonant frequency that matches the
generator frequency? Note that you must decide whether C2 is added in series or in parallel with C1. 35. E A series RCL circuit is at resonance and contains a variable resistor that is set to 175 Ω. The power delivered to the circuit is 2.6 W. Assuming
that the voltage remains constant, how much power is delivered when the
variable resistor is set to 562 Ω?
36. E GO The resonant frequency of an RCL circuit is 1.3 kHz, and the value of the inductance is 7.0 mH. What is the resonant frequency (in kHz)
when the value of the inductance is 1.5 mH?
37. M A series RCL circuit has a resonant frequency of 1500 Hz. When operating at a frequency other than 1500 Hz, the circuit has a capacitive
reactance of 5.0 Ω and an inductive reactance of 30.0 Ω. What are the values
of (a) L and (b) C? 38. M GO In a series RCL circuit the generator is set to a frequency that is not the resonant frequency. This nonresonant frequency is such that the ratio of the
inductive reactance to the capacitive reactance of the circuit is observed to be
5.36. The resonant frequency is 225 Hz. What is the frequency of the generator?
39. M SSM Available in WileyPLUS. 40. M CHALK GO A charged capacitor and an in- ductor are connected as shown in the drawing (this
circuit is the same as that in Animated Figure 23.16a). There is no resistance in the circuit. As Section 23.4 discusses, the electrical energy initially
present in the charged capacitor then oscillates back
and forth between the inductor and the capacitor. The
initial charge on the capacitor has a magnitude of q = 2.90 𝜇C. The capacitance is C = 3.60 𝜇F, and the inductance is L = 75.0 mH. (a) What is the electrical energy stored initially by the charged capacitor? (b) Find the maximum current in the inductor. 41. M V-HINT In the absence of a nearby metal object, the two inductances (LA and LB) in a heterodyne metal detector are the same, and the resonant frequencies of the two oscillator circuits have the same value of 630.0 kHz.
When the search coil (inductor B) is brought near a buried metal object, a
beat frequency of 7.30 kHz is heard. By what percentage does the buried
object increase the inductance of the search coil?
42. H Available in WileyPLUS.
43. E SSM Available in WileyPLUS. 44. E GO A circuit consists of a resistor in series with an inductor and an ac generator that supplies a voltage of 115 V. The inductive reactance is 52.0 Ω, and
the current in the circuit is 1.75 A. Find the average power delivered to the circuit.
45. E In a series circuit, a generator (1350 Hz, 15.0 V) is connected to a 16.0-Ω resistor, a 4.10-𝜇F capacitor, and a 5.30-mH inductor. Find the
voltage across each circuit element.
Additional Problems
C + + –
–
L
PROBLEM 40
682 CHAPTER 23 Alternating Current Circuits
46. E Review Conceptual Example 5 and Figure 23.13. Find the ratio of the current in circuit I to the current in circuit II in the high-frequency limit for the same generator voltage.
47. E SSM At what frequency (in Hz) are the reactances of a 52-mH in- ductor and a 76-𝜇F capacitor equal?
48. E GO The resistor in a series RCL circuit has a resistance of 92 Ω, while the voltage of the generator is 3.0 V. At resonance, what is the average
power delivered to the circuit?
49. E Two ac generators supply the same voltage. However, the fi rst gener- ator has a frequency of 1.5 kHz, and the second has a frequency of 6.0 kHz.
When an inductor is connected across the terminals of the fi rst generator,
the current delivered is 0.30 A. How much current is delivered when this
inductor is connected across the terminals of the second generator?
50. M V-HINT A series circuit contains only a resistor and an inductor. The voltage V of the generator is fi xed. If R = 16 Ω and L = 4.0 mH, fi nd the fre- quency at which the current is one-half its value at zero frequency.
51. M SSM A series RCL circuit contains a 5.10-𝜇F capacitor and a generator whose voltage is 11.0 V. At a resonant frequency of 1.30 kHz
the power delivered to the circuit is 25.0 W. Find the values
of (a) the inductance and (b) the resistance. (c) Calculate the power factor when the generator frequency is 2.31 kHz.
52. H Available in WileyPLUS. 53. M GO SSM Part a of the fi gure shows a heterodyne metal detector being used. As part b of the fi gure illustrates, this device utilizes two capacitor/ inductor oscillator circuits, A and B. Each produces its own resonant fre-
quency, f0A = 1/[2𝜋(LAC)1/2] and f0B = 1/[2𝜋(LBC)1/2]. Any diff erence between these frequencies is detected through earphones as a beat frequency | f0B − f0A|. In the absence of any nearby metal object, the inductances LA and LB are identical. When inductor B (the search coil) comes near a piece of metal,
the inductance LB increases, the corresponding oscillator frequency f0B de- creases, and a beat frequency is heard. Suppose that initially each inductor
is adjusted so that LB = LA, and each oscillator has a resonant frequency of 855.5 kHz. Assuming that the inductance of search coil B increases by
1.000% due to a nearby piece of metal, determine the beat frequency heard
through the earphones.
(a)
© A
n d re
J en
n y /A
la m
y
Additional circuitry
for oscillator B
f0B
Additional circuitry
for oscillator A
Beat frequency amplifier
Metallic object
Headphones
Oscillator circuit AOscillator circuit B
LB LAC C
f0A
f0B – f0A
(b) PROBLEM 53
A capacitor is one of the important elements found in ac circuits. As we have
seen in this chapter, the capacitance of a capacitor infl uences the amount of
current in a circuit. The capacitance, in turn, is determined by the geometry
of the capacitor and the material that fi lls the space between its plates, as
Section 19.5 discusses. When capacitors are connected together, the equi-
valent capacitance depends on the nature of the connection—for example,
whether it is a series or parallel connection. Problem 54 provides a review
of these issues concerning capacitors. In ac circuits that contain capacitance,
inductance, and resistance, it is only the resistance that, on the average, con-
sumes power. The average power delivered to a capacitor or an inductor is
zero. However, the presence of a capacitor and/or an inductor does infl uence
the rms current in the circuit. When the current changes for any reason, the
power in the resistor also changes, as Problem 55 illustrates.
54. M CHALK Two parallel plate capacitors are fi lled with the same dielec- tric material and have the same plate area. However, the plate separation of
capacitor 1 is twice that of capacitor 2. When capacitor 1 is connected across
the terminals of an ac generator, the generator delivers an rms current of
0.60 A. Concepts: (i) Which of the two capacitors has the greater capacit- ance? (ii) Is the equivalent capacitance of the parallel combination (CP) greater or smaller than the capacitance of capacitor 1? (iii) Is the capacitive
reactance of CP greater or smaller than for C1? (iv) When both capacitors are connected in parallel across the terminals of the generator, is the current from
the generator greater or smaller than when capacitor 1 is connected alone?
Calculations: What is the current delivered by the generator when both capa- citors are connected in parallel across the terminals?
55. M CHALK SSM An ac generator has a frequency of 1200 Hz and a con- stant rms voltage. When a 470-Ω resistor is connected between the ter-
minals of the generator, an average power of 0.25 W is consumed by the
resistor. Then, a 0.080-H inductor is connected in series with the resistor,
and the combination is connected between the generator terminals. Con- cepts: (i) In which case does the generator deliver a greater rms current? (ii) In which case is the greater average power consumed by the circuit?
Calculations: What is the average power consumed in the inductor–resistor series circuit?
Concepts and Calculations Problems
Team Problems 683
56. M A Communications Jammer. Radio jamming is the intentional dis- ruption or interference of radio communications by overwhelming the inten-
ded receivers of the signal with random noise. You and your team have been
tasked with jamming a specifi c radio signal at 720 kHz. You have access to
a high-powered transmitter, but the part of its circuitry that tunes the broad-
cast frequency, called the tank circuit, has been damaged. A tank circuit is
a series RCL circuit whose resonance frequency determines the frequency
broadcasted by the antenna. At your disposal are two 220-Ω resistors, one
variable capacitor that ranges from 2.0 to 6.0 nF, and four inductors with the
following values: L1 = 5.0 × 10−6 H, L2 = 7.2 × 10−6 H, L3 = 6.5 × 10−5 H, and L4 = 5.4 × 10−6 H. (a) If you set your variable capacitor at the center of its range, what must be the value of the inductance of your RCL circuit
so that it resonates at 720 kHz? (b) How should you confi gure the available inductors to give you the needed equivalent inductance? (Hint: the rules for
adding inductors in series and parallel are the same as for resistors.) (c) With the inductance set as calculated in (a), what resonant frequency range does
the variable capacitor provide? (d) The two resistors can be confi gured to give diff erent equivalent resistance values. How should you confi gure the
resistors in the RCL circuit in order to maximize the current at the resonant
frequency? (Refer to Section 23.4.)
57. M A Reconfi gurable RCL Circuit. A series RCL circuit is composed of a resistor (R = 220 Ω), two identical capacitors (C = 3.50 nF) connected in series, and two identical inductors (L = 5.50 × 10−5 H) connected in series. You and your team need to determine: (a) the resonant frequency of this confi guration. (b) What are all of the other possible resonant frequencies that can be attained by reconfi guring the capacitors and inductors (while using all
of the components and keeping the proper series RCL order)? (c) If you were to design a circuit using only one of the given inductors and one adjustable
capacitor, what would the range of the variable capacitor need to be in order
to cover all of the resonant frequencies found in (a) and (b)?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
24.1 Describe the nature of electromagnetic waves.
24.2 Calculate speed, frequency, and wavelength for electromagnetic waves.
24.3 Relate the speed of light to electromagnetic quantities.
24.4 Calculate energy, power, and intensity for electromagnetic waves.
24.5 Solve problems involving the Doppler eff ect for electromagnetic waves.
24.6 Solve polarization problems using Malus’ law.
T er
je R
ak k e/
G et
ty I
m ag
es
CHAPTER 24
Electromagnetic Waves
Each of the colors on the sails of these boats corresponds to a diff erent wavelength in the visible region of
the spectrum of electromagnetic waves. As we will see in this chapter, however, the visible wavelengths
comprise only a small part of the total electromagnetic spectrum.
24.1 The Nature of Electromagnetic Waves In Section 13.3 we saw that energy is transported to us from the sun via a class of
waves known as electromagnetic waves. This class includes the familiar visible, ultra-
violet, and infrared waves. In Sections 18.6, 21.1, and 21.2 we studied the concepts
of electric and magnetic fi elds. It was the great Scottish physicist James Clerk Maxwell
(1831–1879) who showed that these two fi elds fl uctuating together can form a
propagating electromagnetic wave. We will now bring together our knowledge of electric and magnetic fi elds in order to understand this important type of wave.
Animated Figure 24.1 illustrates one way to create an electromagnetic wave. The setup consists of two straight metal wires that are connected to the terminals of an
ac generator and serve as an antenna. The potential diff erence between the terminals
changes sinusoidally with time t and has a period T. Part a shows the instant t = 0 s, when there is no charge at the ends of either wire. Since there is no charge, there is no
electric fi eld at the point P just to the right of the antenna. As time passes, the top wire becomes positively charged and the bottom wire negatively charged. One-quarter of a
cycle later ( t = 14 T ) , the charges have attained their maximum values, as part b of the
684
24.1 The Nature of Electromagnetic Waves 685
drawing indicates. The corresponding electric fi eld E→ at point P is represented by the red arrow and has increased to its maximum strength in the downward direction.* Part b also shows that the electric fi eld created at earlier times (see the black arrow in the picture) has not disappeared but
has moved to the right. Here lies the crux of the matter: At distant points, the electric fi eld of the
charges is not felt immediately. Instead, the fi eld is created fi rst near the wires and then, like the
eff ect of a pebble dropped into a pond, moves outward as a wave in all directions. Only the fi eld
moving to the right is shown in the picture for the sake of clarity.
Parts c–e of Animated Figure 24.1 show the creation of the electric fi eld at point P (red arrow) at later times during the generator cycle. In each part, the fi elds produced earlier in the
sequence (black arrows) continue propagating toward the right. Part d shows the charges on the wires when the polarity of the generator has reversed, so the top wire is negative and the bottom
wire is positive. As a result, the electric fi eld at P has reversed its direction and points upward. In part e of the sequence, a complete sine wave has been drawn through the tips of the electric fi eld vectors to emphasize that the fi eld changes sinusoidally.
Along with the electric fi eld in Animated Figure 24.1, a magnetic fi eld B→ is also created, because the charges fl owing in the antenna constitute an electric current, which produces a mag-
netic fi eld. Figure 24.2 illustrates the fi eld direction at point P at the instant when the current in the antenna wire is upward. With the aid of Right-Hand Rule No. 2 (thumb of the right hand points
along the current I, fi ngers curl in the direction of B→), the magnetic fi eld at P can be seen to point into the page. As the oscillating current changes, the magnetic fi eld changes accordingly. The
magnetic fi elds created at earlier times propagate outward as a wave, just as the electric fi elds do.
Notice that the magnetic fi eld in Figure 24.2 is perpendicular to the page, whereas the elec- tric fi eld in Animated Figure 24.1 lies in the plane of the page. Thus, the electric and magnetic fi elds created by the antenna are mutually perpendicular and remain so as they move outward.
Moreover, both fi elds are perpendicular to the direction of travel. These perpendicular electric
and magnetic fi elds, moving together, constitute an electromagnetic wave.
The electric and magnetic fi elds in Animated Figure 24.1 and Figure 24.2 decrease to zero rapidly with increasing distance from the antenna. Therefore, they exist mainly near the antenna
and together are called the near fi eld. Electric and magnetic fi elds do form a wave at large distances from the antenna, however. These fi elds arise from an eff ect that is diff erent from the one that pro-
duces the near fi eld and are referred to as the radiation fi eld. Faraday’s law of induction provides part of the basis for the radiation fi eld. As Section 22.4 discusses, this law describes the emf or po-
tential diff erence produced by a changing magnetic fi eld. And, as Section 19.4 explains, a potential
diff erence can be related to an electric fi eld. Thus, a changing magnetic fi eld produces an electric
fi eld. Maxwell predicted that the reverse eff ect also occurs—namely, that a changing electric fi eld
produces a magnetic fi eld. The radiation fi eld arises because the changing magnetic fi eld creates an
electric fi eld that fl uctuates in time and the changing electric fi eld creates the magnetic fi eld.
Figure 24.3 shows the electromagnetic wave of the radiation fi eld far from the antenna. The picture shows only the part of the wave traveling along the +x axis. The parts traveling in the other directions have been omitted for clarity. It should be clear from the drawing that
(a) t = 0 s P
(b) t = T
E
P
(c) P
(d) t = T
t = T
P
(e) t = T P
+ +
+ +
––
––
1 4
2 4
3 4
ANIMATED FIGURE 24.1 In each part of the drawing, the red arrow represents the electric
fi eld E→ produced at point P by the oscillating charges on the antenna at the indicated time.
The black arrows represent the electric fi elds
created at earlier times. For simplicity, only
the fi elds propagating to the right are shown.
*The direction of the electric fi eld can be obtained by imagining a positive test charge at P and determining the direction in which it would be pushed because of the charges on the wires.
B
I
P
I
FIGURE 24.2 The oscillating current I in the antenna wires creates a magnetic fi eld B→ at point P that is tangent to a circle centered on the wires. The fi eld is directed as shown
when the current is upward and is directed
in the opposite direction when the current is
downward.
y
z
x
B
E Direction of wave travel
FIGURE 24.3 This picture shows the wave of the radiation fi eld far from the antenna. Observe that E→ and B→ are perpendicular to each other, and both are perpendicular to the direction of travel.
686 CHAPTER 24 Electromagnetic Waves
an electromagnetic wave is a transverse wave because the electric and magnetic fi elds are both perpendicular to the direction in which the wave travels. Moreover, an electromagnetic wave,
unlike a wave on a string or a sound wave, does not require a medium in which to propagate.
Electromagnetic waves can travel through a vacuum or a material substance, since electric and magnetic fi elds can exist in either one.
Electromagnetic waves can be produced in situations that do not involve a wire antenna.
In general, any electric charge that is accelerating emits an electromagnetic wave, whether the
charge is inside a wire or not. In an alternating current, an electron oscillates in simple harmonic
motion along the length of the wire and is one example of an accelerating charge.
All electromagnetic waves move through a vacuum at the same speed, and the symbol c is used to denote its value. This speed is called the speed of light in a vacuum and is c = 3.00 × 108 m/s. In air, electromagnetic waves travel at nearly the same speed as they do in a vacuum, but, in general,
they move through a substance such as glass at a speed that is substantially less than c. The frequency of an electromagnetic wave is determined by the oscillation frequency of the
electric charges at the source of the wave. In Figures 24.1–24.3 the wave frequency would equal the frequency of the ac generator. Suppose, for example, that the antenna is broadcasting electro-
magnetic waves known as radio waves. The frequencies of AM radio waves lie between 545 and
1605 kHz, these numbers corresponding to the limits of the AM broadcast band on the radio dial.
In contrast, frequencies of FM radio waves lie between 88 and 108 MHz on the dial. Television
channels 2–6, on the other hand, utilize electromagnetic waves with frequencies between 54 and
88 MHz, and channels 7–13 use frequencies between 174 and 216 MHz.
THE PHYSICS OF . . . radio and television reception. Radio and television reception involves a process that is the reverse of that outlined earlier for the creation of electromagnetic
waves. When broadcasted waves reach a receiving antenna, they interact with the electric charges
in the antenna wires. Either the electric fi eld or the magnetic fi eld of the waves can be used. To
take full advantage of the electric fi eld, the wires of the receiving antenna must be parallel to the
electric fi eld, as Figure 24.4 indicates. The electric fi eld acts on the electrons in the wire, forcing them to oscillate back and forth along the length of the wire. Thus, an ac current exists in the
antenna and the circuit connected to it. The variable-capacitor C ( ) and the inductor L in the circuit provide one way to select the frequency of the desired electromagnetic wave. By adjusting
the value of the capacitance, it is possible to adjust the corresponding resonant frequency f0 of the circuit [ f 0 = 1/(2π √LC ), Equation 23.10] to match the frequency of the wave. Under the condition of resonance, there will be a maximum oscillating current in the inductor. Because of
mutual inductance, this current creates a maximum voltage in the second coil in the drawing, and
this voltage can then be amplifi ed and processed by the remaining radio or television circuitry.
To detect the magnetic fi eld of a broadcasted radio wave, a receiving antenna in the form of
a loop can be used, as Figure 24.5 shows. For best reception, the normal to the plane of the wire loop must be oriented parallel to the magnetic fi eld. Then, as the wave sweeps by, the magnetic
E
To audio/ video
amplifier circuits
Direction of wave travel
Antenna wire
L
C
FIGURE 24.4 A radio wave can be detected with a receiving antenna wire that is parallel
to the electric fi eld of the wave. The magnetic
fi eld of the radio wave has been omitted for
simplicity.
FIGURE 24.5 With a receiving antenna in the form of a loop, the magnetic fi eld of a
broadcasted radio wave can be detected. The
normal to the plane of the loop should be
parallel to the magnetic fi eld for best reception.
For clarity, the electric fi eld of the radio wave
has been omitted.
To audio/ video
amplifier circuits
Normal
Direction of wave travel
Loop antenna
L
C
B
24.1 The Nature of Electromagnetic Waves 687
fi eld penetrates the loop, and the changing magnetic fl ux induces a voltage and a current in the
loop, in accord with Faraday’s law. Once again, the resonant frequency of a capacitor/inductor
combination can be adjusted to match the frequency of the desired electromagnetic wave. Both
straight wire and loop antennas can be seen on the ship’s mast in Figure 24.6. BIO THE PHYSICS OF . . . cochlear implants. Cochlear implants use the broadcasting
and receiving of radio waves to provide assistance to hearing-impaired people who have auditory
nerves that are at least partially intact. These implants utilize radio waves to bypass the damaged
part of the hearing mechanism and access the auditory nerve directly, as Interactive Figure 24.7 illustrates. An external microphone (often set into an ear mold) detects sound waves and sends
a corresponding electrical signal to a speech processor small enough to be carried in a pocket.
The speech processor encodes these signals into a radio wave, which is broadcast from an ex-
ternal transmitter coil placed over the site of a miniature receiver (and its receiving antenna) that
has been surgically inserted beneath the skin. The receiver acts much like a radio. It detects the
broadcasted wave and from the encoded audio information produces electrical signals that rep-
resent the sound wave. These signals are sent along a wire to electrodes that are implanted in the
cochlea of the inner ear. The electrodes stimulate the auditory nerves that feed directly between
structures within the cochlea and the brain. To the extent that the nerves are intact, a person can
learn to recognize sounds.
BIO THE PHYSICS OF . . . wireless capsule endoscopy. The broadcasting and receiving of radio waves are also now being used in the practice of endoscopy. In this medical diagnostic
technique a device called an endoscope is used to peer inside the body. For example, to examine
the interior of the colon for signs of cancer, a conventional endoscope (known as a colonoscope) is
inserted through the rectum. (See Section 26.3.) The wireless capsule endoscope shown in Figure 24.8 bypasses this invasive procedure completely. With a size of about 11 × 26 mm, this capsule can be swallowed and carried through the gastrointestinal tract by the involuntary contractions of
the walls of the intestines (peristalsis). The capsule is self-contained and uses no external wires.
A marvel of miniaturization, it contains a radio transmitter and its associated antenna, batteries, a
white-light-emitting diode (see Section 23.5) for illumination, and an optical system to capture the
digital images. As the capsule moves through the intestine, the transmitter broadcasts the images
to an array of small receiving antennas attached to the patient’s body. These receiving antennas
also are used to determine the position of the capsule within the body. The radio waves that are
used lie in the ultrahigh-frequency, or UHF, band, from 3 × 108 to 3 × 109 Hz.
Radio waves are only one part of the broad spectrum of electromagnetic waves that has been
discovered. The next section discusses the entire spectrum.
© Peter Barritt/Alamy
FIGURE 24.6 This ship’s mast indicates that both straight and loop antennas are being
used to communicate with other vessels and
on-shore stations.
Speech processor
External transmitter coil
External microphone set into ear mold
Wire
Surgically inserted receiver plus antenna
Cochlea
Auditory nerve
Electrodes implanted in cochlea
INTERACTIVE FIGURE 24.7 Hearing-impaired people can sometimes recover part of their hearing with the help of a cochlear implant. Broadcasting and receiving electromagnetic
waves play central roles in this device.
FIGURE 24.8 This wireless capsule endoscope is designed to be swallowed. As
it passes through a patient’s intestines, it
broadcasts video images of the interior of the
intestines.
Courtesy Given Imaging, Ltd.
688 CHAPTER 24 Electromagnetic Waves
Check Your Understanding
(The answers are given at the end of the book.) 1. Refer to Animated Figure 24.1. Between the times indicated in parts c and d in the drawing, what is
the direction of the magnetic fi eld at the point P for the electromagnetic wave being generated? Is it directed (a) upward along the length of the wire, (b) downward along the length of the wire, (c) into the plane of the paper, or (d) out of the plane of the paper?
2. A transmitting antenna is located at the origin of an x, y, z axis system and broadcasts an electromag- netic wave whose electric fi eld oscillates along the y axis. The wave travels along the +x axis. Three possible wire loops are available for use with an LC-tuned circuit to detect this wave: (a) a loop that lies in the xy plane, (b) a loop that lies in the xz plane, and (c) a loop that lies in the yz plane. Which one of the loops will detect the wave?
3. Why does the peak value of the emf induced in a loop antenna (see Figure 24.5) depend on the fre- quency of the electromagnetic wave?
24.2 The Electromagnetic Spectrum An electromagnetic wave, like any periodic wave, has frequency f and wavelength 𝜆 that are re- lated to the speed 𝜐 of the wave by 𝜐 = f𝜆 (Equation 16.1). For electromagnetic waves traveling through a vacuum or, to a good approximation, through air, the speed is 𝜐 = c, so c = f𝜆.
As Figure 24.9 shows, electromagnetic waves exist with an enormous range of frequen- cies, from values less than 104 Hz to greater than 1024 Hz. Since all these waves travel through a
vacuum at the same speed of c = 3.00 × 108 m/s, Equation 16.1 can be used to fi nd the cor- respondingly wide range of wavelengths that the picture also displays. The ordered series of
electromagnetic wave frequencies or wavelengths in Figure 24.9 is called the electromagnetic spectrum. Historically, regions of the spectrum have been given names such as radio waves and infrared waves. Although the boundary between adjacent regions is shown as a sharp line in the
drawing, the boundary is not so well defi ned in practice, and the regions often overlap.
Beginning on the left in Figure 24.9, we fi nd radio waves. Lower-frequency radio waves are generally produced by electrical oscillator circuits, while higher-frequency radio waves (called mi-
crowaves) are usually generated using electron tubes called klystrons. Infrared radiation, sometimes
loosely called heat waves, originates with the vibration and rotation of molecules within a material.
Visible light is emitted by hot objects, such as the sun, a burning log, or the fi lament of an incan-
descent light bulb, when the temperature is high enough to excite the electrons within an atom.
Ultraviolet frequencies can be produced from the discharge of an electric arc. X-rays are produced
4 x 1014
Red Violet
Visible light
7.9 x 1014
104
104 1 10–4 10–8 10–12 10–16
108 1012 1016 1020 1024
Frequency (Hz)
Radio waves
AM FM Microwaves
Infrared X-rays Gamma rays Ultra- violet
Wavelength (m)
Frequency (Hz)
FIGURE 24.9 The electromagnetic spectrum.
24.2 The Electromagnetic Spectrum 689
by the sudden deceleration of high-speed electrons. And, fi nally, gamma rays are radiation from
nuclear decay.
THE PHYSICS OF . . . astronomy and the electromagnetic spectrum. Astronomers use the diff erent regions of the electromagnetic spectrum to gather information about distant celestial
objects. Interactive Figure 24.10, for example, shows four views of the Crab Nebula, each in a diff erent region of the spectrum. The Crab Nebula is located 6.0 × 1016 km away from the earth
and is the remnant of a star that underwent a supernova explosion in 1054 AD.
BIO THE PHYSICS OF . . . a pyroelectric ear thermometer. The human body, like any object, radiates infrared radiation, and the amount emitted depends on the temperature of the
body. Although infrared radiation cannot be seen by the human eye, it can be detected by sensors.
An ear thermometer, like the pyroelectric thermometer shown in Figure 24.11, measures the body’s temperature by determining the amount of infrared radiation that emanates from the
eardrum and surrounding tissue. The ear is one of the best places for this measurement because
it is close to the hypothalamus, an area at the bottom of the brain that controls body temperature.
The ear is also not cooled or warmed by eating, drinking, or breathing. When the probe of the
thermometer is inserted into the ear canal, infrared radiation travels down the barrel of the probe
and strikes the sensor. The absorption of infrared radiation warms the sensor, and, as a result,
its electrical conductivity changes. The change in electrical conductivity is measured by an elec-
tronic circuit. The output from the circuit is sent to a microprocessor, which calculates the body
temperature and displays the result on a digital readout.
Of all the frequency ranges in the electromagnetic spectrum, the most familiar is that of
visible light, although it is the most narrow (see Figure 24.9). Only waves with frequencies between about 4.0 × 1014 Hz and 7.9 × 1014 Hz are perceived by the human eye as visible light.
Usually visible light is discussed in terms of wavelengths (in vacuum) rather than frequencies. As
Example 1 indicates, the wavelengths of visible light are extremely small and, therefore, are nor-
mally expressed in nanometers (nm); 1 nm = 10−9 m. An obsolete (non-SI) unit still occasionally used for wavelengths is the angstrom (Å); 1 Å = 10−10 m.
INTERACTIVE FIGURE 24.10 Four views of the Crab Nebula. Each view is in a diff erent region of the electromagnetic spectrum, as indicated.
(a) Radio wave
N R
A O
/A U
I/ N
S F
/S ci
en ce
P h o to
L ib
ra ry
/
S ci
en ce
S o u rc
e
(b) Infrared
N A
S A
, E
S A
, J.
H es
te r
an d A
. L
o ll
(A ri
zo n a
S ta
te U
n iv
er si
ty )
(c) Visible
M o u n t
S tr
o m
lo a
n d S
id in
g S
p ri
n g
O b se
rv at
o ri
es /S
ci en
ce S
o u rc
e
(d) X-ray
C o u rt
es y N
A S
A
Eardrum
Infrared radiation
Probe
FIGURE 24.11 A pyroelectric thermometer measures body temperature by determining
the amount of infrared radiation emitted by
the eardrum and surrounding tissue.
EXAMPLE 1 The Wavelengths of Visible Light
Find the range in wavelengths (in vacuum) for visible light in the fre-
quency range between 4.0 × 1014 Hz (red light) and 7.9 × 1014 Hz (violet
light). Express the answers in nanometers.
Reasoning According to Equation 16.1, the wavelength (in vacuum) 𝜆 of a light wave is equal to the speed of light c in a vacuum divided by the frequency f of the wave, 𝜆 = c/f.
Solution The wavelength corresponding to a frequency of 4.0 × 1014 Hz is
λ = c f
= 3.00 × 10 8 m/s
4.0 × 10 14 Hz = 7.5 × 10−7 m
Since 1 nm = 10−9 m, it follows that
λ = (7.5 × 10−7 m)( 1 nm10−9m) = 750 nm The calculation for a frequency of 7.9 × 1014 Hz is similar:
λ = c f
= 3.00 × 10 8 m /s
7.9 × 10 14 Hz = 3.8 × 10−7 m or 𝜆 = 380 nm
690 CHAPTER 24 Electromagnetic Waves
The eye/brain recognizes light of diff erent wavelengths as diff erent colors. A wavelength of
750 nm (in vacuum) is approximately the longest wavelength of red light, whereas 380 nm (in
vacuum) is approximately the shortest wavelength of violet light. Between these limits are found
the other familiar colors, as Figure 24.9 indicates. The association between color and wavelength in the visible part of the electromagnetic
spectrum is well known. The wavelength also plays a central role in governing the behavior and
use of electromagnetic waves in all regions of the spectrum. For instance, Conceptual Example 2
considers the infl uence of the wavelength on diff raction.
CONCEPTUAL EXAMPLE 2 The Physics of AM and FM Radio Reception
As we have discussed in Section 17.3, diff raction is the ability of a wave
to bend around an obstacle or around the edges of an opening. Based on
that discussion, which type of radio wave would you expect to bend more
readily around an obstacle such as a building, (a) an AM radio wave or (b) an FM radio wave?
Reasoning Section 17.3 points out that, other things being equal, sound waves exhibit diff raction to a greater extent when the wavelength is
longer than when it is shorter. Based on this information, we expect that
longer-wavelength electromagnetic waves will bend more readily around
obstacles than will shorter-wavelength waves.
Answer (b) is incorrect. Figure 24.9 shows that FM radio waves have considerably shorter wavelengths than do AM waves. Therefore, FM radio
waves exhibit less diff raction than AM waves do and bend less readily
around obstacles.
Answer (a) is correct. Since AM radio waves have greater wavelengths than FM waves do (see Figure 24.9), they exhibit greater diff raction and bend more readily around obstacles than FM waves do.
The picture of light as a wave is supported by experiments that will be discussed
in Chapter 27. However, there are also experiments indicating that light can behave as if it
were composed of discrete particles rather than waves. These experiments will be discussed in
Chapter 29. Wave theories and particle theories of light have been around for hundreds of years,
and it is now widely accepted that light, as well as other electromagnetic radiation, exhibits a
dual nature. Either wave-like or particle-like behavior can be observed, depending on the kind of
experiment being performed.
24.3 The Speed of Light At a speed of 3.00 × 108 m/s, light travels from the earth to the moon in a little over a second,
so the time required for light to travel between two places on earth is very short. Therefore, the
earliest attempts at measuring the speed of light had only limited success. One of the fi rst accur-
ate measurements employed a rotating mirror, and Figure 24.12 shows a simplifi ed version of the setup. It was used fi rst by the French scientist Jean Foucault (1819–1868) and later in a more
refi ned version by the American physicist Albert Michelson (1852–1931). If the angular speed of
the rotating eight-sided mirror in Figure 24.12 is adjusted correctly, light refl ected from one side travels to the fi xed mirror, refl ects, and can be detected after refl ecting from another side that has
rotated into place at just the right time. The minimum angular speed must be such that one side
of the mirror rotates one-eighth of a revolution during the time it takes for the light to make the
round trip between the mirrors. For one of his experiments, Michelson placed his fi xed mirror
and rotating mirror on Mt. San Antonio and Mt. Wilson in California, a distance of 35 km apart.
From a value of the minimum angular speed in such experiments, he obtained the value of c = (2.997 96 ± 0.000 04) × 108 m/s in 1926.
Today, the speed of light has been determined with such high accuracy that it is used to
defi ne the meter. As discussed in Section 1.2, the speed of light is now defi ned to be
Speed of light in a vacuum c = 299 792 458 m/s
However, a value of 3.00 × 108 m/s is adequate for most calculations. The second is defi ned in
terms of a cesium clock, and the meter is then defi ned as the distance light travels in a vacuum
Observer
Rotating octagonal
mirror
Light source
Fixed mirror
35 km
FIGURE 24.12 Between 1878 and 1931, Michelson used a rotating eight-sided
mirror to measure the speed of light. This is
a simplifi ed version of the setup.
24.3 The Speed of Light 691
during a time of 1/(299 792 458) s. Although the speed of light in a vacuum is large, it is fi nite,
so it takes a fi nite amount of time for light to travel from one place to another. The travel time
is especially long for light traveling between astronomical objects, as Conceptual Example 3
discusses.
CONCEPTUAL EXAMPLE 3 Looking Back in Time
A supernova is a violent explosion that occurs at the death of certain
stars. For a few days after the explosion, the intensity of the emitted
light can become a billion times greater than that of our own sun. After
several years, however, the intensity usually returns to zero. Supernovae
are relatively rare events in the universe; only six have been observed
in our galaxy within the past 400 years. A supernova that occurred in a
neighboring galaxy, approximately 1.66 × 1021 m away, was recorded in
1987. Figure 24.13 shows a photograph of the sky just a few hours after the explosion. Astronomers say that viewing an event like the supernova
is like looking back in time. Which one of the following statements
correctly describes what we see when we view such events? (a) The nearer the event is to the earth, the further back in time we are looking.
(b) The farther the event is from the earth, the further back in time we are looking.
Reasoning The light from the supernova traveled to earth at a speed of c = 3.00 × 108 m/s. The time t required for the light to travel the distance d between the event and the earth is t = d/c and is proportional to the distance.
Answer (a) is incorrect. Since the time required for the light to travel the distance between the event and the earth is proportional to the dis-
tance, the light from near-earth events reaches us sooner rather than later.
Therefore, the nearer the event is to the earth, the less into the past it
allows us to see, contrary to what this answer implies.
Answer (b) is correct. The travel time for light from the supernova is
t = d c
= 1.66 × 10 21 m
3.00 × 10 8 m /s = 5.53 × 10 12 s
This corresponds to 175 000 years, so when astronomers saw the explo-
sion in 1987, they were actually seeing the light that left the supernova
175 000 years earlier. In other words, they were looking back in time.
Greater values for the distance d mean greater values for the time t.
Related Homework: Problem 15
FIGURE 24.13 True color image of the 1987 supernova (bright spot at the lower right). The larger cloud-like object
near the middle left is the Tarantula nebula, whose light also
takes approximately 175 000 years to reach the earth.
C el
es ti
al I
m ag
e C
o ./
S ci
en ce
S o u rc
e
In 1865, Maxwell determined theoretically that electromagnetic waves propagate through a
vacuum at a speed given by
c = 1
√ε0μ0 (24.1)
where 𝜀0 = 8.85 × 10−12 C2/(N · m2) is the (electric) permittivity of free space and 𝜇0 = 4𝜋 × 10−7 T · m/A is the (magnetic) permeability of free space. Originally 𝜀0 was introduced in Section 18.5 as an alternative way of writing the proportionality constant k in Coulomb’s law [k = 1/(4𝜋𝜀0)] and, hence, plays a basic role in determining the strengths of the electric fi elds created by point charges. The role of 𝜇0 is similar for magnetic fi elds; it was introduced in Section 21.7 as
part of a proportionality constant in the expression for the magnetic fi eld created by the current in
a long, straight wire. Substituting the values for 𝜀0 and 𝜇0 into Equation 24.1 shows that
c = 1
√[8.85 × 10−12 C2/(N · m2 )](4π × 10−7 T · m/A) = 3.00 × 10 8 m /s
The experimental and theoretical values for c agree. Maxwell’s success in predicting c provided a basis for inferring that light behaves as a wave consisting of oscillating electric and magnetic
fi elds.
692 CHAPTER 24 Electromagnetic Waves
Check Your Understanding
(The answer is given at the end of the book.) 4. The frequency of electromagnetic wave A is twice that of electromagnetic wave B. For these two
waves, what is the ratio 𝜆A/𝜆B of the wavelengths in a vacuum? (a) 𝜆A/𝜆B = 2, because wave A has twice the speed that wave B has. (b) 𝜆A/𝜆B = 2, because wave A has one-half the speed that wave B has. (c) 𝜆A/𝜆B = 12, because wave A has one-half the speed that wave B has. (d) 𝜆A/𝜆B =
1
2, because wave A
has twice the speed that wave B has. (e) 𝜆A/𝜆B = 12, because both waves have the same speed.
24.4 The Energy Carried by Electromagnetic Waves THE PHYSICS OF . . . a microwave oven. Electromagnetic waves, like water waves or sound waves, carry energy. The energy is carried by the electric and magnetic fi elds that comprise the
wave. In a microwave oven, for example, microwaves penetrate food and deliver their energy
to it, as Figure 24.14 illustrates. The electric fi eld of the microwaves is largely responsible for delivering the energy, and water molecules in the food absorb it. The absorption occurs because
each water molecule has a permanent dipole moment; that is, one end of a molecule has a slight
positive charge, and the other end has a negative charge of equal magnitude. As a result, the
positive and negative ends of diff erent molecules can form a bond. However, the electric fi eld of
the microwaves exerts forces on the positive and negative ends of a molecule, causing it to spin.
Because the fi eld is oscillating rapidly—about 2.4 × 109 times a second—the water molecules are
kept spinning at a high rate. In the process, the energy of the microwaves is used to break bonds
between neighboring water molecules and ultimately is converted into internal energy. As the
internal energy increases, the temperature of the water increases, and the food cooks.
BIO THE PHYSICS OF . . . the greenhouse eff ect. The energy carried by electromag- netic waves in the infrared and visible regions of the spectrum plays the key role in the green-
house eff ect that is a contributing factor to global warming. The infrared waves from the sun are
largely prevented from reaching the earth’s surface by carbon dioxide and water in the atmo-
sphere, which refl ect them back into space. The visible waves do reach the earth’s surface, how-
ever, and the energy they carry heats the earth. Heat also fl ows to the surface from the interior of
the earth. The heated surface in turn radiates infrared waves outward, which, if they could, would
carry their energy into space. However, the atmospheric carbon dioxide and water refl ect these
infrared waves back toward the earth, just as they refl ect the infrared waves from the sun. Thus,
their energy is trapped, and the earth becomes warmer, like plants in a greenhouse. In a green-
house, however, energy is trapped mainly for a diff erent reason—namely, the lack of eff ective
convection currents to carry warm air past the cold glass walls.
A measure of the energy stored in the electric fi eld E→ of an electromagnetic wave, such as a microwave, is provided by the electric energy density. As we saw in Section 19.5, this density is
the electric energy per unit volume of space in which the electric fi eld exists:
Electric energy
density =
Electric energy
Volume =
1
2 κε0 E 2 =
1
2 ε0 E 2 (19.12)
In this equation, the dielectric constant 𝜅 has been set equal to unity, since we are dealing with an electric fi eld in a vacuum (or in air). From Section 22.8, the analogous expression for the
magnetic energy density is
Magnetic energy
density =
Magnetic energy
Volume =
1
2μ 0 B 2 (22.11)
The total energy density u of an electromagnetic wave in a vacuum is the sum of these two energy densities:
u = Total energy
Volume =
1
2 ε0 E 2 +
1
2μ 0 B 2 (24.2a)
Fan Microwaves Microwave generator
FIGURE 24.14 A microwave oven. The rotating fan blades refl ect the microwaves to
all parts of the oven.
24.4 The Energy Carried by Electromagnetic Waves 693
In an electromagnetic wave propagating through a vacuum or air, the electric fi eld and the mag-
netic fi eld carry equal amounts of energy per unit volume of space. Since 1
2 ε0E2 = 1
2(B2/𝜇0), it is pos- sible to rewrite Equation 24.2a for the total energy density in two additional, but equivalent, forms:
u = ε0 E 2 (24.2b)
u = 1
μ 0 B 2 (24.2c)
The fact that the two energy densities are equal implies that the electric and magnetic fi elds are
related. To see how, we set the electric energy density equal to the magnetic energy density and obtain
1
2 ε0 E 2 =
1
2μ 0 B 2 or E 2 =
1
ε0 μ0 B 2
However, according to Equation 24.1, c = 1/ √ε0 μ 0, so it follows that E2 = c2B2. Taking the square root of both sides of this result shows that the relation between the magnitudes of the
electric and magnetic fi elds in an electromagnetic wave is
E = cB (24.3)
In an electromagnetic wave, the electric and magnetic fi elds fl uctuate sinusoidally in time, so
Equations 24.2a–c give the energy density of the wave at any instant in time. If an average value
u for the total energy density is desired, average values are needed for E2 and B2. In Section 20.5 we faced a similar situation for alternating currents and voltages and introduced rms (root mean
square) quantities. Using an analogous procedure here, we fi nd that the rms values for the electric
and magnetic fi elds, Erms and Brms, are related to the maximum values of these fi elds, E0 and B0, by
E rms = 1
√2 E 0 and Brms =
1
√2 B0
Equations 24.2a–c can now be interpreted as giving the average energy density u, provided the symbols E and B are interpreted to mean the rms values given above. The average density of the sunlight reaching the earth is determined in the next example.
EXAMPLE 4 The Average Energy Density of Sunlight
Sunlight enters the top of the earth’s atmosphere with an electric fi eld
whose rms value is Erms = 720 N/C. Find (a) the average total energy density of this electromagnetic wave and (b) the rms value of the sun- light’s magnetic fi eld.
Reasoning The average total energy density u of the sunlight can be ob- tained with the aid of Equation 24.2b, provided the rms value is used for
the electric fi eld. Since the magnitudes of the magnetic and electric fi elds
are related according to Equation 24.3, the rms value of the magnetic fi eld
is Brms = Erms/c.
Solution (a) According to Equation 24.2b, the average total energy density is
u = ε0 E 2rms = [8.85 × 10−12 C2/(N · m2)](720 N/C)2
= 4.6 × 10−6 J/m3
(b) Using Equation 24.3, we fi nd that the rms magnetic fi eld is
Brms = E rms
c =
720 N/C
3.0 × 10 8 m /s = 2.4 × 10−6 T
As an electromagnetic wave moves through space, it carries energy from one region to an-
other. This energy transport is characterized by the intensity of the wave. We have encountered the concept of intensity before, in connection with sound waves in Section 16.7. The sound intensity is
the sound power that passes perpendicularly through a surface divided by the area of the surface.
The intensity of an electromagnetic wave is defi ned similarly. For an electromagnetic wave, the
intensity is the electromagnetic power divided by the area of the surface.
Using this defi nition of intensity, we can show that the electromagnetic intensity S is related to the energy density u. According to Equation 16.8 the intensity is the power P that passes per- pendicularly through a surface divided by the area A of that surface, or S = P/A. Furthermore, the power is equal to the total energy passing through the surface divided by the elapsed time t (Equation 6.10b), so that P = (Total energy)/t. Combining these two relations gives
S = P A
= Total energy
tA
694 CHAPTER 24 Electromagnetic Waves
Problem-Solving Insight The concepts of power and intensity are similar, but they are not the same. Intensity is the power that passes perpendicularly through a surface divided by the
area of the surface.
Now, consider Figure 24.15, which shows an electromagnetic wave traveling in a vacuum along the x axis. In a time t the wave travels the distance ct, passing through the surface of area A. Consequently, the volume of space through which the wave passes is ctA. The total (electric and magnetic) energy in this volume is
Total energy = (Total energy density) × Volume = u(ctA)
Using this result in the expression for the intensity, we obtain
S = Total energy
tA =
uctA tA
= cu (24.4)
Thus, the intensity and the energy density are related by the speed of light, c. Substituting Equa- tions 24.2a–c, one at a time, into Equation 24.4 shows that the intensity of an electromagnetic
wave depends on the electric and magnetic fi elds according to the following equivalent relations:
S = cu = 1
2 cε0 E 2 +
c 2μ 0
B 2 (24.5a)
S = cε0 E 2 (24.5b)
S = c μ 0
B 2 (24.5c)
If the rms values for the electric and magnetic fi elds are used in Equations 24.5a–c, the
intensity becomes an average intensity, S, as Example 5 illustrates.
y
z
x
B
E
ct
c
Area = A
FIGURE 24.15 In a time t, an electromagnetic wave moves a distance ct along the x axis and passes through a surface of area A.
Analyzing Multiple-Concept Problems
EXAMPLE 5 Power and Intensity
Figure 24.16 shows a tiny source that is emitting light uniformly in all directions. At a distance of 2.50 m from the source, the rms electric fi eld
strength of the light is 19.0 N/C. Assuming that the light does not refl ect
from anything in the environment, determine the average power of the
light emitted by the source.
Reasoning Recall from Section 16.7 that the power crossing a sur- face perpendicularly is equal to the intensity at the surface times the
area of the surface (see Equation 16.8). Since the source emits light
uniformly in all directions, the light intensity is the same at all points
on the imaginary spherical surface in Figure 24.16. Moreover, the light crosses this surface perpendicularly. Equation 24.5b relates the average
light intensity at the surface to its rms electric fi eld strength (which is
known), and the area of the surface can be found from a knowledge of
its radius.
Light source
r = 2.50 m
Erms = 19.0 N/C
Imaginary sphere
FIGURE 24.16 At a distance of 2.50 m from the
light source, the rms electric
fi eld of the light has a value
of 19.0 N/C.
24.5 The Doppler Eff ect and Electromagnetic Waves 695
Modeling the Problem
STEP 1 Average Intensity According to the discussion in Section 16.7, the average power P that passes perpendicularly through the imaginary spherical surface is equal to the average in-
tensity S times the area A of the surface, or P = SA. The area of a spherical surface is A = 4πr2, where r is the radius of the sphere. Thus, the average power can be written as in Equation 1 at the right. The radius is known, but the average light intensity is not, so we turn to Step 2 to evaluate it.
STEP 2 Average Intensity and Electric Field The average intensity S of the light passing through the imaginary spherical surface is related to the known rms electric fi eld strength Erms at the surface by Equation 24.5b:
S = c𝜀0 E 2rms
where c is the speed of light in a vacuum and 𝜀0 is the permittivity of free space. We can substitute this expression into Equation 1, as indicated at the right.
Solution Algebraically combining the results of each step, we have
P = S(4πr 2) = cε0 E 2rms(4πr 2 )
The average power emitted by the light source is
P = cε0 E 2rms(4πr 2) = (3.00 × 10 8 m /s)[8.85 × 10−12 C 2/(N · m 2 )](19.0 N/C) 2 4π (2.50 m) 2 = 75.3 W
Related Homework: Problems 27, 28, 29
STEP 1 STEP 2
P = S(4πr 2) (1)
?
P = S(4πr 2) (1)
S = c𝜀0 E 2rms
Knowns and Unknowns The following data are available:
Description Symbol Value Rms electric field strength 2.50 m from light source Erms 19.0 N/C
Distance from light source r 2.50 m
Unknown Variable
Average power emitted by light source P ?
Check Your Understanding
(The answers are given at the end of the book.) 5. If both the electric and magnetic fi elds of an electromagnetic wave double in magnitude, how does the
intensity of the wave change? The intensity (a) decreases by a factor of four (b) decreases by a factor of two (c) increases by a factor of two (d) increases by a factor of four (e) increases by a factor of eight.
6. Suppose that the electric fi eld of an electromagnetic wave decreases in magnitude. Does the magnitude of the magnetic fi eld (a) increase, (b) decrease, or (c) remain the same?
24.5 The Doppler Eff ect and Electromagnetic Waves Section 16.9 presents a discussion of the Doppler eff ect that sound waves exhibit when either the
source of a sound wave, the observer of the wave, or both are moving with respect to the medium
of propagation (e.g., air). This eff ect is one in which the observed sound frequency is greater
696 CHAPTER 24 Electromagnetic Waves
or smaller than the frequency emitted by the source. A diff erent Doppler eff ect arises when the
source moves than when the observer moves.
Electromagnetic waves also can exhibit a Doppler eff ect, but it diff ers from that for sound
waves for two reasons. First, sound waves require a medium such as air in which to propagate.
In the Doppler eff ect for sound, it is the motion (of the source, the observer, and the waves
themselves) relative to this medium that is important. In the Doppler eff ect for electromagnetic
waves, motion relative to a medium plays no role, because the waves do not require a medium in
which to propagate. They can travel in a vacuum. Second, in the equations for the Doppler eff ect
in Section 16.9, the speed of sound plays an important role, and it depends on the reference frame
relative to which it is measured. For example, the speed of sound with respect to moving air is
diff erent than it is with respect to stationary air. As we will see in Section 28.2, electromagnetic
waves behave in a diff erent way. The speed at which they travel has the same value, whether it
is measured relative to a stationary observer or relative to one moving at a constant velocity.
For these two reasons, the same Doppler eff ect arises for electromagnetic waves when either
the source or the observer of the waves moves; only the relative motion of the source and the
observer with respect to one another is important.
When electromagnetic waves and the source and the observer of the waves all travel along
the same line in a vacuum (or in air, to a good degree of approximation), the single equation that
specifi es the Doppler eff ect is
fo = fs (1 ± υrel c ) if υrel << c (24.6)
In this expression, fo is the observed frequency, and fs is the frequency emitted by the source. The symbol 𝜐rel stands for the speed of the source and the observer relative to one another, and c is the speed of light in a vacuum. Equation 24.6 applies only if 𝜐rel is very small compared to c—that is, if υrel << c. Since 𝜐rel is the relative speed of the source and the observer, it is like any speed and has no algebraic sign associated with it to denote the direction. The direction of the relative
motion is taken into account by choosing the plus or minus sign in Equation 24.6. The plus sign is used when the source and the observer come together, and the minus sign is used when they move apart.
For instance, suppose that the source and the observer are both traveling due east, the source
at a speed of 28 m/s with respect to the ground and the observer at a speed of 22 m/s with respect
to the ground. Neither of these speeds with respect to the ground is used for the symbol 𝜐rel in
Equation 24.6. Instead, the value for 𝜐rel is |28 m/s − 22 m/s| = 6 m/s. If the faster source is behind
the slower observer, the source and the observer come together because the source is catching
up. Therefore, the plus sign is chosen in Equation 24.6. On the other hand, if the slower observer
is behind the faster source, the source and the observer move apart because the source is pulling
away. In this case, the minus sign is chosen in Equation 24.6.
THE PHYSICS OF . . . astronomy and the Doppler eff ect. The Doppler eff ect of electro- magnetic waves provides a powerful tool for astronomers. For instance, Example 10 in Chapter 5
discusses how astronomers have identifi ed a supermassive black hole at the center of galaxy M87
Math Skills The choice of the plus or minus sign in Equation 24.6 is critical. Without the right choice, the equation cannot be used successfully to solve problems. Whether the plus or the minus
sign is used depends on the nature of the individual problem, and the following two lists outline the
possibilities.
PLUS SIGN (SOURCE AND OBSERVER COME TOGETHER) (1) The source is catching up with the observer.
(2) The observer is catching up with the source.
(3) The source and the observer both move toward one another.
MINUS SIGN (SOURCE AND OBSERVER MOVE APART) (1) The source is pulling away from the observer.
(2) The observer is pulling away from the source.
(3) The source and the observer both move away from one another.
24.6 Polarization 697
by using the Hubble Space Telescope. They focused the telescope on regions to either side of the
center of the galaxy (see Figure 5.14). From the light emitted by these two regions, they were
able to use the Doppler eff ect to determine that one side is moving away from the earth, while
the other side is moving toward the earth. In other words, the galaxy is rotating. The speeds of
recession and approach enabled astronomers to determine the rotational speed of the galaxy, and
Example 10 in Chapter 5 shows how the value for this speed leads to the identifi cation of the
black hole. Astronomers routinely study the Doppler eff ect of the light that reaches the earth from
distant parts of the universe. From such studies, they have determined the speeds at which distant
light-emitting objects are receding from the earth.
Check Your Understanding
(The answers are given at the end of the book.) 7. An astronomer measures the Doppler change in frequency for the light reaching the earth from a distant
star. From this measurement, can the astronomer tell whether the star is moving away from the earth or
the earth is moving away from the star?
8. CYU Figure 24.1 shows three situations—A, B, and C—in which an observer and a source of electromagnetic waves
are moving along the same line. In each case the source
emits a wave of the same frequency. The arrows in each
situation denote velocity vectors relative to the ground and
have magnitudes of either 𝜐 or 2𝜐. Rank the magnitudes of
the frequencies of the observed waves in descending order
(largest fi rst).
24.6 Polarization
Polarized Electromagnetic Waves One of the essential features of electromagnetic waves is that they are transverse waves, and
because of this feature they can be polarized. Figure 24.17 illustrates the idea of polarization by showing a transverse wave as it travels along a rope toward a slit. The wave is said to be linearly polarized, which means that its vibrations always occur along one direction. This direction is called the direction of polarization. In part a of the picture, the direction of polarization is ver- tical, parallel to the slit. Consequently, the wave passes through easily. However, when the slit is
turned perpendicular to the direction of polarization, as in part b, the wave cannot pass, because the slit prevents the rope from oscillating. For longitudinal waves, such as sound waves, the no-
tion of polarization has no meaning. In a longitudinal wave the direction of vibration is along the
direction of travel, and the orientation of the slit would have no eff ect on the wave.
In an electromagnetic wave such as the one in Figure 24.3, the electric fi eld oscillates along the y axis. Similarly, the magnetic fi eld oscillates along the z axis. Therefore, the wave is linearly polarized, with the direction of polarization taken arbitrarily to be the direction
along which the electric fi eld oscillates. If the wave is a radio wave generated by a straight-
wire antenna, the direction of polarization is determined by the orientation of the antenna.
A
Observer
2
Source
B
C 2
2
2
CYU FIGURE 24.1
(a)
Direction of wave travel
Direction of rope vibrations
(b)
FIGURE 24.17 A transverse wave is linearly polarized when its vibrations always occur
along one direction. (a) A linearly polarized wave on a rope can pass through a slit that is
parallel to the direction of the rope vibrations,
but (b) cannot pass through a slit that is per- pendicular to the vibrations.
698 CHAPTER 24 Electromagnetic Waves
In comparison, the visible light given off by an incandescent light bulb consists of electro-
magnetic waves that are completely unpolarized. In this case the waves are emitted by a large
number of atoms in the hot fi lament of the bulb. When an electron in an atom oscillates, the
atom behaves as a miniature antenna that broadcasts light for brief periods of time, about
10−8 seconds. However, the directions of these atomic antennas change randomly as a result
of collisions. Unpolarized light, then, consists of many individual waves, emitted in short
bursts by many “atomic antennas,” each with its own direction of polarization. Figure 24.18 compares polarized and unpolarized light. In the unpolarized case, the arrows shown around
the direction of wave travel symbolize the random directions of polarization of the individual
waves that comprise the light.
Linearly polarized light can be produced from unpolarized light with the aid of certain mater-
ials. One commercially available material goes under the name of Polaroid. Such materials allow
only the component of the electric fi eld along one direction to pass through, while absorbing the
fi eld component perpendicular to this direction. As Figure 24.19 indicates, the direction of polar-
ization that a polarizing material allows through is called the transmission axis. No matter how this axis is oriented, the average intensity of the transmitted polarized light is one-half the average
intensity of the incident unpolarized light. The reason for this is that the unpolarized light contains
all polarization directions to an equal extent. Moreover, the electric fi eld for each direction can be
resolved into components perpendicular and parallel to the transmission axis, with the result that
the average components perpendicular and parallel to the axis are equal. As a result, the polarizing
material absorbs as much of the electric (and magnetic) fi eld strength as it transmits.
Malus’ Law Once polarized light has been produced with a piece of polarizing material, it is possible to use
a second piece to change the polarization direction and simultaneously adjust the intensity of the
light. Figure 24.20 shows how. As in this picture, the fi rst piece of polarizing material is called the polarizer and the second piece is referred to as the analyzer. The transmission axis of the analyzer is oriented at an angle 𝜃 relative to the transmission axis of the polarizer. If the elec- tric fi eld strength of the polarized light incident on the analyzer is E, the fi eld strength passing through is the component parallel to the transmission axis, or E cos 𝜃. According to Equation 24.5b, the intensity is proportional to the square of the electric fi eld strength. Consequently, the
average intensity of polarized light passing through the analyzer is proportional to cos2 𝜃. Thus,
both the polarization direction and the intensity of the light can be adjusted by rotating the trans-
mission axis of the analyzer relative to that of the polarizer. The average intensity S of the light leaving the analyzer, then, is
Malus’ law S = S0 cos2 θ (24.7)
Single direction for electric field
Direction of wave travel
(a) Polarized light
(b) Unpolarized light
Random electric field directions
Direction of wave travel
FIGURE 24.18 (a) In polarized light, the electric fi eld of the electromagnetic wave
fl uctuates along a single direction.
(b) Unpolarized light consists of short bursts of electromagnetic waves emitted by many
diff erent atoms. The electric fi eld directions
of these bursts are perpendicular to the
direction of wave travel but are distributed
randomly about it.
Unpolarized light
intensity = S
Polarizing material
Direction of
wave travel
Polarized light
intensity = S12
Transmission axis
FIGURE 24.19 With the aid of a piece of polarizing material, polarized light may be
produced from unpolarized light. The trans-
mission axis of the material is the direction of
polarization of the light that passes through
the material.
Unpolarized light
Polarizer
90°
E cos
E
E
Analyzer Photocell
E cos
θθ
θ
θ
FIGURE 24.20 Two sheets of polarizing material, called the polarizer and the analyzer, may be used to adjust the polarization direction and intensity of the light reaching the
photocell. This can be done by changing the angle 𝜃 between the transmission axes of the polarizer and analyzer.
24.6 Polarization 699
where S0 is the average intensity of the light entering the analyzer. Equation 24.7 is sometimes called Malus’ law, for it was discovered by the French engineer Étienne Louis Malus (1775–1812). Example 6 illustrates the use of Malus’ law.
EXAMPLE 6 Using Polarizers and Analyzers
What value of 𝜃 should be used in Figure 24.20, so that the average in- tensity of the polarized light reaching the photocell will be one-tenth the
average intensity of the unpolarized light?
Reasoning Both the polarizer and the analyzer reduce the intensity of the light. The polarizer reduces the intensity by a factor of one-half, as
discussed earlier. Therefore, if the average intensity of the unpolarized
light is I , the average intensity of the polarized light leaving the polarizer and striking the analyzer is S0 = I /2. The angle θ must now be selected so that the average intensity of the light leaving the analyzer will be
S = I /10. Malus’ law provides the solution.
Problem-Solving Insight Remember that when unpolarized light strikes a polarizer, only one-half of the incident light is transmitted, the other half being absorbed by the polarizer.
Solution Using S0 = I /2 and S = I /10 in Malus’ law, we fi nd 1
10 I = 1
2 I cos2 θ
1
5 = cos2 θ or θ = cos−1 ( 1√5) = 63.4°
When 𝜃 = 90° in Figure 24.20, the polarizer and analyzer are said to be crossed, and no light is transmitted by the polarizer/analyzer combination. As an illustration of this eff ect,
Interactive Figure 24.21 shows two pairs of Polaroid sunglasses in uncrossed and crossed confi gurations.
THE PHYSICS OF . . . IMAX 3-D fi lms. An exciting application of crossed polarizers is used in viewing IMAX 3-D movies. These movies are recorded on two separate rolls of fi lm,
using a camera that provides images from the two diff erent perspectives that correspond to what
is observed by human eyes and allow us to see in three dimensions. The camera has two aper-
tures or openings located at roughly the spacing between our eyes. The fi lms are projected using
a projector with two lenses, as Figure 24.22 indicates. Each lens has its own polarizer, and the two polarizers are crossed (see the drawing). In one type of theater, viewers watch the action
on-screen using glasses with corresponding polarizers for the left and right eyes, as the drawing
shows. Because of the crossed polarizers the left eye sees only the image from the left lens of the
projector, and the right eye sees only the image from the right lens. Since the two images have the
approximate perspectives that the left and right eyes would see in reality, the brain combines the
images to produce a realistic 3-D eff ect.
Conceptual Example 7 illustrates an interesting result that occurs when a piece of polarizing
material is inserted between a crossed polarizer and analyzer.
INTERACTIVE FIGURE 24.21 When Polaroid sunglasses are uncrossed (left side), the transmitted light is dimmed due to the extra thickness of tinted plastic. However, when they are crossed (right side), the
intensity of the transmitted light is reduced to zero because of the eff ects of polarization.
© D
ia n e
H ir
sc h /F
u n d am
en ta
l P
h o to
g ra
p h s,
N Y
C
© D
ia n e
H ir
sc h /F
u n d am
en ta
l P
h o to
g ra
p h s,
N Y
C
700 CHAPTER 24 Electromagnetic Waves
Projector
FIGURE 24.22 In an IMAX 3-D fi lm, two separate rolls of fi lm are projected using a projector with two lenses, each with its own polarizer. The two polarizers are crossed.
Viewers watch the action on-screen through glasses that have corresponding crossed
polarizers for each eye. The result is a 3-D moving picture, as the text discusses.
CONCEPTUAL EXAMPLE 7 How Can a Crossed Polarizer and Analyzer Transmit Light?
As explained earlier, no light reaches the photocell in Figure 24.20 when the polarizer and the analyzer are crossed. Suppose that a
third piece of polarizing material is inserted between the polarizer
and analyzer, as in Figure 24.23a. With the insert in place, will light reach the photocell when (a) 𝜃 = 0°, (b) 𝜃 = 90°, or (c) 𝜃 is between 0 and 90°?
Reasoning If any light is to pass through the analyzer, it must have an electric fi eld component parallel to the transmission axis of the analyzer.
Thus, without the insert in Figure 24.23a, no light reaches the photocell, because the analyzer and polarizer are crossed, which means that the elec-
tric fi eld of the light reaching the analyzer has no component parallel to
the analyzer’s transmission axis. We need to consider, then, whether the
presence of the insert leads to an electric fi eld component parallel to the
analyzer’s transmission axis.
Answers (a) and (b) are incorrect. With 𝜃 = 0°, the polarizer and the insert have parallel transmission axes, so the light leaving the polarizer
passes through the insert unaff ected. It reaches the analyzer with its
electric fi eld perpendicular to the analyzer’s transmission axis and is,
thus, prevented from reaching the photocell. With 𝜃 = 90°, the polarizer
and the insert are crossed, so no light leaves the insert to reach the ana-
lyzer and the photocell.
Answer (c) is correct. Parts b and c of Figure 24.23 show that, with the insert present, the light reaching the analyzer has an electric fi eld
component that is parallel to the analyzer’s transmission axis when 𝜃 is
between 0 and 90°. In part b the electric fi eld E of the light leaving the polarizer makes an angle 𝜃 with respect to the transmission axis of the
insert and has a component E cos 𝜃 with respect to that axis. This com- ponent passes through the insert. In part c the fi eld (E cos 𝜃) incident on the analyzer has a component parallel to the transmission axis of the
analyzer—namely, (E cos 𝜃) sin 𝜃. This component passes through the analyzer and reaches the photocell.
Related Homework: Problems 43, 46
Light
InsertPolarizer Analyzer Photocell (a)
(E cos ) sin
E cos E
(b) (c)
E cos
θ
θ
θ θ
θ
θ
θ
FIGURE 24.23 (a) Light reaches the photocell when a piece of polarizing material
is inserted between a crossed polarizer and
analyzer. (b) The electric-fi eld component parallel to the insert’s transmission axis is
E cos 𝜃. (c) Light incident on the analyzer has a component (E cos 𝜃) sin 𝜃 parallel to its transmission axis.
24.6 Polarization 701
THE PHYSICS OF . . . a liquid crystal display (LCD). An application of a crossed polarizer/analyzer combination occurs in one kind of liquid crystal display (LCD). LCDs are
widely used in pocket calculators and cell phones. The display usually consists of blackened
numbers and letters set against a light gray background. As Figure 24.24 indicates, each number or letter is formed from a combination of liquid crystal segments that have been turned on and
appear black. The liquid crystal part of an LCD segment consists of the liquid crystal material
sandwiched between two transparent electrodes, as in Figure 24.25. When a voltage is applied between the electrodes, the liquid crystal is said to be “on.” Part a of the picture shows that lin- early polarized incident light passes through the “on” material without having its direction of
polarization aff ected. When the voltage is removed, as in part b, the liquid crystal is said to be “off ” and now rotates the direction of polarization by 90°. A complete LCD segment also includes a
crossed polarizer/analyzer combination, as Figure 24.26 illustrates. The polarizer, analyzer, elec- trodes, and liquid crystal material are packaged as a single unit. The polarizer produces polarized
light from incident unpolarized light. With the display segment turned on, as in Figure 24.26, the polarized light emerges from the liquid crystal only to be absorbed by the analyzer, since the light
is polarized perpendicular to the transmission axis of the analyzer. Since no light emerges from the
analyzer, an observer sees a black segment against a light gray background, as in Figure 24.24. On the other hand, the segment is turned off when the voltage is removed, in which case the liquid crystal
rotates the direction of polarization by 90° to coincide with the axis of the analyzer. The light now
passes through the analyzer and enters the eye of the observer. However, the light coming from the
segment has been designed to have the same color and shade (light gray) as the background of the
display, so the segment becomes indistinguishable from the background.
Color LCD display screens and computer monitors are popular because they occupy less
space and weigh less than traditional cathode-ray tube (CRT) units do. An LCD display screen,
such as the one in Figure 24.27, uses thousands of LCD segments arranged like the squares on graph paper. To produce color, three segments are grouped together to form a tiny picture element
RM C
CE
M+M–
98
X65
+–32
Segments turned on
FIGURE 24.24 Liquid crystal displays (LCDs) use liquid crystal segments to form the
numbers.
Incident light
(b) OFF
Incident light
No voltageVoltage + –
Transparent electrode
Transparent electrode
Liquid crystal
(a) ON
FIGURE 24.25 A liquid crystal in its (a) “on” state and (b) “off ” state.
Voltage + –
ON
Polarizer
Eye sees black LCD segment
Analyzer
FIGURE 24.26 An LCD incorporates a crossed polarizer/analyzer combination. When the LCD segment is turned on (voltage applied), no light is transmitted
through the analyzer, and the observer sees a black segment.
FIGURE 24.27 Want to see a photograph of yourself? Just take a picture with a properly
equipped cell phone and look at the LCD
display.
©Simon Marcus/Corbis
702 CHAPTER 24 Electromagnetic Waves
(or “pixel”). Color fi lters are used to enable one segment in the pixel to produce red light, one to
produce green, and one to produce blue. The eye blends the colors from each pixel into a com-
posite color. By varying the intensity of the red, green, and blue colors, the pixel can generate an
entire spectrum of colors.
The Occurrence of Polarized Light in Nature THE PHYSICS OF . . . Polaroid sunglasses. Polaroid is a familiar material because of its widespread use in sunglasses. Such sunglasses are designed so that the transmission axis of
the Polaroid is oriented vertically when the glasses are worn in the usual fashion. Thus, the
glasses prevent any light that is polarized horizontally from reaching the eye. Light from the
sun is unpolarized, but a considerable amount of horizontally polarized sunlight originates by
refl ection from horizontal surfaces such as that of a lake. Section 26.4 discusses this eff ect.
Polaroid sunglasses reduce glare by preventing the horizontally polarized refl ected light from
reaching the eyes.
Polarized sunlight also originates from the scattering of light by molecules in the atmo-
sphere. Figure 24.28 shows light being scattered by a single atmospheric molecule. The electric fi elds in the unpolarized sunlight cause the electrons in the molecule to vibrate perpendicular
to the direction in which the light is traveling. The electrons, in turn, reradiate the electromag-
netic waves in diff erent directions, as the drawing illustrates. The light radiated straight ahead
in direction A is unpolarized, just like the incident light; but light radiated perpendicular to the incident light in direction C is polarized. Light radiated in the intermediate direction B is partially polarized.
BIO THE PHYSICS OF . . . butterfl ies and polarized light. Researchers have dis- covered that at least one butterfl y species uses polarized light to attract members of the op-
posite sex. The butterfl y species Heliconius has patterns on its wings that cause light refl ected from them to be polarized. This polarized light, invisible to the human eye but visible to other
butterfl ies, is attractive to potential mates. When males were shown the female wings with
their polarized light patterns, they swarmed toward the wings. When the males were shown
the wings through a fi lter that blocked out the polarization eff ects, they largely ignored the
wings. Figure 24.29 shows the polarized light refl ected from the wings of the Heliconius cydno butterfl y. The left wing is shown as it normally appears. The light refl ected from the white pattern is highly polarized. The right wing is shown as it appears when viewed through
a polarizing fi lter whose transmission axis is crossed with respect to the direction in which
the refl ected light is polarized. The white patterns in the right wing are black when viewed
through the fi lter, a clear indication that the light refl ected from them is indeed polarized.
There is also experimental evidence that some bird species use polarized light as a naviga-
tional aid.
Unpolarized light
Polarized light
Unpolarized sunlight
Molecule
C
B
A
Partially polarized light
FIGURE 24.28 In the process of being scattered from atmospheric
molecules, unpolarized light from
the sun becomes partially polarized.
FIGURE 24.29 A Heliconius cydno butterfl y. The left wing is shown as it appears normally,
and the right wing as it appears when viewed
through a polarizing fi lter. The light refl ected
from the white patterns is polarized. These
patterns in the right wing are black because
the transmission axis of the fi lter is crossed
with respect to the polarization direction of
the refl ected light.
Courtesy Alison Sweeney, Duke University. Image
from Nature 423: 31–32 (May 1, 2003). Reproduced with permission.
24.6 Polarization 703
Check Your Understanding
(The answers are given at the end of the book.) 9. Malus’ law applies to the setup in Figure 24.20, which shows the analyzer rotated through an angle 𝜃
and the polarizer held fi xed. Does Malus’ law apply when the analyzer is held fi xed and the polarizer is
rotated?
10. In Example 6, we saw that when the angle between the polarizer and analyzer is 63.4°, the average intensity of the transmitted light drops to one-tenth of the average intensity of the incident unpolarized
light. What happens to the light intensity that is not transmitted?
11. CYU Figure 24.2 shows two sheets of polarizing material. The trans- mission axis of one is vertical, and that of the other makes an angle
of 45° with the vertical. Unpolarized light shines on this arrangement
fi rst from the left and then from the right. From which direction does at
least some light pass through both sheets? (a) From the left (b) From the right (c) From either direction (d) From neither direction. What is the answer when the light is horizontally polarized? What is the answer
when the light is vertically polarized?
12. You are sitting upright on the beach near a lake on a sunny day, wearing Polaroid sunglasses. When you lie down on your side, facing the lake, the sunglasses don’t work as well as they do while you are
sitting upright. Why not?
45°
CYU FIGURE 24.2
EXAMPLE 8 BIO The Physics of the Laser Scalpel
A laser scalpel is a tool used for general surgery, which may include cut-
ting or vaporizing biological tissues using the energy from coherent laser
light. This surgical technique is very precise and can minimize bleeding,
swelling, and general discomfort commonly associated with traditional
surgical techniques. A gas laser using CO2 (carbon dioxide) is the highest
power continuous-operation laser that is currently available. It operates at
wavelengths of 9.4 − 10.6 μm, which correspond to frequencies that are readily absorbed by water molecules, and therefore soft tissues. One such
laser is being used to remove a precancerous mole from a person’s arm.
The average power of the laser is 7.5 W, and it creates a circular beam
(spot size) with a diameter of 0.25 mm. What is the average total energy
density contained in the beam? How does this value compare to the aver-
age total energy density of sunlight?
Reasoning The average total energy density (u) of the laser light in the beam is related to the average intensity (S) by Equation 24.4. We can then use Equation 16.8 to write the average intensity in terms of the average
power of the laser.
Solution According to Equation 24.4, the average total energy density is directly related to the average intensity: S = cu . Using Equation 16.8, we
write the average intensity in terms of the average power, S = P A
, and then
substitute this into the equation above: P A
= cu. Rearranging, we solve for
the average total energy density: u = P cA
. Since the beam is circular, the
cross-sectional area will be equal to A = πr 2 = π(d2) 2
= πd 2
4 , where d is
the diameter of the circular spot size. Substituting this expression for the
area into the average total energy density equation, we get our fi nal result:
u = P cA
= 4P
cπd 2 =
4(7.5 W)
π(3.0 × 108 m/s)(0.25 × 10−3 m)2 = 0.51 J/m3
From our result in Example 4 of this chapter, we see the laser has an
average total energy density that is approximately 100,000 times greater
than that of sunlight!
FIGURE 24.30 Surgeon using a laser scalpel to operate on the heart.
M at
h il
d e
R en
ar d /M
ed ic
al I
m ag
es
704 CHAPTER 24 Electromagnetic Waves
Concept Summary 24.1 The Nature of Electromagnetic Waves An electromagnetic wave consists of mutually perpendicular and oscillating electric and magnetic
fi elds. The wave is a transverse wave, since the fi elds are perpendicular to
the direction in which the wave travels. Electromagnetic waves can travel
through a vacuum or a material substance. All electromagnetic waves travel
through a vacuum at the same speed, which is known as the speed of light c (c = 3.00 × 108 m/s).
24.2 The Electromagnetic Spectrum The frequency f and wavelength 𝜆 of an electromagnetic wave in a vacuum are related to its speed c through the relation c = f𝜆.
The series of electromagnetic waves, arranged in order of their frequen-
cies or wavelengths, is called the electromagnetic spectrum. In increasing
order of frequency (decreasing order of wavelength), the spectrum includes
radio waves, infrared radiation, visible light, ultraviolet radiation, X-rays,
and gamma rays. Visible light has frequencies between about 4.0 × 1014 and
7.9 × 1014 Hz. The human eye and brain perceive diff erent frequencies or
wavelengths as diff erent colors.
24.3 The Speed of Light James Clerk Maxwell showed that the speed of light in a vacuum is given by Equation 24.1, where 𝜀0 is the (electric) permittivity of free space and 𝜇0 is the (magnetic) permeability of free
space.
c = 1
√ε0μ 0 (24.1)
24.4 The Energy Carried by Electromagnetic Waves The total en- ergy density u of an electromagnetic wave is the total energy per unit volume of the wave and, in a vacuum, is given by Equation 24.2a, where E and B, respectively, are the magnitudes of the electric and magnetic fi elds of the
wave. Since the electric and magnetic parts of the total energy density are equal,
Equations 24.2b and 24.2c are equivalent to Equation 24.2a. In a vacuum,
E and B are related according to Equation 24.3.
u = 1
2 ε0 E 2 +
1
2μ 0 B 2 (24.2a)
u = ε0 E 2 (24.2b)
u = 1
μ0 B 2 (24.2c)
E = cB (24.3)
Equations 24.2a–c can be used to determine the average total energy den-
sity, if the rms average values Erms and Brms are used in place of the symbols
E and B. The rms values are related to the peak values E0 and B0 in the usual way, as shown in Equations 1 and 2.
The intensity of an electromagnetic wave is the power that the wave car-
ries perpendicularly through a surface divided by the area of the surface. In
a vacuum, the intensity S is related to the total energy density u according to Equation 24.4.
Erms = 1
√2 E 0 (1) Brms =
1
√2 B 0 (2)
S = cu (24.4)
24.5 The Doppler Eff ect and Electromagnetic Waves When electromag- netic waves and the source and observer of the waves all travel along the same
line in a vacuum, the Doppler eff ect is given by Equation 24.6, where fo and fs are, respectively, the observed and emitted wave frequencies and 𝜐rel is the relative
speed of the source and the observer. The plus sign is used when the source and
the observer come together, and the minus sign is used when they move apart.
fo = fs (1 ± υrel c ) if υrel << c (24.6)
24.6 Polarization A linearly polarized electromagnetic wave is one in which the oscillation of the electric fi eld occurs only along one direction,
which is taken to be the direction of polarization. The magnetic fi eld also oscil-
lates along only one direction, which is perpendicular to the electric fi eld dir-
ection. In an unpolarized wave such as the light from an incandescent bulb, the
direction of polarization does not remain fi xed, but fl uctuates randomly in time.
Polarizing materials allow only the component of the wave’s electric fi eld
along one direction (and the associated magnetic fi eld component) to pass
through them. The preferred transmission direction for the electric fi eld is
called the transmission axis of the material.
When unpolarized light is incident on a piece of polarizing material, the
transmitted polarized light has an average intensity that is one-half the aver-
age intensity of the incident light.
When two pieces of polarizing material are used one after the other, the
fi rst is called the polarizer, and the second is referred to as the analyzer. If the
average intensity of polarized light falling on the analyzer is S0, the average intensity S of the light leaving the analyzer is given by Malus’ law, as shown in Equation 24.7, where 𝜃 is the angle between the transmission axes of the
polarizer and analyzer. When 𝜃 = 90°, the polarizer and the analyzer are said
to be “crossed,” and no light passes through the analyzer.
S = S0 cos2 θ (24.7)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 24.1 The Nature of Electromagnetic Waves 1. The drawing shows an x, y, z coordinate system. A circular loop of wire lies in the z, x plane and, when used with an LC-tuned circuit, detects an
electromagnetic wave. Which one of the following statements is correct?
(a) The wave travels along the x axis, and its electric fi eld oscillates along the y axis. (b) The wave travels along the z axis, and its electric fi eld oscil- lates along the x axis. (c) The wave travels along the z axis, and its electric fi eld oscillates along the y axis. (d) The wave travels along the y axis, and its electric fi eld oscillates along the x axis. (e) The wave travels along the y axis, and its electric fi eld oscillates along the z axis.
Focus on Concepts
Problems 705
QUESTION 1
+x
+z
+y
Section 24.2 The Electromagnetic Spectrum 2. An electromagnetic wave travels in a vacuum. The wavelength of the wave is tripled. How is this accomplished? (a) By tripling the frequency of the wave (b) By tripling the speed of the wave (c) By reducing the frequency of the wave by a factor of three (d) By reducing the speed of the wave by a factor of three (e) By tripling the magnitudes of the electric and magnetic fi elds that comprise the wave
Section 24.4 The Energy Carried by Electromagnetic Waves 3. An electromagnetic wave is traveling in a vacuum. The magnitudes of the electric and magnetic fi elds of the wave are ______, and the electric and
magnetic energies carried by the wave are ______. (a) equal, proportional (but not equal) to each other (b) proportional (but not equal) to each other, equal (c) equal, equal (d) proportional (but not equal) to each other, unequal
Section 24.5 The Doppler Eff ect and Electromagnetic Waves 6. The drawing shows four situations—A, B, C, and D—in which an ob- server and a source of electromagnetic waves can move along the same line.
In each case the source emits a wave of the same frequency, and in each
case only the source or the observer is moving. The arrow in each situation
denotes the velocity vector, which has the same magnitude in each situation.
When there is no arrow, the observer or the source is stationary. Rank the fre-
quencies of the observed electromagnetic waves in descending order (largest
fi rst) according to magnitude. (a) A and B (a tie), C and D (a tie) (b) C and D
(a tie), A and B (a tie) (c) A and D (a tie), B and C (a tie) (d) B and D (a tie), A and C (a tie) (e) B and C (a tie), A and D (a tie)
QUESTION 6
A
Observer Source
B
C
D
Section 24.6 Polarization 10. The drawing shows two sheets of polarizing material. Polarizer 1 has its transmission axis aligned vertically, and polarizer 2 has its transmission
axis aligned at an angle of 45° with respect to the vertical. Light that is com-
pletely polarized along the vertical direction is incident either from the far
left or from the far right. In either case, the average intensity of the incident
light is the same. Which one of the following statements is true concerning
the average intensity of the light that is transmitted by the pair of sheets?
(a) When the light is incident from either the left or the right, the transmitted intensity is one-half the incident intensity. (b) When the light is incident from either the left or the right, the transmitted intensity is one-fourth the incident
intensity. (c) When the light is incident from the left, the transmitted intensity is one-half the incident intensity; when the light is incident from the right,
the transmitted intensity is zero. (d) When the light is incident from the left, the transmitted intensity is one-fourth the incident intensity; when the light
is incident from the right, the transmitted intensity is one-half the incident
intensity. (e) When the light is incident from the left, the transmitted intensity is one-half the incident intensity; when the light is incident from the right, the
transmitted intensity is one-fourth the incident intensity.
QUESTION 10
45°
Polarizer 1 Polarizer 2
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 24.1 The Nature of Electromagnetic Waves 1. E The team monitoring a space probe exploring the outer solar system fi nds that radio transmissions from the probe take 2.53 hours to reach earth.
How distant (in meters) is the probe?
2. E (a) Neil A. Armstrong was the fi rst person to walk on the moon. The distance between the earth and the moon is 3.85 × 108 m. Find the time it
took for his voice to reach the earth via radio waves. (b) Someday a person will walk on Mars, which is 5.6 × 1010 m from the earth at the point of closest
approach. Determine the minimum time that will be required for a message
from Mars to reach the earth via radio waves.
3. E SSM In astronomy, distances are often expressed in light-years. One light-year is the distance traveled by light in one year. The dis-
tance to Alpha Centauri, the closest star other than our own sun that can
be seen by the naked eye, is 4.3 light-years. Express this distance in
meters.
4. E GO FM radio stations use radio waves with frequencies from 88.0 to 108 MHz to broadcast their signals. Assuming that the inductance in
Figure 24.4 has a value of 6.00 × 10−7 H, determine the range of capacitance values that are needed so the antenna can pick up all the radio waves broad-
casted by FM stations.
5. M SSM Available in WileyPLUS. 6. H Available in WileyPLUS.
Problems
706 CHAPTER 24 Electromagnetic Waves
Section 24.2 The Electromagnetic Spectrum 7. E A truck driver is broadcasting at a frequency of 26.965 MHz with a CB (citizen’s band) radio. Determine the wavelength of the electromagnetic
wave being used. The speed of light is c = 2.9979 × 108 m/s. 8. E In a dentist’s offi ce an X-ray of a tooth is taken using X-rays that have a frequency of 6.05 × 1018 Hz. What is the wavelength in vacuum of these
X-rays?
9. E SSM In a certain UHF radio wave, the shortest distance between posi- tions at which the electric and magnetic fi elds are zero is 0.34 m. Determine
the frequency of this UHF radio wave.
10. E FM radio waves have frequencies between 88.0 and 108.0 MHz. Determine the range of wavelengths for these waves.
11. E BIO Magnetic resonance imaging, or MRI (see Section 21.7), and positron emission tomography, or PET scanning (see Section 32.6), are two
medical diagnostic techniques. Both employ electromagnetic waves. For
these waves, fi nd the ratio of the MRI wavelength (frequency = 6.38 × 107 Hz)
to the PET scanning wavelength (frequency = 1.23 × 1020 Hz).
12. E GO A certain type of laser emits light that has a frequency of 5.2 × 1014 Hz. The light, however, occurs as a series of short pulses, each lasting
for a time of 2.7 × 10−11 s. (a) How many wavelengths are there in one pulse? (b) The light enters a pool of water. The frequency of the light remains the same, but the speed of the light slows down to 2.3 × 108 m/s. How many
wavelengths are there now in one pulse?
13. E Two radio waves are used in the operation of a cellular telephone. To receive a call, the phone detects the wave emitted at one frequency by the
transmitter station or base unit. To send your message to the base unit, your
phone emits its own wave at a diff erent frequency. The diff erence between
these two frequencies is fi xed for all channels of cell phone operation. Sup-
pose that the wavelength of the wave emitted by the base unit is 0.34339 m
and the wavelength of the wave emitted by the phone is 0.36205 m. Using
a value of 2.9979 × 108 m/s for the speed of light, determine the diff erence
between the two frequencies used in the operation of a cell phone.
14. M V-HINT A positively charged object with a mass of 0.115 kg oscillates at the end of a spring, generating ELF (extremely low frequency) radio waves
that have a wavelength of 4.80 × 107 m. The frequency of these radio waves
is the same as the frequency at which the object oscillates. What is the spring
constant of the spring?
Section 24.3 The Speed of Light 15. E Review Conceptual Example 3 for information pertinent to this prob- lem. When we look at the star Polaris (the North Star), we are seeing it as it
was 680 years ago. How far away from us (in meters) is Polaris?
16. E GO Figure 24.12 illustrates Michelson’s setup for measuring the speed of light with the mirrors placed on Mt. San Antonio and Mt. Wilson
in California, which are 35 km apart. Using a value of 3.00 × 108 m/s for
the speed of light, fi nd the minimum angular speed (in rev/s) for the rotating
mirror.
17. E SSM Two astronauts are 1.5 m apart in their spaceship. One speaks to the other. The conversation is transmitted to earth via electromagnetic waves.
The time it takes for sound waves to travel at 343 m/s through the air between
the astronauts equals the time it takes for the electromagnetic waves to travel
to the earth. How far away from the earth is the spaceship?
18. E V-HINT A laptop computer communicates with a router wirelessly, by means of radio signals. The router is connected by cable directly to the Inter-
net. The laptop is 8.1 m from the router, and is downloading text and images
from the Internet at an average rate of 260 Mbps, or 260 megabits per second.
(A bit, or binary digit, is the smallest unit of digital information.) On average, how many bits are downloaded to the laptop in the time it takes the wireless
signal to travel from the router to the laptop?
19. E A lidar (laser radar) gun is an alternative to the standard radar gun that uses the Doppler eff ect to catch speeders. A lidar gun uses an infrared laser
and emits a precisely timed series of pulses of infrared electromagnetic waves.
The time for each pulse to travel to the speeding vehicle and return to the gun
is measured. In one situation a lidar gun in a stationary police car observes a
diff erence of 1.27 × 10−7 s in round-trip travel times for two pulses that are
emitted 0.450 s apart. Assuming that the speeding vehicle is approaching the
police car essentially head-on, determine the speed of the vehicle.
20. M GO A politician holds a press conference that is televised live. The sound picked up by the microphone of a TV news network is broadcast via
electromagnetic waves and heard by a television viewer. This viewer is seated
2.3 m from his television set. A reporter at the press conference is located
4.1 m from the politician, and the sound of the words travels directly from the
celebrity’s mouth, through the air, and into the reporter’s ears. The reporter
hears the words exactly at the same instant that the television viewer hears them. Using a value of 343 m/s for the speed of sound, determine the max-
imum distance between the television set and the politician. Ignore the small
distance between the politician and the microphone. In addition, assume that
the only delay between what the microphone picks up and the sound being
emitted by the television set is that due to the travel time of the electromag-
netic waves used by the network.
21. M GO A mirror faces a cliff located some distance away. Mounted on the cliff is a second mirror, directly opposite the fi rst mirror and facing toward
it. A gun is fi red very close to the fi rst mirror. The speed of sound is 343 m/s.
How many times does the fl ash of the gunshot travel the round-trip distance
between the mirrors before the echo of the gunshot is heard?
Section 24.4 The Energy Carried by Electromagnetic Waves 22. E A laser emits a narrow beam of light. The radius of the beam is 1.0 × 10−3 m, and the power is 1.2 × 10−3 W. What is the intensity of the laser beam?
23. E An industrial laser is used to burn a hole through a piece of metal. The average intensity of the light is S = 1.23 × 109 W/m2. What is the rms value of (a) the electric fi eld and (b) the magnetic fi eld in the electromag- netic wave emitted by the laser?
24. E The maximum strength of the magnetic fi eld in an electromagnetic wave is 3.3 × 10−6 T. What is the maximum strength of the wave’s electric
fi eld?
25. E SSM The microwave radiation left over from the Big Bang explosion of the universe has an average energy density of 4 × 10−14 J/m3. What is the
rms value of the electric fi eld of this radiation?
26. E GO On a cloudless day, the sunlight that reaches the surface of the earth has an intensity of about 1.0 × 103 W/m2. What is the electromagnetic
energy contained in 5.5 m3 of space just above the earth’s surface?
27. E SSM Available in WileyPLUS. 28. E GO Consult Multiple-Concept Example 5 to review the concepts on which this problem depends. A light bulb emits light uniformly in all direc-
tions. The average emitted power is 150.0 W. At a distance of 5.00 m from
the bulb, determine (a) the average intensity of the light, (b) the rms value of the electric fi eld, and (c) the peak value of the electric fi eld. 29. E Multiple-Concept Example 5 provides some pertinent background for this problem. The mean distance between earth and the sun is 1.50 × 1011 m.
The average intensity of solar radiation incident on the upper atmosphere of
the earth is 1390 W/m2. Assuming that the sun emits radiation uniformly in
all directions, determine the total power radiated by the sun.
30. E GO A stationary particle of charge q = 2.6 × 10−8 C is placed in a laser beam (an electromagnetic wave) whose intensity is 2.5 × 103 W/m2. De-
termine the magnitudes of the (a) electric and (b) magnetic forces exerted on the charge. If the charge is moving at a speed of 3.7 × 104 m/s perpendicular
Problems 707
to the magnetic fi eld of the electromagnetic wave, fi nd the magnitudes of the
(c) electric and (d) magnetic forces exerted on the particle. 31. M The power radiated by the sun is 3.9 × 1026 W. The earth orbits the sun in a nearly circular orbit of radius 1.5 × 1011 m. The earth’s axis of ro-
tation is tilted by 27° relative to the plane of the orbit (see the drawing), so
sunlight does not strike the equator perpendicularly. What power strikes a
0.75-m2 patch of fl at land at the equator at point Q?
PROBLEM 31
Equator
27° Sunlight
Axis of rotation
Q
32. M V-HINT An electromagnetic wave strikes a 1.30-cm2 section of wall perpendicularly. The rms value of the wave’s magnetic fi eld is determined
to be 6.80 × 10−4 T. How long does it take for the wave to deliver 1850 J of
energy to the wall?
33. M BIO A heat lamp emits infrared radiation whose rms electric fi eld is Erms = 2800 N/C. (a) What is the average intensity of the radiation? (b) The radiation is focused on a person’s leg over a circular area of radius 4.0 cm.
What is the average power delivered to the leg? (c) The portion of the leg being irradiated has a mass of 0.28 kg and a specifi c heat capacity of 3500 J/(kg · C°). How long does it take to raise its temperature by 2.0 C°? Assume that there is
no other heat transfer into or out of the portion of the leg being heated.
34. H Available in WileyPLUS.
Section 24.5 The Doppler Eff ect and Electromagnetic Waves 35. E MMH A distant galaxy emits light that has a wavelength of 434.1 nm. On earth, the wavelength of this light is measured to be 438.6 nm. (a) Decide whether this galaxy is approaching or receding from the earth. Give your
reasoning. (b) Find the speed of the galaxy relative to the earth. 36. E GO A speeder is pulling directly away and increasing his distance from a police car that is moving at 25 m/s with respect to the ground. The
radar gun in the police car emits an electromagnetic wave with a frequency
of 7.0 × 109 Hz. The wave refl ects from the speeder’s car and returns to the
police car, where its frequency is measured to be 320 Hz less than the emitted
frequency. Find the speeder’s speed with respect to the ground.
37. M CHALK SSM A distant galaxy is simultan eously rotating and receding from the
earth. As the drawing shows, the galactic center
is receding from the earth at a relative speed
of uG = 1.6 × 106 m/s. Relative to the center, the tangential speed is 𝜐T = 0.4 × 10
6 m/s for
locations A and B, which are equidistant from the center. When the frequencies of the light
coming from regions A and B are measured on earth, they are not the same and each is diff erent
from the emitted frequency of 6.200 × 1014 Hz.
Find the measured frequency for the light from
(a) region A and (b) region B. 38. M GO The drawing shows three situations— A, B, and C—in which an observer and a source
of electromagnetic waves are moving along the
same line. In each case the source emits a wave that
has a frequency of 4.57 × 1014 Hz. The arrows in each situation denote velocity
vectors of the observer and source relative to the ground and have the magnitudes
indicated (𝜐 or 2𝜐), where the speed 𝜐 is 1.50 × 106 m/s. Calculate the observed
frequency in each of the three cases.
PROBLEM 38
A
Observer Source
B
C
2
2
υ
υ
υ
υ
υ
υ
Section 24.6 Polarization 39. E Unpolarized light whose intensity is 1.10 W/m2 is incident on the polarizer in Figure 24.20. (a) What is the intensity of the light leaving the polarizer? (b) If the analyzer is set at an angle of 𝜃 = 75° with respect to the polarizer, what is the intensity of the light that reaches the photocell?
40. E GO The drawing shows three polarizer/analyzer pairs. The incident light beam for each pair is unpolarized and has the same average intensity of
48 W/m2. Find the average intensity of the transmitted beam for each of the
three cases (A, B, and C) shown in the drawing.
PROBLEM 40
Incident beam
30.0°
Transmitted beam
30.0°
30.0° 60.0°
60.0° 30.0°
A
B
C
41. E SSM The average intensity of light emerging from a polarizing sheet is 0.764 W/m2, and the average intensity of the horizontally polarized light
incident on the sheet is 0.883 W/m2. Determine the angle that the transmis-
sion axis of the polarizing sheet makes with the horizontal.
42. E GO Light that is polarized along the vertical direction is incident on a sheet of polarizing material. Only 94% of the intensity of the light passes
through the sheet and strikes a second sheet of polarizing material. No light
passes through the second sheet. What angle does the transmission axis of the
second sheet make with the vertical?
43. E Available in WileyPLUS. 44. E GO The drawing shows light incident on a polarizer whose transmis- sion axis is parallel to the z axis. The polarizer is rotated clockwise through an angle 𝛼. The average intensity of the incident light is 7.0 W/m2. Determine the average intensity of the transmitted light for each of the six cases shown
in the table.
Earth
Galaxy
uG
T
T
BA
PROBLEM 37
708 CHAPTER 24 Electromagnetic Waves
Intensity of Transmitted Light Incident Light 𝞪 = 0° 𝞪 = 35° (a) Unpolarized
(b) Polarized parallel to z axis
(c) Polarized parallel to y axis
PROBLEM 44
Incident light
Transmitted light
x
z
y
45. E MMH For each of the three sheets of polarizing material shown in the drawing, the orientation of the transmission axis is labeled relative to the ver-
tical. The incident beam of light is unpolarized and has an intensity of 1260.0
W/m2. What is the intensity of the beam transmitted through the three sheets
when 𝜃1 = 19.0°, 𝜃2 = 55.0°, and 𝜃3 = 100.0°?
PROBLEM 45
Incident beam
Vertical
1 2
Transmitted beam
3θ θ θ
46. M V-HINT Before attempting this problem, review Conceptual Example 7. The intensity of the light that reaches the photocell in Figure 24.23a is 110 W/m2, when 𝜃 = 23°. What would be the intensity reaching the photocell
if the analyzer were removed from the setup, everything else remaining the same?
47. M SSM More than one analyzer can be used in a setup like the one in Figure 24.20, each analyzer following the previous one. Suppose that the transmission axis of the fi rst analyzer is rotated 27° relative to the transmis-
sion axis of the polarizer, and that the transmission axis of each additional
analyzer is rotated 27° relative to the transmission axis of the previous one.
What is the minimum number of analyzers needed for the light reaching the
photocell to have an intensity that is reduced by at least a factor of 100 relat-
ive to the intensity of the light striking the fi rst analyzer?
48. M CHALK GO The drawing shows four sheets of polarizing material, each with its transmission axis oriented diff erently. Light that is polarized
in the vertical direction is incident from the left and has an average intens-
ity of 27 W/m2. Determine the average intensity of the light that emerges
on the right in the drawing when sheet A alone is removed, when sheet B
alone is removed, when sheet C alone is removed, and when sheet D alone
is removed.
30°Vertical Horizontal 60°
Light
A B C D
PROBLEM 48
49. E Obtain the wavelengths in vacuum for (a) blue light whose frequency is 6.34 × 1014 Hz, and (b) orange light whose frequency is 4.95 × 1014 Hz. Express your answers in nanometers (1 nm = 10−9 m).
50. E GO The magnitude of the electric fi eld of an electromagnetic wave increases from 315 to 945 N/C. (a) Determine the wave intensities for the two values of the electric fi eld. (b) What is the magnitude of the magnetic fi eld associated with each electric fi eld? (c) Determine the wave intensity for each value of the magnetic fi eld.
51. E SSM Available in WileyPLUS. 52. E BIO The human eye is most sensitive to light with a frequency of about 5.5 × 1014 Hz, which is in the yellow-green region of the electromag-
netic spectrum. How many wavelengths of this light can fi t across the width
of your thumb, a distance of about 2.0 cm?
53. E SSM A future space station in orbit about the earth is being powered by an electromagnetic beam from the earth. The beam has a cross-sectional
area of 135 m2 and transmits an average power of 1.20 × 104 W. What are the
rms values of the (a) electric and (b) magnetic fi elds? 54. E V-HINT Suppose that a police car is moving to the right at 27 m/s, while a speeder is coming up from behind at a speed of 39 m/s, both speeds being
with respect to the ground. Assume that the electromagnetic wave emitted by
the police car’s radar gun has a frequency of 8.0 × 109 Hz. Find the diff erence
between the frequency of the wave that returns to the police car after refl ecting
from the speeder’s car and the original frequency emitted by the police car.
55. E SSM Available in WileyPLUS. 56. M CHALK GO The electromagnetic wave that delivers a cellular phone call to a car has a magnetic fi eld with an rms value of 1.5 × 10−10 T. The
wave passes perpendicularly through an open window, the area of which is
0.20 m2. How much energy does this wave carry through the window during
a 45-s phone call?
57. M Available in WileyPLUS. 58. M V-HINT A beam of polarized light with an average intensity of 15 W/m2 is sent through a polarizer. The transmission axis makes an angle of 25° with
respect to the direction of polarization. Determine the rms value of the elec-
tric fi eld of the transmitted beam.
59. M An argon–ion laser produces a cylindrical beam of light whose average power is 0.750 W. How much energy is contained in a 2.50-m length
of the beam?
60. M V-HINT What fraction of the power radiated by the sun is intercepted by the planet Mercury? The radius of Mercury is 2.44 × 106 m, and its mean
distance from the sun is 5.79 × 1010 m. Assume that the sun radiates uni-
formly in all directions.
Additional Problems
Concepts and Calculations Problems 709
61. M SSM MMH The drawing shows an edge-on view of the solar panels on a communications satellite. The dashed line specifi es the normal to the
panels. Sunlight strikes the panels at an angle 𝜃 with respect to the normal.
If the solar power impinging on the panels is 2600 W when 𝜃 = 65°, what is
it when 𝜃 = 25°?
PROBLEM 61
Normal
Sunlight
θ
62. H Available in WileyPLUS. 63. M GO SSM Police use radar guns and the Doppler eff ect to catch speed- ers. The fi gure illustrates a moving car approaching a stationary police car. A
radar gun emits an electromagnetic wave that refl ects from the oncoming car.
The refl ected wave returns to the police car with a frequency (measured by
on-board equipment) that is diff erent from the emitted frequency. One such
radar gun emits a wave whose frequency is 8.0 × 109 Hz. When the speed of
the car is 39 m/s and the approach is essentially head-on, what is the diff er- ence between the frequency of the wave returning to the police car and that emitted by the radar gun?
Outgoing electromagnetic
wave
Reflected electromagnetic
wave
PROBLEM 63
One of the central ideas of this chapter is that electromagnetic waves carry
energy. Two concepts are used to describe this energy—the wave’s intensity
and its energy density. Problem 64 reviews this important idea. We have seen
how the intensities of completely polarized or completely unpolarized light
beams can change when they pass through a polarizer. But what about light
that is partially polarized or partially unpolarized? Can the concepts that we
discussed in Section 24.6 be applied to such light? The answer is “yes,” and
Problem 65 illustrates how.
64. M CHALK The fi gure shows the popular dish antenna that receives digital TV signals from a satellite. The average intensity of the electromagnetic wave
that carries a particular TV program is S = 7.5 × 10−14 W/m2, and the circu- lar aperture of the antenna has a radius of r = 15 cm. Concepts: (i) How is the average power passing through the circular aperture of the antenna related to
the average intensity of the TV signal? (ii) How much energy does the antenna
receive in a time t? (iii) What is the average energy density, or average energy per unit volume, of the electromagnetic wave? Calculations: (a) Determine the electromagnetic energy delivered to the dish during a one-hour program.
(b) What is the average energy density of the electromagnetic wave? 65. M CHALK SSM The light beam in the fi gure passes through a polarizer whose transmission axis makes an angle ϕ with the vertical. The beam is partially polarized and partially unpolarized, and the average intensity S0 of the incident light is the sum of the average intensity S0, polar of the po- larized light and the average intensity S0, unpolar of the unpolarized light; S0 = S0, polar + S0, unpolar. The intensity S of the transmitted light is also the sum of two parts: S = Spolar + Sunpolar. As the polarizer is rotated clockwise, the intensity of the transmitted light has a minimum value of S = 2.0 W/m2 when ϕ = 20.0° and has a maximum value of S = 8.0 W/m2 when the angle is ϕ = ϕmax. Concepts: (i) How is Sunpolar related to S0, unpolar? (ii) How is Spolar related to S0, polar? (iii) The minimum transmitted intensity is 2.0 W/m2. Why isn’t it 0 W/m2? Calculations: (a) What is the intensity S0, unpolar of the incident light that is unpolarized? (b) What is the intensity S0, polar of the incident light that is polarized?
PROBLEM 65
Incident light
Transmitted light
0 = 0, polar + 0, unpolar
S–S–
S– S– S–
S– = polar + unpolar
Concepts and Calculations Problems
TV signal
Area A
r
x = ct
PROBLEM 64
710 CHAPTER 24 Electromagnetic Waves
66. M A Turbo-shaft Helicopter. You and your team are tasked with cov- ertly acquiring information about a new helicopter being developed by an adversary. You are given a handheld device that has many functions, one of which is to send out a broad pulse of electromagnetic waves at a frequency of f0 = 9.00 × 109 Hz, and then collect the scattered light that returns from whatever it hits. The device then analyzes the scattered light and returns a graph of maximum frequency shift as a function of collection angle (see the drawing). The device also has a built-in rangefi nder that measures the dis- tance to an object. As the helicopter engine powers up and the helicopter just starts to lift off the ground, you point the device at it and pull the trigger. It sends out a pulse and, a few seconds later, it gives you (i) the distance to the helicopter (d = 82.7 m), and (ii) a graph of the frequency shift (Δf) versus collection angle, as shown in the fi gure. (a) Assuming that light detected by your device has scattered from the moving rotor of the helicopter, what is the diameter of the rotor? (b) What is the speed of the tips of the rotor? (c) What is the rotational speed (in rpm) of the rotor?
PROBLEM 66
θ (deg.)
−12.48 kHZ
+12.48 kHZ
+5.35°
−5.35°
Δf (kHz)
67. M A Magneto-optic Device. The Faraday eff ect is a magneto-optic phenomenon where the polarization of linearly polarized light rotates when
the light passes through a magnetized material. You and your team are tasked with analyzing the results of an experiment designed to measure how much a certain thin magnetic fi lm rotates the polarization of the light that passes through it. As the drawing shows, an unpolarized laser beam of average in- tensity S0 = 1000 W/m2 passes through a vertical polarizer. It then passes through a thin magnetic fi lm that can be in one of three states: (i) unmag- netized, (ii) magnetized to the right (when looking from the laser), and (iii) magnetized to the left. It is assumed that the fi lm does not absorb any of the light. The light then passes through another polarizer (called the analyzer) whose transmission axis is rotated 7.50° clockwise from the horizontal (when looking from the laser). (a) What is the intensity of the beam after it passes through the fi rst polarizer? (b) In the case that the fi lm is unmagnetized, the polarization will not rotate when it passes through the fi lm. What should be the light intensity measured at the detector? (c) When the fi lm is magnet- ized to the left, the intensity measured by the detector is IL = 12.2 W/m2, and when magnetized to the right the intensity is IR = 5.46 W/m2. In each case, determine the direction (clockwise or counterclockwise when looking from the laser) and the magnitude of the angle through which the magnetic fi lm rotates the polarization of the light from the vertical.
Unpolarized light
Thin magnetic film
Light detector
Vertical Polarizer Analyzer
LASER
PROBLEM 67
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
25.1 Relate wave fronts and rays.
25.2 Apply the law of reflection to plane mirrors.
25.3 Describe image formation by a plane mirror.
25.4 Calculate the focal length of a spherical mirror.
25.5 Perform ray tracing for spherical mirrors.
25.6 Use the mirror and magnification equations to solve problems.
D ig
it al
V is
io n /G
et ty
I m
ag es
CHAPTER 25
The Reflection of Light: Mirrors
The image of the zebras drinking at the waterhole is produced when light refl ects from the plane surface
of the water, which acts as a mirror. This chapter discusses the images formed by the refl ection of light
from plane and spherical mirrors.
25.1 Wave Fronts and Rays Mirrors are usually close at hand. It is diffi cult, for example, to put on makeup, shave,
or drive a car without them. We see images in mirrors because some of the light that
strikes them is refl ected into our eyes. To discuss refl ection, it is necessary to introduce
the concepts of a wave front and a ray of light, and we can do so by taking advantage of
the familiar topic of sound waves (see Chapter 16). Both sound and light are kinds of
waves. Sound is a pressure wave, whereas light is electromagnetic in nature. However,
the ideas of a wave front and a ray apply to both.
Consider a small spherical object whose surface is pulsating in simple harmonic
motion. A sound wave is emitted that moves spherically outward from the object
at a constant speed. To represent this wave, we draw surfaces through all points of
the wave that are in the same phase of motion. These surfaces of constant phase are
called wave fronts. Figure 25.1 shows a hemispherical view of the wave fronts. In this view they appear as concentric spherical shells about the vibrating object. If
the wave fronts are drawn through the condensations, or crests, of the sound wave,
as they are in the picture, the distance between adjacent wave fronts equals the
wavelength 𝜆. The radial lines pointing outward from the source and perpendicular to the wave fronts are called rays. The rays point in the direction of the velocity of the wave.
711
712 CHAPTER 25 The Reflection of Light: Mirrors
l
Wave fronts
Pulsating sphere
Rays
FIGURE 25.1 A hemispherical view of a sound wave emitted by a pulsating sphere.
The wave fronts are drawn through the
condensations of the wave, so the distance
between two successive wave fronts is the
wavelength 𝜆. The rays are perpendicular to the wave fronts and point in the direction of
the velocity of the wave.
Rays
Curved wave fronts
Pulsating sphere
(a) (b)
Plane wave fronts
FIGURE 25.2 (a) Portions of two spherical wave fronts are shown. The rays are perpendicular to the wave fronts and diverge. (b) For a plane wave, the wave fronts are fl at surfaces, and the rays are parallel to each other.
Figure 25.2a shows small sections of two adjacent spherical wave fronts. At large distances from the source, the wave fronts become less and less curved and approach the shape of fl at
surfaces, as in part b of the drawing. Waves whose wave fronts are fl at surfaces (i.e., planes) are known as plane waves and are important in understanding the properties of mirrors and lenses. Since rays are perpendicular to the wave fronts, the rays for a plane wave are parallel to each other.
The concepts of wave fronts and rays can also be used to describe light waves. For light
waves, the ray concept is particularly convenient when showing the path taken by the light. We
will make frequent use of light rays, which can be regarded essentially as narrow beams of light
much like those that lasers produce.
25.2 The Reflection of Light Most objects refl ect a certain portion of the light falling on them. Suppose that a ray of light is
incident on a fl at, shiny surface, such as the mirror in Figure 25.3. As the drawing shows, the angle of incidence 𝜃i is the angle that the incident ray makes with respect to the normal, which is a line drawn perpendicular to the surface at the point of incidence. The angle of refl ection 𝜃r is the angle that the refl ected ray makes with the normal. The law of refl ection describes the behavior of the incident and refl ected rays.
LAW OF REFLECTION The incident ray, the refl ected ray, and the normal to the surface all lie in the same plane, and the angle of refl ection 𝞱r equals the angle of incidence 𝞱i:
𝞱r = 𝞱i
When parallel light rays strike a smooth, plane surface, such as the ones in Figure 25.4a, the refl ected rays are parallel to each other. This type of refl ection is one example of what is known
as specular refl ection and is important in determining the properties of mirrors. Most surfaces, however, are not perfectly smooth, because they contain irregularities the sizes of which are equal
to or greater than the wavelength of the light. The law of refl ection applies to each ray, but the
irregular surface refl ects the light rays in various directions, as Figure 25.4b suggests. This type
Normal
Incident ray
Mirror
i
r
Reflected ray
θ θ
FIGURE 25.3 The angle of refl ection 𝜃r equals the angle of incidence 𝜃i. These angles are measured with respect to the normal,
which is a line drawn perpendicular to the
surface of the mirror at the point of incidence.
(a) Specular reflection (b) Diffuse reflection
FIGURE 25.4 (a) The drawing shows specular refl ection from a polished plane surface, such
as a mirror. The refl ected rays are parallel to
each other. (b) A rough surface refl ects the light rays in all directions; this type of refl ection is
known as diff use refl ection.
25.3 The Formation of Images by a Plane Mirror 713
of refl ection is known as diff use refl ection. Common surfaces that give rise to diff use refl ection are most papers, wood, nonpolished metals, and walls covered with a “fl at” (nongloss) paint.
THE PHYSICS OF . . . digital movie projectors and micromirrors. A revolution in digital technology is occurring in the movie industry, where digital techniques are now being
used to produce fi lms. Until recently, fi lms have been viewed primarily by using projectors that
shine light directly through a strip of fi lm containing the images. Now, however, projectors are
available that allow a movie produced using digital techniques to be viewed completely without
fi lm by using a digital representation (zeros and ones) of the images. One form of digital projec-
tor depends on the law of refl ection and tiny mirrors called micromirrors, each about the size of
one-fourth the diameter of a human hair. Each micromirror creates a tiny portion of an individual
movie frame on the screen and serves as a pixel, like one of the glowing spots that comprise the
picture on a TV screen or computer monitor. This pixel action is possible because a micromirror
pivots about 10° in one direction or the reverse in response to the “zero” or “one” in the digital
representation of the frame. One of the directions puts a portion of the light from a powerful
xenon lamp on the screen, and the other does not. The pivoting action can occur as fast as 1000
times per second, leading to a series of light pulses for each pixel that the eye and the brain
combine and interpret as a continuously changing image. Present-generation digital micromirror
projectors use up to several million micromirrors to reproduce each of the three primary colors
(red, green, and blue) that comprise a color image.
25.3 The Formation of Images by a Plane Mirror When you look into a plane (fl at) mirror, you see an image of yourself that has three properties:
1. The image is upright. 2. The image is the same size as you are. 3. The image is located as far behind the mirror as you are in front of it. As Figure 25.5a illustrates, the image of yourself in the mirror is also reversed right to left and left to right. If you wave your right hand, it is the left hand of the image that waves back. Similarly, letters and words held up to a mirror are reversed. Ambulances and other emergency
vehicles are often lettered in reverse, as in Figure 25.5b, so that the letters will appear normal when seen in the rearview mirror of a car.
To illustrate why an image appears to originate from behind a plane mirror, Figure 25.6a shows a light ray leaving the top of an object. This ray refl ects from the mirror (angle of refl ection
equals angle of incidence) and enters the eye. To the eye, it appears that the ray originates from
behind the mirror, somewhere back along the dashed line. Actually, rays going in all directions
leave each point on the object, but only a small bundle of such rays is intercepted by the eye. Part b of the fi gure shows a bundle of two rays leaving the top of the object. All the rays that leave a
given point on the object, no matter what angle 𝜃 they have when they strike the mirror, appear
to originate from a corresponding point on the image behind the mirror (see the dashed lines in
part b). For each point on the object, there is a single corresponding point on the image, and it is this fact that makes the image in a plane mirror a sharp and undistorted one.
Although rays of light seem to come from the image, it is evident from Figure 25.6b that they do not originate from behind the plane mirror where the image appears to be. Because none
(b)
(a)
Right hand Left hand
of image
Dennis MacDonald/Age Fotostock
FIGURE 25.5 (a) The person’s right hand becomes the image’s left hand in a plane
mirror. (b) Many emergency vehicles are reverse-lettered so the lettering appears normal
when viewed in the rearview mirror of a car.
Plane mirror
(a)
Object
Apparent path of light ray
Eye
(b)
Object Virtual image
Eye
θ
θ
FIGURE 25.6 (a) A ray of light from the top of the chess piece refl ects from the mirror. To
the eye, the ray seems to come from behind
the mirror. (b) The bundle of rays from the top of the object appears to originate from
the image behind the mirror.
714 CHAPTER 25 The Reflection of Light: Mirrors
of the light rays actually emanate from the image, it is called a virtual image. In this text the parts of the light rays that appear to come from a virtual image are represented by dashed lines.
Curved mirrors, on the other hand, can produce images from which all the light rays actually do emanate. Such images are known as real images and are discussed later.
With the aid of the law of refl ection, it is possible to show that the image is located as far
behind a plane mirror as the object is in front of it. In Figure 25.7 the object distance is do and the image distance is di. A ray of light leaves the base of the object, strikes the mirror at an angle of incidence 𝜃, and is refl ected at the same angle. To the eye, this ray appears to come from the
base of the image. For the angles 𝛽1 and 𝛽2 in the drawing it follows that 𝜃 + 𝛽1 = 90° and 𝛼 + 𝛽2 = 90°. But the angle 𝛼 is equal to the angle of refl ection 𝜃, since the two are opposite angles formed by intersecting lines. Therefore, 𝛽1 = 𝛽2. As a result, triangles ABC and DBC are identical (congruent) because they share a common side BC and have equal angles (𝛽1 = 𝛽2) at the top and equal angles (90°) at the base. Thus, the magnitude of the object distance do equals the magnitude of the image distance di.
By starting with a light ray from the top of the object, rather than the bottom, we can use the
same line of reasoning to show also that the height of the image equals the height of the object.
Conceptual Examples 1 and 2 discuss some interesting features of plane mirrors.
BNormal
1 2
dido
A C D
90°90°
θ
θ
β β
α
FIGURE 25.7 This drawing illustrates the geometry used with a plane mirror to show
that the image distance di equals the object distance do.
CONCEPTUAL EXAMPLE 1 Full-Length Versus Half-Length Mirrors
In Figure 25.8 a woman is standing in front of a plane mirror. Is the mini- mum mirror height that is necessary for her to see her full image (a) equal to her height, or (b) equal to one-half her height?
Reasoning The woman sees her image because light emanating from her body is refl ected by the mirror (labeled ABCD in Figure 25.8) and enters her eyes. Consider, for example, a ray of light from her foot F. This ray strikes the mirror at B and enters her eyes at E. According to the law of refl ection, the angles of incidence and refl ection are both 𝜃. This law will
allow us to deduce how the height of the mirror is related to her own height.
Answer (a) is incorrect. The mirror in Figure 25.8 is the same height as the woman. Any light from her foot that strikes the mirror below B is refl ected toward a point on her body that is below her eyes. Since light
striking the mirror below B does not enter her eyes, the part of the mirror between B and A may be removed. Thus, the necessary minimum height of the mirror is not equal to the woman’s height.
Answer (b) is correct. As discussed above, the section AB of the mirror is not necessary in order for the woman to see her full image. The section
BC of the mirror that produces the image is one-half the woman’s height between F and E. This follows because the right triangles FBM and EBM are identical. They are identical because they share a common side BM and have two angles, 𝜃 and 90°, that are the same. The blowup in Figure 25.8 illustrates a similar line of reasoning, starting with a ray from the woman’s head at H. This ray is refl ected from the mirror at P and enters her eyes. The top mirror section PD may be removed without disturbing this refl ection. The necessary section CP is one-half the woman’s height between her head at H and her eyes at E. We fi nd, then, that only the
sections BC and CP are needed for the woman to see her full length. The height of section BC plus section CP is exactly one-half the woman’s height. The conclusions here are valid regardless of how far the person
stands from the mirror. Thus, to view one’s full length in a mirror, only a
half-length mirror is needed.
Related Homework: Problems 7, 39
H
M
D
C
P
B
AF
E
H D
CE
90° 90°
θ
θ
FIGURE 25.8 A woman stands in front of a plane mirror and sees her full image.
CONCEPTUAL EXAMPLE 2 Multiple Reflections
A person is sitting in front of two mirrors that intersect at a 90° angle.
As Figure 25.9a illustrates, the person sees three images of herself. (The person herself is only partially visible at the bottom of the photo.) These
images arise because rays of light emanate from her body, refl ect from
the mirrors, and enter her eyes. Consider the light that enters her eyes and
appears to come from each of the three images identifi ed in Figure 25.9b. The following table shows three possibilities for the number of refl ections
that the light undergoes before entering her eyes. Which one is correct?
25.3 The Formation of Images by a Plane Mirror 715
Number of Reflections Possibility Image 1 Image 2 Image 3 (a) 2 2 3
(b) 3 3 3
(c) 1 1 2
Reasoning Images of the woman are formed when light emanating from her body enters her eyes after being refl ected by one, or both, mir-
rors. For each refl ection, the angle of the light refl ected from a mirror is
equal to the angle of the light incident on the mirror (law of refl ection).
We will see that there are three ways that light can reach her eyes from
the two mirrors.
Answers (a) and (b) are incorrect. Figure 25.9b represents a top view of the person in front of the two mirrors and has been repeated in the
margin for convenience. It is a straightforward matter to understand two
of the images that she sees. These are the images that are normally seen
when one sits in front of a mirror. Sitting in front of mirror 1, she sees
image 1, which is located as far behind that mirror as she is in front of
it. She also sees image 2 behind mirror 2, at a distance that matches her
distance in front of that mirror. Each of these images arises from light
emanating from her body and refl ecting only once from a single mirror.
Therefore, each ray of light does not refl ect two or three times before
entering her eyes.
Answer (c) is correct. As discussed above, images 1 and 2 arise, respectively, from single refl ections from mirrors 1 and 2. The third image arises when light undergoes two refl ections in sequence, fi rst from one
mirror and then from the other. When such a double refl ection occurs, an
additional image becomes possible. Figure 25.9b shows two rays of light that strike mirror 1. Each one, according to the law of refl ection, has an
angle of refl ection that equals the angle of incidence. The rays then strike
mirror 2, where they again are refl ected according to the law of refl ection.
When the outgoing rays are extended backward (see the dashed lines in
the drawing), they intersect and appear to originate from image 3. Thus,
the third image arises when an incident ray of light is refl ected twice, once
from each mirror, before entering her eyes.
Related Homework: Problem 1
FIGURE 25.9 (a) These two perpendicular plane mirrors produce three images of the
person (not completely visible) sitting in front
of them. (b) A “double” refl ection occurs, one from each mirror, and produces Image 3.(b)
Mirror 2Mirror 1
Image 1 Image 2
Image 3
Person
(a)
A n d y W
as h n ik
(b)
Mirror 2Mirror 1
Image 1 Image 2
Image 3
Person
FIGURE 25.9 (REPEATED) (b) A “double” refl ection occurs, one from each mirror,
and produces Image 3.
Check Your Understanding
(The answers are given at the end of the book.) 1. CYU Figure 25.1 shows a light ray undergoing multiple
refl ections from a mirrored corridor. The walls of the cor-
ridor are either parallel or perpendicular to one another.
If the initial angle of incidence is 35°, what is the angle of
refl ection when the ray makes its last refl ection?
2. A sign painted on a store window is reversed when viewed from inside the store. If a person inside the store views the
reversed sign in a plane mirror, does the sign appear as it
would when viewed from outside the store? (Try it by writ-
ing some letters on a transparent sheet of paper and then
holding the back side of the paper up to a mirror.)
3. If a clock is held in front of a mirror, its image is reversed left to right. From the point of view of a person looking into the mirror, does the image of the second hand rotate in the reverse (counterclockwise)
direction?
CYU FIGURE 25.1
716 CHAPTER 25 The Reflection of Light: Mirrors
25.4 Spherical Mirrors The most common type of curved mirror is a spherical mirror. As Interactive Figure 25.10 shows, a spherical mirror has the shape of a section from the surface of a hollow sphere. If the
inside surface of the mirror is polished, it is a concave mirror. If the outside surface is polished, it is a convex mirror. The drawing shows both types of mirrors, with a light ray refl ecting from the polished surface. The law of refl ection applies, just as it does for a plane mirror. For either
type of spherical mirror, the normal is drawn perpendicular to the mirror at the point of inci-
dence. For each type, the center of curvature is located at point C, and the radius of curvature is R. The principal axis of the mirror is a straight line drawn through C and the midpoint of the mirror.
Figure 25.11 shows a tree in front of a concave mirror. A point on this tree lies on the princi- pal axis of the mirror and is beyond the center of curvature C. Light rays emanate from this point and refl ect from the mirror, consistent with the law of refl ection. If the rays are near the principal
axis, they cross it at a common point after refl ection. This point is called the image point. The rays continue to diverge from the image point as if there were an object there. Since light rays actually
come from the image point, the image is a real image.
If the tree in Figure 25.11 is infi nitely far from the mirror, the rays are parallel to each other and to the principal axis as they approach the mirror. Figure 25.12 shows rays near and parallel to the principal axis, as they refl ect from the mirror and pass through an image point.
In this special case the image point is referred to as the focal point F of the mirror. Therefore, an object infi nitely far away on the principal axis gives rise to an image at the focal point of the
mirror. The distance between the focal point and the middle of the mirror is the focal length f of the mirror.
We can show that the focal point F lies halfway between the center of curvature C and the middle of a concave mirror. In Figure 25.13, a light ray parallel to the principal axis strikes the mirror at point A. The line CA is the radius of the mirror and, therefore, is the normal to the spheri- cal surface at the point of incidence. The ray refl ects from the mirror, and the angle of refl ection 𝜃
equals the angle of incidence. Furthermore, the angle ACF is also 𝜃 because the radial line CA
R
C
Light ray
Principal axis
R
CPrincipal axis
Convex mirror Concave mirror
Spherical mirror
INTERACTIVE FIGURE 25.10 A spherical mirror has the shape of a segment of a spherical surface. The center of curvature is point C and the radius is R. For a concave mirror, the refl ecting surface is the inner one; for a convex mirror it is the outer one.
C Principal axis
Concave mirror
Image point
FIGURE 25.11 A point on the tree lies on the principal axis of the concave mirror. Rays from this point that are near the principal axis are refl ected from the mirror and cross the axis at
the image point.
C F Principal axis
f
FIGURE 25.12 Light rays near and parallel to the principal axis are refl ected from a con-
cave mirror and converge at the focal point F. The focal length f is the distance between F and the mirror.
25.4 Spherical Mirrors 717
*Paraxial rays are close to the principal axis but not necessarily parallel to it.
is a transversal of two parallel lines. Since two of its angles are equal, the colored triangle CAF is an isosceles triangle; thus, sides CF and FA are equal. However, when the incoming ray lies close to the principal axis, the angle of incidence 𝜃 is small, and the distance FA does not diff er appreciably from the distance FB. Therefore, in the limit that 𝜃 is small, CF = FA = FB, and so the focal point F lies halfway between the center of curvature and the mirror. In other words, the focal length f is one-half of the radius R:
Focal length of a concave mirror
f = 12R (25.1)
Rays that lie close to the principal axis are known as paraxial rays,* and Equation 25.1 is valid only for such rays. Rays that are far from the principal axis do not converge to a single point
after refl ection from the mirror, as Figure 25.14 shows. The result is a blurred image. The fact that a spherical mirror does not bring all rays parallel to the principal axis to a single image point
is known as spherical aberration. Spherical aberration can be minimized by using a mirror whose height is small compared to the radius of curvature.
A sharp image point can be obtained with a large mirror, if the mirror is parabolic in shape
instead of spherical. The shape of a parabolic mirror is such that all light rays parallel to the prin-
cipal axis, regardless of their distance from the axis, are refl ected through a single image point.
However, parabolic mirrors are costly to manufacture and are used where the sharpest images are
required, as in research-quality telescopes.
THE PHYSICS OF . . . capturing solar energy with mirrors. Parabolic mirrors are also used in one method of collecting solar energy for commercial purposes. Figure 25.15 shows a long row of concave parabolic mirrors that refl ect the sun’s rays to the focal point. Located at
the focal point and running the length of the row is an oil-fi lled pipe. The focused rays of the sun
heat the oil. In a solar-thermal electric plant, the heat from many such rows is used to generate
steam. The steam, in turn, drives a turbine connected to an electric generator.
THE PHYSICS OF . . . automobile headlights. Another application of parabolic mir- rors is in automobile headlights. Here, however, the situation is reversed from the operation of
a solar collector. In a headlight, a high-intensity light source is placed at the focal point of the
mirror, and light emerges parallel to the principal axis.
A convex mirror also has a focal point, and Figure 25.16 illustrates its meaning. In this pic- ture, parallel rays are incident on a convex mirror. Clearly, the rays diverge after being refl ected.
If the incident parallel rays are paraxial, the refl ected rays seem to come from a single point F
C F
FIGURE 25.14 Rays that are farthest from the principal axis have the greatest angle of
incidence and miss the focal point F after refl ection from the mirror.
C F B
A
R
θ
θ θ
FIGURE 25.13 This drawing is used to show that the focal point F of a concave mirror is halfway between the center of curvature C and the mirror at point B.
FIGURE 25.15 This long row of parabolic mirrors focuses the sun’s rays to heat an
oil-fi lled pipe located at the focal point of
each mirror. Many such rows are used by a
solar-thermal electric plant in the Mojave
Desert.
Oil-filled pipe
© Ji
m W
es t/
A la
m y
718 CHAPTER 25 The Reflection of Light: Mirrors
behind the mirror. This point is the focal point of the convex mirror, and its distance from the
midpoint of the mirror is the focal length f. The focal length of a convex mirror is also one-half of the radius of curvature, just as it is for a concave mirror. However, we assign the focal length
of a convex mirror a negative value because it will be convenient later on:
Focal length of a convex mirror f = −
1
2 R (25.2)
Spherical aberration is a problem with convex mirrors, just as it is with concave mirrors.
Rays that emanate from a single point on an object but are far from the principal axis do not
appear to originate from a single image point after refl ection from the mirror. As with a concave
mirror, the result is a blurred image.
Check Your Understanding
(The answers are given at the end of the book.) 4. A section of the surface of a hollow sphere has a radius
of curvature of 0.60 m, and both the inside and outside
surfaces have a mirror-like polish. What are the focal
lengths of the inside and outside surfaces?
5. Photo 25.1 shows an experimental device at Sandia National Laboratories in New Mexico. This device is
a mirror that focuses sunlight to heat sodium to a boil,
which then heats helium gas in an engine. The engine does
the work of driving a generator to produce electricity.
The sodium unit and the engine are labeled in the photo.
(a) What kind of mirror, concave or convex, is being used? (b) Where is the sodium unit located relative to the mirror? Express your answer in terms of the focal
length of the mirror.
6. Refer to Figure 25.14 and the related discussion about spherical aberration. To bring the top ray closer to the
focal point F after refl ection, describe how you would change the shape of the mirror. Would you open it up to produce a more gently curving shape or bring
the top and bottom edges closer to the principal axis?
25.5 The Formation of Images by Spherical Mirrors As we have seen, some of the light rays emitted from an object in front of a mirror strike the mir-
ror, refl ect from it, and form an image. We can analyze the image produced by either concave or
convex mirrors by using a graphical method called ray tracing. This method is based on the law of refl ection and the notion that a spherical mirror has a center of curvature C and a focal point F. Ray tracing enables us to fi nd the location of the image, as well as its size, by taking advantage
of the following fact: paraxial rays leave from a point on the object and intersect, or appear to
intersect, at a corresponding point on the image after refl ection.
Concave Mirrors Three specifi c paraxial rays are especially convenient to use in the ray-tracing method. Interactive Figure 25.17 shows an object in front of a concave mirror, and these three rays leave from a point on the top of the object. The rays are labeled 1, 2, and 3, and when tracing their paths, we use the
following reasoning strategy.
R
F
f
C
FIGURE 25.16 When paraxial light rays that are parallel to the principal axis strike
a convex mirror, the refl ected rays appear to
originate from the focal point F. The radius of curvature is R and the focal length is f.
Sodium unit and engine
C o u rt
es y S
an d ia
N at
io n al
L ab
o ra
to ri
es
PHOTO 25.1
25.5 The Formation of Images by Spherical Mirrors 719
REASONING STRATEGY Ray Tracing for a Concave Mirror Ray 1. This ray is initially parallel to the principal axis and, therefore, passes through the
focal point F after refl ection from the mirror. Ray 2. This ray initially passes through the focal point F and is refl ected parallel to the princi-
pal axis. Ray 2 is analogous to ray 1 except that the refl ected, rather than the incident, ray is parallel to the principal axis.
Ray 3. This ray travels along a line that passes through the center of curvature C and follows a radius of the spherical mirror; as a result, the ray strikes the mirror perpendicularly and refl ects back on itself.
If rays 1, 2, and 3 are superimposed on a scale drawing, they converge at a point on the top
of the image, as can be seen in Animated Figure 25.18a.* Although three rays have been used here to locate the image, only two are really needed; the third ray is usually drawn to serve as a
check. In a similar fashion, rays from all other points on the object locate corresponding points
on the image, and the mirror forms a complete image of the object. If you were to place your eye
as shown in the drawing, you would see an image that is larger and inverted relative to the object. The image is real because the light rays actually pass through the image.
If the locations of the object and image in Animated Figure 25.18a are interchanged, the situation in part b of the drawing results. The three rays in part b are the same as those in part a, except that the directions are reversed. These drawings illustrate the principle of reversibility, which states the following:
Problem-Solving Insight If the direction of a light ray is reversed, the light retraces its original path.
This principle is quite general and is not restricted to refl ection from mirrors. The image is
real, and it is smaller and inverted relative to the object. When the object is placed between the focal point F and a concave mirror, as in Figure 25.19a,
three rays can again be drawn to fi nd the image. Now, however, ray 2 does not go through the
focal point on its way to the mirror, since the object is closer to the mirror than the focal point
is. When projected backward, though, ray 2 appears to come from the focal point. Therefore,
INTERACTIVE FIGURE 25.17 The rays labeled 1, 2, and 3 are useful in locating the
image of an object placed in front of a concave
spherical mirror. The object is represented as
a vertical arrow.
C
Object 1
F
C F
C F
2
3
*In the drawings that follow, we assume that the rays are paraxial, although the distance between the rays and the principal
axis is often exaggerated for clarity.
Real image
(a)
Object
C F
3
1
2
Object (b)
Real image
C F
ANIMATED FIGURE 25.18 (a) When an object is placed between the focal point F and the center of curvature C of a concave mirror, a real image is formed. The image is enlarged and inverted relative to the object. (b) When the object is located beyond the center of curvature C, a real image is created that is reduced in size and inverted relative to the object.
720 CHAPTER 25 The Reflection of Light: Mirrors
after refl ection, ray 2 is directed parallel to the principal axis. In this case the three refl ected
rays diverge from each other and do not converge to a common point. However, when projected
behind the mirror, the three rays appear to come from a common point; thus, a virtual image is formed. This virtual image is larger than the object and upright.
THE PHYSICS OF . . . makeup and shaving mirrors. Makeup and shaving mirrors are concave mirrors. When you place your face between the mirror and its focal point, you see an
enlarged virtual image of yourself, as Figure 25.19b shows. THE PHYSICS OF . . . a head-up display for automobiles. Concave mirrors are
also used in one method for displaying the speed of a car. The method presents a digital read-
out (e.g., “51 km/h”) that the driver sees when looking directly through the windshield, as in
Figure 25.20a. The advantage of the method, which is called a head-up display (HUD), is that the driver does not need to take his or her eyes off the road to monitor the speed. Figure 25.20b shows how one type of HUD works. Below the windshield is a readout device that displays the
speed in digital form. This device is located between a concave mirror and its focal point. The
arrangement is similar to the one in Figure 25.19a and produces a virtual, upright, and enlarged image of the speed readout (see virtual image 1 in Figure 25.20b). Light rays that appear to come from this image strike the windshield at a place where a so-called “combiner” is located. The pur-
pose of the combiner is to combine the digital readout information with the fi eld of view that the
driver sees through the windshield. The combiner is virtually undetectable by the driver because
it allows all colors except one to pass through it unaff ected. The one exception is the color pro-
duced by the digital readout device. For this color, the combiner behaves as a plane mirror and
refl ects the light that appears to originate from image 1. Thus, the combiner produces image 2,
which is what the driver sees. The location of image 2 is out above the front bumper. The driver
can then read the speed with eyes focused just as they are to see the road.
FIGURE 25.19 (a) When an object is located between a concave mirror and its focal point F, an enlarged, upright, and virtual image is produced. (b) A makeup mirror (or shaving mirror) is a concave mirror that functions in exactly this fashion, as this photograph shows.
(a) (b)
C
F
3
1
2
Object Virtual image
fa n to
m _ rd
/ S
h u tt
er st
o ck
FIGURE 25.20 (a) A head-up display (HUD) presents the driver with a digital readout of the car’s speed in the fi eld of view seen through the windshield. (b) One version of a HUD uses a concave mirror. (See the text for explanation.)
Digital readout device
Virtual image 2
Virtual image 1
Concave mirror
Windshield
Combiner
F
(b)(a)
C o u rt
es y o
f B
M W
o f
N o rt
h A
m er
ic a,
L L
C .
25.5 The Formation of Images by Spherical Mirrors 721
Convex Mirrors The ray-tracing procedure for determining the location and size of an image in a convex mirror
is similar to that for a concave mirror. The same three rays are used. However, the focal point
and center of curvature of a convex mirror lie behind the mirror, not in front of it. Interactive Figure 25.21a shows the rays. When tracing their paths, we use the following reasoning strategy, which takes into account these locations of the focal point and center of curvature.
REASONING STRATEGY Ray Tracing for a Convex Mirror Ray 1. This ray is initially parallel to the principal axis and, therefore, appears to originate
from the focal point F after refl ection from the mirror. Ray 2. This ray heads toward F, emerging parallel to the principal axis after refl ection. Ray 2
is analogous to ray 1, except that the refl ected, rather than the incident, ray is parallel to the principal axis.
Ray 3. This ray travels toward the center of curvature C; as a result, the ray strikes the mirror perpendicularly and refl ects back on itself.
The three rays in Interactive Figure 25.21a appear to come from a point on a virtual image that is behind the mirror. The virtual image is diminished in size and upright, relative to the object. A convex mirror always forms a virtual image of the object, no matter where in front of the mirror the object is placed. Interactive Figure 25.21b shows an example of such an image.
INTERACTIVE FIGURE 25.21 (a) An object placed in front of a convex mirror always produces a virtual image behind the mirror; the image is reduced in size and is upright. (b) This chromed motorcycle helmet acts as a convex mirror and produces an image of other motorcycles and pedestrians.
(a) (b)
3
1
2
CFObject Virtual image
M cP
H O
T O
/A g e
F o to
st o ck
INTERACTIVE FIGURE 25.21 (REPEATED) (a) An object placed in front of a convex mirror always produces a virtual image behind the mirror; the image is reduced in size and is upright. (b) This chromed motorcycle helmet acts as a convex mirror and produces an image of other motorcycles and pedestrians.
(a) (b)
3
1
2
CFObject Virtual image
M cP
H O
T O
/A g e
F o to
st o ck
722 CHAPTER 25 The Reflection of Light: Mirrors
THE PHYSICS OF . . . passenger-side automobile mirrors. Because of its shape, a convex mirror gives a wider fi eld of view than do other types of mirrors. A mirror with a wide
fi eld of view is needed to give a driver a good rear view. Thus, the outside mirror on the pas-
senger side is often a convex mirror. Printed on such a mirror is usually the warning “VEHICLES
IN MIRROR ARE CLOSER THAN THEY APPEAR.” The reason for the warning is that, as in Interactive Figure 25.21a, the virtual image is reduced in size and therefore looks smaller, just as a distant object would appear in a plane mirror. An unwary driver, thinking that the side-view mirror is a
plane mirror, might incorrectly deduce from the small size of the image that the car behind is far
enough away to ignore. Because of their wide fi eld of view, convex mirrors are also used in stores
for security purposes.
Check Your Understanding
(The answers are given at the end of the book.) 7. Concept Simulation 25.3 at www.wiley.com/college/cutnell allows you to explore the concepts to
which this question relates. Is it possible to use a convex mirror to produce an image that is larger than
the object?
8. (a) When you look at the back side of a shiny teaspoon held at arm’s length, do you see yourself upright or upside down? (b) When you look at the other side of the spoon, do you see yourself upright or upside down? Assume in both cases that the distance between you and the spoon is greater than the
focal length of the spoon.
9. (a) Can the image formed by a concave mirror ever be projected directly onto a screen without the help of other mirrors or lenses? If so, specify where the object should be placed relative to the mirror.
(b) Repeat part (a) assuming that the mirror is convex. 10. Suppose that you stand in front of a spherical mirror (concave or convex). Is it possible for your image
to be (a) real and upright (b) virtual and inverted? 11. An object is placed between the focal point and the center of curvature of a concave mirror. The object
is then moved closer to the mirror, but still remains between the focal point and the center of curvature.
Do the magnitudes of (a) the image distance and (b) the image height become larger or smaller? 12. When you see the image of yourself formed by a mirror, it is because (1) light rays actually coming
from a real image enter your eyes or (2) light rays appearing to come from a virtual image enter your
eyes. If light rays from the image do not enter your eyes, you do not see yourself. Are there any places
on the principal axis where you cannot see yourself when you are standing in front of a mirror that is
(a) convex (b) concave? If so, where are these places? Assume that you have only the one mirror to use.
25.6 The Mirror Equation and the Magnification Equation Ray diagrams drawn to scale are useful for determining the location and size of the image formed
by a mirror. However, for an accurate description of the image, a more analytical technique is
needed, so we will derive two equations, known as the mirror equation and the magnifi cation equation. These equations are based on the law of refl ection and provide relationships between:
f = the focal length of the mirror do = the object distance, which is the distance between the object and the mirror di = the image distance, which is the distance between the image and the mirror m = the magnifi cation of the mirror, which is the ratio of the height of the image to the
height of the object.
Concave Mirrors We begin our derivation of the mirror equation by referring to Figure 25.22a, which shows a ray leaving the top of the object and striking a concave mirror at the point where the principal axis
intersects the mirror. Since the principal axis is perpendicular to the mirror, it is also the normal
(a)
Object
Image F hi
ho
di
do
(b)
F hi
ho
fdo – f
FIGURE 25.22 These diagrams are used to derive the mirror equation and the magnifi ca-
tion equation. (a) The two colored triangles are similar triangles. (b) If the ray is close to the principal axis, the two colored regions are
almost similar triangles.
25.6 The Mirror Equation and the Magnification Equation 723
at this point of incidence. Therefore, the ray refl ects at an equal angle and passes through the
image. The two colored triangles are similar triangles because they have equal angles, so
ho −h i
= do d i
where ho is the height of the object and hi is the height of the image. The minus sign appears on the left in this equation because the image is inverted in Figure 25.22a. In part b another ray leaves the top of the object, this one passing through the focal point F, refl ecting parallel to the principal axis, and then passing through the image. Provided the ray remains close to the axis, the
two colored areas can be considered to be similar triangles, with the result that
ho −h i
= do − f
f
Setting the two equations above equal to each other yields do/di = (do − f )/f. Rearranging this result gives the mirror equation:
Mirror equation
1
do +
1
di =
1
f (25.3)
We have derived this equation for a real image formed in front of a concave mirror. In this
case, the image distance is a positive quantity, as are the object distance and the focal length.
However, we have seen in the last section that a concave mirror can also form a virtual image, if
the object is located between the focal point and the mirror. Equation 25.3 can also be applied to
such a situation, provided that we adopt the convention that di is negative for an image behind the mirror, as it is for a virtual image.
In deriving the magnifi cation equation, we remember that the magnifi cation m of a mirror is the ratio of the image height to the object height: m = hi/ho. If the image height is less than the object height, the magnitude of m is less than one, and if the image is larger than the object, the magnitude of m is greater than one. We have already shown that ho/(−hi) = do/di, so it follows that
Magnifi cation equation
m = Image height, h i Object height, ho
= − d i do
(25.4)
As Examples 3 and 4 show, the value of m is negative if the image is inverted and positive if the image is upright.
EXAMPLE 3 A Real Image Formed by a Concave Mirror
A 2.0-cm-high object is placed 7.10 cm from a concave mirror whose
radius of curvature is 10.20 cm. Find (a) the location of the image and (b) its size.
Reasoning For a concave mirror, Equation 25.1 gives the focal length as f = 12 R. Therefore, the focal length is f =
1
2(10.20 cm) = 5.10 cm, and
the object is located between the focal point F and the center of curvature C of the mirror, as in Animated Figure 25.18a. Based on this fi gure, we expect that the image is real and that, relative to the object, it is farther
away from the mirror, inverted, and larger.
Problem-Solving Insight According to the mirror equa- tion, the image distance di has a reciprocal given by di−1 = f −1 − do−1. After combining the reciprocals f −1 and do−1, do not forget to take the reciprocal of the result to fi nd di.
Solution (a) With do = 7.10 cm and f = 5.10 cm, the mirror equation (Equation 25.3) can be used to fi nd the image distance:
1
di =
1
f −
1
do =
1
5.10 cm −
1
7.10 cm = 0.055 cm−1 or d i = 18 cm
In this calculation, f and do are positive numbers, indicating that the focal point and the object are in front of the mirror. The positive answer for di means that the image is also in front of the mirror, and the refl ected rays
actually pass through the image, as Animated Figure 25.18a shows. In other words, the positive value for di indicates that the image is a real image.
(b) According to the magnifi cation equation (Equation 25.4), the image height hi is related to the object height ho and the magnifi cation m by hi = mho, where m = −di/do. Thus, we fi nd that
h i = −( d i do)ho = −(
18 cm
7.10 cm)(2.0 cm) = −5.1 cm The negative value for hi indicates that the image is inverted with respect to the object, as in Animated Figure 25.18a.
724 CHAPTER 25 The Reflection of Light: Mirrors
Convex Mirrors The mirror equation and the magnifi cation equation can also be used with convex mirrors, pro-
vided the focal length f is taken to be a negative number, as indicated explicitly in Equation 25.2. One way to remember this is to recall that the focal point of a convex mirror lies behind the mirror. Example 5 deals with a convex mirror.
EXAMPLE 4 A Virtual Image Formed by a Concave Mirror
An object is placed 6.00 cm in front of a concave mirror that has a 10.0-cm
focal length. (a) Determine the location of the image. (b) The object is 1.2 cm high. Find the image height.
Reasoning The object is located between the focal point and the mirror, as in Figure 25.19a. The setup is analogous to a person using a makeup or shaving mirror. Therefore, we expect that the image is virtual and that,
relative to the object, it is upright and larger.
Solution (a) Using the mirror equation with do = 6.00 cm and f = 10.0 cm, we have
1
di =
1
f −
1
do =
1
10.0 cm −
1
6.00 cm = −0.067 cm−1 or di = −15 cm
The answer for di is negative, indicating that the image is behind the mirror. Thus, as expected, the image is virtual.
(b) The image height hi can be found from the magnifi cation equation, which indicates that hi = mho, where ho is the object height and m = −di/do. It follows, then, that
h i = −( d i do)ho = −(
−15 cm
6.00 cm)(1.2 cm) = 3.0 cm The image is larger than the object, and the positive value for hi indicates that the image is upright (see Figure 25.19a).
EXAMPLE 5 A Virtual Image Formed by a Convex Mirror
A convex mirror is used to refl ect light from an object placed 66 cm in
front of the mirror. The focal length of the mirror is f = −46 cm (note the minus sign). Find (a) the location of the image and (b) the magnifi cation.
Reasoning We have seen that a convex mirror always forms a virtual image, as in Interactive Figure 25.21a, where the image is upright and smaller than the object. These characteristics should also be indicated
by the results of our analysis here.
Problem-Solving Insight When using the mirror equation, it is useful to construct a ray diagram to guide your thinking and to check your calculation.
Solution (a) With do = 66 cm and f = −46 cm, the mirror equation gives 1
d i =
1
f −
1
do =
1
−46 cm −
1
66 cm = −0.037 cm−1 or di = −27 cm
The negative sign for di indicates that the image is behind the mirror and, therefore, is a virtual image.
(b) According to the magnifi cation equation, the magnifi cation is
m = − d i do
= − (−27 cm)
66 cm = 0.41
The image is smaller (m is less than one) and upright (m is positive) with respect to the object.
Convex mirrors, like plane (fl at) mirrors, always produce virtual images behind the mirror.
However, the virtual image in a convex mirror is closer to the mirror than it would be if the mirror
were planar, as Example 6 illustrates.
EXAMPLE 6 A Convex Versus a Plane Mirror
An object is placed 9.00 cm in front of a mirror. The image is 3.00 cm
closer to the mirror when the mirror is convex than when it is planar (see
Figure 25.23). Find the focal length of the convex mirror.
Reasoning For a plane mirror, the image and the object are the same distance on either side of the mirror. Thus, the image would be 9.00 cm
behind a plane mirror. If the image in a convex mirror is 3.00 cm closer
than this, the image must be located 6.00 cm behind the convex mirror. In
other words, when the object distance is do = 9.00 cm, the image distance
for the convex mirror is di = −6.00 cm (negative because the image is virtual). The mirror equation can be used to fi nd the focal length of the
mirror.
Solution According to the mirror equation, the reciprocal of the focal length is
1
f =
1
do +
1
d i =
1
9.00 cm +
1
−6.00 cm = −0.056 cm−1 or f = −18 cm
25.6 The Mirror Equation and the Magnification Equation 725
Contact lenses are worn to correct vision problems. Optometrists take advantage of the mirror
equation and the magnifi cation equation in providing lenses that fi t the patient’s eyes properly, as
the next example illustrates.
9.00 cm 3.00 cm
9.00 cm 9.00 cm
FIGURE 25.23 The object distance (9.00 cm) is the same for the plane mirror (top part of
drawing) as for the convex mirror (bottom
part of drawing). However, as discussed in
Example 6, the image formed by the convex
mirror is 3.00 cm closer to the mirror.
Analyzing Multiple -Concept Problems
EXAMPLE 7 BIO The Physics of Keratometers
A contact lens rests against the cornea of the eye. Figure 25.24 shows an optometrist using a keratometer to measure the radius of curvature of
the cornea, thereby ensuring that the prescribed lenses fi t accurately. In
the keratometer, light from an illuminated object refl ects from the corneal
surface, which acts like a convex mirror and forms an upright virtual image
that is smaller than the object (see Interactive Figure 25.21a). With the object placed 9.0 cm in front of the cornea, the magnifi cation of the cor-
neal surface is measured to be 0.046. Determine the radius of the cornea.
Reasoning The radius of a convex mirror can be determined from the mirror’s focal length, since the two are related. The focal length is related
to the distances of the object and its image from the mirror via the mirror
equation. The magnifi cation of the mirror is also related to the object and
image distances according to the magnifi cation equation. By using the
mirror equation and the magnifi cation equation, we will be able to deter-
mine the focal length and, hence, the radius.
Knowns and Unknowns The following table summarizes the available data:
M A
R K
T H
O M
A S
/S ci
en ce
S o u rc
e
FIGURE 25.24 An optometrist is using a keratometer to measure the radius of curvature of the cornea of the eye, which is the surface against
which a contact lens rests.
Description Symbol Value Comment Object distance do 9.0 cm Distance of object from cornea.
Magnification of corneal surface m 0.046 Cornea acts like a convex mirror and forms a virtual image.
Unknown Variable Radius of cornea R ?
Modeling the Problem
STEP 1 Relation Between Radius and Focal Length The focal length f of a convex mirror is given by Equation 25.2 as
f = − 12 R
where R is the radius of the spherical surface. Solving this expression for the radius gives Equation 1 at the right. In Step 2, we determine the unknown focal length.
R = −2f (1)
?
726 CHAPTER 25 The Reflection of Light: Mirrors
STEP 2 The Mirror Equation The focal length is related to the object distance do and the image distance di via the mirror equation, which specifi es that
1
f =
1
do +
1
d i (25.3)
Solving this equation for f gives
f = ( 1do + 1
d i) −1
which can be substituted into Equation 1 as shown in the right column. A value for do is given in the data table, and we turn to Step 3 to determine a value for di.
STEP 3 The Magnifi cation Equation According to the magnifi cation equation, the magnifi - cation m is given by
m = − di do
(25.4)
Solving for di, we obtain
di = −mdo
and can substitute this result into Equation 2, as shown at the right.
Solution Combining the results of each step algebraically, we fi nd that
R = −2 f = −2( 1do + 1
d i) −1
= −2[ 1do + 1
(−mdo) ] −1
Thus, the radius is
R = −2 [ 1do + 1
(−mdo) ] −1
= 2dom 1 − m
= 2(9.0 cm)(0.046)
1 − 0.046 = 0.87 cm
Related Homework: Problem 33
STEP 1 STEP 2 STEP 3
R = −2f (1)
f = ( 1do + 1
d i) −1
(2)
?
R = −2f (1)
f = ( 1do + 1
d i) −1
(2)
di = −mdo
Math Skills To show that the radius R is R = 2dom 1 − m
, we proceed in the following way.
The fi rst step is to factor out the term 1
do in the result for R:
R = −2[ 1do + 1
(−mdo) ] −1
= −2[ 1do(1 − 1
m)] −1
Rearranging the term within the brackets is the next step:
R = −2[ 1do(1 − 1
m)] −1
= −2[ 1do( m m
− 1
m)] −1
= −2(m − 1do m ) −1
Finally, taking the reciprocal of the term within the parentheses shows that
R = −2(m − 1do m ) −1
= −2( dom
m − 1) = 2do m 1 − m
The following Reasoning Strategy summarizes the sign conventions that are used with the
mirror equation and the magnifi cation equation. These conventions apply to both concave and
convex mirrors.
REASONING STRATEGY Summary of Sign Conventions for Spherical Mirrors Focal length
f is + for a concave mirror. f is − for a convex mirror.
25.6 The Mirror Equation and the Magnification Equation 727
Object distance do is + if the object is in front of the mirror (real object). do is − if the object is behind the mirror (virtual object).*
Image distance di is + if the image is in front of the mirror (real image). di is − if the image is behind the mirror (virtual image).
Magnifi cation m is + for an image that is upright with respect to the object. m is − for an image that is inverted with respect to the object.
Check Your Understanding
(The answers are given at the end of the book.) 13. An object is placed in front of a spherical mirror, and the magnifi cation of the system is m = −6. What does
this number tell you about the image? (Select one or more of the following choices.) (a) The image is larger than the object. (b) The image is smaller than the object. (c) The image is upright relative to the object. (d) The image is inverted relative to the object. (e) The image is a real image. (f) The image is a virtual image.
14. Concept Simulation 25.3 at www.wiley.com/college/cutnell reviews the concepts that are important in this question. Plane mirrors and convex mirrors form virtual images. With a plane mirror, the image
may be infi nitely far behind the mirror, depending on where the object is located in front of the mirror.
For an object in front of a single convex mirror, what is the greatest distance behind the mirror at which
the image can be found?
*Sometimes optical systems use two (or more) mirrors, and the image formed by the fi rst mirror serves as the object for
the second mirror. Occasionally, such an object falls behind the second mirror. In this case the object distance is negative, and the object is said to be a virtual object.
EXAMPLE 8 BIO The Physics of a Head Mirror
A head mirror is a simple medical diagnostic tool that is used to illuminate
a patient’s ear, throat, and nasal passages. It consists of a concave spherical
mirror with a small hole drilled in the center (Figure 25.25). The physician places the mirror over one eye and looks through the hole in the center.
Light from a bright lamp that is placed near the patient’s head refl ects off
the mirror along the line of sight of the doctor and illuminates the area on
the patient that is under examination. During a routine physical, a patient
sitting 0.50 m away from the physician sees the refl ection of her nose in
the head mirror. If the focal length of the mirror is 25 cm, (a) where is the image located, and (b) what is its magnifi cation?
Reasoning The head mirror is a small concave spherical mirror. We can use the mirror equation (Equation 25.3) to calculate the location of the
image and then Equation 25.4 to calculate the magnifi cation.
Solution (a) Rearranging the mirror equation, we have: 1 di
= 1
f −
1
do .
Plugging in the values in the problem, we fi nd:
1
di =
1
0.25 m −
1
0.50 m ⇒ di = 0.50 m
(b) The magnifi cation is determined from Equation 25.4:
m = −di do
= − 0.50 m
0.50 m = −1
Since the absolute value of the magnifi cation is 1, the image is the same size
as the object, and the negative sign tells us the image is real and inverted
with respect to the object.
FIGURE 25.25 On the left is the patient’s view of a physician wearing
a head mirror. The image on the right
shows the bright light refl ected by the
mirror onto the patient under examina-
tion. Notice the lamp adjacent to the
patient’s head above her right shoulder.R o b er
t K
n es
ch k e/
A la
m y S
to ck
P h o to
D m
it ry
K al
in o v sk
y /S
h u tt
er st
o ck
728 CHAPTER 25 The Reflection of Light: Mirrors
Concept Summary 25.1 Wave Fronts and Rays Wave fronts are surfaces on which all points of a wave are in the same phase of motion. Waves whose wave fronts are fl at
surfaces are known as plane waves. Rays are lines that are perpendicular to
the wave fronts and point in the direction of the velocity of the wave.
25.2 The Refl ection of Light When light refl ects from a smooth surface, the refl ected light obeys the law of refl ection: The incident ray, the refl ected
ray, and the normal to the surface all lie in the same plane, and the angle of
refl ection 𝜃r equals the angle of incidence 𝜃i (𝜃r = 𝜃i).
25.3 The Formation of Images by a Plane Mirror A virtual image is one from which all the rays of light do not actually come, but only appear to do
so. A real image is one from which all the rays of light actually do emanate.
A plane mirror forms an upright, virtual image that is located as far
behind the mirror as the object is in front of it. In addition, the heights of the
image and the object are equal.
25.4 Spherical Mirrors A spherical mirror has the shape of a section from the surface of a hollow sphere. If the inside surface of the mirror is polished,
it is a concave mirror. If the outside surface is polished, it is a convex mirror.
The principal axis of a mirror is a straight line drawn through the center
of curvature and the middle of the mirror’s surface. Rays that are close to the
principal axis are known as paraxial rays. Paraxial rays are not necessarily
parallel to the principal axis. The radius of curvature R of a mirror is the distance from the center of curvature to the mirror.
The focal point of a concave spherical mirror is a point on the principal
axis, in front of the mirror. Incident paraxial rays that are parallel to the prin-
cipal axis converge to the focal point after being refl ected from the concave
mirror.
The focal point of a convex spherical mirror is a point on the principal
axis, behind the mirror. For a convex mirror, incident paraxial rays that are
parallel to the principal axis diverge after refl ecting from the mirror. These
rays seem to originate from the focal point.
The fact that a spherical mirror does not bring all rays parallel to the
principal axis to a single image point after refl ection is known as spherical
aberration.
The focal length f indicates the distance along the principal axis between the focal point and the mirror. The focal length and the radius of curvature R are related by Equations 25.1 and 25.2.
f = 12 R (Concave mirror) (25.1)
f = −12 R (Convex mirror) (25.2)
25.5 The Formation of Images by Spherical Mirrors The image pro- duced by a mirror can be located by a graphical method known as ray tracing.
For a concave mirror, the following paraxial rays are useful for ray tracing
(see Interactive Figure 25.17):
Ray 1. This ray leaves the object traveling parallel to the principal axis. The ray refl ects from the mirror and passes through the focal
point.
Ray 2. This ray leaves the object and passes through the focal point. The ray refl ects from the mirror and travels parallel to the principal
axis.
Ray 3. This ray leaves the object and travels along a line that passes through the center of curvature. The ray strikes the mirror per-
pendicularly and refl ects back on itself.
For a convex mirror, the following paraxial rays are useful for ray tracing
(see Interactive Figure 25.21a):
Ray 1. This ray leaves the object traveling parallel to the principal axis. After refl ection from the mirror, the ray appears to originate
from the focal point of the mirror.
Ray 2. This ray leaves the object and heads toward the focal point. After refl ection, the ray travels parallel to the principal axis.
Ray 3. This ray leaves the object and travels toward the center of cur- vature. The ray strikes the mirror perpendicularly and refl ects
back on itself.
25.6 The Mirror Equation and the Magnifi cation Equation The mirror equation (Equation 25.3) specifi es the relation between the object distance do, the image distance di, and the focal length f of the mirror. The mirror equation can be used with either concave or convex mirrors.
1
do +
1
di =
1
f (25.3)
The magnifi cation m of a mirror is the ratio of the image height hi to the object height ho: m = h i /ho. The magnifi cation is also related to di and do by the magnifi cation equation (Equation 25.4). The algebraic sign conventions
for the variables appearing in these equations are summarized in the Reason-
ing Strategy at the end of Section 25.6.
m = − d i do
(25.4)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 25.1 Wave Fronts and Rays 2. A ray is _______. (a) always parallel to other rays (b) parallel to the velocity of the wave (c) perpendicular to the velocity of the wave (d) parallel to the wave fronts
Section 25.2 The Reflection of Light 4. The drawing shows a top view of an object located to the right of a mirror. A single ray of light is shown
leaving the object. After refl ection from the mirror,
through which location, A, B, C, or D, does the ray
pass? (a) A (b) B (c) C (d) D
Focus on Concepts
A
C
D
B
Mirror Object
Ray
QUESTION 4
Problems 729
Section 25.3 The Formation of Images by a Plane Mirror 6. A friend is standing 2 m in front of a plane mirror. You are standing 3 m directly behind your friend. What is the distance between you and the image
of your friend? (a) 2 m (b) 3 m (c) 5 m (d) 7 m (e) 10 m 7. You hold the words TOP DOG in front of a plane mirror. What does the image of these words look like? (a) DOG TOP (b) TOP DOG (c) TOP DOG (d) DOG TOP (e)
TOP DOG
Section 25.4 Spherical Mirrors 8. Rays of light coming from the sun (a very distant object) are near and par- allel to the principal axis of a concave mirror. After refl ecting from the mirror,
where will the rays cross each other at a single point? The rays _________.
(a) will not cross each other after refl ecting from a concave mirror (b) will cross at the point where the principal axis intersects the mirror (c) will cross at the center of curvature (d) will cross at the focal point (e) will cross at a point beyond the center of curvature
Section 25.5 The Formation of Images by Spherical Mirrors 12. Which one of the following statements concerning spherical mirrors is correct? (a) Only a convex mirror can produce an enlarged image. (b) Both
concave and convex mirrors can produce an enlarged image. (c) Only a con- cave mirror can produce an enlarged image, provided the object distance is less
than the radius of curvature. (d) Only a concave mirror can produce an enlarged image, provided the object distance is greater than the radius of curvature.
13. Suppose that you hold up a small convex mirror in front of your face. Which answer describes the image of your face? (a) Virtual, inverted (b) Vir- tual, upright (c) Virtual, enlarged (d) Real, inverted (e) Real, reduced in size
Section 25.6 The Mirror Equation and the Magnification Equation 14. An object is placed at a known distance in front of a mirror whose focal length is also known. You apply the mirror equation and fi nd that the
image distance is a negative number. This result tells you that _______.
(a) the image is larger than the object (b) the image is smaller than the object (c) the image is inverted relative to the object (d) the image is real (e) the image is virtual
15. An object is situated at a known distance in front of a convex mirror whose focal length is also known. A friend of yours does a calculation that
shows that the magnifi cation is −2. After some thought, you conclude cor- rectly that _______. (a) your friend’s answer is correct (b) the magnifi cation should be +2 (c) the magnifi cation should be +12 (d) the magnifi cation should be −
1
2
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 25.2 The Reflection of Light
Section 25.3 The Formation of Images by a Plane Mirror 1. E Available in WileyPLUS. 2. E On the +y axis a laser is loc- ated at y = +3.0 cm. The coordinates of a small target are x = +9.0 cm and y = +6.0 cm. The +x axis represents the edge-on view of a plane mirror. At
what point on the +x axis should the laser be aimed in order for the laser
light to hit the target after refl ection?
3. E SSM You are trying to photo- graph a bird sitting on a tree branch,
but a tall hedge is blocking your view.
However, as the drawing shows, a
plane mirror refl ects light from the bird
into your camera. For what distance
must you set the focus of the camera
lens in order to snap a sharp picture of
the bird’s image?
4. E GO Suppose that you are walking perpendicularly with a velocity of +0.90 m/s toward a stationary plane mirror. What is the velocity of your im- age relative to you? The direction in which you walk is the positive direction.
5. E SSM Two plane mirrors are separated by 120°, as the drawing illustrates. If a ray strikes mirror M1 at a 65° angle of incidence, at what angle 𝜃 does it leave mirror M2?
PROBLEM 5
65° 120°
M2
M1
θ
6. E CHALK The drawing shows a laser beam shining on a plane mirror that is perpendicular to the fl oor. The beam’s angle of incidence is 33.0°. The
beam emerges from the laser at a point that is 1.10 m from the mirror and
1.80 m above the fl oor. After refl ection, how far from the base of the mirror
does the beam strike the fl oor?
PROBLEM 6
1.10 m
33.0° 1.80 m
Floor
Problems
4.3 m
2.1 m
3.7 m
PROBLEM 3
730 CHAPTER 25 The Reflection of Light: Mirrors
7. E Available in WileyPLUS. 8. M GO A small mirror is attached to a vertical wall, and it hangs a distance of 1.80 m above the fl oor. The mirror is facing due east, and a ray of sunlight
strikes the mirror early in the morning and then again later in the morning.
The incident and refl ected rays lie in a plane that is perpendicular to both the
wall and the fl oor. Early in the morning, the refl ected ray strikes the fl oor at a
distance of 3.86 m from the base of the wall. Later on in the morning, the ray
is observed to strike the fl oor at a distance of 1.26 m from the wall. The earth
rotates at a rate of 15.0° per hour. How much time (in hours) has elapsed
between the two observations?
9. M V-HINT In an experiment designed to measure the speed of light, a laser is aimed at a mirror that is 50.0 km due north. A detector is placed 117 m
due east of the laser. The mirror is to be aligned so that light from the laser
refl ects into the detector. (a) When properly aligned, what angle should the normal to the surface of the mirror make with due south? (b) Suppose the mirror is misaligned, so that the actual angle between the normal to the sur-
face and due south is too large by 0.004°. By how many meters (due east) will
the refl ected ray miss the detector?
10. M GO The drawing shows two plane mirrors that intersect at an angle of 50°. An incident light ray refl ects from one mirror and then the other. What
is the angle 𝜃 between the incident and outgoing rays?
PROBLEM 10 50°
Outgoing ray
Incident ray
θ
11. M Two plane mirrors are facing each other. They are parallel, 3.00 cm apart, and 17.0 cm in length, as the drawing indicates. A laser beam is dir-
ected at the top mirror from the left edge of the bottom mirror. What is the
smallest angle of incidence with respect to the top mirror, such that the laser
beam (a) hits only one of the mirrors and (b) hits each mirror only once?
17.0 cm
Laser 3.00 cm
PROBLEM 11
12. H Available in WileyPLUS.
Section 25.4 Spherical Mirrors
Section 25.5 The Formation of Images by Spherical Mirrors 13. E When an object is located very far away from a convex mirror, the image of the object is 18 cm behind the mirror. Using a ray diagram drawn
to scale, determine where the image is located when the object is placed
9.0 cm in front of the mirror. Note that the mirror must be drawn to scale also.
In your drawing, assume that the height of the object is 3.0 cm.
14. E The image of a very distant car is located 12 cm behind a convex mir- ror. (a) What is the radius of curvature of the mirror? (b) Draw a ray diagram to scale showing this situation.
15. E SSM An object is placed 11 cm in front of a concave mirror whose focal length is 18 cm. The object is 3.0 cm tall. Using a ray diagram drawn
to scale, measure (a) the location and (b) the height of the image. The mirror must be drawn to scale.
16. E MMH A 2.0-cm-high object is situated 15.0 cm in front of a concave mirror that has a radius of curvature of 10.0 cm. Using a ray diagram drawn
to scale, measure (a) the location and (b) the height of the image. The mirror must be drawn to scale.
17. E MMH A convex mirror has a focal length of −40.0 cm. A 12.0-cm-tall object is located 40.0 cm in front of this mirror. Using a ray diagram drawn
to scale, determine the (a) location and (b) size of the image. Note that the mirror must be drawn to scale.
18. M CHALK A plane mirror and a concave mirror ( f = 8.0 cm) are facing each other and are separated by a distance of 20.0 cm. An object is placed
between the mirrors and is 10.0 cm from each mirror. Consider the light from
the object that refl ects fi rst from the plane mirror and then from the concave
mirror. Using a ray diagram drawn to scale, fi nd the location of the image
that this light produces in the concave mirror. Specify this distance relative
to the concave mirror.
Section 25.6 The Mirror Equation and the Magnification Equation 19. E SSM The image produced by a concave mirror is located 26 cm in front of the mirror. The focal length of the mirror is 12 cm. How far in front
of the mirror is the object located?
20. E The image behind a convex mirror (radius of curvature = 68 cm) is located 22 cm from the mirror. (a) Where is the object located and (b) what is the magnifi cation of the mirror? Determine whether the image is (c) upright or inverted and (d) larger or smaller than the object. 21. E MMH A concave mirror (R = 56.0 cm) is used to project a transparent slide onto a wall. The slide is located at a distance of 31.0 cm from the mirror,
and a small fl ashlight shines light through the slide and onto the mirror. The
setup is similar to that in Animated Figure 25.18a. (a) How far from the wall should the mirror be located? (b) The height of the object on the slide is 0.95 cm. What is the height of the image? (c) How should the slide be oriented, so that the picture on the wall looks normal?
22. E GO A small statue has a height of 3.5 cm and is placed in front of a concave mirror. The image of the statue is inverted, 1.5 cm tall, and located
13 cm in front of the mirror. Find the focal length of the mirror.
23. E GO SSM A mirror produces an image that is located 34.0 cm behind the mirror when the object is located 7.50 cm in front of the mirror. What is
the focal length of the mirror, and is the mirror concave or convex?
24. E GO A concave mirror (f = 45 cm) produces an image whose distance from the mirror is one-third the object distance. Determine (a) the object distance and (b) the (positive) image distance. 25. E The outside mirror on the passenger side of a car is convex and has a focal length of −7.0 m. Relative to this mirror, a truck traveling in the rear has an object distance of 11 m. Find (a) the image distance of the truck and (b) the magnifi cation of the mirror. 26. E GO A convex mirror has a focal length of −27.0 cm. Find the mag- nifi cation produced by the mirror when the object distance is 9.0 cm and
18.0 cm.
27. E SSM When viewed in a spherical mirror, the image of a setting sun is a virtual image. The image lies 12.0 cm behind the mirror. (a) Is the mirror concave or convex? Why? (b) What is the radius of curvature of the mirror? 28. E V-HINT A concave mirror has a focal length of 12 cm. This mirror forms an image located 36 cm in front of the mirror. What is the magnifi ca-
tion of the mirror?
29. M V-HINT An object is located 14.0 cm in front of a convex mirror, the image being 7.00 cm behind the mirror. A second object, twice as tall as the
fi rst one, is placed in front of the mirror, but at a diff erent location. The image
of this second object has the same height as the other image. How far in front
of the mirror is the second object located?
Concepts and Calculations Problems 731
30. M BIO GO A dentist’s mirror is placed 2.0 cm from a tooth. The enlarged image is located 5.6 cm behind the mirror. (a) What kind of mirror (plane, concave, or convex) is being used? (b) Determine the focal length of the mirror. (c) What is the magnifi cation? (d) How is the image oriented relative to the object?
31. M GO A tall tree is growing across a river from you. You would like to know the distance between yourself and the tree, as well as its height, but
are unable to make the measurements directly. However, by using a mirror
to form an image of the tree and then measuring the image distance and the
image height, you can calculate the distance to the tree as well as its height.
Suppose that this mirror produces an image of the sun, and the image is
located 0.9000 m from the mirror. The same mirror is then used to produce
an image of the tree. The image of the tree is 0.9100 m from the mirror.
(a) How far away is the tree? (b) The image height of the tree has a magnitude of 0.12 m. How tall is the tree?
32. M A spherical mirror is polished on both sides. When the concave side is used as a mirror, the magnifi cation is +2.0. What is the magnifi cation when the convex side is used as a mirror, the object remaining the same distance
from the mirror?
33. M GO Consult Multiple-Concept Example 7 to see a model for solving this type of problem. A concave makeup mirror is designed so the virtual
image it produces is twice the size of the object when the distance between
the object and the mirror is 14 cm. What is the radius of curvature of the
mirror?
34. H A concave mirror has a focal length of 30.0 cm. The distance between an object and its image is 45.0 cm. Find the object and image distances,
assuming that (a) the object lies beyond the center of curvature and (b) the object lies between the focal point and the mirror.
35. H SSM Available in WileyPLUS.
36. E An object is placed in front of a convex mirror. Draw the convex mir- ror (radius of curvature = 15 cm) to scale, and place the object 25 cm in front
of it. Make the object height 4 cm. Using a ray diagram, locate the image and
measure its height. Now move the object closer to the mirror, so the object
distance is 5 cm. Again, locate its image using a ray diagram. As the object
moves closer to the mirror, (a) does the magnitude of the image distance become larger or smaller, and (b) does the magnitude of the image height become larger or smaller? (c) What is the ratio of the image height when the object distance is 5 cm to its height when the object distance is 25 cm? Give
your answer to one signifi cant fi gure.
37. E SSM An object that is 25 cm in front of a convex mirror has an image located 17 cm behind the mirror. How far behind the mirror is the image
located when the object is 19 cm in front of the mirror?
38. E GO A concave mirror has a focal length of 42 cm. The image formed by this mirror is 97 cm in front of the mirror. What is the object distance?
39. E Review Conceptual Example 1 before attempting this problem. A person whose eyes are 1.70 m above the fl oor stands in front of a plane mir-
ror. The top of her head is 0.12 m above her eyes. (a) What is the height of the shortest mirror in which she can see her entire image? (b) How far above the fl oor should the bottom edge of the mirror be placed?
40. E V-HINT A drop of water on a countertop refl ects light from a fl ower held 3.0 cm directly above it. The fl ower’s diameter is 2.0 cm, and the dia-
meter of the fl ower’s image is 0.10 cm. What is the focal length of the water
drop, assuming that it may be treated as a convex spherical mirror?
41. E SSM Available in WileyPLUS.
42. M V-HINT Available in WileyPLUS. 43. M GO You walk at an angle of 𝜃 = 50.0° toward a plane mirror, as in the drawing. Your walking velocity has a magnitude of 0.90 m/s. What is the
velocity of your image relative to you (magnitude and direction)?
PROBLEM 43
You +x
vYM
+y
θ
44. M CHALK GO A candle is placed 15.0 cm in front of a convex mirror. When the convex mirror is replaced with a plane mirror, the image moves
7.0 cm farther away from the mirror. Find the focal length of the convex
mirror.
45. M SSM MMH Available in WileyPLUS. 46. H A man holds a double-sided spherical mirror so that he is looking directly into its convex surface, 45 cm from his face. The magnifi cation of the
image of his face is +0.20. What will be the image distance when he reverses the mirror (looking into its concave surface), maintaining the same distance
between the mirror and his face? Be sure to include the algebraic sign (+ or −) with your answer. 47. H SSM Available in WileyPLUS.
Additional Problems
Relative to the object in front of a spherical mirror, the image can diff er in a
number of respects. The image can be real (in front of the mirror) or virtual
(behind the mirror). It can be larger or smaller than the object, and it can be
upright or inverted. As you solve problems dealing with spherical mirrors,
keep these image characteristics in mind. They can help guide you to the
correct answer, as Problems 48 and 49 illustrate.
48. M CHALK An object is located 7.0 cm in front of a mirror. The virtual image is located 4.5 cm away from the mirror and is smaller than the object.
Concepts: (i) Based solely on the fact that the image is virtual, is the mirror concave or convex, or is either type possible? (ii) The image is smaller than
the object, as well as virtual. Do these characteristics together indicate a
concave or convex mirror, or is either type possible? (iii) Is the focal length
positive or negative? Explain. Calculation: Find the focal length of the mirror.
49. M CHALK SSM The radius of curvature of a mirror is 24 cm. A diamond ring is placed in front of this mirror. The image is twice the size of the ring.
Concepts and Calculations Problems
732 CHAPTER 25 The Reflection of Light: Mirrors
Concepts: (i) Is the mirror concave or convex, or is either type possible? (ii) How many places are there in front of a concave mirror where the ring
can be placed and produce an image twice the size of the object? (iii) What
are the possible values for the magnifi cation of the image of the ring? Calcu- lation: Find the object distance of the ring.
50. M An Unidentifi ed Flying Object. You and your team spot a strange object hovering over the open ocean in broad daylight. You have nothing to
reference in order to estimate its distance, height, or size, but you get the idea
to use a concave mirror from a signal light. You disassemble the light, extract
the mirror, and point it at the sun. You measure the distance to the sun’s image
from the center of the mirror to be 3.405 m. You then point the mirror at the
object and fi nd that its image forms 3.443 m from the center of the mirror.
The angle between the line of sight to the object and the horizontal is 28.5°.
(a) What is the distance between you and the object? (b) What is the height of the object above the ground? (c) If the width of the object’s image is 11.5 cm, what is the width of the object?
51. M Radius of Curvature of a Partial Sphere. You and your team need to estimate the radius of curvature of a panel that had been removed from
some unknown object. You were told that the object was spherical and, by the
size of the panel (about one square meter in area) and its slight curvature, you
estimate that the spherical object from which it came had been quite large.
You notice that the outer surface has a mirrored metallic fi nish (like a convex
mirror) and you get an idea. You fi nd a wrench that is 21.0 cm long, and hold
it at a distance of 10.0 m from the middle of the mirrored surface. The virtual
image of the wrench is 14.5 cm long. Determine the radius of the sphere from
which the panel came.
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
26.1 Define the index of refraction. 26.2 Use Snell’s law of refraction to solve
problems. 26.3 Analyze total internal reflection problems. 26.4 Define Brewster’s angle. 26.5 Analyze examples involving dispersion
of light. 26.6 Trace rays passing through converging
and diverging lenses. 26.7 Trace rays from objects through lenses
to form images. 26.8 Apply the lens and magnification
equations to solve problems. 26.9 Solve problems involving lenses in
combination. 26.10 Apply ray tracing and the lens and
magnification equations to the human eye. 26.11 Calculate angular size and angular
magnification. 26.12 Apply optical principles to the
compound microscope. 26.13 Apply optical principles to the telescope. 26.14 Describe spherical and chromatic lens
aberrations.
D es
ig n P
ic s/
S u p er
S to
ck
CHAPTER 26
The Refraction of Light: Lenses and Optical Instruments
When light moves from one medium into another, its direction of travel changes, and this change in direction
is called refraction. The human eye is an incredible optical instrument, and, as we will see, refraction plays
a major role in the way it works to produce clear vision.
26.1 The Index of Refraction As Section 24.3 discusses, light travels through a vacuum at a speed of c = 3.00 × 108 m/s. It can also travel through many materials, such as air, water, and glass. Atoms
in the material absorb, reemit, and scatter the light, however. Therefore, light travels
through the material at a speed that is less than c, the actual speed depending on the nature of the material. In general, we will see that the change in speed as a ray of light
goes from one material to another causes the ray to deviate from its incident direc-
tion. This change in direction is called refraction. To describe the extent to which the speed of light in a material medium diff ers from that in a vacuum, we use a parameter
called the index of refraction (or refractive index). The index of refraction is an important parameter because it appears in Snell’s law of refraction, which will be
discussed in the next section. This law is the basis of all the phenomena discussed in
this chapter.
733
734 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
DEFINITION OF THE INDEX OF REFRACTION The index of refraction n of a material is the ratio of the speed c of light in a vacuum to the speed 𝝊 of light in the material:
n = Speed of light in a vacuum
Speed of light in the material =
c υ
(26.1)
Table 26.1 lists the refractive indices for some common substances. The values of n are greater than unity because the speed of light in a material medium is less than it is in a vacuum.
For example, the index of refraction for diamond is n = 2.419, so the speed of light in diamond is 𝜐 = c/n = (3.00 × 108 m/s)/2.419 = 1.24 × 108 m/s. In contrast, the index of refraction for air (and also for other gases) is so close to unity that nair = 1 for most purposes. The index of refrac- tion depends slightly on the wavelength of the light, and the values in Table 26.1 correspond to a wavelength of 𝜆 = 589 nm in a vacuum.
26.2 Snell’s Law and the Refraction of Light
Snell’s Law When light strikes the interface between two transparent materials, such as air and water, the
light generally divides into two parts, as Figure 26.1a illustrates. Part of the light is refl ected, with the angle of refl ection equaling the angle of incidence. The remainder is transmitted
across the interface. If the incident ray does not strike the interface at normal incidence, the
transmitted ray has a diff erent direction than the incident ray. When a ray enters the second
material and changes direction, it is said to be refracted and behaves in one of the following
two ways:
1. When light travels from a medium where the refractive index is smaller into a medium where it is larger, the refracted ray is bent toward the normal, as in Figure 26.1a.
2. When light travels from a medium where the refractive index is larger into a medium where it is smaller, the refracted ray is bent away from the normal, as in Figure 26.1b.
These two possibilities illustrate that both the incident and refracted rays obey the principle
of reversibility. Thus, the directions of the rays in part a of the drawing can be reversed to give the situation depicted in part b. In part b the refl ected ray lies in the water rather than in the air.
In both parts of Figure 26.1 the angles of incidence, refraction, and refl ection are measured relative to the normal. Note that the index of refraction of air is labeled n1 in part a, whereas it is n2 in part b, because we label all variables associated with the incident (and refl ected) ray with subscript 1 and all variables associated with the refracted ray with subscript 2.
The angle of refraction 𝜃2 depends on the angle of incidence 𝜃1 and on the indices of refrac- tion, n2 and n1, of the two media. The relation between these quantities is known as Snell’s law of refraction, after the Dutch mathematician Willebrord Snell (1591–1626), who discovered it experimentally. At the end of this section is a proof of Snell’s law.
SNELL’S LAW OF REFRACTION When light travels from a material with refractive index n1 into a material with refrac- tive index n2, the refracted ray, the incident ray, and the normal to the interface between the materials all lie in the same plane. The angle of refraction 𝜽2 is related to the angle of incidence 𝜽1 by
n1 sin θ1 = n2 sin θ2 (26.2)
Example 1 illustrates the use of Snell’s law.
TABLE 26.1 Index of Refraction a
for Various Substances
Substance Index of
Refraction, n Solids at 20 °C Diamond 2.419
Glass, crown 1.523
Ice (0 °C) 1.309
Sodium chloride 1.544
Quartz
Crystalline 1.544
Fused 1.458
Liquids at 20 °C Benzene 1.501
Carbon disulfide 1.632
Carbon tetrachloride 1.461
Ethyl alcohol 1.362
Water 1.333
Gases at 0 °C, 1 atm Air 1.000 293
Carbon dioxide 1.000 45
Oxygen, O2 1.000 271
Hydrogen, H2 1.000 139
a Measured with light whose wavelength in a vacuum is
589 nm.
Water (n2 = 1.33)
Air (n1 = 1.00)
Normal Incident
ray
(a)
Reflected ray
Refracted ray
2θ
1θ 1θ
Water (n1 = 1.33)
Air (n2 = 1.00)
Normal
Incident ray
Reflected ray
Refracted ray
2θ
1θ 1θ
(b)
FIGURE 26.1 (a) When a ray of light is directed from air into water, part of the
light is refl ected at the interface and the
remainder is refracted into the water. The
refracted ray is bent toward the normal (𝜃2 < 𝜃1). (b) When a ray of light is directed from water into air, the refracted ray in air is bent
away from the normal (𝜃2 > 𝜃1).
26.2 Snell’s Law and the Refraction of Light 735
We have seen that refl ection and refraction of light waves occur simultaneously at the inter-
face between two transparent materials. It is important to keep in mind that light waves are
composed of electric and magnetic fi elds, which carry energy. The principle of conservation of
energy (see Chapter 6) indicates that the energy refl ected plus the energy refracted must add up
to equal the energy carried by the incident light, provided that none of the energy is absorbed by
the materials. The percentage of incident energy that appears as refl ected versus refracted light
depends on the angle of incidence and the refractive indices of the materials on either side of the
interface. For instance, when light travels from air toward water at perpendicular incidence, most
of its energy is refracted and little is refl ected. But when the angle of incidence is nearly 90° and
the light barely grazes the water surface, most of its energy is refl ected, with only a small amount
refracted into the water. On a rainy night, you probably have experienced the annoying glare that
results when light from an oncoming car just grazes the wet road. Under such conditions, most of
the light energy refl ects into your eyes.
THE PHYSICS OF . . . rearview mirrors. The simultaneous refl ection and refraction of light have applications in a number of devices. For instance, interior rearview mirrors in cars
often have adjustment levers. One position of the lever is for day driving, while the other is for
night driving and reduces glare from the headlights of the car behind. As Interactive Figure 26.2a indicates, this kind of mirror is a glass wedge with a back side that is silvered and highly refl ect-
ing. Part b of the picture shows the day setting. Light from the car behind follows path ABCD in reaching the driver’s eye. At points A and C, where the light strikes the air–glass surface, there are both refl ected and refracted rays. The refl ected rays are drawn as thin lines, the thinness
denoting that only a small percentage (about 10%) of the light during the day is refl ected at A and C. The weak refl ected rays at A and C do not reach the driver’s eye. In contrast, almost all
EXAMPLE 1 Determining the Angle of Refraction
A light ray strikes an air/water surface at an angle of 46° with respect
to the normal. The refractive index for water is 1.33. Find the angle
of refraction when the direction of the ray is (a) from air to water and (b) from water to air.
Reasoning Snell’s law of refraction applies to both part (a) and part (b). However, in part (a) the incident ray is in air, whereas in part (b) it is in
water. We keep track of this diff erence by always labeling the variables
associated with the incident ray with a subscript 1 and the variables asso-
ciated with the refracted ray with a subscript 2.
Problem-Solving Insight The angle of incidence 𝜽1 and the angle of refraction 𝜽2 that appear in Snell’s law are mea- sured with respect to the normal to the surface, and not with respect to the surface itself.
Solution (a) The incident ray is in air, so 𝜃1 = 46° and n1 = 1.00. The refracted ray is in water, so n2 = 1.33. Snell’s law can be used to fi nd the angle of refraction 𝜃2:
sin θ2 = n1sin θ1
n 2 =
(1.00) sin 46°
1.33 = 0.54 (26.2)
θ2 = sin−1(0.54) = 33°
Since 𝜃2 is less than 𝜃1, the refracted ray is bent toward the normal, as Figure 26.1a shows. (b) With the incident ray in water, we fi nd that
sin θ2 = n 1sin θ1
n 2 =
(1.33) sin 46°
1.00 = 0.96
θ2 = sin−1(0.96) = 74°
Since 𝜃2 is greater than 𝜃1, the refracted ray is bent away from the normal, as in Figure 26.1b.
Silvered mirror (back surface
of wedge)
Driver
Light from car behind
Transparent glass wedge
Day–night lever
(a) (b) Day setting
D
C B A
Driver
Light from car behind
(c) Night setting
D
C
BA
INTERACTIVE FIGURE 26.2 A car’s interior rearview mirror with a day–night adjustment lever.
736 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
the light reaching the silvered back surface at B is refl ected toward the driver. Since most of the light follows path ABCD, the driver sees a bright image of the car behind. During the night, the adjustment lever can be used to rotate the top of the mirror away from the driver (see part c of the drawing). Now, most of the light from the headlights behind follows path ABC and does not reach the driver. Only the light that is weakly refl ected from the front surface along path AD is seen, and the result is signifi cantly less glare.
Apparent Depth One interesting consequence of refraction is that an object lying under water appears to be closer
to the surface than it actually is. Example 2 sets the stage for explaining why, by showing what
must be done to shine a light on such an object.
EXAMPLE 2 Finding a Sunken Chest
A searchlight on a yacht is being used at night to illuminate a sunken
chest, as in Figure 26.3. At what angle of incidence 𝜃1 should the light be aimed?
Reasoning The angle of incidence 𝜃1 must be such that, after refrac- tion, the light strikes the chest. The angle of incidence can be obtained
from Snell’s law, once the angle of refraction 𝜃2 is determined. This angle can be found using the data in Figure 26.3 and trigonometry. The light travels from a region of lower into a region of higher refrac-
tive index, so the light is bent toward the normal and we expect 𝜃1 to be greater than 𝜃2.
Problem-Solving Insight Remember that the refractive indices are written as n1 for the medium in which the incident light travels and n2 for the medium in which the refracted light travels.
Solution From the data in the drawing it follows that tan 𝜃2 = (2.0 m)/ (3.3 m), so 𝜃2 = 31°. With n1 = 1.00 for air and n2 = 1.33 for water, Snell’s law gives
sin θ1 = n2 sin θ2
n1 =
(1.33) sin 31°
1.00 = 0.69
θ1 = sin−1(0.69) = 44°
As expected, 𝜃1 is greater than 𝜃2.
3.3 m
1θ
2θ Water
(n2 = 1.33)
Air (n1 = 1.00)
Chest
2.0 m
FIGURE 26.3 The beam from the searchlight is refracted when it enters the water.
When the sunken chest in Example 2 is viewed from the boat (Figure 26.4a), light rays from the chest pass upward through the water, refract away from the normal when they enter the air, and
then travel to the observer. This picture is similar to Figure 26.3, except that the direction of the rays is reversed and the searchlight is replaced by an observer. When the rays entering the air are
extended back into the water (see the dashed lines), they indicate that the observer sees a virtual
(a)
Actual depth
Chest
Image
Apparent depth
(b)
Observer
Apparent depth = d ´ Actual
depth = d
FIGURE 26.4 (a) Because light from the chest is refracted
away from the normal when the
light enters the air, the apparent
depth of the image is less than
the actual depth. (b) The observer is viewing the submerged object
from directly overhead.
26.2 Snell’s Law and the Refraction of Light 737
image of the chest at an apparent depth that is less than the actual depth. The image is virtual because light rays do not actually pass through it. For the situation shown in Figure 26.4a, it is dif- fi cult to determine the apparent depth. A much simpler case is shown in part b, where the observer is directly above the submerged object, and the apparent depth dʹ is related to the actual depth d by
Apparent depth, observer directly above object
d′ = d (n2n1) (26.3)
In this result, n1 is the refractive index of the medium associated with the incident ray (the medium in which the object is located), and n2 refers to the medium associated with the refracted ray (the medium in which the observer is situated). The proof of Equation 26.3 is the focus of
Problem 23 at the end of the chapter. Example 3 illustrates that the eff ect of apparent depth is
quite noticeable in water.
EXAMPLE 3 The Apparent Depth of a Swimming Pool
A swimmer is treading water (with her head above the water) at the sur-
face of a pool 3.00 m deep. She sees a coin on the bottom directly below.
How deep does the coin appear to be?
Reasoning Equation 26.3 may be used to fi nd the apparent depth, pro- vided we remember that the light rays travel from the coin to the swimmer.
Therefore, the incident ray is coming from the coin under the water (n1 = 1.33), while the refracted ray is in the air (n2 = 1.00).
Solution The apparent depth dʹ of the coin is
d′ = d ( n2 n1) = (3.00 m) (
1.00
1.33) = 2.26 m (26.3)
In Example 3, a person sees a coin on the bottom of a pool at an apparent depth that is less
than the actual depth. Conceptual Example 4 considers the reverse situation—namely, a person
looking from under the water at a coin in the air.
CONCEPTUAL EXAMPLE 4 On the Inside Looking Out
A swimmer is under water and looking up at the surface. Someone holds
a coin in the air, directly above the swimmer’s eyes. To the swimmer,
the coin appears to be at a certain height above the water. Is the apparent
height of the coin (a) greater than, (b) less than, or (c) the same as its actual height?
Reasoning Figure 26.5 shows two rays of light leaving a point P on the coin. When the rays enter the water, they are refracted toward the normal
because water has a larger index of refraction than air has. By extending
the refracted rays backward (see the dashed lines in the drawing), we fi nd
that they appear to originate from a point Pʹ on a virtual image, which is what the swimmer sees.
Answers (b) and (c) are incorrect. These answers are incorrect because the point Pʹ in Figure 26.5 is located at a height that is greater than, not less than or the same as, the actual height of the coin.
Answer (a) is correct. The point Pʹ in Figure 26.5 is on a virtual image that is located at an apparent height dʹ that is greater than the actual height d. Equation 26.3 [dʹ = d(n2/n1)] reveals the same result, because n1 repre- sents the medium (air) associated with the incident ray and n2 represents the medium (water) associated with the refracted ray. Since n2 for water is greater than n1 for air, the ratio n2/n1 is greater than one and dʹ is larger than d. This situation is the opposite of that in Figure 26.4b, where an object beneath the water appears to a person above the water to be closer
to the surface than it actually is.
Related Homework: Problems 19, 108
Swimmer´s eye
Actual height = d
Apparent height = d ´
Coin (edge view)
Air
Water
P´
P
FIGURE 26.5 Rays from point P on a coin in the air above the water refract toward the normal as they enter the water. An underwater swimmer
perceives the rays as originating from a point Pʹ that is farther above the surface than the actual point P.
738 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
The Displacement of Light by a Transparent Slab of Material A windowpane is an example of a transparent slab of material. It consists of a plate of glass with
parallel surfaces. When a ray of light passes through the glass, the emergent ray is parallel to the
incident ray but displaced from it, as Figure 26.6 shows. This result can be verifi ed by applying Snell’s law to each of the two glass surfaces, with the result that n1 sin 𝜃1 = n2 sin 𝜃2 = n3 sin 𝜃3. Since air surrounds the glass, n1 = n3, and it follows that sin 𝜃1 = sin 𝜃3. Therefore, 𝜃1 = 𝜃3, and the emergent and incident rays are parallel. However, as the drawing shows, the emergent ray
is displaced laterally relative to the incident ray. The extent of the displacement depends on the
angle of incidence, the thickness of the slab, and the refractive index of the slab.
Derivation of Snell’s Law Snell’s law can be derived by considering what happens to the wave fronts when the light passes
from one medium into another. Figure 26.7a shows light propagating from medium 1, where the speed is relatively large, into medium 2, where the speed is smaller; therefore, n1 is less than n2. The plane wave fronts in this picture are drawn perpendicular to the incident and refracted rays. Since the part of each wave front that penetrates medium 2 slows down, the wave fronts in
medium 2 are rotated clockwise relative to those in medium 1. Correspondingly, the refracted ray
in medium 2 is bent toward the normal, as the drawing shows.
Although the incident and refracted waves have diff erent speeds, they have the same fre- quency f. The fact that the frequency does not change can be understood in terms of the atomic mechanism underlying the generation of the refracted wave. When the electromagnetic wave
strikes the surface, the oscillating electric fi eld forces the electrons in the molecules of medium
2 to oscillate at the same frequency as the wave. The accelerating electrons behave like atomic
antennas that radiate “extra” electromagnetic waves, which combine with the original wave. The
net electromagnetic wave within medium 2 is a superposition of the original wave plus the extra
radiated waves, and it is this superposition that constitutes the refracted wave. Since the extra
waves are radiated at the same frequency as the original wave, the refracted wave also has the
same frequency as the original wave.
The distance between successive wave fronts in Figure 26.7a has been chosen to be the wavelength 𝜆. Since the frequencies are the same in both media but the speeds are diff erent,
it follows from Equation 16.1 that the wavelengths are diff erent: 𝜆1 = 𝜐1/f and 𝜆2 = 𝜐2/f. Since 𝜐1 is assumed to be larger than 𝜐2, 𝜆1 is larger than 𝜆2, and the wave fronts are farther apart in
medium 1.
Figure 26.7b shows an enlarged view of the incident and refracted wave fronts at the surface. The angles 𝜃1 and 𝜃2 within the colored right triangles are, respectively, the angles of incidence and refraction. In addition, the triangles share the same hypotenuse h. Therefore,
sin θ1 = λ1 h
= υ1 /f
h =
υ1 hf
Glass (n2)
Air (n3 = n1)
Air (n1)
Incident ray
Emergent ray
Displacement
2θ
2θ
1θ
3θ
FIGURE 26.6 When a ray of light passes through a pane of glass that has parallel
surfaces and is surrounded by air, the
emergent ray is parallel to the incident ray
(𝜃3 = 𝜃1) but is displaced from it.
Medium 1
Medium 2
Incident ray
Fast-moving incident
wave fronts
Refracted ray
Slow-moving refracted
wave fronts
h
(a) (b)
λ 1
λ 2
λ 1 θ 1
θ 1
θ 2
θ 2
λ 2
FIGURE 26.7 (a) The wave fronts are refracted as the light passes from medium 1
into medium 2. (b) An enlarged view of the in- cident and refracted wave fronts at the surface.
26.3 Total Internal Reflection 739
and
sin θ2 = λ2 h
= υ2 /f
h =
υ2 hf
Combining these two equations into a single equation by eliminating the common term hf gives
sin θ1 υ1
= sin θ2
υ2 By multiplying each side of this result by c, the speed of light in a vacuum, and recognizing that the ratio c/𝜐 is the index of refraction n, we arrive at Snell’s law of refraction: n1 sin 𝜃1 = n2 sin 𝜃2.
Check Your Understanding
(The answers are given at the end of the book.) 1. Two slabs with parallel faces are made from diff erent types of
glass. A ray of light travels through air and enters each slab at the
same angle of incidence, as CYU Figure 26.1 shows. Which slab has the greater index of refraction?
2. CYU Figure 26.2 shows three layers of liquids, A, B, and C, each with a diff erent index of refraction. Light begins in liquid A, passes
into B, and eventually into C, as the ray of light in the drawing shows.
The dashed lines denote the normals to the interfaces between
the layers. Which liquid has the smallest index of refraction?
3. Light traveling through air is incident on a fl at piece of glass at a 35° angle of incidence and enters the glass at an angle of
refraction 𝜃glass. Suppose that a layer of water is added on top of the glass. Then the light travels through air and is incident
on the water at the 35° angle of incidence. Does the light enter
the glass at the same angle of refraction 𝜃glass as it did when the water was not present?
4. Two identical containers, one fi lled with water (n = 1.33) and the other with benzene (n = 1.50), are viewed from directly above. Which container (if either) appears to have a greater
depth of fl uid?
5. When an observer peers over the edge of a deep, empty, metal bowl on a kitchen table, he does not see the entire bottom surface. Therefore, a small object lying on
the bottom is hidden from view, but the object can be seen when the bowl is fi lled with liquid A. When
the bowl is fi lled with liquid B, however, the object remains hidden from view. Which liquid has the
greater index of refraction?
6. A man is fi shing from a dock, using a bow and arrow. To strike a fi sh that he sees beneath the water, should he aim (a) somewhat above the fi sh, (b) directly at the fi sh, or (c) somewhat below the fi sh?
7. A man is fi shing from a dock. He is using a laser gun that emits an intense beam of light. To strike a fi sh that he sees beneath the water, should he aim (a) somewhat above the fi sh, (b) directly at the fi sh, or (c) somewhat below the fi sh?
8. Two rays of light converge to a point on a screen. A thick plate of glass with parallel surfaces is placed in the path of this converging light, with the parallel surfaces parallel to the screen. Will the point of conver-
gence (a) move away from the glass plate, (b) move toward the glass plate, or (c) remain on the screen?
26.3 Total Internal Reflection When light passes from a medium of larger refractive index into one of smaller refractive index—
for example, from water to air—the refracted ray bends away from the normal, as in Animated Figure 26.8a. As the angle of incidence increases, the angle of refraction also increases. When the angle of incidence reaches a certain value, called the critical angle 𝜃c, the angle of refraction is 90°. Then the refracted ray points along the surface; Animated Figure 26.8b illustrates
Slab A Slab B
CYU FIGURE 26.1
Liquid A
Liquid B
Liquid C
CYU FIGURE 26.2
740 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
what happens at the critical angle. When the angle of incidence exceeds the critical angle, as in
Animated Figure 26.8c, there is no refracted light. All the incident light is refl ected back into the medium from which it came, a phenomenon called total internal refl ection. Total internal refl ec- tion occurs only when light travels from a higher-index medium toward a lower-index medium.
It does not occur when light propagates in the reverse direction—for example, from air to water.
An expression for the critical angle 𝜃c can be obtained from Snell’s law by setting 𝜃1 = 𝜃c and 𝜃2 = 90° (see Animated Figure 26.8b):
sin θc = n 2sin 90°
n1
Critical angle sin θc = n 2 n1 (n1 > n 2) (26.4)
For instance, the critical angle for light traveling from water (n1 = 1.33) to air (n2 = 1.00) is 𝜃c = sin−1(1.00/1.33) = 48.8°. For incident angles greater than 48.8°, Snell’s law predicts that sin 𝜃2 is greater than unity, a value that is not possible. Thus, light rays with incident angles exceeding 48.8°
yield no refracted light, and the light is totally refl ected back into the water, as Animated Figure 26.8c indicates. Then, the air–water interface acts like a mirror. Figure 26.9, for example, shows the mirror-like ability of the interface to form a refl ected image of a salamander with its snout near
the surface of the water. Light from the salamander’s body that strikes the surface at angles exceed-
ing the critical angle is refl ected to form the image in the upper part of the photograph.
The next example illustrates how the critical angle changes when the indices of refraction
change.
Water (n1 = 1.33)
Air (n2 = 1.00)
Incident ray
Reflected ray
Refracted ray 2θ
1θ 1θ
(a)
2 = 90°θ
cθ cθ
(b)
n1
n2
Total internal reflection
cθ
(c)
n1
n2
ANIMATED FIGURE 26.8 (a) When light travels from a higher-index medium (water) into a lower-index medium (air), the refracted ray is bent away from the normal. (b) When the angle of incidence is equal to the critical angle 𝜃c, the angle of refraction is 90°. (c) If 𝜃1 is greater than 𝜃c, there is no refracted ray, and total internal refl ection occurs.
FIGURE 26.9 This underwater photograph shows a salamander with its snout near the
surface of the water. Some of the light from
its body strikes the air–water interface at
angles greater than the critical angle and is
refl ected. Thus, the interface acts like a mirror
and forms the image in the upper part of the
photograph.
Reinhard Dirscherl/Age Fotostock
EXAMPLE 5 Total Internal Reflection
A beam of light is propagating through diamond (n1 = 2.42) and strikes a diamond–air interface at an angle of incidence of 28°. (a) Will part of the beam enter the air (n2 = 1.00) or will the beam be totally refl ected at the interface? (b) Repeat part (a), assuming that the diamond is surrounded by water (n2 = 1.33) instead of air.
Reasoning Total internal refl ection occurs only when the beam of light has an angle of incidence that is greater than the critical angle 𝜃c. The crit- ical angle is diff erent in parts (a) and (b), since it depends on the ratio n2/ n1 of the refractive indices of the incident (n1) and refracting (n2) media.
Solution (a) The critical angle 𝜃c for total internal refl ection at the diamond–air interface is given by Equation 26.4 as
θc = sin−1 ( n 2 n1 ) = sin−1 (
1.00
2.42) = 24.4°
Because the angle of incidence of 28° is greater than the critical angle, there is no refraction, and the light is totally refl ected back into the diamond.
(b) If water, rather than air, surrounds the diamond, the critical angle for total internal refl ection becomes larger:
θc = sin−1 ( n 2 n1 ) = sin−1 (
1.33
2.42) = 33.3° Now a beam of light that has an angle of incidence of 28° (less than the critical angle of 33.3°) at the diamond–water interface is refracted into the water.
The critical angle plays an important role in why a diamond sparkles, as Conceptual
Example 6 discusses.
26.3 Total Internal Reflection 741
Many optical instruments, such as binoculars, periscopes, and telescopes, use glass prisms
and total internal refl ection to turn a beam of light through 90° or 180°. Figure 26.11a shows a light ray entering a 45°–45°–90° glass prism (n1 = 1.5) and striking the hypotenuse of the prism at an angle of incidence of 𝜃1 = 45°. Equation 26.4 shows that the critical angle for a glass–air interface is 𝜃c = sin−1(n2/n1) = sin−1(1.0/1.5) = 42°. Since the angle of incidence is greater than
CONCEPTUAL EXAMPLE 6 The Physics of Why a Diamond Sparkles
A diamond gemstone is famous for its sparkle in air because the light
coming from it glitters as the diamond is moved about. The sparkle
is related to the total internal refl ection of light that occurs within the
diamond. What happens to the sparkle when the diamond is placed under
water? (a) Nothing happens, for the water has no eff ect on total internal refl ection. (b) The water reduces the sparkle markedly by making the total internal refl ection less likely to occur.
Reasoning When a diamond is held in a certain way in air, the inten- sity of the light coming from within it is greatly enhanced. Figure 26.10 helps to explain that this enhancement or sparkle is related to total inter-
nal refl ection. Part a of the drawing shows a ray of light striking a lower facet of the diamond at an angle of incidence that exceeds the critical
angle for a diamond–air interface. As a result, this ray undergoes total
internal refl ection back into the diamond and eventually exits the top sur-
face. Since diamond has a relatively small critical angle in air, many of the
rays striking a lower facet behave in this fashion and create the diamond’s
sparkle. Part (a) of Example 5 shows that the critical angle is 24.4° and
is so small because the index of refraction of diamond (n = 2.42) is large compared to that of air (n = 1.00).
Answer (a) is incorrect. The water does indeed have an eff ect on the total internal refl ection that occurs. This is because the critical angle
depends on the index of refraction of the water as well as that of the dia-
mond (see Equation 26.4).
Answer (b) is correct. Figure 26.10b illustrates what happens to the same ray of light within the diamond when the diamond is surrounded
by water. Because water has a larger index of refraction than air does,
the critical angle for the diamond–water interface is no longer 24.4°
but increases to 33.3°, as part (b) of Example 5 shows. Therefore, this
particular ray is no longer totally internally refl ected. As Figure 26.10b indicates, only some of the light is now refl ected back into the dia-
mond, while the remainder escapes into the water. Consequently, less
light exits from the top of the diamond, causing it to lose much of its
sparkle.
Critical angle for diamond in air
(b)
Critical angle for diamond in water
Entering light
(a)
FIGURE 26.10 (a) Near the bottom of the diamond, light is totally internally refl ected, because the incident angle exceeds the critical angle for diamond and air. (b) When the diamond is in water, the same light is partially refl ected and partially refracted, since the incident angle is less than the critical angle for diamond and water.
1 = 45°θ
45° 45°
45°
(a) (b) (c)
Normal
45°
45°
45°
45°
Prisms
Light ray
FIGURE 26.11 Total internal refl ection at a glass–air interface can be used to turn a ray of light through an angle of (a) 90° or (b) 180°. (c) Two prisms, each refl ecting the light twice by total internal refl ection, are sometimes used in binoculars to produce a lateral displacement of a light ray.
742 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
the critical angle, the light is totally refl ected at the hypotenuse and is directed vertically upward
in the drawing, having been turned through an angle of 90°. Figure 26.11b shows how the same prism can turn the beam through 180° when total internal refl ection occurs twice. Prisms can also
be used in tandem to produce a lateral displacement of a light ray, while leaving its initial direc-
tion unaltered. Figure 26.11c illustrates such an application in binoculars. THE PHYSICS OF . . . fiber optics. An important application of total internal refl ec-
tion occurs in fi ber optics, where hair-thin threads of glass or plastic, called optical fi bers, “pipe”
light from one place to another. Figure 26.12a shows that an optical fi ber consists of a cylindri- cal inner core that carries the light and an outer concentric shell, the cladding. The core is made from transparent glass or plastic that has a relatively high index of refraction. The cladding is
also made of glass, but of a type that has a relatively low index of refraction. Light enters one
end of the core, strikes the core/cladding interface at an angle of incidence greater than the
critical angle, and, therefore, is refl ected back into the core. Light thus travels inside the optical
fi ber along a zigzag path. In a well-designed fi ber, little light is lost as a result of absorption by
the core, so light can travel many kilometers before its intensity diminishes appreciably. Optical
fi bers are often bundled together to produce cables. Because the fi bers themselves are so thin, the
cables are relatively small and fl exible and can fi t into places inaccessible to larger metal wires.
Example 7 deals with the light entering and traveling in an optical fi ber.
G eo
rg e
D o y le
/G et
ty I
m ag
es
Light ray Cladding Core
(a) (b)
FIGURE 26.12 (a) Light can travel with little loss in a curved optical fi ber, because the
light is totally refl ected whenever it strikes
the core–cladding interface and because the
absorption of light by the core itself is small.
(b) Light being transmitted by a bundle of optical fi bers.
Analyzing Multiple-Concept Problems
EXAMPLE 7 An Optical Fiber
Figure 26.13 shows an optical fi ber that consists of a core made of fl int glass (nfl int = 1.667) surrounded by a cladding made of crown glass (ncrown = 1.523). A ray of light in air enters the fi ber at an angle 𝜃1 with respect to the normal. What is 𝜃1 if this light also strikes the core–cladding interface at an angle that just barely exceeds the critical angle?
Reasoning The angle of incidence 𝜃1 is related to the angle of refraction 𝜃2 (see Figure 26.13) by Snell’s law, where 𝜃2 is part of the right triangle in the drawing. The critical angle 𝜃c for the core–cladding interface is also part of the same right triangle, so that 𝜃2 = 90° − 𝜃c. The critical angle can be determined from a knowledge of the indices of refraction of the
core and the cladding.
Knowns and Unknowns The data used in this problem are:
Description Symbol Value Comment Index of refraction of core material (flint glass) nflint 1.667
Index of refraction of cladding material (crown glass) ncrown 1.523
Index of refraction of air nair 1.000 See Table 26.1.
Unknown Variable Angle of incidence of light ray entering optical fiber 𝜃1 ?
CoreAir Cladding
cθ
1θ 2θ
FIGURE 26.13 A ray of light enters the left end of an optical fi ber and strikes the core–
cladding interface at an angle that just barely
exceeds the critical angle 𝜃c.
CoreAir Cladding
cθ
1θ 2θ
FIGURE 26.13 (REPEATED) A ray of light enters the left end of an optical
fi ber and strikes the core–cladding
interface at an angle that just barely
exceeds the critical angle 𝜃c.
26.3 Total Internal Reflection 743
Optical fi ber cables are the medium of choice for high-quality telecommunications because
the cables are relatively immune to external electrical interference and because a light beam can
carry information through optical fi bers just as electricity carries information through copper
wires. The information-carrying capacity of light, however, is thousands of times greater than
that of electricity. A laser beam traveling through a single optical fi ber can carry tens of thou-
sands of telephone conversations and several TV programs simultaneously.
BIO THE PHYSICS OF . . . endoscopy. In the fi eld of medicine, optical fi ber cables have had extraordinary impact. In the practice of endoscopy, for instance, a device called an
endoscope is used to peer inside the body. Figure 26.14 shows a bronchoscope being used, which is a kind of endoscope that is inserted through the nose or mouth, down the bronchial
tubes, and into the lungs. It consists of two optical fi ber cables. One provides light to illuminate
interior body parts, while the other sends back an image for viewing. A bronchoscope greatly
simplifi es the diagnosis of pulmonary disease. Tissue samples can even be collected with some
bronchoscopes. A colonoscope is another kind of endoscope, and its design is similar to that of
the bronchoscope. It is inserted through the rectum and used to examine the interior of the colon
(see Figure 26.15). The colonoscope currently off ers the best hope for diagnosing colon cancer in its early stages, when it can be treated.
Modeling the Problem
STEP 1 Snell’s Law of Refraction The ray of light, initially traveling in air, strikes the left end of the optical fi ber at an angle of incidence labeled 𝜃1 in Figure 26.13. When the light en- ters the fl int-glass core, its angle of refraction is 𝜃2. Snell’s law of refraction gives the relation between these angles as
nair sin θ1 = nflint sin θ2 (26.2)
Solving this equation for 𝜃1 yields Equation 1 at the right. Values for nair and nfl int are known. The angle 𝜃2 will be evaluated in the next step.
STEP 2 The Critical Angle We know that the light ray inside the core strikes the core– cladding interface at an angle that just barely exceeds the critical angle 𝜃c. When the angle of incidence exceeds the critical angle, all the light is refl ected back into the core. From the right
triangle in Figure 26.13, we see that the critical angle is related to 𝜃2 by 𝜃2 = 90° − 𝜃c. The critical angle depends on the indices of refraction of the core (fl int glass) and cladding (crown glass)
according to Equation 26.4:
sin θc = n crown n flint or θc = sin−1 (
n crown nflint )
Substituting this expression for 𝜃c into 𝜃2 = 90° − 𝜃c gives
θ2 = 90° − sin−1 ( n crown nflint )
This result for 𝜃2 can be substituted into Equation 1, as indicated at the right.
Solution Combining the results of Steps 1 and 2 algebraically to produce a single equation gives a rather cumbersome result. Hence, we follow the simpler procedure of evaluating Equation 2
numerically and then substituting the result into Equation 1:
θ 2 = 90° − sin−1 ( n crown nflint ) = 90° − sin−1 (
1.523
1.667) = 23.99° (2)
θ1 = sin−1 ( nflint sin θ 2
n air ) = sin−1 ( 1.667 sin 23.99°
1.000 ) = 42.67° Related Homework: Problem 33
66.01°
θ1 = sin−1 ( nflint sin θ 2
n air ) (1) ?
θ1 = sin−1 ( nflint sin θ 2
n air ) (1)
θ2 = 90° − sin−1 ( n crown nflint ) (2)
744 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
BIO THE PHYSICS OF . . . arthroscopic surgery. The use of optical fi bers has also revolutionized surgical techniques. In arthroscopic surgery, a small surgical instrument, several
millimeters in diameter, is mounted at the end of an optical fi ber cable. The surgeon can insert the
instrument and cable into a joint, such as the knee, with only a tiny incision and minimal dam-
age to the surrounding tissue (see Figure 26.16). Consequently, recovery from the procedure is relatively rapid compared to recovery from traditional surgical techniques.
Check Your Understanding
(The answers are given at the end of the book.) 9. CYU Figure 26.3 shows a 30°–
60°–90° prism and two light rays,
A and B, that both strike the prism
perpendicularly. The prism is sur-
rounded by an unknown liquid,
which is the same in both parts of
the drawing. When ray A reaches
the hypotenuse in the drawing,
it is totally internally refl ected.
Which one of the following state-
ments applies to ray B when it reaches the hypotenuse? (a) It may or may not be totally internally refl ected, depending on what the surrounding liquid is. (b) It is not totally internally refl ected, no matter what the surrounding liquid is. (c) It is totally internally refl ected, no matter what the surround- ing liquid is.
10. A shallow swimming pool has a constant depth. A point source of light is located in the middle of the bottom of this pool and emits light in all directions. However, no light exits the surface of the water
except through a relatively small circular area that is centered on and directly above the light source.
Why does the light exit the water through such a limited area?
11. Refer to Figure 26.6. Note that the ray within the glass slab is traveling from a medium with a larger refractive index toward a medium with a smaller refractive index. Is it possible, for 𝜃1 less than 90°, that the ray within the glass will experience total internal refl ection at the glass–air interface?
FIGURE 26.14 A doctor is using a broncho- scope to examine the lungs of a patient
who has a history of asthma and allergies.
JA M
E S
K IN
G -H
O L
M E
S /S
P L
/S ci
en ce
S o u rc
e Polyp
FIGURE 26.15 A colonoscope revealed this benign (noncancerous) polyp attached to the wall of the colon
(large intestine). Polyps that can turn cancerous or
grow large enough to obstruct the colon are removed
surgically.
IS M
/M ed
ic al
I m
ag es
A
30°
60°
B
30°
60°
CYU FIGURE 26.3
FIGURE 26.16 Optical fi bers have made arthroscopic surgery possible, such as the repair
of the damaged knee shown here.
M ar
g ar
et R
o se
O rt
h o p ae
d ic
H o sp
it al
/S ci
en ce
S o u rc
e
26.4 Polarization and the Reflection and Refraction of Light 745
26.4 Polarization and the Reflection and Refraction of Light For incident angles other than 0°, unpolarized light becomes partially polarized in refl ecting from
a nonmetallic surface, such as water. To demonstrate this fact, rotate a pair of Polaroid sunglasses
in the sunlight refl ected from a lake. You will see that the light intensity transmitted through the
glasses is a minimum when the glasses are oriented as they are normally worn. Since the trans-
mission axis of the glasses is aligned vertically, it follows that the light refl ected from the lake is
partially polarized in the horizontal direction.
There is one special angle of incidence at which the refl ected light is completely polarized
parallel to the surface, the refracted ray being only partially polarized. This angle is called the
Brewster angle 𝜃B. Figure 26.17 summarizes what happens when unpolarized light strikes a nonmetallic surface at the Brewster angle. The value of 𝜃B is given by Brewster’s law, in which n1 and n2 are, respectively, the refractive indices of the materials in which the incident and refracted rays propagate:
Brewster’s law tan θB = n 2 n1
(26.5)
Math Skills Since the refl ected and refracted rays are perpendicular in Figure 26.17, it follows that θB + 90° + θ2 = 180° or θB + θ2 = 90°. To see that this is indeed the case, we take advantage of Snell’s law (Equation 26.2). For an incident angle θ1 = θB, this law is
sin θB = n2 sin θ2
n1
In addition, Brewster’s law states that tan θB = n2 n1
(Equation 26.5), and tan θB = sin θB cos θB
(see Appendix E.2,
Other Trigonometric Identities, Equation 4). Therefore, we can substitute sin θB cos θB
= n 2 n1
into Snell’s law
and obtain
sin θB = ( n2 n1) sin θ2 =
sin θB cos θB
sin θ2
or cos θB = sin θ2
This result is what we are looking for, because sin θ2 = cos (90° − θ2) (see Appendix E.2, Other Trigonometric Identities, Equation 7). Thus, we have
cos θB = sin θ2 = cos (90° − θ2 ) or θB = 90° − θ2 or θB + θ2 = 90°
90°
Partially polarized refracted
light
θB θB
θ2
n1
n2
Polarized reflected lightUnpolarized incident light
FIGURE 26.17 When unpolarized light is incident on a nonmetallic surface at the
Brewster angle 𝜃B, the refl ected light is 100% polarized in a direction parallel to the
surface. The angle between the refl ected and
refracted rays is 90°.
This relation is named after the Scotsman David Brewster (1781–1868), who discovered it.
Figure 26.17 also indicates that the refl ected and refracted rays are perpendicular to each other when light strikes the surface at the Brewster angle.
746 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
Check Your Understanding
(The answer is given at the end of the book.) 12. You are sitting by the shore of a lake on a sunny and windless day. When are your Polaroid sunglasses
most eff ective in reducing the glare of the sunlight refl ected from the lake surface? When the angle of
incidence of the sunlight on the lake is ______. (a) almost 90° because the sun is low in the sky (b) 0° because the sun is directly overhead (c) somewhere between 90° and 0°
26.5 The Dispersion of Light: Prisms and Rainbows Figure 26.18a shows a ray of monochromatic light passing through a glass prism surrounded by air. When the light enters the prism at the left face, the refracted ray is bent toward the normal,
because the refractive index of glass is greater than that of air. When the light leaves the prism at
the right face, it is refracted away from the normal. Thus, the net eff ect of the prism is to change
the direction of the ray, causing it to bend downward upon entering the prism, and downward
again upon leaving. Because the refractive index of the glass depends on wavelength (see
Table 26.2), rays corresponding to diff erent colors are bent by diff erent amounts by the prism and depart traveling in diff erent directions. The greater the index of refraction for a given color,
the greater the bending, and Figure 26.18b shows the refractions for the colors red and violet, which are at opposite ends of the visible spectrum. If a beam of sunlight, which contains all colors,
is sent through the prism, the sunlight is separated into a spectrum of colors, as Figure 26.18c shows. The spreading of light into its color components is called dispersion.
In Figure 26.18a the ray of light is refracted twice by a glass prism surrounded by air. Con- ceptual Example 8 explores what happens to the light when the prism is surrounded by materials
other than air.
TABLE 26.2 Indices of Refraction n of Crown Glass at Various Wavelengths
Colora
Vacuum Wavelength
(nm)
Index of Refraction,
n
Red 660 1.520
Orange 610 1.522
Yellow 580 1.523
Green 550 1.526
Blue 470 1.531
Violet 410 1.538
aApproximate
FIGURE 26.18 (a) A ray of light is refracted as it passes through a prism. The prism is surrounded by air. (b) Two diff erent colors are refracted by diff erent amounts. For clarity, the amount of refraction has been exaggerated. (c) Sunlight is dispersed into its color components by this prism.
Glass prism
Normal Normal
Incident light
Incident light
(a) (b)
Red (660 nm)
Violet (410 nm)
(c)
G IP
h o to
S to
ck /S
ci en
ce S
o u rc
e
CONCEPTUAL EXAMPLE 8 The Refraction of Light Depends on Two Refractive Indices
In Figure 26.18a the glass prism is surrounded by air and bends the ray of light downward. It is also possible for the prism to bend the ray upward, as
in Figure 26.19a, or to not bend the ray at all, as in part b of the drawing. How can the situations illustrated in Figure 26.19 arise?
Reasoning and Solution Snell’s law of refraction includes the refrac- tive indices of both materials on either side of an interface. With this in mind, we note that the ray bends upward, or away from the normal, as
it enters the prism in Figure 26.19a. A ray bends away from the normal
26.5 The Dispersion of Light: Prisms and Rainbows 747
THE PHYSICS OF . . . rainbows. Another example of dispersion occurs in rainbows, in which refraction by water droplets gives rise to the colors. You can often see a rainbow just as
a storm is leaving, if you look at the departing rain with the sun at your back. When light from
the sun enters a spherical raindrop, as in Figure 26.20, light of each color is refracted or bent by an amount that depends on the refractive index of water for that wavelength. After refl ection
from the back surface of the droplet, the diff erent colors are again refracted as they reenter the
air. Although each droplet disperses the light into its full spectrum of colors, the observer in
Figure 26.21a sees only one color of light coming from any given droplet, since only one color travels in the right direction to reach the observer’s eyes. However, all colors are visible in a
rainbow (see Figure 26.21b) because each color originates from diff erent droplets at diff erent angles of elevation.
Water droplet
Sunlight
Violet
Red
FIGURE 26.20 When sunlight emerges from a water droplet, the light is dispersed
into its constituent colors, of which only two
are shown.
FIGURE 26.21 (a) The diff erent colors seen in a rainbow originate from water droplets at diff erent angles of elevation. (b) A rock climber beneath a rainbow.
Sun
Violet
Violet
Red
(a)
Red
Red
Violet
(b)
© A
C E
S T
O C
K L
IM IT
E D
/A la
m y
when it travels from a medium with a larger refractive index into a
medium with a smaller refractive index. When the ray leaves the prism,
it again bends upward, which is toward the normal at the point of exit.
A ray bends toward the normal when traveling from a smaller toward a
larger refractive index. Thus, the situation in Figure 26.19a could arise if the prism were immersed in a fl uid, such as carbon disulfi de, that has a larger refractive index than does glass (see Table 26.1).
We have seen in Figures 26.18a and 26.19a that a glass prism can bend a ray of light either downward or upward, depending on whether
the surrounding fl uid has a smaller or larger index of refraction than the
glass. It is logical to conclude, then, that a prism will not bend a ray at all, neither up nor down, if the surrounding fl uid has the same index of refraction as the glass—a condition known as index matching. This is exactly what is happening in Figure 26.19b, where the ray proceeds straight through the prism as if the prism were not even there. If the index
of refraction of the surrounding fl uid equals that of the glass prism, then
n1 = n2, and Snell’s law (n1 sin 𝜃1 = n2 sin 𝜃2) reduces to sin 𝜃1 = sin 𝜃2. Therefore, the angle of refraction equals the angle of incidence, and no
bending of the light occurs.
Related Homework: Check Your Understanding 16
(a)
(b)
FIGURE 26.19 A ray of light passes through identical prisms, each surrounded
by a diff erent fl uid. The ray of light is
(a) refracted upward and (b) not refracted at all.
748 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
Check Your Understanding
(The answers are given at the end of the book.) 13. Two blocks, made from the same transparent ma-
terial, are immersed in diff erent liquids. A ray of
light strikes each block at the same angle of inci-
dence. From CYU Figure 26.4, determine which liquid, A or B, has the greater index of refraction.
14. A beam of violet-colored light is propagating in crown glass. When the light reaches the bound-
ary between the glass and the surrounding air, the
beam is totally refl ected back into the glass. What
happens if the light is red and has the same angle of incidence 𝜃1 at the glass–air interface as does the violet-colored light? (a) Depending on the value for 𝜃1, red light may not be totally refl ected, and some of it may be refracted into the air. (b) No matter what the value for 𝜃1, the red light behaves exactly the same as the violet-colored light. (Hint: Refer to Table 26.2 and review Section 26.3.)
26.6 Lenses The lenses used in optical instruments, such as eyeglasses, cameras, and telescopes, are made
from transparent materials that refract light. They refract the light in such a way that an image
of the source of the light is formed. Figure 26.22a shows a crude lens formed from two glass prisms. Suppose that an object centered on the principal axis is infi nitely far from the lens so
the rays from the object are parallel to the principal axis. In passing through the prisms, these
rays are bent toward the axis because of refraction. Unfortunately, the rays do not all cross the
axis at the same place, and, therefore, such a crude lens gives rise to a blurred image of the
object.
A better lens can be constructed from a single piece of transparent material with properly
curved surfaces, often spherical, as in Figure 26.22b. With this improved lens, rays that are near the principal axis (paraxial rays) and parallel to it converge to a single point on the axis
after emerging from the lens. This point is called the focal point F of the lens. Thus, an object located infi nitely far away on the principal axis leads to an image at the focal point of the
lens. The distance between the focal point and the lens is the focal length f. In what follows, we assume the lens is so thin compared to f that it makes no diff erence whether f is measured between the focal point and either surface of the lens or the center of the lens. The type of lens
in Figure 26.22b is known as a converging lens because it causes incident parallel rays to converge at the focal point.
Another type of lens found in optical instruments is a diverging lens, which causes inci- dent parallel rays to diverge after exiting the lens. Two prisms can also be used to form a crude
diverging lens, as in Figure 26.23a. In a properly designed diverging lens, such as the one in part b of the picture, paraxial rays that are parallel to the principal axis appear to originate from a single point on the axis after passing through the lens. This point is the focal point F, and its distance f from the lens is the focal length. Again, we assume that the lens is thin compared to the focal length.
Liquid BLiquid A
CYU FIGURE 26.4
Converging lens
Principal axis
Principal axis F
f = focal length
(a) (b)
FIGURE 26.22 (a) These two prisms cause rays of light that are parallel to the principal axis to change direction and cross the axis at diff erent points. (b) With a converging lens, paraxial rays that are parallel to the principal axis converge to the focal point F after passing through the lens.
26.7 The Formation of Images by Lenses 749
Converging and diverging lenses come in a variety of shapes, as Figure 26.24 illustrates. Observe that converging lenses are thicker at the center than at the edges, whereas diverging
lenses are thinner at the center.
Check Your Understanding
(The answers are given at the end of the book.) 15. A beacon in a lighthouse is to produce a parallel beam of light. The beacon consists of a light source
and a converging lens. Should the light source be placed (a) between the focal point and the lens, (b) at the focal point of the lens, or (c) beyond the focal point? (Hint: Refer to Section 25.5 and review the principle of reversibility.)
16. Review Conceptual Example 8 as an aid in answering this question. Is it possible for a lens to behave as a converging lens when surrounded by air but to behave as a diverging lens when surrounded by another
medium?
26.7 The Formation of Images by Lenses
Ray Diagrams and Ray Tracing Each point on an object emits light rays in all directions, and when some of these rays pass
through a lens, they form an image. As with mirrors, the ray-tracing method can be used to
determine the location and size of the image. Lenses diff er from mirrors, however, in that light
can pass through a lens from left to right or from right to left. Therefore, when constructing ray
diagrams, begin by locating a focal point F on each side of the lens; each point lies on the princi- pal axis at the same distance f from the lens. The lens is assumed to be thin, in that its thickness is small compared with the focal length and the distances of the object and the image from the
lens. For convenience, it is also assumed that the object is located to the left of the lens and is
oriented perpendicular to the principal axis. There are three paraxial rays that leave a point on the
top of the object and are especially helpful in drawing ray diagrams. They are labeled 1, 2, and 3
in Figure 26.25. When tracing their paths, we use the following reasoning strategy.
Principal axis
Diverging lens
Principal axisF
f = focal length (b)(a)
FIGURE 26.23 (a) These two prisms cause parallel rays to diverge. (b) With a diverging lens, paraxial rays that are parallel to the principal axis appear to originate from the focal point F after passing through the lens.
Double convex
Convex meniscus
Plano- convex
Converging lenses
Double concave
Concave meniscus
Plano- concave
Diverging lenses
FIGURE 26.24 Converging and diverging lenses come in a variety of shapes.
750 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
REASONING STRATEGY Ray Tracing for Converging and Diverging Lenses
Converging Lens Diverging Lens
Ray 1 This ray initially travels parallel to the prin- cipal axis. In passing through a converging lens, the ray is refracted toward the axis and travels through the focal point on the right side of the lens, as Figure 26.25a shows.
This ray initially travels parallel to the prin- cipal axis. In passing through a diverging lens, the ray is refracted away from the axis, and appears to have originated from the focal point on the left of the lens. The dashed line in Figure 26.25d represents the apparent path of the ray.
Ray 2 This ray fi rst passes through the focal point on the left and then is refracted by the lens in such a way that it leaves traveling parallel to the axis, as in Figure 26.25b.
This ray leaves the object and moves toward the focal point on the right of the lens. Before reach- ing the focal point, however, the ray is refracted by the lens so as to exit parallel to the axis. See Figure 26.25e, where the dashed line indicates the ray’s path in the absence of the lens.
Ray 3* This ray travels directly through the center of the thin lens without any appreciable bend- ing, as in Figure 26.25c.
This ray travels directly through the cen- ter of the thin lens without any appreciable bending, as in Figure 26.25f.
*Ray 3 does not bend as it proceeds through the lens because the left and right surfaces of each type of lens are nearly parallel at the center. Thus, in either case, the lens behaves as a transparent slab. As Figure 26.6 shows, the rays incident on and exiting from a slab travel in the same direction with only a lateral displace- ment. If the lens is suffi ciently thin, the displacement is negligibly small.
Image Formation by a Converging Lens Figure 26.26a illustrates the formation of a real image by a converging lens. Here the object is located at a distance from the lens that is greater than twice the focal length (beyond the point
F
Object
Converging lenses
Diverging lenses
F
F
Object F
1
1
FF
2
(a)
(d) (e)
F
F
F
F
3
3
(c)
( f )
F F
2
(b)
FIGURE 26.25 The rays shown here are useful in determining the nature of the images formed by converging and diverging lenses.
F2FObject Object
F Real
image
1
3
2
(a) (b)
Image sensor
Real image
(inverted)
FIGURE 26.26 (a) When the object is placed to the left of the point labeled 2F, a real, inverted, and smaller image is formed.
(b) The arrangement in part a is like that used in a camera.
26.7 The Formation of Images by Lenses 751
labeled 2F). To locate the image, any two of the three special rays can be drawn from the tip of the object, although all three are shown in the drawing. The point on the right side of the lens
where these rays intersect locates the tip of the image. The ray diagram indicates that the image
is real, inverted, and smaller than the object. THE PHYSICS OF . . . a camera. This optical arrangement is similar to that used in a camera, where an image sensor* or a piece of fi lm records
the image (see Figure 26.26b). When the object is placed between 2F and F, as in Figure 26.27a, the image is still real and
inverted; however, the image is now larger than the object. THE PHYSICS OF . . . a slide or film projector. This optical system is used in a slide or fi lm projector in which a small piece of fi lm is the object and the enlarged image falls on a screen. However, to obtain an image that is
right-side up, the fi lm must be placed in the projector upside down.
When the object is located between the focal point and the lens, as in Figure 26.28, the rays diverge after leaving the lens. To a person viewing the diverging rays, they appear to come from
an image behind (to the left of) the lens. Because none of the rays actually come from the image,
it is a virtual image. The ray diagram shows that the virtual image is upright and enlarged. THE PHYSICS OF . . . a magnifying glass. A magnifying glass uses this arrangement, as can be seen in part b of the drawing.
Image Formation by a Diverging Lens We have seen that a converging lens can form a real image or a virtual image, depending on
where the object is located with respect to the lens. In contrast, regardless of the position of a real
object, a diverging lens always forms a virtual image that is on the same side of the lens as the
object and is upright and smaller relative to the object, as Figure 26.29 illustrates.
F
2F
Object
F Real
image
Bulb Object (upside down)
Projector
Screen
1
32
(a) (b)
Real image
FIGURE 26.27 (a) When the object is placed between 2F and F, the image is real, inverted, and larger than the object. (b) This arrangement is found in projectors.
*One type of image sensor used in today’s digital cameras utilizes a charge-coupled device (CCD). See Section 29.3 for
a discussion of CCDs.
OPQRSTUVWXYZ
1
3
FF
Object
Virtual image
(a)
(b)
EFGHI
Magnifying glass
FIGURE 26.28 (a) When an object is placed between the focal point F of a converging lens and the lens, an upright, enlarged, and virtual image is created. (b) Such an image is seen when looking through a magnifying glass.
752 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
ABC DEF
1
3
FF
Object Virtual image
(a)
(b)
ABC DEF
Diverging lens
FIGURE 26.29 (a) A diverging lens always forms a virtual image of a real object. The
image is upright and smaller relative to the
object. (b) The image seen through a diverging lens.
Check Your Understanding
(The answer is given at the end of the book.) 17. A converging lens is used to produce a real image, as in Figure 26.27a. A piece of black tape is then
placed over the upper half of the lens. Which one of the following statements is true concerning the
image that results with the tape in place? (a) The image is of the entire object, although its brightness is reduced since fewer rays produce it. (b) The image is of the object’s lower half only, but its brightness is not reduced. (c) The image is of the object’s upper half only, but its brightness is not reduced.
26.8 The Thin-Lens Equation and the Magnification Equation When an object is placed in front of a spherical mirror, we can determine the location, size, and
nature of its image by using the technique of ray tracing or the mirror and magnifi cation equa-
tions. Both options are based on the law of refl ection. The mirror and magnifi cation equations
relate the distances do and di of the object and image from the mirror to the focal length f and magnifi cation m. For an object placed in front of a lens, Snell’s law of refraction leads to the technique of ray tracing and to equations that are identical to the mirror and magnifi cation equa-
tions. Thus, mirrors work because of the refl ection of light, whereas lenses work because of the
refraction of light, a distinction between the two devices that is important to keep in mind.
The equations that result from applying Snell’s law to lenses are referred to as the thin-lens
equation and the magnifi cation equation:
Thin-lens equation 1
do +
1
di =
1
f (26.6)
Math Skills The thin-lens equation ( 1do + 1
d i =
1
f ) is sometimes thought to imply that d o + d i = f . To emphasize that the focal length f does not equal the object distance do plus the image distance di, we can solve the thin lens equation for f. First, we multiply the left side of the thin-lens equation by 1
in the form of d o d i d o d i
:
( d o d i d o d i)(
1
d o +
1
d i) = 1
f or ( 1d od i)(
d o d i d o
+ d od i d i ) =
1
f
Simplifying this result gives
( 1d o d i)( d o di d o
+ d o d i
d i ) = 1
f or
d i + d o d o d i
= 1
f Taking the reciprocal of both sides of the simplifi ed result shows that
( d i + d o
d o d i ) −1
= ( 1f ) −1
or d o d i
d i + d o = f
Clearly, it is not true that d o + d i = f . Do not make this mistake when solving problems.
1
26.8 The Thin-Lens Equation and the Magnification Equation 753
Magnifi cation equation
m = Image height
Object height =
h i h o
= − d i d o
(26.7)
Figure 26.30 defi nes the symbols in these expressions with the aid of a thin converging lens, but the expressions also apply to a diverging lens, if it is thin. The derivations of these equations are
presented at the end of this section.
Certain sign conventions accompany the use of the thin-lens and magnifi cation equations,
and the conventions are similar to those used with mirrors in Section 25.6. The issue of real
versus virtual images, however, is slightly diff erent with lenses than with mirrors. With a mirror,
a real image is formed on the same side of the mirror as the object (see Figure 25.18), in which case the image distance di is a positive number. With a lens, a positive value for di also means the image is real. However, starting with an actual object, a real image is formed on the side of
the lens opposite to the object (see Figure 26.30). The sign conventions listed in the following Reasoning Strategy apply to light rays traveling from left to right from a real object.
REASONING STRATEGY Summary of Sign Conventions for Lenses Focal length
f is + for a converging lens. f is − for a diverging lens.
Object distance do is + if the object is to the left of the lens (real object), as is usual. do is − if the object is to the right of the lens (virtual object).*
Image distance di is + for an image (real) formed to the right of the lens by a real object. di is − for an image (virtual) formed to the left of the lens by a real object.
Magnifi cation m is + for an image that is upright with respect to the object. m is − for an image that is inverted with respect to the object.
*This situation arises in systems containing more than one lens, where the image formed by the fi rst lens becomes the object for the second lens. In such a case, the object of the second lens may lie to the right of that lens, in which event do is assigned a negative value and the object is called a virtual object.
Examples 9 and 10 illustrate the use of the thin-lens and magnifi cation equations.
Fho
hi
Object Real
imageF
do
f
di
FIGURE 26.30 The drawing shows the focal length f, the object distance do, and the image distance di for a converging lens. The object and image heights are, respectively, ho and hi.
EXAMPLE 9 The Real Image Formed by a Camera Lens
A person 1.70 m tall is standing 2.50 m in front of a digital camera. The
camera uses a converging lens whose focal length is 0.0500 m. (a) Find the image distance (the distance between the lens and the image sensor)
and determine whether the image is real or virtual. (b) Find the magnifi - cation and the height of the image on the image sensor.
Reasoning This optical arrangement is similar to that in Figure 26.26a, where the object distance is greater than twice the focal length of the lens.
Therefore, we expect the image to be real, inverted, and smaller than the
object.
Solution (a) To fi nd the image distance di we use the thin-lens equation with do = 2.50 m and f = 0.0500 m:
1
d i =
1
f −
1
d o =
1
0.0500 m −
1
2.50 m = 19.6 m−1 or di = 0.0510 m
Since the image distance is a positive number, a real image is formed on
the image sensor.
(b) The magnifi cation follows from the magnifi cation equation:
m = − d i d o
= − 0.0510 m
2.50 m = −0.0204
The image is 0.0204 times as large as the object, and it is inverted since
m is negative. Since the object height is ho = 1.70 m, the image height is
hi = mho = (−0.0204)(1.70 m) = −0.0347 m
754 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
The thin-lens and magnifi cation equations can be derived by considering rays 1 and 3 in
Figure 26.31a. Ray 1 is shown separately in part b of the drawing, where the angle 𝜃 is the same in each of the two colored triangles. Thus, tan 𝜃 is the same for each triangle:
tan θ = h o f
= −h i
d i − f A minus sign has been inserted in the numerator of the ratio hi/(di − f ) for the following rea-
son. The angle 𝜃 in Figure 26.31b is assumed to be positive. Since the image is inverted relative to the object, the image height hi is a negative number. The insertion of the minus sign ensures that the term −hi/(di − f ), and hence tan 𝜃, is a positive quantity.
Ray 3 is shown separately in Figure 26.31c, where the two angles labeled 𝜃ʹ are the same. Therefore,
tan θ′ = h o d o
= −h i d i
A minus sign has been inserted in the numerator of the term hi/di for the same reason that a minus sign was inserted earlier—namely, to ensure that tan 𝜃ʹ is a positive quantity. The fi rst equation
EXAMPLE 10 The Virtual Image Formed by a Diverging Lens
An object is placed 7.10 cm to the left of a diverging lens whose focal
length is f = −5.08 cm (a diverging lens has a negative focal length). (a) Find the image distance and determine whether the image is real or virtual. (b) Obtain the magnifi cation. Reasoning This situation is similar to that in Figure 26.29a. The ray diagram shows that the image is virtual, erect, and smaller than the object.
Problem-Solving Insight In the thin-lens equation, the reciprocal of the image distance di is given by di−1 = f −1 − do−1, where f is the focal length and do is the object distance. After combining the reciprocals f −1 and do−1, do not forget to take the reciprocal of the result to fi nd di.
Solution (a) The thin-lens equation can be used to fi nd the image distance di:
1
d i =
1
f −
1
d o =
1
−5.08 cm −
1
7.10 cm
= −0.338 cm−1 or di = −2.96 cm
The image distance is negative, indicating that the image is virtual and
located to the left of the lens.
(b) Since di and do are known, the magnifi cation equation shows that
m = − di do
= − −2.96 cm
7.10 cm = 0.417
The image is upright (m is +) and smaller (m < 1) than the object.
Fho
hi Object
(a)
ImageF
f
dido
1
3
ho
hi
(c)
dido
3
ho ho
hi
(b)
f
di
1
θ ́ θ ́
θ θ
FIGURE 26.31 These ray diagrams are used for deriving the thin-lens and magnifi cation
equations.
26.9 Lenses in Combination 755
gives hi/ho = −(di − f )/f, while the second equation yields hi/ho = −di /do. Equating these two expressions for hi/ho and rearranging the result produces the thin-lens equation, 1/do + 1/di = 1/f. The magnifi cation equation follows directly from the equation hi/ho = −di /do, if we recognize that hi/ho is the magnifi cation m of the lens.
Check Your Understanding
(The answers are given at the end of the book.) 18. A spherical mirror and a lens are immersed in water. Compared to the way they work in air, which one
do you expect will be more aff ected by the water?
19. An object is located at a distance do in front of a lens. The lens has a focal length f and produces an upright image that is twice as tall as the object. What kind of lens is it, and what is the object distance?
Express your answer as a fraction or multiple of the focal length.
20. In an old movie a photographic fi lm negative is introduced as evidence in a trial. The negative shows an image of a house that no longer exists. The verdict depends on knowing exactly how far above the
ground a window ledge was (the object height ho). The distance between the ground and the ledge on the negative (the image height hi) can be measured. What additional information is needed to calculate ho? (a) Nothing else is needed. (b) Just the object distance do, which is the distance between the house and the camera lens. (c) Just the focal length f of the lens. (d) Both do and f are needed.
26.9 Lenses in Combination Many optical instruments, such as microscopes and telescopes, use a number of lenses together to
produce an image. Among other things, a multiple-lens system can produce an image that is magni-
fi ed more than is possible with a single lens. For instance, Figure 26.32a shows a two-lens system
Fe
Fo
Fo
Object
(a)
Lens 1 (Objective) First
image (real)
Lens 2 (Eyepiece)
Fe
Final image
(virtual)
Fe (c)
First image
Eyepiece
Fe
Final image
FoFo
Object
(b)
Objective First
image
fo do1 di1
61.0 mm
fe
do2
di2
FIGURE 26.32 (a) This two-lens system can be used as a compound microscope to
produce a virtual, enlarged, and inverted fi nal
image. (b) The objective forms the fi rst image and (c) the eyepiece forms the fi nal image.
756 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
used in a microscope. The fi rst lens, the lens closest to the object, is referred to as the objective. The second lens is known as the eyepiece (or ocular). The object is placed just outside the focal point Fo of the objective. The image formed by the objective—called the “fi rst image” in the drawing—is real, inverted, and enlarged compared to the object. This fi rst image then serves as the object for the
eyepiece. Since the fi rst image falls between the eyepiece and its focal point Fe, the eyepiece forms an enlarged, virtual, fi nal image, which is what the observer sees.
The location of the fi nal image in a multiple-lens system can be determined by applying the
thin-lens equation to each lens separately. The key point to remember in such situations is the
following:
Problem-Solving Insight The image produced by one lens serves as the object for the next lens.
The next example illustrates this point.
EXAMPLE 11 A Microscope—Two Lenses in Combination
The objective and eyepiece of the compound microscope in Figure 26.32 are both converging lenses and have focal lengths of fo = 15.0 mm and fe = 25.5 mm. A distance of 61.0 mm separates the lenses. The micro- scope is being used to examine an object placed do1 = 24.1 mm in front of the objective. Find the fi nal image distance.
Reasoning The thin-lens equation can be used to locate the fi nal image produced by the eyepiece. We know the focal length of the eyepiece,
but to determine the fi nal image distance from the thin-lens equation we
also need to know the object distance, which is not given. To obtain this
distance, we recall that the image produced by one lens (the objective) is
the object for the next lens (the eyepiece). We can use the thin-lens equa-
tion to locate the image produced by the objective, since the focal length
and the object distance for this lens are given. The location of this image
relative to the eyepiece will tell us the object distance for the eyepiece.
Solution The fi nal image distance relative to the eyepiece is di2, and we can determine it by using the thin-lens equation:
1
di2 =
1
fe −
1
do2
The focal length fe of the eyepiece is known, but to obtain a value for the object distance do2 we must locate the fi rst image produced by the objec- tive. The fi rst image distance di1 (see Figure 26.32b) can be determined using the thin-lens equation with do1 = 24.1 mm and fo = 15.0 mm.
1
d i1 =
1
fo −
1
do1 =
1
15.0 mm −
1
24.1 mm
= 0.0252 mm−1 or d i1 = 39.7 mm
The fi rst image now becomes the object for the eyepiece, as indicated
in Figure 26.32c. Since the distance between the lenses is 61.0 mm, the object distance for the eyepiece is do2 = 61.0 mm − di1 = 61.0 mm − 39.7 mm = 21.3 mm. Noting that the focal length of the eyepiece is fe = 25.5 mm, we can fi nd the fi nal image distance with the thin-lens equation:
1
d i2 =
1
fe −
1
do2 =
1
25.5 mm −
1
21.3 mm
= −0.0077 mm−1 or di2 = −130 mm
The fact that di2 is negative indicates that the fi nal image is virtual. It lies to the left of the eyepiece, as the drawing shows.
Problem-Solving Insight The overall magnifi cation m of a two-lens system is the product of the magnifi cations m1 and m2 of the individual lenses, or m = m1 × m2.
Suppose, for example, that the image of lens 1 is magnifi ed by a factor of 5 relative to the
original object, so that m1 = 5. As we know, the image of lens 1 serves as the object for lens 2. Suppose, in addition, that lens 2 magnifi es this object further by a factor of 8, so that m2 = 8. The fi nal image of the two-lens system, then, would be 5 × 8 = 40 times as large as the original object.
In other words, the overall magnifi cation is m = m1 × m2.
26.10 The Human Eye
Anatomy Without doubt, the human eye is the most remarkable of all optical devices. Interactive Figure 26.33 shows some of its main anatomical features. The eyeball is approximately spherical with a diameter of about 25 mm. Light enters the eye through a transparent membrane (the
Iris
Lens
Iris
Aqueous humor
Vitreous humor
Optic nerve
Suspensory ligament
Ciliary muscle
Retina
Cornea
INTERACTIVE FIGURE 26.33 A cross- sectional view of the human eye.
26.10 The Human Eye 757
cornea). This membrane covers a clear liquid region (the aqueous humor), behind which are a diaphragm (the iris), the lens, a region fi lled with a jelly-like substance (the vitreous humor), and, fi nally, the retina. The retina is the light-sensitive part of the eye, consisting of millions of struc- tures called rods and cones. When stimulated by light, these structures send electrical impulses via the optic nerve to the brain, which interprets the image detected by the retina.
The iris is the colored portion of the eye and controls the amount of light reaching the retina.
The iris acts as a controller because it is a muscular diaphragm with a variable opening at its
center, through which the light passes. The opening is called the pupil. The diameter of the pupil varies from about 2 to 7 mm, decreasing in bright light and increasing (dilating) in dim light.
Of prime importance to the operation of the eye is the fact that the lens is fl exible, and its
shape can be altered by the action of the ciliary muscle. The lens is connected to the ciliary mus- cle by the suspensory ligaments (see the drawing). We will see shortly how the shape-changing ability of the lens aff ects the focusing ability of the eye.
Optics BIO THE PHYSICS OF . . . the human eye. Optically, the eye and the camera are simi-
lar; both have a lens system and a diaphragm with a variable opening or aperture at its center.
Moreover, the retina of the eye and the image sensor in a camera serve similar functions, for both
record the image formed by the lens system. In the eye, the image formed on the retina is real,
inverted, and smaller than the object, just as it is in a camera. Although the image on the retina is
inverted, it is interpreted by the brain as being right-side up.
For clear vision, the eye must refract the incoming light rays, so as to form a sharp image on
the retina. In reaching the retina, the light travels through fi ve diff erent media, each with a diff er-
ent index of refraction n: air (n = 1.00), the cornea (n = 1.38), the aqueous humor (n = 1.33), the lens (n = 1.40, on the average), and the vitreous humor (n = 1.34). Each time light passes from one medium into another, it is refracted at the boundary. The greatest amount of refraction, about
70% or so, occurs at the air/cornea boundary. According to Snell’s law, the large refraction at this
interface occurs primarily because the refractive index of air (n = 1.00) is so diff erent from that of the cornea (n = 1.38). The refraction at all the other boundaries is relatively small because the indices of refraction on either side of these boundaries are nearly equal. The lens itself con-
tributes only about 20–25% of the total refraction, since the surrounding aqueous and vitreous
humors have indices of refraction that are nearly the same as that of the lens.
Even though the lens contributes only a quarter of the total refraction or less, its function
is an important one. The eye has a fi xed image distance; that is, the distance between the lens
and the retina is constant. Therefore, the only way that objects located at diff erent distances
can produce sharp images on the retina is for the focal length of the lens to be adjustable. It
is the ciliary muscle that adjusts the focal length. When the eye looks at a very distant object,
the ciliary muscle is not tensed. The lens has its least curvature and, consequently, its longest
focal length. Under this condition the eye is said to be “fully relaxed,” and the rays form a
sharp image on the retina, as in Figure 26.34a. When the object moves closer to the eye, the
Image on
retina
Close object
Distant object
(a)
(b)
Image on
retina
Relaxed lens
Tensed lens
FIGURE 26.34 (a) When fully relaxed, the lens of the eye has its longest focal length,
and an image of a very distant object is
formed on the retina. (b) When the ciliary muscle is tensed, the lens has a shorter focal
length. Consequently, an image of a closer
object is formed on the retina.
758 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
ciliary muscle tenses automatically, thereby increasing the curvature of the lens, shortening the
focal length, and permitting a sharp image to form again on the retina (Figure 26.34b). When a sharp image of an object is formed on the retina, we say the eye is “focused” on the object.
The process in which the lens changes its focal length to focus on objects at diff erent distances
is called accommodation. When you hold a book too close, the print is blurred because the lens cannot adjust enough
to bring the book into focus. The point nearest the eye at which an object can be placed and still
produce a sharp image on the retina is called the near point of the eye. The ciliary muscle is fully tensed when an object is placed at the near point. For people in their early twenties with normal
vision, the near point is located about 25 cm from the eye. It increases to about 50 cm at age 40
and to roughly 500 cm at age 60. Since most reading material is held at a distance of 25–45 cm
from the eye, older adults typically need eyeglasses to overcome the loss of accommodation. The
far point of the eye is the location of the farthest object on which the fully relaxed eye can focus. A person with normal eyesight can see objects very far away, such as the planets and stars, and
thus has a far point located nearly at infi nity.
Nearsightedness BIO THE PHYSICS OF . . . nearsightedness. A person who is nearsighted (myopic)
can focus on nearby objects but cannot clearly see objects far away. For such a person, the far
point of the eye is not at infi nity and may even be as close to the eye as three or four meters.
When a nearsighted eye tries to focus on a distant object, the eye is fully relaxed, like a normal
eye. However, the nearsighted eye has a focal length that is shorter than it should be, so rays from
the distant object form a sharp image in front of the retina, as Figure 26.35a shows, and blurred vision results.
The nearsighted eye can be corrected with glasses or contacts that use diverging lenses, as Figure 26.35b suggests. The rays from the object diverge after leaving the eyeglass lens. There- fore, when they are subsequently refracted toward the principal axis by the eye, a sharp image is
formed farther back and falls on the retina. Since the relaxed (but nearsighted) eye can focus on
Image formed in front of retina
Far point of nearsighted eye
Far point of nearsighted eye
Far point of nearsighted eye
Relaxed lens
Distant object
(a)
Image formed
on retina
Virtual image formed by
diverging lens
Diverging lensDistant
object
(b)
Distant object
(c)
FIGURE 26.35 (a) When a nearsighted person views a distant object, the image is formed in front of the retina. The result is blurred vision. (b) With a diverging lens in front of the eye, the image is moved onto the retina and clear vision results. (c) The diverging lens is designed to form a virtual image at the far point of the nearsighted eye.
26.10 The Human Eye 759
Farsightedness BIO THE PHYSICS OF . . . farsightedness. A farsighted (hyperopic) person can usu-
ally see distant objects clearly, but cannot focus on those nearby. Whereas the near point of a
young and normal eye is located about 25 cm from the eye, the near point of a farsighted eye may
be considerably farther away than that, perhaps as far as several hundred centimeters. When a far-
sighted eye tries to focus on a book held closer than the near point, it accommodates and shortens
its focal length as much as it can. However, even at its shortest, the focal length is longer than it
should be. Therefore, the light rays from the book would form a sharp image behind the retina if
they could do so, as Figure 26.36a suggests. In reality, no light passes through the retina, but a blurred image does form on it.
EXAMPLE 12 Eyeglasses for the Nearsighted Person
A nearsighted person has a far point located only 521 cm from the eye.
Assuming that eyeglasses are to be worn 2 cm in front of the eye, fi nd the
focal length needed for the diverging lenses of the glasses so the person
can see distant objects.
Reasoning In Figure 26.35c the far point is 521 cm away from the eye. Since the glasses are worn 2 cm from the eye, the far point is 519 cm to
the left of the diverging lens. The image distance, then, is −519 cm, the
negative sign indicating that the image is a virtual image formed to the
left of the lens. The object is assumed to be infi nitely far from the diverg-
ing lens. The thin-lens equation can be used to fi nd the focal length of the
eyeglasses. We expect the focal length to be negative, since the lens is a
diverging lens.
Problem-Solving Insight Eyeglasses are worn about 2 cm from the eyes. Be sure, if necessary, to take this 2 cm into account when determining the object and image distances (do and di) that are used in the thin-lens equation.
Solution With di = −519 cm and do = ∞, the focal length can be found as follows:
1
f =
1
do +
1
di =
1
∞ +
1
−519 cm or f = −519 cm (26.6)
The value for f is negative, as expected for a diverging lens.
Tensed lens
Object
Near point of farsighted eye
Near point of farsighted eye
Virtual image formed by
converging lens
Near point of farsighted eye
(a)
Sharp image behind retina
Sharp image
on retina
Converging lens
Object
(b)
Converging lens
Object
(c)
FIGURE 26.36 (a) When a farsighted person views an object located between the near
point and the eye, a sharp image would be
formed behind the retina if light could pass
through it. Only a blurred image forms on
the retina. (b) With a converging lens in front of the eye, the sharp image is moved onto
the retina and clear vision results. (c) The converging lens is designed to form a virtual
image at the near point of the farsighted eye.
an object at the eye’s far point—but not on objects farther away—the diverging lens is designed
to transform a very distant object into an image located at the far point. Figure 26.35c shows this transformation, and the next example illustrates how to determine the focal length of the diverg-
ing lens that accomplishes it.
760 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
The Refractive Power of a Lens—The Diopter The extent to which rays of light are refracted by a lens depends on its focal length. However,
optometrists who prescribe correctional lenses and opticians who make the lenses do not specify
the focal length directly in prescriptions. Instead, they use the concept of refractive power to describe the extent to which a lens refracts light:
Refractive power
of a lens (in diopters) =
1
f (in meters) (26.8)
The refractive power is measured in units of diopters. One diopter is 1 m−1. Equation 26.8 shows that a converging lens has a refractive power of 1 diopter if it focuses
parallel light rays to a focal point 1 m beyond the lens. If a lens refracts parallel rays even more
and converges them to a focal point only 0.25 m beyond the lens, the lens has four times more
refractive power, or 4 diopters. Since a converging lens has a positive focal length and a diverging
lens has a negative focal length, the refractive power of a converging lens is positive and that of a
diverging lens is negative. Thus, the eyeglasses in Example 12 would be described in an optom-
etrist’s prescription in the following way: Refractive power = 1/(−5.19 m) = −0.193 diopters.
The contact lenses in Example 13 would be described in a similar fashion: Refractive power =
1/(0.284 m) = 3.52 diopters.
Check Your Understanding
(The answers are given at the end of the book.) 21. Two people who wear glasses are camping. One is nearsighted, and the other is farsighted. Whose
glasses may be useful in starting a fi re by concentrating the sun’s rays into a small region at the focal
point of the lens used in the glasses?
22. Suppose that a person with a near point of 26 cm is standing in front of a plane mirror. How close can he stand to the mirror and still see himself in focus?
23. BIO To a swimmer under water, objects look blurred. However, goggles that keep the water away from the eyes allow the swimmer to see objects in sharp focus. Why?
24. When glasses use diverging lenses to correct for nearsightedness or converging lenses to correct for farsightedness, the eyes of the person wearing the glasses lie between the lenses and their focal points.
When you look at the eyes of this person, they do not appear to have their normal size. Which one of
EXAMPLE 13 Contact Lenses for the Farsighted Person
A farsighted person has a near point located 210 cm from the eyes. Obtain
the focal length of the converging lenses in a pair of contacts that can be
used to read a book held 25.0 cm from the eyes.
Reasoning A contact lens is placed directly against the eye. Thus, the object distance, which is the distance from the book to the lens, is 25.0 cm.
The lens forms an image of the book at the near point of the eye, so the
image distance is −210 cm. The minus sign indicates that the image is a
virtual image formed to the left of the lens, as in Figure 26.36c. The focal length can be obtained from the thin-lens equation.
Solution With do = 25.0 cm and di = −210 cm, the focal length can be determined from the thin-lens equation as follows:
1
f =
1
do +
1
di =
1
25.0 cm +
1
−210 cm = 0.0352 cm−1 or f = 28.4 cm
Figure 26.36b shows that farsightedness can be corrected by placing a converging lens in front of the eye. The lens refracts the light rays more toward the principal axis before they enter
the eye. Consequently, when the rays are refracted even more by the eye, they converge to form
an image on the retina. Part c of the fi gure illustrates what the eye sees when it looks through the converging lens. The lens is designed so that the eye perceives the light to be coming from a
virtual image located at the near point. Example 13 shows how the focal length of the converging
lens is determined to correct for farsightedness.
26.11 Angular Magnification and the Magnifying Glass 761
the following describes what you see? (a) The converging lenses make the eyes appear smaller, and the diverging lenses make the eyes appear larger. (b) The converging lenses make the eyes appear larger, and the diverging lenses make the eyes appear smaller. (c) Both types of lenses make the eyes appear larger. (d) Both types of lenses make the eyes appear smaller.
26.11 Angular Magnification and the Magnifying Glass If you hold a penny at arm’s length, the penny looks larger than the moon. The reason is that the
penny, being so close, forms a larger image on the retina of the eye than does the more distant
moon. The brain interprets the larger image of the penny as arising from a larger object. The size
of the image on the retina determines how large an object appears to be. However, the size of the
image on the retina is diffi cult to measure. Alternatively, the angle 𝜃 subtended by the image can be used as an indication of the image size. Figure 26.37 shows this alternative, which has the advantage that 𝜃 is also the angle subtended by the object and, hence, can be measured more easily. The angle 𝜃 is called the angular size of both the image and the object. The larger the angular size, the larger the image on the retina, and the larger the object appears to be.
According to Equation 8.1, the angle 𝜃 (measured in radians) is the length of the circular arc that is subtended by the angle divided by the radius of the arc, as Figure 26.38a indicates. Part b of the drawing shows the situation for an object of height ho viewed at a distance do from the eye. When 𝜃 is small, ho is approximately equal to the arc length and do is nearly equal to the radius, so that
θ ( in radians) = Angular size ≈ ho do
This approximation is good to within one percent for angles of 9° or smaller. In the next example
the angular size of a penny is compared with that of the moon.
FIGURE 26.37 The angle 𝜃 is the angular size of both the image and the object.
Object
θ
θ
(a)
Arc length
Radius
Arc length Radius
(in radians) = θ
θ
(b)
ho
ho
do
do (in radians) ≈ θ
θ
FIGURE 26.38 (a) The angle 𝜃, measured in radians, is the arc length divided by the
radius. (b) For small angles (less than 9°), 𝜃 in radians is approximately equal to ho/do, where ho and do are the object height and distance.
EXAMPLE 14 A Penny and the Moon
Compare the angular size of a penny (diameter = ho = 1.9 cm) held at arm’s length (do = 71 cm) with the angular size of the moon (diameter = ho = 3.5 × 106 m, and do = 3.9 × 108 m).
Reasoning The angular size 𝜃 of an object is given approximately by its height ho divided by its distance do from the eye, 𝜃 ≈ ho/do, provided that the angle involved is less than roughly 9°; this approximation applies
here. The “heights” of the penny and the moon are their diameters.
Solution The angular sizes of the penny and moon are
Penny θ ≈ h o d o
= 1.9 cm
71 cm = 0.027 rad (1.5°)
Moon θ ≈ h o d o
= 3.5 × 10 6 m
3.9 × 10 8 m = 0.0090 rad (0.52°)
The penny thus appears to be about three times as large as the moon.
An optical instrument, such as a magnifying glass, allows us to view small or distant objects
because it produces a larger image on the retina than would be possible otherwise. In other
words, an optical instrument magnifi es the angular size of the object. The angular magnifi cation (or magnifying power) M is the angular size 𝜃ʹ of the fi nal image produced by the instrument divided by a reference angular size 𝜃. The reference angular size is the angular size of the object when seen without the instrument.
Angular magnifi cation
M =
Angular size of
final image produced
by optical instrument
Reference angular size
of object seen without
optical instrument
= θ′ θ (26.9)
762 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
A magnifying glass is the simplest device that provides angular magnifi cation. In this
case, the reference angular size 𝜃 is chosen to be the angular size of the object when placed at the near point of the eye and seen without the magnifying glass. Since an object cannot be
brought closer than the near point and still produce a sharp image on the retina, 𝜃 represents the largest angular size obtainable without the magnifying glass. Figure 26.39a indicates that the reference angular size is 𝜃 ≈ ho/N, where N is the distance from the eye to the near point. To compute 𝜃ʹ, recall from Section 26.7 and Figure 26.28 that a magnifying glass is usually a single converging lens, with the object located between the focal point of the lens and the lens.
In this situation, Figure 26.39b indicates that the lens produces a virtual image that is enlarged and upright with respect to the object. Assuming that the eye is next to the magnifying glass,
the angular size 𝜃ʹ seen by the eye is 𝜃ʹ ≈ ho/do, where do is the object distance. The angular magnifi cation is
M = θ′ θ
≈ h o /d o h o /N
= N d o
According to the thin-lens equation, do is related to the image distance di and the focal length f of the lens by
1
d o =
1
f −
1
d i
Substituting this expression for 1/do into the previous expression for M leads to the following result:
Angular magnifi cation of a magnifying glass M =
θ′ θ
≈ (1f − 1
d i) N (26.10) Two special cases of this result are of interest, depending on whether the image is located
as close to the eye as possible or as far away as possible. To be seen clearly, the closest the
image can be relative to the eye is at the near point, or di = −N. The minus sign indicates that the image lies to the left of the lens and is virtual. In this event, Equation 26.10 becomes M ≈ (N/f) + 1. The farthest the image can be from the eye is at infi nity (di = −∞); this occurs when the object is placed at the focal point of the lens. When the image is at infi nity, Equation 26.10
simplifi es to M ≈ N/f. Clearly, the angular magnifi cation is greater when the image is at the near point of the eye rather than at infi nity. In either case, however, the greatest magnifi cation
is achieved by using a magnifying glass with the shortest possible focal length. Example 15
illustrates how to determine the angular magnifi cation of a magnifying glass that is used in
these two ways.
(b)
Virtual image
Magnifying glass
Object
F θ
(a)
ho
ho
do di
hi
N
Object
θ
′
FIGURE 26.39 (a) Without a magnifying glass, the largest angular size 𝜃 occurs when the object is placed at the near point, a distance
N from the eye. (b) A magnifying glass produces an enlarged, virtual image of an
object placed between the focal point F of the lens and the lens. The angular size of both the
image and the object is 𝜃ʹ.
EXAMPLE 15 Examining a Diamond with a Magnifying Glass
A jeweler, whose near point is 40.0 cm from his eye and whose far point is
at infi nity, is using a small magnifying glass (called a loupe) to examine a
diamond. The lens of the magnifying glass has a focal length of 5.00 cm,
and the image of the gem is −185 cm from the lens. The image distance
is negative because the image is virtual and is formed on the same side
of the lens as the object. (a) Determine the angular magnifi cation of the magnifying glass. (b) Where should the image be located so the jeweler’s eye is fully relaxed and has the least strain? What is the angular magnifi -
cation under this “least strain” condition?
Reasoning The angular magnifi cation of the magnifying glass can be determined from Equation 26.10. In part (a) the image distance is −185 cm.
In part (b) the ciliary muscle of the jeweler’s eye is fully relaxed, so
the image must be located infi nitely far from the eye, at its far point, as
Section 26.10 discusses.
Solution (a) With f = 5.00 cm, di = −185 cm, and N = 40.0 cm, the angular magnifi cation is
M = ( 1f − 1
di) N = ( 1
5.00 cm −
1
−185 cm) (40.0 cm) = 8.22 (b) With f = 5.00 cm, di = −∞, and N = 40.0 cm, the angular magni- fi cation is
M = (1f − 1
di) N = ( 1
5.00 cm −
1
−∞) (40.0 cm) = 8.00 Jewelers often prefer to minimize eyestrain when viewing objects, even
though it means a slight reduction in angular magnifi cation.
26.12 The Compound Microscope 763
Check Your Understanding
(The answers are given at the end of the book.) 25. A bird-watcher sees the following three raptors in the air at the distances indicated: a kestrel (wing
span = 0.58 m at a distance of 21 m), a bald eagle (wing span = 2.29 m at a distance of 95 m), and a
red-tailed hawk (wing span = 1.27 m at a distance of 41 m). Rank the raptors in descending order
(largest fi rst) according to the angular size seen by the bird-watcher.
26. Who benefi ts more from using a magnifying glass, a person whose near point is located at a distance away from the eyes of (a) 75 cm or (b) 25 cm?
27. A person who has a near point of 25.0 cm is looking with unaided eyes at an object that is located at the near point. The object has an angular size of 0.012 rad. Then, holding a magnifying glass (f = 10.0 cm) next to her eye, she views the image of this object, the image being located at her near point. What is
the angular size of the image?
26.12 The Compound Microscope THE PHYSICS OF . . . the compound microscope. To increase the angular magnifi cation beyond that possible with a magnifying glass, an additional converging lens can be included to
“premagnify” the object before the magnifying glass comes into play. The result is an optical
instrument known as the compound microscope (Figure 26.40). As discussed in Section 26.9, the magnifying glass is called the eyepiece, and the additional lens is called the objective.
The angular magnifi cation of the compound microscope is M = 𝜃ʹ/𝜃 (Equation 26.9), where 𝜃ʹ is the angular size of the fi nal image and 𝜃 is the reference angular size. As with the magnify- ing glass in Figure 26.39, the reference angular size is determined by the height ho of the object when the object is located at the near point of the unaided eye: 𝜃 ≈ ho/N, where N is the distance between the eye and the near point. Assuming that the object is placed just outside the focal point
Fo of the objective (see Figure 26.32a) and that the fi nal image is very far from the eyepiece (i.e., near infi nity; see Figure 26.32c), it can be shown that
Angular magnifi cation of a compound microscope
M ≈ − (L − fe )N
fo fe (L > fo + fe ) (26.11)
In Equation 26.11, fo and fe are, respectively, the focal lengths of the objective and the eyepiece. The angular magnifi cation is greatest when fo and fe are as small as possible (since they are in the denominator in Equation 26.11) and when the distance L between the lenses is as large as possible. Furthermore, L must be greater than the sum of fo and fe for this equation to be valid. Example 16 deals with the angular magnifi cation of a compound microscope.
Object
Objective
Eyepiece
FIGURE 26.40 A compound microscope.
EXAMPLE 16 The Angular Magnification of a Compound Microscope
The focal length of the objective of a compound microscope is fo = 0.40 cm, and the focal length of the eyepiece is fe = 3.0 cm. The two lenses are separated by a distance of L = 20.0 cm. A person with a near point distance of N = 25 cm is using the microscope. (a) Determine the angular magnifi cation of the microscope. (b) Compare the answer in part (a) with the largest angular magnifi cation obtainable by using the eyepiece alone
as a magnifying glass.
Reasoning The angular magnifi cation of the compound microscope can be obtained directly from Equation 26.11, since all the variables are
known. When the eyepiece is used alone as a magnifying glass, as in
Figure 26.39b, the largest angular magnifi cation occurs when the image seen through the eyepiece is as close as possible to the eye. The image in
this case is at the near point, and according to Equation 26.10, the angular
magnifi cation is M ≈ (N/fe) + 1.
Solution (a) The angular magnifi cation of the compound microscope is
M ≈ − (L − fe ) N
fo fe = −
(20.0 cm − 3.0 cm)(25 cm)
(0.40 cm)(3.0 cm) = −350
The minus sign indicates that the fi nal image is inverted relative to the
initial object.
(b) The maximum angular magnifi cation of the eyepiece by itself is
M ≈ N fe
+ 1 = 25 cm
3.0 cm + 1 = 9.3
The eff ect of the objective is to increase the angular magnifi cation of
the compound microscope by a factor of 350/9.3 = 38 compared to the
angular magnifi cation of a magnifying glass.
764 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
26.13 The Telescope THE PHYSICS OF . . . the telescope. A telescope is an instrument for magnifying distant objects, such as stars and planets. Like a microscope, a telescope consists of an objective and
an eyepiece (also called the ocular). When the objective is a lens, as is the case in this section,
the telescope is referred to as a refracting telescope, since lenses utilize the refraction of light.* Usually the object being viewed is far away, so the light rays entering the telescope are
nearly parallel, and the “fi rst image” is formed just beyond the focal point Fo of the objective, as Figure 26.41a illustrates. The fi rst image is real and inverted. Unlike the fi rst image in the com- pound microscope, however, this image is smaller than the object. If, as in part b of the drawing, the telescope is constructed so the fi rst image lies just inside the focal point Fe of the eyepiece, the eyepiece acts like a magnifying glass. It forms a fi nal image that is greatly enlarged, virtual, and
located near infi nity. This fi nal image can then be viewed with a fully relaxed eye.
The angular magnifi cation M of a telescope, like that of a magnifying glass or a microscope, is the angular size 𝜃ʹ subtended by the fi nal image of the telescope divided by the reference angular size 𝜃 of the object. For an astronomical object, such as a planet, it is convenient to use as a refer- ence the angular size of the object seen in the sky with the unaided eye. Since the object is far away,
the angular size seen by the unaided eye is nearly the same as the angle 𝜃 subtended at the objective of the telescope in Figure 26.41a. Moreover, 𝜃 is also the angle subtended by the fi rst image, so 𝜃 ≈ −hi/fo, where hi is the height of the fi rst image and fo is the focal length of the objective. A minus sign has been inserted into this equation because the fi rst image is inverted relative to the object and
the image height hi is a negative number. The insertion of the minus sign ensures that the term −hi/ fo, and hence 𝜃, is a positive quantity. To obtain an expression for 𝜃ʹ, we refer to Figure 26.41b and note that the fi rst image is located very near the focal point Fe of the eyepiece, which has a focal length fe. Therefore, 𝜃ʹ ≈ hi/fe. The angular magnifi cation of the telescope is approximately
Angular magnifi cation of an astronomical telescope M =
θ ′ θ
≈ h i / fe
−h i / fo ≈ −
fo fe
(26.12)
The angular magnifi cation is determined by the ratio of the focal length of the objective to the
focal length of the eyepiece. For large angular magnifi cations, the objective should have a long
focal length and the eyepiece a short one. Some of the design features of a telescope are the topic
of the next example.
EXAMPLE 17 The Angular Magnification of an Astronomical Telescope
A telescope similar to that in Figure 26.42 has the following specifi ca- tions: fo = 985 mm and fe = 5.00 mm. From these data, fi nd (a) the angular magnifi cation and (b) the approximate length of this telescope.
Reasoning The angular magnifi cation of the telescope follows directly from Equation 26.12, since the focal lengths of the objective and eyepiece
are known. We can fi nd the length of the telescope by noting that it is
*Another type of telescope utilizes a mirror instead of a lens for the objective and is called a refl ecting telescope.
Objective
Distant object
First image
Eyepiece
θ θ
fo
hi
Fo
L
′
First image
Final image
(near ∞)
θ hi Fe
fe
(a) (b)
FIGURE 26.41 (a) An astronomical telescope is used to view distant objects. (Note the “break” in the principal axis, between the object and the objective.) The objective produces a real, inverted fi rst image.
(b) The eyepiece magnifi es the fi rst image to produce the fi nal image near infi nity.
26.14 Lens Aberrations 765
Check Your Understanding
(The answers are given at the end of the book.) 28. In the construction of a telescope, one of two lenses is to be used as the objective and one as the eyepiece.
The focal lengths of the lenses are (a) 3 cm and (b) 45 cm. Which lens should be used as the objective? 29. Two refracting telescopes have identical eyepieces, although one telescope is twice as long as the other.
Which telescope has the greater angular magnifi cation?
30. A well-designed optical instrument is composed of two converging lenses separated by 14 cm. The focal lengths of the lenses are 0.60 and 4.5 cm. Is the instrument a microscope or a telescope?
31. It is often thought that virtual images are somehow less important than real images. To show that this is not true, identify which of the following instruments normally produce fi nal images that are virtual:
(a) a projector, (b) a camera, (c) a magnifying glass, (d) eyeglasses, (e) a compound microscope, and (f) an astronomical telescope.
26.14 Lens Aberrations Rather than forming a sharp image, a single lens typically forms an image that is slightly out of
focus. This lack of sharpness arises because the rays originating from a single point on the object
are not focused to a single point on the image. As a result, each point on the image becomes a small
blur. The lack of point-to-point correspondence between object and image is called an aberration. One common type of aberration is spherical aberration, and it occurs with converging and
diverging lenses made with spherical surfaces. Figure 26.43a shows how spherical aberration arises with a converging lens. Ideally, all rays traveling parallel to the principal axis are refracted
so they cross the axis at the same point after passing through the lens. However, rays far from
the principal axis are refracted more by the lens than are those closer in. Consequently, the outer
rays cross the axis closer to the lens than do the inner rays, so a lens with spherical aberration
does not have a unique focal point. Instead, as the drawing suggests, there is a location along the
principal axis where the light converges to the smallest cross-sectional area. This area is circular
and is known as the circle of least confusion. The circle of least confusion is where the most satisfactory image can be formed by the lens.
Spherical aberration can be reduced substantially by using a variable-aperture diaphragm to
allow only those rays close to the principal axis to pass through the lens. Figure 26.43b indicates that a reasonably sharp focal point can be achieved by this method, although less light now passes
through the lens. Lenses with parabolic surfaces are also used to reduce this type of aberration,
but they are diffi cult and expensive to make.
approximately equal to the distance L between the objective and eyepiece. Figure 26.41a shows that the fi rst image is located just beyond the focal point Fo of the objective. Figure 26.41b shows that the fi rst image is also just to the right of the focal point Fe of the eyepiece. These two focal points are, therefore, very close together, so the distance L is approxi- mately the sum of the two focal lengths: L ≈ fo + fe.
Solution (a) The angular magnifi cation is approximately
M ≈ − fo fe
= − 985 mm
5.00 mm = −197 (26.12)
(b) The approximate length of the telescope is
L ≈ fo + fe = 985 mm + 5.00 mm = 990 mm
FIGURE 26.42 An astronomical telescope
typically includes a
viewfi nder, which
is a separate small
telescope with low
magnifi cation and
serves as an aid in
locating the object.
Once the object has
been found, the viewer
uses the eyepiece to
obtain the full magnifi -
cation of the telescope.
Viewfinder
Eyepiece
D o rl
in g K
in d er
sl ey
/G et
ty I
m ag
es
(b)
F
Circle of least
confusion
Variable-aperture diaphragm
(a)
FIGURE 26.43 (a) In a converging lens, spherical aberration prevents light rays parallel
to the principal axis from converging to a
common point. (b) Spherical aberration can be reduced by allowing only rays near the
principal axis to pass through the lens. The
refracted rays now converge more nearly to a
single focal point F.
766 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
Chromatic aberration also causes blurred images. It arises because the index of refraction of the material from which the lens is made varies with wavelength. Section 26.5 discusses how
this variation leads to the phenomenon of dispersion, in which diff erent colors refract by diff erent
amounts. Figure 26.44a shows sunlight incident on a converging lens, in which the light spreads into its color spectrum because of dispersion. For clarity, however, the picture shows only the colors at the
opposite ends of the visible spectrum—red and violet. Violet is refracted more than red, so the violet
ray crosses the principal axis closer to the lens than does the red ray. Thus, the focal length of the lens
is shorter for violet than for red, with intermediate values of the focal length corresponding to the colors
in between. As a result of chromatic aberration, an undesirable color fringe surrounds the image.
Chromatic aberration can be greatly reduced by using a compound lens, such as the com-
bination of a converging lens and a diverging lens shown in Figure 26.44b. Each lens is made from a diff erent type of glass. With this lens combination the red and violet rays almost come
to a common focus and, thus, chromatic aberration is reduced. A lens combination designed to
reduce chromatic aberration is called an achromatic lens (from the Greek “achromatos,” meaning “without color”). All high-quality cameras use achromatic lenses.
Check Your Understanding
(The answer is given at the end of the book.) 32. Why does chromatic aberration occur in lenses but not in mirrors?
(b)
FV F
FR
Red Red
Sunlight Sunlight
Violet Violet
(a)
FIGURE 26.44 (a) Chromatic aberration arises when diff erent colors are focused at
diff erent points along the principal axis: FV = focal point for violet light, FR = focal point for red light. (b) A converging and a diverging lens in tandem can be designed to bring
diff erent colors more nearly to the same focal
point F.
EXAMPLE 18 BIO Through a Baby’s Eyes—Infant Vision
Healthy newborn babies have the ability to see shapes of objects and colors,
but they cannot see objects more than 8–15 inches away (Figure 26.45). They naturally prefer rounded objects with contrast (light and dark shades),
so it is not surprising they often fi xate on the faces of their parents. They
also have diminished visual acuity, or the ability of their eyes to resolve
objects in fi ne detail. This is in large part due to the smaller size of a baby’s
eye compared to an adult. The cornea-to-retina distance in a baby’s eye can
be 6–9 mm shorter than in an adult, which results in smaller retinal images.
The newborn’s pupil also grows with age. Assume that an infant and an
adult are both staring at a teddy bear that is located 35 cm from their eyes.
If the lens-to-retina distance in the adult and infant is 25 mm and 16 mm, re-
spectively, what is the ratio of the eff ective focal lengths of their eyes (fA/fI)?
Reasoning We can apply the thin-lens equation (Equation 26.6) twice— once for the adult, and once for the infant—to calculate the focal lengths
of the eyes and then take their ratio.
Solution Applying Equation 26.6 to the adult, we have: 1
fA =
1
do +
1
diA =
1
35 cm +
1
2.5 cm ⇒ fA = 2.33 cm.
Repeating this calculation for the infant, we fi nd:
1
fI =
1
do +
1
diI =
1
35 cm +
1
1.6 cm ⇒ fI = 1.53 cm.
We can now calculate the ratio of the two focal lengths:
( fA fI ) =
2.33 cm
1.53 cm = 1.52 .
The greater focal length in the adult eye is due in part to its larger
cornea.
FIGURE 26.45 The smaller structures of an
infant’s eyes result in less
visual acuity as compared
to an adult with normal
vision. However, the infant’s
vision improves dramatically
in just a few months.P u b li
cD o m
ai n P
ic tu
re s/
P ix
ab ay
Concept Summary 767
Concept Summary 26.1 The Index of Refraction The change in speed as a ray of light goes from one material to another causes the ray to deviate from its incident dir-
ection. This change in direction is called refraction. The index of refraction n of a material is the ratio of the speed c of light in a vacuum to the speed 𝜐 of light in the material, as shown in Equation 26.1. The values for n are greater than unity, because the speed of light in a material medium is less than it is
in a vacuum.
n = c υ
(26.1)
26.2 Snell’s Law and the Refraction of Light The refraction that occurs at the interface between two materials obeys Snell’s law of refraction. This
law states that (1) the refracted ray, the incident ray, and the normal to the
interface all lie in the same plane, and (2) the angle of refraction 𝜃2 is related to the angle of incidence 𝜃1 according to Equation 26.2, where n1 and n2 are the indices of refraction of the incident and refracting media, respectively.
The angles are measured relative to the normal.
n1 sin θ1 = n 2 sin θ 2 (26.2)
Because of refraction, a submerged object has an apparent depth that is
diff erent from its actual depth. If the observer is directly above (or below)
the object, the apparent depth (or height) dʹ is related to the actual depth (or height) d according to Equation 26.3, where n1 and n2 are the refractive indices of the materials (the media) in which the object and the observer,
respectively, are located.
d ′ = d ( n 2 n1 ) (26.3)
26.3 Total Internal Refl ection When light passes from a material with a larger refractive index n1 into a material with a smaller refractive index n2, the refracted ray is bent away from the normal. If the incident ray is at the crit-
ical angle 𝜃c, the angle of refraction is 90°. The critical angle is determined from Snell’s law and is given by Equation 26.4. When the angle of incidence
exceeds the critical angle, all the incident light is refl ected back into the ma-
terial from which it came, a phenomenon known as total internal refl ection.
sin θc = n2 n1 (n1 > n2) (26.4)
26.4 Polarization and the Refl ection and Refraction of Light When light is incident on a nonmetallic surface at the Brewster angle 𝜃B, the refl ec- ted light is completely polarized parallel to the surface. The Brewster angle
is given by Equation 26.5, where n1 and n2 are the refractive indices of the incident and refracting media, respectively. When light is incident at the
Brewster angle, the refl ected and refracted rays are perpendicular to each other.
tan θ B = n 2 n1
(26.5)
26.5 The Dispersion of Light: Prisms and Rainbows A glass prism can spread a beam of sunlight into a spectrum of colors because the index
of refraction of the glass depends on the wavelength of the light. Thus, a
prism bends the refracted rays corresponding to diff erent colors by diff er-
ent amounts. The spreading of light into its color components is known as
dispersion. The dispersion of light by water droplets in the air leads to the
formation of rainbows. A prism will not bend a light ray at all, neither up nor
down, if the surrounding fl uid has the same refractive index as the material
from which the prism is made, a condition known as index matching.
26.6 Lenses 26.7 The Formation of Images by Lenses Converging lenses and diverging lenses depend on the phenomenon of refraction in forming an
image. With a converging lens, paraxial rays that are parallel to the principal
axis are focused to a point on the axis by the lens. This point is called the
focal point of the lens, and its distance from the lens is the focal length f. Paraxial light rays that are parallel to the principal axis of a diverging lens
appear to originate from its focal point after passing through the lens. The
distance of this point from the lens is the focal length f. The image produced by a converging or a diverging lens can be located via a technique known as
ray tracing, which utilizes the three rays outlined in the Reasoning Strategy
given in Section 26.7.
The nature of the image formed by a converging lens depends on where
the object is situated relative to the lens. When the object is located at a
distance from the lens that is greater than twice the focal length, the image
is real, inverted, and smaller than the object. When the object is located at
a distance from the lens that is between the focal length and twice the focal
length, the image is real, inverted, and larger than the object. When the object
is located between the focal point and the lens, the image is virtual, upright,
and larger than the object.
Regardless of the position of a real object, a diverging lens always pro-
duces an image that is virtual, upright, and smaller than the object.
26.8 The Thin-Lens Equation and the Magnifi cation Equation The thin-lens equation (Equation 26.6) can be used with either converging or
diverging lenses that are thin, and it relates the object distance do, the image distance di, and the focal length f of the lens.
1
d o +
1
d i =
1
f (26.6)
The magnifi cation m of a lens is the ratio of the image height hi to the object height ho and is also related to do and di by the magnifi cation equation (Equation 26.7).
m = h i h o
= − d i d o
(26.7)
The algebraic sign conventions for the variables appearing in the thin-lens
and magnifi cation equations are summarized in the Reasoning Strategy given
in Section 26.8.
26.9 Lenses in Combination When two or more lenses are used in com- bination, the image produced by one lens serves as the object for the next lens.
26.10 The Human Eye In the human eye, a real, inverted image is formed on a light-sensitive surface, called the retina. Accommodation is the process
by which the focal length of the eye is automatically adjusted, so that objects
at diff erent distances produce sharp images on the retina. The near point of
the eye is the point nearest the eye at which an object can be placed and still
have a sharp image produced on the retina. The far point of the eye is the
location of the farthest object on which the fully relaxed eye can focus. For a
young and normal eye, the near point is located 25 cm from the eye, and the
far point is located at infi nity.
A nearsighted (myopic) eye is one that can focus on nearby objects, but
not on distant objects. Nearsightedness can be corrected with eyeglasses or
contacts made from diverging lenses. A farsighted (hyperopic) eye can see
distant objects clearly, but not objects close up. Farsightedness can be cor-
rected with converging lenses.
The refractive power of a lens is measured in diopters and is given by
Equation 26.8, where f is the focal length of the lens and must be expressed in meters. A converging lens has a positive refractive power, and a diverging
lens has a negative refractive power.
Refractive power (in diopters) = 1
f ( in meters) (26.8)
768 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
26.11 Angular Magnifi cation and the Magnifying Glass The angular size of an object is the angle that it subtends at the eye of the viewer. For
small angles, the angular size 𝜃 in radians is given approximately by Equa- tion 1, where ho is the height of the object and do is the object distance. The angular magnifi cation M of an optical instrument is the angular size 𝜃ʹ of the fi nal image produced by the instrument divided by the reference angular size 𝜃 of the object, which is that seen without the instrument (see Equation 26.9).
θ ( in radians) ≈ ho do
(1)
M = θ′ θ
(26.9)
A magnifying glass is usually a single converging lens that forms
an enlarged, upright, and virtual image of an object placed at the focal
point of the lens or between the focal point and the lens. For a magni-
fying glass held close to the eye, the angular magnifi cation M is given approximately by Equation 26.10, where f is the focal length of the lens, di is the image distance, and N is the distance of the viewer’s near point from the eye.
M ≈ (1f − 1
d i) N (26.10)
26.12 The Compound Microscope A compound microscope usually con- sists of two lenses, an objective and an eyepiece. The fi nal image is enlarged,
inverted, and virtual. The angular magnifi cation M of such a microscope is given approximately by Equation 26.11, where fo and fe are, respectively, the focal lengths of the objective and eyepiece, L is the distance between the two lenses, and N is the distance of the viewer’s near point from his or her eye.
M ≈ − (L − fe)N
fo fe (L > fo + fe ) (26.11)
26.13 The Telescope An astronomical telescope magnifi es distant objects with the aid of an objective and an eyepiece, and it produces a fi nal image
that is enlarged, inverted, and virtual. The angular magnifi cation M of a tele- scope is given approximately by Equation 26.12, where fo and fe are, respect- ively, the focal lengths of the objective and the eyepiece.
M ≈ − fo fe
(26.12)
26.14 Lens Aberrations Lens aberrations limit the formation of perfectly focused or sharp images by optical instruments. Spherical aberration occurs
because rays that pass through the outer edge of a lens with spherical surfaces
are not focused at the same point as rays that pass through near the center of
the lens. Chromatic aberration arises because a lens focuses diff erent colors
at slightly diff erent points.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 26.2 Snell’s Law and the Refraction of Light 1. The drawings show two examples in which a ray of light is refracted at the interface between two liquids. In each example the incident ray is in liquid
A and strikes the interface at the same angle of incidence. In one case the
ray is refracted into liquid B, and in the other it is refracted into liquid C.
The dashed lines denote the normals to the interfaces. Rank the indices of
refraction of the three liquids in descending order (largest fi rst). (a) nA, nB, nC (b) nA, nC, nB (c) nC, nA, nB (d) nB, nA, nC (e) nC, nB, nA
QUESTION 1
A
B
A
C
5. A coin is resting on the bottom of an empty container. The container is then fi lled to the brim three times, each time with a diff erent liquid. An ob-
server (in air) is directly above the coin and looks down at it. With liquid A
in the container, the apparent depth of the coin is 7 cm, with liquid B it is
6 cm, and with liquid C it is 5 cm. Rank the indices of refraction of the liquids
in descending order (largest fi rst). (a) nA, nB, nC (b) nA, nC, nB (c) nC, nA, nB (d) nC, nB, nA (e) nB, nA, nC
Section 26.3 Total Internal Reflection 6. The refractive index of material A is greater than the refractive index of material B. A ray of light is incident on the interface between these two
materials in a number of ways, as the drawings illustrate. The dashed lines
denote the normals to the interfaces. Which one of the drawings shows a
situation that is not possible? (a) Drawing 1 (b) Drawing 2 (c) Drawing 3 (d) Drawing 4
A
B
Drawing 1
A
B
Drawing 2
A
B
Drawing 3
A
B
Drawing 4
QUESTION 6
7. The drawing shows a rectangular block of glass (n = 1.52) surrounded by air. A ray of light starts out within the glass and travels to-
ward point A, where some or all of it is refl ected
toward point B. At which points does some of
the light escape the glass? (a) Only at point A (b) Only at point B (c) At both points A and B (d) At neither point A nor point B
Focus on Concepts
35°
B
A
QUESTION 7
Problems 769
Section 26.4 Polarization and the Reflection and Refraction of Light 8. A diamond (n = 2.42) is lying on a table. At what angle of incidence 𝜃 is the light that is refl ected from one of the facets of the diamond completely
polarized?
Section 26.5 The Dispersion of Light: Prisms and Rainbows 9. The indices of refraction for red, green, and violet light in glass are nred = 1.520, ngreen = 1.526, and nviolet = 1.538. When a ray of light passes through a transparent slab of glass, the emergent ray is parallel to the incident ray,
but can be displaced relative to it. For light passing through a glass slab that
is surrounded by air, which color is displaced the most? (a) All colors are displaced equally. (b) Red (c) Green (d) Violet
Section 26.7 The Formation of Images by Lenses 11. An object is situated to the left of a lens. A ray of light from the object is close to and parallel to the principal axis of the lens. The ray passes
through the lens. Which one of the following statements is true? (a) The ray crosses the principal axis at a distance from the lens equal to twice the
focal length, no matter whether the lens is converging or diverging. (b) The ray passes through the lens without changing direction, no matter whether
the lens is converging or diverging. (c) The ray passes through a focal point of the lens, no matter whether the lens is converging or diverging. (d) The ray passes through a focal point of the lens only if the lens is a diverging
lens. (e) The ray passes through a focal point of the lens only if the lens is a converging lens.
12. What type of single lens produces a virtual image that is inverted with respect to the object? (a) Both a converging and a diverging lens can produce such an image. (b) Neither a converging nor a diverging lens produces such an image. (c) A converging lens (d) A diverging lens
Section 26.9 Lenses in Combination 15. Two converging lenses have the same focal length of 5.00 cm. They have a common principal axis and are separated by 21.0 cm. An object is
located 10.0 cm to the left of the left-hand lens. What is the image distance
(relative to the lens on the right) of the fi nal image produced by this two-
lens system?
Section 26.10 The Human Eye 17. Here are a number of statements concerning the refractive power of lenses.
A. A positive refractive power means that a lens always creates an image that is larger than the object.
B. Two lenses with the same refractive power have the same focal lengths. C. A lens with a positive refractive power is a converging lens, whereas a lens with a negative refractive power is a diverging lens.
D. Two lenses with diff erent refractive powers can have the same focal length.
E. The fact that lens A has twice the refractive power of lens B means that the focal length of lens A is twice that of lens B.
Which of these statements are false? (a) A, B, C (b) C, D, E (c) A, D, E (d) B, C, E (e) B, C, D
Section 26.11 Angular Magnification and the Magnifying Glass 18. The table lists the angular sizes in radians and distances from the eye for three objects, A, B, and C. In each case the angular size is small.
Object Angular Size (in Radians)
Distance of Object from Eye
A 𝜃 do
B 2𝜃 2do
C 𝜃 2do
Rank the heights of these objects in descending order (largest fi rst). (a) B, C, A (b) B, A, C (c) A, B, C (d) A, C, B (e) C, A, B
Section 26.13 The Telescope 19. An astronomical telescope has an angular magnifi cation of –125 when used properly. What would the angular magnifi cation M be if the objective and the eyepiece were interchanged?
Section 26.14 Lens Aberrations 20. Which one of the fi ve choices below best completes the following state- ment? The fact that the refractive index depends on the wavelength of light is
the cause of __________. (a) dispersion (b) chromatic aberration (c) spher- ical aberration (d) dispersion and chromatic aberration (e) spherical aberra- tion and chromatic aberration
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details. Note: Unless specifi ed otherwise, use the values given in Table 26.1 for the refractive indices.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 26.1 The Index of Refraction 1. E SSM A plate glass window (n = 1.5) has a thickness of 4.0 × 10−3 m. How long does it take light to pass perpendicularly through the plate?
2. E In an ultra-low-temperature experiment, a collection of sodium atoms enter a special state called a Bose-Einstein condensate in which the index of refraction is 1.57 × 107. What is the speed of light in this
condensate?
3. E The refractive indices of materials A and B have a ratio of nA/nB = 1.33. The speed of light in material A is 1.25 × 108 m/s. What is the speed of light in material B?
Problems
770 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
4. E GO The frequency of a light wave is the same when the light travels in ethyl alcohol or in carbon disulfi de. Find the ratio of the wavelength of the
light in ethyl alcohol to that in carbon disulfi de.
5. E SSM Light travels at a speed of 2.201 × 108 m/s in a certain substance. What substance from Table 26.1 could this be? For the speed of light in a vacuum use 2.998 × 108 m/s; show your calculations.
6. E Light has a wavelength of 340.0 nm and a frequency of 5.403 × 1014 Hz when traveling through a certain substance. What substance from Table 26.1 could this be? Show your calculations.
7. M MMH In a certain time, light travels 6.20 km in a vacuum. During the same time, light travels only 3.40 km in a liquid. What is the refractive index
of the liquid?
8. M V-HINT A fl at sheet of ice has a thickness of 2.0 cm. It is on top of a fl at sheet of crystalline quartz that has a thickness of 1.1 cm. Light strikes
the ice perpendicularly and travels through it and then through the quartz. In
the time it takes the light to travel through the two sheets, how far (in centi-
meters) would it have traveled in a vacuum?
Section 26.2 Snell’s Law and the Refraction of Light 9. E GO The drawing shows four diff erent situations in which a light ray is traveling from one medium into another. In some of the cases, the refraction
is not shown correctly. For cases (a), (b), and (c), the angle of incidence is 55°; for case (d), the angle of incidence is 0°. Determine the angle of refrac- tion in each case. If the drawing shows the refraction incorrectly, explain why
it is incorrect.
PROBLEM 9
n1 = 1.4 n1 = 1.5
n2 = 1.6
n2 = 1.6
(a) (b)
n1 = 1.6
n1 = 1.6
n2 = 1.4
n2 = 1.4
(c)
(d)
10. E A layer of oil (n = 1.45) fl oats on an unknown liquid. A ray of light originates in the oil and passes into the unknown liquid. The angle of in-
cidence is 64.0°, and the angle of refraction is 53.0°. What is the index of
refraction of the unknown liquid?
11. E SSM A ray of light impinges from air onto a block of ice (n = 1.309) at a 60.0° angle of incidence. Assuming that this angle remains the same, fi nd
the diff erence 𝜃2, ice − 𝜃2, water in the angles of refraction when the ice turns to water (n = 1.333). 12. E A narrow beam of light from a laser travels through air (n = 1.00) and strikes point A on the surface of the water (n = 1.33) in a lake. The angle of incidence is 55°. The depth of the lake is 3.0 m. On the fl at lake-bottom
is point B, directly below point A. (a) If refraction did not occur, how far away from point B would the laser beam strike the lake-bottom? (b) Consid- ering refraction, how far away from point B would the laser beam strike the
lake-bottom?
13. E SSM The drawing shows a coin resting on the bottom of a beaker fi lled with an unknown liquid. A ray of light from the coin travels to the
surface of the liquid and is refracted as it enters into the air. A person sees
the ray as it skims just above the surface of the liquid. How fast is the light
traveling in the liquid?
PROBLEM 13 Coin
5.00 cm
6 .0
0 c
m
14. E Amber (n = 1.546) is a transparent brown-yellow fossil resin. An insect, trapped and preserved within the amber, appears to be 2.5 cm beneath
the surface when viewed directly from above. How far below the surface is
the insect actually located?
15. E SSM A beam of light is traveling in air and strikes a material. The angles of incidence and refraction are 63.0° and 47.0°, respectively. Obtain
the speed of light in the material.
16. E GO The drawing shows a ray of light traveling through three materials whose surfaces are parallel to each other. The refracted rays (but not the
refl ected rays) are shown as the light passes through each material. A ray of light
strikes the a–b interface at a 50.0° angle of incidence. The index of refraction of material a is na = 1.20. The angles of refraction in materials b and c are, respectively, 45.0° and 56.7°. Find the indices of refraction in these two media.
PROBLEM 16
a cb
17. E GO Light in a vacuum is incident on a transparent glass slab. The angle of incidence is 35.0°. The slab is then immersed in a pool of liquid.
When the angle of incidence for the light striking the slab is 20.3°, the angle
of refraction for the light entering the slab is the same as when the slab was
in a vacuum. What is the index of refraction of the liquid?
18. M V-HINT A stone held just beneath the surface of a swimming pool is released and sinks to the bottom at a constant speed of 0.48 m/s. What is the
apparent speed of the stone, as viewed from directly above by an observer
who is in air?
19. M SSM Review Conceptual Example 4 as background for this problem. A man in a boat is looking straight down at a fi sh in the water directly beneath
him. The fi sh is looking straight up at the man. They are equidistant from the
air–water interface. To the man, the fi sh appears to be 2.0 m beneath his eyes.
To the fi sh, how far above its eyes does the man appear to be?
20. M V-HINT The drawing shows a rectangular block of glass (n = 1.52) surrounded by liquid carbon disulfi de (n = 1.63). A ray of light is incident on the glass at point A with a 30.0° angle of incidence. At what angle of refrac-
tion does the ray leave the glass at point B?
PROBLEM 20
30.0° A
B
21. M SSM In Figure 26.6, suppose that the angle of incidence is 𝜃1 = 30.0°, the thickness of the glass pane is 6.00 mm, and the refractive index of the
glass is n2 = 1.52. Find the amount (in mm) by which the emergent ray is displaced relative to the incident ray.
Problems 771
22. M GO The back wall of a home aquarium is a mirror that is a distance of 40.0 cm away from the front wall. The walls of the tank are negligibly thin.
A fi sh, swimming midway between the front and back walls, is being viewed
by a person looking through the front wall. The index of refraction of air is
nair = 1.000 and that of water is nwater = 1.333. (a) Calculate the apparent dis- tance between the fi sh and the front wall. (b) Calculate the apparent distance between the image of the fi sh and the front wall.
23. M Refer to Figure 26.4b and assume the observer is nearly above the submerged object. For this situation, derive the expression for the apparent
depth: dʹ = d(n2/n1), Equation 26.3. (Hint: Use Snell’s law of refraction and the fact that the angles of incidence and refraction are small, so tan 𝜃 ≈ sin 𝜃.) 24. H Available in WileyPLUS. 25. H A small logo is embedded in a thick block of crown glass (n = 1.52), 3.20 cm beneath the top surface of the glass. The block is put under water,
so there is 1.50 cm of water above the top surface of the block. The logo is
viewed from directly above by an observer in air. How far beneath the top
surface of the water does the logo appear to be?
Section 26.3 Total Internal Reflection 26. E For the liquids in Table 26.1, determine the smallest critical angle for light that originates in one of them and travels toward the air–liquid interface.
27. E SSM A glass is half-full of water, with a layer of vegetable oil (n = 1.47) fl oating on top. A ray of light traveling downward through the oil is
incident on the water at an angle of 71.4°. Determine the critical angle for the
oil–water interface and decide whether the ray will penetrate into the water.
28. E A point source of light is submerged 2.2 m below the surface of a lake and emits rays in all directions. On the surface of the lake, directly above the
source, the area illuminated is a circle. What is the maximum radius that this
circle could have?
29. E MMH A ray of light is traveling in glass and strikes a glass–liquid interface. The angle of incidence is 58.0°, and the index of refraction of glass
is n = 1.50. (a) What must be the index of refraction of the liquid so that the direction of the light entering the liquid is not changed? (b) What is the largest index of refraction that the liquid can have, so that none of the light is
transmitted into the liquid and all of it is refl ected back into the glass?
30. E GO The drawing shows three layers of diff erent materials, with air above and below the layers. The interfaces between the layers are parallel.
The index of refraction of each layer is given in the drawing. Identical rays of
light are sent into the layers, and light zigzags through each layer, refl ecting
from the top and bottom surfaces. The index of refraction for air is nair = 1.00. For each layer, the ray of light has an angle of incidence of 75.0°. For the
cases in which total internal refection is possible from either the top or bot-
tom surface of a layer, determine the amount by which the angle of incidence
exceeds the critical angle.
PROBLEM 30
c n = 1.40
b n = 1.50
a n = 1.30
Air
Air
31. E The drawing shows a crown glass slab with a rectangular cross sec- tion. As illustrated, a laser beam strikes the upper surface at an angle of
60.0°. After refl ecting from the upper surface, the beam refl ects from the side
and bottom surfaces. (a) If the glass is surrounded by air, determine where part of the beam fi rst exits the glass, at point A, B, or C. (b) Repeat part (a), assuming that the glass is surrounded by water instead of air.
PROBLEM 31
60.0°
A
B
C
Crown glass
Las er b
eam
32. E GO The drawing shows three materials, a, b, and c. A ray of light strikes the a–b interface at an angle that just barely exceeds its critical angle of 40.0°. The refl ected ray then strikes the a–c interface at an angle of incidence that just barely exceeds its critical angle (which is not 40.0°). The
index of refraction of material a is na = 1.80. Find the indices of refraction for the two other materials.
PROBLEM 32 c
na = 1.80
b
a
40.0°
33. M CHALK SSM MMH Multiple-Concept Example 7 provides helpful background for this problem. The drawing shows a crystalline quartz slab
with a rectangular cross section. A ray of light strikes the slab at an incident
angle of 𝜃1 = 34°, enters the quartz, and travels to point P. This slab is sur- rounded by a fl uid with a refractive index n. What is the maximum value of n for which total internal refl ection occurs at point P?
PROBLEM 33
P
θ1
34. M V-HINT The drawing shows a ray of light traveling from point A to point B, a distance of 4.60 m in a material that has an index of refraction n1. At point B, the light encounters a diff erent substance whose index of refrac- tion is n2 = 1.63. The light strikes the interface at the critical angle of 𝜃c = 48.1°. How much time does it take for the light to travel from A to B?
PROBLEM 34
B
A
n2 = 1.63
n1 cθ
35. M GO A layer of liquid B fl oats on liquid A. A ray of light begins in liquid A and undergoes total internal refl ection at the interface between the liquids when the angle of incidence exceeds 36.5°. When liquid B is replaced with liquid C, total internal refl ection occurs for angles of incidence greater than 47.0°. Find the ratio nB/nC of the refractive indices of liquids B and C.
Section 26.4 Polarization and the Reflection and Refraction of Light 36. E For light that originates within a liquid and strikes the liquid–air in- terface, the critical angle is 39°. What is Brewster’s angle for this light?
772 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
37. E SSM Light is refl ected from a glass coff ee table. When the angle of incidence is 56.7°, the refl ected light is completely polarized parallel to the
surface of the glass. What is the index of refraction of the glass?
38. E V-HINT Light is incident from air onto the surface of a liquid. The angle of incidence is 53.0°, and the angle of refraction is 34.0°. At what angle
of incidence would the refl ected light be 100% polarized?
39. E SSM When light strikes the surface between two materials from above, the Brewster angle is 65.0°. What is the Brewster angle when the light
encounters the same surface from below?
40. E A laser is mounted in air, at a distance of 0.476 m above the edge of a large, horizontal pane of crown glass, as shown in the drawing. The laser
is aimed at the glass in such a way that the refl ected beam is 100% polarized.
Determine the distance d between the edge of the pane and the point at which the laser beam is refl ected.
PROBLEM 40
0.476 m
Laser
Glass paned
41. M Available in WileyPLUS. 42. M Available in WileyPLUS.
Section 26.5 The Dispersion of Light: Prisms and Rainbows 43. E A ray of sunlight is passing from diamond into crown glass; the angle of incidence is 35.00°. The indices of refraction for the blue and red
components of the ray are: blue (ndiamond = 2.444, ncrown glass = 1.531), and red (ndiamond = 2.410, ncrown glass = 1.520). Determine the angle between the refracted blue and red rays in the crown glass.
44. E Violet light and red light travel through air and strike a block of plastic at the same angle of incidence. The angle of refraction is 30.400°
for the violet light and 31.200° for the red light. The index of refraction for
violet light in plastic is greater than that for red light by 0.0400. Delaying any
rounding off of calculations until the very end, fi nd the index of refraction for
violet light in plastic.
45. E SSM A beam of sunlight encounters a plate of crown glass at a 45.00° angle of incidence. Using the data in Table 26.2, fi nd the angle between the violet ray and the red ray in the glass.
46. E Horizontal rays of red light (𝜆 = 660 nm, in vacuum) and violet light (𝜆 = 410 nm, in vacuum) are incident on the fl int-glass prism shown in
the drawing. The indices of refraction for the red and violet light are nred = 1.662 and nviolet = 1.698. The prism is surrounded by air. What is the angle of refraction for each ray as it emerges from the prism?
PROBLEM 46 90.0°
90°
25.0°
Red and violet light
47. M SSM This problem relates to Figure 26.18, which illustrates the dis- persion of light by a prism. The prism is made from glass, and its cross sec-
tion is an equilateral triangle. The indices of refraction for the red and violet
light are 1.662 and 1.698, respectively. The angle of incidence for both the
red and the violet light is 60.0°. Find the angles of refraction at which the red
and violet rays emerge into the air from the prism.
48. M V-HINT The drawing shows a horizontal ray of white light incident perpendicularly on the vertical face of a prism (crown glass). The light enters
the prism, and part of it undergoes refraction at the slanted face and emerges
into the surrounding material. The rest of it is totally internally refl ected and
exits through the horizontal base of the prism. The colors of light that emerge
from the slanted face may be chosen by altering the index of refraction of the
material surrounding the prism. Find the required index of refraction of the
surrounding material so that (a) only red light and (b) all colors except violet emerge from the slanted face. (See Table 26.2.)
PROBLEM 48
90.00°
45.00°
Section 26.6 Lenses, Section 26.7 The Formation of Images by Lenses, Section 26.8 The Thin-Lens Equation and the Magnification Equation (Note: When drawing ray diagrams, be sure that the object height ho is much smaller than the focal length f of the lens or mirror.) 49. E SSM An object is located 9.0 cm in front of a converging lens (f = 6.0 cm). Using an accurately drawn ray diagram, determine where the image
is located.
50. E The owner of a van installs a rear-window lens that has a focal length of −0.300 m. When the owner looks out through the lens at a person standing
directly behind the van, the person appears to be just 0.240 m from the back
of the van, and appears to be 0.34 m tall. (a) How far from the van is the person actually standing, and (b) how tall is the person? 51. E MMH A camera is supplied with two interchangeable lenses, whose focal lengths are 35.0 and 150.0 mm. A woman whose height is 1.60 m
stands 9.00 m in front of the camera. What is the height (including sign)
of her image on the image sensor, as produced by (a) the 35.0-mm lens and (b) the 150.0-mm lens? 52. E When a diverging lens is held 13.0 cm above a line of print, as in Figure 26.29, the image is 5.0 cm beneath the lens. (a) Is the image real or virtual? (b) What is the focal length of the lens? 53. E A slide projector has a converging lens whose focal length is 105.00 mm. (a) How far (in meters) from the lens must the screen be loc- ated if a slide is placed 108.00 mm from the lens? (b) If the slide measures 24.0 mm × 36.0 mm, what are the dimensions (in mm) of its image?
54. E (a) For a diverging lens (f = −20.0 cm), construct a ray diagram to scale and fi nd the image distance for an object that is 20.0 cm from the lens.
(b) Determine the magnifi cation of the lens from the diagram. 55. E GO A tourist takes a picture of a mountain 14 km away using a cam- era that has a lens with a focal length of 50 mm. She then takes a second
picture when she is only 5.0 km away. What is the ratio of the height of the
mountain’s image on the camera’s image sensor for the second picture to its
height on the image sensor for the fi rst picture?
56. E GO An object is placed to the left of a lens, and a real image is formed to the right of the lens. The image is inverted relative to the object and is one-
half the size of the object. The distance between the object and the image is
Problems 773
90.0 cm. (a) How far from the lens is the object? (b) What is the focal length of the lens?
57. E MMH A converging lens has a focal length of 88.00 cm. An object 13.0 cm tall is located 155.0 cm in front of this lens. (a) What is the image distance? (b) Is the image real or virtual? (c) What is the image height? Be sure to include the proper algebraic sign.
58. M CHALK MMH The distance between an object and its image formed by a diverging lens is 49.0 cm. The focal length of the lens is −233.0 cm. Find
(a) the image distance and (b) the object distance. 59. M SSM The moon’s diameter is 3.48 × 106 m, and its mean distance from the earth is 3.85 × 108 m. The moon is being photographed by a camera
whose lens has a focal length of 50.0 mm. (a) Find the diameter of the moon’s image on the slide fi lm. (b) When the slide is projected onto a screen that is 15.0 m from the lens of the projector ( f = 110.0 mm), what is the diameter of the moon’s image on the screen?
60. M When a converging lens is used in a camera (as in Figure 26.26b), the fi lm must be at a distance of 0.210 m from the lens to record an image of
an object that is 4.00 m from the lens. The same lens and fi lm are used in a
projector (see Figure 26.27b), with the screen 0.500 m from the lens. How far from the projector lens should the fi lm be placed?
61. M SSM An object is 18 cm in front of a diverging lens that has a focal length of −12 cm. How far in front of the lens should the object be placed so
that the size of its image is reduced by a factor of 2.0?
62. M V-HINT An object is placed in front of a converging lens in such a position that the lens (f = 12.0 cm) creates a real image located 21.0 cm from the lens. Then, with the object remaining in place, the lens is replaced with
another converging lens (f = 16.0 cm). A new, real image is formed. What is the image distance of this new image?
63. H A converging lens ( f = 25.0 cm) is used to project an image of an object onto a screen. The object and the screen are 125 cm apart, and between
them the lens can be placed at either of two locations. Find the two object
distances.
64. H Available in WileyPLUS.
Section 26.9 Lenses in Combination 65. E GO Two identical diverging lenses are separated by 16 cm. The focal length of each lens is −8.0 cm. An object is located 4.0 cm to the left of the
lens that is on the left. Determine the fi nal image distance relative to the lens
on the right.
66. E GO Two systems are formed from a converging lens and a diverging lens, as shown in parts a and b of the drawing. (The point labeled “Fconverging” is the focal point of the converging lens.) An object is placed inside the focal
point of lens 1 at a distance of 10.00 cm to the left of lens 1. The focal lengths
of the converging and diverging lenses are 15.00 and −20.0 cm, respectively.
The distance between the lenses is 50.0 cm. Determine the fi nal image dis-
tance for each system, measured with respect to lens 2.
Fconverging
Object
(a)
Object
Fconverging
(b)
Lens 1 Lens 2 Lens 1 Lens 2
PROBLEM 66
67. E CHALK Two converging lenses are separated by 24.00 cm. The focal length of each lens is 12.00 cm. An object is placed 36.00 cm to the left of
the lens that is on the left. Determine the fi nal image distance relative to the
lens on the right.
68. E GO A converging lens ( f1 = 24.0 cm) is located 56.0 cm to the left of a diverging lens (f2 = −28.0 cm). An object is placed to the left of the converging lens, and the fi nal image produced by the two-lens combination
lies 20.7 cm to the left of the diverging lens. How far is the object from the
converging lens?
69. E SSM A converging lens ( f = 12.0 cm) is located 30.0 cm to the left of a diverging lens ( f = −6.00 cm). A postage stamp is placed 36.0 cm to the left of the converging lens. (a) Locate the fi nal image of the stamp relative to the diverging lens. (b) Find the overall magnifi cation. (c) Is the fi nal image real or virtual? With respect to the original object, is the fi nal image (d) upright or inverted, and is it (e) larger or smaller? 70. E MMH A diverging lens ( f = −10.0 cm) is located 20.0 cm to the left of a converging lens ( f = 30.0 cm). A 3.00-cm-tall object stands to the left of the diverging lens, exactly at its focal point. (a) Determine the distance of the fi nal image relative to the converging lens. (b) What is the height of the fi nal image (including the proper algebraic sign)?
71. M SSM An object is placed 20.0 cm to the left of a diverging lens (f = −8.00 cm). A concave mirror (f = 12.0 cm) is placed 30.0 cm to the right of the lens. (a) Find the fi nal image distance, measured relative to the mirror. (b) Is the fi nal image real or virtual? (c) Is the fi nal image upright or inverted with respect to the original object?
72. M Two converging lenses (f1 = 9.00 cm and f2 = 6.00 cm) are separated by 18.0 cm. The lens on the left has the longer focal length. An object stands
12.0 cm to the left of the left-hand lens in the combination. (a) Locate the fi nal image relative to the lens on the right. (b) Obtain the overall magnifi ca- tion. (c) Is the fi nal image real or virtual? With respect to the original object, (d) is the fi nal image upright or inverted and (e) is it larger or smaller? 73. M V-HINT Visitors at a science museum are invited to sit in a chair to the right of a full-length diverging lens (f1 = −3.00 m) and observe a friend sitting in a second chair, 2.00 m to the left of the lens. The visitor then presses
a button and a converging lens (f2 = +4.00 m) rises from the fl oor to a posi- tion 1.60 m to the right of the diverging lens, allowing the visitor to view the
friend through both lenses at once. Find (a) the magnifi cation of the friend when viewed through the diverging lens only and (b) the overall magnifi ca- tion of the friend when viewed through both lenses. Be sure to include the
algebraic signs (+ or −) with your answers.
Section 26.10 The Human Eye 74. E BIO A student is reading material written on a blackboard. Her con- tact lenses have a refractive power of 57.50 diopters; the lens-to-retina dis-
tance is 1.750 cm. (a) How far (in meters) is the blackboard from her eyes? (b) If the material written on the blackboard is 5.00 cm high, what is the size of the image on her retina?
75. E BIO A nearsighted person cannot read a sign that is more than 5.2 m from his eyes. To deal with this problem, he wears contact lenses that do
not correct his vision completely, but do allow him to read signs located
up to distances of 12.0 m from his eyes. What is the focal length of the
contacts?
76. E BIO GO A woman can read the large print in a newspaper only when it is at a distance of 65 cm or more from her eyes. (a) Is she nearsighted (my- opic) or farsighted (hyperopic), and what kind of lens is used in her glasses
to correct her eyesight? (b) What should be the refractive power (in diopters) of her glasses (worn 2.0 cm from the eyes), so she can read the newspaper at
a distance of 25 cm from her eyes?
77. E BIO SSM Your friend has a near point of 138 cm, and she wears con- tact lenses that have a focal length of 35.1 cm. How close can she hold a
magazine and still read it clearly?
78. E BIO GO A farsighted woman breaks her current eyeglasses and is using an old pair whose refractive power is 1.660 diopters. Since these
774 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
eyeglasses do not completely correct her vision, she must hold a newspaper
42.00 cm from her eyes in order to read it. She wears the eyeglasses 2.00 cm
from her eyes. How far is her near point from her eyes?
79. E BIO SSM A person has far points of 5.0 m from the right eye and 6.5 m from the left eye. Write a prescription for the refractive power of each
corrective contact lens.
80. M BIO V-HINT A farsighted man uses eyeglasses with a refractive power of 3.80 diopters. Wearing the glasses 0.025 m from his eyes, he is able to read
books held no closer than 0.280 m from his eyes. He would like a prescrip-
tion for contact lenses to serve the same purpose. What is the correct contact
lens prescription, in diopters?
81. H BIO The far point of a nearsighted person is 6.0 m from her eyes, and she wears contacts that enable her to see distant objects clearly. A tree is 18.0 m
away and 2.0 m high. (a) When she looks through the contacts at the tree, what is its image distance? (b) How high is the image formed by the contacts? 82. H BIO The contacts worn by a farsighted person allow her to see ob- jects clearly that are as close as 25.0 cm, even though her uncorrected near
point is 79.0 cm from her eyes. When she is looking at a poster, the contacts
form an image of the poster at a distance of 217 cm from her eyes. (a) How far away is the poster actually located? (b) If the poster is 0.350 m tall, how tall is the image formed by the contacts?
Section 26.11 Angular Magnification and the Magnifying Glass 83. E SSM A jeweler whose near point is 72 cm from his eye uses a magnify- ing glass as in Figure 26.39b to examine a watch. The watch is held 4.0 cm from the magnifying glass. Find the angular magnifi cation of the magnifying glass.
84. E A spectator, seated in the left-fi eld stands, is watching a baseball player who is 1.9 m tall and is 75 m away. On a TV screen, located 3.0 m
from a person watching the game at home, the image of this same player is
0.12 m tall. Find the angular size of the player as seen by (a) the spectator watching the game live and (b) the TV viewer. (c) To whom does the player appear to be larger?
85. E An engraver uses a magnifying glass (f = 9.50 cm) to examine some work, as in Figure 26.39b. The image he sees is located 25.0 cm from his eye, which is his near point. (a) What is the distance between the work and the magnifying glass? (b) What is the angular magnifi cation of the magni- fying glass?
86. E GO The near point of a naked eye is 32 cm. When an object is placed at the near point and viewed by the naked eye, it has an angular size of 0.060
rad. A magnifying glass has a focal length of 16 cm, and is held next to the
eye. The enlarged image that is seen is located 64 cm from the magnifying
glass. Determine the angular size of the image.
87. E V-HINT An object has an angular size of 0.0150 rad when placed at the near point (21.0 cm) of an eye. When the eye views this object using a
magnifying glass, the largest possible angular size of the image is 0.0380 rad.
What is the focal length of the magnifying glass?
88. M V-HINT Available in WileyPLUS. 89. H SSM A farsighted person can read printing as close as 25.0 cm when she wears contacts that have a focal length of 45.4 cm. One day, she forgets
her contacts and uses a magnifying glass, as in Figure 26.39b. Its maximum angular magnifi cation is 7.50 for a young person with a normal near point of
25.0 cm. What is the maximum angular magnifi cation that the magnifying
glass can provide for her?
Section 26.12 The Compound Microscope 90. E A forensic pathologist is viewing heart muscle cells with a micro- scope that has two selectable objectives with refracting powers of 100 and
300 diopters. When he uses the 100-diopter objective, the image of a cell
subtends an angle of 3 × 10−3 rad with the eye. What angle is subtended when
he uses the 300-diopter objective?
91. E SSM A compound microscope has a barrel whose length is 16.0 cm and an eyepiece whose focal length is 1.4 cm. The viewer has a near point
located 25 cm from his eyes. What focal length must the objective have so
that the angular magnifi cation of the microscope will be −320?
92. E The distance between the lenses in a compound microscope is 18 cm. The focal length of the objective is 1.5 cm. If the microscope is
to provide an angular magnifi cation of −83 when used by a person with a
normal near point (25 cm from the eye), what must be the focal length of
the eyepiece?
93. E GO The near point of a naked eye is 25 cm. When placed at the near point and viewed by the naked eye, a tiny object would have an
angular size of 5.2 × 10−5 rad. When viewed through a compound micro-
scope, however, it has an angular size of −8.8 × 10−3 rad. (The minus sign
indicates that the image produced by the microscope is inverted.) The
objective of the microscope has a focal length of 2.6 cm, and the distance
between the objective and the eyepiece is 16 cm. Find the focal length of
the eyepiece.
94. M V-HINT Available in WileyPLUS. 95. M In a compound microscope, the focal length of the objective is 3.50 cm and that of the eyepiece is 6.50 cm. The distance between the lenses is
26.0 cm. (a) What is the angular magnifi cation of the microscope if the per- son using it has a near point of 35.0 cm? (b) If, as usual, the fi rst image lies just inside the focal point of the eyepiece (see Figure 26.32), how far is the object from the objective? (c) What is the magnifi cation (not the angular magnifi cation) of the objective?
Section 26.13 The Telescope 96. E An astronomical telescope has an angular magnifi cation of −132. Its objective has a refractive power of 1.50 diopters. What is the refractive power
of its eyepiece?
97. E SSM Mars subtends an angle of 8.0 × 10−5 rad at the unaided eye. An astronomical telescope has an eyepiece with a focal length of 0.032 m. When
Mars is viewed using this telescope, it subtends an angle of 2.8 × 10−3 rad.
Find the focal length of the telescope’s objective lens.
98. E GO A telescope has an objective with a refractive power of 1.25 diopters and an eyepiece with a refractive power of 250 diopters. What is the
angular magnifi cation of the telescope?
99. E SSM Available in WileyPLUS. 100. E An amateur astronomer decides to build a telescope from a dis- carded pair of eyeglasses. One of the lenses has a refractive power of 11
diopters, and the other has a refractive power of 1.3 diopters. (a) Which lens should be the objective? (b) How far apart should the lenses be separated? (c) What is the angular magnifi cation of the telescope? 101. M Available in WileyPLUS. 102. M GO The lengths of three telescopes are LA = 455 mm, LB = 615 mm, and LC = 824 mm. The focal length of the eyepiece for each telescope is 3.00 mm. Find the angular magnifi cation of each telescope.
103. M V-HINT Available in WileyPLUS. 104. H An astronomical telescope is being used to examine a relatively close object that is only 114.00 m away from the objective of the telescope.
The objective and eyepiece have focal lengths of 1.500 and 0.070 m, respect-
ively. Noting that the expression M ≈ −fo/fe is no longer applicable because the object is so close, use the thin-lens and magnifi cation equations to fi nd
the angular magnifi cation of this telescope. (Hint: See Figure 26.41 and note that the focal points Fo and Fe are so close together that the distance between them may be ignored.)
Concepts and Calculations Problems 775
105. E SSM An object is located 30.0 cm to the left of a converging lens whose focal length is 50.0 cm. (a) Draw a ray diagram to scale and from it determine the image distance and the magnifi cation. (b) Use the thin-lens and magnifi cation equations to verify your answers to part (a).
106. E Available in WileyPLUS. 107. E SSM MMH A glass block (n = 1.56) is immersed in a liquid. A ray of light within the glass hits a glass–liquid surface at a 75.0° angle of incidence.
Some of the light enters the liquid. What is the smallest possible refractive
index for the liquid?
108. E As an aid in understanding this problem, refer to Conceptual Example 4. A swimmer, who is looking up from under the water, sees a
diving board directly above at an apparent height of 4.0 m above the water.
What is the actual height of the diving board above the water?
109. E BIO SSM Available in WileyPLUS. 110. E Available in WileyPLUS. 111. E BIO SSM Available in WileyPLUS. 112. E A camper is trying to start a fi re by focusing sunlight onto a piece of paper. The diameter of the sun is 1.39 × 109 m, and its mean distance from
the earth is 1.50 × 1011 m. The camper is using a converging lens whose
focal length is 10.0 cm. (a) What is the area of the sun’s image on the paper? (b) If 0.530 W of sunlight passes through the lens, what is the intensity of the sunlight at the paper?
113. E SSM Available in WileyPLUS. 114. E Available in WileyPLUS. 115. E BIO MMH Available in WileyPLUS. 116. E GO Red light (n = 1.520) and violet light (n = 1.538) traveling in air are incident on a slab of crown glass. Both colors enter the glass at the same
angle of refraction. The red light has an angle of incidence of 30.00°. What
is the angle of incidence of the violet light?
117. E A converging lens ( f = 12.0 cm) is held 8.00 cm in front of a news- paper that has a print size with a height of 2.00 mm. Find (a) the image dis- tance (in cm) and (b) the height (in mm) of the magnifi ed print.
118. E GO To focus a camera on objects at diff erent distances, the conver- ging lens is moved toward or away from the image sensor, so a sharp image
always falls on the sensor. A camera with a telephoto lens ( f = 200.0 mm) is to be focused on an object located fi rst at a distance of 3.5 m and then at
50.0 m. Over what distance must the lens be movable?
119. E SSM An offi ce copier uses a lens to place an image of a document onto a rotating drum. The copy is made from this image. (a) What kind of lens is used, converging or diverging? If the document and its copy are to
have the same size, but are inverted with respect to one another, (b) how far from the document is the lens located and (c) how far from the lens is the im- age located? Express your answers in terms of the focal length f of the lens. 120. M Available in WileyPLUS. 121. M BIO SSM At age forty, a man requires contact lenses ( f = 65.0 cm) to read a book held 25.0 cm from his eyes. At age forty-fi ve, while wearing
these contacts he must now hold a book 29.0 cm from his eyes. (a) By what distance has his near point changed? (b) What focal-length lenses does he require at age forty-fi ve to read a book at 25.0 cm?
122. M V-HINT An object is in front of a converging lens ( f = 0.30 m). The magnifi cation of the lens is m = 4.0. (a) Relative to the lens, in what direction should the object be moved so that the magnifi cation changes to m = −4.0? (b) Through what distance should the object be moved? 123. H SSM The angular magnifi cation of a telescope is 32 800 times as large when you look through the correct end of the telescope as when
you look through the wrong end. What is the angular magnifi cation of the
telescope?
124. H Available in WileyPLUS. 125. H BIO Bill is farsighted and has a near point located 125 cm from his eyes. Anne is also farsighted, but her near point is 75.0 cm from her
eyes. Both have glasses that correct their vision to a normal near point
(25.0 cm from the eyes), and both wear the glasses 2.0 cm from the eyes.
Relative to the eyes, what is the closest object that can be seen clearly (a) by Anne when she wears Bill’s glasses and (b) by Bill when he wears Anne’s glasses?
Additional Problems
One important phenomenon discussed in this chapter is how a ray of light
is refracted when it goes from one medium into another. Problem 126 re-
views some of the important aspects of refraction, including Snell’s law, the
concept of a critical angle, and the notion of index matching. One of the most
important applications of refraction is in lenses, the behaviors of which are
governed by the thin-lens and magnifi cation equations. Problem 127 reviews
how these equations are applied to a two-lens system, along with the all-
important sign conventions that must be followed.
126. M CHALK A ray of light is incident on a glass–water interface at the crit- ical angle 𝜃c as the fi gure illustrates. The refl ected light then passes through a liquid (immiscible with water) and into air. The indices of refraction for
the four substances are given in the drawing. Concepts: (i) What determines the critical angle when the ray strikes the glass–water interface? (ii) When
the light is incident at the glass–water interface at the critical angle, what is
the angle of refraction, and how is the angle 𝜃1 related to the critical angle?
(iii) When the refl ected ray strikes the glass–liquid interface, how is the angle
of refraction 𝜃3 related to the angle of incidence 𝜃2? Note that the two mater- ials have the same indices of refraction. (iv) When the ray passes from the
liquid into the air, is the ray refracted? Explain. Calculation: Determine the angle of refraction 𝜃5 for the ray as it passes into the air.
PROBLEM 126
n = 1.33 Water
n = 1.00 Aircθ 1θ
2θ
3θ 4θ
5θ
n = 1.52 Liquid
n = 1.52 Glass
Concepts and Calculations Problems
776 CHAPTER 26 The Refraction of Light: Lenses and Optical Instruments
lens when its object is a virtual object? Calculation: What are (a) the image distance di1 and (b) the height hi1 of the image produced by the fi rst lens? (c) What is the object distance for the second (diverging) lens? Find (d) the im- age distance di2 and (e) the height hi2 of the image produced by the second lens.
PROBLEM 127 do1
ho1
di1
hi1
10.0 cm
#1 #2Object First image
127. M CHALK SSM In the fi gure, a converging lens ( f1 = +20.0 cm) and a diverging lens ( f2 = −15.0 cm) are separated by a distance of 10.0 cm. An object with a height of ho1 = 5.00 mm is placed at a distance of do1 = 45.0 cm to the left of the fi rst (converging) lens. Concepts: (i) Is the image produced by the fi rst (converging) lens real or virtual? (ii) As far as the second lens is con-
cerned, what role does the image produced by the fi rst lens play? (iii) Note in
the fi gure that the image produced by the fi rst lens is called the “fi rst image,”
and it falls to the right of the second lens. This image acts as the object for
the second lens. Normally, however, an object would lie to the left of the lens.
How do we take into account that this object lies to the right of the diverging
lens? (iv) How do we fi nd the location of the image produced by the second
128. M An Optical Spectrometer. You and your team are tasked with characterizing an equilateral, triangular prism to be used in an optical spec-
trometer. An optical spectrometer contains a dispersive element (in this
case, the prism) that separates an incoming beam of light into its constitu-
ent wavelengths (or colors), and a photocell that measures the intensity of
each color (wavelength) by measuring the intensity of the dispersed light as a
function of angle. The index of refraction of the prism material you are using
depends on the wavelength as
n(λ) = −(1.080 × 10−4 nm−1) λ (nm) + 1.586
PROBLEM 128
Normal
Red (660 nm)
Violet (410 nm)
θ
An incident beam of white light impinges on the surface (see drawing) at
an angle of 45.0 degrees below the normal. The prism is in air (n = 1.000). Relative to the prism base (i.e., the horizontal in the drawing), at what angles
do (a) red light (𝜆 = 660.0 nm) and (b) violet light (𝜆 = 410.0 nm) emerge on the opposite side? (c) What is the angular range of the full spectrum, from red to violet?
129. M Emergency Replacement Glasses. One of your team members lost her glasses in a river. She is nearsighted and cannot see long distances
without them. You are on an expedition to map a remote area in southern
Argentina, and her long-distance vision is crucial to her role in the group.
You can request a new pair of glasses for her that will be delivered with
the next airdrop of supplies, but she does not know her lens prescription.
(a) Does she need a converging or diverging lens? (b) You do a simple eye test and estimate her far point to be 623.0 cm from her eyes. Assuming she
will wear her glasses 2.0 cm in front of her eyes, what should be the focal
length of her new lenses? (c) What should be the refractive power of her new lenses (in diopters)?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
27.1 Apply the principle of linear superposition to light waves.
27.2 Analyze double-slit interference.
27.3 Analyze thin-film interference.
27.4 Understand the operation of the Michelson interferometer.
27.5 Analyze single-slit diff raction.
27.6 Determine the resolving power of lenses.
27.7 Apply interference principles to the diff raction grating.
27.8 Analyze the role of interference in reading compact discs (CDs) and digital video discs (DVDs).
27.9 Describe X-ray diff raction in crystals. H
ei n ri
ch v
an d
en B
er g /G
al lo
I m
ag es
/G et
ty I
m ag
es
CHAPTER 27
Interference and the Wave Nature of Light
Wave interference occurs when two or more waves exist simultaneously at the same place. Light is an
electromagnetic wave and, therefore, can exhibit interference eff ects. The interference of light waves is
responsible for the lovely iridescent colors of the feathers on this purple-crested turaco from South Africa.
27.1 The Principle of Linear Superposition Chapter 17 examines what happens when several sound waves are present at the same
place at the same time. The pressure disturbance that results is governed by the princi- ple of linear superposition, which states that the resultant disturbance is the sum of the disturbances from the individual waves. Light is also a wave, an electromagnetic wave, and it too obeys the superposition principle. When two or more light waves pass
through a given point, their electric fi elds combine according to the principle of linear
superposition and produce a resultant electric fi eld. According to Equation 24.5b, the
square of the electric fi eld strength is proportional to the intensity of the light, which,
in turn, is related to its brightness. Thus, interference can and does alter the brightness
of light, just as it aff ects the loudness of sound.
Interactive Figure 27.1 illustrates what happens when two identical waves (same wavelength 𝜆 and same amplitude) arrive at the point P in phase—that is, crest-to-crest and trough-to-trough. According to the principle of linear superposition, the waves
reinforce each other and constructive interference occurs. The resulting total wave at P has an amplitude that is twice the amplitude of either individual wave, and, in the case of light waves, the brightness at P is greater than that due to either wave alone.
777
778 CHAPTER 27 Interference and the Wave Nature of Light
The waves start out in phase and are in phase at P because the distances ℓ1 and ℓ2 between this spot and the sources of the waves diff er by one wavelength 𝜆. In Interactive Figure 27.1, these distances are ℓ1 = 2
1
4 wavelengths and ℓ2 = 3 1
4 wavelengths. In general, when the waves start out
in phase, constructive interference will result at P whenever the distances are the same or diff er by any integer number of wavelengths—in other words, assuming that ℓ2 is the larger distance,
whenever ℓ2 − ℓ1 = m𝜆, where m = 0, 1, 2, 3, . . . . Interactive Figure 27.2 shows what occurs when two identical waves arrive at the point P
out of phase with one another, or crest-to-trough. Now the waves mutually cancel, according to
the principle of linear superposition, and destructive interference results. With light waves this would mean that there is no brightness. The waves begin with the same phase but are out of phase
at P because the distances through which they travel in reaching this spot diff er by one-half of a wavelength (ℓ1 = 2
3
4λ and ℓ2 = 3 1
4λ in the drawing). In general, for waves that start out in phase, destructive interference will take place at P whenever the distances diff er by any odd integer number of half-wavelengths—that is, whenever ℓ2 − ℓ1 =
1
2λ , 3
2λ, 5
2λ, . . . , where ℓ2 is the larger distance. This is equivalent to ℓ2 − ℓ1 = (m +
1
2 )λ, where m = 0, 1, 2, 3, . . . . Examples illustrating the application of the principle of linear superposition to explain the
interference of light waves can be found throughout this chapter. For relatively straightforward
examples that deal with two sources of sound waves and the resulting constructive or destructive
interference, see Examples 1 and 2 in Chapter 17 and Example 11 in this chapter.
If constructive or destructive interference is to continue occurring at a point, the sources of
the waves must be coherent sources. Two sources are coherent if the waves they emit maintain a
INTERACTIVE FIGURE 27.1 The waves emitted by source 1 and source 2 start out in
phase and arrive at point P in phase, leading to constructive interference at that point.
Constructive interference
Source 1
Source 2
Source 1
Source 2
P
+ =
1 = 2 4 1–
2 = 3 4 1–𝜆
𝜆
Destructive interference
Source 1
Source 2
Source 1
+ =
1 = 2 4 3–
2 = 3 4 1–
P
Source 2
𝜆
𝜆
INTERACTIVE FIGURE 27.2 The waves emitted by the two sources have the same phase
to begin with, but they arrive at point P out of phase. As a result, destructive interference
occurs at P.
27.2 Young’s Double-Slit Experiment 779
constant phase relation. Eff ectively, this means that the waves do not shift relative to one another
as time passes. For instance, suppose that the wave pattern of source 1 in Interactive Figure 27.2 shifted forward or backward by random amounts at random moments. Then, on average, neither
constructive nor destructive interference would be observed at point P because there would be no stable relation between the two wave patterns. Lasers are coherent sources of light, whereas
incandescent light bulbs and fl uorescent lamps are incoherent sources.
Check Your Understanding
(The answers are given at the end of the book.) 1. Two separate coherent sources produce waves whose wavelengths are 0.10 m. The two waves spread
out and overlap at a certain point. Does constructive or destructive interference occur at this point when
(a) one wave travels 3.20 m and the other travels 3.00 m, (b) one wave travels 3.20 m and the other travels 3.05 m, (c) one wave travels 3.20 m and the other travels 2.95 m?
2. Suppose that a radio station broadcasts simultaneously from two transmitting antennas at two diff erent locations. Compared with only one transmitting antenna, the reception with two transmitting antennas (a) is always better (b) is always worse (c) can be either better or worse, depending on the distance traveled by each wave.
3. Two sources of waves are in phase and produce identical waves. These sources are mounted at the corners of a square and broadcast waves uniformly in all directions. At the center of the square, will the
waves always produce constructive interference no matter which two corners of the square are occupied
by the sources?
27.2 Young’s Double-Slit Experiment In 1801 the English scientist Thomas Young (1773–1829) performed a historic experiment that
demonstrated the wave nature of light by showing that two overlapping light waves can interfere
with each other. His experiment was particularly important because he was also able to determine
the wavelength of the light from his measurements, the fi rst such determination of this important
property. Figure 27.3 shows one arrangement of Young’s experiment, in which light of a single wavelength (monochromatic light) passes through a single narrow slit and falls on two closely
spaced, narrow slits S1 and S2. These two slits act as coherent sources of light waves that interfere
constructively and destructively at diff erent points on the screen to produce a pattern of alternat-
ing bright and dark fringes. The purpose of the single slit is to ensure that only light from one
direction falls on the double slit. Without it, light coming from diff erent points on the light source
would strike the double slit from diff erent directions and cause the pattern on the screen to be
washed out. The slits S1 and S2 act as coherent sources of light waves because the light from each
originates from the same primary source—namely, the single slit.
To help explain the origin of the bright and dark fringes, Figure 27.4 presents three top views of the double slit and the screen. Part a illustrates how a bright fringe arises directly oppo- site the midpoint between the two slits. In this part of the drawing the waves (identical) from
each slit travel to the midpoint on the screen. At this location, the distances ℓ1 and ℓ2 to the slits
are equal, each containing the same number of wavelengths. Therefore, constructive interfer-
ence results, leading to the bright fringe. Part b indicates that constructive interference produces another bright fringe on one side of the midpoint when the distance ℓ2 is larger than ℓ1 by exactly
one wavelength. A bright fringe also occurs symmetrically on the other side of the midpoint
when the distance ℓ1 exceeds ℓ2 by one wavelength; for clarity, however, this additional bright
fringe is not shown. Constructive interference produces other bright fringes (also not shown) on
both sides of the middle wherever the diff erence between ℓ1 and ℓ2 is an integer number of wave-
lengths: 𝜆, 2𝜆, 3𝜆, and so on. Part c shows how the fi rst dark fringe arises. Here the distance ℓ2 is larger than ℓ1 by exactly one-half a wavelength, so the waves interfere destructively, giving rise
to the dark fringe. Destructive interference creates other dark fringes on both sides of the center
wherever the diff erence between ℓ1 and ℓ2 equals an odd integer number of half-wavelengths: 1
2λ, 3
2λ, 5
2λ, and so on.
S0
Light source (single wavelength)
Single slit
Double slit
Screen
S1 S2
Dark fringe Bright fringe
FIGURE 27.3 In Young’s double-slit experiment, two slits S1 and S2 act as coherent
sources of light. Light waves from these slits
interfere constructively and destructively on the
screen to produce, respectively, the bright and
dark fringes. The slit widths and the distance
between the slits have been exaggerated for
clarity.
780 CHAPTER 27 Interference and the Wave Nature of Light
The brightness of the fringes in Young’s experiment varies, as the fringe pattern in Figure 27.5 shows. Below the fringe pattern is a graph to suggest the way in which the intensity varies for the
fringes. The central fringe is labeled with a zero, and the other bright fringes are numbered in
ascending order on either side of the center. It can be seen that the central fringe has the greatest
intensity. To either side of the center, the intensities of the other fringes decrease symmetrically
in a way that depends on how small the slit widths are relative to the wavelength of the light.
The position of the fringes observed on the screen in Young’s experiment can be calculated
with the aid of Figure 27.6. If the screen is located far away compared with the separation d of the slits, then the lines labeled ℓ1 and ℓ2 in part a are nearly parallel. Being nearly parallel, these lines make approximately equal angles 𝜃 with the horizontal. The distances ℓ1 and ℓ2 diff er by an amount Δℓ, which is the length of the short side of the colored triangle in part b of the drawing. Since the triangle is a right triangle, it follows that Δℓ = d sin 𝜃. Constructive interference occurs when the distances diff er by an integer number m of wavelengths 𝜆, or Δℓ = d sin 𝜃 = m𝜆. There- fore, the angle 𝜃 for the interference maxima can be determined from the following expression:
Bright fringes of a double slit
sin θ = m λ d m = 0, 1, 2, 3, . . . (27.1)
The value of m specifi es the order of the fringe. Thus, m = 2 identifi es the “second-order” bright fringe. Part c of Figure 27.6 stresses that the angle 𝜃 given by Equation 27.1 locates bright fringes on either side of the midpoint between the slits. A similar line of reasoning leads to the
conclusion that the dark fringes, which lie between the bright fringes, are located according to
Dark fringes of a double slit
sin θ = (m + 12 ) λ d m = 0, 1, 2, 3, . . . (27.2)
Example 1 illustrates how to determine the distance of a higher-order bright fringe from the
central bright fringe with the aid of Equation 27.1.
1
2 = 1
S1
(a) (b) (c)
S2
1 S1
S2
2 = 1 +
Bright fringe
Bright fringe 1S1
S2
Dark fringe
2 = 1 + 2 1–
2 1–
ℓ ℓ
ℓ
ℓ
ℓ ℓ ℓ ℓ
ℓ
𝜆 𝜆 𝜆
𝜆
FIGURE 27.4 The waves that originate from slits S1 and S2 interfere constructively (parts a and b) or destructively (part c) on the screen, depending on the diff erence in distances between the slits and the screen. Note that the slit widths and the distance between the slits have been exaggerated for clarity.
3 2 1 0
Central or zeroth fringe
1 2 3
FIGURE 27.5 The results of Young’s double-slit experiment, showing the pattern
of the bright and dark fringes formed on the
screen and a graph of the light intensity. The
central or zeroth fringe is the brightest fringe
(greatest intensity).
S1
d
Screen
1
2
2
1
Δ S2
S1
S2
S1 S2
m__
3
2
1
0
1
2
3
d
(a) (b) (c)
ℓ
ℓ
ℓ
ℓℓ
𝜃
𝜃 𝜃
𝜃
𝜃
𝜃 𝜃
FIGURE 27.6 (a) Rays from slits S1 and S2, which make approximately the same angle 𝜃 with the horizontal, strike a distant screen at the same spot. (b) The diff erence in the path lengths of the two rays is Δℓ = d sin 𝜃. (c) The angle 𝜃 is the angle at which a bright fringe (m = 2, here) occurs on either side of the central bright fringe (m = 0).
27.2 Young’s Double-Slit Experiment 781
In the preceding version of Young’s experiment, monochromatic light has been used. Light
that contains a mixture of wavelengths can also be used. Conceptual Example 2 deals with some
of the interesting features of the resulting interference pattern.
EXAMPLE 1 Young’s Double-Slit Experiment
Red light (𝜆 = 664 nm in vacuum) is used in Young’s experiment with the slits separated by a distance d = 1.20 × 10−4 m. The screen in Figure 27.7 is located at a distance of L = 2.75 m from the slits. Find the distance y on the screen between the central bright fringe and the third-order bright fringe.
Reasoning This problem can be solved by fi rst using Equation 27.1 to determine the value of 𝜃 that locates the third-order (m = 3) bright fringe. Then trigonometry can be used to obtain the distance y.
Solution According to Equation 27.1, we fi nd
θ = sin−1 (mλd ) = sin−1[ 3(664 × 10−9 m)
1.20 × 10−4 m ] = 0.951° According to Figure 27.7, the distance y can be calculated from tan 𝜃 = y/L:
y = L tan θ = (2.75 m) tan 0.951° = 0.0456 m
d = 1.20 × 10–4 m
L = 2.75 m
m = 3 (Bright fringe)
m = 0 (Bright fringe)
m = 3 (Bright fringe)
y
y
𝜃 𝜃
FIGURE 27.7 The third-order bright fringe (m = 3) is observed on the screen at a distance y from the central bright fringe (m = 0).
CONCEPTUAL EXAMPLE 2 White Light and Young’s Experiment
Figure 27.8 shows a photograph that illustrates the kind of interference fringes that can result when white light, which is a mixture of all colors, is
used in Young’s experiment. Except for the central fringe, which is white,
the bright fringes are a rainbow of colors. Why does Young’s experiment
separate white light into its constituent colors? In any group of colored
fringes, such as the two singled out in Figure 27.8, why is red farther out from the central fringe than green is? And fi nally, why is the central fringe
white rather than colored?
Reasoning and Solution To understand how the color separation arises, we need to remember that each color corresponds to a diff erent
wavelength 𝜆 and that constructive and destructive interference depend on the wavelength. According to Equation 27.1 (sin 𝜃 = m𝜆/d), there is a diff erent angle that locates a bright fringe for each value of 𝜆, and thus for each color. These diff erent angles lead to the separation of colors on
the observation screen. In fact, on either side of the central fringe, there
is one group of colored fringes for m = 1 and another for each additional value of m.
Now, consider what it means that, within any single group of colored
fringes, red is farther out from the central fringe than green is. It means
that, in the equation sin 𝜃 = m𝜆/d, red light has a larger angle 𝜃 than green light does. Does this make sense? Yes, because red has the larger wave-
length (see Table 26.2, where 𝜆red = 660 nm and 𝜆green = 550 nm).
In Figure 27.8, the central fringe is distinguished from all the other colored fringes by being white. In Equation 27.1, the central fringe is dif-
ferent from the other fringes because it is the only one for which m = 0. In Equation 27.1, a value of m = 0 means that sin 𝜃 = m𝜆/d = 0, which reveals that 𝜃 = 0°, no matter what the wavelength 𝜆 is. In other words, all wavelengths have a zeroth-order bright fringe located at the same place
on the screen, so that all colors strike the screen there and mix together to
produce the white central fringe.
Related Homework: Problem 60
FIGURE 27.8 This photograph shows the results observed on the screen in one version
of Young’s experiment in which white light
(a mixture of all colors) is used.
Colored fringes
m = 0
A n d y W
as h n ik
Historically, Young’s experiment provided strong evidence that light has a wave-like charac-
ter. If light behaved only as a stream of “tiny particles,” as others believed at the time,* then the
two slits would deliver the light energy into only two bright fringes located directly opposite the
slits on the screen. Instead, Young’s experiment shows that wave interference redistributes the
energy from the two slits into many bright fringes.
782 CHAPTER 27 Interference and the Wave Nature of Light
Check Your Understanding
(The answers are given at the end of the book.) 4. Replace the slits S1 and S2 in Figure 27.3 with identical in-phase loudspeakers and use the same ac
electrical signal to drive them. The two sound waves produced will then be identical, and you will have
the audio equivalent of Young’s double-slit experiment. In terms of loudness and softness, what would
you hear as you walk along the screen, starting from the center and going to either end? (a) Loud, then soft, then loud, then soft, etc., with the loud sounds decreasing in intensity as you walk away from the center (b) Loud, then soft, then loud, then soft, etc., with the loud sounds increasing in intensity as you walk away from the center (c) Soft, then loud, then soft, then loud, etc., with the loud sounds decreas- ing in intensity as you walk away from the center (d) Soft, then loud, then soft, then loud, etc., with the loud sounds increasing in intensity as you walk away from the center
5. CYU Figure 27.1 shows two double slits that have slit separations of d1 and d2. Light whose wavelength is either 𝜆1 or 𝜆2 passes through the slits. For comparison, the wavelengths are also illustrated in the drawing. For which combination of slit separation and wavelength would the
pattern of bright and dark fringes on the observation screen be (a) the most spread out and (b) the least spread out?
2
1
d2d1
𝜆
𝜆
CYU FIGURE 27.1
6. Suppose the light waves coming from both slits in a Young’s double-slit experiment had their phases shifted by an amount equivalent to a half-wavelength. (a) Would the pattern be the same or would the positions of the light and dark fringes be interchanged? (b) Would the pattern be the same or would the positions of the light and dark fringes be interchanged if the light coming from only one of the slits had its phase shifted by an amount equivalent to a half-wavelength?
7. In Young’s double-slit experiment, is it possible to see interference fringes when the wavelength of the light is greater than the distance between the slits?
27.3 Thin-Film Interference Young’s double-slit experiment is one example of interference between light waves. Interfer-
ence also occurs in more common circumstances. For instance, Interactive Figure 27.9 shows a thin fi lm such as gasoline fl oating on water. To begin with, let us assume that the fi lm has a
constant thickness. Consider what happens when monochromatic light (a single wavelength)
strikes the fi lm nearly perpendicularly. At the top surface of the fi lm refl ection occurs and pro-
duces the light wave represented by ray 1. However, refraction also occurs, and some light enters
the fi lm. Part of this light refl ects from the bottom surface of the fi lm and passes back up through
the fi lm, eventually reentering the air. Thus, a second light wave, which is represented by ray
2, also exists. Moreover, this wave, having traversed the fi lm twice, has traveled farther than
wave 1. Because of the extra travel distance, there can be interference between the two waves.
If constructive interference occurs, an observer whose eyes detect the superposition of waves 1
and 2 would see a uniformly bright fi lm. If destructive interference occurs, an observer would
see a uniformly dark fi lm.
*It is now known that the particle, or corpuscular, theory of light, which Isaac Newton promoted, does
indeed explain some experiments that the wave theory cannot explain. Today, light is regarded as having
both particle and wave characteristics. Chapter 29 discusses this dual nature of light.
Incident light
nair = 1.00
ngasoline = 1.40
nwater = 1.33
t
1 2
INTERACTIVE FIGURE 27.9 Because of refl ection and refraction, two light waves,
represented by rays 1 and 2, enter the eye
when light shines on a thin fi lm of gasoline
fl oating on a thick layer of water.
27.3 Thin-Film Interference 783
In Interactive Figure 27.9 the diff erence in path lengths between waves 1 and 2 occurs inside the thin fi lm. Therefore, we note the following:
Problem-Solving Insight The wavelength that is important for thin-fi lm interference is the wavelength within the fi lm, not the wavelength in vacuum.
The wavelength within the fi lm can be calculated from the wavelength in vacuum by using the
index of refraction n for the fi lm. With the aid of Equations 26.1 and 16.1, it can be shown that n = c/𝜐 = (c/f )/(𝜐/f ) = 𝜆vacuum/𝜆fi lm. In other words,
λfilm = λvacuum
n (27.3)
In explaining the interference that can occur in Interactive Figure 27.9, we need to add one other important part to the story. Whenever waves refl ect at a boundary, it is possible for them
to change phase. Animated Figure 27.10, for example, shows that a wave on a string is inverted when it refl ects from the end that is tied to a wall (see also Figure 17.16). This inversion is equiva-
lent to a half-cycle of the wave, as if the wave had traveled an additional distance of one-half of a
wavelength. In contrast, a phase change does not occur when a wave on a string refl ects from the
end of a string that is hanging free. When light waves undergo refl ection, similar phase changes
occur as follows:
1. When light travels through a material with a smaller refractive index toward a material with a larger refractive index (e.g., air to gasoline), refl ection at the boundary occurs along with a
phase change that is equivalent to one-half of a wavelength in the fi lm.
2. When light travels from a larger toward a smaller refractive index, there is no phase change upon refl ection at the boundary.
The next example indicates how the phase change that can accompany refl ection is taken into
account when dealing with thin-fi lm interference.
13
2
31
2
(a)
(b)
Incident wave
Reflected wave
ANIMATED FIGURE 27.10 When a wave on a string refl ects from a wall, the wave
undergoes a phase change. Thus, an upward-
pointing half-cycle of the wave becomes,
after refl ection, a downward-pointing half-
cycle, and vice versa, as the numbered labels
in the drawing indicate.
EXAMPLE 3 A Colored Thin Film of Gasoline
A thin fi lm of gasoline fl oats on a puddle of water. Sunlight falls almost
perpendicularly on the fi lm and refl ects into your eyes. Although sunlight
is white since it contains all colors, the fi lm looks yellow because destruc-
tive interference eliminates the color of blue (𝜆vacuum = 469 nm) from the refl ected light. The refractive indices of the blue light in gasoline and in
water are 1.40 and 1.33, respectively. Determine the minimum nonzero
thickness t of the fi lm.
Reasoning To solve this problem, we must express the condition for destructive interference in terms of the fi lm thickness t and the wave- length 𝜆fi lm in the gasoline fi lm. We must also take into account any phase changes that occur upon refl ection.
In Interactive Figure 27.9, the phase change for wave 1 is equiva- lent to one-half of a wavelength, since this light travels from a smaller
refractive index (nair = 1.00) toward a larger refractive index (ngasoline = 1.40). In contrast, there is no phase change when wave 2 refl ects from the
bottom surface of the fi lm, since this light travels from a material with a
larger refractive index (ngasoline = 1.40) toward a material with a smaller one (nwater = 1.33). The net phase change between waves 1 and 2 due to refl ec- tion is, thus, equivalent to one-half of a wavelength,
1
2λfilm. This half-wave- length must be combined with the extra travel distance for wave 2, to deter-
mine the condition for destructive interference. For destructive interference,
the combined total must be an odd integer number of half-wavelengths.
Since wave 2 travels back and forth through the fi lm and since light strikes
the fi lm nearly perpendicularly, the extra travel distance is twice the fi lm
thickness, or 2t. Thus, the condition for destructive interference is
2t + 12λ film = 1
2λfilm, 3
2λfilm, 5
2λfilm, . . .
After subtracting the term 1
2 λfilm from the left-hand side of this equation and from each term on the right-hand side, we can solve for the thickness
t of the fi lm that yields destructive interference:
t = mλ film
2 m = 0, 1, 2, 3, . . .
Problem-Solving Insight When analyzing thin-fi lm inter- ference eff ects, remember to use the wavelength of the light in the fi lm (𝛌fi lm) instead of the wavelength in a vacuum (𝛌vacuum).
Solution In order to calculate t, we need to know the wavelength of the blue light in the fi lm. Equation 27.3, with n = 1.40, gives this wavelength as
λfilm = λvacuum
n =
469 nm
1.40 = 335 nm
With this value for 𝜆fi lm and m = 1, our result for t gives the minimum nonzero fi lm thickness for which the blue color is missing in the refl ected
light as follows:
t = mλfilm
2 =
(1)(335 nm)
2 = 168 nm
Extra distance
traveled by
wave 2
}
Half-wavelength
net phase change
due to refl ection
Condition for
destructive interference
⏟
784 CHAPTER 27 Interference and the Wave Nature of Light
In Example 3 a half-wavelength net phase change occurs due to the refl ections at the upper
and lower surfaces of the thin fi lm. Depending on the refractive indices of the materials above
and below the fi lm, it is also possible that these refl ections yield a zero net phase change.
The thin fi lm in Example 3 has the same yellow color everywhere. In nature, such a uni-
formly colored thin fi lm would be unusual; the next example is more realistic.
The colors that you see when sunlight is refl ected from a thin fi lm also depend on your
viewing angle. At an oblique angle, the light corresponding to ray 2 in Interactive Figure 27.9, for instance, would travel a greater distance within the fi lm than it does at nearly perpendicular
incidence. The greater distance would lead to destructive interference for a diff erent wavelength.
THE PHYSICS OF . . . nonreflecting lens coatings. Thin-fi lm interference can be benefi cial in optical instruments. For example, some cameras contain six or more lenses. Refl ec-
tions from all the lens surfaces can reduce considerably the amount of light directly reaching the
fi lm. In addition, multiple refl ections from the lenses often reach the fi lm indirectly and degrade
the quality of the image. To minimize such unwanted refl ections, high-quality lenses are often
covered with a thin nonrefl ective coating of magnesium fl uoride (n = 1.38). The thickness of the coating is usually chosen to ensure that destructive interference eliminates the refl ection of green
light, which is in the middle of the visible spectrum. It should be pointed out that the absence of
any refl ected light does not mean that it has been destroyed by the nonrefl ective coating. Rather,
the “missing” light has been transmitted into the coating and the lens.
CONCEPTUAL EXAMPLE 4 Multicolored Thin Films
Under natural conditions, thin fi lms, like gasoline on water or like the
soap bubble in Figure 27.11, have a multicolored appearance that often changes while you are watching them. Why are such fi lms multicolored,
and what can be inferred from the fact that the colors change in time?
Reasoning and Solution In Example 3 we have seen that a thin fi lm can appear yellow if destructive interference removes blue light from the
refl ected sunlight. The thickness of the fi lm is the key. If the thickness
were diff erent, so that destructive interference removed green light from
the refl ected sunlight, the fi lm would appear magenta. Constructive inter-
ference can also cause certain colors to appear brighter than others in
the refl ected light and thereby give the fi lm a colored appearance. The
colors that are enhanced by constructive interference, like those removed
by destructive interference, depend on the thickness of the fi lm. Thus, we
conclude the following:
Problem-Solving Insight The diff erent colors in a thin fi lm of gasoline on water or in a soap bubble arise because the thickness is diff erent in diff erent places on the fi lm. More- over, the fact that the colors change as you watch them indi- cates that the thickness is changing. A number of factors can cause the thickness to change, including air cur-
rents, temperature fl uctuations, and the pull of gravity, which tends to make
a vertical fi lm sag, leading to thicker regions at the bottom than at the top.
Related Homework: Problem 17
FIGURE 27.11 This fantastic soap bubble is multicolored when viewed in sunlight because
of the eff ects of thin-fi lm interference. © A
lb er
to P
ar ed
es /A
g e
F o to
st o ck
27.3 Thin-Film Interference 785
Another interesting illustration of thin-fi lm interference is the air wedge. As Figure 27.12a shows, an air wedge is formed when two fl at plates of glass are separated along one side, perhaps
by a thin sheet of paper. The thickness of this fi lm of air varies between zero, where the plates
touch, and the thickness of the paper. When monochromatic light refl ects from this arrangement,
alternate bright and dark fringes are formed by constructive and destructive interference, as the
drawing indicates and Example 5 discusses.
Light source
(a)
Glass plates
Sheet of paper
Incident light
nglass = 1.52
nglass = 1.52
nair = 1.00
(b)
1 2
FIGURE 27.12 (a) The wedge of air formed between two fl at glass plates causes an inter-
ference pattern of alternating dark and bright
fringes to appear in refl ected light. (b) A side view of the glass plates and the air wedge.
EXAMPLE 5 An Air Wedge
(a) Assuming that green light (𝜆vacuum = 552 nm) strikes the glass plates nearly perpendicularly in Figure 27.12, determine the number of bright fringes that occur between the place where the plates touch and the edge
of the sheet of paper (thickness = 4.10 × 10−5 m). (b) Explain why there is a dark fringe where the plates touch.
Reasoning A bright fringe occurs wherever there is constructive inter- ference, as determined by any phase changes due to refl ection and by the
thickness of the air wedge. There is no phase change upon refl ection for
wave 1, since this light travels from a larger (glass) toward a smaller (air)
refractive index. In contrast, there is a half-wavelength phase change for
wave 2, since the ordering of the refractive indices is reversed at the lower
air/glass boundary where refl ection occurs. The net phase change due to
refl ection for waves 1 and 2, then, is equivalent to a half-wavelength. Now
we combine any extra distance traveled by ray 2 with this half-wavelength
and determine the condition for the constructive interference that creates
the bright fringes. Constructive interference occurs whenever the combi- nation yields an integer number of wavelengths. At nearly perpendicular incidence, the extra travel distance for wave 2 is approximately twice the
thickness t of the wedge at any point, so the condition for constructive interference is
2t + 12λ film = λ film, 2λ film, 3λ film, . . .
Extra distance
traveled by
wave 2
Half-wavelength
net phase change
due to refl ection
⏟
Condition for
destructive interference
}
Subtracting the term 1
2λ film from the left-hand side of this equation and from each term on the right-hand side yields
2t = 12λfilm, 3
2λfilm, 5
2λfilm, . . .
Therefore,
t = (m + 12 )λfilm
2 m = 0, 1, 2, 3, . . .
In this expression, note that the “fi lm” is a fi lm of air. Since the refractive
index of air is nearly one, 𝜆fi lm is virtually the same as that in a vacuum, so 𝜆fi lm = 552 nm.
Solution (a) When t equals the thickness of the paper holding the plates apart, the corresponding value of m can be obtained from the equation above:
m = 2t
λfilm −
1
2 =
2(4.10 × 10−5 m)
552 × 10−9 m −
1
2 = 148
Since the fi rst bright fringe occurs when m = 0, the number of bright fringes is m + 1 = 149 .
(b) Where the plates touch, there is a dark fringe because of destructive interference between the light waves represented by rays 1 and 2. Destruc-
tive interference occurs because the thickness of the wedge is zero here
and the only diff erence between the rays is the half-wavelength phase
change due to refl ection from the lower plate.
(m + 12)λfilm m = 0, 1, 2, 3, . . .
Another type of air wedge can also be used to determine the degree to which the surface of a
lens or mirror is spherical. When an accurate spherical surface is put in contact with an optically
fl at plate, as in Figure 27.13a, the circular interference fringes shown in part b of the fi gure can be observed. The circular fringes are called Newton’s rings. They arise in the same way that the straight fringes arise in Figure 27.12a.
Problem-Solving Insight Refl ected light will experience a phase change only if the light travels from a material with a smaller refractive index toward a material with a larger refractive
index. Be sure to take such a phase change into account when analyzing thin-fi lm interference.
786 CHAPTER 27 Interference and the Wave Nature of Light
Check Your Understanding
(The answers are given at the end of the book.) 8. A camera lens is covered with a nonrefl ective coating that eliminates the refl ection of perpendicularly
incident green light. Recalling Snell’s law of refraction (see Section 26.2), would you expect the re-
fl ected green light to be eliminated if it were incident on the nonrefl ective coating at an angle of 45°
rather than perpendicularly? (a) No, because the distance traveled by the light in the fi lm is less than twice the fi lm thickness. (b) No, because the distance traveled by the light in the fi lm is greater than twice the fi lm thickness. (c) Yes, the green light will still be eliminated.
9. Two pieces of the same glass are covered with thin fi lms of diff erent materials. In refl ected sunlight, however, the fi lms have diff erent colors. Why? (a) The fi lms could have the same thickness, but diff er- ent refractive indices. (b) The fi lms could have diff erent thicknesses, but the same refractive indices. (c) Both of the preceding answers could be correct.
10. A transparent coating is deposited on a glass plate and has a refractive index that is larger than that of the glass. For a certain wavelength within the coating, the thickness of the coating is a quarter-wavelength. Does the coating enhance or reduce the refl ection of the light corresponding to this wavelength?
11. The drawings in CYU Figure 27.2 show three situations—A, B, and C—in which light refl ects almost perpendicularly from the top and bottom surfaces of a thin fi lm, with the indices of refraction as shown.
(a) For which situation(s) will there be a net phase shift (due to refl ection) between waves 1 and 2 that is equivalent to either zero wavelengths or one wavelength (𝜆fi lm), where 𝜆fi lm is the wavelength of the light in the fi lm? (b) For which situation(s) will the fi lm appear dark when the thickness of the fi lm is equal to 12𝜆fi lm?
1.4 Film
A B C
1.5
1.3
1
2
1
2
1
2
1.3
1.5
1.4
1.4
1.3
1.5
Film Film
CYU FIGURE 27.2
12. When sunlight refl ects from a thin fi lm of soapy water (air on both sides), the fi lm appears multicol- ored, in part because destructive interference removes diff erent wavelengths from the light refl ected
at diff erent places, depending on the thickness of the fi lm. What happens as the fi lm becomes thinner
and thinner? (a) Nothing happens, and the fi lm remains multicolored. (b) The fi lm looks brighter and brighter in refl ected light, appearing totally white just before it breaks. (c) The fi lm looks darker and darker in refl ected light, appearing black just before it breaks.
13. Two thin fi lms are fl oating on water (n = 1.33). The fi lms have refractive indices of n1 = 1.20 and n2 = 1.45. Suppose that the thickness of each fi lm approaches zero. In refl ected light, fi lm 1 will look ____
and fi lm 2 will look ____. (a) bright, bright (b) bright, dark (c) dark, bright (d) dark, dark
27.4 The Michelson Interferometer THE PHYSICS OF . . . the Michelson interferometer. An interferometer is an apparatus that can be used to measure the wavelength of light by utilizing interference between two
light waves. One particularly famous interferometer was developed by Albert A. Michelson
(1852–1931). The Michelson interferometer uses refl ection to set up conditions where two light
waves interfere. Figure 27.14 presents a schematic drawing of the instrument. Waves emitted by the monochromatic light source strike a beam splitter, so called because it splits the beam of light into two parts. The beam splitter is a glass plate, the far side of which is coated with a thin layer
of silver that refl ects part of the beam upward as wave A in the drawing. The coating is so thin,
however, that it also allows the remainder of the beam to pass directly through as wave F. Wave A
strikes an adjustable mirror and refl ects back on itself. It again crosses the beam splitter and then
(b)
(a)
FIGURE 27.13 (a) The air wedge between a convex spherical glass surface and an
optically fl at plate leads to (b) a pattern of circular interference fringes that are known
as Newton’s rings.
© s
ci en
ce p h o to
s/ A
la m
y
DF
DA
Adjustable mirror
Wave A
Wave A
Light source
Beam splitter Compensating
plate
Thin silver coating
Wave F
Wave F
Fixed mirror
Viewing telescope
FIGURE 27.14 A schematic drawing of a Michelson interferometer.
27.5 Diff raction 787
enters the viewing telescope. Wave F strikes a fi xed mirror and returns, to be partly refl ected into
the viewing telescope by the beam splitter. Note that wave A passes through the glass plate of
the beam splitter three times in reaching the viewing scope, while wave F passes through it only
once. The compensating plate in the path of wave F has the same thickness as the beam splitter
plate and ensures that wave F also passes three times through the same thickness of glass on the
way to the viewing scope. Thus, an observer viewing the superposition of waves A and F through
the telescope sees constructive or destructive interference, depending only on the diff erence in
path lengths DA and DF traveled by the two waves. Now suppose that the mirrors are perpendicular to each other, the beam splitter makes a 45°
angle with each, and the distances DA and DF are equal. Waves A and F travel the same distance, and the fi eld of view in the telescope is uniformly bright due to constructive interference. How-
ever, if the adjustable mirror is moved away from the telescope by a distance of 1
4λ, wave A travels back and forth by an amount that is twice this value, leading to an extra distance of
1
2λ. Then, the waves are out of phase when they reach the viewing scope, destructive interference occurs, and
the viewer sees a dark fi eld. If the adjustable mirror is moved farther, full brightness returns as
soon as the waves are in phase and interfere constructively. The in-phase condition occurs when
wave A travels a total extra distance of 𝜆 relative to wave F. Thus, as the mirror is continuously moved, the viewer sees the fi eld of view change from bright to dark, then back to bright, and so
on. The amount by which DA has been changed can be measured and related to the wavelength of the light, since a bright fi eld changes into a dark fi eld and back again each time DA is changed by a half-wavelength. (The back-and-forth change in distance is 𝜆.) If a suffi ciently large number of wavelengths are counted in this manner, the Michelson interferometer can be used to obtain a
very accurate value for the wavelength from the measured changes in DA.
27.5 Diff raction As we have seen in Section 17.3, diff raction is the bending of waves around obstacles or the edges of an opening. In Figure 27.15, sound waves are leaving a room through an open doorway and bend, or diff ract, around the edges of the opening. Therefore, a listener hears the sound even
when he is around the corner from the doorway.
Diff raction is an interference eff ect, and the Dutch scientist Christian Huygens (1629–1695)
developed a principle that is useful in explaining why diff raction arises. Huygens’ principle describes how a wave front that exists at one instant gives rise to the wave front that exists later
on. This principle states that:
Every point on a wave front acts as a source of tiny wavelets that move forward with the same speed as the wave; the wave front at a later instant is the surface that is tangent to the wavelets.
We begin by using Huygens’ principle to explain the diff raction of sound waves in Figure 27.15. The drawing shows the top view of a plane wave front of sound approaching a doorway and identi-
fi es fi ve points on the wave front just as it is leaving the opening. According to Huygens’ principle,
each of these points acts as a source of wavelets, which are shown as red circular arcs at some
moment after they are emitted. The tangent to the wavelets from points 2, 3, and 4 indicates that in
front of the doorway the wave front is fl at and moving straight ahead. At the edges, however, points
1 and 5 are the last points that produce wavelets. Huygens’ principle suggests that in conforming to
the curved shape of the wavelets near the edges, the new wave front moves into regions that it would
not reach otherwise. The sound wave, then, bends or diff racts around the edges of the doorway.
Huygens’ principle applies not just to sound waves, but to all kinds of waves. For instance,
light has a wave-like nature and, consequently, exhibits diff raction. Therefore, you may ask,
“Since I can hear around the edges of a doorway, why can’t I also see around them?” As a matter
of fact, light waves do bend around the edges of a doorway. However, the degree of bending is
extremely small, so the diff raction of light is not enough to allow you to see around the corner.
As we will learn, the extent to which a wave bends around the edges of an opening is deter-
mined by the ratio 𝜆/W, where 𝜆 is the wavelength of the wave and W is the width of the opening. The photographs in Figure 27.16 illustrate the eff ect of this ratio on the diff raction of water waves. The degree to which the waves are diff racted or bent is indicated by the two red arrows
in each photograph. In part a, the ratio 𝜆/W is small because the wavelength (as indicated by the
Listener hears sound around
the corner
1
2
3
4
5Plane wave front of sound
Wall containing doorway
(top view)
FIGURE 27.15 Sound bends, or diff racts, around the edges of a doorway, so even a
person who is not standing directly in front of
the opening can hear the sound. The fi ve red
points within the doorway act as sources and
emit the fi ve Huygens wavelets shown in red.
788 CHAPTER 27 Interference and the Wave Nature of Light
distance between the wave fronts) is small relative to the width of the opening. The wave fronts
move through the opening with little bending or diff raction into the regions around the edges.
In part b, the wavelength is larger and the width of the opening is smaller. As a result, the ratio 𝜆/W is larger, and the wave fronts bend more into the regions around the edges of the opening.
Based on the pictures in Figure 27.16, we expect that light waves of wavelength 𝜆 will bend or diff ract appreciably when they pass through an opening whose width W is small enough to make the ratio 𝜆/W suffi ciently large. This is indeed the case, as Figure 27.17 illustrates. In this picture, it is assumed that parallel rays (or plane wave fronts) of light fall on a very narrow slit
and illuminate a viewing screen that is located far from the slit. Part a of the drawing shows what would happen if light were not diff racted: it would pass through the slit without bending around the edges and would produce an image of the slit on the screen. Part b shows what actually hap- pens. The light diff racts around the edges of the slit and brightens regions on the screen that are
not directly opposite the slit. The diff raction pattern on the screen consists of a bright central
band, accompanied by a series of narrower faint fringes that are parallel to the slit itself.
To help explain how the pattern of diff raction fringes arises, Figure 27.18 shows a top view of a plane wave front approaching the slit and singles out fi ve sources of Huygens wavelets. Consider how
the light from these fi ve sources reaches the midpoint on the screen. To simplify things, the screen is
assumed to be so far from the slit that the rays from each Huygens source are nearly parallel.* Then,
all the wavelets travel virtually the same distance to the midpoint, arriving there in phase. As a result,
constructive interference creates a bright central fringe on the screen, directly opposite the slit.
FIGURE 27.16 These photographs show water waves (horizontal lines) approaching an opening whose width W is greater in (a) than in (b). In addition, the wavelength 𝜆 of the waves is smaller in (a) than in (b). Therefore, the ratio 𝜆/W increases from (a) to (b) and so does the extent of the diff raction, as the red arrows indicate. (a) Smaller value for /W, less diffraction (b) Larger value for 𝜆 /W, more diffraction
W
𝜆
𝜆
C o u rt
es y E
d u ca
ti o n D
ev el
o p m
en t
C en
te r
C o u rt
es y E
d u ca
ti o n D
ev el
o p m
en t
C en
te r
FIGURE 27.17 (a) If light were to pass through a very narrow slit
without being diff racted, only the region on the screen directly oppo-
site the slit would be illuminated.
(b) Diff raction causes the light to bend around the edges of the slit
into regions it would not otherwise
reach, forming a pattern of alter-
nating bright and dark fringes on
the screen. The slit width has been
exaggerated for clarity.
(a) Without diffraction (b) With diffraction
*When the rays are parallel, the diff raction is called Fraunhofer diff raction in tribute to the German optician Joseph von
Fraunhofer (1787–1826). When the rays are not parallel, the diff raction is referred to as Fresnel diff raction, named for
the French physicist Augustin Jean Fresnel (1788–1827).
27.5 Diff raction 789
The wavelets emitted by the Huygens sources in the slit can also interfere destructively on
the screen, as Figure 27.19 illustrates. Part a shows light rays directed from each source toward the fi rst dark fringe. The angle 𝜃 gives the position of this dark fringe relative to the line between the midpoint of the slit and the midpoint of the central bright fringe. Since the screen is very far
from the slit, the rays from each Huygens source are nearly parallel and are oriented at nearly the
same angle 𝜃, as in part b of the drawing. The wavelet from source 1 travels the shortest distance to the screen, while the wavelet from source 5 travels the farthest. Destructive interference creates
the fi rst dark fringe when the extra distance traveled by the wavelet from source 5 is exactly
one wavelength, as the colored right triangle in the drawing indicates. Under this condition, the
extra distance traveled by the wavelet from source 3 at the center of the slit is exactly one-half
of a wavelength. Therefore, wavelets from sources 1 and 3 in Figure 27.19b are exactly out of phase and interfere destructively when they reach the screen. Similarly, a wavelet that originates
slightly below source 1 cancels a wavelet that originates the same distance below source 3. Thus,
each wavelet from the upper half of the slit cancels a corresponding wavelet from the lower half,
and no light reaches the screen. As can be seen from the colored right triangle, the angle 𝜃 locat- ing the fi rst dark fringe is given by sin 𝜃 = 𝜆/W, where W is the width of the slit.
Figure 27.21 shows the condition that leads to destructive interference at the second dark fringe on either side of the midpoint on the screen. In reaching the screen, the light from source
1
2
3
4
5
Incident plane wave
Distant screenSlit
Midpoint of central bright
fringe
FIGURE 27.18 A plane wave front is inci- dent on a single slit. This top view of the slit
shows fi ve sources of Huygens wavelets. The
wavelets travel toward the midpoint of the cen-
tral bright fringe on the screen, as the red rays
indicate. The screen is very far from the slit.
1
2
3
4
5
Incident plane wave
Midpoint of central bright
fringe
First dark
fringe
/2
1
2
3
4
5
W
(b)
(a)
𝜃
𝜃
𝜃
FIGURE 27.19 These drawings pertain to single-slit diff raction and show how destructive interference leads to the fi rst dark fringe on
either side of the central bright fringe. For clarity, only one of the dark
fringes is shown. The screen is very far from the slit.
Math Skills To understand why the colored right triangle in Figure 27.19b implies that sin 𝜃 = 𝜆/W, it is necessary to see why there are two angles labeled 𝜃 in the fi gure. To help explain these angles, we show a simplifi ed version of Figure 27.19b in Figure 27.20, where we label the angle in the colored triangle as 𝛼. We do this so that we can show that the angle 𝛼 is, in fact, the same as the angle 𝜃 between the red ray at the top of the slit and the horizontal dashed line. Since the slit is oriented vertically, we know
that the line AC in Figure 27.20 is perpendicular to the horizontal dashed line, with the result that the angles 𝛼 and 𝛽 form a right angle:
α + β = 90° or α = 90° − β
In addition, we know that the line AB in Figure 27.20 has been drawn per- pendicular to the red rays, which means that the angles 𝜃 and 𝛽 also form a right angle:
θ + β = 90° or β = 90° − θ
Substituting this result for 𝛽 into the result for 𝛼 reveals that
α = 90° − β = 90° − (90° − θ) = θ
A
B C
𝛼
𝛽
𝜃
FIGURE 27.20 Math Skills drawing.
1
2
3
4
5
W
2
3 /2
/2
𝜃
𝜃
𝜆
𝜆
𝜆
𝜆
FIGURE 27.21 In a single-slit diff raction pattern, multiple dark fringes occur on either
side of the central bright fringe. This drawing
shows how destructive interference creates the
second dark fringe on a very distant screen.
790 CHAPTER 27 Interference and the Wave Nature of Light
5 now travels a distance of two wavelengths farther than the light from source 1. Under this
condition, the wavelet from source 5 travels one wavelength farther than the wavelet from source
3, and the wavelet from source 3 travels one wavelength farther than the wavelet from source 1.
Therefore, each half of the slit can be treated as the entire slit was in the previous paragraph; all
the wavelets from the top half interfere destructively with each other, and all the wavelets from
the bottom half do likewise. As a result, no light from either half reaches the screen, and another
dark fringe occurs. The colored triangle in the drawing shows that this second dark fringe occurs
when sin 𝜃 = 2𝜆/W. Similar arguments hold for the third- and higher-order dark fringes, with the general result being
Dark fringes for single-slit diff raction sin θ = m
λ W m = 1, 2, 3, . . . (27.4)
Between each pair of dark fringes there is a bright fringe due to constructive interference.
The brightness of the fringes is related to the light intensity, just as loudness is related to
sound intensity. The intensity of the light at any location on the screen is the amount of light
energy per second per unit area that strikes the screen there. Figure 27.22 gives a graph of the light intensity, along with the single-slit diff raction pattern. The central bright fringe,
which is approximately twice as wide as the other bright fringes, has by far the greatest
intensity.
The width of the central fringe provides some indication of the extent of the diff raction, as
Example 6 illustrates.
Midpoint of central
bright fringe
Light intensity
FIGURE 27.22 A single-slit diff raction pattern, with a bright and wide central fringe.
The higher-order bright fringes are much less
intense than the central fringe, as the graph
indicates.
EXAMPLE 6 Single-Slit Diff raction
Light passes through a slit and shines on a fl at screen that is located L = 0.40 m away (see Figure 27.23). The wavelength of the light in a vacuum is 𝜆 = 410 nm. The distance between the midpoint of the central bright
fringe and the fi rst dark fringe is y. Determine the width 2y of the cen- tral bright fringe when the width of the slit is (a) W = 5.0 × 10−6 m and (b) W = 2.5 × 10−6 m. Reasoning The width of the central bright fringe is determined by two factors. One is the angle 𝜃 that locates the fi rst dark fringe on either side of the midpoint. The other is the distance L between the screen and the slit. Larger values for 𝜃 and L lead to a wider central bright fringe. Larger values of 𝜃 mean greater diff raction and occur when the ratio 𝜆/W is larger. Thus, we expect the width of the central bright fringe to be greater
when the slit width W is smaller.
Solution (a) The angle 𝜃 in Equation 27.4 locates the fi rst dark fringe when m = 1: sin 𝜃 = (1)𝜆/W. Therefore,
θ = sin−1 ( λW) = sin−1 ( 410 × 10−9 m
5.0 × 10−6 m ) = 4.7° According to Figure 27.23, tan 𝜃 = y/L, so the width 2y of the central bright fringe is
2y = 2L tan θ = 2 (0.40 m) tan 4.7° = 0.066 m
(b) Repeating the same calculations as in part (a) with W = 2.5 × 10−6 m reveals that 2y = 0.13 m . As expected for a given wavelength, the width 2y of the central maximum in the diff raction pattern is greater when the width of the slit is smaller.
y
y
L = 0.40 m
W
First dark fringe (m = 1)
First dark fringe (m = 1)
Midpoint of central bright fringe
𝜃 𝜃
FIGURE 27.23 The distance 2y is the width of the central bright fringe.
THE PHYSICS OF . . . producing computer chips using photolithography. In the production of computer chips, it is important to minimize the eff ects of diff raction. Such chips
are very small and yet contain enormous numbers of electronic components, as Figure 23.32 illustrates. Such miniaturization is achieved using the techniques of photolithography. The
patterns on the chip are created fi rst on a “mask,” which is similar to a photographic slide.
Light is then directed through the mask onto silicon wafers that have been coated with a photo-
sensitive material. The light-activated parts of the coating can be removed chemically, to leave
the ultrathin lines that correspond to the miniature patterns on the chip. As the light passes
27.6 Resolving Power 791
through the narrow slit-like patterns on the mask, the light spreads out due to diff raction. If
excessive diff raction occurs, the light spreads out so much that sharp patterns are not formed
on the photosensitive material coating the silicon wafer. Ultraminiaturization of the patterns
requires the absolute minimum of diff raction, and currently this is achieved by using ultravio-
let light, which has a wavelength shorter than that of visible light. The shorter the wavelength
𝜆, the smaller the ratio 𝜆/W, and the less the diff raction. The wavelengths of X-rays are much shorter than those of ultraviolet light and, thus, will reduce diff raction even more, allowing
further miniaturization.
Another example of diff raction can be seen when light from a point source falls on an
opaque disk, such as a coin (Figure 27.24). The eff ects of diff raction modify the dark shadow cast by the disk in several ways. First, the light waves diff racted around the circular edge of
the disk interfere constructively at the center of the shadow to produce a small bright spot.
There are also circular bright fringes in the shadow area. In addition, the boundary between
the circular shadow and the lighted screen is not sharply defi ned but consists of concentric
bright and dark fringes. The various fringes are analogous to those produced by a single slit
and are due to interference between Huygens wavelets that originate from diff erent points near
the edge of the disk.
Check Your Understanding
(The answers are given at the end of the book.) 14. A diff raction pattern is produced on a viewing screen by using a single slit with blue light. Does the
pattern broaden or contract (become narrower) (a) when the blue light is replaced by red light (b) when the slit width is increased?
15. A sound wave has a much greater wavelength than does a light wave. When the two waves pass through a doorway, which one, if either, diff racts to a greater extent? (a) The sound wave (b) The light wave (c) Both waves diff ract by the same amount.
27.6 Resolving Power Figure 27.25 shows three photographs of an automobile’s headlights taken at progressively greater distances from the camera. In parts a and b, the two separate headlights can be seen clearly. In part c, however, the car is so far away that the headlights are barely distinguishable and appear almost as a single light. The resolving power of an optical instrument, such as a camera, is its ability to distinguish between two closely spaced objects. If a camera with a higher resolv-
ing power had taken these pictures, the photograph in part c would have shown two distinct and separate headlights. Any instrument used for viewing objects that are close together must have a
FIGURE 27.24 The diff raction pattern formed by an opaque disk consists of a small
bright spot in the center of the dark shadow,
circular bright fringes within the shadow, and
concentric bright and dark fringes surrounding
the shadow.
Opaque disk
Light
FIGURE 27.25 These automobile headlights were photographed at various distances from the camera, closest in part a and farthest in part c. In part c, the headlights are so far away that they are barely distinguishable.
© T
ru ax
/T h e
Im ag
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in d er
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Im ag
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792 CHAPTER 27 Interference and the Wave Nature of Light
high resolving power. This is true, for example, for a telescope used to view distant stars or for
a microscope used to view tiny organisms. We will now see that diff raction occurs when light
passes through the circular, or nearly circular, openings that admit light into cameras, telescopes,
microscopes, and human eyes. The resulting diff raction pattern places a limit on the resolving
power of these instruments.
Figure 27.26 shows the diff raction pattern created by a small circular opening when the viewing screen is far from the opening. The pattern consists of a central bright circular region,
surrounded by alternating bright and dark circular fringes. These fringes are analogous to the
rectangular fringes that a single slit produces. The angle 𝜃 in the picture locates the fi rst circular dark fringe relative to the center of the central bright region and is given by
sin θ = 1.22 λ D
(27.5)
where 𝜆 is the wavelength of the light and D is the diameter of the opening. This expression is similar to Equation 27.4 for a slit (sin 𝜃 = 𝜆/W, when m = 1) and is valid when the distance to the screen is much larger than the diameter D.
An optical instrument with the ability to resolve two closely spaced objects can produce
images of them that can be identifi ed separately. Think about the images on the image sensor
when light from two widely separated point objects passes through the circular aperture of a
camera. As Figure 27.27 illustrates, each image is a circular diff raction pattern, but the two patterns do not overlap and are completely resolved. On the other hand, if the objects are suf-
fi ciently close together, the intensity patterns created by the diff raction overlap, as Figure 27.28a suggests. In fact, if the overlap is extensive, it may no longer be possible to distinguish the patterns separately. In such a case, the picture from a camera would show a single blurred
object instead of two separate objects. In Figure 27.28b the diff raction patterns overlap, but not enough to prevent us from seeing that two objects are present. Ultimately, then, diff raction
limits the ability of an optical instrument to produce distinguishable images of objects that are
close together.
It is useful to have a criterion for judging whether two closely spaced objects will be resolved
by an optical instrument. Figure 27.28a presents the Rayleigh criterion for resolution, fi rst pro- posed by Lord Rayleigh (1842–1919):
Two point objects are just resolved when the fi rst dark fringe in the diff raction pattern of one falls directly on the central bright fringe in the diff raction pattern of the other.
FIGURE 27.26 When light passes through a small circular opening, a circular diff raction
pattern is formed on a screen. The angle 𝜃 locates the fi rst dark fringe relative to the
central bright region. The intensities of the
bright fringes and the diameter of the opening
have been exaggerated for clarity.
𝜃
FIGURE 27.27 When light from two point objects passes through the circular aperture
of a camera, two circular diff raction patterns
are formed as images on the image sensor.
The images here are completely separated
or resolved because the objects are widely
separated.
Object 1 Object 2
Camera aperture
Image sensor
FIGURE 27.28 (a) According to the Rayleigh criterion, two point objects are just resolved when the fi rst dark fringe (zero intensity) of one image falls on the central bright fringe (maximum intensity) of the other
image. (b) This drawing shows two overlapping but still resolvable diff raction patterns.
min
min
Intensities
Object 1 Object 2
(a) (b)
𝜃
𝜃
27.6 Resolving Power 793
According to the Rayleigh criterion, the minimum angle 𝜃min between the two objects in Figure 27.28a is the angle given by Equation 27.5. If 𝜃min is small (less than about 9°) and is expressed in radians, sin 𝜃min ≈ 𝜃min. Then, Equation 27.5 becomes
θmin ≈ 1.22 λ D
(θmin in radians) (27.6)
For a given wavelength 𝜆 and aperture diameter D, Equation 27.6 specifi es the smallest angle that two point objects can subtend at the aperture and still be resolved. According to this
equation, optical instruments designed to resolve closely spaced objects (small values of 𝜃min) must utilize the smallest possible wavelength and the largest possible aperture diameter. For
example, when short-wavelength ultraviolet light is collected by its large 2.4-m-diameter mirror,
the Hubble Space Telescope is capable of resolving two closely spaced stars that have an angular
separation of about 𝜃min = 1 × 10−7 rad. This angle is equivalent to resolving two objects only 1 cm apart when they are 1 × 105 m (about 62 miles) from the telescope. Example 7 deals with
the resolving power of the human eye.
Math Skills To see why sin θmin ≈ θmin when θmin is small and is expressed in radians, we drop the subscript (for simplicity) and consider Equation 8.1, which defi nes an angle 𝜃 in radians. According to this defi nition, 𝜃 is the length s of the circular arc that the angle subtends divided by the radius r of the arc (see Figure 27.29a):
θ = s r
On the other hand, Equation 1.1 defi nes sin 𝜃 as
sin θ = ho h
where ho is the length of the side of a right triangle that is opposite the angle 𝜃 and h is the length of the hypotenuse (see Figure 27.29b). As 𝜃 becomes smaller and smaller in both parts of Figure 27.29, we can see that ho also becomes smaller and approaches the arc length s, whereas h approaches the radius r. Therefore, for a small angle 𝜃 expressed in radians, we conclude that
sin θ = ho h
≈ s r = θ or sin θ ≈ θ
Note that the symbol “≈” means “approximately equal to.”
FIGURE 27.29 Math Skills drawing.
r s
Circle
h ho
90°
(a) (b)
𝜃 𝜃
Analyzing Multiple -Concept Problems
EXAMPLE 7 BIO The Physics of Comparing Human Eyes and Eagle Eyes
(a) A hang glider is fl ying at an altitude of 120 m. Green light (wavelength = 555 nm in vacuum) enters the pilot’s eye through a pupil that has a diam-
eter of 2.5 mm. Determine how far apart two point objects must be on the
ground if the pilot is to have any hope of distinguishing between them (see
Figure 27.30). (b) An eagle’s eye has a pupil with a diameter of 6.2 mm. Repeat part (a) for an eagle fl ying at the same altitude as the glider.
794 CHAPTER 27 Interference and the Wave Nature of Light
*In applying the Rayleigh criterion, we use the given wavelength in vacuum because it is nearly identical to the
wavelength in air. We use the wavelength in air or vacuum, even though the diff raction occurs within the eye, where
the index of refraction is about n = 1.36 and the wavelength is 𝜆eye = 𝜆vacuum/n, according to Equation 27.3. The reason is that in entering the eye, the light is refracted according to Snell’s law (Section 26.2), which also includes an eff ect
due to the index of refraction. If the angle of incidence is small, the eff ect of n in Snell’s law cancels the eff ect of n in Equation 27.3, to a good degree of approximation.
Modeling the Problem
STEP 1 Radian Measure The angle that the two objects subtend at the pupil of the eye must be at least as large as the angle 𝜃min specifi ed by the Rayleigh criterion for resolution. Using radian measure as discussed in Section 8.1, we refer to Figure 27.30 and express this angle as
θmin ≈ s H
This is an approximate application of Equation 8.1, which states that an angle in radians is the
arc length divided by the radius. Here, the arc length is approximately the separation distance s, assuming that the altitude H is much greater than s. Solving for s gives Equation 1 at the right. In this result, the altitude is known, and we proceed to Step 2 to evaluate the angle 𝜃min.
STEP 2 The Rayleigh Criterion The Rayleigh criterion specifi es the angle 𝜃min in radians as
θmin ≈ 1.22 λ D
(27.6)
where 𝜆 is the wavelength of the light in vacuum* and D is the diameter of the pupil of the eye. The substitution of this expression into Equation 1 is shown at the right.
Problem-Solving Insight The minimum angle 𝜽min between two objects that are just resolved must be expressed in radians, not degrees, when using Equation 27.6 (𝜽min ≈ 1.22 𝞴/D).
Solution Combining the results of each step algebraically, we fi nd that
s ≈ θmin H ≈ (1.22 λD) H STEP 1 STEP 2
Reasoning A greater distance s of separation between the objects on the ground makes it easier for the eye of the observer (the pilot or the eagle;
see Figure 27.30) to resolve them as separate objects. This is because the angle that the two objects subtend at the pupil of the eye is greater when
the separation distance is greater. This angle must be at least as large as
the angle 𝜃min specifi ed by the Rayleigh criterion for resolution. In apply- ing this criterion, we will use the concept of the radian to express the
angle as an arc length (approximately the separation distance) divided by
a radius (the altitude), as discussed in Section 8.1.
Knowns and Unknowns The following table summarizes the data that are given:
FIGURE 27.30 The Rayleigh criterion can
be used to estimate the
smallest distance s that can separate two objects
on the ground, if a person
on a hang glider is to
be able to distinguish
between them.
s Object 1 Object 2
H = 120 mmin 𝜃
Description Symbol Value Comment Altitude H 120 m Same for pilot and eagle.
Wavelength of light in vacuum 𝜆 555 nm 1 nm = 10−9 m
Diameter of pupil of eye D 2.5 mm or 6.2 mm Smaller value is for pilot; larger value is for eagle.
Unknown Variables Separation between objects on ground s ?
?
s ≈ θmin H (1)
s ≈ θmin H (1)
θmin ≈ 1.22 λ D
(27.6)
27.6 Resolving Power 795
Many optical instruments have a resolving power exceeding that of the human eye. The typi-
cal camera does, for instance. Conceptual Example 8 compares the abilities of the human eye and
a camera to resolve two closely spaced objects.
The separation distance between the objects on the ground can now be obtained.
(a) For the pilot to have any hope of distinguishing between the objects, the separation distance must be at least
s ≈ (1.22 λD ) H = 1.22 ( 555 × 10−9 m
2.5 × 10−3 m ) (120 m) = 0.033 m (b) For the eagle, we fi nd that
s ≈ (1.22 λ D ) H = 1.22 ( 555 × 10−9 m
6.2 × 10−3 m) (120 m) = 0.013 m Since the pupil of the eagle’s eye is larger than that of a human eye, diff raction creates less of
a limitation for the eagle; the two objects can be closer together and still be resolved by the
eagle’s eye.
Related Homework: Problem 41
CONCEPTUAL EXAMPLE 8 Is What You See What You Get?
The French postimpressionist artist Georges Seurat developed a painting
technique in which dots of color are placed close together on the canvas.
From suffi ciently far away the individual dots are not distinguishable, and
the images in the picture take on a more normal appearance. Figure 27.31 shows a person in a museum looking at one of Seurat’s paintings. Suppose
that the person stands close to the painting, then backs up until the dots just
become indistinguishable to his eyes and takes a picture from this position.
The light enters his eyes through pupils that have diameters of 2.5 mm and
enters the digital camera through an aperture, or opening, with a diameter
of 25 mm. He then goes home and prints an enlarged photograph of the
painting. Can he see the individual dots in the photograph? (a) No, because if his eye cannot see the dots at the museum, the camera is also unable to re-
cord the individual dots. (b) Yes, because the camera gathers light through a much larger aperture than does the eye. (c) Yes, because, unlike the eye, a photograph taken by a camera is not limited by the eff ects of diff raction.
Reasoning To answer this question, we turn to Equation 27.6, which expresses the Rayleigh criterion for resolving two point objects (such as
the dots)—namely, θmin ≈ 1.22 λ/D. Here 𝜃min is the minimum angle that exists between light rays from two adjacent dots as the rays pass through the
aperture (see Figure 27.28), 𝜆 is the wavelength of the light, and D is the
diameter of the aperture. A larger value of D implies a smaller value for 𝜃min, which, in turn, means that the instrument has a greater resolving power.
Answer (a) is incorrect. Diff raction limits the ability of any instrument to see two closely spaced objects as distinct. This ability depends on the
diameter of the aperture through which the light enters the instrument.
Since the eye and the camera have apertures with diff erent diameters, the
camera may record the individual dots in the painting even though the eye
does not see them as distinct.
Answer (c) is incorrect. The eff ects of diff raction limit the resolving power of both the eye and the camera.
Answer (b) is correct. For the eye and the camera, the aperture diam- eters are Deye = 2.5 mm and Dcamera = 25 mm, so the diameter for the camera is ten times larger than that for the eye. Thus, at the distance at
which the eye loses its ability to resolve the individual dots in the paint-
ing, the camera can still easily resolve them. As discussed in the footnote
to Example 7, we can ignore the eff ect on the wavelength of the index of
refraction of the material from which the eye is made.
Related Homework: Check Your Understanding Question 18, Problem 38
FIGURE 27.31 This person is about to take a photograph of a famous painting by
Georges Seurat, who developed the technique
of using tiny dots of color to construct his
images. Conceptual Example 8 discusses what
the person sees when the photograph is printed. A rt
I n st
it u te
o f
C h ic
ag o ©
B ri
d g em
an A
rt L
ib ra
ry ,
L o n d o n /S
u p er
S to
ck
796 CHAPTER 27 Interference and the Wave Nature of Light
Check Your Understanding
(The answers are given at the end of the book.)
16. BIO Suppose that the pupil of your eye were elliptical instead of circular in shape, with the long axis of the ellipse oriented in the vertical direction. Would the resolving power of your eye be the same in
the horizontal and vertical directions and, if not, in which direction would it be greater? The resolving
power would (a) be the same in both directions (b) be greater in the horizontal direction (c) be greater in the vertical direction.
17. BIO Suppose that you were designing an eye and could select the size of the pupil and the wave- lengths of the electromagnetic waves to which the eye is sensitive. As far as the limitation created by
diff raction is concerned, rank the following design choices in order of decreasing resolving power
(greatest fi rst): (a) Large pupil and ultraviolet wavelengths (b) Small pupil and infrared wavelengths (c) Small pupil and ultraviolet wavelengths
18. Review Conceptual Example 8 before answering this question. A person is viewing one of Seurat’s paintings that consists of dots of color. She is so close to the painting that the dots are distinguishable.
Without moving, she squints, thus reducing the size of the opening in her eyes. Does squinting make
the painting take on a more normal appearance?
19. On many cameras one can select the f-number setting, or f-stop. The f-number gives the ratio of the focal length of the camera lens to the diameter of the aperture through which light enters the camera. If
you want to resolve two closely spaced objects in a picture, should you use a small or a large f-number setting?
27.7 The Diff raction Grating THE PHYSICS OF . . . a diff raction grating. Diff raction patterns of bright and dark fringes occur when monochromatic light passes through a single or double slit. Fringe patterns also
result when light passes through more than two slits, and an arrangement consisting of a large
number of parallel, closely spaced slits called a diff raction grating has proved very useful. Gratings with as many as 40 000 slits per centimeter can be made, depending on the production
method. In one method a diamond-tipped cutting tool is used to inscribe closely spaced parallel
lines on a glass plate, the spaces between the lines serving as the slits. In fact, the number of slits
per centimeter is often quoted as the number of lines per centimeter.
Figure 27.32 illustrates how light travels to a distant viewing screen from each of fi ve slits in a grating and forms the central bright fringe and the fi rst-order bright fringes on either side.
Higher-order bright fringes are also formed but are not shown in the drawing. Each bright fringe
is located by an angle 𝜃 relative to the central fringe. These bright fringes are sometimes called the principal fringes or principal maxima, since they are places where the light intensity is a maximum. The term “principal” distinguishes them from other, much less bright, fringes that are
referred to as secondary fringes or secondary maxima.
FIGURE 27.32 When light passes through a diff raction grating, a central
bright fringe (m = 0) and higher-order bright fringes (m = 1, 2, . . .) form when the light falls on a distant viewing screen.
First-order maximum (m = 1)
Diffraction grating
Incident plane wave of light
First-order maximum (m = 1)
Central or zeroth-order maximum (m = 0)
𝜃
𝜃
27.7 The Diff raction Grating 797
Constructive interference creates the principal fringes. To show how, we assume the screen
is far from the grating, so that the rays remain nearly parallel while the light travels toward the
screen. In reaching the place on the screen where a fi rst-order maximum is located, light from slit
2 travels a distance of one wavelength farther than light from slit 1, as in Figure 27.33. Similarly, light from slit 3 travels one wavelength farther than light from slit 2, and so forth, as emphasized by
the four colored right triangles on the right-hand side of the drawing. For the fi rst-order maximum,
the blow-up view of slits 1 and 2 shows that constructive interference occurs when sin 𝜃 = 𝜆/d, where d is the separation between slits. A second-order maximum forms when the extra distance traveled by light from adjacent slits is two wavelengths, so that sin 𝜃 = 2𝜆/d. The general result is
Principal maxima of a diffraction grating sin θ = m
λ d m = 0, 1, 2, 3, . . . (27.7)
The separation d between the slits can be calculated from the number of slits per centimeter of grating; for instance, a grating with 2500 slits per centimeter has a slit separation of d = (1/2500) cm = 4.0 × 10−4 cm. Equation 27.7 is identical to Equation 27.1 for the double slit. A
grating, however, produces bright fringes that are much narrower or sharper than those from a double slit, as the intensity patterns in Figure 27.34 reveal. Between the principal maxima of a diff raction grating there are secondary maxima with much smaller intensities. For a large number
of slits, these secondary maxima are very small.
The next example illustrates the ability of a grating to separate the components in a mixture
of colors.
Second-order maximum
1
1
5 2
d
First-order maximum
1
2
d
2 4
3
2
𝜃
𝜃
𝜃
𝜃
𝜃
𝜆
𝜆
FIGURE 27.33 The conditions shown here lead to the fi rst- and second-order intensity maxima in the diff raction pattern produced by the diff raction grating on the right.
m = 2 m = 1 m = 0
Grating (5 slits)
Double slit
Li gh
t in
te ns
it y
Li gh
t in
te ns
it y
m = 1 m = 2
m = 2 m = 1 m = 0 m = 1 m = 2
FIGURE 27.34 The bright fringes produced by a diff raction grating are much narrower
than those produced by a double slit. Note the
three small secondary bright fringes between
the principal bright fringes of the grating.
EXAMPLE 9 Separating Colors with a Diff raction Grating
A mixture of violet light (𝜆 = 410 nm in vacuum) and red light (𝜆 = 660 nm in vacuum) falls on a grating that contains 1.0 × 104 lines/cm. For each
wavelength, fi nd the angle 𝜃 that locates the fi rst-order maxima.
Reasoning Before Equation 27.7 can be used here, a value for the sepa- ration d between the slits is needed: d = 1/(1.0 × 104 lines/cm) = 1.0 × 10−4 cm, or 1.0 × 10−6 m. For violet light, the angle 𝜃violet for the fi rst-order maxima (m = 1) is given by sin 𝜃violet = m𝜆violet/d, with an analogous equa- tion applying for the red light.
Solution For violet light, the angle locating the fi rst-order maxima is
θviolet = sin−1 λviolet
d = sin−1 ( 410 × 10
−9 m
1.0 × 10−6 m ) = 24°
For red light, a similar calculation with 𝜆red = 660 × 10−9 m shows that θred = 41° . Because 𝜃violet and 𝜃red are diff erent, separate fi rst-order bright fringes are seen for violet and red light on a viewing screen.
If the light in Example 9 had been sunlight, the angles for the fi rst-order maxima would cover
all values in the range between 24° and 41°, since sunlight contains all colors or wavelengths
between violet and red. Consequently, a rainbow-like dispersion of the colors would be observed
to either side of the central fringe on a screen, as can be seen in Figure 27.35. This drawing shows that the spectrum of colors associated with the m = 2 order is completely separate from
798 CHAPTER 27 Interference and the Wave Nature of Light
the spectrum of the m = 1 order. For higher orders, however, the spectra from adjacent orders may overlap (see Problems 51 and 61). The central maximum (m = 0) is white because all the colors overlap there.
THE PHYSICS OF . . . a grating spectroscope. An instrument designed to measure the angles at which the principal maxima of a grating occur is called a grating spectroscope. With
a measured value of the angle, calculations such as those in Example 9 can be turned around to
provide the corresponding value of the wavelength. As we will discuss in Chapter 30, the atoms
in a hot gas emit discrete wavelengths, and determining the values of these wavelengths is one
important technique used to identify the atoms. Figure 27.36 shows the principle of a grating spectroscope. The slit that admits light from the source (e.g., a hot gas) is located at the focal
point of the collimating lens, so the light rays striking the grating are parallel. The telescope is
used to detect the bright fringes and, hence, to measure the angle 𝜃.
Check Your Understanding
(The answers are given at the end of the book.) 20. CYU Figure 27.3 shows a top view of a dif-
fraction grating and the mth-order principal maxima that are obtained with red and blue
light. Red light has the longer wavelength.
(a) Which principal maximum is associated with blue light, the one farther from or the one
closer to the central maximum? (b) If the num- ber of slits per centimeter in the grating were
increased, would these two principal maxima
move away from the central maximum, move
toward the central maximum, or remain in the
same place?
21. What would happen to the distance between the bright fringes produced by a diff raction grating if the entire interference apparatus (light source, grating, and screen) were immersed in water?
27.8 *Compact Discs, Digital Video Discs, and the Use of Interference The compact disc (CD) and the digital video disc (DVD) have revolutionized how text, graphics,
music, and movies are stored for use in computers, stereo sound systems, and televisions. The
operation of these discs uses interference eff ects in some interesting ways. Each disc contains a
spiral track that holds the information, which is detected using a laser beam that refl ects from the
bottom of the disc, as Figure 27.37 illustrates. The information is encoded in the form of raised areas on the bottom of the disc. Under a microscope these raised areas appear as “pits” when
viewed from the top or labeled side of the disc. They are separated by fl at areas called “land.” The pits and land are covered with a transparent plastic coating, which has been omitted from the
drawing for simplicity.
THE PHYSICS OF . . . retrieving information from compact discs and digital video discs. As the disc rotates, the laser beam refl ects off the bottom and into a detector. The refl ected light intensity fl uctuates as the pits and land areas pass by, and the fl uctuations
convey the information as a series of binary numbers (zeros and ones). To make the fl uctuations
easier to detect, the pit thickness t (see Figure 27.37) is chosen with destructive interference in mind. As the laser beam overlaps the edges of a pit, part of the beam is refl ected from the raised
pit surface and part from the land. The part that refl ects from the land travels an additional dis-
tance of 2t. The thickness of the pits is chosen so that 2t is one-half of a wavelength of the laser beam in the plastic coating. With this choice, destructive interference occurs when the two parts
of the refl ected beam combine. As a result, there is markedly less refl ected intensity when the
laser beam passes over a pit edge than when it passes over other places on the surface. Thus, the
Sunlight
m = 3 m = 3m = 2 m = 2
m = 1 m = 1
FIGURE 27.35 When sunlight falls on a diff raction grating, a rainbow of colors is
produced at each principal maximum (m = 1, 2, . . .). The central maximum (m = 0), how- ever, is white but is not shown in the drawing.
Collimating lens
Grating
Telescope
Source of light
Slit 𝜃
FIGURE 27.36 A grating spectroscope.
mth-order maxima
Diffraction grating
Screen
Central maximum (m = 0)
𝜃
CYU FIGURE 27.3
Spiral track
Laser beam incident on bottom side
of disc
Bottom side of disc
LandPit
t
FIGURE 27.37 The bottom surface of a compact disc (CD) or digital video disc
(DVD) carries information in the form of
raised areas (“pits”) and fl at areas (“land”)
along a spiral track. A CD or DVD is played
by using a laser beam that strikes the bottom
surface and refl ects from it.
27.9 X-Ray Diff raction 799
fl uctuations in refl ected light that occur while the disc rotates are large enough to detect because
of the eff ects of destructive interference. Example 10 determines the theoretical thickness of the
pits on a compact disc. In reality, a value slightly less than that obtained in the example is used
for technical reasons that are not pertinent here.
EXAMPLE 10 Pit Thickness on a Compact Disc
The laser in a CD player has a wavelength of 780 nm in a vacuum. The
plastic coating over the pits has an index of refraction of n = 1.5. Find the thickness of the pits on a CD.
Reasoning As we have discussed, the thickness t is chosen so that 2t = 12λcoating in order to achieve destructive interference. Equation 27.3 gives the wavelength in the plastic coating as 𝜆coating = 𝜆vacuum/n.
Solution The thickness of the pits is
t = λcoating
4 =
λvacuum 4n
= 780 × 10−9 m
4(1.5) = 1.3 × 10 −7 m
The pit thickness calculated in Example 10 applies only to a CD. The pit thickness (and other
dimensions as well) are smaller on a DVD because the lasers used for DVDs have smaller wave-
lengths (635 nm, for example). The fact that the pit dimensions are smaller is one of the reasons
that a DVD can store more information than a CD can—from 7 to 26 times more, depending on
the type of DVD.
THE PHYSICS OF . . . the three-beam tracking method for compact discs. As a CD or DVD rotates, the laser beam must accurately follow or track the pits and the land along
the spiral. One method that has been used to ensure accurate tracking for CDs is the three-beam
method, in which a diff raction grating is the key element, as Figure 27.38 shows. Before the laser beam strikes the CD, the beam passes through a grating that produces a central maximum and
two fi rst-order maxima, one on either side. As the picture indicates, the central maximum beam
falls directly on the spiral track. This beam refl ects into a detector, and the refl ected light intensity
fl uctuates as the pits and land areas pass by, the fl uctuations conveying the information. The two
fi rst-order maxima beams are called tracking beams. They hit the CD between the arms of the spiral and also refl ect into detectors of their own. Under perfect conditions, the intensities of
the two refl ected tracking beams do not fl uctuate, since they originate from the smooth surface
between the arms of the spiral where there are no pits. As a result, each tracking-beam detec-
tor puts out the same constant electrical signal. However, if the tracking drifts to either side, the
refl ected intensity of each tracking beam changes because of the pits. In response, the tracking-
beam detectors produce diff erent electrical signals. The diff erence between the signals is used in a
“feedback” circuit to correct for the drift and put the three beams back into their proper positions.
27.9 X-Ray Diff raction THE PHYSICS OF . . . X-ray diff raction. Not all diff raction gratings are commercially made. Nature also creates diff raction gratings, although these gratings do not look like an array of
closely spaced slits. Instead, nature’s gratings are the arrays of regularly spaced atoms that exist
in crystalline solids. For example, Figure 27.39 shows the structure of a crystal of ordinary salt (NaCl). Typically, the atoms in a crystalline solid are separated by distances of about 1.0 × 10−10 m,
so we might expect a crystalline array of atoms to act like a grating with roughly this “slit” spac-
ing for electromagnetic waves of the appropriate wavelength. Assuming that sin 𝜃 = 0.5 and that m = 1 in Equation 27.7, then 0.5 = 𝜆/d. A value of d = 1.0 × 10−10 m in this equation gives a wavelength of 𝜆 = 0.5 × 10−10 m. This wavelength is much shorter than that of visible light and falls in the X-ray region of the electromagnetic spectrum. (See Figure 24.9.)
A diff raction pattern does indeed result when X-rays are directed onto a crystalline mate-
rial, as Figure 27.40a illustrates for a crystal of NaCl. The pattern consists of a complicated arrangement of spots because a crystal has a complex three-dimensional structure. It is from
Central maximum beam
First-order maximum
tracking beam
First-order maximum
tracking beam
Diffraction grating
Laser
FIGURE 27.38 A three-beam tracking method has been used in CD players to
ensure that the laser follows the spiral track
correctly. The three beams are derived from a
single laser beam with the aid of a diff raction
grating.
800 CHAPTER 27 Interference and the Wave Nature of Light
patterns such as this that the spacing between atoms and the nature of the crystal structure can be
determined. X-ray diff raction has also been applied with great success toward understanding the
structure of biologically important molecules, such as proteins and nucleic acids. One of the most
famous results was the discovery in 1953 by James Watson and Francis Crick that the structure of
the nucleic acid DNA is a double helix. X-ray diff raction patterns such as that in Figure 27.40b played the pivotal role in their research.
FIGURE 27.39 In this drawing of the crys- talline structure of sodium chloride, the small
red spheres represent positive sodium ions,
and the large blue spheres represent negative
chloride ions.
FIGURE 27.40 The X-ray diff raction patterns of (a) crystalline NaCl and (b) DNA. The image of DNA was obtained by Rosalind Franklin in 1953.
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EXAMPLE 11 BIO Predator or Prey? Pupils of Diff erent Shapes
As discussed earlier in the chapter, pupils with diff erent shapes will aff ect
an animal’s optical resolution along diff erent directions. Some animals,
like goats, and other large herbivores, have horizontal pupils, while others,
like cats and crocodiles, have vertical pupils (Figure 27.41). Recent research suggests that animals that are ambush predators tend to have
pupils with vertical slits, while plant-eating prey species have horizontal
slits located near the sides of their heads. This is especially true for ani-
mals whose heads are close to the ground (i.e., grazing animals and small
predators). Suppose a goat’s eye has a horizontal, rectangular pupil that
has a width-to-height ratio of 5:1. If the goat can optically resolve two-
closely spaced objects separated by a distance s in the horizontal direc- tion, how much closer would the objects have to be moved toward the goat
for it to distinguish them in the vertical direction?
Reasoning We can apply Rayleigh’s criterion for resolution (Equation 27.6) to the pupil in both directions.
Solution Beginning with Equation 27.6, we see that the minimum angle for resolution is inversely related to the pupil diameter:
θmin ∝ 1
D .
Using Equation 8.1, we can write the angle in terms of the separation
distance (s) between the two objects and the distance from the objects (r): s r
∝ 1
D .
Rearranging this equation for r, we have: r ∝ sD. Notice that the distance to the objects is directly proportional to the pupil diameter. Therefore,
the objects would have to be moved fi ve times closer for the goat to re-
solve them in the vertical direction. The goat’s greater optical resolution
in the horizontal direction allows it to detect predators along the ground
at greater distances.
FIGURE 27.41 The pupils of animals come in all shapes and sizes. Some are horizontal,
such as in the goat, and others are vertical,
such as in the domestic cat and crocodile.
The shape of the pupil will aff ect the optical
resolution of the eyes in diff erent directions.
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Concept Summary 801
Concept Summary 27.1 The Principle of Linear Superposition The principle of linear su- perposition states that when two or more waves are present simultaneously in
the same region of space, the resultant disturbance is the sum of the disturb-
ances from the individual waves.
Constructive interference occurs at a point when two waves meet there
crest-to-crest and trough-to-trough, thus reinforcing each other. When two
waves that start out in phase and have traveled some distance meet at a point,
constructive interference occurs whenever the travel distances are the same
or diff er by any integer number of wavelengths: ℓ2 − ℓ1 = m𝜆, where ℓ1 and ℓ2 are the distances traveled by the waves, and m = 0, 1, 2, 3, . . . .
Destructive interference occurs at a point when two waves meet there
crest-to-trough, thus mutually canceling each other. When two waves that
start out in phase and have traveled some distance meet at a point, destructive
interference occurs whenever the travel distances diff er by any odd integer
number of half-wavelengths: ℓ2 − ℓ1 = (m + 1
2)𝜆, where ℓ1 and ℓ2 are the distances traveled by the waves, and m = 0, 1, 2, 3, . . . .
Two sources are coherent if the waves they emit maintain a constant phase
relation. In other words, the waves do not shift relative to one another as time
passes. If constructive and destructive interference are to be observed, coher-
ent sources are necessary.
27.2 Young’s Double-Slit Experiment In Young’s double-slit experi- ment, light passes through a pair of closely spaced narrow slits and produces
a pattern of alternating bright and dark fringes on a viewing screen. The
fringes arise because of constructive and destructive interference. The angle
𝜃 that locates the mth-order bright fringe is given by Equation 27.1, where 𝜆 is the wavelength of the light, and d is the spacing between the slits. The angle that locates the mth dark fringe is given by Equation 27.2.
sin θ = mλ d
m = 0, 1, 2, 3, . . . (27.1)
sin θ = (m + 12 )λ
d m = 0, 1, 2, 3, . . . (27.2)
27.3 Thin-Film Interference Constructive and destructive interference of light waves can occur with thin fi lms of transparent materials. The interfer-
ence occurs between light waves that refl ect from the top and bottom surfaces
of the fi lm. One important factor in thin-fi lm interference is the thickness of
a fi lm relative to the wavelength of the light within the fi lm. The wavelength
𝜆fi lm within a fi lm is given by Equation 27.3, where 𝜆vacuum is the wavelength in a vacuum, and n is the index of refraction of the fi lm.
λfilm = λvacuum
n (27.3)
A second important factor is the phase change that can occur when light
refl ects at each surface of the fi lm:
1. When light travels through a material with a smaller index of refrac- tion toward a material with a larger index of refraction, refl ection at the boundary occurs along with a phase change that is equivalent to one-half a wavelength in the fi lm.
2. When light travels through a material with a larger index of refraction toward a material with a smaller index of refraction, there is no phase change upon refl ection at the boundary.
27.4 The Michelson Interferometer An interferometer is an instrument that can be used to measure the wavelength of light by employing interference
between two light waves. The Michelson interferometer splits the light into
two beams. One beam travels to a fi xed mirror, refl ects from it, and returns.
The other beam travels to a movable mirror, refl ects from it, and returns.
When the two returning beams are combined, interference is observed, the
amount of which depends on the travel distances.
27.5 Diff raction Diff raction is the bending of waves around obstacles or around the edges of an opening. Diff raction is an interference eff ect that can
be explained with the aid of Huygens’ principle. This principle states that
every point on a wave front acts as a source of tiny wavelets that move for-
ward with the same speed as the wave; the wave front at a later instant is the
surface that is tangent to the wavelets.
When light passes through a single narrow slit and falls on a viewing
screen, a pattern of bright and dark fringes is formed because of the superpo-
sition of Huygens wavelets. The angle 𝜃 that specifi es the mth dark fringe on either side of the central bright fringe is given by Equation 27.4, where 𝜆 is the wavelength of the light and W is the width of the slit.
sin θ = m λ W m = 1, 2, 3, . . . (27.4)
27.6 Resolving Power The resolving power of an optical instrument is the ability of the instrument to distinguish between two closely spaced objects.
Resolving power is limited by the diff raction that occurs when light waves
enter an instrument, often through a circular opening.
The Rayleigh criterion specifi es that two point objects are just resolved
when the fi rst dark fringe in the diff raction pattern of one falls directly on
the central bright fringe in the diff raction pattern of the other. According
to this specifi cation, the minimum angle (in radians) that two point objects
can subtend at a circular aperture of diameter D and still be resolved as separate objects is given by Equation 27.6, where 𝜆 is the wavelength of the light.
θmin ≈ 1.22 λ D (θmin in radians) (27.6)
27.7 The Diff raction Grating A diff raction grating consists of a large number of parallel, closely spaced slits. When light passes through a dif-
fraction grating and falls on a viewing screen, the light forms a pattern
of bright and dark fringes. The bright fringes are referred to as principal
maxima and are found at an angle 𝜃 that is specifi ed by Equation 27.7, where 𝜆 is the wavelength of the light and d is the separation between two adjacent slits.
sin θ = m λ d m = 0, 1, 2, 3, . . . (27.7)
27.8 Compact Discs, Digital Video Discs, and the Use of Interference Compact discs and digital video discs depend on interference for their
operation.
27.9 X-Ray Diff raction A diff raction pattern forms when X-rays are dir- ected onto a crystalline material. The pattern arises because the regularly
spaced atoms in a crystal act like a diff raction grating. Because the spacing
is extremely small, on the order of 1 × 10−10 m, the wavelength of the elec-
tromagnetic waves must also be very small—hence, the use of X-rays. The
crystal structure of a material can be determined from its X-ray diff raction
pattern.
802 CHAPTER 27 Interference and the Wave Nature of Light
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 27.1 The Principle of Linear Superposition 1. The two loudspeakers in the drawing are producing identical sound waves. The waves spread out and overlap at the point P. What is the diff erence ℓ2 − ℓ1 in the two path lengths if point P is at the third sound intensity minimum from the central sound intensity maximum? Express this diff erence in terms
of the wavelength 𝜆 of the sound. (a) 12𝜆 (b) 𝜆 (c) 3
2𝜆 (d) 3𝜆 (e) 5
2𝜆
QUESTION 1
Central maximum
1
2
Pℓ
ℓ
Section 27.2 Young’s Double-Slit Experiment 2. In a certain Young’s double-slit experiment, a diff raction pattern is formed on a distant screen, as the drawing shows. The angle that locates a
given bright fringe is small, so that the approximation sin 𝜃 ≈ 𝜃 is valid. As- suming that 𝜃 remains small, by what factor does it change if the wavelength 𝜆 is doubled and the slit separation d is doubled? (a) The angle does not change. (b) The angle increases by a factor of 2. (c) The angle increases by a factor of 4. (d) The angle decreases by a factor of 2. (e) The angle decreases by a factor of 4.
QUESTION 2
Bright fringe
Double slit
𝜃
Section 27.3 Thin-Film Interference 6. Light of wavelength 600 nm in vacuum is incident nearly perpendicularly on a thin fi lm whose index of refraction is 1.5. The light travels from the top
surface of the fi lm to the bottom surface, refl ects from the bottom surface,
and returns to the top surface, as the drawing indicates. How far has the light
traveled inside the fi lm? Express your answer in terms of the wavelength 𝜆fi lm of the light within the fi lm. (a) 2𝜆fi lm (b) 3𝜆fi lm (c) 4𝜆fi lm (d) 6𝜆fi lm (e) 12𝜆fi lm
QUESTION 6
Light
1200 nm
8. Light is incident perpendicularly on four transparent fi lms of diff erent thickness. The thickness of each fi lm is given in the drawings in terms of
the wavelength 𝜆fi lm of the light within the fi lm. The index of refraction of each fi lm is 1.5, and each is surrounded by air. Which fi lm (or fi lms)
will appear bright due to constructive interference when viewed from the
top surface, upon which the light is incident? (a) 1, 2, 3, 4 (b) 2, 3 (c) 3 (d) 3, 4 (e) 4
Light
1 2 3 4
film 1.5 film
2 film film 1–– 4
𝜆 𝜆 𝜆 𝜆
QUESTION 8
Section 27.5 Diff raction 12. Light passes through a single slit. If the width of the slit is reduced, what happens to the width of the central bright fringe? (a) The width of the central bright fringe does not change, because it depends only on the
wavelength of the light and not on the width of the slit. (b) The central bright fringe becomes wider, because the angle that locates the fi rst dark
fringe on either side of the central bright fringe becomes smaller. (c) The central bright fringe becomes wider, because the angle that locates the
fi rst dark fringe on either side of the central bright fringe becomes larger.
(d) The central bright fringe becomes narrower, because the angle that loc- ates the fi rst dark fringe on either side of the central bright fringe becomes
larger. (e) The central bright fringe becomes narrower, because the angle that locates the fi rst dark fringe on either side of the central bright fringe
becomes smaller.
13. Light of wavelength 𝜆 passes through a single slit of width W and forms a diff raction pattern on a viewing screen. If this light is then replaced by
light of wavelength 2𝜆, the original diff raction pattern is exactly reproduced if the width of the slit ______. (a) is changed to 14W (b) is changed to
1
2W (c) is changed to 2W (d) is changed to 4W (e) remains the same—no change is necessary
Section 27.6 Resolving Power 15. Suppose that you are using a microscope to view two closely spaced cells. For a given lens diameter, which color of light would you use to achieve
the best possible resolving power? (a) Red (b) Yellow (c) Green (d) Blue (e) All the colors give the same resolving power.
Section 27.7 The Diff raction Grating 18. A diff raction grating is illuminated with yellow light. The diff raction pattern seen on a viewing screen consists of three yellow bright fringes, one
at the central maximum (𝜃 = 0°) and one on either side of it at 𝜃 = ±50°. Then the grating is simultaneously illuminated with red light. Where a red
and a yellow fringe overlap, an orange fringe is produced. The new pattern
consists of _________. (a) only red fringes at 0° and ±50° (b) only yellow fringes at 0° and ±50° (c) only orange fringes at 0° and ±50° (d) an orange fringe at 0°, yellow fringes at ±50°, and red fringes farther out (e) an orange fringe at 0°, yellow fringes at ±50°, and red fringes closer in
Focus on Concepts
Problems 803
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 27.1 The Principle of Linear Superposition,
Section 27.2 Young’s Double-Slit Experiment 1. E SSM In a Young’s double-slit experiment, the wavelength of the light used is 520 nm (in vacuum), and the separation between the slits is 1.4 ×
10−6 m. Determine the angle that locates (a) the dark fringe for which m = 0, (b) the bright fringe for which m = 1, (c) the dark fringe for which m = 1, and (d) the bright fringe for which m = 2. 2. E In a Young’s double-slit experiment, the angle that locates the second dark fringe on either side of the central bright fringe is 5.4°. Find the ratio d/𝜆 of the slit separation d to the wavelength 𝜆 of the light. 3. E Two in-phase sources of waves are separated by a distance of 4.00 m. These sources produce identical waves that have a wavelength of 5.00 m.
On the line between them, there are two places at which the same type of
interference occurs. (a) Is it constructive or destructive interference, and (b) where are the places located? 4. E The dark fringe for m = 0 in a Young’s double-slit experiment is located at an angle of 𝜃 = 15°. What is the angle that locates the dark fringe for m = 1? 5. E V-HINT In a Young’s double-slit experiment, the seventh dark fringe is located 0.025 m to the side of the central bright fringe on a fl at screen, which
is 1.1 m away from the slits. The separation between the slits is 1.4 × 10−4 m.
What is the wavelength of the light being used?
6. E GO MMH Two parallel slits are illuminated by light composed of two wavelengths. One wavelength is 𝜆A = 645 nm. The other wavelength is 𝜆B and is unknown. On a viewing screen, the light with wavelength 𝜆A = 645 nm produces its third-order bright fringe at the same place where the light with
wavelength 𝜆B produces its fourth dark fringe. The fringes are counted re- lative to the central or zeroth-order bright fringe. What is the unknown
wavelength?
7. E GO In a setup like that in Figure 27.7, a wavelength of 625 nm is used in a Young’s double-slit experiment. The separation between the slits is d = 1.4 × 10−5 m. The total width of the screen is 0.20 m. In one version of the
setup, the separation between the double slit and the screen is LA = 0.35 m, whereas in another version it is LB = 0.50 m. On one side of the central bright fringe, how many bright fringes lie on the screen in the two versions of the
setup? Do not include the central bright fringe in your counting.
8. M V-HINT At most, how many bright fringes can be formed on either side of the central bright fringe when light of wavelength 625 nm falls on a double
slit whose slit separation is 3.76 × 10−6 m?
9. M CHALK MMH In a Young’s double-slit experiment the separation y between the second-order bright fringe and the central bright fringe on a fl at
screen is 0.0180 m when the light has a wavelength of 425 nm. Assume that
the angles that locate the fringes on the screen are small enough so that sin
𝜃 ≈ tan 𝜃. Find the separation y when the light has a wavelength of 585 nm.
10. H In Young’s experiment a mixture of orange light (611 nm) and blue light (471 nm) shines on the double slit. The centers of the fi rst-order bright
blue fringes lie at the outer edges of a screen that is located 0.500 m away
from the slits. However, the fi rst-order bright orange fringes fall off the
screen. By how much and in which direction (toward or away from the slits)
should the screen be moved so that the centers of the fi rst-order bright orange
fringes will just appear on the screen? It may be assumed that 𝜃 is small, so that sin 𝜃 ≈ tan 𝜃. 11. H SSM A sheet that is made of plastic (n = 1.60) covers one slit of a double slit (see the drawing). When the double slit is illuminated by mono-
chromatic light (𝜆vacuum = 586 nm), the center of the screen appears dark rather than bright. What is the minimum thickness of the plastic?
PROBLEM 11 Plastic
t
Section 27.3 Thin-Film Interference 12. E You are standing in air and are looking at a fl at piece of glass (n = 1.52) on which there is a layer of transparent plastic (n = 1.61). Light whose wavelength is 589 nm in vacuum is incident nearly perpendicularly on the
coated glass and refl ects into your eyes. The layer of plastic looks dark. Find
the two smallest possible nonzero values for the thickness of the layer.
13. E SSM A nonrefl ective coating of magnesium fl uoride (n = 1.38) covers the glass (n = 1.52) of a camera lens. Assuming that the coating prevents refl ection of yellow-green light (wavelength in vacuum = 565 nm), determine
the minimum nonzero thickness that the coating can have.
14. E GO When monochromatic light shines perpendicularly on a soap fi lm (n = 1.33) with air on each side, the second smallest nonzero fi lm thickness for which destructive interference of refl ected light is observed is 296 nm.
What is the vacuum wavelength of the light in nm?
15. E MMH A transparent fi lm (n = 1.43) is deposited on a glass plate (n = 1.52) to form a nonrefl ecting coating. The fi lm has a thickness that is 1.07 × 10−7 m. What is the longest possible wavelength (in vacuum) of light
for which this fi lm has been designed?
16. E GO A tank of gasoline (n = 1.40) is open to the air (n = 1.00). A thin fi lm of liquid fl oats on the gasoline and has a refractive index that is between
1.00 and 1.40. Light that has a wavelength of 625 nm (in vacuum) shines
perpendicularly down through the air onto this fi lm, and in this light the fi lm
looks bright due to constructive interference. The thickness of the fi lm is
242 nm and is the minimum nonzero thickness for which constructive inter-
ference can occur. What is the refractive index of the fi lm?
17. E V-HINT Review Conceptual Example 4 before beginning this prob- lem. A soap fi lm with diff erent thicknesses at diff erent places has an un-
known refractive index n and air on both sides. In refl ected light it looks multicolored. One region looks yellow because destructive interference has
removed blue (𝜆vacuum = 469 nm) from the refl ected light, while another looks magenta because destructive interference has removed green (𝜆vacuum = 555 nm).
Problems
804 CHAPTER 27 Interference and the Wave Nature of Light
In these regions the fi lm has the minimum nonzero thickness t required for the destructive interference to occur. Find the ratio tmagenta/tyellow. 18. M MMH A fi lm of oil lies on wet pavement. The refractive index of the oil exceeds that of the water. The fi lm has the minimum nonzero thickness
such that it appears dark due to destructive interference when viewed in red
light (wavelength = 640.0 nm in vacuum). Assuming that the visible spec-
trum extends from 380 to 750 nm, for which visible wavelength(s) in vacuum
will the fi lm appear bright due to constructive interference?
19. M CHALK SSM Orange light (𝜆vacuum = 611 nm) shines on a soap fi lm (n = 1.33) that has air on either side of it. The light strikes the fi lm perpen- dicularly. What is the minimum thickness of the fi lm for which constructive
interference causes it to look bright in refl ected light?
20. M V-HINT Available in WileyPLUS. 21. H Available in WileyPLUS. 22. H MMH Available in WileyPLUS.
Section 27.5 Diff raction 23. E (a) As Section 17.3 discusses, high-frequency sound waves exhibit less diff raction than low-frequency sound waves do. However, even high-
frequency sound waves exhibit much more diff raction under normal circum-
stances than do light waves that pass through the same opening. The highest
frequency that a healthy ear can typically hear is 2.0 × 104 Hz. Assume that
a sound wave with this frequency travels at 343 m/s and passes through a
doorway that has a width of 0.91 m. Determine the angle that locates the fi rst
minimum to either side of the central maximum in the diff raction pattern for
the sound. This minimum is equivalent to the fi rst dark fringe in a single-slit
diff raction pattern for light. (b) Suppose that yellow light (wavelength = 580 nm in vacuum) passes through a doorway and that the fi rst dark fringe in its
diff raction pattern is located at the angle determined in part (a). How wide
would this hypothetical doorway have to be?
24. E A dark fringe in the diff raction pattern of a single slit is located at an angle of 𝜃A = 34°. With the same light, the same dark fringe formed with another single slit is at an angle of 𝜃B = 56°. Find the ratio WA/WB of the widths of the two slits.
25. E SSM A diff raction pattern forms when light passes through a single slit. The wavelength of the light is 675 nm. Determine the angle that locates the fi rst
dark fringe when the width of the slit is (a) 1.8 × 10−4 m and (b) 1.8 × 10−6 m. 26. E GO A slit has a width of W1 = 2.3 × 10−6 m. When light with a wavelength of 𝜆1 = 510 nm passes through this slit, the width of the central bright fringe on a fl at observation screen has a certain value. With the screen
kept in the same place, this slit is replaced with a second slit (width W2), and a wavelength of 𝜆2 = 740 nm is used. The width of the central bright fringe on the screen is observed to be unchanged. Find W2. 27. E SSM Light that has a wavelength of 668 nm passes through a slit 6.73 × 10−6 m wide and falls on a screen that is 1.85 m away. What is the
distance on the screen from the center of the central bright fringe to the third
dark fringe on either side?
28. E GO Light shines through a single slit whose width is 5.6 × 10−4 m. A diff raction pattern is formed on a fl at screen located 4.0 m away. The distance
between the middle of the central bright fringe and the fi rst dark fringe is
3.5 mm. What is the wavelength of the light?
29. M V-HINT Light waves with two diff erent wavelengths, 632 nm and 474 nm, pass simultaneously through a single slit whose width is 7.15 ×
10−5 m and strike a screen 1.20 m from the slit. Two diff raction patterns are
formed on the screen. What is the distance (in cm) between the common
center of the diff raction patterns and the fi rst occurrence of a dark fringe from
one pattern falling on top of a dark fringe from the other pattern?
30. M GO The central bright fringe in a single-slit diff raction pattern has a width that equals the distance between the screen and the slit. Find the ratio
𝜆/W of the wavelength 𝜆 of the light to the width W of the slit.
31. M SSM How many dark fringes will be produced on either side of the central maximum if light (𝜆 = 651 nm) is incident on a single slit that is 5.47 × 10−6 m wide?
32. H In a single-slit diff raction pattern, the central fringe is 450 times as wide as the slit. The screen is 18 000 times farther from the slit than the slit
is wide. What is the ratio 𝜆/W, where 𝜆 is the wavelength of the light shining through the slit and W is the width of the slit? Assume that the angle that locates a dark fringe on the screen is small, so that sin 𝜃 ≈ tan 𝜃.
Section 27.6 Resolving Power 33. E Two stars are 3.7 × 1011 m apart and are equally distant from the earth. A telescope has an objective lens with a diameter of 1.02 m and just
detects these stars as separate objects. Assume that light of wavelength 550
nm is being observed. Also assume that diff raction eff ects, rather than at-
mospheric turbulence, limit the resolving power of the telescope. Find the
maximum distance that these stars could be from the earth.
34. E BIO It is claimed that some professional baseball players can see which way the ball is spinning as it travels toward home plate. One way to
judge this claim is to estimate the distance at which a batter can fi rst hope to
resolve two points on opposite sides of a baseball, which has a diameter of
0.0738 m. (a) Estimate this distance, assuming that the pupil of the eye has a diameter of 2.0 mm and the wavelength of the light is 550 nm in vacuum.
(b) Considering that the distance between the pitcher’s mound and home plate is 18.4 m, can you rule out the claim based on your answer to part (a)?
35. E BIO CHALK SSM Late one night on a highway, a car speeds by you and fades into the distance. Under these conditions the pupils of your eyes
have diameters of about 7.0 mm. The taillights of this car are separated by a
distance of 1.2 m and emit red light (wavelength = 660 nm in vacuum). How
far away from you is this car when its taillights appear to merge into a single
spot of light because of the eff ects of diff raction?
36. E GO An inkjet printer uses tiny dots of red, green, and blue ink to produce an image. Assume that the dot separation on the printed page is the same for all
colors. At normal viewing distances, the eye does not resolve the individual
dots, regardless of color, so that the image has a normal look. The wavelengths
for red, green, and blue are 𝜆red = 660 nm, 𝜆green = 550 nm, and 𝜆blue = 470 nm. The diameter of the pupil through which light enters the eye is 2.0 mm. For a
viewing distance of 0.40 m, what is the maximum allowable dot separation?
37. E BIO GO A hunter who is a bit of a braggart claims that from a dis- tance of 1.6 km he can selectively shoot either of two squirrels who are sitting
ten centimeters apart on the same branch of a tree. What’s more, he claims
that he can do this without the aid of a telescopic sight on his rifl e. (a) De- termine the diameter of the pupils of his eyes that would be required for him
to be able to resolve the squirrels as separate objects. In this calculation use a
wavelength of 498 nm (in vacuum) for the light. (b) State whether his claim is reasonable, and provide a reason for your answer. In evaluating his claim,
consider that the human eye automatically adjusts the diameter of its pupil
over a typical range of 2 to 8 mm, the larger values coming into play as the
lighting becomes darker. Note also that under dark conditions, the eye is most
sensitive to a wavelength of 498 nm.
38. E BIO Review Conceptual Example 8 as background for this problem. In addition to the data given there, assume that the dots in the painting are
separated by 1.5 mm and that the wavelength of the light is 𝜆vacuum = 550 nm. Find the distance at which the dots can just be resolved by (a) the eye and (b) the camera. 39. E V-HINT Astronomers have discovered a planetary system orbiting the star Upsilon Andromedae, which is at a distance of 4.2 × 1017 m from the
earth. One planet is believed to be located at a distance of 1.2 × 1011 m from
the star. Using visible light with a vacuum wavelength of 550 nm, what is the
minimum necessary aperture diameter that a telescope must have so that it
can resolve the planet and the star?
Additional Problems 805
40. M BIO GO The pupil of an eagle’s eye has a diameter of 6.0 mm. Two fi eld mice are separated by 0.010 m. From a distance of 176 m, the eagle sees
them as one unresolved object and dives toward them at a speed of 17 m/s.
Assume that the eagle’s eye detects light that has a wavelength of 550 nm in
vacuum. How much time passes until the eagle sees the mice as separate objects?
41. M SSM MMH Available in WileyPLUS. 42. H Available in WileyPLUS.
Section 27.7 The Diff raction Grating,
Section 27.8 Compact Discs, Digital Video Discs, and the Use of Interference 43. E SSM A diff raction grating is 1.50 cm wide and contains 2400 lines. When used with light of a certain wavelength, a third-order maximum is
formed at an angle of 18.0°. What is the wavelength (in nm)?
44. E The light shining on a diff raction grating has a wavelength of 495 nm (in vacuum). The grating produces a second-order bright fringe whose posi-
tion is defi ned by an angle of 9.34°. How many lines per centimeter does the
grating have?
45. E For a wavelength of 420 nm, a diff raction grating produces a bright fringe at an angle of 26°. For an unknown wavelength, the same grating pro-
duces a bright fringe at an angle of 41°. In both cases the bright fringes are of
the same order m. What is the unknown wavelength? 46. E GO Two diff raction gratings, A and B, are located at the same dis- tance from the observation screens. Light with the same wavelength 𝜆 is used for each. The separation between adjacent principal maxima for grating A is
2.7 cm, and for grating B it is 3.2 cm. Grating A has 2000 lines per meter.
How many lines per meter does grating B have? (Hint: The diff raction angles are small enough that the approximation sin 𝜃 ≈ tan 𝜃 can be used.) 47. E SSM The wavelength of the laser beam used in a compact disc player is 780 nm. Suppose that a diff raction grating produces fi rst-order tracking
beams that are 1.2 mm apart at a distance of 3.0 mm from the grating. Estim-
ate the spacing between the slits of the grating.
48. E The fi rst-order principle maximum produced by a grating is located at an angle of 𝜃 = 18.0°. What is the angle for the third-order maximum with the same light?
49. M V-HINT A diff raction grating has 2604 lines per centimeter, and it produces a principal maximum at 𝜃 = 30.0°. The grating is used with light that contains all wavelengths between 410 and 660 nm. What is (are) the
wavelength(s) of the incident light that could have produced this maximum?
50. M GO Light of wavelength 410 nm (in vacuum) is incident on a diff rac- tion grating that has a slit separation of 1.2 × 10−5 m. The distance between
the grating and the viewing screen is 0.15 m. A diff raction pattern is pro-
duced on the screen that consists of a central bright fringe and higher-order
bright fringes (see the drawing). (a) Determine the distance y from the central bright fringe to the second-order bright fringe. (Hint: The diff raction angles are small enough that the approximation tan 𝜃 ≈ sin 𝜃 can be used.) (b) If the entire apparatus is submerged in water (nwater = 1.33), what is the distance y?
2nd-order maximum
Diffraction grating
Screen
Central maximum (m = 0)
y
L
𝜃
PROBLEM 50
51. M SSM Violet light (wavelength = 410 nm) and red light (wavelength = 660 nm) lie at opposite ends of the visible spectrum. (a) For each wavelength, fi nd the angle 𝜃 that locates the fi rst-order maximum produced by a grating with 3300 lines/cm. This grating converts a mixture of all colors between
violet and red into a rainbow-like dispersion between the two angles. Repeat
the calculation above for (b) the second-order maximum and (c) the third- order maximum. (d) From your results, decide whether there is an overlap between any of the “rainbows” and, if so, specify which orders overlap.
52. H Available in WileyPLUS. 53. H Available in WileyPLUS.
54. E GO A soap fi lm (n = 1.33) is 465 nm thick and lies on a glass plate (n = 1.52). Sunlight, whose wavelengths (in vacuum) extend from 380 to 750 nm, travels through the air and strikes the fi lm perpendicularly. For
which wavelength(s) in this range does destructive interference cause the fi lm
to look dark in refl ected light?
55. E SSM In a Young’s double-slit experiment, two rays of monochromatic light emerge from the slits and meet at a point on a distant screen, as in Figure 27.6a. The point on the screen where these two rays meet is the eighth-order bright fringe. The diff erence in the distances that the two rays travel is 4.57 ×
10−6 m. What is the wavelength (in nm) of the monochromatic light?
56. E GO Point A is the midpoint of one of the sides of a square. On the side opposite this spot, two in-phase loudspeakers are located at adjacent corners,
as shown in the fi gure. Standing at point A you hear a loud sound because
of constructive interference between the identical sound waves coming from
the speakers. As you walk along the side of the square toward either empty
corner, the loudness diminishes gradually to nothing and then increases again
until you hear a maximally loud sound at the corner. If the length of each side
of the square is 4.6 m, fi nd the wavelength of the sound waves.
PROBLEM 56
A
57. E SSM Available in WileyPLUS. 58. E GO A fl at screen is located 0.60 m away from a single slit. Light with a wavelength of 510 nm (in vacuum) shines through the slit and produces
a diff raction pattern. The width of the central bright fringe on the screen is
0.050 m. What is the width of the slit?
Additional Problems
806 CHAPTER 27 Interference and the Wave Nature of Light
59. E BIO A large group of football fans comes to the game with colored cards that spell out the name of their team when held upsimultaneously. Most
of the cards are colored blue (𝜆vacuum = 480 nm). When displayed, the average distance between neighboring cards is 5.0 cm. If the cards are to blur together
into solid blocks of color when viewed by a spectator at the other end of the
stadium (160 m away), what must be the maximum diameter (in mm) of the
spectator’s pupils?
60. M Review Conceptual Example 2 before attempting this problem. Two slits are 0.158 mm apart. A mixture of red light (wavelength = 665 nm)
and yellow-green light (wavelength = 565 nm) falls on the slits. A fl at ob-
servation screen is located 2.24 m away. What is the distance on the screen
between the third-order red fringe and the third-order yellow-green fringe?
61. M SSM Available in WileyPLUS. 62. M GO A spotlight sends red light (wavelength = 694.3 nm) to the moon. At the surface of the moon, which is 3.77 × 108 m away, the light strikes a
refl ector left there by astronauts. The refl ected light returns to the earth, where
it is detected. When it leaves the spotlight, the circular beam of light has a dia-
meter of about 0.20 m, and diff raction causes the beam to spread as the light
travels to the moon. In eff ect, the fi rst circular dark fringe in the diff raction
pattern defi nes the size of the central bright spot on the moon. Determine the
diameter (not the radius) of the central bright spot on the moon.
63. M In a single-slit diff raction pattern on a fl at screen, the central bright fringe is 1.2 cm wide when the slit width is 3.2 × 10−5 m. When the slit is
replaced by a second slit, the wavelength of the light and the distance to the
screen remaining unchanged, the central bright fringe broadens to a width of
1.9 cm. What is the width of the second slit? It may be assumed that 𝜃 is so small that sin 𝜃 ≈ tan 𝜃. 64. M GO A beam of light is sent directly down onto a glass plate (n = 1.5) and a plastic plate (n = 1.2) that form a thin wedge of air (see the drawing). An observer looking down through the glass plate sees the fringe pattern
shown in the lower part of the drawing, with the dark fringes at the ends A and B. The wavelength of the light is 520 nm. Using the fringe pattern shown in the drawing, determine the thickness of the air wedge at B.
PROBLEM 64
Plastic n = 1.2
Glass n = 1.5
Thin wedge of air
A
A B
B
65. H There are 5620 lines per centimeter in a grating that is used with light whose wavelength is 471 nm. A fl at observation screen is located at a
distance of 0.750 m from the grating. What is the minimum width that the
screen must have so the centers of all the principal maxima formed on either side of the central maximum fall on the screen?
66. H Available in WileyPLUS.
The ability to exhibit interference eff ects is a fundamental characteristic of
any kind of wave. Our understanding of these eff ects depends on the prin-
ciple of linear superposition, which we fi rst encountered in Chapter 17. Only
by means of this principle can we understand the constructive and destructive
interference of light waves that lie at the heart of every topic in this chapter.
Problem 67 serves as a review of the essence of this principle. Problem 68
deals with thin-fi lm interference and reviews the factors that must be con-
sidered in such cases.
67. M CHALK SSM A square is 3.5 m on a side, and point A is the mid-
point of one of the sides. On the
side opposite this spot, two in-phase
loud-speakers are located at adjacent
corners, as shown in the fi gure. Stand-
ing at point A, you hear a loud sound
because constructive interference
occurs between the identical sound
waves coming from the speakers. As
you walk along the side of the square
toward either empty corner, the loud-
ness diminishes gradually but does
not entirely disappear until you reach
either empty corner, where you hear
no sound at all. Thus, at each empty corner destructive interference occurs.
Concepts: (i) Why does constructive interference occur at point A? (ii) What is the general condition that leads to destructive interference? (iii) The con-
dition that leads to destructive interference entails a number of possibilities.
Which of them applies at either empty corner of the square? Calculation: Find the wavelength of the sound waves.
68. M CHALK A soap fi lm (n = 1.33) is 375 nm thick and coats a fl at piece of glass (n = 1.52). Thus, air is on one side of the fi lm and glass is on the other side, as the fi gure illustrates. Sunlight, whose wavelengths (in vacuum)
extend from 380 to 750 nm, travels through air and strikes the fi lm nearly
perpendicularly. Concepts: (i) What, if any, phase change occurs when light, traveling in air, refl ects from the air–fi lm interface? (ii) What, if any, phase
change occurs when light, traveling in the fi lm, refl ects from the fi lm–glass
interface? (iii) Is the wavelength of the light in the fi lm greater than, smal-
ler than, or equal to the wavelength in a vacuum? Calculations: For what wavelengths in the range of 380 to 750 nm does constructive interference
cause the fi lm to look bright in refl ected light?
PROBLEM 68
Incident light
nair = 1.00
nsoap = 1.33
nglass = 1.52
t
1 2
Concepts and Calculations Problems
A
PROBLEM 67
Team Problems 807
69. M An Optical Monochromator. You and your team are designing a device that inputs a beam of white light (i.e., a continuous spectrum of visible
light spanning all wavelengths from 410 nm to 660 nm), and outputs a nearly
monochromatic beam (i.e., a single color). Such a device is called an optical
monochromator and is used in a wide variety of instruments and scientifi c
experiments. In the instrument you are building, white light impinges upon
the backside of a diff raction grating that has 1200 lines/cm. A movable rect-
angular aperture (a slit) is located on the opposite side of the grating, and can
translate along a circular arc of radius 20.0 cm, the center of which is located
at the grating. (a) At what angle relative to the normal of the grating should the center of the slit be located in order to pass green light (𝜆 = 550 nm) from
fi rst order (m = 1) diff racted light? (b) How wide should the slit be so that the wavelengths passing through the slit fall in the range 540 nm ≤ 𝜆 ≤ 560 nm?
70. M A Crude Thickness Monitor. You and your team need to determine the thicknesses of two extremely thin sheets of plastic and do not have a
measurement instrument capable of the job. You fi nd a white light source
with color fi lters (i.e., tinted glass windows that only let certain colors pass
through) including red (𝜆 = 660 nm), green (𝜆 = 550 nm), and blue (𝜆 =
470 nm). You locate two glass microscope slides, each of length 10.0 cm,
stack one on top of the other, and tape their ends together on one side. On
the very edge of the side opposite the tape, you sandwich a piece of plastic
between the slides to form a wedge of air between the plates. (a) When you shine blue light perpendicular to the slides, 55 bright fringes form along the
full length of the slide. How thick is the plastic? (b) When you replace the fi rst sheet with the second sheet of plastic, the fringes that appear are too
closely spaced to count. You switch to red light (a longer wavelength), and
count 124 fringes. How thick is the plastic? (c) How many fringes would you expect in each case, (a) and (b), if you instead used green light?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
28.1 Define inertial reference frames.
28.2 List the postulates of special relativity.
28.3 Use time dilation to calculate time intervals in diff erent frames of reference.
28.4 Use length contraction to calculate distance in diff erent frames of reference.
28.5 Calculate the relativistic momentum of a high-speed particle.
28.6 Calculate the value of the various forms of energy a moving body possesses.
28.7 Calculate the relative velocity between relativistically moving bodies.
A ct
io n F
o r
T h e
W il
d /
R ex
F ea
tu re
s /A
P /W
id e
W o rl
d P
h o to
s
CHAPTER 28
Special Relativity
These researchers are attaching a Global Positioning System (GPS) tracking unit to a cheetah in Ecuador.
The unit will allow the researchers to track the cheetah’s movements because GPS technology can locate
objects on the earth with remarkable accuracy. The accuracy results, in part, because the system incorporates
Einstein’s theory of special relativity.
28.1 Events and Inertial Reference Frames In the theory of special relativity, an event, such as the launching of the space shuttle in Figure 28.1, is a physical “happening” that occurs at a certain place and time. In this drawing two observers are watching the lift-off , one standing on the earth and one
in an airplane that is fl ying at a constant velocity relative to the earth. To record the
event, each observer uses a reference frame that consists of a set of x, y, z axes (called a coordinate system) and a clock. The coordinate systems are used to establish where the event occurs, and the clocks to specify when. Each observer is at rest relative to
his own reference frame. However, the earth-based observer and the airborne observer
are moving relative to each other and so, also, are their respective reference frames.
The theory of special relativity deals with a “special” kind of reference frame,
called an inertial reference frame. As Section 4.2 discusses, an inertial reference frame is one in which Newton’s law of inertia is valid. That is, if the net force acting on a body is zero, the body either remains at rest or moves at a constant velocity. In other
words, the acceleration of such a body is zero when measured in an inertial reference
frame. Rotating and otherwise accelerating reference frames are not inertial reference
frames. The earth-based reference frame in Figure 28.1 is not quite an inertial frame because it is subjected to centripetal accelerations as the earth spins on its axis and
revolves around the sun. In most situations, however, the eff ects of these accelerations
are small, and we can neglect them. To the extent that the earth-based reference frame
is an inertial frame, so is the plane-based reference frame, because the plane moves at
808
28.2 The Postulates of Special Relativity 809
a constant velocity relative to the earth. The next section discusses why inertial reference frames
are important in relativity.
28.2 The Postulates of Special Relativity Einstein built his theory of special relativity on two fundamental assumptions or postulates about
the way nature behaves.
THE POSTULATES OF SPECIAL RELATIVITY 1. The Relativity Postulate. The laws of physics are the same in every inertial reference frame. 2. The Speed-of-Light Postulate. The speed of light in a vacuum, measured in any inertial
reference frame, always has the same value of c, no matter how fast the source of light and the observer are moving relative to each other.
It is not too diffi cult to accept the relativity postulate. For instance, in Figure 28.1 each observer, using his own inertial reference frame, can make measurements on the motion of the
space shuttle. The relativity postulate asserts that both observers fi nd their data to be consistent
with Newton’s laws of motion. Similarly, both observers fi nd that the behavior of the electronics
on the space shuttle is described by the laws of electromagnetism. According to the relativity pos-
tulate, any inertial reference frame is as good as any other for expressing the laws of physics. As far as inertial reference frames are concerned, nature does not play favorites.
Since the laws of physics are the same in all inertial reference frames, there is no experiment
that can distinguish between an inertial frame that is at rest and one that is moving at a constant
velocity. When you are seated on the aircraft in Figure 28.1, for instance, it is just as valid to say that you are at rest and the earth is moving as it is to say the converse. It is not possible to single
out one particular inertial reference frame as being at “absolute rest.” Consequently, it is mean-
ingless to talk about the “absolute velocity” of an object—that is, its velocity measured relative to
a reference frame at “absolute rest.” Thus, the earth moves relative to the sun, which itself moves
relative to the center of our galaxy. And the galaxy moves relative to other galaxies, and so on.
According to Einstein, only the relative velocity between objects, not their absolute velocities,
can be measured and is physically meaningful.
Whereas the relativity postulate seems plausible, the speed-of-light postulate defi es common
sense. For instance, Figure 28.2 illustrates a person standing on the bed of a truck that is moving at a constant speed of 15 m/s relative to the ground. Now, suppose that you are standing on the
ground and the person on the truck shines a fl ashlight at you. The person on the truck observes
the speed of light to be c. What do you measure for the speed of light? You might guess that the speed of light would be c + 15 m/s. However, this guess is inconsistent with the speed-of-light postulate, which states that all observers in inertial reference frames measure the speed of light to
be c—nothing more, nothing less. Therefore, you must also measure the speed of light to be c, the same as that measured by the person on the truck. According to the speed-of-light postulate, the
fact that the fl ashlight is moving has no infl uence whatsoever on the speed of the light approach-
ing you. This property of light, although surprising, has been verifi ed many times by experiment.
FIGURE 28.1 Using an earth-based reference frame, an observer standing on the earth
records the location and time of an event (the
space shuttle lift-off ). Likewise, an observer
in the airplane uses a plane-based reference
frame to describe the event.
Clock
Clock
Plane-based reference frame
x´
y´
x
y
Earth-based reference frame
810 CHAPTER 28 Special Relativity
Since waves, such as water waves and sound waves, require a medium through which to
propagate, it was natural for scientists before Einstein to assume that light did too. This hypothetical
medium was called the luminiferous ether and was assumed to fi ll all of space. Furthermore, it was believed that light traveled at the speed c only when measured with respect to the ether. According to this view, an observer moving relative to the ether would measure a speed for light that was smaller
or greater than c, depending on whether the observer moved with or against the light, respectively. During the years 1883–1887, however, the American scientists A. A. Michelson and E. W. Morley
carried out a series of famous experiments whose results were not consistent with the ether theory.
Their results indicated that the speed of light is indeed the same in all inertial reference frames and
does not depend on the motion of the observer. These experiments, and others, led eventually to the
demise of the ether theory and the acceptance of the theory of special relativity.
The remainder of this chapter reexamines, from the viewpoint of special relativity, a num-
ber of fundamental concepts that have been discussed in earlier chapters from the viewpoint of
classical physics. These concepts are time, length, momentum, kinetic energy, and the addition
of velocities. We will see that each is modifi ed by special relativity in a way that depends on the
speed 𝜐 of a moving object relative to the speed c of light in a vacuum. Figure 28.3 illustrates that
15 m/s
Observer on earth
c
FIGURE 28.2 Both the person on the truck and the observer on the
earth measure the speed of the light
to be c, regardless of the speed of the truck.
FIGURE 28.3 Albert Einstein (1879–1955), the author of the theory of special relativity, is one of the most famous scientists of the twentieth century. This fi gure emphasizes that the ratio 𝜐/c of the speed 𝜐 of a moving object to the speed c of light in a vacuum is what determines how great the eff ects of special relativity are.
Classical Version
1. Δt0 (Section 1.2)
1. Δt =
(Section 28.3)
Relativistic Version
v c
Concepts
1. Time Interval 2. Length 3. Momentum 4. Kinetic Energy 5. Addition of Velocities
Δt0 1 – v2/c2
3. p =
(Section 28.5)
mv 1 – v2/c2
4. KE = mc2
(Section 28.6)
5. vAB =
(Section 28.7)
– 11 1 – v2/c2
vAC + vCB 1 + vACvCB/c2
2. L = L0 (Section 28.4)
1 – v2/c2
v << c
2. L0 (Section 1.2)
3. p = mv (Section 7.1)
1 2 mv
24. KE = (Section 6.2)
5. vAB = vAC + vCB (Section 3.4)
E .O
. H
o p p e/
T im
e &
L if
e P
ic tu
re s
/G et
ty I
m ag
es
28.3 The Relativity of Time: Time Dilation 811
when the object moves slowly [𝜐 is much smaller than c (𝜐 << c)], the modifi cation is negligibly small, and the classical version of each concept provides an accurate description of reality. How-
ever, when the object moves so rapidly that v is an appreciable fraction of the speed of light [𝜐 is approximately equal to c (𝜐 ≈ c)], the eff ects of special relativity must be considered. The gold panel in Figure 28.3 lists the various equations that convey the modifi cations imposed by special relativity. Each of these equations will be discussed in later sections of this chapter.
It is important to realize that the modifi cations imposed by special relativity do not imply
that the classical concepts of time, length, momentum, kinetic energy, and the addition of velocit-
ies, as developed by Newton and others, are wrong. They are just limited to speeds that are very
small compared to the speed of light. In contrast, the relativistic view of the concepts applies to
all speeds between zero and the speed of light.
28.3 The Relativity of Time: Time Dilation
Time Dilation Common experience indicates that time passes just as quickly for a person standing on the ground
as it does for an astronaut in a spacecraft. In contrast, special relativity reveals that the person on
the ground measures time passing more slowly for the astronaut than for herself. We can see how
this curious eff ect arises with the help of the clock illustrated in Figure 28.4, which uses a pulse of light to mark time. A short pulse of light is emitted by a light source, refl ects from a mirror, and
then strikes a detector that is situated next to the source. Each time a pulse reaches the detector, a
“tick” registers on the chart recorder, another short pulse of light is emitted, and the cycle repeats.
Thus, the time interval between successive “ticks” is marked by a beginning event (the fi ring of
the light source) and an ending event (the pulse striking the detector). The source and detector are
so close to each other that the two events can be considered to occur at the same location.
Suppose two identical clocks are built. One is kept on earth, and the other is placed aboard
a spacecraft that travels at a constant velocity relative to the earth. The astronaut is at rest with
respect to the clock on the spacecraft and, therefore, sees the light pulse move along the up/down
path shown in Animated Figure 28.5a. According to the astronaut, the time interval Δt0 required for the light to follow this path is the distance 2D divided by the speed of light c; Δt0 = 2D/c. To the astronaut, Δt0 is the time interval between the “ticks” of the spacecraft clock—that is, the time interval between the beginning and ending events of the clock. An earth-based observer,
however, does not measure Δt0 as the time interval between these two events. Since the spacecraft is moving, the earth-based observer sees the light pulse follow the diagonal path shown in red
in part b of the drawing. This path is longer than the up/down path seen by the astronaut. But light travels at the same speed c for both observers, in accord with the speed-of-light postulate.
Chart recorder
Detector
Light source
Light pulse
Mirror
“Ticks”
FIGURE 28.4 A light clock.
D
D
(a)
(b)
Astronaut
Beginning event
Ending event
Observer on earth
Δt0
Δt
L
s s
L ANIMATED FIGURE 28.5 (a) The astronaut
measures the time interval Δt0 between successive “ticks” of his light clock. (b) An observer on earth watches the astronaut’s
clock and sees the light pulse travel a greater
distance between “ticks” than it does in part a. Consequently, the earth-based observer
measures a time interval Δt between “ticks” that is greater than Δt0.
812 CHAPTER 28 Special Relativity
Therefore, the earth-based observer measures a time interval Δt between the two events that is greater than the time interval Δt0 measured by the astronaut. In other words, the earth-based observer, using her own earth-based clock to measure the performance of the astronaut’s clock, fi nds that the astronaut’s clock runs slowly. This result of special relativity is known as time dilation. (To dilate means to expand, and the time interval Δt is “expanded” relative to Δt0.)
The time interval Δt that the earth-based observer measures in Animated Figure 28.5b can be determined as follows. While the light pulse travels from the source to the detector, the space- craft moves a distance 2L = 𝜐 Δt to the right, where 𝜐 is the speed of the spacecraft relative to the earth. From the drawing it can be seen that the light pulse travels a total diagonal distance of 2s during the time interval Δt. Applying the Pythagorean theorem, we fi nd that
2s = 2√D2 + L 2 = 2√D2 + (υ∆t2 ) 2
But the distance 2s is also equal to the speed of light times the time interval Δt, so that 2s = c Δt. Therefore,
c ∆t = 2√D 2 + (υ ∆t2 ) 2
Squaring this result and solving for Δt gives
∆t = 2D c
1
√1 − υ 2
c 2
However, 2D/c = Δt0, where Δt0 is the time interval between successive “ticks” of the spacecraft’s clock as measured by the astronaut. With this substitution, the equation for Δt can be expressed as
∆t = ∆t0
√1 − υ 2
c 2 (28.1)
The symbols in this formula are defi ned as follows:
Δt0 = proper time interval, which is the interval between two events as measured by an observer who is at rest with respect to the events and who views them as occurring at the same place
Δt = dilated time interval, which is the interval measured by an observer who is in motion with respect to the events and who views them as occurring at diff erent places
𝜐 = relative speed between the two observers c = speed of light in a vacuum
For a speed 𝜐 that is less than c, the term √1 − υ2/c2 in Equation 28.1 is less than 1, and the dilated time interval Δt is greater than Δt0. Example 1 illustrates the extent of this time dilation eff ect.
Time dilation
EXAMPLE 1 Time Dilation
The spacecraft in Animated Figure 28.5 is moving past the earth at a constant speed υ that is 0.92 times the speed of light. Thus, 𝜐 = (0.92) (3.0 × 108 m/s), which is often written as υ = 0.92c. The astronaut mea- sures the time interval between successive “ticks” of the spacecraft clock to be Δt0 = 1.0 s. What is the time interval Δt that an earth observer measures between “ticks” of the astronaut’s clock?
Reasoning Since the clock on the spacecraft is moving relative to the earth, the earth-based observer measures a greater time interval Δt between “ticks” than does the astronaut, who is at rest relative to the clock. The dilated time interval Δt can be determined from the time dila- tion relation, Equation 28.1.
Solution The dilated time interval is
∆ t = ∆t0
√1 − υ 2
c2
= 1.0 s
√1 − (0.92cc ) 2
= 2.6 s
From the point of view of the earth-based observer, the astronaut is using a clock that is running slowly, because the earth-based observer mea- sures a time between “ticks” that is longer (2.6 s) than what the astronaut measures (1.0 s).
28.3 The Relativity of Time: Time Dilation 813
THE PHYSICS OF . . . the Global Positioning System and special relativity. Present-day spacecrafts fl y nowhere near as fast as the craft in Example 1. Yet circumstances
exist in which time dilation can create appreciable errors if not accounted for. The Global Posi-
tioning System (GPS), for instance, uses highly accurate and stable atomic clocks on board each
of 24 satellites orbiting the earth at speeds of about 4000 m/s. These clocks make it possible to
measure the time it takes for electromagnetic waves to travel from a satellite to a ground-based
GPS receiver. From the speed of light and the times measured for signals from three or more of
the satellites, it is possible to locate the position of the receiver (see Section 5.5). The stability of
the clocks must be better than one part in 1013 to ensure the positional accuracy demanded of the
GPS. Using Equation 28.1 and the speed of the GPS satellites, we can calculate the diff erence
between the dilated time interval and the proper time interval as a fraction of the proper time
interval and compare the result to the stability of the GPS clocks:
∆t − ∆t0
∆t0 =
1
√1 − υ2/c2 − 1 =
1
√1 − (4000 m /s)2/ (3.00 × 108 m /s)2 − 1
= 1
1.1 × 1010
This result is approximately one thousand times greater than the GPS-clock stability of one part
in 1013. Thus, if not taken into account, time dilation would cause an error in the measured pos-
ition of the earth-based GPS receiver roughly equivalent to the error caused by a thousand-fold
degradation in the stability of the atomic clocks.
Proper Time Interval In Animated Figure 28.5 both the astronaut and the person standing on the earth are measuring the time interval between a beginning event (the fi ring of the light source) and an ending event
(the light pulse striking the detector). For the astronaut, who is at rest with respect to the light
clock, the two events occur at the same location. (Remember, we are assuming that the light
source and detector are so close together that they are considered to be at the same place.) Being
at rest with respect to a clock is the usual or “proper” situation, so the time interval Δt0 mea- sured by the astronaut is called the proper time interval. In general, the proper time interval Δt0 between two events is the time interval measured by an observer who is at rest relative to the events and sees them at the same location in space. On the other hand, the earth-based observer does not see the two events occurring at the same location in space, since the spacecraft is in mo-
tion. The time interval Δt that the earth-based observer measures is, therefore, not a proper time interval in the sense that we have defi ned it.
To understand situations involving time dilation, it is essential to distinguish between Δt0 and Δt. It is helpful if one fi rst identifi es the two events that defi ne the time interval. These may be something other than the fi ring of a light source and the light pulse striking a detector. Then
determine the reference frame in which the two events occur at the same place. An observer at
rest in this reference frame measures the proper time interval Δt0.
Space Travel One of the intriguing aspects of time dilation occurs in conjunction with space travel. Since
enormous distances are involved, travel to even the closest star outside our solar system would
take a long time. However, as the following example shows, the travel time can be considerably
less for the passengers than one might guess.
EXAMPLE 2 The Physics of Space Travel and Special Relativity
𝜐 = 0.95c relative to the earth, by how much will the passengers have aged, according to their own clock, when they reach their destination? Assume
that the earth and Alpha Centauri are stationary with respect to one another.
Alpha Centauri, a nearby star in our galaxy, is 4.3 light-years away. This
means that, as measured by a person on earth, it would take light 4.3 years to
reach this star. If a rocket leaves for Alpha Centauri and travels at a speed of
814 CHAPTER 28 Special Relativity
Reasoning The two events in this problem are the departure from earth and the arrival at Alpha Centauri. At departure, earth is just out-
side the spaceship. Upon arrival at the destination, Alpha Centauri is
just outside. Therefore, relative to the passengers, the two events occur
at the same place—namely, just outside the spaceship. Thus, the pas-
sengers measure the proper time interval Δt0 on their clock, and it is this interval that we must fi nd. For a person left behind on earth, the
events occur at diff erent places, so such a person measures the dilated time interval Δt rather than the proper time interval. To fi nd Δt we note that the time to travel a given distance is inversely proportional to the
speed. Since it takes 4.3 years to traverse the distance between earth
and Alpha Centauri at the speed of light, it would take even longer at
the slower speed of 𝜐 = 0.95c. Thus, a person on earth measures the dilated time interval to be Δt = (4.3 years)/0.95 = 4.5 years. This value can be used with the time-dilation equation to fi nd the proper time
interval Δt0.
Problem-Solving Insight In dealing with time dilation, decide which interval is the proper time interval as follows: (1) Identify the two events that defi ne the interval. (2) De- termine the reference frame in which the events occur at the same place; an observer at rest in this frame measures the proper time interval Δt0.
Solution Using the time-dilation equation, we fi nd that the proper time interval by which the passengers judge their own aging is
∆t0 = ∆t √1 − υ 2
c2 = (4.5 years) √1 − (0.95cc )
2
= 1.4 years
Thus, the people aboard the rocket will have aged by only 1.4 years when
they reach Alpha Centauri, and not the 4.5 years an earthbound observer
has calculated.
Verification of Time Dilation A striking confi rmation of time dilation was achieved in 1971 by an experiment carried out
by J. C. Hafele and R. E. Keating.* They transported very precise cesium-beam atomic clocks
around the world on commercial jets. Since the speed of a jet plane is considerably less than c, the time-dilation eff ect is extremely small. However, the atomic clocks were accurate to about
±10−9 s, so the eff ect could be measured. The clocks were in the air for 45 hours, and their times
were compared to reference atomic clocks kept on earth. The experimental results revealed that,
within experimental error, the readings on the clocks on the planes were diff erent from those on
earth by an amount that agreed with the prediction of relativity.
The behavior of subatomic particles called muons provides additional confi rmation of time dilation. These particles are created high in the atmosphere, at altitudes of about 10 000 m. When
at rest, muons exist only for about 2.2 × 10−6 s before disintegrating. With such a short lifetime,
these particles could never make it down to the earth’s surface, even traveling at nearly the speed
of light. However, a large number of muons do reach the earth. The only way they can do so is to live longer because of time dilation, as Example 3 illustrates.
*J. C. Hafele and R. E. Keating, “Around-the-World Atomic Clocks: Observed Relativistic Time Gains,” Science, Vol. 177, July 14, 1972, p. 168.
EXAMPLE 3 The Lifetime of a Muon
The average lifetime of a muon at rest is 2.2 × 10−6 s. A muon created in
the upper atmosphere, thousands of meters above sea level, travels toward
the earth at a speed of 𝜐 = 0.998c. Find, on the average, (a) how long a muon lives according to an observer on earth, and (b) how far the muon travels before disintegrating.
Reasoning The two events of interest are the generation and subsequent disintegration of the muon. When the muon is at rest, these events occur
at the same place, so the muon’s average (at rest) lifetime of 2.2 × 10−6 s
is a proper time interval Δt0. When the muon moves at a speed 𝜐 = 0.998c relative to the earth, an observer on the earth measures a dilated lifetime
Δt that is given by Equation 28.1. The average distance x traveled by a muon, as measured by an earth observer, is equal to the muon’s speed
times the dilated time interval.
Problem-Solving Insight The proper time interval Δt0 is always shorter than the dilated time interval Δt.
Solution (a) The observer on earth measures a dilated lifetime. Using the time-dilation equation, we fi nd that
∆t = ∆t0
√1 − υ 2
c2
= 2.2 × 10−6 s
√1 − (0.998cc ) 2
= 35 × 10−6 s (28.1)
(b) The distance traveled by the muon before it disintegrates is
x = υ ∆t = (0.998)(3.00 × 108 m /s)(35 × 10−6 s) = 1.0 × 104 m
Thus, the dilated, or extended, lifetime provides suffi cient time for the
muon to reach the surface of the earth. If its lifetime were only 2.2 × 10−6 s,
a muon would travel only 660 m before disintegrating and could never
reach the earth.
28.4 The Relativity of Length: Length Contraction 815
Check Your Understanding
(The answers are given at the end of the book.) 1. Which one of the following statements concerning the dilated time interval is false? (a) It is always
greater than the proper time interval. (b) It depends on the relative speed between the observers who measure the proper and dilated time intervals. (c) It depends on the speed of light in a vacuum. (d) It is measured by an observer who is at rest with respect to the events that defi ne the time interval.
2. A baseball player at home plate hits a pop fl y straight up (the beginning event) that is caught by the catcher at home plate (the ending event). Which one or more of the following observers record(s) the
proper time interval between the events? (a) A person sitting in the stands (b) A person watching the game on TV (c) The pitcher running in to cover the play
3. A playground carousel is a circular platform that can rotate about an axis perpendicular to the plane of the platform at its center. It behaves approximately as an inertial reference frame. An observer is looking
down at this platform from an inertial reference frame directly above the rotational axis. Three clocks are
attached to the platform. Clock A is attached directly to the axis. Clock B is attached to a point midway
between the axis and the outer edge of the platform. Clock C is attached to the outer edge of the platform.
Rank the clocks according to how slow the observer fi nds them to be running (slowest fi rst).
28.4 The Relativity of Length: Length Contraction Because of time dilation, observers moving at a constant velocity relative to each other measure dif-
ferent time intervals between two events. For instance, Example 2 in the previous section illustrates
that a trip from earth to Alpha Centauri at a speed of 𝜐 = 0.95c takes 4.5 years according to a clock on earth, but only 1.4 years according to a clock in the rocket. These two times diff er by the factor
√1 − υ2/c2. Since the times for the trip are diff erent, one might ask whether the observers measure diff erent distances between earth and Alpha Centauri. The answer, according to special relativity, is
yes. After all, both the earth-based observer and the rocket passenger agree that the relative speed
between the rocket and earth is 𝜐 = 0.95c. Since speed is distance divided by time and the time is diff erent for the two observers, it follows that the distances must also be diff erent, if the relative
speed is to be the same for both individuals. Thus, the earth observer determines the distance to
Alpha Centauri to be L0 = 𝜐 Δt = (0.95c)(4.5 years) = 4.3 light-years. On the other hand, a pas- senger aboard the rocket fi nds the distance is only L = 𝜐 Δt0 = (0.95c)(1.4 years) = 1.3 light-years. The passenger, measuring the shorter time, also measures the shorter distance. This shortening of
the distance between two points is one example of a phenomenon known as length contraction. The relation between the distances measured by two observers in relative motion at a con-
stant velocity can be obtained with the aid of Interactive Figure 28.6. Part a of the drawing shows the situation from the point of view of the earth-based observer. This person measures
(a) (b)
Δt0
Δt
L L
Earth
Alpha Centauri
0
υυ
υ
INTERACTIVE FIGURE 28.6 (a) As measured by an observer on the earth, the distance to Alpha Centauri is L0, and the time required to make the trip is Δt. (b) According to the passenger on the spacecraft, the earth and Alpha Centauri move with speed 𝜐 relative to the craft. The passenger measures the distance and time of the trip to be L and Δt0, respectively, both quantities being less than those in part a.
816 CHAPTER 28 Special Relativity
the time of the trip to be Δt, the distance to be L0, and the relative speed of the rocket to be 𝜐 = L0/Δt. Part b of the drawing presents the point of view of the passenger, for whom the rocket is at rest, and the earth and Alpha Centauri appear to move by at a speed 𝜐. The passenger determines the distance of the trip to be L, the time to be Δt0, and the relative speed to be 𝜐 = L/Δt0. Since the relative speed computed by the passenger equals that computed by the earth-based observer,
it follows that 𝜐 = L/Δt0 = L0/Δt. Using this result and the time- dilation equation, Equation 28.1, we obtain the following relation between L and L0:
Length contraction
L = L0√1 − υ 2
c2 (28.2)
The length L0 is called the proper length; it is the length (or distance) between two points as measured by an observer at rest with respect to them. Since 𝜐 is less than c, the term √1 − υ2/c2 is less than 1, and L is less than L0. It is important to note that this length contraction occurs only along the direction of the motion. Those dimensions that are perpendicular to the motion are not
shortened, as the next example discusses.
EXAMPLE 4 The Contraction of a Spacecraft
An astronaut, using a meter stick that is at rest relative to a cylindrical
spacecraft, measures the length and diameter of the spacecraft to be
82 m and 21 m, respectively. The spacecraft moves with a constant
speed of 𝜐 = 0.95c relative to the earth, as in Interactive Figure 28.6. What are the dimensions of the spacecraft, as measured by an observer
on earth?
Reasoning The length of 82 m is a proper length L0, since it is mea- sured using a meter stick that is at rest relative to the spacecraft. The
length L measured by the observer on earth can be determined from the length-contraction formula, Equation 28.2. On the other hand, the dia-
meter of the spacecraft is perpendicular to the motion, so the earth ob-
server does not measure any change in the diameter.
Problem-Solving Insight The proper length L0 is always larger than the contracted length L.
Solution The length L of the spacecraft, as measured by the observer on earth, is
L = L0√1 − υ 2
c2 = (82 m) √1 − (0.95cc )
2
= 26 m
Both the astronaut and the observer on earth measure the same value for
the diameter of the spacecraft: Diameter = 21 m . Interactive Figure 28.6a shows the size of the spacecraft as measured by the earth observer, and
part b shows the size as measured by the astronaut.
When dealing with relativistic eff ects we need to distinguish carefully between the criteria
for the proper time interval and the proper length. The proper time interval Δt0 between two events is the time interval measured by an observer who is at rest relative to the events and sees
them occurring at the same place. All other moving inertial observers will measure a larger value for this time interval. The proper length L0 of an object is the length measured by an observer who is at rest with respect to the object. All other moving inertial observers will measure a shorter value for this length. The observer who measures the proper time interval may not be the same
one who measures the proper length. For instance, Interactive Figure 28.6 shows that the astro- naut measures the proper time interval Δt0 for the trip between earth and Alpha Centauri, whereas the earth-based observer measures the proper length (or distance) L0 for the trip.
It should be emphasized that the word “proper” in the phrases “proper time” and “proper length”
does not mean that these quantities are the correct or preferred quantities in any absolute sense. If this were so, the observer measuring these quantities would be using a preferred reference frame for
making the measurement, a situation that is prohibited by the relativity postulate. According to this
postulate, there is no preferred inertial reference frame. When two observers are moving relative to
each other at a constant velocity, each measures the other person’s clock to run more slowly than
his own, and each measures the other person’s length, along that person’s motion, to be contracted.
Check Your Understanding
(The answers are given at the end of the book.) 4. If the speed c of light in a vacuum were infi nitely large instead of 3.0 × 108 m/s, would the eff ects of
time dilation and length contraction be observable?
28.5 Relativistic Momentum 817
5. Suppose that you are standing at a railroad crossing, watching a train go by. Both you and a passenger in the train are looking at a clock on the train. Who measures the proper time interval, and who measures
the proper length of a train car? (a) You measure the proper time interval, and the passenger measures the proper length. (b) You measure both the proper time interval and the proper length. (c) The passen- ger measures both the proper time interval and the proper length. (d) You measure the proper length, and the passenger measures the proper time interval.
6. Which one or more of the following quantities will two observers always measure to be the same, regardless of the relative velocity between the observers? (a) The time interval between two events (b) The length of an object (c) The speed of light in a vacuum (d) The relative speed between the observers
7. CYU Figure 28.1 shows an object that has the shape of a square when it is at rest in inertial reference frame R. When the object moves relative
to this reference frame, the object’s velocity vector is in the plane of the
square and is parallel to the diagonal AC. Since the speed of the motion
is an appreciable fraction of the speed of light in a vacuum, noticeable
length contraction occurs. Does an observer in reference frame R see the
object as a square? (Hint: Consider what happens to each of the diagon- als AC and BD.)
28.5 Relativistic Momentum Thus far we have discussed how time intervals and distances between two events are measured
by observers moving at a constant velocity relative to each other. Special relativity also alters our
ideas about momentum and energy.
Recall from Section 7.2 that when two or more objects interact, the principle of conservation
of linear momentum applies if the system of objects is isolated. This principle states that the total
linear momentum of an isolated system remains constant at all times. (An isolated system is one
in which the sum of the external forces acting on the objects is zero.) The conservation of linear
momentum is a law of physics and, in accord with the relativity postulate, is valid in all inertial
reference frames. That is, when the total linear momentum is conserved in one inertial reference
frame, it is conserved in all inertial reference frames.
As an example of momentum conservation, suppose that several people are watching two
billiard balls collide on a frictionless pool table. One person is standing next to the pool table,
and the other is moving past the table with a constant velocity. Since the two balls constitute an
isolated system, the relativity postulate requires that both observers must fi nd the total linear
momentum of the two-ball system to be the same before, during, and after the collision. For
this kind of situation, Section 7.1 defi nes the classical linear momentum p→ of an object to be the product of its mass m and velocity v→ . As a result, the magnitude of the classical momentum is p = m𝜐. As long as the speed of an object is considerably smaller than the speed of light, this defi nition is adequate. However, when the speed approaches the speed of light, an analysis of the
collision shows that the total linear momentum is not conserved in all inertial reference frames
if one defi nes linear momentum simply as the product of mass and velocity. In order to preserve
the conservation of linear momentum, it is necessary to modify this defi nition. The theory of
special relativity reveals that the magnitude of the relativistic momentum must be defi ned as in Equation 28.3:
Magnitude of the relativistic momentum
p =
mυ
√1 − υ 2
c2 (28.3)
The total relativistic momentum of an isolated system is conserved in all inertial reference frames.
From Equation 28.3, we can see that the magnitudes of the relativistic and nonrelativistic
momenta diff er by the same factor of √1 − υ2/c2 that occurs in the time-dilation and length- contraction equations. Since this factor is always less than 1 and occurs in the denominator in
Equation 28.3, the relativistic momentum is always larger than the nonrelativistic momentum.
To illustrate how the two quantities diff er as the speed 𝜐 increases, Figure 28.7 shows a plot of the ratio of the momentum magnitudes (relativistic/nonrelativistic) as a function of 𝜐. According
B
A
C
D
CYU FIGURE 28.1
5.0
4.0
3.0
2.0
1.0
0.2c 0.4c 0.6c 0.8c c Speed, υ
R el
at iv
is ti
c m
om en
tu m
N on
re la
ti vi
st ic
m om
en tu
m =
υ1 1
–
2 / c
2
FIGURE 28.7 This graph shows how the ratio of the magnitude of the relativistic
momentum to the magnitude of the nonre-
lativistic momentum increases as the speed of
an object approaches the speed of light.
818 CHAPTER 28 Special Relativity
to Equation 28.3, this ratio is just 1/ √1 − υ2/c2. The graph shows that for speeds attained by ordinary objects, such as cars and planes, the relativistic and nonrelativistic momenta are almost
equal because their ratio is nearly 1. Thus, at speeds much less than the speed of light, either the
nonrelativistic momentum or the relativistic momentum can be used to describe collisions. On
the other hand, when the speed of the object becomes comparable to the speed of light, the re-
lativistic momentum becomes signifi cantly greater than the nonrelativistic momentum and must
be used. Example 5 deals with the relativistic momentum of an electron traveling close to the
speed of light.
EXAMPLE 5 The Relativistic Momentum of a High-Speed Electron
The particle accelerator at Stanford University (Figure 28.8) is 3 km long and accelerates electrons to a speed of 0.999 999 999 7c, which is very nearly equal to the speed of light. Find the magnitude of the relativistic
momentum of an electron that emerges from the accelerator, and compare
it with the nonrel ativistic value.
Reasoning and Solution The magnitude of the electron’s relativistic momentum can be obtained from Equation 28.3 if we recall that the mass
of an electron is m = 9.11 × 10−31 kg:
p = mυ
√1 − υ 2
c2
= (9.11 × 10−31 kg)(0.999 999 999 7c)
√1 − (0.999 999 999 7c) 2
c2
= 1 × 10−17 kg · m /s
This value for the magnitude of the momentum agrees with the value
measured experimentally. The relativistic momentum is greater than the
nonrelativistic momentum by a factor of
1
√1 − υ 2
c2
= 1
√1 − (0.999 999 999 7c) 2
c2
= 4 × 104
Math Skills Using your calculator to obtain the answers in Exam-
ple 5 may not be possible due to the term √1 − υ 2
c2 in the pertinent
equations. The potential diffi culty is that your calculator may not let
you enter a number such as 0.999 999 999 7, because it cannot accept
ten places after the decimal point. Since the value for 𝜐 is nearly equal
to c and υ c
≈ 1, one way to deal with such a situation is to note that
√1 − υ 2
c2 = √(1 + υc)(1 −
υ c) ≈ √2 (1 −
υ c)
Thus, we fi nd that
1
√1 − υ 2
c2
≈ 1
√2 (1 − υc) =
1
√2 (1 − 0.999 999 999 7 cc ) =
1
√2(3 × 10−10)
≈ 4 × 104
In this answer the speed 𝜐 is given to ten signifi cant fi gures. However, the answer is given to only one signifi cant fi gure! This is because the
subtraction causes a loss of signifi cant fi gures as follows:
1 − 0.999 999 999 7 = 0.000 000 000 3 = 3 × 10−10
Particle accelerator
FIGURE 28.8 The Stanford 3-km linear accelerator accelerates electrons almost to the speed of light. B
il l
M ar
sh /S
ci en
ce S
o u rc
e
28.6 The Equivalence of Mass and Energy 819
28.6 The Equivalence of Mass and Energy
The Total Energy of an Object One of the most astonishing results of special relativity is that mass and energy are equivalent,
in the sense that a gain or loss of mass can be regarded equally well as a gain or loss of energy.
Consider, for example, an object of mass m traveling at a speed 𝜐. Einstein showed that the total energy E of the moving object is related to its mass and speed by the following relation:
E = mc2
√1 − υ 2
c2
(28.4)
To gain some understanding of Equation 28.4, consider the special case in which the object
is at rest. When 𝜐 = 0 m/s, the total energy is called the rest energy E0, and Equation 28.4 reduces to Einstein’s now-famous equation:
E0 = mc2 (28.5)
The rest energy represents the energy equivalent of the mass of an object at rest. As Example 6
shows, even a small mass is equivalent to an enormous amount of energy.
Total energy of an object
Rest energy of an object
Analyzing Multiple-Concept Problems
EXAMPLE 6 The Energy Equivalent of a Golf Ball
A 0.046-kg golf ball is lying on the green, as Figure 28.9 illustrates. If the rest energy of this ball were used to operate a 75-W light bulb, how long
would the bulb remain lit?
Reasoning The average power delivered to the light bulb is 75 W, which means that it uses 75 J of energy per second. Therefore, the time
that the bulb would remain lit is equal to the total energy used by the light
bulb divided by the energy per second (i.e., the average power) delivered
to it. This energy comes from the rest energy of the golf ball, which is
equal to its mass times the speed of light squared.
Knowns and Unknowns The data for this problem are:
Description Symbol Value Mass of golf ball m 0.046 kg
Average power delivered to light bulb P 75 W
Unknown Variable Time that light bulb would remain lit t ?
Rest Energy
FIGURE 28.9 The rest energy of a golf ball is
suffi cient to keep a 75-W
light bulb burning for an
incredibly long time (see
Example 6).
Modeling the Problem
STEP 1 Power The average power P is equal to the energy delivered to the light bulb divided by the time t (see Section 6.7 and Equation 6.10b), or P = Energy/t. In this case the energy comes from the rest energy E0 of the golf ball, so P = E0 /t. Solving for the time gives Equation 1 at the right. The average power is known, and the rest energy will be evaluated in Step 2.
t = E 0 P
(1)
?
820 CHAPTER 28 Special Relativity
STEP 2 Rest Energy The rest energy E0 is the total energy of the golf ball as it rests on the green. If the golf ball’s mass is m, then its rest energy is
E 0 = mc2 (28.5)
where c is the speed of light in a vacuum. Both m and c are known, so we substitute this expres- sion for the rest energy into Equation 1, as indicated at the right.
Solution Algebraically combining the results of each step, we have
t = E 0 P =
mc2
P The time that the light bulb would remain lit is
t = mc2
P = (0.046 kg)(3.0 × 10 8 m/s)2
75 W = 5.5 × 1013 s
Expressed in years (1 yr = 3.2 × 107 s), this time is equivalent to
(5.5 × 1013 s)( 1 yr
3.2 × 10 7 s) = 1.7 × 10 6 yr or 1.7 million years! Related Homework: Problems 30, 31
STEP 2STEP 1
t = E 0 P
(1)
E 0 = mc2 (28.5)
When an object is accelerated from rest to a speed 𝜐, the object acquires kinetic energy in addition to its rest energy. The total energy E is the sum of the rest energy E0 and the kinetic energy KE, or E = E0 + KE. Therefore, the kinetic energy is the diff erence between the object’s total energy and its rest energy. Using Equations 28.4 and 28.5, we can write the kinetic energy as
Kinetic energy of an object KE = E − E0 = mc
2
( 1
√1 − υ 2
c2
− 1) (28.6) This equation is the relativistically correct expression for the kinetic energy of an object of mass
m moving at speed 𝜐. Equation 28.6 looks nothing like the kinetic energy expression introduced in Section 6.2—
namely, KE = 1
2 mυ2 (Equation 6.2). However, for speeds much less than the speed of light (𝜐 << c), the relativistic equation for the kinetic energy reduces to KE =
1
2 mυ2, as can be seen by using the binomial expansion* to represent the square root term in Equation 28.6:
1
√1 − υ 2
c2
= 1 + 1
2 (υ 2
c2) + 38 ( υ2
c2) 2
+ ⋅ ⋅ ⋅
Suppose that 𝜐 is much smaller than c—say, 𝜐 = 0.01c. The second term in the expansion has the value
1
2 (υ2/c2) = 5.0 × 10−5, while the third term has the much smaller value 3
8 (υ2/c2)2 = 3.8 × 10−9. The additional terms are smaller still, so if 𝜐 << c, we can neglect the third and addi- tional terms in comparison with the fi rst and second terms. Substituting the fi rst two terms into
Equation 28.6 gives
KE ≈ mc2 (1 + 12 υ 2
c2 − 1) = 12 mυ2
which is the familiar form for the kinetic energy. However, Equation 28.6 gives the correct kinetic
energy for all speeds and must be used for speeds near the speed of light, as in Example 7.
*The binomial expansion states that (1 − x)n = 1 −nx + n(n − 1)x2/2 + . . .. In our case, x = 𝜐2/c2 and n = −1/2.
28.6 The Equivalence of Mass and Energy 821
Since mass and energy are equivalent, any change in one is accompanied by a corresponding
change in the other. For instance, life on earth is dependent on electromagnetic energy (light)
from the sun. Because this energy is leaving the sun (see Figure 28.10), there is a decrease in the sun’s mass. Example 8 illustrates how to determine this decrease.
EXAMPLE 7 A High-Speed Electron
An electron (m = 9.109 × 10−31 kg) is accelerated from rest to a speed of 𝜐 = 0.9995c in a particle accelerator. Determine the electron’s (a) rest energy, (b) total energy, and (c) kinetic energy in millions of electron volts or MeV.
Reasoning and Solution (a) The electron’s rest energy is
E0 = mc2 = (9.109 × 10−31 kg)(2.998 × 108 m/s)2 = 8.187 × 10−14 J (28.5)
Since 1 eV = 1.602 × 10−19 J, the electron’s rest energy is
(8.187 × 10−14 J) ( 1 eV1.602 × 10−19 J) = 5.11 × 10 5 eV or 0.511 MeV (b) The total energy of an electron traveling at a speed of 𝜐 = 0.9995c is
E = mc 2
√1 − υ 2
c2
= (9.109 × 10−31 kg)(2.998 × 10 8 m /s) 2
√1 − (0.9995cc ) 2
(28.4)
= 2.59 × 10−12 J or 16.2 MeV
(c) The kinetic energy is the diff erence between the total energy and the rest energy:
KE = E − E0 = 2.59 × 10−12 J − 8.2 × 10−14 J (28.6)
= 2.51 × 10−12 J or 15.7 MeV
For comparison, if the kinetic energy of the electron had been calculated
from 1
2 mυ2, a value of only 0.255 MeV would have been obtained.
FIGURE 28.10 The sun emits electromagnetic energy over a broad portion of the electro-
magnetic spectrum. These photographs were
obtained using that energy in the indicated
regions of the spectrum. Visible light imageX-ray image
N A
S A
/J IS
A S
/S ci
en ce
S o u rc
e
EXAMPLE 8 The Sun Is Losing Mass
The sun radiates electromagnetic energy at the rate of 3.92 × 1026 W.
(a) What is the change in the sun’s mass during each second that it is radi- ating energy? (b) The mass of the sun is 1.99 × 1030 kg. What fraction of the sun’s mass is lost during a human lifetime of 75 years?
Reasoning Since 1 W = 1 J/s, the amount of electromagnetic energy radiated during each second is 3.92 × 1026 J. Thus, during each second,
the sun’s rest energy decreases by this amount. The change ΔE0 in the sun’s rest energy is related to the change Δm in its mass by ΔE0 = (Δm)c2, according to Equation 28.5.
Solution (a) For each second that the sun radiates energy, the change in its mass is
∆m = ∆E0 c2
= 3.92 × 10 26 J
(3.00 × 10 8 m /s)2 = 4.36 × 10 9 kg
Over 4 billion kilograms of mass are lost by the sun during each second.
(b) The amount of mass lost by the sun in 75 years is
∆m = (4.36 × 10 9 kg/s) (3.16 × 10 7 s
1 year )(75 years) = 1.0 × 10 19 kg Although this is an enormous amount of mass, it represents only a tiny
fraction of the sun’s total mass:
∆m msun
= 1.0 × 10 19 kg
1.99 × 10 30 kg = 5.0 × 10−12
822 CHAPTER 28 Special Relativity
Any change ΔE0 in the rest energy of a system causes a change in the mass of the system according to ΔE0 = (Δm)c2. It does not matter whether the change in energy is due to a change in electromagnetic energy, potential energy, thermal energy, or so on. Although any change in
energy gives rise to a change in mass, in most instances the change in mass is too small to be
detected. For instance, when 4186 J of heat is used to raise the temperature of 1 kg of water by
1 °C, the mass changes by only Δm = ΔE0/c2 = (4186 J)/(3.00 × 108 m/s)2 = 4.7 × 10−14 kg. Conceptual Example 9 illustrates further how a change in the energy of an object leads to an
equivalent change in its mass.
CONCEPTUAL EXAMPLE 9 When Is a Massless Spring Not Massless?
Interactive Figure 28.11a shows a top view of a massless spring on a horizontal table. Initially the spring is unstrained. Then the spring is
either stretched or compressed by an amount x from its unstrained length, as Interactive Figure 28.11b illustrates. What is the mass of the spring in Interactive Figure 28.11b? (a) It is greater than zero by an amount that is larger when the spring is stretched. (b) It is greater than zero by an amount that is larger when the spring is compressed. (c) It is greater than zero by an amount that is the same when the spring is stretched or compressed.
(d) It remains zero.
Reasoning When a spring is stretched or compressed, its elastic po- tential energy changes. As discussed in Section 10.3, the elastic potential
energy of an ideal spring is equal to 1
2 kx 2, where k is the spring constant and x is the amount of stretch or compression. Consistent with the theory of special relativity, any change in the total energy of a system, including
a change in the elastic potential energy, is equivalent to a change in the
mass of the system.
Answers (a), (b), and (d) are incorrect. In being stretched or com- pressed by the same amount x, the spring acquires the same amount of elastic potential energy (
1
2 kx 2). Therefore, according to special relativity, the spring acquires the same mass regardless of whether it is stretched or
compressed, so these answers must be incorrect.
Answer (c) is correct. The spring acquires elastic potential energy in being stretched or compressed. Special relativity indicates that this
additional energy is equivalent to additional mass. Since the amount of
stretch or compression is the same, the potential energy is the same in
either case, and so is the additional mass.
Related Homework: Problem 26
+x
(a)
(b) –x
INTERACTIVE FIGURE 28.11 (a) This spring is unstrained and assumed to have no
mass. (b) When the spring is either stretched or compressed by an amount x, it gains elastic potential energy and, hence, mass.
It is also possible to transform matter itself into other forms of energy. For example, the
positron (see Section 31.4) has the same mass as an electron but an opposite electrical charge. If
these two particles of matter collide, they are completely annihilated, and a burst of high- energy
electromagnetic waves is produced. Thus, matter is transformed into electromagnetic waves,
the energy of the electromagnetic waves being equal to the total energies of the two colliding
particles. The medical diagnostic technique known as positron emission tomography or PET
scanning depends on the electromagnetic energy produced when a positron and an electron are
annihilated (see Section 32.6).
The transformation of electromagnetic waves into matter also happens. In one experi-
ment, an extremely high-energy electromagnetic wave, called a gamma ray (see Section 31.4),
passes close to the nucleus of an atom. If the gamma ray has suffi cient energy, it can create
an electron and a positron. The gamma ray disappears, and the two particles of matter appear
in its place. Except for picking up some momentum, the nearby nucleus remains unchanged.
The process in which the gamma ray is transformed into the two particles is known as pair production.
28.6 The Equivalence of Mass and Energy 823
The Relation Between Total Energy and Momentum It is possible to derive a useful relation between the total relativistic energy E and the relativistic momentum p. We begin by rearranging Equation 28.3 for the momentum, to obtain
m
√1 − υ2/c2 =
p υ
With this substitution, Equation 28.4 for the total energy becomes
E = mc2
√1 − υ2/c2 =
pc2
υ or υ c =
pc E
Using this expression to replace 𝜐/c in Equation 28.4 gives
E = mc2
√1 − υ2/c2 =
mc2
√1 − p2c2/E2
Solving this expression for E2 reveals that
E2 = p2c2 + m2c4 (28.7)
Math Skills To solve the equation E = mc2
√1 − p 2c2/E 2 for E, we begin by squaring both sides:
E 2 = ( mc 2
√1 − p 2c 2/E 2) 2
= m 2c 4
1 − p 2c 2/E 2 (1)
The next step is to isolate the terms containing E 2 on the left side of Equation 1. To do this, we multiply each side of the equation by 1 − p 2c 2/E 2:
E2(1−p2 c2/E 2) = m2 c4
1 − p 2 c2/E 2 (1 − p 2c 2/E 2) or E 2 (1 −
p2c2
E 2 ) = m 2c 4 (2) Multiplying terms on the left side of Equation 2 gives
E 2 − p 2c 2 = m 2c 4 (3)
Finally, to isolate E2 on the left side of Equation 3, we add p2c2 to both sides of the equation:
E 2 − p 2c 2 + ( p 2c 2 ) = ( p 2c 2 ) + m 2c 4 or E 2 = p 2c 2 + m 2c 4
The Speed of Light in a Vacuum Is the Ultimate Speed One of the important consequences of the theory of special relativity is that objects with mass
cannot reach the speed c of light in a vacuum. Thus, c represents the ultimate speed. To see that this speed limit is a consequence of special relativity, consider Equation 28.6, which gives
the kinetic energy of an object moving at a speed 𝜐. As 𝜐 approaches the speed of light c, the √1 − υ2/c2 term in the denominator approaches zero. Hence, the kinetic energy becomes infi n- itely large. However, the work–energy theorem (Section 6.2) tells us that an infi nite amount of
work would have to be done to give the object an infi nite kinetic energy. Since an infi nite amount
of work is not available, we are left with the conclusion that objects with mass cannot attain the
speed of light c.
Check Your Understanding
(The answers are given at the end of the book.) 8. Consider the same cup of coff ee sitting on the same table in the following four situations: (a) The coff ee
is hot (95 °C), and the table is at sea level. (b) The coff ee is cold (60 °C), and the table is at sea level. (c) The coff ee is hot (95 °C), and the table is on a mountain top. (d) The coff ee is cold (60 °C), and
(Continued)
824 CHAPTER 28 Special Relativity
the table is on a mountain top. In which situation does the cup of coff ee have the greatest mass, and in
which the smallest mass?
9. A system consists of two positive charges. Is the total mass of the system greater when the two charges are (a) separated by a fi nite distance or (b) infi nitely far apart?
10. A parallel plate capacitor is initially uncharged. Then it is fully charged up by removing electrons from one plate and placing them on the other plate. Is the mass of the capacitor greater when it is
(a) uncharged or (b) fully charged? 11. It takes work to accelerate a particle from rest to a given speed close to the speed of light in a vacuum.
For which particle is less work required, (a) an electron or (b) a proton?
28.7 The Relativistic Addition of Velocities The velocity of an object relative to an observer plays a central role in special relativity, and to
determine this velocity, it is sometimes necessary to add two or more velocities together. We fi rst
encountered relative velocity in Section 3.4, so we will begin by reviewing some of the ideas
presented there. Figure 28.12 illustrates a truck moving at a constant velocity of 𝜐TG = +15 m/s relative to an observer standing on the ground, where the plus sign denotes a direction to the
right. Suppose someone on the truck throws a baseball toward the observer at a velocity of 𝜐BT = +8.0 m/s relative to the truck. We might conclude that the observer on the ground would see the
ball approaching at a velocity of 𝜐BG = 𝜐BT + 𝜐TG = 8.0 m/s + 15 m/s = +23 m/s. These symbols are similar to those used in Section 3.4 and have the following meaning:
𝜐 BG = velocity of the Baseball relative to the Ground = +23 m/s 𝜐 BT = velocity of the Baseball relative to the Truck = +8.0 m/s 𝜐 TG = velocity of the Truck relative to the Ground = +15.0 m/s
Although the result for the velocity of the baseball relative to the ground (𝜐BG = +23 m/s) seems reasonable, careful measurements would show that it is not quite right. According to special re-
lativity, the equation υBG = υBT + υTG is not valid for the following reason. If the velocity of the truck had a magnitude suffi ciently close to the speed of light in a vacuum, the equation would
predict that the observer on the earth could see the baseball moving faster than the speed of light.
This is not possible, since no object with a fi nite mass can move faster than the speed of light in
a vacuum.
For the case in which the truck and ball are moving along the same straight line, the theory
of special relativity reveals that the velocities are related according to
υBG = υBT + υ TG
1 + υBTυ TG
c2
The subscripts in this equation have been chosen for the specifi c situation shown in Figure 28.12. For the general situation, the relative velocities are related by the following velocity-addition formula: Velocity addition
υAB = υAC + υCB
1 + υACυCB
c2 (28.8)
Ground-based observer
BT = +8.0 m/sυ
TG = +15 m/sυFIGURE 28.12 The truck is ap- proaching the ground-based observer
at a relative velocity of 𝜐TG = +15 m/s. The velocity of the baseball relative to
the truck is 𝜐BT = +8.0 m/s.
28.7 The Relativistic Addition of Velocities 825
where all the velocities are assumed to be constant and the symbols have the following meanings:
𝜐 AB = velocity of object A relative to object B 𝜐 AC = velocity of object A relative to object C 𝜐 CB = velocity of object C relative to object B
The ordering of the subscripts in Equation 28.8 follows the discussion in Section 3.4. For mo-
tion along a straight line, the velocities can have either positive or negative values, depending
on whether they are directed along the positive or negative direction. Furthermore, switching
the order of the subscripts changes the sign of the velocity, so, for example, υBA = −υAB (see Example 12 in Chapter 3).
Equation 28.8 diff ers from the nonrelativistic formula (υAB = υAC + υCB) by the presence of the υAC υCB /c2 term in the denominator. This term arises because of the eff ects of time dilation and length contraction that occur in special relativity. When 𝜐AC and 𝜐CB are small compared to c, the 𝜐AC 𝜐CB/c2 term is small compared to 1, so the velocity-addition formula reduces to υAB ≈ υAC + υCB. However, when either 𝜐AC or 𝜐CB is comparable to c, the results can be quite diff erent, as Example 10 illustrates.
EXAMPLE 10 The Relativistic Addition of Velocities
Imagine a hypothetical situation in which the truck in Figure 28.12 is moving relative to the ground with a velocity of 𝜐TG = +0.8c. A person riding on the truck throws a baseball at a velocity relative to the truck of
𝜐TG = +0.5c. What is the velocity 𝜐BG of the baseball relative to a person standing on the ground?
Reasoning The observer standing on the ground does not see the base- ball approaching at 𝜐BG = 0.5c + 0.8c = 1.3c. This cannot be, because the speed of the ball would then exceed the speed of light in a vacuum. The
velocity-addition formula gives the correct velocity, which has a mag-
nitude less than the speed of light.
Solution The ground-based observer sees the ball approaching with a velocity of
υBG = υBT + υTG
1 + υBTυTG
c2
= 0.5c + 0.8c
1 + (0.5c) (0.8c)
c2
= 0.93c (28.8)
Example 10 discusses how the speed of a baseball is viewed by observers in diff erent iner-
tial reference frames. The next example deals with a similar situation, except that the baseball is
replaced by the light of a laser beam.
CONCEPTUAL EXAMPLE 11 The Speed of a Laser Beam
Answer (c) is incorrect. The velocity at which the renegades see the laser beam move away from the cruiser cannot be 𝜐 = +0.7c, because they see the cruiser moving at a velocity of +0.7c and the laser beam moving at a velocity of only +c (not +1.4c).
Answer (d) is correct. The renegades see the cruiser approach them at a relative velocity of 𝜐CS = +0.7c and see the laser beam approach them at a relative velocity of 𝜐LS = +c. Both these velocities are mea- sured relative to the same inertial reference frame—namely, that of their own spacecraft. Therefore, the renegades see the laser beam move
away from the cruiser at a velocity that is the diff erence between these
two velocities, or +c −(+0.7c) = +0.3c. The velocity-addition formula, Equation 28.8, does not apply here because both velocities are measured
relative to the same inertial reference frame. Equation 28.8 is used only when the velocities are measured relative to diff erent inertial reference frames.
Related Homework: Problem 39
Figure 28.13 shows an intergalactic cruiser approaching a hostile space- craft. Both vehicles move at a constant velocity. The velocity of the
cruiser relative to the spacecraft is 𝜐CS = +0.7c, the direction to the right being the positive direction. The cruiser fi res a beam of laser light at the
hostile renegades. The velocity of the laser beam relative to the cruiser is
𝜐LC = +c. Which one of the following statements correctly describes the velocity 𝜐LS of the laser beam relative to the renegades’ spacecraft and the velocity 𝜐 at which the renegades see the laser beam move away from the cruiser? (a) 𝜐LS = +0.7c and 𝜐 = +c (b) 𝜐LS = +0.3c and 𝜐 = +c (c) 𝜐LS = +c and 𝜐 = +0.7c (d) 𝜐LS = +c and 𝜐 = +0.3c
Reasoning Since both vehicles move at a constant velocity, each con- stitutes an inertial reference frame. According to the speed-of-light postu-
late, all observers in inertial reference frames measure the speed of light in a vacuum to be c.
Answers (a) and (b) are incorrect. Since the renegades’ spacecraft con- stitutes an inertial reference frame, the velocity of the laser beam relative to it
can only have a value of 𝜐LS = +c, according to the speed-of-light postulate.
826 CHAPTER 28 Special Relativity
It is a straightforward matter to show that the velocity-addition formula is consistent with
the speed-of-light postulate. Consider Figure 28.14, which shows a person riding on a truck and holding a fl ashlight. The velocity of the light relative to the person on the truck is 𝜐LT = +c. The velocity 𝜐LG of the light relative to the observer standing on the ground is given by the velocity-addition formula as
υLG = υLT + υTG
1 + υLTυTG
c2
= c + υTG
1 + cυTG c2
= (c + υTG)c (c + υTG)
= c
Thus, the velocity-addition formula indicates that the observer on the ground and the person on
the truck both measure the speed of light to be c, independent of the relative velocity 𝜐TG between them. This conclusion is completely consistent with the speed-of-light postulate.
FIGURE 28.13 An intergalactic cruiser, closing in on a hostile spacecraft, fi res a beam
of laser light.
Laser beam
Hostile spacecraftIntergalactic cruiser
υ
Ground-based observer
LT = +cυ
TG FIGURE 28.14 The speed of the
light emitted by the fl ashlight is c relative to both the truck and the
observer on the ground.
Check Your Understanding
(The answer is given at the end of the book.) 12. Car A and car B are both traveling due east on a straight section of an interstate highway. The speed of
car A relative to the ground is 10 m/s faster than the speed of car B relative to the ground. According to
special relativity, is the speed of car A relative to car B (a) 10 m/s, (b) less than 10 m/s, or (c) greater than 10 m/s?
EXAMPLE 12 BIO The Physics of Space Travel Revisited
Relativistic time dilation aff ects not only the operation of clocks, but also
all physiological and biological processes, including the rates of chemical
reactions. This is why a person moving on a spaceship, for example, will
age slower than one that stays at home on earth. Imagine an astronaut in
a spaceship that is moving away from the earth at 98% the speed of light.
Given that it takes the human body only 27 days to replace the entire outer
layer of the skin, how many times has the person on earth replaced their
skin, if 27 days pass on the spaceship?
Reasoning We recognize this to be an example of relativistic time dilation. We can apply Equation 28.1 to calculate the dilated time interval.
Since the astronaut measures the time on his clock at the same location
(inside the ship), he is measuring the proper time interval Δt0. The ship is moving relative to the reference frame of the earth, so the earth-bound
observer measures the dilated time interval.
Solution Beginning with Equation 28.1, we have:
∆t = ∆t0
√1 − υ 2
c2
.
Since we want to calculate the dilated time interval in days, we keep the
proper time in those units as well. The speed of the ship is 98% the speed of
light, which is 𝜐 = 0.98c. We make these substitutions above and solve for Δt:
∆t = 27 days
√1 − (0.98c) 2
c2
= 27 days
√1 − (0.98)2 = (5.0)(27 days) .
The length of time that passes on earth during the 27 days on the ship is
fi ve times longer. Therefore, the person on earth will have replaced their
skin fi ve times!
Focus on Concepts 827
Concept Summary 28.1 Events and Inertial Reference Frames An event is a physical “hap- pening” that occurs at a certain place and time. To record the event an ob-
server uses a reference frame that consists of a coordinate system and a clock.
Diff erent observers may use diff erent reference frames. The theory of special
relativity deals with inertial reference frames. An inertial reference frame is
one in which Newton’s law of inertia is valid. Accelerating reference frames
are not inertial reference frames.
28.2 The Postulates of Special Relativity The theory of special relativity is based on two postulates. The relativity postulate states that the laws of
physics are the same in every inertial reference frame. The speed-of-light
postulate says that the speed of light in a vacuum, measured in any iner-
tial reference frame, always has the same value of c, no matter how fast the source of the light and the observer are moving relative to each other.
28.3 The Relativity of Time: Time Dilation The proper time interval Δt0 between two events is the time interval measured by an observer who is at rest
relative to the events and views them occurring at the same place. An observer
who is in motion with respect to the events and who views them as occurring
at diff erent places measures a dilated time interval Δt. The dilated time in- terval is greater than the proper time interval, according to the time-dilation
equation (Equation 28.1). In this expression, 𝜐 is the relative speed between the observer who measures Δt0 and the observer who measures Δt.
∆t = ∆t0
√1 − υ 2
c2
(28.1)
28.4 The Relativity of Length: Length Contraction The proper length L0 between two points is the length measured by an observer who is at rest re- lative to the points. An observer moving with a relative speed 𝜐 parallel to the line between the two points does not measure the proper length. Instead, such
an observer measures a contracted length L given by the length-contraction formula (Equation 28.2). Length contraction occurs only along the direction
of the motion. Those dimensions that are perpendicular to the motion are
not shortened. The observer who measures the proper length may not be the
observer who measures the proper time interval.
L = L0√1 − υ 2
c2 (28.2)
28.5 Relativistic Momentum An object of mass m, moving with speed 𝜐, has a relativistic momentum whose magnitude p is given by Equation 28.3.
p = mυ
√1 − υ 2
c2
(28.3)
28.6 The Equivalence of Mass and Energy Energy and mass are equival- ent. The total energy E of an object of mass m, moving at speed 𝜐, is given by Equation 28.4. The rest energy E0 is the total energy of an object at rest (𝜐 = 0 m/s), as given by Equation 28.5. An object’s total energy is the sum of its
rest energy and its kinetic energy KE, or E = E0 + KE. Therefore, the kinetic energy is given by Equation 28.6.
E = mc2
√1 − υ 2
c2
(28.4)
E0 = mc2 (28.5)
KE = E − E0 = mc2( 1
√1 − υ 2
c2
− 1
) (28.6) The relativistic total energy and momentum are related according to
Equation 28.7.
E 2 = p2c2 + m2c4 (28.7)
Objects with mass cannot attain the speed of light c, which is the ultimate speed for such objects.
28.7 The Relativistic Addition of Velocities According to special re- lativity, the velocity-addition formula specifi es how the relative velocities
of moving objects are related. For objects that move along the same straight
line, this formula is given by Equation 28.8, where 𝜐AB is the velocity of object A relative to object B, 𝜐AC is the velocity of object A relative to object C, and 𝜐CB is the velocity of object C relative to object B. The velocities can have positive or negative values, depending on whether they are dir-
ected along the positive or negative direction. Furthermore, switching the
order of the subscripts changes the sign of the velocity, so that, for example,
𝜐BA = −𝜐AB.
υAB = υAC + υCB
1 + υAC υCB
c2
(28.8)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 28.1 Events and Inertial Reference Frames 1. Consider a person along with a frame of reference in each of the follow- ing situations. In which one or more of the following situations is the frame
of reference an inertial frame of reference? (a) The person is oscillating in simple harmonic motion at the end of a bungee cord. (b) The person is in a
car going around a circular curve at a constant speed. (c) The person is in a plane that is landing on an aircraft carrier. (d) The person is in the space shuttle during lift-off . (e) None of the above.
Section 28.3 The Relativity of Time: Time Dilation 2. On a highway there is a fl ashing light to mark the start of a section of the road where work is being done. Who measures the proper time between
two fl ashes of light? (a) A worker standing still on the road (b) A driver in a car approaching at a constant velocity (c) Both the worker and the driver (d) Neither the worker nor the driver
Focus on Concepts
828 CHAPTER 28 Special Relativity
Section 28.4 The Relativity of Length: Length Contraction 4. Two spacecrafts A and B are moving relative to each other at a constant velocity. Observers in spacecraft A see spacecraft B. Likewise, observers in
spacecraft B see spacecraft A. Who sees the proper length of either spacecraft?
(a) Observers in spacecraft A see the proper length of spacecraft B. (b) Ob- servers in spacecraft B see the proper length of spacecraft A. (c) Observers in both spacecrafts see the proper length of the other spacecraft. (d) Observers in neither spacecraft see the proper length of the other spacecraft.
6. In a baseball game the batter hits the ball into center fi eld and takes off for fi rst base. The catcher can only stand and watch. Assume that the batter runs
at a constant velocity. Who measures the proper time it takes for the runner to
reach fi rst base, and who measures the proper length between home plate and
fi rst base? (a) The catcher measures the proper time, and the runner measures the proper length. (b) The runner measures the proper time, and the catcher measures the proper length. (c) The catcher measures both the proper time and the proper length. (d) The runner measures both the proper time and the proper length.
7. To which one or more of the following situations do the time-dilation and length-contraction equations apply? (a) With respect to an inertial frame, two observers have diff erent constant accelerations. (b) With respect to an inertial frame, two observers have the same constant acceleration. (c) With respect to an inertial frame, two observers are moving with diff erent constant velocities.
(d) With respect to an inertial frame, one observer has a constant velocity, and another observer has a constant acceleration. (e) All of the above.
Section 28.5 Relativistic Momentum 10. Which one of the following statements about linear momentum is true (p = magnitude of the momentum, m = mass, and 𝜐 = speed)?
(a) When the magnitude p of the momentum is defi ned as p = mυ √1 − υ2/c2
,
the linear momentum of an isolated system is conserved only if the speeds of the various parts of the system are very high. (b) When the magnitude p of the momentum is defi ned as p = m𝜐, the linear momentum of an isolated system is conserved only if the speeds of the various parts of the system
are very high. (c) When the magnitude p of the momentum is defi ned as p = mυ
√1 − υ2/c2 , the linear momentum of an isolated system is conserved no
matter what the speeds of the various parts of the system are. (d) When the magnitude p of the momentum is defi ned as p = m𝜐, the linear momentum of an isolated system is conserved no matter what the speeds of the various
parts of the system are.
11. Which of the following two expressions for the magnitude p of the linear momentum can be used when the speed 𝜐 of an object of mass m is very small compared to the speed of light c in a vacuum?
A. p = mυ
B. p = mυ
√1 − υ 2
c2
(a) Only A (b) Only B (c) Neither A nor B (d) Both A and B
Section 28.6 The Equivalence of Mass and Energy 13. Consider the following three possibilities for a glass of water at rest on a kitchen counter. The temperature of the water is 0 °C. Rank the mass of the
water in descending order (largest fi rst).
A. The water is half liquid and half ice. B. The water is all liquid. C. The water is all ice.
(a) C, A, B (b) B, A, C (c) A, C, B (d) B, C, A (e) C, B, A 15. An object has a kinetic energy KE and a potential energy PE. It also has a rest energy E0. Which one of the following is the correct way to express the object’s total energy E? (a) E = KE + PE (b) E = E0 + KE (c) E = E0 + KE + PE (d) E = E0 + KE − PE 17. The kinetic energy of an object of mass m is equal to its rest energy. What is the magnitude p of the object’s momentum? (a) p = √3 mc (b) p = 2mc (c) p = 4mc (d) p = √2mc (e) p = 3mc
Section 28.7 The Relativistic Addition of Velocities 18. Two spaceships are traveling in the same direction. With respect to an inertial frame of reference, spaceship A has a speed of 0.900c. With respect to the same inertial frame, spaceship B has a speed of 0.500c. Find the speed 𝜐AB of spaceship A relative to spaceship B.
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details. Note: Before doing any calculations involving time dilation or length contraction, it is useful to identify which observer measures the proper time interval Δt0 or the proper length L0.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 28.3 The Relativity of Time: Time Dilation 1. E SSM A particle known as a pion lives for a short time before breaking apart into other particles. Suppose that a pion is moving at a speed of 0.990c, and an observer who is stationary in a laboratory measures the pion’s lifetime
to be 3.5 × 10−8 s. (a) What is the lifetime according to a hypothetical person who is riding along with the pion? (b) According to this hypothetical person, how far does the laboratory move before the pion breaks apart?
2. E A radar antenna is rotating and makes one revolution every 25 s, as measured on earth. However, instruments on a spaceship moving with re-
spect to the earth at a speed 𝜐 measure that the antenna makes one revolution every 42 s. What is the ratio 𝜐/c of the speed 𝜐 to the speed c of light in a vacuum?
Problems
Problems 829
3. E SSM Suppose that you are planning a trip in which a spacecraft is to travel at a constant velocity for exactly six months, as measured by a clock
on board the spacecraft, and then return home at the same speed. Upon your
return, the people on earth will have advanced exactly one hundred years into
the future. According to special relativity, how fast must you travel? Express
your answer to fi ve signifi cant fi gures as a multiple of c—for example, 0.955 85c. 4. E CHALK GO Suppose that you are traveling on board a spacecraft that is moving with respect to the earth at a speed of 0.975c. You are breathing at a rate of 8.0 breaths per minute. As monitored on earth, what is your breathing
rate?
5. M GO MMH A 6.00-kg object oscillates back and forth at the end of a spring whose spring constant is 76.0 N/m. An observer is traveling at a speed
of 1.90 × 108 m/s relative to the fi xed end of the spring. What does this
observer measure for the period of oscillation?
6. M V-HINT A spaceship travels at a constant speed from earth to a planet orbiting another star. When the spacecraft arrives, 12 years have elapsed on
earth, and 9.2 years have elapsed on board the ship. How far away (in meters)
is the planet, according to observers on earth?
7. H As observed on earth, a certain type of bacterium is known to double in number every 24.0 hours. Two cultures of these bacteria are prepared, each
consisting initially of one bacterium. One culture is left on earth and the other
placed on a rocket that travels at a speed of 0.866c relative to the earth. At a time when the earthbound culture has grown to 256 bacteria, how many bac-
teria are in the culture on the rocket, according to an earth-based observer?
Section 28.4 The Relativity of Length: Length Contraction 8. E Suppose the straight-line distance between New York and San Francisco is 4.1 × 106 m (neglecting the curvature of the earth). A UFO is
fl ying between these two cities at a speed of 0.70c relative to the earth. What do the voyagers aboard the UFO measure for this distance?
9. E SSM How fast must a meter stick be moving if its length is observed to shrink to one-half of a meter?
10. E V-HINT MMH The distance from earth to the center of our galaxy is about 23 000 ly (1 ly = 1 light-year = 9.47 × 1015 m), as measured by
an earth-based observer. A spaceship is to make this journey at a speed of
0.9990c. According to a clock on board the spaceship, how long will it take to make the trip? Express your answer in years (1 yr = 3.16 × 107 s).
11. E A tourist is walking at a speed of 1.3 m/s along a 9.0-km path that follows an old canal. If the speed of light in a vacuum were 3.0 m/s, how long
would the path be, according to the tourist?
12. E GO A Martian leaves Mars in a spaceship that is heading to Venus. On the way, the spaceship passes earth with a speed 𝜐 = 0.80c relative to it. Assume that the three planets do not move relative to each other during the
trip. The distance between Mars and Venus is 1.20 × 1011 m, as measured
by a person on earth. (a) What does the Martian measure for the distance between Mars and Venus? (b) What is the time of the trip (in seconds) as measured by the Martian?
13. E Two spaceships A and B are exploring a new planet. Relative to this planet, spaceship A has a speed of 0.60c, and spaceship B has a speed of 0.80c. What is the ratio DA/DB of the values for the planet’s diameter that each spaceship measures in a direction that is parallel to its motion?
14. E An unstable high-energy particle is created in the laboratory, and it moves at a speed of 0.990c. Relative to a stationary reference frame fi xed to the laboratory, the particle travels a distance of 1.05 × 10−3 m before disin-
tegrating. What are (a) the proper distance and (b) the distance measured by a hypothetical person traveling with the particle? Determine the particle’s
(c) proper lifetime and (d) its dilated lifetime.
15. M CHALK As the drawing shows, a carpenter on a space station has con- structed a 30.0° ramp. A rocket moves past the space station with a relative
speed of 0.730c in a direction parallel to side x0. What does a person aboard the rocket measure for the angle of the ramp?
PROBLEM 15 x0 30.0° 90.0°
y0
16. H Available in WileyPLUS. 17. H Available in WileyPLUS.
Section 28.5 Relativistic Momentum 18. E At what speed is the magnitude of the relativistic momentum of a particle three times the magnitude of the nonrelativistic momentum?
19. E What is the magnitude of the relativistic momentum of a proton with a relativistic total energy of 2.7 × 10−10 J?
20. E GO A spacecraft has a nonrelativistic (or classical) momentum whose magnitude is 1.3 × 1013 kg · m /s. The spacecraft moves at such a speed that the pilot measures the proper time interval between two events to be one-half
the dilated time interval. Find the relativistic momentum of the spacecraft.
21. E SSM A woman is 1.6 m tall and has a mass of 55 kg. She moves past an observer with the direction of the motion parallel to her height.
The observer measures her relativistic momentum to have a magnitude of
2.0 × 1010 kg · m /s. What does the observer measure for her height? 22. E GO Three particles are listed in the table. The mass and speed of each particle are given as multiples of the variables m and 𝜐, which have the values m = 1.20 × 10−8 kg and 𝜐 = 0.200c. The speed of light in a vacuum is c = 3.00 × 108 m/s. Determine the momentum for each particle according to special relativity.
Particle Mass Speed a m υ
b 1 2 m 2υ
c 1
4 m 4υ
23. M SSM Starting from rest, two skaters push off against each other on smooth level ice, where friction is negligible. One is a woman and one is a
man. The woman moves away with a velocity of +2.5 m/s relative to the ice.
The mass of the woman is 54 kg, and the mass of the man is 88 kg. Assuming
that the speed of light is 3.0 m/s, so that the relativistic momentum must
be used, fi nd the recoil velocity of the man relative to the ice. (Hint: This problem is similar to Example 6 in Chapter 7.)
Section 28.6 The Equivalence of Mass and Energy 24. E Radium is a radioactive element whose nucleus emits an 𝛼 particle (a helium nucleus) with a kinetic energy of about 7.8 × 10−13 J (4.9 MeV).
To what amount of mass is this energy equivalent?
25. E SSM How much work must be done on an electron to accelerate it from rest to a speed of 0.990c? 26. E Available in WileyPLUS. 27. E Suppose that one gallon of gasoline produces 1.1 × 108 J of energy, and this energy is suffi cient to operate a car for twenty miles. An aspirin
830 CHAPTER 28 Special Relativity
tablet has a mass of 325 mg. If the aspirin could be converted completely into
thermal energy, how many miles could the car go on a single tablet?
28. E GO Two kilograms of water are changed (a) from ice at 0 °C into liquid water at 0 °C and (b) from liquid water at 100 °C into steam at 100 °C. For each situation, determine the change in mass of the water.
29. E CHALK SSM Determine the ratio of the relativistic kinetic energy to the nonrelativistic kinetic energy (
1
2 mυ2) when a particle has a speed of (a) 1.00 × 10−3c and (b) 0.970c. 30. E Multiple-Concept Example 6 reviews the principles that play a role in this problem. A nuclear power reactor generates 3.0 × 109 W of power. In
one year, what is the change in the mass of the nuclear fuel due to the energy
being taken from the reactor?
31. M V-HINT Multiple-Concept Example 6 explores the approach taken in problems such as this one. Quasars are believed to be the nuclei of galaxies
in the early stages of their formation. Suppose that a quasar radiates elec-
tromagnetic energy at the rate of 1.0 × 1041 W. At what rate (in kg/s) is the
quasar losing mass as a result of this radiation?
32. M GO An electron is accelerated from rest through a potential diff erence that has a magnitude of 2.40 × 107 V. The mass of the electron is 9.11 ×
10−31 kg, and the negative charge of the electron has a magnitude of 1.60 ×
10−19 C. (a) What is the relativistic kinetic energy (in joules) of the electron? (b) What is the speed of the electron? Express your answer as a multiple of c, the speed of light in a vacuum.
33. M V-HINT Available in WileyPLUS.
Section 28.7 The Relativistic Addition of Velocities 34. E GO You are driving down a two-lane country road, and a truck in the opposite lane is traveling toward you. Suppose that the speed of light in a
vacuum is c = 65 m/s. Determine the speed of the truck relative to you when (a) your speed is 25 m/s and the truck’s speed is 35 m/s and (b) your speed is 5.0 m/s and the truck’s speed is 55 m/s. The speeds given in parts (a) and (b)
are relative to the ground.
35. E SSM A spacecraft approaching the earth launches an exploration vehicle. After the launch, an observer on earth sees the spacecraft approaching
at a speed of 0.50c and the exploration vehicle approaching at a speed of 0.70c. What is the speed of the exploration vehicle relative to the spaceship?
36. E GO Spaceships of the future may be powered by ion-propulsion en- gines in which ions are ejected from the back of the ship to drive it forward.
In one such engine the ions are to be ejected with a speed of 0.80c relative to the spaceship. The spaceship is traveling away from the earth at a speed
of 0.70c relative to the earth. What is the velocity of the ions relative to the earth? Assume that the direction in which the spaceship is traveling is the
positive direction, and be sure to assign the correct plus or minus signs to
the velocities.
37. E The spaceship Enterprise 1 is moving directly away from earth at a velocity that an earth-based observer measures to be +0.65c. A sister ship, Enterprise 2, is ahead of Enterprise 1 and is also moving directly away from earth along the same line. The velocity of Enterprise 2 relative to Enterprise 1 is +0.31c. What is the velocity of Enterprise 2, as measured by the earth- based observer?
38. M V-HINT A person on earth notices a rocket approaching from the right at a speed of 0.75c and another rocket approaching from the left at 0.65c. What is the relative speed between the two rockets, as measured by a passenger on one of them?
39. M SSM Refer to Conceptual Example 11 as an aid in solving this prob- lem. An intergalactic cruiser has two types of guns: a photon cannon that fi res
a beam of laser light and an ion gun that shoots ions at a velocity of 0.950c relative to the cruiser. The cruiser closes in on an alien spacecraft at a velo-
city of 0.800c relative to this spacecraft. The captain fi res both types of guns. At what velocity do the aliens see (a) the laser light and (b) the ions approach them? At what velocity do the aliens see (c) the laser light and (d) the ions move away from the cruiser?
40. M GO Two identical spaceships are under construction. The construc- ted length of each spaceship is 1.50 km. After being launched, spaceship A
moves away from earth at a constant velocity (speed is 0.850c) with respect to the earth. Spaceship B follows in the same direction at a diff erent constant
velocity (speed is 0.500c) with respect to the earth. Determine the length that a passenger on one spaceship measures for the other spaceship.
41. H Available in WileyPLUS.
42. E An electron and a positron have masses of 9.11 × 10−31 kg. They collide and both vanish, with only electromagnetic radiation appearing after
the collision. If each particle is moving at a speed of 0.20c relative to the laboratory before the collision, determine the energy of the electromagnetic
radiation.
43. E SSM MMH Available in WileyPLUS. 44. E GO The speed of an ion in a particle accelerator is doubled from 0.460c to 0.920c. The initial relativistic momentum of the ion is 5.08 × 10−17 kg ⋅m/s. Determine (a) the mass and (b) the magnitude of the fi nal relativ- istic momentum of the ion.
45. E GO A Klingon spacecraft has a speed of 0.75c with respect to the earth. The Klingons measure 37.0 h for the time interval between two events
on the earth. What value for the time interval would they measure if their ship
had a speed of 0.94c with respect to the earth?
46. M V-HINT Available in WileyPLUS. 47. M SSM The crew of a rocket that is moving away from the earth launches an escape pod, which they measure to be 45 m long. The pod is launched to-
ward the earth with a speed of 0.55c relative to the rocket. After the launch,
the rocket’s speed relative to the earth is 0.75c. What is the length of the escape pod as determined by an observer on earth?
48. M GO The table gives the total energy and the rest energy for three ob- jects in terms of an energy increment 𝜖. For each object, determine the speed
as a multiple of the speed c of light in a vacuum.
Object Total Energy (E) Rest Energy (E0) A 2.00𝜖 𝜖
B 3.00𝜖 𝜖
C 3.00𝜖 2.00𝜖
49. H GO Twins who are 19.0 years of age leave the earth and travel to a distant planet 12.0 light-years away. Assume that the planet and earth are at
rest with respect to each other. The twins depart at the same time on diff erent
spaceships. One twin travels at a speed of 0.900c, and the other twin travels at 0.500c. (a) According to the theory of special relativity, what is the diff er- ence between their ages when they meet again at the earliest possible time?
(b) Which twin is older?
Additional Problems
Team Problems 831
There are many astonishing consequences of special relativity, two of which
are time dilation and length contraction. Problem 50 reviews these important
concepts in the context of a golf game in a hypothetical world where the
speed of light is only a little faster than that of a golf cart. Other important
consequences of special relativity are the equivalence of mass and energy,
and the dependence of kinetic energy on the total energy and on the rest en-
ergy. Problem 51 serves as a review of the roles played by mass and energy
in special relativity.
50. M CHALK Imagine playing golf in a world where the speed of light is only c = 3.40 m/s. Golfer A drives a ball down a fl at horizontal fairway for
a distance that he measures as 75.0 m. Golfer B, riding in a cart, happens to
pass by just as the ball is hit (see the fi gure). Golfer A stands at the tee and
watches while golfer B moves down the fairway toward the ball at a con-
stant speed of 2.80 m/s. Concepts: (i) Who measures the proper length of the drive, and who measures the contracted length? (ii) Who measures the proper
time interval, and who measures the dilated time interval? Calculations: (a) How far is the ball hit according to golfer B? (b) According to each golfer, how much time does it take golfer B to reach the ball?
51. M CHALK SSM The rest energy E0 and the total energy E of three particles, expressed in terms of a basic amount of energy E′ = 5.98 × 10−10 J, are listed in the table. The speeds of these particles are large, in some cases
approaching the speed of light. Concepts: (i) Given the rest energies specifi ed in the table, what is the ranking (largest fi rst) of the masses of the particles?
(ii) Is the kinetic energy KE given by the expression KE = 1/2m𝜐2, and what is the ranking (largest fi rst) of the kinetic energies of the particles? Calcula- tions: For each particle, determine its (a) mass and (b) kinetic energy.
Particle Rest Energy Total Energy a Eʹ 2Eʹ
b Eʹ 4Eʹ
c 5Eʹ 6Eʹ
Concepts and Calculations Problems
Golfer A
Golfer B
PROBLEM 50
52. M A Super Thruster. You and your team are evaluating a new thruster that will be used to propel a 6.00 × 104 kg ship. The thruster has a power
output of 2.88 × 106 W, calculated to initially accelerate the ship at 9.80 m/s2
(safe for humans). (a) Assuming that all of the energy of the thruster is con- verted into kinetic energy of the ship, what is the velocity of the ship after 1
year? (b) After 1000 years? (c) Assuming the thruster converts mass directly into energy, how much mass would be converted into energy over the 1000-
year trip?
53. M A Long Trip. You and your team are on a journey to a solar system in another part of our galaxy. Your destination is 4 000 ly (1 ly = 1 light-year =
9.47 × 1015 m) from earth, as measured by an earth-based observer. (a) If the ship has a speed (relative to earth) of 0.9999c, how long will the trip take according to the clocks on board the ship? Express your answer in years.
(b) You have to pass by the sun on the way out of our solar system. According to the clocks on your ship, how much time (in minutes) will it take to get to
the sun from earth? The sun-earth mean distance is 1.50 × 1011 m. (c) The sun will not look spherical as you pass by. What is the ratio of the shortest
to the longest dimensions (i.e., the ratio of the semi-minor to the semi-major
axes) of the sun as you see it?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
29.1 Define wave–particle duality.
29.2 Explain the origin of Planck’s constant from blackbody radiation.
29.3 Use photon energy to explain in detail the photoelectric eff ect.
29.4 Use photon momentum to explain in detail the Compton eff ect.
29.5 Solve problems involving the de Broglie wavelength of a particle.
29.6 Calculate quantum uncertainty using the Heisenberg uncertainty principle.
S u su
m u N
is h in
ag a/
S ci
en ce
S o u rc
e
CHAPTER 29
Particles and Waves
This photograph shows a highly magnifi ed view of a female mosquito, made with a scanning electron
microscope (SEM). In the twentieth century, physicists were astonished when it was discovered that particles
could behave like waves. In fact, we will see in this chapter that there is a wavelength associated with
a moving particle such as an electron. The microscope used for the photograph takes advantage of the
electron wavelength, which can be made much smaller than that of visible light. It is this small electron
wavelength that is responsible for the exceptional resolution of fi ne detail in the photograph.
29.1 The Wave–Particle Duality The ability to exhibit interference eff ects is an essential characteristic of waves. For
instance, Section 27.2 discusses Young’s famous experiment in which light passes
through two closely spaced slits and produces a pattern of bright and dark fringes on
a screen (see Figure 27.3). The fringe pattern is a direct indication that interference is occurring between the light waves coming from each slit.
One of the most incredible discoveries of twentieth-century physics is that particles
can also behave like waves and exhibit interference eff ects. For instance, Interactive Figure 29.1 shows a version of Young’s experiment performed by directing a beam of electrons onto a double slit. In this experiment, the screen is like a television screen and glows wherever an electron strikes it. Part a of the drawing indicates the pattern that would be seen on the screen if each electron, behaving strictly as a particle, were
to pass through one slit or the other and strike the screen. The pattern would consist
of an image of each slit. Part b shows the pattern actually observed, which consists of bright and dark fringes, reminiscent of what is obtained when light waves pass through
a double slit. The fringe pattern indicates that the electrons are exhibiting the interfer-
ence eff ects associated with waves.
But how can electrons behave like waves in the experiment shown in Interactive Figure 29.1b? And what kind of waves are they? The answers to these profound 832
29.2 Blackbody Radiation and Planck’s Constant 833
questions will be discussed later in this chapter. For the moment, we intend only to emphasize
that the concept of an electron as a tiny discrete particle of matter does not account for the fact
that the electron can behave as a wave in some circumstances. In other words, the electron exhib-
its a dual nature, with both particle-like characteristics and wave-like characteristics.
Here is another interesting question: If a particle can exhibit wave-like properties, can
waves exhibit particle-like behavior? As the next three sections reveal, the answer is yes. In
fact, experiments that demonstrated the particle-like behavior of waves were performed near
the beginning of the twentieth century, before the experiments that demonstrated the wave-like
properties of the electrons. Scientists now accept the wave–particle duality as an essential part of nature:
Waves can exhibit particle-like characteristics, and particles can exhibit wave-like characteristics.
Section 29.2 begins the remarkable story of the wave–particle duality by discussing the elec-
tromagnetic waves that are radiated by a perfect blackbody. It is appropriate to begin with black-
body radiation, because it provided the fi rst link in the chain of experimental evidence leading to
our present understanding of the wave–particle duality.
29.2 Blackbody Radiation and Planck’s Constant All bodies, no matter how hot or cold, continuously radiate electromagnetic waves. For instance,
we see the glow of very hot objects because they emit electromagnetic waves in the visible re-
gion of the spectrum. Our sun, which has a surface temperature of about 6000 K, appears yellow,
while the cooler star Betelgeuse has a red-orange appearance due to its lower surface temperature
of 2900 K. However, at relatively low temperatures, cooler objects emit visible light waves only
weakly and, as a result, do not appear to be glowing. Certainly the human body, at only 310 K,
does not emit enough visible light to be seen in the dark with the unaided eye. But the body does
emit electromagnetic waves in the infrared region of the spectrum, and these can be detected with
infrared-sensitive devices.
At a given temperature, the intensities of the electromagnetic waves emitted by an object
vary from wavelength to wavelength throughout the visible, infrared, and other regions of the
spectrum. Figure 29.2 illustrates how the intensity per unit wavelength depends on wavelength for a perfect blackbody emitter. As Section 13.3 discusses, a perfect blackbody at a constant tem-
perature absorbs and reemits all the electromagnetic radiation that falls on it. The two curves in
Figure 29.2 show that at a higher temperature the maximum emitted intensity per unit wavelength increases and shifts to shorter wavelengths, toward the visible region of the spectrum. In account-
ing for the shape of these curves, the German physicist Max Planck (1858–1947) took the fi rst
step toward our present understanding of the wave–particle duality.
In 1900 Planck calculated the blackbody radiation curves, using a model that represents
a blackbody as a large number of atomic oscillators, each of which emits and absorbs electro-
magnetic waves. To obtain agreement between the theoretical and experimental curves, Planck
assumed that the energy E of an atomic oscillator could have only the discrete values of E = 0, hf, 2hf, 3hf, and so on. In other words, he assumed that
E = nhf n = 0, 1, 2, 3, . . . (29.1)
where n is either zero or a positive integer, f is the frequency of vibration (in hertz), and h is a constant now called Planck’s constant.* It has been determined experimentally that Planck’s constant has a value of
h = 6.626 068 96 × 10−34 J · s
INTERACTIVE FIGURE 29.1 (a) If electrons behaved as discrete particles with no wave
properties, they would pass through one or
the other of the two slits and strike the screen,
causing it to glow and produce exact images
of the slits. (b) In reality, the screen reveals a pattern of bright and dark fringes, similar
to the pattern produced when a beam of light
is used and interference occurs between the
light waves coming from each slit.
Screen
Double slit
Double slit
(b)
Screen
Double slit
Image of the double slit
Beam of electrons
Beam of electrons
(a)
6000 K
Visible
4000 K
0 500 1000 Wavelength (nm)
R ad
ia ti
on in
te ns
it y
pe r
un it
w av
el en
gt h
1500
FIGURE 29.2 The electromagnetic radiation emitted by a perfect blackbody has an intensity
per unit wavelength that varies from
wavelength to wavelength, as each curve
indicates. At the higher temperature, the
intensity per unit wavelength is greater, and
the maximum occurs at a shorter wavelength. *It is now known that the energy of a harmonic oscillator is E = (n + 12 )hf; the extra term of
1
2 is unimportant to the
present discussion.
834 CHAPTER 29 Particles and Waves
The radical feature of Planck’s assumption was that the energy of an atomic oscillator could
have only discrete values (hf, 2hf, 3hf, etc.), with energies in between these values being for- bidden. Whenever the energy of a system can have only certain defi nite values, and nothing in
between, the energy is said to be quantized. This quantization of the energy was unexpected on the basis of the traditional physics of the time. However, it was soon realized that energy quant-
ization had wide-ranging and valid implications.
Conservation of energy requires that the energy carried off by the radiated electromag-
netic waves must equal the energy lost by the atomic oscillators in Planck’s model. Suppose, for
example, that an oscillator with an energy of 3hf emits an electromagnetic wave. According to Equation 29.1, the next smallest allowed value for the energy of the oscillator is 2hf. In such a case, the energy carried off by the electromagnetic wave would have the value of hf, equaling the amount of energy lost by the oscillator. Thus, Planck’s model for blackbody radiation sets
the stage for the idea that electromagnetic energy occurs as a collection of discrete amounts, or
packets, of energy, with the energy of a packet being equal to hf. Einstein made the proposal that light consists of such energy packets.
29.3 Photons and the Photoelectric Eff ect We have seen in Chapter 24 that light is an electromagnetic wave and that such waves are con-
tinuous patterns of electric and magnetic fi elds. It is not unexpected, then, that light beams, such
as those in the photograph in Figure 29.3, or those coming from fl ashlights, look like continuous beams. However, we must now discuss the surprising fact that visible light and all other types
of electromagnetic waves are composed of discrete particle-like entities called photons. As dis- cussed in Chapters 6 and 7, the total energy E and the linear momentum p→ are fundamental concepts in physics that apply to moving particles such as electrons and protons. The total energy
of a (nonrelativistic) particle is the sum of its kinetic energy (KE) and potential energy (PE), or
E = KE + PE. The magnitude p of the particle’s momentum is the product of its mass m and speed 𝜐, or p = m𝜐. We will see that the ideas of energy and momentum also apply to photons. The defi ning equations for photon energy and photon momentum, however, are not the same as
they are for particles such as electrons and protons.
Experimental evidence that light consists of photons comes from a phenomenon called the
photoelectric eff ect, in which electrons are emitted from a metal surface when light shines on it. Interactive Figure 29.4 illustrates the eff ect. The electrons are emitted if the light being used has a suffi ciently high frequency. The ejected electrons move toward a positive electrode
called the collector and cause a current to register on the ammeter. Because the electrons are ejected with the aid of light, they are called photoelectrons. As will be discussed shortly, a number of features of the photoelectric eff ect could not be explained solely with the ideas of
classical physics.
In 1905 Einstein presented an explanation of the photoelectric eff ect that took advantage of
Planck’s work concerning blackbody radiation. It was primarily for his theory of the photoelec-
tric eff ect that he was awarded the Nobel Prize in physics in 1921. In his photoelectric theory,
Einstein proposed that light of frequency f could be regarded as a collection of discrete packets of energy (photons), each packet containing an amount of energy E given by
Energy of a photon E = hf (29.2)
where h is Planck’s constant. The light energy given off by a light bulb, for instance, is carried by photons. The brighter the bulb, the greater is the number of photons emitted per second. Example 1
estimates the number of photons emitted per second by a typical light bulb.
FIGURE 29.3 Although the spotlight beams in the photograph look like continuous beams
of light, each is composed of discrete photons.
Albert Normandin/Masterfi le
Light
Photoelectrons
Ammeter
Phototube (evacuated)
Metal plate (negative)
Collector (positive)
+ –
V
INTERACTIVE FIGURE 29.4 In the photo- electric eff ect, light with a suffi ciently high
frequency ejects electrons from a metal
surface. These photoelectrons, as they are
called, are drawn to the positive collector,
thus producing a current.
EXAMPLE 1 Photons from a Light Bulb
In converting electrical energy into light energy, a sixty-watt incandescent
light bulb operates at about 2.1% effi ciency. Assuming that all the light
is green light (vacuum wavelength = 555 nm), determine the number of
photons per second given off by the bulb.
29.3 Photons and the Photoelectric Eff ect 835
According to Einstein, when light shines on a metal, a photon can give up its energy to an
electron in the metal. If the photon has enough energy to do the work of removing the electron
from the metal, the electron can be ejected. The work required depends on how strongly the
electron is held. For the least strongly held electrons, the necessary work has a minimum value W0 and is called the work function of the metal. If a photon has energy in excess of the work needed to remove an electron, the excess appears as kinetic energy of the ejected electron. Thus,
the least strongly held electrons are ejected with the maximum kinetic energy KEmax. Einstein
applied the conservation-of-energy principle and proposed the following relation to describe the
photoelectric eff ect:
hf = KEmax + W0 (29.3)
According to this equation, KEmax = hf − W0, which is plotted in Figure 29.5, with KEmax along the y axis and f along the x axis. The graph is a straight line that crosses the x axis at f = f0. At this frequency, the electron departs from the metal with no kinetic energy (KEmax = 0 J). According
to Equation 29.3, when KEmax = 0 J the energy hf0 of the incident photon is equal to the work function W0 of the metal: hf0 = W0.
The photon concept provides an explanation for a number of features of the photoelectric
experiment that are diffi cult to explain without photons. It is observed, for instance, that only light
with a frequency above a certain minimum value f0 will eject electrons. If the frequency is below this value, no electrons are ejected, regardless of how intense the light is. Example 2 determines
the minimum frequency value for a silver surface. }
Photon
energy
}
Maximum
kinetic energy
of ejected
electron
}
Minimum
work needed to
eject electron
Reasoning The number of photons emitted per second can be found by dividing the amount of light energy emitted per second by the energy
E of one photon. The energy of a single photon is E = hf, according to Equation 29.2. The frequency f of the photon is related to its wavelength 𝜆 by Equation 16.1 as f = c/𝜆.
Solution At an effi ciency of 2.1%, the light energy emitted per second by a sixty-watt bulb is (0.021)(60.0 J/s) = 1.3 J/s. The energy of a single photon is
E = hf = hc λ
= (6.63 × 10−34 J · s)(3.00 × 10 8 m /s)
555 × 10−9 m = 3.58 × 10−19 J
Therefore,
Number of
photons emitted
per second
= 1.3 J/s
3.58 × 10−19 J/photon = 3.6 × 10 18 photons/s
K E
m ax
o f
ej ec
te d
el ec
tr on
f0 Light frequency, f
FIGURE 29.5 Photons can eject electrons from a metal when the light frequency is
above a minimum value f0. For frequencies above this value, ejected electrons have
a maximum kinetic energy KEmax that is
linearly related to the frequency, as the graph
shows.
EXAMPLE 2 | The Photoelectric Eff ect for a Silver Surface
The work function for a silver surface is W0 = 4.73 eV. Find the minimum frequency that light must have to eject electrons from this surface.
Reasoning The minimum frequency f0 is that frequency at which the photon energy equals the work function W0 of the metal, so the electron is ejected with zero kinetic energy. Since 1 eV = 1.60 × 10−19 J, the work
function expressed in joules is
W0 = (4.73 eV )(1.60 × 10 −19 J
1 eV ) = 7.57 × 10−19 J Using Equation 29.3, we fi nd
hf0 = KEmax + W0 or f0 = W0 h
= 0 J
}
Problem-Solving Insight The work function of a metal is the minimum energy needed to eject an electron from the metal. An electron that has received this minimum energy has no kinetic energy once outside the metal.
Solution The minimum frequency f0 is
f0 = W0 h
= 7.57 × 10−19 J
6.63 × 10−34 J · s = 1.14 × 10 15 Hz
Photons with frequencies less than f0 do not have enough energy to eject electrons from a silver surface. Since 𝜆0 = c/f0, the wavelength of this light is 𝜆0 = 263 nm, which is in the ultraviolet region of the electromagnetic spectrum.
In Example 2 the electrons are ejected with no kinetic energy, because the light shining on
the silver surface has the minimum possible frequency that will eject them. When the frequency
of the light exceeds this minimum value, the electrons that are ejected do have kinetic energy. The
next example deals with such a situation.
836 CHAPTER 29 Particles and Waves
Analyzing Multiple -Concept Problems
EXAMPLE 3 The Maximum Speed of Ejected Photoelectrons
Light with a wavelength of 95 nm shines on a selenium surface, which has
a work function of 5.9 eV. The ejected electrons have some kinetic energy.
Determine the maximum speed with which electrons are ejected.
Reasoning The maximum speed of the ejected electrons is related to their maximum kinetic energy. Conservation of energy dictates that this
maximum kinetic energy is related to the work function of the surface
and the energy of the incident photons. The work function is given. The
energy of the photons can be obtained from the frequency of the light,
which is related to the wavelength.
Knowns and Unknowns We have the following data:
Description Symbol Value Comment Wavelength of light 𝜆 95 nm 1 nm = 10−9 m
Work function of selenium surface W0 5.9 eV Will be converted to joules.
Unknown Variable Maximum speed of photoelectrons 𝜐max ?
Modeling the Problem
STEP 1 Kinetic Energy and Speed The maximum kinetic energy KEmax of the ejected elec- trons is KEmax =
1
2 mυ 2max (Equation 6.2), where m is the mass of an electron. Solving for the maximum speed 𝜐max gives Equation 1 at the right. The mass of the electron is m = 9.11 × 10−31 kg (see inside of front cover). The maximum kinetic energy is unknown, but we will evaluate it in
Step 2.
STEP 2 Conservation of Energy According to the principle of conservation of energy, as expressed by Equation 29.3, we have
hf = KEmax + W0
where f is the frequency of the light. Solving for KEmax gives
KEmax = hf − W0 (2)
which can be substituted into Equation 1, as shown at the right. In this expression the work func-
tion W0 is known, and we will deal with the unknown frequency f in Step 3.
STEP 3 Relationship Between Frequency and Wavelength The frequency and wavelength of the light are related to the speed of light c according to f𝜆 = c (Equation 16.1). Solving for the frequency gives
f = c λ
which we substitute into Equation 2, as shown at the right.
Solution Combining the results of each step algebraically, we fi nd that
υmax = √ 2KE maxm = √ 2(hf − W0)
m = √2(h
c λ
− W0) m
}
Photon
energy
}
Maximum
kinetic energy
of ejected
electron
}
Minimum
work needed to
eject electron
STEP 3STEP 2STEP 1
υmax = √ 2KE maxm (1) ?
υmax = √ 2KE maxm (1) KEmax = hf − W0 (2)
?
υmax = √ 2KE maxm (1) KEmax = hf − W0 (2)
f = c λ
29.3 Photons and the Photoelectric Eff ect 837
Another signifi cant feature of the photoelectric eff ect is that the maximum kinetic energy of
the ejected electrons remains the same when the intensity of the light increases, provided the light
frequency remains the same. As the light intensity increases, more photons per second strike the
metal, and consequently more electrons per second are ejected. However, since the frequency is
the same for each photon, the energy of each photon is also the same. Thus, the ejected electrons
always have the same maximum kinetic energy.
Whereas the photon model of light explains the photoelectric eff ect satisfactorily, the elec-
tromagnetic wave model of light does not. Certainly, it is possible to imagine that the electric
fi eld of an electromagnetic wave would cause electrons in the metal to oscillate and tear free from
the surface when the amplitude of oscillation becomes large enough. However, were this the case,
higher-intensity light would eject electrons with a greater maximum kinetic energy, a fact that
experiment does not confi rm. Moreover, in the electromagnetic wave model, a relatively long
time would be required with low-intensity light before the electrons would build up a suffi ciently
large oscillation amplitude to tear free. Instead, experiment shows that even the weakest light
intensity causes electrons to be ejected almost instantaneously, provided the frequency of the
light is above the minimum value f0. The failure of the electromagnetic wave model to explain the photoelectric eff ect does not mean that the wave model should be abandoned. However, we must
recognize that the wave model does not account for all the characteristics of light. The photon
model also makes an important contribution to our understanding of the way light behaves when
it interacts with matter.
Because a photon has energy, the photon can eject an electron from a metal surface when
it interacts with the electron. However, a photon is diff erent from a normal particle. A normal
particle has a mass and can travel at speeds up to, but not equal to, the speed of light. A photon,
on the other hand, travels at the speed of light in a vacuum and does not exist as an object at rest.
The energy of a photon is entirely kinetic in nature, because it has no rest energy and no mass. To
show that a photon has no mass, we rewrite Equation 28.4 for the total energy E as
E √1 − υ 2
c 2 = mc 2
The term √1 − (υ 2/c 2) is zero because a photon travels at the speed of light, υ = c. Since the energy E of the photon is fi nite, the left side of the equation above is zero. Thus, the right side must also be zero, so m = 0 kg and the photon has no mass.
THE PHYSICS OF . . . charge-coupled devices and digital cameras. One of the most exciting and useful applications of the photoelectric eff ect is the charge-coupled device
(CCD). An array of these devices is used instead of fi lm in digital cameras (see Figure 29.6) to capture images in the form of many small groups of electrons. CCD arrays are also used in
digital camcorders and electronic scanners, and they provide the method of choice with which
astronomers capture those spectacular images of the planets and the stars. For use with visible
light, a CCD array consists of a sandwich of semiconducting silicon, insulating silicon dioxide,
and a number of electrodes, as Figure 29.7 shows. The array is divided into many small sections,
Thus, the maximum speed of the photoelectrons is
υmax = √2 (h c λ
− W0) m
υmax = √2 [ (6.63 × 10 −34 J · s)
(3.00 × 10 8 m/s)
(95 × 10−9 m) − (5.9 eV)
(1.60 × 10−19 J)
(1 eV) ] 9.11 × 10−31 kg
= 1.6 × 10 6 m /s
Note that in this calculation we have converted the value of the work function from electron volts
to joules.
Related Homework: Problems 8, 50
838 CHAPTER 29 Particles and Waves
or pixels, sixteen of which are shown in the drawing. Each pixel captures a small part of a picture.
Digital cameras can have up to 24 million pixels, depending on price. The greater the number
of pixels, the better is the resolution of the photograph. The blow-up in Figure 29.7 shows a single pixel. Incident photons of visible light strike the silicon and generate electrons via the
photoelectric eff ect. The range of energies of the visible photons is such that approximately one
electron is released when a photon interacts with a silicon atom. The electrons do not escape from
the silicon, but are trapped within a pixel because of a positive voltage applied to the electrodes
beneath the insulating layer. Thus, the number of electrons that are released and trapped is pro-
portional to the number of photons striking the pixel. In this fashion, each pixel in the CCD array
accumulates an accurate representation of the light intensity at that point on the image. Color in-
formation is provided using red, green, or blue fi lters or a system of prisms to separate the colors.
Astronomers use CCD arrays not only in the visible region of the electromagnetic spectrum but
in other regions as well.
In addition to trapping the photoelectrons, the electrodes beneath the pixels are used to read
out the electron representation of the picture. By changing the positive voltages applied to the
electrodes, it is possible to cause all of the electrons trapped in one row of pixels to be transferred
to the adjacent row. In this fashion, for instance, row 1 in Figure 29.7 is transferred into row 2, row 2 into row 3, and row 3 into the bottom row, which serves a special purpose. The bottom row
functions as a horizontal shift register, from which the contents of each pixel can be shifted to the
right, one at a time, and read into an analog signal processor. This processor senses the varying
number of electrons in each pixel in the shift register as a kind of wave that has a fl uctuating amp-
litude. After another shift in rows, the information in the next row is read out, and so forth. The
output of the analog signal processor is sent to an analog-to-digital converter, which produces a
digital representation of the image in terms of the zeros and ones that computers recognize.
THE PHYSICS OF . . . a safety feature of garage door openers. Another application of the photoelectric eff ect depends on the fact that the moving photoelectrons in Interactive Figure 29.4 constitute a current—a current that changes as the intensity of the light changes. All automatic garage door openers have a safety feature that prevents the door from closing when
it encounters an obstruction (person, vehicle, etc.). As Figure 29.8 illustrates, a sending unit transmits an invisible (infrared) beam across the opening of the door. The beam is detected by a
receiving unit that contains a photodiode. A photodiode is a type of p-n junction diode (see Sec- tion 23.5). When infrared photons strike the photodiode, electrons bound to the atoms absorb the
photons and become liberated. These liberated, mobile electrons cause the current in the photo-
diode to increase. When a person walks through the beam, the light is momentarily blocked from
reaching the receiving unit, and the current in the photodiode decreases. The change in current is
sensed by electronic circuitry that immediately stops the downward motion of the door and then
causes it to rise up.
THE PHYSICS OF . . . photoevaporation and star formation. Figure 29.9a shows a portion of the Eagle Nebula, a giant star-forming region some 7000 light-years from earth. The
photo was taken by the Hubble Space Telescope and reveals clouds of molecular gas and dust,
in which there is dramatic evidence of the energy carried by photons. These clouds extend more
than a light-year from base to tip and are the birthplace of stars. A star begins to form within a
cloud when the gravitational force pulls together suffi cient gas to create a high-density “ball.”
Analog signal processor
Horizontal shift register
Row 3
Row 2
Row 1
Electrodes
Electron
Pixel
Semiconducting silicon
Incident visible photon
Insulating silicon dioxide
Analog-to- digital converter
Digital representation of the picture
FIGURE 29.7 A CCD array can be used to capture photographic images using the
photoelectric eff ect.
Sending unit
Infrared light beam
Receiving unit
FIGURE 29.8 When an obstruction prevents the infrared light beam from reaching the
receiving unit, the current in the receiving
unit drops. This drop in current is detected by
an electronic circuit that stops the downward
movement of the garage door and then causes
it to rise.
FIGURE 29.6 Digital cameras like this one use an array of
charge-coupled devices instead
of fi lm to capture an image. © Y
en H
u n g /S
h u tt
er st
o ck
29.3 Photons and the Photoelectric Eff ect 839
When the gaseous ball becomes suffi ciently dense, thermonuclear fusion (see Section 32.5)
occurs at its core, and the star begins to shine. The newly born stars are buried within the cloud
and cannot be seen from earth. However, the process of photoevaporation allows astronomers to
see many of the high-density regions where stars are being formed. Photoevaporation is the pro-
cess in which high-energy, ultraviolet (UV) photons from hot stars outside the cloud heat it up,
much like microwave photons heat food in a microwave oven. Figure 29.9a shows streamers of gas photoevaporating from the cloud as it is illuminated by stars located beyond the photograph’s
upper edge. As photoevaporation proceeds, globules of gas that are denser than their surround-
ings are exposed. The globules are known as evaporating gaseous globules (EGGs), and they are slightly larger than our solar system. The drawing in part b of Figure 29.9 shows that the EGGs shade the gas and dust behind them from the UV photons, creating the many fi nger-like protru-
sions seen on the surface of the cloud. Astronomers believe that some of these EGGs contain
young stars within them.
Check Your Understanding
(The answers are given at the end of the book.) 1. The photons emitted by a source of light do not all have the same energy. Is the source monochromatic?
(A monochromatic light source emits light that has a single wavelength.)
2. Which colored light bulb—red, orange, yellow, green, or violet—emits photons with (a) the least energy and (b) the greatest energy? (See Example 1 in Chapter 24.)
3. Does a photon emitted by a higher-wattage red light bulb have more energy than a photon emitted by a lower-wattage red bulb?
4. Radiation of a given wavelength causes electrons to be emitted from the surface of metal 1 but not from the surface of metal 2. Why could this be? (a) Metal 1 has a greater work function than metal 2 has. (b) Metal 1 has a smaller work function than metal 2 has. (c) The energy of a photon striking metal 1 is greater than the energy of a photon striking metal 2.
5. In the photoelectric eff ect, electrons are ejected from the surface of a metal when light shines on it. Which one or more of the following would lead to an increase in the maximum kinetic energy of
the ejected electrons? (a) Increasing the frequency of the incident light (b) Increasing the number of photons per second striking the surface (c) Using photons whose frequency f0 is less than W0/h, where W0 is the work function of the metal and h is Planck’s constant (d) Selecting a metal that has a greater work function
6. In the photoelectric eff ect, suppose that the intensity of the light is increased, while the frequency of the light is kept constant. The frequency is greater than the minimum frequency f0. State whether each of the following will increase, decrease, or remain the same: (a) The current in the phototube (b) The number of electrons emitted per second from the metal surface (c) The maximum kinetic energy that an electron could have (d) The maximum momentum that an electron could have
FIGURE 29.9 (a) Photoevaporation produces fi nger-like projections on the surface of the gas clouds in the Eagle Nebula. At the fi ngertips are high-density evaporating gaseous globules (EGGs). (b) This drawing illustrates the photoevaporation that is occurring in the photograph in part a.
EGG
UV photons Cloud of gas
(b)
Streaming gas
“Fingers” containing EGGs at their tips
(a)
C o u rt
es y N
A S
A
840 CHAPTER 29 Particles and Waves
29.4 The Momentum of a Photon and the Compton Eff ect Although Einstein presented his photon model for the photoelectric eff ect in 1905, it was not until
1923 that the photon concept began to achieve widespread acceptance. It was then that the Amer-
ican physicist Arthur H. Compton (1892–1962) used the photon model to explain his research on
the scattering of X-rays by the electrons in graphite. X-rays are high-frequency electromagnetic
waves and, like light, they are composed of photons.
Animated Figure 29.10 illustrates what happens when an X-ray photon strikes an electron in a piece of graphite. Like two billiard balls colliding on a pool table, the X-ray photon scatters in
one direction after the collision, and the electron recoils in another direction. Compton observed
that the scattered photon has a frequency fʹ that is smaller than the frequency f of the incident photon, indicating that the photon loses energy during the collision. In addition, he found that
the diff erence between the two frequencies depends on the angle 𝜃 at which the scattered photon leaves the collision. The phenomenon in which an X-ray photon is scattered from an electron,
with the scattered photon having a smaller frequency than the incident photon, is called the
Compton eff ect. In Section 7.3, collisions between two objects are analyzed using the fact that the total
kinetic energy and the total linear momentum of the objects are the same before and after an
elastic collision. Similar analysis can be applied to the collision between a photon and an elec-
tron. The electron is assumed to be initially at rest and essentially free—that is, not bound to the
atoms of the material. According to the principle of conservation of energy,
hf = hf ʹ + KE (29.4)
where the relation E = hf has been used for the photon energies. It follows, then, that hf ʹ = hf − KE, which shows that the energy and corresponding frequency f ʹ of the scattered photon are less than the energy and frequency of the incident photon, just as Compton observed.
Since 𝜆ʹ = c/f ʹ (Equation 16.1), the wavelength of the scattered X-rays is larger than that of the incident X-rays.
For an initially stationary electron, conservation of total linear momentum requires that
p→ = p→′ + p→ electron (29.5)
Energy of
incident
photon
}
Energy of
scattered
photon
}
Kinetic energy
of recoil
electron
}
Momentum of
incident photon
Momentum of
scattered photon
Momentum
of recoil
electron
Incident X-ray photon
Electron at rest
Recoil electron
Scattered X-ray photon
θ ϕ
+y
+x
ANIMATED FIGURE 29.10 In an experiment performed by Arthur H. Compton, an X-ray
photon collides with a stationary electron. The
scattered photon and the recoil electron depart
from the collision in diff erent directions.
Incident X-ray photon
Electron at rest
Recoil electron
Scattered X-ray photon
θ ϕ
+y
+x
ANIMATED FIGURE 29.10 (REPEATED) In an experiment performed by Arthur H.
Compton, an X-ray photon collides with a
stationary electron. The scattered photon and
the recoil electron depart from the collision in
diff erent directions.
Math Skills Equation 29.5 is a relationship between the momentum p→ of the incident photon, the momentum p→′ of the scattered photon, and the momentum p→ electron of the recoil electron in Animated Figure 29.10. These momenta are vector quantities. Therefore, Equation 29.5 is equivalent to two equations; one is for the x components of the vectors and one for the y components of the vectors (see Sections 1.7 and 1.8). Using components with respect to the x, y axis in Animated Figure 29.10, we can see that the following two equations are equivalent to Equation 29.5:
x component p = p′cos θ + pelectron cos ϕ
y component 0 = −p′sin θ + pelectron sin ϕ
In these equations, the symbols p and p′ denote the vector magnitudes of the momenta. Note that the y component of the momentum is zero for the incident photon, because that photon travels along the x axis in Animated Figure 29.10. Note also that the y component of the momentum is negative for the scattered photon, because the direction in which that photon travels is below the x axis.
Recoil electronScattered photon
Incident photon
Recoil electronScattered photon
Incident photon
29.4 The Momentum of a Photon and the Compton Eff ect 841
To fi nd an expression for the magnitude p of a photon’s momentum, we use Equations 28.3 and 28.4. According to these equations, the momentum p and the total energy E of any particle are
p = mυ
√1 − (υ 2/c 2) (28.3)
E = mc 2
√1 − (υ 2/c 2) (28.4)
Rearranging Equation 28.4 to show that m
√1 − (υ 2/c 2) =
E c 2
and substituting this result into
Equation 28.3 gives
p = mυ
√1 − (υ 2/c 2) =
Eυ c 2
A photon travels at the speed of light, so that we have υ = c, and the momentum of a photon is
p = Eυ c2
= Ec c2
= E c
This result only applies to a photon and does not apply to a particle with mass, because such a
particle cannot travel at the speed of light. We also know that the energy of a photon is related to
its frequency f according to E = hf (Equation 29.2) and that the speed c of a photon is related to its frequency and wavelength 𝜆 according to c = f𝜆 (Equation 16.1). With these substitutions, our expression for the momentum of a photon becomes
p = E c =
hf fλ
= h λ
(29.6)
Using Equations 29.4, 29.5, and 29.6, Compton showed that the diff erence between the wavelength
𝜆ʹ of the scattered photon and the wavelength 𝜆 of the incident photon is related to the scattering angle 𝜃 by
λ′ − λ = h
mc (1 − cos θ ) (29.7)
In this equation m is the mass of the electron. The quantity h/(mc) is called the Compton wavelength of the electron and has the value h/(mc) = 2.43 × 10−12 m. Since cos 𝜃 varies between +1 and −1, the shift 𝜆ʹ − 𝜆 in the wavelength can vary between zero and 2h/(mc), depending on the value of 𝜃, a fact observed by Compton.
The photoelectric eff ect and the Compton eff ect provide compelling evidence that light can
exhibit particle-like characteristics attributable to energy packets called photons. But what about
the interference phenomena discussed in Chapter 27, such as Young’s double-slit experiment
and single-slit diff raction, which demonstrate that light behaves as a wave? Does light have two
distinct personalities, in which it behaves like a stream of particles in some experiments and like
a wave in others? The answer is yes, for physicists now believe that this wave–particle duality is
an inherent property of light. Light is a far more interesting (and complex) phenomenon than just
a stream of particles or an electromagnetic wave.
In the Compton eff ect the electron recoils because it gains some of the photon’s momentum.
In principle, then, the momentum that photons have can be used to make other objects move.
Conceptual Example 4 considers a propulsion system for an interstellar spaceship that is based
on the momentum of a photon.
CONCEPTUAL EXAMPLE 4 The Physics of Solar Sails and Spaceship Propulsion
One propulsion method that is currently being studied for interstellar
travel uses a large sail. The intent is that sunlight striking the sail will cre-
ate a force that pushes the ship away from the sun (Figure 29.11), much as the wind propels a sailboat. To get the greatest possible force, the surface
of the sail facing the sun (a) should be shiny like a mirror, (b) should be black, or (c) could be either shiny or black, since the same force will be created for either type of surface.
Reasoning In Conceptual Example 3 in Chapter 7, we found that hail- stones striking the roof of a car exert a force on it because the collision
changes their momentum. Photons also have momentum, so, like the hail-
stones, they can apply a force to the sail.
As in Chapter 7, we will be guided by the impulse–momentum
theorem (Equation 7.4) in assessing the force. This theorem states that
when a net force acts on an object, the impulse of the net force is equal to
842 CHAPTER 29 Particles and Waves
Check Your Understanding
(The answers are given at the end of the book.) 7. In the Compton eff ect, an incident X-ray photon of wavelength 𝜆 is scattered by an electron, and the
scattered photon has a wavelength of 𝜆ʹ. Suppose that the incident photon is scattered by a proton in- stead of an electron. For a given scattering angle 𝜃, is the change 𝜆ʹ − 𝜆 in the wavelength of the photon scattered by the proton greater than, less than, or the same as the wavelength of the photon scattered by
the electron? (Hint: Use Equation 29.7 for a proton instead of an electron.) 8. In a Compton scattering experiment, an incident X-ray photon is traveling along the +x direction. An
electron, initially at rest, is struck by the photon and is accelerated straight ahead in the same direction
as the incident X-ray photon. Which way does the scattered photon move? (a) Along the +y direction (b) Along the −y direction (c) Along the −x direction (Hint: Use the principle of conservation of momentum to guide your reasoning.)
9. The speed of a particle is much less than the speed of light. Thus, when the particle’s speed doubles,
the particle’s momentum doubles, and its kinetic en-
ergy becomes four times greater. However, when the
momentum of a photon doubles, its energy becomes
(a) two times greater (b) four times greater (c) one-half as much (d) one-fourth as much.
10. Review Conceptual Example 4 as background for this question. CYU Figure 29.1 shows a device called a radiometer. The four regular panels are black on one
side and shiny like a mirror on the other side. In bright
light, the panel arrangement spins around in a direction
from the black side of a panel toward the shiny side. Do
photon collisions with both sides of the panels cause the
observed spinning?
the change in momentum of the object. Greater impulses lead to greater
forces for a given time interval. Thus, when a photon collides with the
sail, the photon’s momentum changes because of the force that the sail
applies to the photon. Newton’s action–reaction law (Section 4.5) indic-
ates that the photon simultaneously applies a force of equal magnitude,
but opposite direction, to the sail. It is this reaction force that propels
the spaceship, and it will be greater when the momentum change experi-
enced by the photon is greater. The surface of the sail facing the sun, then,
should be such that it causes the largest possible momentum change for
the impinging photons.
Answers (b) and (c) are incorrect. In Conceptual Example 3 in Chapter 7 we examined whether hailstones or raindrops exert the greater
force when they strike the roof of a car. The diff erence is that hailstones,
being hard objects, bounce off the roof, while raindrops splatter and do not
bounce very much. We concluded that hailstones, because of the bounce,
experience a greater change in momentum than raindrops do, so the roof
exerts a greater force on the hailstones. By Newton’s action–reaction law,
the car roof, then, experiences a greater force from the hailstones than
from the raindrops. We saw in Section 13.3 that radiation is refl ected from
a shiny mirror-like surface and is absorbed by a black surface. Therefore,
by analogy with raindrops that stick to the car roof, the sail experiences a
smaller force when the surface facing the sun is black.
Answer (a) is correct. The sun’s radiation refl ects from a shiny mirror- like surface and is absorbed by a black surface. Now, consider a photon
that strikes the sail perpendicularly. When a photon refl ects from a mir-
ror-like surface, the photon’s momentum changes from its value in the for-
ward direction to a value of the same magnitude in the reverse direction.
This is a greater change than the one that occurs when the photon is ab-
sorbed by a black surface. In the latter case, the momentum changes only
from its value in the forward direction to a value of zero. Consequently,
the surface of the sail facing the sun should be shiny in order to produce
the greatest possible propulsion force. A shiny surface causes the photons
to bounce like hailstones on the roof of a car and, in doing so, to apply a
greater force to the sail.
Related Homework: Problem 51
Sunlight
FIGURE 29.11 A solar sail provides the propulsion for this interstellar spaceship.
CYU FIGURE 29.1
C h ar
le s
D . W
in te
rs /S
ci en
ce S
o u rc
e
29.5 The De Broglie Wavelength and the Wave Nature of Matter 843
29.5 The De Broglie Wavelength and the Wave Nature of Matter As a graduate student in 1923, Louis de Broglie (1892–1987) made the astounding suggestion
that since light waves could exhibit particle-like behavior, particles of matter should exhibit
wave-like behavior. De Broglie proposed that all moving matter has a wavelength associated with
it, just as a wave does. He made the explicit proposal that the wavelength 𝜆 of a particle is given by the same relation (Equation 29.6) that applies to a photon:
De Broglie wavelength λ = h p (29.8)
where h is Planck’s constant and p is the magnitude of the relativistic momentum of the particle. Today, 𝜆 is known as the de Broglie wavelength of the particle.
Confi rmation of de Broglie’s suggestion came in 1927 from the experiments of the American
physicists Clinton J. Davisson (1881–1958) and Lester H. Germer (1896–1971) and, independ-
ently, those of the English physicist George P. Thomson (1892–1975). Davisson and Germer
directed a beam of electrons onto a crystal of nickel and observed that the electrons exhibited
a diff raction behavior, analogous to that seen when X-rays are diff racted by a crystal (see Sec-
tion 27.9 for a discussion of X-ray diff raction). The wavelength of the electrons revealed by the
diff raction pattern matched that predicted by de Broglie’s hypothesis, 𝜆 = h/p. More recently, Young’s double-slit experiment has been performed with electrons and reveals the eff ects of
wave interference illustrated in Interactive Figure 29.1. Particles other than electrons can also exhibit wave-like properties. For instance, neut-
rons are sometimes used in diff raction studies of crystal structure. Figure 29.12 compares the neutron diff raction pattern and the X-ray diff raction pattern caused by a crystal of rock
salt (NaCl).
Although all moving particles have a de Broglie wavelength, the eff ects of this wavelength
are observable only for particles whose masses are very small, on the order of the mass of an
electron or a neutron, for instance. Example 5 illustrates why. FIGURE 29.12 (a) The neutron diff raction
pattern and (b) the X-ray diff raction pattern for a crystal of sodium chloride (NaCl).
(b)
Courtesy Edwin Jones, University of South Carolina
From “Phys. Rev.” 73:527 (1948), by Wollan, Shull
and Marney. ©1948 by the American Physical Society
(a)
EXAMPLE 5 The De Broglie Wavelength of an Electron and of a Baseball
Determine the de Broglie wavelength for (a) an electron (mass = 9.1 × 10−31 kg) moving at a speed of 6.0 × 106 m/s and (b) a baseball (mass = 0.15 kg) moving at a speed of 13 m/s.
Reasoning In each case, the de Broglie wavelength is given by Equation 29.8 as Planck’s constant divided by the magnitude of the momentum.
Since the speeds are small compared to the speed of light, we can ignore
relativistic eff ects and express the magnitude of the momentum as the
product of the mass and the speed, as in Equation 7.2.
Solution (a) Since the magnitude p of the momentum is the product of the mass m of the particle and its speed υ, we have p = mυ (Equation 7.2). Using this expression in Equation 29.8 for the de Broglie wavelength, we
obtain
λ = h p
= h
mυ =
6.63 × 10−34 J · s (9.1 × 10−31 kg)(6.0 × 10 6 m/s)
= 1.2 × 10−10 m
A de Broglie wavelength of 1.2 × 10−10 m is about the size of the
interatomic spacing in a solid, such as the nickel crystal used by
Davisson and Germer, and, therefore, leads to the observed diffrac-
tion effects.
(b) A calculation similar to that in part (a) shows that the de Broglie wavelength of the baseball is λ = 3.3 × 10−34 m . This wavelength is incredibly small, even by comparison with the size of an atom (10−10 m)
or a nucleus (10−14 m). Thus, the ratio 𝜆/W of this wavelength to the width W of an ordinary opening, such as a window, is so small that the diff rac- tion of a baseball passing through the window cannot be observed.
The de Broglie equation for particle wavelength provides no hint as to what kind of wave is
associated with a particle of matter. To gain some insight into the nature of this wave, we turn our
attention to Figure 29.13. Part a shows the fringe pattern on the screen when electrons are used in a version of Young’s double-slit experiment. The bright fringes occur in places where particle
844 CHAPTER 29 Particles and Waves
waves coming from each slit interfere constructively, while the dark fringes occur in places where
the waves interfere destructively.
When an electron passes through the double-slit arrangement and strikes a spot on the
screen, the screen glows at that spot, and parts b, c, and d of Figure 29.13 illustrate how the spots accumulate in time. As more and more electrons strike the screen, the spots eventually form the
fringe pattern that is evident in part d. Bright fringes occur where there is a high probability of electrons striking the screen, and dark fringes occur where there is a low probability. Here lies
the key to understanding particle waves. Particle waves are waves of probability, waves whose magnitude at a point in space gives an indication of the probability that the particle will be found
at that point. At the place where the screen is located, the pattern of probabilities conveyed by the
particle waves causes the fringe pattern to emerge. The fact that no fringe pattern is apparent in
part b of the fi gure does not mean that there are no probability waves present; it just means that too few electrons have struck the screen for the pattern to be recognizable.
The pattern of probabilities that leads to the fringes in Figure 29.13 is analogous to the pattern of light intensities that is responsible for the fringes in Young’s original experiment with
light waves (see Figure 27.3). Section 24.4 discusses the fact that the intensity of the light is
proportional to either the square of the electric fi eld strength or the square of the magnetic fi eld
strength of the wave. In an analogous fashion in the case of particle waves, the probability is
proportional to the square of the magnitude (Greek letter psi) of the wave. is referred to as
the wave function of the particle. In 1925 the Austrian physicist Erwin Schrödinger (1887–1961) and the German physicist
Werner Heisenberg (1901–1976) independently developed theoretical frameworks for deter-
mining the wave function. In so doing, they established a new branch of physics called quantum mechanics. The word “quantum” refers to the fact that in the world of the atom, where particle waves must be considered, the particle energy is quantized, so only certain energies are allowed.
To understand the structure of the atom and the phenomena related to it, quantum mechanics is
essential, and the Schrödinger equation for calculating the wave function is now widely used.
In the next chapter, we will explore the structure of the atom based on the ideas of quantum
mechanics.
(a)
(b) After 100 electrons
Double slit
Moving electrons
(c) After 3000 electrons
(d) After 70 000 electrons
FIGURE 29.13 In this electron version of Young’s double-slit experiment, the characteristic fringe pattern becomes recognizable only after a suffi cient number of electrons have struck the screen.
C o u rt
es y A
k ir
a to
n o m
u ra
, J.
E n d o , T
. M
at su
d a
an d T
. K
aw as
ak i, A
m . J.
P h y s.
5 7 (
2 ):
1 1 7 ,
F eb
ru ar
y 1
9 8 9 .
29.6 The Heisenberg Uncertainty Principle 845
Check Your Understanding
(The answers are given at the end of the book.) 11. A stone is dropped from the top of a building. As the stone falls, does its de Broglie wavelength increase,
decrease, or remain the same?
12. An electron and a neutron have diff erent masses. Is it possible, according to Equation 29.8, that they can have the same de Broglie wavelength? (a) Yes, provided the magnitudes of their momenta are dif- ferent. (b) Yes, provided their speeds are diff erent. (c) No; two particles with diff erent masses always have diff erent de Broglie wavelengths.
13. In Interactive Figure 29.1b, replace the electrons with protons that have the same speed. With the aid of Equation 27.1 for the bright fringes in Young’s double-slit experiment and Equation 29.8, decide
whether the angular separation between the fringes would increase, decrease, or remain the same,
relative to the angular separation produced by the electrons.
14. A beam of electrons passes through a single slit, and a beam of protons passes through a second, but identical, slit. The electrons and the protons have the same speed. Which one of the following correctly
describes the beam that experiences the greatest amount of diff raction? (a) The electrons, because they have the smaller momentum and, hence, the smaller de Broglie wavelength (b) The electrons, because they have the smaller momentum and, hence, the larger de Broglie wavelength (c) The protons, because they have the smaller momentum and, hence, the smaller de Broglie wavelength (d) The protons, because they have the larger momentum and, hence, the smaller de Broglie wavelength (e) Both beams experience the same amount of diff raction, because the electrons and protons have the same de Broglie wavelength.
29.6 The Heisenberg Uncertainty Principle As the previous section discusses, the bright fringes in Figure 29.13 indicate the places where there is a high probability of an electron striking the screen. Since there are a number of bright
fringes, there is more than one place where each electron has some probability of hitting. As a
result, it is not possible to specify in advance exactly where on the screen an individual electron
will hit. All we can do is speak of the probability that the electron may end up in a number of
diff erent places. No longer is it possible to say, as Newton’s laws would suggest, that a single
electron, fi red through the double slit, will travel directly forward in a straight line and strike
the screen. This simple model just does not apply when a particle as small as an electron passes
through a pair of closely spaced narrow slits. Because the wave nature of particles is important
in such circumstances, we lose the ability to predict with 100% certainty the path that a single
particle will follow. Instead, only the average behavior of large numbers of particles is predict-
able, and the behavior of any individual particle is uncertain.
To see more clearly into the nature of the uncertainty, consider electrons passing through a
single slit, as in Figure 29.14. After a suffi cient number of electrons strike the screen, a diff raction pattern emerges. The electron diff raction pattern consists of alternating bright and dark fringes
and is analogous to the pattern for light waves shown in Figure 27.22. Figure 29.14 shows the
px
px
Δpy
θ θ
θ WMoving
electron
Single slit
Screen First dark fringe
First dark fringe
Midpoint of central
bright fringe
FIGURE 29.14 When a suffi cient number of electrons pass through a single slit and strike
the screen, a diff raction pattern of bright and
dark fringes emerges. (Only the central bright
fringe is shown.) This pattern is due to the
wave nature of the electrons and is analogous
to that produced by light waves.
846 CHAPTER 29 Particles and Waves
slit and locates the fi rst dark fringe on either side of the central bright fringe. The central fringe
is bright because electrons strike the screen over the entire region between the dark fringes. If the
electrons striking the screen outside the central bright fringe are neglected, the extent to which
the electrons are diff racted is given by the angle 𝜃 in the drawing. To reach locations within the central bright fringe, some electrons must have acquired momentum in the y direction, despite the fact that they enter the slit traveling along the x direction and have no momentum in the y direc- tion to start with. The fi gure illustrates that the y component of the momentum may be as large as Δpy. The notation Δpy indicates the diff erence between the maximum value of the y component of the momentum after the electron passes through the slit and its value of zero before the electron
passes through the slit. Δpy represents the uncertainty in the y component of the momentum, in the sense that the y component may have any value from zero to Δpy.
It is possible to relate Δpy to the width W of the slit. To do this, we assume that Equation 27.4, which applies to light waves, also applies to particle waves whose de Broglie wavelength is
𝜆. This equation, sin 𝜃 = 𝜆/W, specifi es the angle 𝜃 that locates the fi rst dark fringe. If 𝜃 is small, then sin 𝜃 ≈ tan 𝜃. Moreover, Figure 29.14 indicates that tan 𝜃 = Δpy /px, where px is the x com- ponent of the momentum of the electron. Therefore, Δpy /px < 𝜆/W. However, px = h/𝜆 according to de Broglie’s equation, so that
∆py px
= ∆py h/λ
≈ λ W
As a result,
∆ py ≈ h W
(29.9)
which indicates that a smaller slit width leads to a larger uncertainty in the y component of the electron’s momentum.
It was Heisenberg who fi rst suggested that the uncertainty Δpy in the y component of the momentum is related to the uncertainty in the y position of the electron as the electron passes through the slit. To get a feel for this relationship, let’s assume that the center of the
slit is at y = 0 m. Because the width of the slit is W, the electron is somewhere within ±12W
Math Skills To see why sin θ ≈ tan θ when 𝜃 is small, refer to Figure 29.15a and recall that the sine and tangent functions are defi ned as follows in Section 1.4:
sin θ = ho h (1.1) and tan θ =
ho h a
(1.3)
where ho is the length of the side of a right triangle opposite the angle 𝜃, ha is the length of the side adjacent to the angle 𝜃, and h is the hypotenuse. When 𝜃 is small, h and ha become approximately equal, or h ≈ ha, and the right-hand sides of Equations 1.1 and 1.3 become approximately the same.
To see why tan 𝜃 = Δpy /px, refer to Figure 29.15b, which shows in enlarged form the por- tion of Figure 29.14 that establishes the angle 𝜃. A comparison of the shaded right triangle in Figure 29.15b with the shaded right triangle in Figure 29.15a reveals that ho = Δpy and ha = px. Substituting these values into Equation 1.3, we fi nd that
tan θ = ho ha
= ∆py px
θ
Δpy
ha
ho h
θ
px
(b)(a)
90°
FIGURE 29.15 Math Skills drawing.
29.6 The Heisenberg Uncertainty Principle 847
from the center of the slit. Thus, we take the uncertainty in the y position of the electron to be ∆y = 12W, so that W = 2 ∆y. Substituting this relation into Equation 29.9 shows that ∆py ≈ h / (2 ∆y) or (∆py)(∆y) ≈
1
2 h. The result of Heisenberg’s more complete analysis is given below in Equation 29.10 and is known as the Heisenberg uncertainty principle. Note that the Heisenberg principle is a general principle with wide applicability. It does
not just apply to the case of single-slit diff raction, which we have used here for the sake of
convenience.
THE HEISENBERG UNCERTAINTY PRINCIPLE Momentum and position
(∆py) (∆y) ≥ h
4π (29.10)
Δy = uncertainty in a particle’s position along the y direction Δpy = uncertainty in the y component of the linear momentum of the particle
Energy and time
(∆E ) (∆t) ≥ h
4π (29.11)
ΔE = uncertainty in the energy of a particle when the particle is in a certain state Δt = time interval during which the particle is in the state
The Heisenberg uncertainty principle places limits on the accuracy with which the mo-
mentum and position of a particle can be specifi ed simultaneously. These limits are not just limits
due to faulty measuring techniques. They are fundamental limits imposed by nature, and there
is no way to circumvent them. Equation 29.10 indicates that Δpy and Δy cannot both be arbit- rarily small at the same time. If one is small, then the other must be large, so that their product
equals or exceeds (≥) Planck’s constant divided by 4𝜋. For example, if the position of a particle is known exactly, so that Δy is zero, then Δpy is an infi nitely large number, and the momentum of the particle is completely uncertain. Conversely, if we assume that Δpy is zero, then Δy is an infi nitely large number, and the position of the particle is completely uncertain. In other words,
the Heisenberg uncertainty principle states that it is impossible to specify precisely both the mo-
mentum and position of a particle at the same time.
There is also an uncertainty principle that deals with energy and time, as expressed by Equa-
tion 29.11. The product of the uncertainty ΔE in the energy of a particle and the time interval Δt during which the particle remains in a given energy state is greater than or equal to Planck’s constant divided by 4𝜋. Therefore, the shorter the lifetime of a particle in a given state, the greater is the uncertainty in the energy of that state.
Example 6 shows that the uncertainty principle has signifi cant consequences for the motion
of tiny particles such as electrons but has little eff ect on the motion of macroscopic objects, even
those with as little mass as a Ping-Pong ball.
EXAMPLE 6 The Heisenberg Uncertainty Principle
Assume that the position of an object is known so precisely that the
uncertainty in the position is only Δy = 1.5 × 10−11 m. (a) Determine the minimum uncertainty in the momentum of the object. Find the corres-
ponding minimum uncertainty in the speed of the object in the case when
the object is (b) an electron (mass = 9.1 × 10−31 kg) and (c) a Ping-Pong ball (mass = 2.2 × 10−3 kg).
Reasoning The minimum uncertainty Δpy in the y component of the momentum is given by the Heisenberg uncertainty principle as Δpy = h/ (4𝜋 Δy), where Δy is the uncertainty in the position of the object along the y direction. Both the electron and the Ping-Pong ball have the same uncer- tainty in their momenta because they have the same uncertainty in their po-
sitions. However, these objects have very diff erent masses. As a result, we
will fi nd that the uncertainty in the speeds of these objects is very diff erent.
Problem-Solving Insight The Heisenberg uncertainty principle states that the product of Δpy and Δy is greater than or equal to h/4𝞹. For a given value of Δpy or Δy, the minimum uncertainty in the other term occurs when the product is equal to h/4𝞹.
Solution (a) The minimum uncertainty in the y component of the momentum is
∆py = h
4π ∆y =
6.63 × 10−34 J · s 4π(1.5 × 10−11 m)
= 3.5 × 10−24 kg · m/s (29.10)
(b) The magnitude py of the momentum is py = mυy (Equation 7.2), where m is the mass of the object and 𝜐y is its speed. Therefore, the uncertainty
848 CHAPTER 29 Particles and Waves
Example 6 emphasizes how the uncertainty principle imposes diff erent uncertainties on the
speeds of an electron (small mass) and a Ping-Pong ball (large mass). For objects like the ball,
which have relatively large masses, the uncertainties in position and speed are so small that
they have no eff ect on our ability to determine simultaneously where such objects are and how
fast they are moving. The uncertainties calculated in Example 6 depend on more than just the
mass, however. They also depend on Planck’s constant, which is a very small number. It is in-
teresting to speculate about what life would be like if Planck’s constant were much larger than
6.63 × 10−34 J · s. Conceptual Example 7 deals with just such speculation.
Δpy is Δpy = m Δ𝜐y, and the minimum uncertainty in the speed of the electron is
∆υy = ∆py m
= 3.5 × 10−24 kg · m/s
9.1 × 10−31 kg = 3.8 × 10 6 m /s
Thus, the small uncertainty in the y position of the electron gives rise to a large uncertainty in the speed of the electron.
(c) The minimum uncertainty in the speed of the Ping-Pong ball is
∆υy = ∆py m
= 3.5 × 10−24 kg · m/s
2.2 × 10−3 kg = 1.6 × 10−21 m /s
Because the mass of the Ping-Pong ball is relatively large, the small un-
certainty in its y position gives rise to an uncertainty in its speed that is much smaller than that for the electron. Thus, in contrast to the case for
the electron, we can know simultaneously where the ball is and how fast
it is moving, to a very high degree of certainty.
CONCEPTUAL EXAMPLE 7 What If Planck’s Constant Were Large?
Suppose that you are target shooting at a stationary target. A bullet leaving
the barrel of a gun is analogous to an electron passing through the single
slit in Figure 29.14. With this analogy in mind and assuming that the mag- nitude of the bullet’s momentum is not abnormally large, what would target
shooting be like if Planck’s constant had a relatively large value instead of
its extremely small value of 6.63 × 10−34 J · s? (a) It would be more accur- ate because there would be less uncertainty in where the bullet hits the tar-
get. (b) It would be less accurate because there would be greater uncertainty in where the bullet hits the target. (c) There would be no diff erence.
Reasoning Let’s assume that the bullet is moving down the barrel of the gun in the +x direction and that the target lies on the x axis. When it exits the barrel, the bullet—like the electron passing through a single
slit—acquires a momentum component that is perpendicular (in the y dir- ection) to the barrel. This happens even though inside the barrel the bullet
travels only along the x direction and has no momentum component in the y direction. Analogous to the discussion relating to Figure 29.14, the y component of the momentum may be as large as Δpy, where Δpy indicates the diff erence between the maximum value of the y component of the mo- mentum after the bullet leaves the barrel and its value of zero while the
bullet is in the barrel. Δpy is related to Planck’s constant h and the diameter
W of the barrel opening via the relation Δpy ≈ h/W (Equation 29.9). Since we are now postulating that Planck’s constant is large, Δpy is also large.
Answers (a) and (c) are incorrect. Target shooting becomes more ac- curate if Planck’s constant becomes smaller, not larger. Here’s the reason:
Inside the barrel the bullet is moving in the +x direction. However, upon exiting the barrel, the bullet acquires a momentum component Δpy in the y direction and begins to deviate from its original path by moving in the y direction. According to Δpy ≈ h/W (Equation 29.9), the smaller the value of h, the smaller is Δpy. If, in the extreme limit, Planck’s constant were zero, Δpy would also be zero, and the bullet would move only in the +x direction and, thus, would hit the target.
Answer (b) is correct. If the bullet, after leaving the barrel, had only a momentum component that was parallel to the barrel, the bullet would
strike the target. However, upon leaving the barrel, the bullet also ac-
quires a momentum component Δpy that is perpendicular to the barrel. The relation Δpy ≈ h/W (Equation 29.9) shows that the larger the value of Planck’s constant h, the larger is the value of Δpy. Since this momentum component is perpendicular to the barrel itself, the bullet can strike at loc-
ations other than the target. Thus, target shooting would be less accurate if
Planck’s constant had a relatively large value.
EXAMPLE 8 BIO Breathing in Electrons
Our lungs contain approximately 500 million alveoli, which are the small,
hollow chambers lined with a membrane that allows the exchange of
oxygen and carbon dioxide in our blood. Consider the situation of an elec-
tron located in one of these sacks and (a) calculate the uncertainty in its momentum using the Heisenberg uncertainty principle. For the uncer-
tainty in the electron’s position, use the diameter of the alveoli, which is
approximately 0.05 mm. Next, assume that at some instant in time, the
momentum of the electron is equal to the uncertainty in its momentum
and (b) calculate the kinetic energy of the electron.
Reasoning We simply apply the Heisenberg uncertainty principle for position and momentum (Equation 29.10) to calculate the uncer-
tainty in the electron’s momentum. We then assume this value to be
equal to the electron’s momentum and calculate its kinetic energy
using Equation 6.2.
Solution (a) From Equation 29.10, we have:
∆py = h
(4π) (∆y) =
6.63 × 10−34 J · s 4π(0.05 × 10−3 m)
= 1.1 × 10−30 kg · m/s
(b) Now assume that p = Δpy = 1.1 × 10−30 kg · m/s and calculate the electron’s kinetic energy:
KE = 1
2 mυ2 =
p2
2m =
(1.1 × 10−30 kg · m/s)2
2(9.11 × 10−31 kg) = 6.1 × 10−31 J
While this is an incredibly small kinetic energy, the speed of the electron
is still ≈ 1 m/s.
Focus on Concepts 849
Concept Summary 29.1 The Wave–Particle Duality, 29.2 Blackbody Radiation and Planck’s Constant The wave–particle duality refers to the fact that a wave can exhibit particle-like characteristics and a particle can exhibit wave-like
characteristics.
At a constant temperature, a perfect blackbody absorbs and reemits all the
electromagnetic radiation that falls on it. Max Planck calculated the emitted
radiation intensity per unit wavelength as a function of wavelength. In his
theory, Planck assumed that a blackbody consists of atomic oscillators that
can have only discrete, or quantized, energies. Planck’s quantized energies
are given by Equation 29.1, where h is Planck’s constant (6.63 × 10−34 J · s) and f is the vibration frequency of an oscillator.
E = nhf n = 0, 1, 2, 3, . . . (29.1)
29.3 Photons and the Photoelectric Eff ect All electromagnetic radiation consists of photons, which are packets of energy. The energy of a photon is
given by Equation 29.2, where h is Planck’s constant and f is the frequency of the photon. A photon has no mass and always travels at the speed of light
c in a vacuum.
E = hf (29.2)
The photoelectric eff ect is the phenomenon in which light shining on a metal
surface causes electrons to be ejected from the surface. The work function W0 of a metal is the minimum work that must be done to eject an electron from the
metal. In accordance with the conservation of energy, the electrons ejected from
a metal have a maximum kinetic energy KEmax that is related to the energy hf of the incident photon and the work function of the metal by Equation 29.3.
hf = KEmax + W0 (29.3)
29.4 The Momentum of a Photon and the Compton Eff ect The mag- nitude p of a photon’s momentum is given by Equation 29.6, where h is Planck’s constant and 𝜆 is the wavelength of the photon.
p = h λ
(29.6)
The Compton eff ect is the scattering of a photon by an electron in a ma-
terial, the scattered photon having a smaller frequency and, hence, a smaller
energy than the incident photon. Part of the photon’s energy and momentum
are transferred to the recoiling electron. The diff erence between the wave-
length 𝜆ʹ of the scattered photon and the wavelength 𝜆 of the incident photon is related by Equation 29.7 to the scattering angle 𝜃 (see Animated Figure 29.10), where m is the mass of the electron. The quantity h/(mc) is known as the Compton wavelength of the electron.
λ′ − λ = h
mc (1 − cos θ ) (29.7)
29.5 The De Broglie Wavelength and the Wave Nature of Matter The de Broglie wavelength 𝜆 of a particle is given by Equation 29.8, where h is Planck’s constant and p is the magnitude of the relativistic momentum of the particle. Because of its wavelength, a particle can exhibit wave-like charac-
teristics. The wave associated with a particle is a wave of probability.
λ = h p
(29.8)
29.6 The Heisenberg Uncertainty Principle The Heisenberg uncer- tainty principle places limits on our knowledge about the behavior of a
particle. The uncertainty principle is stated according to Equation 29.10,
where Δy is the uncertainty in the particle’s position along the y direction, and Δpy is the uncertainty in the y component of the linear momentum of the particle.
(∆py) (∆y) ≥ h
4π (29.10)
The uncertainty principle can also be stated according to Equation 29.11,
where ΔE is the uncertainty in the energy of a particle when it is in a certain state, and Δt is the time interval during which the particle is in the state.
(∆E ) (∆t) ≥ h
4π (29.11)
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 29.2 Blackbody Radiation and Planck’s Constant 1. An astronomer is measuring the electromagnetic radiation emitted by two stars, which are both assumed to be perfect blackbody emitters. For each star
she makes a plot of the radiation intensity per unit wavelength as a function
of wavelength. She notices that the curve for star A has a maximum that
occurs at a shorter wavelength than does the curve for star B. What can she
conclude about the surface temperatures of the two stars? (a) Star A has the greater surface temperature. (b) Star B has the greater surface temperature. (c) Both stars, being perfect blackbody emitters, have the same surface tem- perature. (d) There is not enough information to draw a conclusion about the temperatures.
Section 29.3 Photons and the Photoelectric Eff ect 2. Photons are generated by a microwave oven in a kitchen and by an X-ray machine at a dentist’s offi ce. Which type of photon has the greater frequency,
the greater energy, and the greater wavelength?
Greater Frequency
Greater Energy
Greater Wavelength
(a) X-ray X-ray X-ray
(b) X-ray X-ray Microwave
(c) Microwave X-ray Microwave
(d) Microwave Microwave X-ray
(e) X-ray Microwave Microwave
Focus on Concepts
850 CHAPTER 29 Particles and Waves
5. A laser emits a beam of light whose photons all have the same fre- quency. When the beam strikes the surface of a metal, photoelectrons are
ejected from the surface. What happens if the laser emits twice the num-
ber of photons per second? (a) The photoelectrons are ejected from the surface with twice the maximum kinetic energy. (b) The photoelectrons are ejected from the surface with the same maximum kinetic energy.
(c) The number of photoelectrons ejected per second from the surface doubles. (d) Both b and c happen. (e) Both a and c happen. 6. The surface of a metal plate is illuminated with light of a certain fre- quency. Which of the following conditions determine whether or not photo-
electrons are ejected from the metal?
1. The number of photons per second emitted by the light source 2. The length of time that the light is turned on 3. The thermal conductivity of the metal 4. The surface area of the metal illuminated by the light 5. The type of metal from which the plate is made
(a) 1 and 2 (b) 5 (c) 3 and 5 (d) 4 (e) 2 and 3
Section 29.4 The Momentum of a Photon and the Compton Eff ect 9. Does a photon, like a moving particle such as an electron, have a mo- mentum? (a) No, because a photon is a wave, and a wave does not have a mo- mentum. (b) No, because a photon has no mass, and mass is necessary in order to have a momentum. (c) No, because a photon, always traveling at the speed
of light in a vacuum, would have an infi nite momentum. (d) Yes, and the mag- nitude p of the photon’s momentum is related to its wavelength 𝜆 by p = h/𝜆, where h is Planck’s constant. (e) Yes, and the magnitude p of the photon’s mo- mentum is related to its wavelength 𝜆 by p = h𝜆, where h is Planck’s constant.
Section 29.5 The De Broglie Wavelength and the Wave Nature of Matter 13. Two particles, A and B, have the same mass, but particle A has a charge of +q and B has a charge of +2q. The particles are accelerated from rest through the same potential diff erence. Which one has the longer de Broglie
wavelength at the end of the acceleration? (a) Particle A, because it has the greater momentum, and, hence, the longer de Broglie wavelength (b) Particle B, because it has the greater momentum, and, hence, the longer de Broglie
wavelength (c) Particle A, because it has the smaller momentum, and, hence, the longer de Broglie wavelength (d) Particle B, because it has the smaller momentum, and, hence, the longer de Broglie wavelength (e) Both particles have the same de Broglie wavelength.
Section 29.6 The Heisenberg Uncertainty Principle 16. Suppose that the momentum of an electron is measured with complete accuracy (i.e., the uncertainty in its momentum is zero). The uncertainty in a
simultaneous measurement of the electron’s position __________. (a) is also zero (b) is infi nitely large (c) is some fi nite value between zero and infi nity (d) cannot be measured, because one cannot measure the position and mo- mentum of a particle, such as an electron, simultaneously
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
Note: In these problems, ignore relativistic eff ects unless instructed otherwise, and assume that wavelengths are in a vacuum unless otherwise specifi ed.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 29.3 Photons and the Photoelectric Eff ect 1. E The dissociation energy of a molecule is the energy required to break the molecule apart into its separate atoms. The dissociation energy for the
cyanogen molecule is 1.22 × 10−18 J. Suppose that this energy is provided
by a single photon. Determine the (a) wavelength and (b) frequency of the photon. (c) In what region of the electromagnetic spectrum (see Figure 24.9) does this photon lie?
2. E An AM radio station broadcasts an electromagnetic wave with a fre- quency of 665 kHz, whereas an FM station broadcasts an electromagnetic
wave with a frequency of 91.9 MHz. How many AM photons are needed to
have a total energy equal to that of one FM photon?
3. E GO SSM Ultraviolet light with a frequency of 3.00 × 1015 Hz strikes a metal surface and ejects electrons that have a maximum kinetic energy of
6.1 eV. What is the work function (in eV) of the metal?
4. E GO Light is shining perpendicularly on the surface of the earth with an intensity of 680 W/m2. Assuming that all the photons in the light have the
same wavelength (in vacuum) of 730 nm, determine the number of photons
per second per square meter that reach the earth.
5. E SSM Ultraviolet light is responsible for sun tanning. Find the wavelength (in nm) of an ultraviolet photon whose energy is 6.4 × 10−19 J.
6. E The maximum wavelength that an electromagnetic wave can have and still eject electrons from a metal surface is 485 nm. What is the work function
W0 of this metal? Express your answer in electron volts. 7. E Radiation of a certain wavelength causes electrons with a maximum kinetic energy of 0.68 eV to be ejected from a metal whose work function is
2.75 eV. What will be the maximum kinetic energy (in eV) with which this
same radiation ejects electrons from another metal whose work function is
2.17 eV?
8. E GO Multiple-Concept Example 3 reviews the concepts necessary to solve this problem. Radiation with a wavelength of 238 nm shines on a metal
surface and ejects electrons that have a maximum speed of 3.75 × 105 m/s.
Which one of the following metals is it, the values in parentheses being the
work functions: potassium (2.24 eV), calcium (2.71 eV), uranium (3.63 eV),
aluminum (4.08 eV), or gold (4.82 eV)?
9. M SSM MMH An owl has good night vision because its eyes can detect a light intensity as small as 5.0 × 10−13 W/m2. What is the minimum number
of photons per second that an owl eye can detect if its pupil has a diameter of
8.5 mm and the light has a wavelength of 510 nm?
10. M V-HINT A proton is located at a distance of 0.420 m from a point charge of +8.30 𝜇C. The repulsive electric force moves the proton until it is at a distance of 1.58 m from the charge. Suppose that the electric potential
Problems
Problems 851
energy lost by the system were carried off by a photon. What would be its
wavelength?
11. M CHALK When light with a wavelength of 221 nm is incident on a cer- tain metal surface, electrons are ejected with a maximum kinetic energy of
3.28 × 10−19 J. Determine the wavelength (in nm) of light that should be
used to double the maximum kinetic energy of the electrons ejected from
this surface.
12. M GO A glass plate has a mass of 0.50 kg and a specifi c heat capacity of 840 J/ (kg · C°). The wavelength of infrared light is 6.0 × 10−5 m, while the wavelength of blue light is 4.7 × 10−7 m. Find the number of infrared
photons and the number of blue photons needed to raise the temperature of
the glass plate by 2.0 C°, assuming that all the photons are absorbed by the
glass.
13. H SSM A laser emits 1.30 × 1018 photons per second in a beam of light that has a diameter of 2.00 mm and a wavelength of 514.5 nm. Determine
(a) the average electric fi eld strength and (b) the average magnetic fi eld strength for the electromagnetic wave that constitutes the beam.
14. H Available in WileyPLUS.
Section 29.4 The Momentum of a Photon and the Compton Eff ect 15. E A light source emits a beam of photons, each of which has a mo- mentum of 2.3 × 10−29 kg · m/s. (a) What is the frequency of the photons? (b) To what region of the electromagnetic spectrum do the photons belong? Consult Figure 24.9 if necessary.
16. E A photon of red light (wavelength = 720 nm) and a Ping-Pong ball (mass = 2.2 × 10−3 kg) have the same momentum. At what speed is the ball
moving?
17. E CHALK SSM In a Compton scattering experiment, the incident X-rays have a wavelength of 0.2685 nm, and the scattered X-rays have a wavelength
of 0.2703 nm. Through what angle 𝜃 in Animated Figure 29.10 are the X-rays scattered?
18. E V-HINT A sample is bombarded by incident X-rays, and free electrons in the sample scatter some of the X-rays at an angle of 𝜃 = 122.0° with respect to the incident X-rays (see Animated Figure 29.10). The scattered X-rays have a momentum whose magnitude is 1.856 × 10−24 kg · m/s. Determine the wavelength (in nm) of the incident X-rays. (For accuracy, use
h = 6.626 × 10−34 J · s, c = 2.998 × 108 m/s, and m = 9.109 × 10−31 kg for the mass of an electron.)
19. E MMH An incident X-ray photon of wavelength 0.2750 nm is scattered from an electron that is initially at rest. The photon is scattered at an angle of
𝜃 = 180.0° in Animated Figure 29.10 and has a wavelength of 0.2825 nm. Use the conservation of linear momentum to fi nd the momentum gained by
the electron.
20. E GO In the Compton eff ect, momentum conservation applies, so the total momentum of the photon and the electron is the same before and after
the scattering occurs. Suppose that in Animated Figure 29.10 the incident photon moves in the +x direction and the scattered photon emerges at an angle of 𝜃 = 90.0°, which is in the −y direction. The incident photon has a wavelength of 9.00 × 10−12 m. Find the x and y components of the momentum of the scattered electron.
21. M SSM What is the maximum amount by which the wavelength of an incident photon could change when it undergoes Compton scattering from a
nitrogen molecule (N2)?
22. M GO Animated Figure 29.10 shows the setup for measuring the Compton eff ect. With a fi xed incident wavelength, a wavelength of 𝜆ʹ1 is measured for a scattering angle of 𝜃1 = 30.0°, whereas a wavelength of 𝜆ʹ2 is measured for a scattering angle of 𝜃2 = 70.0°. Find the diff erence in wavelengths, 𝜆ʹ2 − 𝜆ʹ1.
23. M GO A photon of wavelength 0.45000 nm strikes a free electron that is initially at rest. The photon is scattered straight backward. What is the speed
of the recoil electron after the collision?
24. H Available in WileyPLUS.
Section 29.5 The De Broglie Wavelength and the Wave Nature of Matter 25. E A bacterium (mass = 2 × 10−15 kg) in the blood is moving at 0.33 m/s. What is the de Broglie wavelength of this bacterium?
26. E What are (a) the wavelength of a 5.0-eV photon and (b) the de Broglie wavelength of a 5.0-eV electron?
27. E SSM Available in WileyPLUS. 28. E An electron and a proton have the same speed. Ignore relativistic eff ects and determine the ratio 𝜆electron/𝜆proton of their de Broglie wavelengths. 29. E Recall from Section 14.3 that the average kinetic energy of an atom in a monatomic ideal gas is given by KE =
3
2 kT, where k = 1.38 × 10−23 J/K and T is the Kelvin temperature of the gas. Determine the de Broglie wavelength of a helium atom (mass = 6.65 × 10−27 kg) that has the average kinetic energy
at room temperature (293 K).
30. E GO In a Young’s double-slit experiment that uses electrons, the angle that locates the fi rst-order bright fringes is 𝜃A = 1.6 × 10−4 degrees when the magnitude of the electron momentum is pA = 1.2 × 10−22 kg · m/s. With the same double slit, what momentum magnitude pB is necessary so that an angle of 𝜃B = 4.0 × 10−4 degrees locates the fi rst-order bright fringes? 31. M SSM A particle has a de Broglie wavelength of 2.7 × 10−10 m. Then its kinetic energy doubles. What is the particle’s new de Broglie wavelength,
assuming that relativistic eff ects can be ignored?
32. M GO From a cliff that is 9.5 m above a lake, a young woman (mass = 41 kg) jumps from rest, straight down into the water. At the instant she strikes
the water, what is her de Broglie wavelength?
33. M V-HINT The width of the central bright fringe in a diff raction pattern on a screen is identical when either electrons or red light (vacuum wavelength =
661 nm) pass through a single slit. The distance between the screen and the
slit is the same in each case and is large compared to the slit width. How fast
are the electrons moving?
34. M GO Particle A is at rest, and particle B collides head-on with it. The collision is completely inelastic, so the two particles stick together after the
collision and move off with a common velocity. The masses of the particles
are diff erent, and no external forces act on them. The de Broglie wavelength
of particle B before the collision is 2.0 × 10−34 m. What is the de Broglie
wavelength of the object that moves off after the collision?
35. M SSM An electron, starting from rest, accelerates through a potential diff erence of 418 V. What is the fi nal de Broglie wavelength of the electron,
assuming that its fi nal speed is much less than the speed of light?
36. H The kinetic energy of a particle is equal to the energy of a photon. The particle moves at 5.0% of the speed of light. Find the ratio of the photon
wavelength to the de Broglie wavelength of the particle.
Section 29.6 The Heisenberg Uncertainty Principle 37. E SSM An object is moving along a straight line, and the uncertainty in its position is 2.5 m. (a) Find the minimum uncertainty in the momentum of the object. Find the minimum uncertainty in the object’s velocity, assuming
that the object is (b) a golf ball (mass = 0.045 kg) and (c) an electron. 38. E CHALK A proton is confi ned to a nucleus that has a diameter of 5.5 × 10−15 m. If this distance is considered to be the uncertainty in the posi-
tion of the proton, what is the minimum uncertainty in its momentum?
39. E SSM In the lungs there are tiny sacs of air, which are called alveoli. An oxygen molecule (mass = 5.3 × 10−26 kg) is trapped within a sac, and the
852 CHAPTER 29 Particles and Waves
uncertainty in its position is 0.12 mm. What is the minimum uncertainty in
the speed of this oxygen molecule?
40. E GO Particles pass through a single slit of width 0.200 mm (see Figure 29.14). The de Broglie wavelength of each particle is 633 nm. After the particles pass through the slit, they spread out over a range of angles. Assume that the un-
certainty in the position of the particles is one-half the width of the slit, and use
the Heisenberg uncertainty principle to determine the minimum range of angles.
41. M GO The minimum uncertainty Δy in the position y of a particle is equal to its de Broglie wavelength. Determine the minimum uncertainty in
the speed of the particle, where this minimum uncertainty Δ𝜐y is expressed
as a percentage of the particle’s speed υy (Percentage = ∆υy υy
× 100%). Assume that relativistic eff ects can be ignored.
42. M V-HINT A subatomic particle created in an experiment exists in a cer- tain state for a time of Δt = 7.4 × 10−20 s before decaying into other particles. Apply both the Heisenberg uncertainty principle and the equivalence of
energy and mass (see Section 28.6) to determine the minimum uncertainty
involved in measuring the mass of this short-lived particle.
43. E The interatomic spacing in a crystal of table salt is 0.282 nm. This crystal is being studied in a neutron diff raction experiment, similar to the one that
produced the photograph in Figure 29.12a. How fast must a neutron (mass = 1.67 × 10−27 kg) be moving to have a de Broglie wavelength of 0.282 nm?
44. E Available in WileyPLUS. 45. E SSM The de Broglie wavelength of a proton in a particle accelerator is 1.30 × 10−14 m. Determine the kinetic energy (in joules) of the proton.
46. E V-HINT Find the de Broglie wavelength of an electron with a speed of 0.88c. Take relativistic eff ects into account. 47. E GO The work function of a metal surface is 4.80 × 10−19 J. The max- imum speed of the electrons emitted from the surface is 𝜐A = 7.30 × 105 m/s
when the wavelength of the light is 𝜆A. However, a maximum speed of 𝜐B = 5.00 × 105 m/s is observed when the wavelength is 𝜆B. Find the wavelengths 𝜆A and 𝜆B. 48. E GO How fast does a proton have to be moving in order to have the same de Broglie wavelength as an electron that is moving with a speed of
4.50 × 106 m/s?
49. M MMH Available in WileyPLUS. 50. M V-HINT Available in WileyPLUS. 51. H Available in WileyPLUS.
Additional Problems
In the photoelectric eff ect, electrons can be emitted from a metal surface when
light shines on it. Einstein explained this phenomenon in terms of photons
and the conservation of energy. Our discussion of this topic in Section 29.3
deals with a single wavelength. Problem 52, in contrast, considers a mixture
of wavelengths and reviews the basic concepts that come into play in this
important phenomenon. In this chapter we have seen that moving particles of
matter not only possess kinetic energy and momentum but also are character-
ized by a wavelength that is known as the de Broglie wavelength. Problem 53
reviews kinetic energy and momentum, and focuses on the relation between
these fundamental quantities and the de Broglie wavelength.
52. M CHALK Sunlight, whose visible wavelengths range from 380 to 750 nm, is incident on a sodium surface. The work function for sodium is W0 = 2.28 eV. Concepts: (i) Will electrons with a greater value of KEmax be emitted when the incident photons have a relatively greater or relatively smaller amount
of energy? (ii) In the range of visible wavelengths, which wavelength cor-
responds to incident photons that carry the greatest energy? (iii) What is
the smallest value of KEmax with which an electron can be ejected from the
sodium? Calculations: Find the maximum kinetic energy KEmax (in joules) of the photoelectrons emitted from the surface and the range of wavelengths
that will cause photoelectrons to be emitted.
53. M CHALK SSM An electron and a proton have the same kinetic energy and are moving at speeds much less than the speed of light. Concepts: (i) How is the de Broglie wavelength 𝜆 related to the magnitude p of the mo- mentum? (ii) How is the magnitude of the momentum related to the kinetic
energy of a particle of mass m that is moving at a speed that is much less than the speed of light? (iii) Which has the greater de Broglie wavelength, the
electron or the proton? Calculations: Determine the ratio of the de Broglie wavelength of the electron to that of the proton.
Concepts and Calculations Problems
54. M Identifying Unknown Metals. You and your team are tasked with sorting a hundred metallic samples composed of pure silver (Ag), nickel
(Ni), indium (In), or cobalt (Co). The problem is that they all look the same
(metallic) and are not labeled. The work functions (W0) of the materials are: Ag (4.50 eV), Ni (5.20 eV), In (4.10 eV), and Co (4.90 eV). You have a mono-
chromatic light source that can be tuned to output wavelengths from 250 nm
to 400 nm. You get the idea to use it to measure the threshold frequencies of
the samples and, therefore, to identify the metals. (a) Calculate the threshold frequencies and wavelengths of all of the metals. (b) Can the light source
reach the threshold frequencies of all of the metals? If not, can it still be used
to sort the samples?
55. M Electron Diff raction. You and your team have set up an experiment where a beam of electrons is accelerated from rest through a potential dif-
ference (V), and then passes through a crystalline material that eff ectively acts as a set of slits separated by 9.62 × 10−11 m. (a) If the fi rst order (m = 1) bright fringe is located at 𝜃 = 12.0° relative to the initial direction of the electron beam, what is the de Broglie wavelength of the electrons? (b) What is the potential diff erence through which the electrons are accelerated?
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
30.1 Describe the nuclear atom.
30.2 Calculate the wavelengths of hydrogen line spectra.
30.3 Use the Bohr model to predict the energy levels in hydrogen.
30.4 Explain Bohr’s assumption regarding angular momentum.
30.5 Apply quantum mechanics to electron energy levels in hydrogen.
30.6 Use the Pauli exclusion principle to explain the periodic table.
30.7 Apply the Bohr model to X-ray production in atoms.
30.8 Explain how a laser operates.
30.9 Describe laser applications in medicine.
30.10 Explain how holographic images are made and viewed.
A n to
in e
R o ss
et /S
ci en
ce S
o u rc
e
CHAPTER 30
The Nature of the Atom
CAT scanning is an important noninvasive technique that utilizes X-rays to provide image “slices” of the
interior of the human body. This colored 3D CAT scan of an adult jaw and part of the skull illustrates the
level of detail achievable today. A computer with suitable imaging software assembles the slices into such 3D
images. Surgeons can even navigate around the body using rapid animations of CAT data. The production of
X-rays is related to the structure of the atom, and that structure is the main topic of this chapter.
30.1 Rutherford Scattering and the Nuclear Atom An atom contains a small, positively charged nucleus (radius ≈ 10−15 m), which is
surrounded at relatively large distances (radius ≈ 10−10 m) by a number of electrons, as
Figure 30.1 (not to scale) illustrates. In the natural state, an atom is electrically neu- tral because the nucleus contains a number of protons (each with a charge of +e) that equals the number of electrons (each with a charge of −e). This model of the atom is universally accepted now and is referred to as the nuclear atom.
The nuclear atom is a relatively recent idea. In the early part of the twentieth
century a widely accepted model, developed by the English physicist Joseph J. Thom-
son (1856–1940), pictured the atom very diff erently. In Thomson’s view there was no
nucleus at the center of an atom. Instead, the positive charge was assumed to be spread
throughout the atom, forming a kind of paste or pudding, in which the negative elec-
trons were suspended like plums.
The “plum-pudding” model was discredited in 1911 when the New Zealand
physicist Ernest Rutherford (1871–1937) published experimental results that the
model could not explain. As Interactive Figure 30.2 indicates, Rutherford and his co-workers directed a beam of alpha particles (𝛼 particles) at a thin metal foil made of gold. Alpha particles are positively charged particles (the nuclei of helium atoms,
although this was not recognized at the time) emitted by some radioactive materials. If 853
854 CHAPTER 30 The Nature of the Atom
the plum-pudding model were correct, the 𝛼 particles would be expected to pass nearly straight through the foil. After all, there is nothing in this model to defl ect the relatively massive 𝛼 par- ticles, since the electrons have a comparatively small mass and the positive charge is spread out
in a “diluted” pudding. Using a zinc sulfi de screen, which fl ashed briefl y when struck by an 𝛼 particle, Rutherford and co-workers were able to determine that not all the 𝛼 particles passed straight through the foil. Instead, some were defl ected at large angles, even backward. Rutherford
himself said, “It was almost as incredible as if you had fi red a fi fteen-inch shell at a piece of tissue
and it came back and hit you.” Rutherford concluded that the positive charge, instead of being
distributed thinly and uniformly throughout the atom, was concentrated in a small region called
the nucleus.
But how could the electrons in a nuclear atom remain separated from the positively charged
nucleus? If the electrons were stationary, they would be pulled inward by the attractive electric
force of the nuclear charge. Therefore, the electrons must be moving around the nucleus in some
fashion, like planets in orbit around the sun. In fact, the nuclear model of the atom is sometimes
referred to as the “planetary” model. The dimensions of the atom, however, are such that it
contains a larger fraction of empty space than our solar system does, as Conceptual Example 1
discusses.
FIGURE 30.1 In the nuclear atom a small positively charged nucleus is surrounded at
relatively large distances by a number of
electrons. Drawing is not to scale.
–
–
––
–
–
– –
Positive nucleus
+
Negative electron
Screen
Source of particles
Gold foil
INTERACTIVE FIGURE 30.2 A Rutherford scattering experiment in which 𝛼 particles are scattered by a thin gold foil. The entire
apparatus is located within a vacuum chamber
(not shown).
CONCEPTUAL EXAMPLE 1 Are Atoms Mostly Empty Space?
In the planetary model of the atom, the radius of the nucleus (≈1 × 10−15 m)
is analogous to the radius of the sun (≈7 × 108 m). The electrons orbit the
nucleus at a radial distance (≈1 × 10−10 m) that is analogous to the radial
distance (≈1.5 × 1011 m) at which the earth orbits the sun. Suppose that
the dimensions of the sun and the earth’s orbit had the same proportions
as those of an atomic nucleus and an electron’s orbit. What then would
be true about the distance between the earth and the sun? (a) It would be much greater than it actually is. (b) It would be much smaller than it actu- ally is. (c) It would be roughly the same as it actually is.
Reasoning The radius of an electron orbit is one hundred thousand times larger than the radius of the nucleus: (1 × 10−10 m)/(1 × 10−15 m) =
105. Using this factor with the radius of the sun will reveal the correct
answer.
Answers (b) and (c) are incorrect. Suppose that the earth’s orbital radius about the sun were indeed 105 times the sun’s radius. The distance between
the earth and the sun, then, would be 105 × (7 × 108 m) = 7 × 1013 m, which
is neither smaller than nor roughly the same as the actual distance.
Answer (a) is correct. If the earth’s orbital radius about the sun were 105 times the sun’s radius, the distance between the earth and the sun
would be 105 × (7 × 108 m) = 7 × 1013 m, which is more than four hun-
dred times greater than the actual orbital radius of 1.5 × 1011 m. In fact,
the earth would be more than ten times farther from the sun than is Pluto,
which has an orbital radius of about 6 × 1012 m. An atom, then, contains a
much greater fraction of empty space than does our solar system.
Related Homework: Problem 3
30.2 Line Spectra 855
Although the planetary model of the atom is easy to visualize, it too is fraught with dif-
fi culties. For instance, an electron moving on a curved path has a centripetal acceleration, as
Section 5.2 discusses. And when an electron is accelerating, it radiates electromagnetic waves,
as Section 24.1 discusses. These waves carry away energy. With their energy constantly being
depleted, the electrons would spiral inward and eventually collapse into the nucleus. Since
matter is stable, such a collapse does not occur. Thus, the planetary model, although providing
a more realistic picture of the atom than the “plum-pudding” model, must be telling only part
of the story. The full story of atomic structure is fascinating, and the next section describes
another aspect of it.
30.2 Line Spectra We have seen in Sections 13.3 and 29.2 that all objects emit electromagnetic waves, and we will
see in Section 30.3 how this radiation arises. For a solid object, such as the hot fi lament of a light
bulb, these waves have a continuous range of wavelengths, some of which are in the visible region
of the spectrum. The continuous range of wavelengths is characteristic of the entire collection
of atoms that make up the solid. In contrast, individual atoms, free of the strong interactions
that are present in a solid, emit only certain specifi c wavelengths rather than a continuous range.
These wavelengths are characteristic of the atom and provide important clues about its structure.
To study the behavior of individual atoms, low-pressure gases are used in which the atoms are
relatively far apart.
A low-pressure gas in a sealed tube can be made to emit electromagnetic waves by apply-
ing a suffi ciently large potential diff erence between two electrodes located within the tube. With
a grating spectroscope like that in Figure 27.36, the individual wavelengths emitted by the gas
can be separated and identifi ed as a series of bright fringes. The series of fringes is called a line spectrum because each bright fringe appears as a thin rectangle (a “line”) resulting from the large number of parallel, closely spaced slits in the grating of the spectroscope.
THE PHYSICS OF . . . neon signs and mercury vapor street lamps. Two familiar examples of low-pressure gases are the neon in neon signs and the mercury in mercury vapor
street lamps. Figure 30.3 shows the visible parts of the line spectra for these two atoms. The specifi c visible wavelengths that the atoms emit give neon signs and mercury vapor street lamps
their characteristic colors.
The simplest line spectrum is that of atomic hydrogen, and much eff ort has been devoted
to understanding the pattern of wavelengths that it contains. Figure 30.4 illustrates in schematic form some of the groups or series of lines in the spectrum of atomic hydrogen. Only one of the
Mercury (Hg)
Neon (Ne)
FIGURE 30.3 The line spectra for neon and mercury.
C o u rt
es y D
av id
P . Y
o u n g
856 CHAPTER 30 The Nature of the Atom
groups is in the visible region of the electromagnetic spectrum; it is known as the Balmer series, in recognition of Johann J. Balmer (1825–1898), a Swiss schoolteacher who found an empirical
equation that gave the values for the observed wavelengths. This equation is given next, along
with similar equations that apply to the Lyman series at shorter wavelengths and the Paschen series at longer wavelengths, which are also shown in the drawing:
Lyman series 1
λ = R ( 112 −
1
n2) n = 2, 3, 4, . . . (30.1)
Balmer series 1
λ = R ( 122 −
1
n2) n = 3, 4, 5, . . . (30.2)
Paschen series 1
λ = R ( 132 −
1
n2) n = 4, 5, 6, . . . (30.3) In these equations, the constant term R has the value of R = 1.097 × 107 m−1 and is called the Rydberg constant. An essential feature of each group of lines is that there are long and short wavelength limits, with the lines being increasingly crowded toward the short wavelength limit.
Figure 30.4 also gives these limits for each series, and Example 2 determines them for the Balmer series.
Lyman series
9 1
n m
1 2
2 n
m
3 6
5 n
m
6 5
6 n
m
8 2
0 n
m
1 8
7 5
n m
Balmer series
Wavelength, λ
Paschen series
FIGURE 30.4 Line spectrum of atomic hydrogen. Only the Balmer series lies in the visible region of the electromagnetic spectrum.
EXAMPLE 2 The Balmer Series
Find (a) the longest and (b) the shortest wavelengths of the Balmer series.
Reasoning Each wavelength in the series corresponds to one value for the integer n in Equation 30.2. Longer wavelengths are associated with smaller values of n. The longest wavelength occurs when n has its small- est value of n = 3. The shortest wavelength arises when n has a very large value, so that 1/n2 is essentially zero.
Solution (a) With n = 3, Equation 30.2 reveals that for the longest wavelength
1
λ = R ( 122 −
1
n2) = (1.097 × 107 m−1)( 1
22 −
1
32) = 1.524 × 106 m−1 or λ = 656 nm
(b) With 1/n2 = 0, Equation 30.2 reveals that for the shortest wavelength 1
λ = (1.097 × 107 m−1)( 122 − 0) = 2.743 × 106 m−1
or λ = 365 nm
Equations 30.1–30.3 are useful because they reproduce the wavelengths that hydrogen atoms
radiate. However, these equations are empirical and provide no insight as to why certain wave- lengths are radiated and others are not. It was the great Danish physicist, Niels Bohr (1885–
1962), who provided the fi rst model of the atom that predicted the discrete wavelengths emitted
by atomic hydrogen. Bohr’s model started us on the way toward understanding how the structure
of the atom restricts the radiated wavelengths to certain values. In 1922 Bohr received the Nobel
Prize in physics for his accomplishment.
30.3 The Bohr Model of the Hydrogen Atom 857
30.3 The Bohr Model of the Hydrogen Atom In 1913 Bohr presented a model that led to equations such as Balmer’s for the wavelengths that
the hydrogen atom radiates. Bohr’s theory begins with Rutherford’s picture of an atom as a
nucleus surrounded by electrons moving in circular orbits. In his theory, Bohr made a number
of assumptions and combined the new quantum ideas of Planck and Einstein with the traditional
description of a particle in uniform circular motion.
Adopting Planck’s idea of quantized energy levels (see Section 29.2), Bohr hypothesized that
in a hydrogen atom there can be only certain values of the total energy (electron kinetic energy plus
potential energy). These allowed energy levels correspond to diff erent orbits for the electron as it
moves around the nucleus, the larger orbits being associated with larger total energies. Animated Figure 30.5 illustrates two of the orbits. In addition, Bohr assumed that an electron in one of these orbits does not radiate electromagnetic waves. For this reason, the orbits are called stationary orbits or stationary states. Bohr recognized that radiationless orbits violated the laws of physics, as they were then known. But the assumption of such orbits was necessary, because the traditional
laws indicated that an electron radiates electromagnetic waves as it accelerates around a circular
path, and the loss of the energy carried by the waves would lead to the collapse of the orbit.
To incorporate Einstein’s photon concept (see Section 29.3), Bohr theorized that a photon is
emitted only when the electron changes orbits from a larger one with a higher energy to a smaller one with a lower energy, as Animated Figure 30.5 indicates. How do electrons get into the higher-energy orbits in the fi rst place? They get there by picking up energy when atoms collide,
which happens more often when a gas is heated, or by acquiring energy when a high voltage is
applied to a gas.
When an electron in an initial orbit with a larger energy Ei changes to a fi nal orbit with a smaller energy Ef, the emitted photon has an energy of Ei − Ef, consistent with the law of conser- vation of energy. But according to Einstein, the energy of a photon is hf, where f is its frequency and h is Planck’s constant. As a result, we fi nd that
Ei − Ef = hf (30.4)
Since the frequency of an electromagnetic wave is related to the wavelength by f = c/𝜆, Bohr could use Equation 30.4 to determine the wavelengths radiated by a hydrogen atom. First, how-
ever, he had to derive expressions for the energies Ei and Ef.
The Energies and Radii of the Bohr Orbits For an electron of mass m and speed 𝜐 in an orbit of radius r (see Figure 30.6), the total energy is the kinetic energy (KE =
1
2 mυ2) of the electron plus the electric potential energy EPE. The potential energy is the product of the charge (−e) on the electron and the electric potential produced by the positive nuclear charge, in accord with Equation 19.3. We assume that the nucleus contains Z pro- tons,* for a total nuclear charge of +Ze. The electric potential at a distance r from a point charge of +Ze is given as +kZe/r by Equation 19.6, where the constant k is k = 8.988 × 109 N · m2/C2. The elec- tric potential energy is, then, EPE = (−e)(+kZe/r). Consequently, the total energy E of the atom is
E = KE + EPE
= 1
2 mυ2 − kZe2
r (30.5)
But a centripetal force of magnitude m𝜐2/r (Equation 5.3) acts on a particle in uniform circular motion. As Figure 30.6 indicates, the centripetal force is provided by the electrostatic force of attraction F→ that the protons in the nucleus exert on the electron. According to Coulomb’s law (Equation 18.1), the magnitude of the electrostatic force is F = kZe2/r2. Therefore, m𝜐2/r = kZe2/r2, or
mυ2 = kZe2
r (30.6)
Electron
Ef
Ei
Nucleus
Photon–
+
ANIMATED FIGURE 30.5 In the Bohr model, a photon is emitted when the electron
drops from a larger, higher-energy orbit
(energy = Ei) to a smaller, lower-energy orbit (energy = Ef).
Electron –e
v
r
F
+Ze
FIGURE 30.6 In the Bohr model, the electron is in uniform circular motion around the
nucleus. The centripetal force F→ is the electrostatic force of attraction that the positive
nuclear charge exerts on the electron.*For hydrogen, Z = 1, but we also wish to consider situations in which Z is greater than 1.
858 CHAPTER 30 The Nature of the Atom
We can use this relation to eliminate the term m𝜐2 from Equation 30.5, with the result that
E = 1
2 (kZe
2
r ) − kZe2
r = − kZe2
2r (30.7)
The total energy of the atom is negative because the negative electric potential energy is larger in
magnitude than the positive kinetic energy.
A value for the radius r is needed, if Equation 30.7 is to be useful. To determine r, Bohr made an assumption about the orbital angular momentum of the electron. The magnitude L of the angular momentum is given by Equation 9.10 as L = I𝜔, where I = mr2 is the moment of inertia of the electron moving on its circular path and 𝜔 = 𝜐/r (Equation 8.9) is the angular speed of the electron in radians per second. Thus, the angular momentum is L = (mr2)(𝜐/r) = m𝜐r. Bohr conjectured that the angular momentum can assume only certain discrete values; in other words,
L is quantized. He postulated that the allowed values are integer multiples of Planck’s constant divided by 2𝜋:
Ln = mυnrn = n h
2π n = 1, 2, 3, . . . (30.8)
Solving this equation for 𝜐n and substituting the result into Equation 30.6 lead to the following expression for the radius rn of the nth Bohr orbit:
rn = ( h 2
4π 2mke2) n2
Z n = 1, 2, 3, . . . (30.9)
Math Skills To obtain Equation 30.9 for the radius rn, we begin by writing Equation 30.6 with the symbols 𝜐n instead of 𝜐 and rn instead of r:
mυ2n = kZe2
rn (30.6)
Next, we solve m𝜐nrn = n h
2π (Equation 30.8) for 𝜐n, by dividing both sides by mrn:
mυn rn (mrn)
= n h
2π(mrn) or υn =
nh 2πmrn
(1)
Substituting Equation 1 into Equation 30.6, we obtain
m ( nh2πmrn) 2
= kZe2
rn or
n2h2
4π 2mr 2n =
kZe2
rn (2)
To isolate rn on one side of the equals sign in Equation 2, we multiply both sides by r 2n
kZe2 :
n2h2
4π2mrn2 (
rn2
kZe2 ) = kZe
2
rn (
rnrn kZe2) or
n2 h2
4π2 mkZe2 = rn (3)
Finally, in Equation 3, we factor out the term n2
Z to give
rn = ( h 2
4π2 mke2) n2
Z (30.9)
υ2n
With h = 6.626 × 10−34 J · s, m = 9.109 × 10−31 kg, k = 8.988 × 109 N · m2/C2, and e = 1.602 × 10−19 C, this expression reveals that
Radii for Bohr orbits (in meters) rn = (5.29 × 10
−11 m) n2
Z n = 1, 2, 3, . . . (30.10)
Therefore, in the hydrogen atom (Z = 1) the smallest Bohr orbit (n = 1) has a radius of r1 = 5.29 × 10−11 m. This particular value is called the Bohr radius. Figure 30.7 shows the fi rst three Bohr orbits for the hydrogen atom.
n = 3
n = 2
n = 1
r1
r2
r3
FIGURE 30.7 The fi rst Bohr orbit in the hydrogen atom has a radius r1 = 5.29 × 10−11 m. The second and third Bohr orbits have radii
r2 = 4r1 and r3 = 9r1, respectively.
30.3 The Bohr Model of the Hydrogen Atom 859
Equation 30.9 for the radius of a Bohr orbit can be substituted into Equation 30.7 to show
that the corresponding total energy for the nth orbit is
En = −(2π 2mk2e4
h2 ) Z 2
n2 n = 1, 2, 3, . . . (30.11)
Substituting values for h, m, k, and e into this expression yields
Bohr energy levels in joules En = −(2.18 × 10
−18 J) Z 2
n2 n = 1, 2, 3, . . . (30.12)
Often, atomic energies are expressed in units of electron volts rather than joules. Since 1.60 ×
10−19 J = 1 eV, Equation 30.12 can be rewritten as
Bohr energy levels in electron volts En = −(13.6 eV)
Z 2
n2 n = 1, 2, 3, . . . (30.13)
Energy Level Diagrams It is useful to represent the energy values given by Equation 30.13 on an energy level diagram, as in Figure 30.8. In this diagram, which applies to the hydrogen atom (Z = 1), the highest energy level corresponds to n = ∞ in Equation 30.13 and has an energy of 0 eV. This is the energy of the atom when the electron is completely removed (r = ∞) from the nucleus and is at rest. In contrast, the lowest energy level corresponds to n = 1 and has a value of −13.6 eV. The lowest energy level is called the ground state, to distinguish it from the higher levels, which are called excited states. Observe how the energies of the excited states come closer and closer together as n increases.
The electron in a hydrogen atom at room temperature spends most of its time in the ground
state. To raise the electron from the ground state (n = 1) to the highest possible excited state (n = ∞), 13.6 eV of energy must be supplied. Supplying this amount of energy removes the electron
from the atom, producing the positive hydrogen ion H+. This is the minimum energy needed to
remove the electron and is called the ionization energy. Thus, the Bohr model predicts that the ionization energy of atomic hydrogen is 13.6 eV, in excellent agreement with the experimental
value. In Example 3 the Bohr model is applied to doubly ionized lithium.
FIGURE 30.8 Energy level diagram for the hydrogen atom.
–0.54 eV –0.85 eV
–1.51 eV
0
–3.40 eV
–13.6 eV n = 1, Ground state
n = 2
n = 3
n = 4 n = 5
Excited states
n = ∞, Electron removed from atom
Total energy, E
EXAMPLE 3 The Ionization Energy of Li2+
The Bohr model does not apply when more than one electron orbits the
nucleus because it does not account for the electrostatic force that one
electron exerts on another. For instance, an electrically neutral lithium
atom (Li) contains three electrons in orbit around a nucleus that in-
cludes three protons (Z = 3), and Bohr’s analysis is not applicable. However, the Bohr model can be used for the doubly charged positive
ion of lithium (Li2+) that results when two electrons are removed from
the neutral atom, leaving only one electron to orbit the nucleus. Obtain
the ionization energy that is needed to remove the remaining electron
from Li2+.
Reasoning The lithium ion Li2+ contains three times the positive nuclear charge that the hydrogen atom contains. Therefore, the orbiting electron
is attracted more strongly to the nucleus in Li2+ than to the nucleus in the
hydrogen atom. As a result, we expect that more energy is required to
ionize Li2+ than the 13.6 eV required for atomic hydrogen.
Solution The Bohr energy levels for Li2+ are obtained from Equation 30.13 with Z = 3; En = −(13.6 eV)(32/n2). Therefore, the ground state (n = 1) energy is
E1 = −(13.6 eV) 32
12 = −122 eV
Removing the electron from Li2+ requires 122 eV of energy:
Ionization energy = 122 eV .
This value for the ionization energy agrees well with the experimental
value of 122.4 eV and, as expected, is greater than the 13.6 eV required
for atomic hydrogen.
The Line Spectra of the Hydrogen Atom To predict the wavelengths in the line spectrum of the hydrogen atom, Bohr combined his ideas
about atoms (electron orbits are stationary orbits and the angular momentum of an electron is
860 CHAPTER 30 The Nature of the Atom
quantized) with Einstein’s idea of the photon. As applied by Bohr, the photon concept is inherent
in Equation 30.4, Ei − Ef = hf, which states that the frequency f of the photon is proportional to the diff erence between two energy levels of the hydrogen atom. If we substitute Equation 30.11
for the total energies Ei and Ef into Equation 30.4 and recall from Equation 16.1 that f = c/𝜆, we obtain the following result:
1
λ =
2π 2mk2e4
h3c (Z 2) ( 1nf 2 −
1
ni 2) (30.14) ni, nf = 1, 2, 3, . . . and ni > nf
Using known values for h, m, k, e, and c, we fi nd that 2𝜋2mk2e4/(h3c) = 1.097 × 107 m−1, in agree- ment with the Rydberg constant R that appears in Equations 30.1–30.3. The agreement between the theoretical and experimental values of the Rydberg constant was a major accomplishment of
Bohr’s theory.
With Z = 1 and nf = 1, Equation 30.14 reproduces Equation 30.1 for the Lyman series. Thus, Bohr’s model shows that the Lyman series of lines occurs when electrons make transi-
tions from higher energy levels with ni = 2, 3, 4, . . . to the fi rst energy level where nf = 1. Figure 30.9 shows these transitions. Notice that when an electron makes a transition from ni = 2 to nf = 1, the longest wavelength photon in the Lyman series is emitted, since the energy change is the smallest possible. When an electron makes a transition from the highest level
where ni = ∞ to the lowest level where nf = 1, the shortest wavelength is emitted, since the energy change is the largest possible. Since the higher energy levels are increasingly close
together, the lines in the series become more and more crowded toward the short wavelength
limit, as can be seen in Figure 30.4. Figure 30.9 also shows the energy level transitions for the Balmer series, where ni = 3, 4, 5, . . . , and nf = 2. In the Paschen series (see Figure 30.4) ni = 4, 5, 6, . . . , and nf = 3. The next example deals further with the line spectrum of the hydrogen atom.
0 –0.54 eV –0.85 eV –1.51 eV
–3.40 eV
–13.6 eV
n = ∞ n = 5 n = 4 n = 3
n = 2
n = 1
Total energy, E
Balmer series
Lyman series
FIGURE 30.9 The Lyman and Balmer series of lines in the hydrogen atom spectrum
correspond to transitions that the electron
makes between higher and lower energy
levels, as indicated here.
EXAMPLE 4 The Brackett Series for Atomic Hydrogen
In the line spectrum of atomic hydrogen there is also a group of lines
known as the Brackett series. These lines are produced when electrons,
excited to high energy levels, make transitions to the n = 4 level. Deter- mine (a) the longest wavelength in this series and (b) the wavelength that corresponds to the transition from ni = 6 to nf = 4. (c) Refer to Figure 24.9 and identify the spectral region in which these lines are found.
Reasoning The longest wavelength corresponds to the transition that has the smallest energy change, which is between the ni = 5 and nf = 4 levels in Figure 30.8. The wavelength for this transition, as well as that for the transition from ni = 6 to nf = 4, can be obtained from Equation 30.14.
Problem-Solving Insight In the line spectrum of atomic hydrogen, all lines in a given series (e.g., the Brackett series) are identifi ed by a single value of the quantum number nf for the lower energy level into which an electron falls. Each line in a given series, however, corresponds to a diff erent value of the quantum number ni for the higher energy level where an electron originates.
Solution (a) Using Equation 30.14 with Z = 1, ni = 5, and nf = 4, we fi nd that
1
λ = (1.097 × 107 m−1)(12)( 142 −
1
52) = 2.468 × 105 m−1 or λ = 4051 nm
(b) The calculation here is similar to that in part (a):
1
λ = (1.097 × 107 m−1)(12)( 142 −
1
62) = 3.809 × 105 m−1
or λ = 2625 nm
(c) According to Figure 24.9, these lines lie in the infrared region of the spectrum.
The various lines in the hydrogen atom spectrum are produced when electrons change from
higher to lower energy levels and photons are emitted. Consequently, the spectral lines are called
emission lines. Electrons can also make transitions in the reverse direction, from lower to higher levels, in a process known as absorption. In this case, an atom absorbs a photon that has precisely
30.4 De Broglie’s Explanation of Bohr’s Assumption About Angular Momentum 861
the energy needed to produce the transition. Thus, if photons with a continuous range of wave-
lengths pass through a gas and then are analyzed with a grating spectroscope, a series of dark
absorption lines appears in the continuous spectrum. The dark lines indicate the wavelengths removed by the absorption process.
THE PHYSICS OF . . . absorption lines in the sun’s spectrum. Absorption lines can be seen in Figure 30.10 in the spectrum of the sun, where they are called Fraunhofer lines, after their discoverer. They are due to atoms, located in the outer and cooler layers of the sun, that absorb
radiation coming from the interior. The interior portion of the sun is too hot for individual atoms
to retain their structures and, therefore, the interior emits a continuous spectrum of wavelengths.
The Bohr model provides a great deal of insight into atomic structure. However, this model
is now known to be oversimplifi ed and has been superseded by a more detailed picture provided
by quantum mechanics and the Schrödinger equation (see Section 30.5).
Check Your Understanding
(The answers are given at the end of the book.) 1. Which one of the following statements is true? (a) An atom is less easily ionized when its outermost
electron is in an excited state than when it is in the ground state. (b) An atom is more easily ionized when its outermost electron is in an excited state than when it is in the ground state. (c) The energy state (excited state or ground state) of the outermost electron in an atom has nothing to do with how easily
the atom can be ionized.
2. An electron in the hydrogen atom is in the n = 4 energy level. When this electron makes a transition to a lower energy level, is the wavelength of the photon emitted in (a) the Lyman series only, (b) the Balmer series only, (c) the Paschen series only, or (d) could it be in the Lyman, the Balmer, or the Paschen series?
3. A tube contains atomic hydrogen, and nearly all of the electrons in the atoms are in the ground state or n = 1 energy level. Electromagnetic radiation with a continuous spectrum of wavelengths (including those in the Lyman, Balmer, and Paschen series) enters one end of the tube and leaves the other end.
The exiting radiation is found to contain strong absorption lines. To which one or more of the series do
the wavelengths of these absorption lines correspond? Assume that once an electron absorbs a photon
and jumps to a higher energy level, it does not absorb yet another photon and jump to an even higher
energy level.
30.4 De Broglie’s Explanation of Bohr’s Assumption About Angular Momentum Of all the assumptions Bohr made in his model of the hydrogen atom, perhaps the most puzzling
is the assumption about the angular momentum of the electron [Ln = m𝜐nrn = nh/(2𝜋); n = 1, 2, 3, . . .]. Why should the angular momentum have only those values that are integer multiples of
Planck’s constant divided by 2𝜋? In 1923, ten years after Bohr’s work, de Broglie pointed out that his own theory for the wavelength of a moving particle could provide an answer to this question.
In de Broglie’s way of thinking, the electron in its circular Bohr orbit must be pictured as
a particle wave. And like waves traveling on a string, particle waves can lead to standing waves
FIGURE 30.10 Illustration of the sun's visible spectrum. Dark lines in the sun's spectrum are absorption lines called Fraunhofer lines, in honor of their discoverer. There are thousands of these absorption lines in
the sun's spectrum. The locations of three of the more prominent Fraunhofer lines are marked by arrows.
862 CHAPTER 30 The Nature of the Atom
under resonant conditions. Section 17.5 discusses these conditions for a string. Standing waves
form when the total distance traveled by a wave down the string and back is one wavelength, two
wavelengths, or any integer number of wavelengths. The total distance around a Bohr orbit of
radius r is the circumference of the orbit or 2𝜋r. By the same reasoning, then, the condition for standing particle waves for the electron in a Bohr orbit would be
2πr = nλ n = 1, 2, 3, . . .
where n is the number of whole wavelengths that fi t into the circumference of the circle. But according to Equation 29.8 the de Broglie wavelength of the electron is𝜆 = h/p, where p is the magnitude of the electron’s momentum. If the speed of the electron is much less than the speed
of light, the momentum is p = m𝜐, and the condition for standing particle waves becomes 2𝜋r = nh/(m𝜐). A rearrangement of this result gives
mυr = n h
2π n = 1, 2, 3, . . .
which is just what Bohr assumed for the angular momentum of the electron. As an example,
Figure 30.11 illustrates the standing particle wave on a Bohr orbit for which 2𝜋r = 4𝜆. De Broglie’s explanation of Bohr’s assumption about angular momentum emphasizes an
important fact—namely, that particle waves play a central role in the structure of the atom. More-
over, the theoretical framework of quantum mechanics includes the Schrödinger equation for
determining the wave function ψ (Greek letter psi) that represents a particle wave. The next
section deals with the picture that quantum mechanics gives for atomic structure, a picture that
supersedes the Bohr model. In any case, the Bohr expression for the energy levels (Equation
30.11) can be applied when a single electron orbits the nucleus, whereas the theoretical frame-
work of quantum mechanics can be applied, in principle, to atoms that contain an arbitrary num-
ber of electrons.
30.5 The Quantum Mechanical Picture of the Hydrogen Atom The picture of the hydrogen atom that quantum mechanics and the Schrödinger equation provide
diff ers in a number of ways from the Bohr model. The Bohr model uses a single integer number n to identify the various electron orbits and the associated energies. Because this number can have
only discrete values, rather than a continuous range of values, n is called a quantum number. In contrast, quantum mechanics reveals that four diff erent quantum numbers are needed to describe
each state of the hydrogen atom. These four are described as follows:
1. The principal quantum number n. As in the Bohr model, this number determines the total energy of the atom and can have only integer values: n = 1, 2, 3, . . . . In fact, the Schrödinger equation predicts* that the energy of the hydrogen atom is identical to the energy obtained
from the Bohr model: En = −(13.6 eV) Z2/n2. 2. The orbital quantum number ℓ. This number determines the angular momentum of the
electron due to its orbital motion. The values that ℓ can have depend on the value of n, and only the following integers are allowed:
ℓ = 0, 1, 2, . . . , (n − 1)
For instance, if n = 1, the orbital quantum number can have only the value ℓ = 0, but if n = 4, the values ℓ = 0, 1, 2, and 3 are possible. The magnitude L of the angular momentum of the electron is
L = √ℓ(ℓ + 1) h
2π (30.15)
r Nucleus
λ
FIGURE 30.11 De Broglie suggested standing particle waves as an explanation for
Bohr’s angular momentum assumption. Here,
a standing particle wave is illustrated on a
Bohr orbit where four de Broglie wavelengths
fi t into the circumference of the orbit.
*This prediction requires that small relativistic eff ects and small interactions within the atom be ignored, and assumes
that the hydrogen atom is not located in an external magnetic fi eld.
30.5 The Quantum Mechanical Picture of the Hydrogen Atom 863
3. The magnetic quantum number mℓ . The word “magnetic” is used here because an externally applied magnetic fi eld infl uences the energy of the atom, and this quantum number is used in describing the eff ect. Since the eff ect was discovered by the Dutch physicist Pieter Zeeman (1865–1943), it is known as the Zeeman eff ect. When there is no external magnetic fi eld, mℓ plays no role in determining the energy. In either event, the magnetic quantum number determines the component of the angular momentum along a specifi c direction, which is called the z direction by convention. The values that mℓ can have depend on the value of ℓ, with only the following positive and negative integers being permitted:
mℓ = −ℓ, . . . , − 2, − 1, 0, + 1, + 2, . . . , + ℓ
For example, if the orbital quantum number is ℓ = 2, then the magnetic quantum number can have the values mℓ = −2, −1, 0, +1, and +2. The component Lz of the angular momentum in the z direction is
Lz = mℓ h
2π (30.16)
4. The spin quantum number ms. This number is needed because the electron has an intrinsic property called “spin angular momentum.” Loosely speaking, we can view the electron as spinning while it orbits the nucleus, analogous to the way the earth spins as it orbits the sun. There are two possible values for the spin quantum number of the electron:
ms = + 1 2 or ms = −
1 2
Sometimes the phrases “spin up” and “spin down” are used to refer to the directions of the spin angular momentum associated with the values for ms.
Table 30.1 summarizes the four quantum numbers that are needed to describe each state of the hydrogen atom. One set of values for n, ℓ, mℓ, and ms corresponds to one state. As the principal quantum number n increases, the number of possible combinations of the four quantum numbers rises rapidly, as Example 5 illustrates.
TABLE 30.1 Quantum Numbers for the Hydrogen Atom
Name Symbol Allowed Values Principal quantum number n 1, 2, 3, . . .
Orbital quantum number ℓ 0, 1, 2, . . . , (n − 1)
Magnetic quantum number mℓ −ℓ, . . . , −2, −1, 0, +1, +2, . . . , +ℓ
Spin quantum number ms −12 or + 1 2
EXAMPLE 5 Quantum Mechanical States of the Hydrogen Atom
Determine the number of possible states for the hydrogen atom when the principal quantum number is (a) n = 1 and (b) n = 2.
Reasoning Each diff erent combination of the four quantum numbers summarized in Table 30.1 corresponds to a diff erent state. We begin with the value for n and fi nd the allowed values for ℓ. Then, for each ℓ value
we fi nd the possibilities for mℓ. Finally, ms may be + 1 2 or −
1 2 for each group
of values for n, ℓ, and mℓ.
Solution (a) The diagram below shows the possibilities for ℓ, mℓ, and ms when n = 1:
n = 1 ℓ = 0 mℓ = 0 ms = + 1 0 0
State
+
n ℓ mℓ ms
1 0 0 − ms = −
1 2
1 2
1 2
1 2
864 CHAPTER 30 The Nature of the Atom
Quantum mechanics provides a more accurate picture of atomic structure than does the Bohr
model. It is important to realize that the two pictures diff er substantially, as Conceptual Example 6
illustrates.
Thus, there are two diff erent states for the hydrogen atom. In the absence
of an external magnetic fi eld, these two states have the same energy, since
they have the same value of n.
With the same value of n = 2, all eight states have the same energy when there is no external magnetic fi eld.
(b) When n = 2, there are eight possible combinations for the values of n, ℓ, mℓ, and ms, as the diagram below indicates:
n = 2
ℓ = 1
ℓ = 0
ms = + mℓ = +1
2 1 +1
State
+
n ℓ mℓ ms
2 1 +1 − ms = −
ms = + mℓ = 0
2 1 0 −
2 1 0 +
ms = −
ms = + mℓ = −1
2 1 −1 −
2 1 −1 +
ms = −
ms = + mℓ = 0
2 0 0 −
2 0 0 +
ms = −
1 2
1 2
1 2
1 2
1 2
1 2
1 2
1 2
1 2
1 2
1 2
1 2
1 2
1 2
1 2
1 2
CONCEPTUAL EXAMPLE 6 The Bohr Model Versus Quantum Mechanics
Consider two hydrogen atoms. There are no external magnetic fi elds pres-
ent, and the electron in each atom has the same energy. According to the
Bohr model and to quantum mechanics, is it possible for the electrons in
these atoms (a) to have zero orbital angular momentum and (b) to have diff erent orbital angular momenta?
Reasoning and Solution (a) In both the Bohr model and quantum mechanics, the energy is proportional to 1/n2, according to Equation 30.13, where n is the principal quantum number. Moreover, the value of n may be n = 1, 2, 3, . . . , and may not be zero. In the Bohr model, the fact that n may not be zero means that it is not possible for the orbital angular momentum to be zero because the angular momentum is pro- portional to n, according to Equation 30.8. In the quantum mechanical picture the magnitude of the orbital angular momentum is proportional to
√ℓ(ℓ + 1), as given by Equation 30.15. Here, ℓ is the orbital quantum
number and may take on the values ℓ = 0, 1, 2, . . . , (n − 1). We note that ℓ [and therefore √ℓ(ℓ + 1)] may be zero, no matter what the value for n is. Consequently, the orbital angular momentum may be zero according to quantum mechanics, in contrast to the case for the Bohr model.
(b) If the electrons have the same energy, they have the same value for the principal quantum number n. In the Bohr model, this means that
they cannot have diff erent values for the orbital angular momentum Ln, since Ln = nh/(2𝜋), according to Equation 30.8. In quantum mechanics, the energy is also determined by n when external magnetic fi elds are ab- sent, but the orbital angular momentum is determined by ℓ. Since ℓ = 0,
1, 2, . . . , (n − 1), diff erent values of ℓ are compatible with the same value of n. For instance, if n = 2 for both electrons, one of them could have ℓ = 0, while the other could have ℓ = 1. According to quantum mechanics, then, the electrons could have diff erent orbital angular momenta, even though they have the same energy.
The following table summarizes the discussion from parts (a) and (b):
Bohr Model
Quantum Mechanics
(a) For a given n, can the angular momentum ever be zero?
No Yes
(b) For a given n, can the angular momentum have different values? No Yes
Related Homework: Problem 57
30.5 The Quantum Mechanical Picture of the Hydrogen Atom 865
According to the Bohr model, the nth orbit is a circle of radius rn, and every time the position of the electron in this orbit is measured, the electron is found exactly at a distance rn away from the nucleus. This simplistic picture is now known to be incorrect, and the quantum mechanical
picture of the atom has replaced it. Suppose that the electron is in a quantum mechanical state
for which n = 1, and we imagine making a number of measurements of the electron’s position with respect to the nucleus. We would fi nd that its position is uncertain, in the sense that there
is a probability of fi nding the electron sometimes very near the nucleus, sometimes very far
from the nucleus, and sometimes at intermediate locations. The probability is determined by
the wave function ψ, as Section 29.5 discusses. We can make a three-dimensional picture of
our fi ndings by marking a dot at each location where the electron is found. More dots occur at
places where the probability of fi nding the electron is higher, and after a suffi cient number of
measurements, a picture of the quantum mechanical state emerges. Figure 30.12 shows the spa- tial distribution for the position of an electron in a state for which n = 1, ℓ = 0, and mℓ = 0. This picture is constructed from so many measurements that the individual dots are no longer visible
but have merged to form a kind of probability “cloud” whose density changes gradually from
place to place. The dense regions indicate places where the probability of fi nding the electron is
higher, and the less dense regions indicate places where the probability is lower. Also indicated in
Figure 30.12 is the radius where quantum mechanics predicts the greatest probability per unit radial distance of fi nding the electron in the n = 1 state. This radius matches exactly the radius of 5.29 × 10−11 m found for the fi rst Bohr orbit.
For a principal quantum number of n = 2, the probability clouds are diff erent than for n = 1. In fact, more than one cloud shape is possible because with n = 2 the orbital quantum number can be either ℓ = 0 or ℓ = 1. Although the value of ℓ does not aff ect the energy of the
hydrogen atom, the value does have a signifi cant eff ect on the shape of the probability clouds.
Figure 30.13a shows the cloud for n = 2, ℓ = 0, and mℓ = 0. Part b of the drawing shows that when n = 2, ℓ = 1, and mℓ = 0, the cloud has a two-lobe shape with the nucleus at the center between the lobes. For larger values of n, the probability clouds become increasingly complex and are spread out over larger volumes of space.
The probability cloud picture of the electron in a hydrogen atom is very diff erent from the
well-defi ned orbit of the Bohr model. The fundamental reason for this diff erence is to be found in
the Heisenberg uncertainty principle, as Conceptual Example 7 discusses.
Most probable distance for the electron
n = 1 ℓ = 0
mℓ = 0
FIGURE 30.12 The electron probability cloud for the ground state (n = 1, ℓ = 0, mℓ = 0) of the hydrogen atom.
n = 2 ℓ = 1
mℓ = 0
(a)
(b)
n = 2 ℓ = 0
mℓ = 0
FIGURE 30.13 The electron probability clouds for the hydrogen atom when (a) n = 2, ℓ = 0, mℓ = 0 and (b) n = 2, ℓ = 1, mℓ = 0.
CONCEPTUAL EXAMPLE 7 The Uncertainty Principle and the Hydrogen Atom
In the Bohr model of the hydrogen atom, the electron in the ground state
(n = 1) is in an orbit that has a radius of exactly 5.29 × 10−11 m, so that the uncertainty Δy in its radial position is Δy = 0 m. According to the Heisen- berg uncertainty principle, what does the fact that there is no uncertainty
in the electron’s radial position imply about the electron’s radial speed?
The uncertainty principle implies (a) nothing about the radial speed, (b) that the radial speed has only a small uncertainty, (c) that the radial speed has an infi nitely large uncertainty.
Reasoning We need to obtain an expression for the uncertainty in the radial speed of the electron to use as a guide. As stated in Equation 29.10,
the Heisenberg principle is (∆py)(∆y) ≥ h/ (4π). In the present con- text, Δy is the uncertainty in the electron’s radial position, so that Δpy
is the uncertainty in the electron’s radial momentum. According to Equa-
tion 7.2, however, the magnitude of the momentum is py = m𝜐y, where m is the electron’s mass and 𝜐y is the electron’s radial speed. As a result, the uncertainty in the momentum is Δpy = Δ(m𝜐y) = mΔ𝜐y. With this substi- tution for Δpy, the Heisenberg principle becomes (mΔ𝜐y)(Δy) ≥ h/(4𝜋), which can be rearranged to show that
∆υy ≥ h
m(∆y) (4π)
Answers (a) and (b) are incorrect. Our result for Δ𝜐y shows that the Heisenberg principle does indeed imply something about the uncertainty
in the electron’s radial speed. Since Δy = 0 m in the Bohr model, our
866 CHAPTER 30 The Nature of the Atom
Check Your Understanding
(The answers are given at the end of the book.) 4. In the Bohr model for the hydrogen atom, the closer the electron is to the nucleus, the smaller is the
total energy of the electron. Is this also true in the quantum mechanical picture of the hydrogen atom?
5. In the quantum mechanical picture of the hydrogen atom, the orbital angular momentum of the elec- tron may be zero in any of the possible energy states. For which energy state must the orbital angular momentum be zero?
6. Consider two diff erent hydrogen atoms. The electron in each atom is in a diff erent excited state, so that each electron has a diff erent total energy. Is it possible for the electrons to have the same orbital angular
momentum L, according to (a) the Bohr model and (b) quantum mechanics? 7. The magnitude of the orbital angular momentum of the electron in a hydrogen atom is observed to
increase. According to (a) the Bohr model and (b) quantum mechanics, does this necessarily mean that the total energy of the electron also increases?
30.6 The Pauli Exclusion Principle and the Periodic Table of the Elements Except for hydrogen, all electrically neutral atoms contain more than one electron, with the num-
ber given by the atomic number Z of the element. In addition to being attracted by the nucleus, the electrons repel each other. This repulsion contributes to the total energy of a multiple-electron
atom. As a result, the one-electron energy expression for hydrogen, En = −(13.6 eV) Z2/n2, does not apply to other neutral atoms. However, the simplest approach for dealing with a multiple-
electron atom still uses the four quantum numbers n, ℓ, mℓ, and ms. Detailed quantum mechanical calculations reveal that the energy level of each state of a multiple-
electron atom depends on both the principal quantum number n and the orbital quantum number ℓ. Figure 30.14 illustrates that the energy generally increases as n increases, but there are exceptions, as the drawing indicates. Furthermore, for a given n, the energy also increases as ℓ increases.
In a multiple-electron atom, all electrons with the same value of n are said to be in the same shell. Electrons with n = 1 are in a single shell (sometimes called the K shell), electrons with n = 2 are in another shell (the L shell), those with n = 3 are in a third shell (the M shell), and so on. Those electrons with the same values for both n and ℓ are often referred to as being in the same subshell. The n = 1 shell consists of a single ℓ = 0 subshell. The n = 2 shell has two subshells, one with ℓ = 0 and one with ℓ = 1. Similarly, the n = 3 shell has three subshells, one with ℓ = 0, one with ℓ = 1, and one with ℓ = 2.
In the hydrogen atom near room temperature, the electron spends most of its time in the lowest
energy level, or ground state—namely, in the n = 1 shell. Similarly, when an atom contains more than one electron and is near room temperature, the electrons spend most of their time in the lowest energy
levels possible. The lowest energy state for an atom is called the ground state. However, when a multiple-electron atom is in its ground state, not every electron is in the n = 1 shell in general because the electrons obey a principle discovered by the Austrian physicist Wolfgang Pauli (1900–1958).
THE PAULI EXCLUSION PRINCIPLE No two electrons in an atom can have the same set of values for the four quantum num- bers n, ℓ, mℓ, and ms.
result for Δ𝜐y shows that the uncertainty in the speed is infi nitely large (Δy is in the denominator on the right). Therefore, answers (a) and (b) cannot be correct.
Answer (c) is correct. Our expression for Δ𝜐y shows that, in fact, the uncertainty in the radial speed is infi nitely large (Δy = 0 m in the Bohr model and Δy is in the denominator on the right in the expression above).
Such a large uncertainty in the radial speed means that the electron may be
moving very rapidly in the radial direction and, therefore, would not remain
in its Bohr orbit. Quantum mechanics, with its probability-cloud picture of
atomic structure, correctly represents the positional and motional uncer-
tainty that the Heisenberg principle reveals. The Bohr model does not cor-
rectly represent this aspect of reality at the atomic level.
Exception
Exception
Highest energy
Lowest energy
ℓ = 2
n = 5
n = 4
n = 3
n = 2
n = 1
ℓ = 0
ℓ = 1
ℓ = 2
ℓ = 0
ℓ = 1
ℓ = 0
ℓ = 1
ℓ = 0
ℓ = 0
FIGURE 30.14 When there is more than one electron in an atom, the total energy of a
given state depends on the principal quantum
number n and the orbital quantum number ℓ. The energy increases with increasing n (with some exceptions) and, for a fi xed n, with increasing ℓ. For clarity, levels for n = 6 and higher are not shown.
30.6 The Pauli Exclusion Principle and the Periodic Table of the Elements 867
Suppose two electrons in an atom have three quantum numbers that are identical: n = 3, mℓ = 1, and ms = −
1
2. According to the exclusion principle, it is not possible for each to have ℓ = 2, for example, since each would then have the same four quantum numbers. Each electron must have
a diff erent value for ℓ (for instance, ℓ = 1 and ℓ = 2) and, consequently, would be in a diff erent subshell. With the aid of the Pauli exclusion principle, we can determine which energy levels are
occupied by the electrons in an atom in its ground state, as the next example demonstrates.
EXAMPLE 8 Ground States of Atoms
Determine which of the energy levels in Figure 30.14 are occupied by the electrons in the ground state of hydrogen (1 electron), helium (2 electrons),
lithium (3 electrons), beryllium (4 electrons), and boron (5 electrons).
Reasoning In the ground state of an atom the electrons are in the low- est available energy levels. Consistent with the Pauli exclusion principle,
they fi ll those levels “from the bottom up”—that is, from the lowest to the
highest energy.
Solution As the colored dot (⦁) in Figure 30.15 indicates, the electron in the hydrogen atom (H) is in the n = 1, ℓ = 0 subshell, which has the lowest possible energy. A second electron is present in the helium atom (He), and
both electrons can have the quantum numbers n = 1, ℓ = 0, and mℓ = 0. How- ever, in accord with the Pauli exclusion principle, each electron must have a
diff erent spin quantum number, ms = + 1
2 for one electron and ms = − 1
2 for
the other. Thus, the drawing shows both electrons in the lowest energy level.
The third electron that is present in the lithium atom (Li) would violate
the exclusion principle if it were also in the n = 1, ℓ = 0 subshell, no matter what the value for ms is. Thus, the n = 1, ℓ = 0 subshell is fi lled when oc- cupied by two electrons. With this level fi lled, the n = 2, ℓ = 0 subshell be- comes the next lowest energy level available and is where the third electron
of lithium is found (see Figure 30.15). In the beryllium atom (Be), the fourth electron is in the n = 2, ℓ = 0 subshell, along with the third electron. This is possible, since the third and fourth electrons can have diff erent values for ms.
With the fi rst four electrons in place as just discussed, the fi fth elec-
tron in the boron atom (B) cannot fi t into the n = 1, ℓ = 0 or the n = 2, ℓ = 0 subshell without violating the exclusion principle. Therefore, the
fi fth electron is found in the n = 2, ℓ = 1 subshell, which is the next avail- able energy level with the lowest energy, as Figure 30.15 indicates. For this electron, mℓ can be −1, 0, or +1, and ms can be +
1
2 or − 1
2 in each case.
However, in the absence of an external magnetic fi eld, all six possibilities
correspond to the same energy.
H He Li Be B
Highest energy
Lowest energy
ℓ = 1
ℓ = 0
ℓ = 0
n = 2
n = 1
FIGURE 30.15 The electrons (⦁) in the ground state of an atom fi ll the available energy levels “from the bottom
up”—that is, from the lowest to the highest energy, consis-
tent with the Pauli exclusion principle. The ranking of the
energy levels in this fi gure is meant to apply for a given
atom only.
Because of the Pauli exclusion principle, there is a maximum number of electrons that can fi t
into an energy level or subshell. Example 8 shows that the n = 1, ℓ = 0 subshell can hold at most two electrons. The n = 2, ℓ = 1 subshell, however, can hold six electrons because with ℓ = 1, there are three possibilities for mℓ (−1, 0, and +1), and for each of these choices, the value of ms can be +
1
2 or − 1
2. In general, mℓ can have the values 0, ±1, ±2, . . . , ±ℓ, for 2ℓ + 1 possibilities. Since each of these can be combined with two possibilities for ms, the total number of diff erent combinations for mℓ and ms is 2(2ℓ + 1). This, then, is the maximum number of electrons the ℓth subshell can hold, as Figure 30.16 summarizes.
For historical reasons, there is a widely used convention in which each subshell of an atom
is referred to by a letter rather than by the value of its orbital quantum number ℓ. For instance, an
ℓ = 0 subshell is called an s subshell. An ℓ = 1 subshell and an ℓ = 2 subshell are known as p
and d subshells, respectively. The higher values of ℓ = 3, 4, and so on, are referred to as f, g, and
so on, in alphabetical sequence, as Table 30.2 indicates. This convention of letters is used in a shorthand notation that is convenient for indicating
simultaneously the principal quantum number n, the orbital quantum number ℓ, and the number of electrons in the n, ℓ subshell. An example of this notation follows:
ℓ = 1
2p5
Number of electrons in the subshell
n = 2
= 5
With this notation, the arrangement, or confi guration, of the electrons in an atom can be specifi ed
effi ciently. For instance, in Example 8, we found that the electron confi guration for boron has two
Highest energy
Lowest energy
ℓ = 2
n = 5
n = 4
n = 3
n = 2
n = 1
ℓ = 0
ℓ = 1
ℓ = 2
ℓ = 0
ℓ = 1
ℓ = 0
ℓ = 1
ℓ = 0
ℓ = 0
Subshell
Maximum number of electrons
in subshell
10
2
6
10
2
6
2
6
2
2
FIGURE 30.16 The maximum number of electrons that the ℓth subshell can hold is
2(2ℓ + 1).
868 CHAPTER 30 The Nature of the Atom
electrons in the n = 1, ℓ = 0 subshell, two in the n = 2, ℓ = 0 subshell, and one in the n = 2, ℓ = 1 subshell. In shorthand notation this arrangement is expressed as 1s2 2s2 2p1. Table 30.3 gives the ground-state electron confi gurations written in this fashion for elements containing up to thirteen
electrons. The fi rst fi ve entries are those worked out in Example 8.
Each entry in the periodic table of the elements often includes the ground-state electronic
confi guration, as Interactive Figure 30.17 illustrates for argon. To save space, only the confi gura- tion of the outermost electrons and unfi lled subshells is specifi ed, using the shorthand notation just
discussed. Originally the periodic table was developed by the Russian chemist Dmitri Mendeleev
(1834–1907) on the basis that certain groups of elements exhibit similar chemical properties. There
are eight of these groups, plus the transition elements in the middle of the table, which include
the lanthanide series and the actinide series. The similar chemical properties within a group can
be explained on the basis of the confi gurations of the outer electrons of the elements in the group.
Thus, quantum mechanics and the Pauli exclusion principle off er an explanation for the chemical
behavior of the atoms. The full periodic table can be found on the inside of the back cover.
Check Your Understanding
(The answers are given at the end of the book.) 8. Using the convention of letters to refer to the orbital quantum number, write down the ground-state
confi guration of the electrons in krypton (Z = 36). 9. Can a 5g subshell contain (a) 22 electrons? (b) 17 electrons? 10. An electronic confi guration for manganese (Z = 25) is written as 1s2 2s2 2p6 3s2 3p6 4s2 3d4 4p1. Does this
confi guration represent (a) the ground state or (b) an excited state?
30.7 X-Rays THE PHYSICS OF . . . X-rays. X-rays were discovered by the Dutch physicist Wilhelm K. Roentgen (1845–1923), who performed much of his work in Germany. X-rays can be produced
when electrons, accelerated through a large potential diff erence, collide with a metal target made,
for example, from molybdenum or platinum. The target is contained within an evacuated glass
tube, as Interactive Figure 30.18 shows. Example 9 discusses the relationship between the wavelength of the emitted X-rays and the speed of the impinging electrons.
Ar
39.948 18
3p6
Symbol for argon
Configuration of outermost electrons
Atomic number
Atomic mass
INTERACTIVE FIGURE 30.17 The entries in the periodic table of the elements often
include the ground-state confi guration of the
outermost electrons.
TABLE 30.2
The Convention of Letters Used to Refer to the Orbital Quantum Number
Orbital Quantum Number ℓ Letter
0 s
1 p
2 d
3 f
4 g
5 h
TABLE 30.3 Ground-State Electronic Configurations of Atoms
Element Number of Element Configuration of the Electrons Hydrogen (H) 1 1s1
Helium (He) 2 1s2
Lithium (Li) 3 1s2 2s1
Beryllium (Be) 4 1s2 2s2
Boron (B) 5 1s2 2s2 2p1
Carbon (C) 6 1s2 2s2 2p2
Nitrogen (N) 7 1s2 2s2 2p3
Oxygen (O) 8 1s2 2s2 2p4
Fluorine (F) 9 1s2 2s2 2p5
Neon (Ne) 10 1s2 2s2 2p6
Sodium (Na) 11 1s2 2s2 2p6 3s1
Magnesium (Mg) 12 1s2 2s2 2p6 3s2
Aluminum (Al) 13 1s2 2s2 2p6 3s2 3p1
INTERACTIVE FIGURE 30.18 In an X-ray tube, electrons are emitted by a heated
fi lament, accelerate through a large potential
diff erence V, and strike a metal target. The X-rays originate when the electrons interact
with the target.
Filament voltage
V
+
–
High- voltage source
Metal target
X-rays
Heated filament
Electrons
30.7 X-Rays 869
Analyzing Multiple-Concept Problems
EXAMPLE 9 X-Rays and Electrons
The highest-energy X-rays produced by an X-ray tube have a wavelength
of 1.20 × 10−10 m. What is the speed of the electrons in Interactive Figure 30.18 just before they strike the metal target? Ignore the eff ects of relativity.
Reasoning We can fi nd the electron’s speed from a knowledge of its kinetic energy, since the two are related. Moreover, it is the electron’s
kinetic energy that determines the energy of any photon. The energy of
any photon, on the other hand, is directly proportional to its frequency,
as discussed in Section 29.3. But we know from our study of waves (see
Section 16.2) that the frequency of a wave is inversely proportional to
its wavelength. Thus, we will be able to fi nd the speed of an impinging
electron from the given X-ray wavelength.
Knowns and Unknowns The following table summarizes what we know and what we seek:
Description Symbol Value Wavelength of highest-energy X-ray photon 𝜆 1.20 × 10−10 m
Unknown Variable Speed of electron just before it strikes target 𝜐 ?
Modeling the Problem
STEP 1 Kinetic Energy The kinetic energy of an electron is the energy it has because of its motion. Since we are ignoring the eff ects of relativity, the kinetic energy KE is given by Equation
6.2 as KE = 12mυ2, where m and 𝜐 are the electron’s mass and speed. Solving this expression for the speed gives Equation 1 at the right. The mass of the electron is known but its kinetic energy
is not, so this will be evaluated in Steps 2 and 3.
STEP 2 Energy of a Photon An X-ray photon is a discrete packet of electromagnetic-wave energy. The photon’s energy E is given by E = hf, where h is Planck’s constant and f is the pho- ton’s frequency (see Equation 29.2). The energy needed to produce an X-ray photon comes from
the kinetic energy of an electron striking the target. We know that the photons have the highest
possible energy. This means that all of an electron’s kinetic energy KE goes into producing a
photon, so KE = E. Substituting KE = E into E = hf gives KE = hf (2)
This result for the energy of the photon can be substituted into Equation 1, as indicated at the right.
The frequency is not known, but Step 3 discusses how it can be obtained from the given wavelength.
STEP 3 Relation Between Frequency and Wavelength Electromagnetic waves such as X-rays travel at the speed c of light in a vacuum. According to Equation 16.1, this speed is related to the frequency f and the wavelength 𝜆 by c = f 𝜆. Solving for the frequency gives
f = c λ
All the variables on the right side of this equation are known, so we substitute it into Equation 2
for the kinetic energy, as shown in the right column.
Solution Algebraically combining the results of the three steps, we have
υ = √2(KE)m = √ 2(hf)
m = √2h (
c λ)
m = √2hcmλ
The speed of an electron just before it strikes the metal target is
υ = √2hcmλ = √ 2(6.63 × 10−34 J · s)(3.00 × 108 m/s) (9.11 × 10−34 kg)(1.20 × 10−10 m)
= 6.03 × 107 m/s
Related Homework: Problem 44
STEP 2STEP 1 STEP 3
υ = √2(KE)m (1) ?
υ = √2(KE)m (1) KE = hf (2)
?
υ = √2(KE)m (1) KE = hf (2)
f = c λ
870 CHAPTER 30 The Nature of the Atom
A plot of X-ray intensity per unit wavelength versus the wavelength looks similar to
Figure 30.19 and consists of sharp peaks or lines superimposed on a broad continuous spectrum. The sharp peaks are called characteristic lines or characteristic X-rays because they are charac- teristic of the target material. The broad continuous spectrum is referred to as Bremsstrahlung (German for “braking radiation”) and is emitted when the electrons decelerate or “brake” upon
hitting the target.
In Figure 30.19 the characteristic lines are marked K𝛼 and K𝛽 because they involve the n = 1 or K shell of a metal atom. If an electron with enough energy strikes the target, one of the K-shell
electrons can be knocked out. An electron in one of the outer shells can then fall into the K shell,
and an X-ray photon is emitted in the process. The K𝛼 line arises when an electron in the n = 2 level falls into the vacancy that the impinging electron has created in the n = 1 level. Similarly, the K𝛽 line arises when an electron in the n = 3 level falls to the n = 1 level. Example 10 shows that a large potential diff erence is needed to operate an X-ray tube so that the electrons impinging
on the metal target will have suffi cient energy to generate the characteristic X-rays. Example 11
determines an estimate for the K𝛼 wavelength of platinum.
FIGURE 30.19 When a molybdenum target is bombarded with electrons that have been
accelerated from rest through a potential
diff erence of 45 000 V, this X-ray spectrum is
produced. The vertical axis is not to scale.
X- ra
y in
te ns
it y
pe r
un it
w av
el en
gt h
Bremsstrahlung
Characteristic lines
Kα
Kβ
λ0
0.02 0.04 0.06 0.08 0.10
Wavelength, nm
EXAMPLE 10 Operating an X-Ray Tube
Strictly speaking, the Bohr model does not apply to multiple-electron atoms,
but it can be used to make estimates. Use the Bohr model to estimate the
minimum energy that an incoming electron must have to knock a K-shell
electron entirely out of an atom in a platinum (Z = 78) target in an X-ray tube.
Reasoning According to the Bohr model, the energy of a K-shell elec- tron is given by Equation 30.13, En = −(13.6 eV) Z 2/n2, with n = 1. When striking a platinum target, an incoming electron must have at least enough
energy to raise the K-shell electron from this low energy level up to the
0-eV level that corresponds to a very large distance from the nucleus.
Only then will the incoming electron knock the K-shell electron entirely
out of a target atom.
Problem-Solving Insight Equation 30.13 for the Bohr energy levels [En = −(13.6 eV)Z2/n2, n = 1] can be used in rough cal- culations of the energy levels involved in the production of K𝞪 X-rays. In this equation, however, the atomic number Z must be reduced by one, to account approximately for the shielding of one K-shell electron by the other K-shell electron.
Solution We will use Equation 30.13 to estimate the minimum energy that an incoming electron must have. However, strictly speaking, this
equation applies only to one-electron atoms, because it neglects the repul-
sive force between electrons in a multiple-electron atom. In the platinum
K-shell, each electron exerts on the other electron a repulsive force that
balances (approximately) the attractive force of one nuclear proton. In
eff ect, one of the K-shell electrons shields the other from the force of that
proton. Therefore, in our calculation we replace Z in Equation 30.13 by Z − 1 and fi nd that
E1 = −(13.6 eV) (Z − 1)2
n2 = −(13.6 eV)
(78 − 1)2
12 = −8.1 × 104 eV
Hence, to raise the K-shell electron up to the 0-eV level, the minimum
energy for an incoming electron is 8.1 × 104 eV . One electron volt is the
kinetic energy acquired when an electron accelerates from rest through
a potential diff erence of one volt. Thus, a potential diff erence of at least
81 000 V must be applied to the X-ray tube.
EXAMPLE 11 The K𝛼 Characteristic X-Ray for Platinum
Use the Bohr model to estimate the wavelength of the K𝛼 line in the X-ray spectrum of platinum (Z = 78).
Reasoning This example is very similar to Example 4, which deals with the emission line spectrum of the hydrogen atom. As in that example, we
use Equation 30.14, this time with the initial value of n being ni = 2 and the fi nal value being nf = 1. As in Example 10, a value of 77 rather than 78 is used for Z to account approximately for the shielding eff ect of the single K-shell electron in canceling out the attraction of one nuclear proton.
Solution Using Equation 30.14, we fi nd that
1
λ = (1.097 × 107 m−1)(78 − 1)2 ( 112 −
1
22) = 4.9 × 1010 m−1
or λ = 2.0 × 10−11 m
This answer is close to an experimental value of 1.9 × 10−11 m.
Another interesting feature of the X-ray spectrum in Figure 30.19 is the sharp cutoff that occurs at a wavelength of 𝜆0 on the short-wavelength side of the Bremsstrahlung. This cutoff wavelength is independent of the target material but depends on the energy of the impinging
electrons. An impinging electron cannot give up any more than all of its kinetic energy when
30.7 X-Rays 871
decelerated by the metal target in an X-ray tube. Thus, at most, an emitted X-ray photon can
have an energy equal to the kinetic energy KE of the electron and a frequency given by Equation
29.2 as f = (KE)/h, where h is Planck’s constant. But the kinetic energy acquired by an electron (charge magnitude = e) in accelerating from rest through a potential diff erence V is e times V, according to earlier discussions in Section 19.2; V is the potential diff erence applied across the X-ray tube (see Interactive Figure 30.18). Thus, the maximum photon frequency is f0 = (eV)/h. Since f0 = c/𝜆0, a maximum frequency corresponds to a minimum wavelength, which is the cutoff wavelength 𝜆0:
λ0 = hc eV
(30.17)
Figure 30.19, for instance, assumes a potential diff erence of 45 000 V, which corresponds to a cutoff wavelength of
λ0 = (6.63 × 10−34 J · s)(3.00 × 108 m /s)
(1.60 × 10−9 C)(45 000 V) = 2.8 × 10−11 m
The medical profession began using X-rays for diagnostic purposes almost immediately after
their discovery. When a conventional X-ray is obtained, the patient is typically positioned in front
of a piece of photographic fi lm, and a single burst of radiation is directed through the patient
and onto the fi lm. Since the dense structure of bone absorbs X-rays much more than soft tissue
does, a shadow-like picture is recorded on the fi lm. As useful as such pictures are, they have an
inherent limitation. The image on the fi lm is a superposition of all the “shadows” that result as
the radiation passes through one layer of body material after another. Interpreting which part of a
conventional X-ray corresponds to which layer of body material is very diffi cult.
BIO THE PHYSICS OF . . . CAT scanning. The technique known as CAT scanning, or CT scanning, has greatly extended the ability of X-rays to provide images of specifi c locations
within the body. The acronym CAT stands for computerized axial tomography or computer- assisted tomography, and the shorter version CT stands for computerized tomography. In this technique a series of X-ray images are obtained as indicated in Figure 30.20. A number of X-ray beams form a “fanned out” array of radiation and pass simultaneously through the patient. Each
of the beams is detected on the other side by a detector, which records the beam intensity. The
various intensities are diff erent, depending on the nature of the body material through which the
beams have passed. The feature of CAT scanning that leads to dramatic improvements over the
conventional technique is that the X-ray source can be rotated to diff erent orientations, so that the
fanned-out array of beams can be sent through the patient from various directions. Figure 30.20a singles out two directions for illustration. In reality many diff erent orientations are used, and the
intensity of each beam in the array is recorded as a function of orientation. The way in which the
intensity of a beam changes from one orientation to another is used as input to a computer. The
computer then constructs a highly resolved image of the cross-sectional slice of body material
through which the fan of radiation has passed. In eff ect, the CAT scanning technique makes it
possible to take an X-ray picture of a cross-sectional “slice” that is perpendicular to the body’s
FIGURE 30.20 (a) In CAT scanning, a “fanned-out” array of X-ray beams is sent through the patient from diff erent orientations. (b) A doctor and a nurse prepare a patient for a CAT scan.
(a) (b)
X-ray source
Detectors
H an
k M
o rg
an /S
ci en
ce S
o u rc
e
872 CHAPTER 30 The Nature of the Atom
FIGURE 30.21 (a) A 3D CAT scan of a human heart. The inferior vena cava and
right atrium are purple. The right ventricle
and pulmonary outfl ow tract are blue. The
pulmonary veins are yellow. The left ven-
tricle is orange, and the aorta is red. (b) A 3D CAT scan of an abdomen in frontal view.
Near the top of the image the large mass is the
liver (green), and beneath it the two smaller
teardrop-shaped objects (green/yellow) are
the kidneys. L
iv in
g A
rt E
n te
rp ri
se s/
S ci
en ce
S o u rc
e (a)
A n to
in e
R o ss
et /S
ci en
ce S
o u rc
e
(b)
long axis. In fact, the word “axial” in the phrase “computerized axial tomography” refers to the
body’s long axis. The chapter-opening photograph and Figure 30.21 show three-dimensional CAT scans of parts of the human anatomy.
Check Your Understanding
(The answers are given at the end of the book.) 11. X-ray tube A and X-ray tube B use the same voltage to accelerate the electrons. However, tube A uses
a copper target, whereas tube B uses a silver target. Which one of the following statements is true?
(a) The cutoff wavelength is greater for tube A. (b) The cutoff wavelength is greater for tube B. (c) Both tubes have the same cutoff wavelengths.
12. Is it possible to adjust the electric potential V used to operate an X-ray tube so that Bremsstrahlung X-rays are created, but characteristic X-rays are not created? (a) Yes, if V is small enough. (b) Yes, if V is large enough. (c) No, regardless of the value of V.
13. Which one of the following statements is true? (a) The K𝛼 wavelength can be smaller than the cutoff wavelength 𝜆0, assuming that both are produced by the same X-ray tube. (b) The K𝛼 wavelength is pro- duced when an electron undergoes a transition from the n = 1 energy level to the n = 2 energy level. (c) The K𝛽 wavelength is always smaller than the K𝛼 wavelength for a given metal target.
30.8 The Laser THE PHYSICS OF . . . the laser. The laser is one of the most useful inventions of the twentieth century. Today, there are many types of lasers, and most of them work in a way that depends
directly on the quantum mechanical structure of the atom.
When an electron makes a transition from a higher energy state to a lower energy state, a
photon is emitted. The emission process can be one of two types, spontaneous or stimulated.
In spontaneous emission (see Figure 30.22a), the photon is emitted spontaneously, in a ran- dom direction, without external provocation. In stimulated emission (see Figure 30.22b), an incoming photon induces, or stimulates, the electron to change energy levels. To produce
stimulated emission, however, the incoming photon must have an energy that exactly matches
the diff erence between the energies of the two levels—namely, Ei − Ef. Stimulated emission is similar to a resonant process, in which the incoming photon “jiggles” the electron at just the
frequency to which it is particularly sensitive and causes the change between energy levels.
This frequency is given by Equation 30.4 as f = (Ei − Ef)/h. The operation of lasers depends on stimulated emission.
Ei (Larger energy)
Ef (Smaller energy)
(a) Spontaneous emission
Photon
Ei
Ef
(b) Stimulated emission
Photon
Photon
Incident photon
FIGURE 30.22 (a) Spontaneous emission of a photon occurs when the electron (⦁) makes
an unprovoked transition from a higher to a
lower energy level, the photon departing in
a random direction. (b) Stimulated emission of a photon occurs when an incoming photon
with the correct energy induces an electron
to change energy levels, the emitted photon
traveling in the same direction as the incoming
photon.
30.8 The Laser 873
Stimulated emission has three important features. First, one photon goes in and two
photons come out (see Figure 30.22b). In this sense, the process amplifi es the number of photons. In fact, this is the origin of the word “laser,” which is an acronym for light ampli- fi cation by the stimulated emission of radiation. Second, the emitted photon travels in the same direction as the incoming photon. Third, the emitted photon is exactly in step with or
has the same phase as the incoming photon. In other words, the two electromagnetic waves
that these two photons represent are coherent (see Section 17.2) and are locked in step with
one another. In contrast, two photons emitted by the fi lament of an incandescent light bulb
are emitted independently. They are not coherent, since one does not stimulate the emission
of the other.
Although stimulated emission plays a pivotal role in a laser, other factors are also important.
For instance, an external source of energy must be available to excite electrons into higher
energy levels. The energy can be provided in a number of ways, including intense fl ashes of
ordinary light and high-voltage discharges. If suffi cient energy is delivered to the atoms, more
electrons will be excited to a higher energy level than remain in a lower level, a condition known
as a population inversion. Figure 30.23 compares a normal energy level population with a population inversion. The population inversions used in lasers involve a higher energy state that
is metastable, in the sense that electrons remain in the metastable state for a much longer period of time than they do in an ordinary excited state (10−3 s versus 10−8 s, for example). The require-
ment of a metastable higher energy state is essential, so that there is more time to enhance the
population inversion.
Figure 30.24 shows the widely used helium/neon laser. To sustain the necessary popula- tion inversion, a high voltage is discharged across a low-pressure mixture of 15% helium and
85% neon contained in a glass tube. The laser process begins when an atom, via spontaneous
emission, emits a photon parallel to the axis of the tube. This photon, via stimulated emis-
sion, causes another atom to emit two photons parallel to the tube axis. These two photons, in
turn, stimulate two more atoms, yielding four photons. Four yield eight, and so on, in a kind
of avalanche. To ensure that more and more photons are created by stimulated emission, both
ends of the tube are silvered to form mirrors that refl ect the photons back and forth through the
helium/neon mixture. One end is only partially silvered, however, so that some of the photons
can escape from the tube to form the laser beam. When the stimulated emission involves only
a single pair of energy levels, the output beam has a single frequency or wavelength and is said
to be monochromatic.
A laser beam is also exceptionally narrow. The width is determined by the size of the
opening through which the beam exits, and very little spreading-out occurs, except that due to
Ei (Larger energy)
Ef (Smaller energy)
Ei
Ef
(a) Normal population
(b) Population inversion
FIGURE 30.23 (a) In a normal situation at room temperature, most of the electrons in
atoms are found in a lower or ground-state
energy level. (b) If an external energy source is provided to excite electrons into a higher
energy level, a population inversion can be
created in which more electrons are in the
higher level than in the lower level.
High voltage
Completely silvered mirror
Partially silvered mirror
FIGURE 30.24 A schematic drawing of a helium/neon laser. The blow-up shows the stimulated emission that occurs when an electron in a neon atom
is induced to change from a higher to a lower energy level.
874 CHAPTER 30 The Nature of the Atom
diff raction around the edges of the opening. A laser beam does not spread much because any
photons emitted at an angle with respect to the tube axis are quickly refl ected out the sides of
the tube by the silvered ends (see Figure 30.24). These ends are carefully arranged to be perpen- dicular to the tube axis. Since all the power in a laser beam can be confi ned to a narrow region,
the intensity, or power per unit area, can be quite large.
Figure 30.25 shows the pertinent energy levels for a helium/neon laser. By coincidence, helium and neon have nearly identical metastable higher energy states, respectively located 20.61
and 20.66 eV above the ground state. The high-voltage discharge across the gaseous mixture
excites electrons in helium atoms to the 20.61-eV state. Then, when an excited helium atom col-
lides inelastically with a neon atom, the 20.61 eV of energy is given to an electron in the neon
atom, along with 0.05 eV of kinetic energy from the moving atoms. As a result, the electron in
the neon atom is raised to the 20.66-eV state. In this fashion, a population inversion is sustained
in the neon, relative to an energy level that is 18.70 eV above the ground state. In producing the
laser beam, stimulated emission causes electrons in neon to drop from the 20.66-eV level to the
18.70-eV level. The energy change of 1.96 eV corresponds to a wavelength of 633 nm, which is
in the red region of the visible spectrum.
The helium/neon laser is not the only kind of laser. There are many diff erent types, including
the ruby laser, the argon-ion laser, the carbon dioxide laser, the gallium arsenide solid-state laser,
and chemical dye lasers. Depending on the type and whether the laser operates continuously or
in pulses, the available beam power ranges from milliwatts to megawatts. Since lasers provide
coherent monochromatic electromagnetic radiation that can be confi ned to an intense narrow
beam, they are useful in a wide variety of situations. Today they are used to reproduce music in
compact disc players, to weld parts of automobile frames together, to transmit telephone conver-
sations and other forms of communication over long distances, to study molecular structure, and
to measure distances accurately.
THE PHYSICS OF . . . a laser altimeter. Figure 30.26 shows an impressive example of how a laser can be used to measure distances accurately. The photograph in the fi gure is a
three-dimensional map of the Martian topography that was obtained by the Mars Orbiter Laser
Altimeter (MOLA) on the Mars Global Surveyor spacecraft. The map was constructed from
27 million height measurements, each made by sending laser pulses to the Martian surface and
measuring their return times. The large Hellas Planitia impact basin (dark blue) is at the lower left and is 1800 km wide. At the upper right edge of the image is Elysium Mons (red, surrounded by a small band of yellow), a large volcano.
Many other uses have been found since the laser was invented in 1960, and the next section
discusses some of them in the fi eld of medicine.
Check Your Understanding
(The answers are given at the end of the book.) 14. A certain laser is designed to operate continuously. Which one of the following statements is false?
(a) The population inversion used in this laser involves a higher energy state and a lower energy state. (b) The population inversion used in this laser involves a metastable higher energy state. (c) The laser needs an external source of energy to operate. (d) The external energy source that the laser uses can be disconnected once the population inversion is established.
15. Laser A produces green light. Laser B produces red light. Which laser utilizes energy levels that have a larger energy diff erence between them? (a) Laser A (b) Laser B (c) The energy diff erence between the levels is the same for both lasers.
30.9 *Medical Applications of the Laser One of the medical areas in which the laser has had a substantial impact is in ophthalmology,
which deals with the structure, function, and diseases of the eye. Section 26.10 discusses the
human eye and the use of contact lenses and eyeglasses to correct nearsightedness and farsight-
edness. In these conditions, the eye cannot refract light properly and produces blurred images on
the retina.
Metastable
Ground state
20.61 eV 20.66 eV
18.70 eV
Helium Neon
Photon
FIGURE 30.25 These energy levels are involved in the operation of a helium/neon
laser.
NASA/Science Source
FIGURE 30.26 A 3D map of the topography of Mars. The elevation is color-coded from
white (highest) through red, yellow, green,
blue, and purple (lowest).
30.9 Medical Applications of the Laser 875
BIO THE PHYSICS OF . . . PRK eye surgery. A laser-based procedure known as PRK (photorefractive keratectomy) off ers an alternative treatment for nearsightedness and farsighted- ness that does not rely on lenses. It involves the use of a laser to remove small amounts of tissue
from the cornea of the eye (see Figure 26.33) and thereby change its curvature. As Section 26.10 points out, light enters the eye through the cornea, and it is at the air/cornea boundary that most of
the refraction of the light occurs. Therefore, changing the curvature of that boundary can correct
defi ciencies in the way the eye refracts light, thus causing the image to be focused onto the retina,
where it belongs. Ideally, the cornea is dome-shaped. If the dome is too steep, however, the rays
of light are focused in front of the retina and nearsightedness results. As Figure 30.27a shows, the laser light removes tissue from the center of the cornea, thereby fl attening it and increasing
the eye’s eff ective focal length. On the other hand, if the shape of the cornea is too fl at, light rays
would come to a focus behind the retina if they could, and farsightedness occurs. As part b of the drawing illustrates, the center of the cornea is now masked and the laser is used to remove
peripheral tissue. This steepens the shape of the cornea, thereby shortening the eye’s eff ective
focal length and allowing rays to be focused on the retina.
BIO THE PHYSICS OF . . . LASIK eye surgery. The LASIK (laser-assisted in situ keratomileusis) procedure uses a motor-powered blade known as a microkeratome to partially detach a thin fl ap (about 0.2 mm thick) in the front of the cornea (see Figure 30.28). The fl ap is pulled back and the laser beam then remodels the corneal tissue underneath by vaporizing cells.
Afterward, the fl ap is folded back into place, with no stitches being required. The laser light in the
PRK and LASIK techniques is pulsed and comes from an ultraviolet excimer laser that produces
a wavelength of 193 nm. The cornea absorbs this wavelength extremely well, so that weak pulses
can be used, leading to highly precise and controllable removal of corneal tissue. Typically, 0.1
to 0.5 𝜇m of tissue is removed by each pulse without damaging adjacent layers. BIO THE PHYSICS OF . . . removing port-wine stains. Another medical application
of the laser is in the treatment of congenital capillary malformations known as port-wine stains,
which aff ect 0.3% of children at birth. These birthmarks are usually found on the head and neck.
Preferred treatment for port-wine stains now utilizes a pulsed dye laser, as shown in Figure 30.29. The light is absorbed by oxyhemoglobin in the malformed capillaries, which are destroyed in the process without damage to adjacent normal tissue. Eventually the destroyed capillaries are
replaced by normal blood vessels, which causes the port-wine stain to fade.
BIO THE PHYSICS OF . . . photodynamic therapy for cancer. In the treatment of cancer, the laser is being used along with light-activated drugs in photodynamic therapy. The
procedure involves administering the drug intravenously, so that the tumor can absorb it from the
bloodstream, the advantage being that the drug is then located right near the cancer cells. When
the drug is activated by laser light, a chemical reaction ensues that disintegrates the cancer cells
and the small blood vessels that feed them. In Figure 30.30 a patient is being treated for cancer
Laser pulses
(a) (b)
Laser pulses
Mask
Removed material
Removed material
Removed material
FIGURE 30.27 (a) To correct for myopia (nearsightedness) using the PRK procedure,
a laser vaporizes tissue (dashed line) on the
center of the cornea, thereby fl attening it.
(b) To correct for hyperopia (farsightedness), a laser vaporizes tissue on the peripheral
region of the cornea, thereby steepening its
contour.
Laser pulses
Cornea Flap
Removed material
FIGURE 30.28 To correct for myopia (nearsightedness) using the LASIK technique,
a laser vaporizes tissue (dashed line) on the
cornea, thereby fl attening it.
FIGURE 30.29 A patient receives treatment from a pulsed dye laser. This
medical application is eff ective at removing
skin abnormalities, such as port-wine stains
and rosacea.
P h il
ip p e
G ar
o /S
ci en
ce S
o u rc
e
FIGURE 30.30 Photodynamic therapy to treat cancer of the esophagus is being administered to this patient. Red
laser light is routed to the tumor site with an endoscope
that incorporates optical fi bers.
F ri
tz H
o ff
m an
n /T
h e
Im ag
e W
o rk
s
876 CHAPTER 30 The Nature of the Atom
of the esophagus. An endoscope that uses optical fi bers is inserted down the patient’s throat to
guide the red laser light to the tumor site and activate the drug. Photodynamic therapy works best
with small tumors in their early stages.
30.10 *Holography THE PHYSICS OF . . . holography. One of the most familiar applications of lasers is in holography, which is a process for producing three-dimensional images. The information used
to produce a holographic image is captured on photographic fi lm, which is referred to as a
hologram. Figure 30.31 illustrates how a hologram is made. Laser light strikes a half-silvered mirror, or beamsplitter, which refl ects part and transmits part of the light. In the drawing, the
refl ected part is called the object beam because it illuminates the object (a chess piece). The transmitted part is called the reference beam. The object beam refl ects from the chess piece at points such as A and B and, together with the reference beam, falls on the fi lm. One of the main characteristics of laser light is that it is coherent. Thus, the light from the two beams has
a stable phase relationship, like the light from the two slits in Young’s double-slit experiment
(see Section 27.2). Because of the stable phase relationship and because the two beams travel
diff erent distances, an interference pattern is formed on the fi lm. This pattern is the hologram
and, although much more complex, is analogous to the pattern of bright and dark fringes formed
in the double-slit experiment.
Figure 30.32 shows in greater detail how a holographic interference pattern arises. This drawing considers only the reference beam and the light (wavelength = 𝜆) coming from point A on the chess piece. As we know from Section 27.1, constructive interference between the two light waves leads to a bright fringe; it occurs when the waves, in reaching the fi lm, travel
distances that diff er by an integer number m of wavelengths. In the drawing, ℓm is the distance between point A and the place on the fi lm where the mth-order bright fringe occurs, and ℓ0 is the perpendicular distance that the reference beam would travel from point A to the m = 0 bright fringe. In addition, rm is the distance along the fi lm that locates the bright fringe. In terms of these distances, we know that
ℓm − ℓ0 = mλ (condition for constructive interference)
ℓ 20 + r 2m = ℓ 2m (Pythagorean theorem)
The fi rst equation indicates that ℓm = m𝜆 + ℓ0, which can be substituted into the second equation. The result can be rearranged to show that
r 2m = mλ(mλ + 2ℓ0)
Film
Laser light
Beamsplitter Reference beam
Object beam
A
B Top view
FIGURE 30.31 An arrangement used to produce a hologram.
Film
Reference beam
A
Object beam
0 90°
m mr
Bright fringe, m
Bright fringe, m + 1
ℓ
ℓ
FIGURE 30.32 This drawing helps to explain how the interference pattern arises
on the fi lm when light from point A (see Figure 30.30) and light from the reference beam combine there.
30.10 Holography 877
Since ℓ0 is typically much larger than 𝜆 (for instance, ℓ0 ≈ 10−1 m and 𝜆 ≈ 10−6 m), it follows that rm ≈ √mλ2ℓ0. In other words, rm is roughly proportional to √m. Therefore, the fringes are farther apart near the top of the fi lm than they are near the bottom. For example, for the m = 1 and m = 2 fringes, we have r2 − r1 ∝ √2 − √1 = 0.41, whereas for the m = 2 and m = 3 fringes, we have r3 − r2 ∝ √3 − √2 = 0.32.
In addition to the fringe pattern just discussed, the total interference pattern on the hologram
includes interference eff ects that are related to light coming from point B and other locations on the object in Figure 30.31. The total pattern is very complicated. Nevertheless, the fringe pattern for point A alone is suffi cient to illustrate the fact that a hologram can be used to produce both a virtual image and a real image of the object, as we will now see.
To produce the holographic images, the laser light is directed through the interference pattern
on the fi lm, as in Figure 30.33. The pattern can be thought of as a kind of diff raction grating, with the bright fringes analogous to the spaces between the slits of the grating. Section 27.7 discusses
how light passing through a grating is split into higher-order bright fringes that are symmetrically
located on either side of a central bright fringe. Figure 30.33 shows the three rays that correspond to the central and fi rst-order bright fringes, as they originate from a spot near the top and a spot
near the bottom of the fi lm. The angle 𝜃, which locates the fi rst-order fringes relative to the central fringe, is given by Equation 27.7 (with m = 1) as sin 𝜃 = 𝜆/d, where d is the separation between the slits of the grating. When the slit separation is greater, as it is near the top of the fi lm, the angle
is smaller. When the slit separation is smaller, as it is near the bottom, the angle is larger. Thus,
Figure 30.33 has been drawn with 𝜃TOP smaller than 𝜃BOTTOM. Of the three rays emerging from the fi lm at the top and the three at the bottom, we use the uppermost one in each case to locate the
real image of point A on the chess piece. The real image is located where these two rays intersect, when extended to the right. To locate the virtual image, we use the lower ray in each of the three-
ray bundles at the top and bottom of the fi lm. When projected to the left, these rays appear to be
originating from the spot where the projections intersect—that is, from the virtual image.
A holographic image diff ers greatly from a photographic image. The most obvious diff erence is
that a hologram provides a three-dimensional image, whereas photographs are two-dimensional.
The three-dimensional nature of the holographic image is inherent in the interference pattern
formed on the fi lm. In Figure 30.31 part of this pattern arises because the light emitted by point A travels diff erent distances in reaching diff erent spots on the fi lm than does the light in the refer- ence beam. The same can be said about the light emitted from point B and other places as well. As a result, the total interference pattern contains information about how much farther from the
fi lm the various points on the object are, and because of this information holographic images are
Film (hologram)
Real image
Virtual image
Laser light
Laser light
Narrower fringe
spacing
TOP
TOP
BOTTOM
BOTTOM
Wider fringe
spacing
θ
θ
θ
θ
FIGURE 30.32 When the laser light used to produce a hologram is shone through it, both a real and a virtual image of the object are produced.
878 CHAPTER 30 The Nature of the Atom
three-dimensional. Furthermore, it is possible to “walk around” a holographic image and view it
from diff erent angles, as you would the original object.
A vast diff erence exists between the methods used to produce holograms and photographs.
As Section 26.7 discusses, a camera uses a converging lens to produce a photograph. The lens
focuses the light rays originating from a point on the object to a corresponding point on the fi lm.
To produce a hologram, lenses are not used in this way, and a point on the object does not cor- respond to a single point on the fi lm. In Figure 30.32, light from point A diverges on its way to the fi lm, and there is no lens to make it converge to a single corresponding point. The light falls
over the entire exposed region of the fi lm and contributes everywhere to the interference pattern
that is formed. Thus, a hologram may be cut into smaller pieces, and each piece will contain some
information about the light originating from point A. For this reason, each smaller piece can be used to produce a three-dimensional image of the object. In contrast, it is not possible to recon-
struct the entire image in a photograph from only a small piece of the original fi lm.
The holograms discussed here are typically viewed with the aid of the laser light used to
produce them. There are also other kinds of holograms. Credit cards, for example, use holograms
for identifi cation purposes, as shown in Figure 30.34. This kind of hologram is called a rainbow hologram and is designed to be viewed in white light that is refl ected from it. Other applications
of holography include head-up displays for instrument panels in high-performance fi ghter planes,
laser scanners at checkout counters, computerized data storage and retrieval systems, and methods
for high-precision biomedical measurements.
GIPhotoStock/Science Source
FIGURE 30.34 A hologram of a dove on a Visa credit card. When illuminated in white
light, the hologram appears to change colors
when viewed from diff erent angles.
EXAMPLE 12 BIO The Physics of Laser Lithotripsy
Solid masses are sometimes produced in the kidneys, known as kidney
stones, and if they are too large, they can become stuck in the ureter,
which is the tube leading from the kidney to the bladder. This condition
can be extremely painful, and it is often corrected with a medical treat-
ment known as lithotripsy, which is designed to break up the stone, so that
it can pass naturally through the urine. One kind of lithotripsy involves
the use of a laser, where a fi ber optic is inserted into the body near the
stone and delivers intense laser pulses to pulverize it. The type of laser
often used in this technique is a holmium YAG laser, which is a solid
state laser that uses a crystal of yttrium aluminum garnet (YAG), where
a small fraction of the yttrium atoms in the crystal have been replaced by
holmium atoms. The laser produces infrared light with a wavelength of
2.10 μm and operates with a frequency of 5 Hz, which means it delivers 5 pulses of light to the stone each second. If the energy delivered in each
pulse is 0.5 J, how many photons of laser light strike the kidney stone in
one second? Round your answer to the nearest whole number.
Reasoning Since we are given the wavelength of the laser light, we can use Equation 29.2 to calculate the energy of an individual photon in the
beam. The number of photons striking the stone will be given by the total
energy delivered divided by the energy per photon.
Solution (a) From Equation 29.2, we have:
Ephoton = hf = hc λ
.
The total energy delivered in one second will be equal to the number of
pulses in one second multiplied by the energy per pulse:
Etot = ( pulses
sec )( energy
pulse ). The number of photons (N) is then given by:
N = Etot
Ephoton =
( pulses
sec )( energy
pulse ) hc/λ
= (5)(0.5 J)(2.10 × 10−6 m)
(6.63 × 10−34 J · s)(3.00 × 108 m/s)
= 3 × 1019 photons
Concept Summary 30.1 Rutherford Scattering and the Nuclear Atom The idea of a nuclear atom originated in 1911 as a result of experiments by Ernest Rutherford in
which 𝛼 particles were scattered by a thin metal foil. The phrase “nuclear atom” refers to the fact that an atom consists of a small, positively charged
nucleus surrounded at relatively large distances by a number of electrons,
whose total negative charge equals the positive nuclear charge when the atom
is electrically neutral.
30.2 Line Spectra A line spectrum is a series of discrete electromag- netic wavelengths emitted by the atoms of a low-pressure gas that is sub-
jected to a suffi ciently high potential diff erence. Certain groups of discrete
wavelengths are referred to as “series.” The following equations can be
used to determine the wavelengths in three of the series that are found in
the line spectrum of atomic hydrogen:
Lyman series 1
λ = R ( 112 −
1
n2) n = 2, 3, 4, . . . (30.1) Balmer series
1
λ = R ( 122 −
1
n2) n = 3, 4, 5, . . . (30.2)
Paschen series 1
λ = R ( 132 −
1
n2) n = 4, 5, 6, . . . (30.3)
Focus on Concepts 879
The constant term R is called the Rydberg constant and has the value R = 1.097 × 107 m−1.
30.3 The Bohr Model of the Hydrogen Atom The Bohr model applies to atoms or ions that have only a single electron orbiting a nucleus contain-
ing Z protons. This model assumes that the electron exists in circular orbits that are called stationary orbits because the electron does not radiate electro-
magnetic waves while in them. According to this model, a photon is emitted
only when an electron changes from an orbit with a higher energy Ei to an orbit with a lower energy Ef. The orbital energies and the photon frequency f are related according to Equation 30.4, where h is Planck’s constant. The model also assumes that the magnitude Ln of the orbital angular momentum of the electron can only have the discrete values indicated in Equation
30.8. With these assumptions, it can be shown that the nth Bohr orbit has a radius rn and is associated with a total energy En, as given in Equations 30.10 and 30.13.
Ei − Ef = hf (30.4)
Ln = n h
2π n = 1, 2, 3, . . . (30.8)
rn = (5.29 × 10−11 m) n2
Z n = 1, 2, 3, . . . (30.10)
En = −(13.6 eV) Z 2
n2 n = 1, 2, 3, . . . (30.13)
The ionization energy is the minimum energy needed to remove an elec-
tron completely from an atom. The Bohr model predicts that the wavelengths
comprising the line spectrum emitted by a hydrogen atom can be calculated
according to Equation 30.14.
1
λ = RZ 2 ( 1n 2f −
1
n 2i ) (30.14) n i, nf = 1, 2, 3, . . . and ni > nf
30.4 De Broglie’s Explanation of Bohr’s Assumption About Angular Momentum Louis de Broglie proposed that the electron in a circular Bohr orbit should be considered as a particle wave and that standing particle waves
around the orbit off er an explanation of the angular momentum assumption
in the Bohr model.
30.5 The Quantum Mechanical Picture of the Hydrogen Atom Quantum mechanics describes the hydrogen atom in terms of the following four
quantum numbers:
(1) The principal quantum number n, which can have the integer values n = 1, 2, 3, . . .
(2) The orbital quantum number ℓ, which can have the integer values ℓ = 0, 1, 2, . . . , (n − 1)
(3) The magnetic quantum number mℓ, which can have the positive and negative values mℓ = −ℓ, . . . , −2, −1, 0, +1, +2, . . . , +ℓ
(4) The spin quantum number ms, which, for an electron, can be either ms = +
1
2 or ms = − 1
2
According to quantum mechanics, an electron does not reside in a circular
orbit but, rather, has some probability of being found at various distances
from the nucleus.
30.6 The Pauli Exclusion Principle and the Periodic Table of the Elements The Pauli exclusion principle states that no two electrons in an atom can
have the same set of values for the four quantum numbers n, ℓ, mℓ, and ms. This principle determines the way in which the electrons in multiple- electron atoms are distributed into shells (defi ned by the value of n) and subshells (defi ned by the value of ℓ).
The following notation is used to refer to the orbital quantum numbers:
s denotes ℓ = 0, p denotes ℓ = 1, d denotes ℓ = 2, f denotes ℓ = 3, g denotes
ℓ = 4, h denotes ℓ = 5, and so on.
The arrangement of the periodic table of the elements is related to the
Pauli exclusion principle.
30.7 X-Rays X-rays are electromagnetic waves emitted when high-energy electrons strike a metal target contained within an evacuated glass tube. The
emitted X-ray spectrum of wavelengths consists of sharp “peaks” or “lines,”
called characteristic X-rays, superimposed on a broad continuous range of
wavelengths called Bremsstrahlung. The K𝛼 characteristic X-ray is emitted when an electron in the n = 2 level (L shell) drops into a vacancy in the n = 1 level (K shell). Similarly, the K𝛽 characteristic X-ray is emitted when an electron in the n = 3 level (M shell) drops into a vacancy in the n = 1 level (K shell). The minimum wavelength, or cutoff wavelength 𝜆0, of the Bremsstrahlung is determined by the kinetic energy of the electrons striking
the target in the X-ray tube, according to Equation 30.17, where h is Planck’s constant, c is the speed of light in a vacuum, e is the magnitude of the charge on an electron, and V is the potential diff erence applied across the X-ray tube.
λ0 = hc eV
(30.8)
30.8 The Laser/30.9 Medical Applications of the Laser A laser is a device that generates electromagnetic waves via a process known as stim-
ulated emission. In this process, one photon stimulates the production of
another photon by causing an electron in an atom to fall from a higher energy
level to a lower energy level. The emitted photon travels in the same direction
as the photon causing the stimulation. Because of this mechanism of photon
production, the electromagnetic waves generated by a laser are coherent and
may be confi ned to a very narrow beam. Stimulated emission contrasts with
the process known as spontaneous emission, in which an electron in an atom
also falls from a higher to a lower energy level, but does so spontaneously, in
a random direction, without any external provocation.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 30.3 The Bohr Model of the Hydrogen Atom 1. Consider applying the Bohr model to a neutral helium atom (Z = 2). The model takes into account a number of factors. Which one of the following
does it not take into account? (a) The quantization of the orbital angular momentum of an electron (b) The centripetal acceleration of an electron
(c) The electric potential energy of an electron (d) The electrostatic repulsion between electrons (e) The electrostatic attraction between the nucleus and an electron
3. According to the Bohr model, what determines the shortest wavelength in a given series of wavelengths emitted by the atom? (a) The quantum number ni that identifi es the higher energy level from which the electron falls into a lower energy level (b) The quantum number nf that identifi es the lower energy level into which the electron falls from a higher energy level (c) The ratio nf /ni, where nf is the quantum number that identifi es the lower energy level into which the electron falls and ni is the quantum number that identifi es
Focus on Concepts
880 CHAPTER 30 The Nature of the Atom
the higher level from which the electron falls (d) The sum nf + ni of two quantum numbers, where nf identifi es the lower energy level into which the electron falls and ni identifi es the higher level from which the electron falls (e) The diff erence nf − ni of two quantum numbers, where nf identifi es the lower energy level into which the electron falls and ni identifi es the higher level from which the electron falls
Section 30.5 The Quantum Mechanical Picture of the Hydrogen Atom 6. According to quantum mechanics, only one of the following combinations of the principal quantum number n and the orbital quantum number ℓ is pos- sible for the electron in a hydrogen atom. Which combination is it? (a) n = 3, ℓ = 3 (b) n = 2, ℓ = 3 (c) n = 1, ℓ = 2 (d) n = 0, ℓ = 0 (e) n = 3, ℓ = 1 8. Which one of the following statements is false? (a) The orbits in the Bohr model have precise sizes, whereas in the quantum mechanical picture of the
hydrogen atom they do not. (b) In the absence of external magnetic fi elds, both the Bohr model and quantum mechanics predict the same total energy
for the electron in the hydrogen atom. (c) The spin angular momentum of the electron plays a role in both the Bohr model and the quantum mechanical
picture of the hydrogen atom. (d) The magnitude of the orbital angular mo- mentum cannot be zero in the Bohr model, but it can be zero in the quantum
mechanical picture of the hydrogen atom.
Section 30.6 The Pauli Exclusion Principle and the Periodic Table of the Elements 10. Each of the following answers indicates the quantum mechanical states of two electrons, A and B. Which pair of states could not describe two of the electrons in a multiple-electron atom?
(a) n ℓ mℓ ms A 4 1 +1 −
1
2
B 3 1 +1 − 1
2
(b) n ℓ mℓ ms A 3 2 −1 −
1
2
B 3 1 −1 + 1
2
(c) n ℓ mℓ ms A 2 0 0 −
1
2
B 2 1 +1 + 1
2
(d) n ℓ mℓ ms A 5 3 +1 −
1
2
B 4 1 0 + 1
2
(e) n ℓ mℓ ms A 3 2 −2 +
1
2
B 3 2 −2 + 1
2
11. Consider the 5f and 6h subshells in a multiple-electron atom. Which of these subshells can contain 19 electrons? (a) Only the 6h subshell (b) Only the 5f subshell (c) Both subshells (d) Neither subshell
Section 30.7 X-Rays 14. Silver (Z = 47), copper (Z = 29), and platinum (Z = 78) can be used as the target in an X-ray tube. Rank in descending order (largest fi rst) the ener-
gies needed for impinging electrons to knock a K-shell electron completely
out of an atom in each of these targets. (a) Silver, copper, platinum (b) Silver, platinum, copper (c) Platinum, silver, copper (d) Platinum, copper, silver (e) Copper, silver, platinum 16. The voltage applied across an X-ray tube is doubled. What happens to the cutoff wavelength in the spectrum of wavelengths emitted by the tube’s
metal target? (a) It also doubles. (b) It decreases by a factor of two. (c) It increases by a factor of four. (d) It decreases by a factor of four. (e) Nothing happens to it.
Section 30.8 The Laser 17. Consider two energy levels that characterize the atoms of a material used in a laser. A population inversion between these two levels
__________. (a) has the lower energy level more populated than it nor- mally is and the higher energy level less populated than it normally is
(b) is the same thing as a metastable state (c) requires no external source of energy to be sustained (d) has the higher energy level more populated than it normally is and the lower energy level less populated than it normally is
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
Note: In working these problems, ignore relativistic eff ects.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 30.1 Rutherford Scattering and the Nuclear Atom 1. E SSM The nucleus of the hydrogen atom has a radius of about 1 × 10−15 m. The electron is normally at a distance of about 5.3 × 10−11 m from
the nucleus. Assuming that the hydrogen atom is a sphere with a radius of 5.3 ×
10−11 m, fi nd (a) the volume of the atom, (b) the volume of the nucleus, and (c) the percentage of the volume of the atom that is occupied by the nucleus. 2. E The nucleus of a hydrogen atom is a single proton, which has a radius of about 1.0 × 10−15 m. The single electron in a hydrogen atom normally
orbits the nucleus at a distance of 5.3 × 10−11 m. What is the ratio of the density
of the hydrogen nucleus to the density of the complete hydrogen atom?
3. E Review Conceptual Example 1 and use the information therein as an aid in working this problem. Suppose that you’re building a scale model of
the hydrogen atom, and the nucleus is represented by a ball that has a radius
of 3.2 cm (somewhat smaller than a baseball). How many miles away (1 mi =
1.61 × 105 cm) should the electron be placed?
4. E V-HINT In a Rutherford scattering experiment a target nucleus has a diameter of 1.4 × 10−14 m. The incoming 𝛼 particle has a mass of 6.64 × 10−27 kg. What is the kinetic energy of an 𝛼 particle that has a de Broglie wavelength equal to the diameter of the target nucleus? Ignore relativistic
eff ects.
Problems
Problems 881
5. M CHALK SSM There are Z protons in the nucleus of an atom, where Z is the atomic number of the element. An 𝛼 particle carries a charge of +2e. In a scattering experiment, an 𝛼 particle, heading directly toward a nucleus in a metal foil, will come to a halt when all the particle’s kinetic energy is
converted to electric potential energy. In such a situation, how close will
an 𝛼 particle with a kinetic energy of 5.0 × 10−13 J come to a gold nucleus (Z = 79)? 6. M GO The nucleus of a copper atom contains 29 protons and has a radius of 4.8 × 10−15 m. How much work (in electron volts) is done by the electric
force as a proton is brought from infi nity, where it is at rest, to the “surface”
of a copper nucleus?
Section 30.2 Line Spectra,
Section 30.3 The Bohr Model of the Hydrogen Atom 7. E SSM For a doubly ionized lithium atom Li2+ (Z = 3), what is the prin- cipal quantum number of the state in which the electron has the same total
energy as a ground-state electron has in the hydrogen atom?
8. E A singly ionized helium atom (He+) has only one electron in orbit about the nucleus. What is the radius of the ion when it is in the second
excited state?
9. E Using the Bohr model, determine the ratio of the energy of the nth orbit of a triply ionized beryllium atom (Be3+, Z = 4) to the energy of the nth orbit of a hydrogen atom (H).
10. E MMH The electron in a hydrogen atom is in the fi rst excited state, when the electron acquires an additional 2.86 eV of energy. What is the
quantum number n of the state into which the electron moves?
11. E SSM Find the energy (in joules) of the photon that is emitted when the electron in a hydrogen atom undergoes a transition from the n = 7 energy level to produce a line in the Paschen series.
12. E GO (a) What is the ionization energy of a hydrogen atom that is in the n = 4 excited state? (b) For a hydrogen atom, determine the ratio of the ionization energy for the n = 4 excited state to the ionization energy for the ground state.
13. E CHALK A hydrogen atom is in the ground state. It absorbs energy and makes a transition to the n = 3 excited state. The atom returns to the ground state by emitting two photons. What are their wavelengths?
14. E In the hydrogen atom, what is the total energy (in electron volts) of an electron that is in an orbit that has a radius of 4.761 × 10−10 m?
15. E Available in WileyPLUS. 16. M GO A sodium atom (Z = 11) contains 11 protons in its nucleus. Strictly speaking, the Bohr model does not apply, because the neutral atom
contains 11 electrons instead of a single electron. However, we can apply the
model to the outermost electron as an approximation, provided that we use
an eff ective value Zeff ective rather than 11 for the number of protons in the nuc- leus. (a) The ionization energy for the outermost electron in a sodium atom is 5.1 eV. Use the Bohr model with Z = Zeff ective to calculate a value for Zeff ective. (b) Using Z = 11 and Z = Zeff ective, determine the corresponding two values for the radius of the outermost Bohr orbit.
17. M GO SSM A wavelength of 410.2 nm is emitted by the hydrogen atoms in a high-voltage discharge tube. What are the initial and fi nal values
of the quantum number n for the energy level transition that produces this wavelength?
18. M V-HINT MMH A hydrogen atom emits a photon that has momentum with a magnitude of 5.452 × 10−27 kg · m/s. This photon is emitted because the electron in the atom falls from a higher energy level into the n = 1 level. What is the quantum number of the level from which the electron falls? Use
a value of 6.626 × 10−34 J · s for Planck’s constant.
19. E SSM For atomic hydrogen, the Paschen series of lines occurs when nf = 3, whereas the Brackett series occurs when nf = 4 in Equation 30.14. Using this equation, show that the ranges of wavelengths in these two series
overlap.
20. M GO Doubly ionized lithium Li2+ (Z = 3) and triply ionized beryllium Be3+ (Z = 4) each emit a line spectrum. For a certain series of lines in the lithium spectrum, the shortest wavelength is 40.5 nm. For the same series of
lines in the beryllium spectrum, what is the shortest wavelength?
21. H Available in WileyPLUS. 22. H In the Bohr model of hydrogen, the electron moves in a circular orbit around the nucleus. Determine the angular speed of the electron, in revolu-
tions per second, when it is in (a) the ground state and (b) the fi rst excited state.
Section 30.5 The Quantum Mechanical Picture of the Hydrogen Atom 23. E A hydrogen atom is in its second excited state. Determine, accord- ing to quantum mechanics, (a) the total energy (in eV) of the atom, (b) the magnitude of the maximum angular momentum the electron can have in this
state, and (c) the maximum value that the z component Lz of the angular momentum can have.
24. E GO The table lists quantum numbers for fi ve states of the hydrogen atom. Which (if any) of them are not possible? For those that are not possible,
explain why.
Process n ℓ mℓ (a) 3 3 0
(b) 2 1 −1
(c) 4 2 3
(d) 5 −3 2
(e) 4 0 0
25. E The orbital quantum number for the electron in a hydrogen atom is ℓ = 5. What is the smallest possible value (the most negative) for the total
energy of this electron? Give your answer in electron volts.
26. E GO It is known that the possible values for the magnetic quantum number mℓ are −4, −3, −2, −1, 0, +1, +2, +3, and +4. Determine the orbital quantum number ℓ and the smallest possible value of the principal quantum
number n.
27. E SSM The maximum value for the magnetic quantum number in state A is mℓ = 2, while in state B it is mℓ = 1. What is the ratio LA/LB of the magnitudes of the orbital angular momenta of an electron in these two
states?
28. M V-HINT The electron in a certain hydrogen atom has an angular momentum of 8.948 × 10−34 J · s. What is the largest possible magnitude for the z component of the angular momentum of this electron? For accuracy, use h = 6.626 × 10−34 J · s. 29. M SSM MMH For an electron in a hydrogen atom, the z component of the angular momentum has a maximum value of Lz = 4.22 × 10−34 J · s. Find the three smallest possible values (the most negative) for the total energy (in
electron volts) that this atom could have.
30. H GO An electron is in the n = 5 state. What is the smallest possible value for the angle between the z component of the orbital angular mo- mentum and the orbital angular momentum?
882 CHAPTER 30 The Nature of the Atom
Section 30.6 The Pauli Exclusion Principle and the Periodic Table of the Elements 31. E Two of the three electrons in a lithium atom have quantum numbers of n = 1, ℓ = 0, mℓ = 0, ms = +
1
2 and n = 1, ℓ = 0, mℓ = 0, ms = − 1
2. What
quantum numbers can the third electron have if the atom is in (a) its ground state and (b) its fi rst excited state? 32. E Following the style used in Table 30.3, determine the electronic con- fi guration of the ground state for yttrium Y (Z = 39). Refer to Figure 30.16 to see the order in which the subshells fi ll.
33. E Figure 30.16 was constructed using the Pauli exclusion principle and indicates that the n = 1 shell holds 2 electrons, the n = 2 shell holds 8 elec- trons, and the n = 3 shell holds 18 electrons. These numbers can be obtained by adding the numbers given in the fi gure for the subshells contained within
a given shell. How many electrons can be put into the n = 5 shell, which is only partly shown in the fi gure?
34. E GO Which of the following subshell confi gurations are not allowed? For those that are not allowed, give the reason why. (a) 3s1 (b) 2d2 (c) 3s4 (d) 4p8 (e) 5f12
35. E SSM When an electron makes a transition between energy levels of an atom, there are no restrictions on the initial and fi nal values of the principal
quantum number n. According to quantum mechanics, however, there is a rule that restricts the initial and fi nal values of the orbital quantum number ℓ.
This rule is called a selection rule and states that Δℓ = ±1. In other words, when an electron makes a transition between energy levels, the value of ℓ can
only increase or decrease by one. The value of ℓ may not remain the same nor
may it increase or decrease by more than one. According to this rule, which
of the following energy level transitions are allowed? (a) 2s → 1s (b) 2p → 1s (c) 4p → 2p (d) 4s → 2p (e) 3d → 3s 36. M In the ground state, the outermost shell (n = 1) of helium (He) is fi lled with electrons, as is the outermost shell (n = 2) of neon (Ne). The full outermost shells of these two elements distinguish them as the fi rst two so-
called “noble gases.” Suppose that the spin quantum number ms had three possible values, rather than two. If that were the case, which elements would
be (a) the fi rst and (b) the second noble gases? Assume that the possible values for the other three quantum numbers are unchanged, and that the Pauli
exclusion principle still applies.
Section 30.7 X-Rays 37. E MMH By using the Bohr model, decide which element is likely to emit a K𝛼 X-ray with a wavelength of 4.5 × 10−9 m.
38. E GO What is the minimum potential diff erence that must be applied to an X-ray tube to knock a K-shell electron completely out of an atom in a
copper (Z = 29) target? Use the Bohr model as needed.
39. E MMH Available in WileyPLUS. 40. E V-HINT In the X-ray spectrum of niobium (Z = 41), a K𝛼 peak is ob- served at a wavelength of 7.462 × 10−11 m. (a) Determine the magnitude of the diff erence between the observed wavelength of the K𝛼 X-ray for niobium and that predicted by the Bohr model. (b) Express the magnitude of this dif- ference as a percentage of the observed wavelength.
41. E CHALK SSM When a certain element is bombarded with high-energy electrons, K𝛼 X-rays that have an energy of 9890 eV are emitted. Determine the atomic number Z of the element, and identify the element. Use the Bohr model as necessary.
42. M GO The Bohr model, although not strictly applicable, can be used to estimate the minimum energy Emin that an incoming electron must have in an X-ray tube in order to knock a K-shell electron entirely out of an atom
in the metal target. The K𝛼 X-ray wavelength of metal A is 2.0 times the K𝛼 X-ray wavelength of metal B. What is the ratio of Emin, A for metal A to Emin, B for metal B?
43. M SSM An X-ray tube contains a silver (Z = 47) target. The high voltage in this tube is increased from zero. Using the Bohr model, fi nd the value of
the voltage at which the K𝛼 X-ray just appears in the X-ray spectrum.
44. M GO Multiple-Concept Example 9 reviews the concepts that are impor- tant in this problem. An electron, traveling at a speed of 6.00 × 107 m/s,
strikes the target of an X-ray tube. Upon impact, the electron decelerates to
one-quarter of its original speed, an X-ray photon being emitted in the pro-
cess. What is the wavelength of the photon?
Section 30.8 The Laser 45. E BIO SSM A laser is used in eye surgery to weld a detached retina back into place. The wavelength of the laser beam is 514 nm, and the power
is 1.5 W. During surgery, the laser beam is turned on for 0.050 s. During this
time, how many photons are emitted by the laser?
46. E BIO GO The ultraviolet excimer laser used in the PRK technique (see Section 30.9) has a wavelength of 193 nm. A carbon dioxide laser produces a
wavelength of 1.06 × 10−5 m. What is the minimum number of photons that
the carbon dioxide laser must produce to deliver at least as much or more
energy to a target as does a single photon from the excimer laser?
47. E GO A pulsed laser emits light in a series of short pulses, each hav- ing a duration of 25.0 ms. The average power of each pulse is 5.00 mW,
and the wavelength of the light is 633 nm. Find the number of photons in
each pulse.
48. E GO The drawing shows three energy levels of a laser that are involved in the lasing action. These levels are analogous to the levels in the Ne atoms
of a He-Ne laser. The E2 level is a metastable level, and the E0 level is the ground state. The diff erence between the energy levels of the laser is shown
in the drawing. (a) What energy (in eV per electron) must an external source provide to start the lasing action? (b) What is the wavelength of the laser light? (c) In what region of the electromagnetic spectrum (see Figure 24.9) does the laser light lie?
PROBLEM 48
0.289 eV
0.165 eV
E2
E1
E0
⎧ ⎪ ⎥ ⎨ ⎥ ⎜ ⎩
⎧ ⎨ ⎩
49. E BIO A laser peripheral iridotomy is a procedure for treating an eye condition known as narrow-angle glaucoma, in which pressure buildup in
the eye can lead to loss of vision. A neodymium YAG laser (wavelength =
1064 nm) is used in the procedure to punch a tiny hole in the peripheral iris,
thereby relieving the pressure buildup. In one application the laser delivers
4.1 × 10−3 J of energy to the iris in creating the hole. How many photons does
the laser deliver?
50. M V-HINT Fusion is the process by which the sun produces energy. One experimental technique for creating controlled fusion utilizes a solid-state
laser that emits a wavelength of 1060 nm and can produce a power of 1.0 ×
1014 W for a pulse duration of 1.1 × 10−11 s. In contrast, the helium/neon laser
used in a bar-code scanner at the checkout counter emits a wavelength of
633 nm and produces a power of about 1.0 × 10−3 W. How long (in days)
would the helium/neon laser have to operate to produce the same number of
photons that the solid-state laser produces in 1.1 × 10−11 s?
Team Problems 883
51. E Available in WileyPLUS. 52. E GO (a) What is the minimum energy (in electron volts) that is required to remove the electron from the ground state of a singly ionized helium atom
(He+, Z = 2)? (b) What is the ionization energy for He+? 53. E Available in WileyPLUS. 54. E Molybdenum has an atomic number of Z = 42. Using the Bohr model, estimate the wavelength of the K𝛼 X-ray. 55. E SSM In the line spectrum of atomic hydrogen there is also a group of lines known as the Pfund series. These lines are produced when electrons,
excited to high energy levels, make transitions to the n = 5 level. Determine (a) the longest wavelength and (b) the shortest wavelength in this series. (c) Refer to Figure 24.9 and identify the region of the electromagnetic spec- trum in which these lines are found.
56. E GO The voltage across an X-ray tube is 35.0 kV. Suppose that the molybdenum (Z = 42) target in the X-ray tube is replaced by a silver (Z = 47) target. Determine (a) the tube’s cutoff wavelength and (b) the wavelengths of the K𝛼 X-ray photons emitted by the molybdenum and silver targets. 57. M Available in WileyPLUS. 58 M V-HINT The energy of the n = 2 Bohr orbit is −30.6 eV for an unidenti- fi ed ionized atom in which only one electron moves about the nucleus. What
is the radius of the n = 5 orbit for this species? 59. M SSM Available in WileyPLUS.
60. M Consider a particle of mass m that can exist only between x = 0 m and x = +L on the x axis. We could say that this particle is confi ned to a “box” of length L. In this situation, imagine the standing de Broglie waves that can fi t into the box. For example, the drawing shows the fi rst three possibilities.
Note in this picture that there are either one, two, or three half-wavelengths
that fi t into the distance L. Use Equation 29.8 for the de Broglie wavelength of a particle and derive an expression for the allowed energies (only kinetic
energy) that the particle can have. This expression involves m, L, Planck’s constant, and a quantum number n that can have only the values 1, 2, 3, . . . .
PROBLEM 60 L
61. H SSM Available in WileyPLUS.
Additional Problems
The Bohr model of the hydrogen atom introduces a number of important fea-
tures that characterize the quantum picture of atomic structure. Among them
are the concepts of quantized energy levels and the photon emission that
occurs when an electron makes a transition from a higher to a lower energy
state. Problem 62 deals with these ideas. Problem 63 reviews the physics of
how a K𝛼 X-ray is produced, how its energy is related to the ionization ener- gies of the target atom, and how to determine the minimum voltage needed
to produce it in an X-ray tube.
62. M CHALK A hydrogen atom (Z = 1) is in the third excited state, and a photon is either emitted or absorbed. Concepts: (i) What is the quantum num- ber of the third excited state? (ii) When an atom emits a photon, is the fi nal
quantum number nf of the atom greater than or less than the initial quantum number ni? (iii) When an atom absorbs a photon, is the fi nal quantum num- ber nf of the atom greater than or less than the initial quantum number ni?
(iv) How is the wavelength of a photon related to its energy? Calculations: Determine the quantum number nf of the fi nal state and the energy of the photon when the photon is (a) emitted with the shortest possible wavelength, (b) emitted with the longest possible wavelength, and (c) absorbed with the longest possible wavelength.
63. M CHALK SSM The K-shell and L-shell ionization energies of a metal are 8979 eV and 951 eV, respectively. Concepts: (i) How is a K𝛼 photon produced, and how much energy does it have? (ii) What must be the minimum voltage
across the X-ray tube to produce a K𝛼 photon? (iii) What is meant by the phrases “K-shell ionization energy” and “L-shell ionization energy”? (iv) What does
the diff erence between the K-shell and L-shell ionization energies represent?
Calculations: (a) Assuming that there is a vacancy in the L shell, what must be the minimum voltage across an X-ray tube with a target made from this metal
to produce K𝛼 X-ray photons? (b) Determine the wavelength of a K𝛼 photon.
Concepts and Calculations Problems
64. M A Simple Spectrometer. In the Balmer series for the atomic emis- sion of hydrogen, emission lines with n going from 3 → 2, 4 → 2, 5 → 2, and 6 → 2 are in the visible spectrum. (a) What are the wavelengths of the light emitted in these transitions? (b) A spectrometer is a device that disperses light into its constituent wavelengths, and provides a means of measuring
these wavelengths. You and your team are designing a simple spectrometer
using a transmission grating with 1500 lines/cm. A collimated beam of light
from a hydrogen discharge tube (which emits light from all possible hydro-
gen atomic transitions) passes through the grating. At what second-order
angles (m = 2) do you expect each of the emission lines calculated in (a) to
Team Problems
884 CHAPTER 30 The Nature of the Atom
appear? (c) You place a screen with a coating that fl uoresces when exposed to ultraviolet light in the light emerging from the grating, and you observe
another line at 𝜃 = 6.84°. Calculate the wavelength of this light. Does it come from the Balmer series?
65. M An X-ray Source. You and your team are building an X-ray source for a diff raction instrument used to study the crystalline structure of ma-
terials. You decide to use the K𝛼 radiation from a copper (Z = 29) target. (a) Estimate the minimum energy that an incoming electron must have in
order to knock a K-shell electron out of the Cu atom. (b) Through what voltage must you accelerate the electrons? (c) What is the cutoff wavelength of the Bremsstrahlung radiation for the electron energy found in (a)?
(d) What is the wavelength of the K𝛼 line? Convert this to the energy of the K𝛼 X-ray photons (in eV) (e) If a fi rst-order peak (m = 1) appears at an angle of 17.0° when the K𝛼 radiation found in (d) passes through a hypothetical diff raction grating, what would be the “line spacing” of the grating? Note:
distances between atoms in solids are on the order of 10−10 .m
885
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
31.1 Identify and explain the properties of the nucleus.
31.2 Describe the strong nuclear force.
31.3 Calculate nuclear binding energy and mass defect.
31.4 Analyze alpha, beta, and gamma decays.
31.5 Explain the role of the neutrino in weak nuclear decay.
31.6 Solve problems involving radioactive decay.
31.7 Calculate age using radioactive dating.
31.8 Analyze radioactive decay series.
31.9 Explain how radiation detectors operate. ©
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ks iy
M ak
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CHAPTER 31
Nuclear Physics and Radioactivity
This horned dinosaur (Chasmosaurus belli) lived 76 million years ago in North America during the Cretaceous period. A fully grown adult had a length of about 5–6 meters and a weight of about 8000 pounds. It was a plant eater. Paleontologists sometimes use the disintegration of radioactive nuclei to date such fossils, a method that this chapter discusses.
31.1 Nuclear Structure Atoms consist of electrons in orbit about a central nucleus. As we have seen in Chapter 30, the electron orbits are quantum mechanical in nature and have interesting characteristics. Little has been said about the nucleus, however. Since the nucleus is interesting in its own right, we now consider it in greater detail.
The nucleus of an atom consists of neutrons and protons, collectively referred to as nucleons. The neutron, discovered in 1932 by the English physicist James Chadwick (1891–1974), carries no electric charge and has a mass slightly larger than that of a proton (see Table 31.1).
The number of protons in the nucleus is diff erent in diff erent elements and is given by the atomic number Z. In an electrically neutral atom, the number of nuclear protons equals the number of electrons in orbit around the nucleus. The number of neutrons in the nucleus is N.
886 CHAPTER 31 Nuclear Physics and Radioactivity
The total number of protons and neutrons is referred to as the atomic mass number A because the total nuclear mass is approximately equal to A times the mass of a single nucleon:
A = Z + N (31.1)
Sometimes A is also called the nucleon number. A shorthand notation is often used to specify Z and A along with the chemical symbol for the element. For instance, the nuclei of all naturally occurring aluminum atoms have A = 27, and the atomic number for aluminum is Z = 13. In shorthand notation, then, the aluminum nucleus is specifi ed as 2713 Al. The number of neutrons in an aluminum nucleus is not given explicitly by this shorthand notation. However, it can be determined easily with the aid of Equation 31.1, which indicates that N = A − Z = 14. In general, for an element whose chemical symbol is X, the symbol for the nucleus is
A ZX
Number of protons and neutrons
Number of protons
For a proton the symbol is 11 H, since the proton is the nucleus of a hydrogen atom. A neutron is denoted by 10 n. In the case of an electron we use −1 0 e, where A = 0 because an electron is not composed of protons or neutrons and Z = −1 because the electron has a negative charge.
Nuclei that contain the same number of protons, but a diff erent number of neutrons, are known as isotopes. Carbon, for example, occurs in nature in two stable forms. In most carbon atoms (98.90%), the nucleus is the 612 C isotope and consists of six protons and six neutrons. A small fraction (1.10%), however, contain nuclei that have six protons and seven neutrons— namely, the 613 C isotope. The percentages given here are the natural abundances of the isotopes. The atomic masses in the periodic table are average atomic masses, taking into account the abundances of the various isotopes.
The protons and neutrons in the nucleus are clustered together to form an approximately spherical region, as Interactive Figure 31.1 illustrates. Experiment shows that the radius r of the nucleus depends on the atomic mass number A and is given approximately in meters by
r ≈ (1.2 × 10−15 m) A1/3 (31.2)
This equation indicates that the radius of the aluminum nucleus (A = 27), for example, is r ≈ (1.2 × 10−15 m)271/3 = 3.6 × 10−15 m. Equation 31.2 leads to an important conclusion concerning the nuclear density of diff erent atoms, as Conceptual Example 1 discusses.
Number of protons and neutrons
(atomic mass number or nucleon number)
⏟⎵⎵⎵⎵⏟⎵⎵⎵⎵⏟
Number of protons (atomic number)
⏟⎵⎵⎵⏟⎵⎵⎵⏟
Number of neutrons
⏟⏟⏟
TABLE 31.1 Properties of Select Particles
Mass
Particle Electric Charge (C) Kilograms (kg) Atomic Mass Units (u)
Electron −1.60 × 10−19 9.109 382 × 10−31 5.485 799 × 10−4
Proton −1.60 × 10−19 1.672 622 × 10−27 1.007 276
Neutron 0 1.674 927 × 10−27 1.008 665
Hydrogen atom 0 1.673 534 × 10−27 1.007 825
r
+
+
+
+ +
+
+
+ +
+ +
+
+
+
INTERACTIVE FIGURE 31.1 The nucleus in an atom is approximately spherical (radius = r) and contains protons (+) clustered closely together with neutrons (●).
31.2 The Strong Nuclear Force and the Stability of the Nucleus 887
Check Your Understanding
(The answers are given at the end of the book.) 1. Two nuclei diff er in their numbers of protons and their numbers of neutrons. Which one or more of the
following statements is/are true? (a) They are diff erent isotopes of the same element. (b) They have the same electric charge. (c) They could have the same radii. (d) They have approximately the same nuclear density.
2. A material is known to be an isotope of lead, although the particular isotope is not known. From such limited information, which of the following quantities can you specify? (a) Its atomic number (b) Its neutron number (c) Its atomic mass number
3. Two nuclei have diff erent nucleon numbers A1 and A2. Are the two nuclei necessarily isotopes of the same element?
4. Can two nuclei have the same radius, even though they contain diff erent numbers of protons and diff erent numbers of neutrons?
31.2 The Strong Nuclear Force and the Stability of the Nucleus Two positive charges that are as close together as they are in a nucleus repel one another with a very strong electrostatic force. What, then, keeps the nucleus from fl ying apart? Clearly, some kind of attractive force must hold the nucleus together, since many kinds of naturally occurring atoms contain stable nuclei. The gravitational force of attraction between nucleons is too weak to counteract the repulsive electric force, so a diff erent type of force must hold the nucleus together. This force is the strong nuclear force and is one of only three fundamental forces that have been discovered, fundamental in the sense that all forces in nature can be explained in terms of these three. The gravitational force is also one of these forces, as is the electroweak force (see Section 31.5).
Many features of the strong nuclear force are well known. For example, it is almost independ- ent of electric charge. At a given separation distance, nearly the same nuclear force of attraction exists between two protons, between two neutrons, or between a proton and a neutron. The range
CONCEPTUAL EXAMPLE 1 Nuclear Density
It is well known that lead and oxygen contain diff erent atoms and that the density of solid lead is much greater than the density of gaseous oxygen. Using the defi nition of density along with Equation 31.2, decide whether the density of the nucleus in a lead atom is (a) greater than, (b) approxim- ately equal to, or (c) less than the density of the nucleus in an oxygen atom.
Reasoning The density ρ of an object, such as the nucleus, is defi ned as its mass M divided by its volume V: ρ = M/V (Equation 11.1). The mass of a nucleus is approximately equal to the number A of nucleons in the nucleus times the mass m of a single nucleon, since the masses of a proton and a neutron are nearly the same. Thus, we have that M ≈ Am, where A is greater for lead than for oxygen, but m is the same for both. The nucleus is approximately spherical with a radius r, so its volume V is given by V = 43 πr 3. The radius, however, depends on the number A of nucleons through the relation r ≈ (1.2 × 10−15 m)A1/3 (Equation 31.2). Therefore, we can write the density of a nucleus as follows:
ρ = M V
≈ Am
4 3πr3
= Am
4 3π [ (1.2 × 10−15 m) A1/3]3
≈ m
4 3π (1.2 × 10−15 m)3
Note that the nucleon number A has been eliminated algebraically from this result, as a direct consequence of Equation 31.2.
Answers (a) and (c) are incorrect. The result obtained in the Reason- ing section for the nuclear density ρ depends only on numerical factors and the value of m, which is the mass of a single nucleon no matter where the nucleon is located. The nuclear density does not depend on the nuclear number A. Thus, the nuclear density of lead, which is the ratio of its mass to its volume, is neither greater than nor less than the nuclear density of oxygen.
Answer (b) is correct. The result obtained in the Reasoning section for the nuclear density ρ indicates that the density of the nucleus in a lead atom is approximately the same as it is in an oxygen atom. In general, because of Equation 31.2, the nuclear density has nearly the same value in all atoms. The diff erence in densities between solid lead and gaseous oxygen, however, arises mainly because of the diff erence in how closely the atoms are packed together in the solid and gaseous phases.
Related Homework: Problem 9
888 CHAPTER 31 Nuclear Physics and Radioactivity
of action of the strong nuclear force is extremely short, with the force of attraction being very strong when two nucleons are as close as 10−15 m and essentially zero at larger distances. In con- trast, the electric force between two protons decreases to zero only gradually as the separation distance increases to large values and, therefore, has a relatively long range of action.
The limited range of action of the strong nuclear force plays an important role in the stability of the nucleus. For a nucleus to be stable, the electrostatic repulsion between the protons must be balanced by the attraction between the nucleons due to the strong nuclear force. But one proton repels all other protons within the nucleus, since the electrostatic force has such a long range of action. In contrast, a proton or a neutron attracts only its nearest neighbors via the strong nuclear force. As the number Z of protons in the nucleus increases under these conditions, the number N of neutrons has to increase even more, if stability is to be maintained. Figure 31.2 shows a plot of N versus Z for naturally occurring elements that have stable nuclei. For reference, the plot also includes the straight line that represents the condition N = Z. With few exceptions, the points representing stable nuclei fall above this reference line, refl ecting the fact that the number of neutrons becomes greater than the number of protons as the atomic number Z increases.
As more and more protons occur in a nucleus, there comes a point when a balance of re- pulsive and attractive forces cannot be achieved by an increased number of neutrons. Eventually, the limited range of action of the strong nuclear force prevents extra neutrons from balancing the long-range electric repulsion of extra protons. The stable nucleus with the largest number of protons (Z = 83) is that of bismuth, 83209 Bi, which contains 126 neutrons. All nuclei with more than 83 protons (e.g., uranium, Z = 92) are unstable and spontaneously break apart or rearrange their internal structures as time passes. This spontaneous disintegration or rearrangement of in- ternal structure is called radioactivity, fi rst discovered in 1896 by the French physicist Antoine Becquerel (1852–1908). Section 31.4 discusses radioactivity in greater detail.
31.3 The Mass Defect of the Nucleus and Nuclear Binding Energy Because of the strong nuclear force, the nucleons in a stable nucleus are held tightly together. Therefore, energy is required to separate a stable nucleus into its constituent protons and neutrons, as Interactive Figure 31.3 illustrates. The more stable the nucleus is, the greater is the amount of energy needed to break it apart. The required energy is called the binding energy of the nucleus.
Two ideas that we have studied previously come into play as we discuss the binding energy of a nucleus. These are the rest energy of an object (Section 28.6) and mass (Section 4.2). In Einstein’s theory of special relativity, energy and mass are equivalent; in fact, the rest energy E0 and the mass m are related via E0 = mc2 (Equation 28.5), where c is the speed of light in a vacuum. Therefore, a change ΔE0 in the rest energy of the system is equivalent to a change Δm in the mass of the system, according to ΔE0 = (Δm)c2. We see, then, that the binding energy used in Interactive Figure 31.3 to disassemble the nucleus appears as extra mass of the separated and stationary nucleons. In other words, the sum of the individual masses of the separated protons and neutrons is greater by an amount Δm than the mass of the stable nucleus. The diff erence in mass Δm is known as the mass defect of the nucleus.
As Example 2 shows, the binding energy of a nucleus can be determined from the mass defect according to Equation 31.3:
Binding energy = (Mass defect)c2 = (∆m)c2 (31.3)
0
140
120
100
80
60
40
20
0 20 40
Proton number Z
N eu
tr on
n um
be r N
= A
– Z
N = Z
60 80
FIGURE 31.2 With few exceptions, the naturally occurring stable nuclei have a number N of neutrons that equals or exceeds the number Z of protons. Each dot in this plot represents a stable nucleus.
Separated nucleons (greater mass)
Nucleus (smaller mass)
+ Bindingenergy+ +
+
+
+ +
INTERACTIVE FIGURE 31.3 Energy, called the binding energy, must be supplied to break the nucleus apart into its constituent protons and neutrons. Each of the separated nucleons is at rest and out of the range of the forces of the other nucleons.
EXAMPLE 2 The Binding Energy of the Helium Nucleus
The most abundant isotope of helium has a 24He nucleus whose mass is 6.6447 × 10−27 kg. For this nucleus, fi nd (a) the mass defect and (b) the binding energy.
Reasoning The symbol 24He indicates that the helium nucleus contains Z = 2 protons and N = 4 − 2 = 2 neutrons. To obtain the mass defect Δm, we fi rst determine the sum of the individual masses of the separated
31.3 The Mass Defect of the Nucleus and Nuclear Binding Energy 889
In calculations such as that in Example 2, it is customary to use the atomic mass unit (u) instead of the kilogram. As introduced in Section 14.1, the atomic mass unit is one-twelfth of the mass of a 612 C atom of carbon. In terms of this unit, the mass of a 612 C atom is exactly 12 u. Table 31.1 also gives the masses of the electron, the proton, and the neutron in atomic mass units. For future calculations, the energy equivalent of one atomic mass unit can be determined by observing that the mass of a proton is 1.6726 × 10−27 kg or 1.0073 u, so that
1u = (1 u)( 1.6726 × 10−27 kg
1.0073 u ) = 1.6605 × 10−27 kg and
∆E 0 = (∆m)c 2 = (1.6605 × 10−27 kg)(2.9979 × 108 m /s) 2 = 1.4924 × 10−10 J
In electron volts, therefore, one atomic mass unit is equivalent to
1 u = (1.4924 × 10−10 J) ( 1 eV1.6022 × 10−19 J) = 9.315 × 108 eV = 931.5 MeV Data tables for isotopes, such as the table in Appendix F, give masses in atomic mass units.
Typically, however, the given masses are not nuclear masses. They are atomic masses—that is, the masses of neutral atoms, including the mass of the orbital electrons. Example 3 deals again with the 42He nucleus and shows how to take into account the eff ect of the orbital electrons when using such data to determine binding energies.
protons and neutrons. Then we subtract from this sum the mass of the 24He nucleus. Finally, we use Equation 31.3 to calculate the binding energy from the value for Δm.
Solution (a) Using data from Table 31.1, we fi nd that the sum of the individual masses of the nucleons is
2(1.6726 × 10−27 kg) + 2(1.6749 × 10−27 kg) = 6.6950 × 10−27 kg
This value is greater than the mass of the intact 24He nucleus, and the mass defect is
∆ m = 6.6950 × 10−27 kg − 6.6447 × 10−27 kg = 0.0503 × 10−27 kg
⏟⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⏟
Two protons ⏟⎵⎵⎵⎵⎵⏟⎵⎵⎵⎵⎵⏟
Two neutrons
(b) According to Equation 31.3, the binding energy is Binding energy
= (∆m)c2 = (0.0503 × 10−27 kg)(3.00 × 108 m/s)2
= 4.53 × 10−12 J
Usually, binding energies are expressed in energy units of electron volts instead of joules (1 eV = 1.60 × 10−19 J):
Binding energy
= (4.53 × 10−12 J) ( 1 eV1.60 × 10−19 J) = 2.83 × 107 eV = 28.3 MeV In this result, one million electron volts is denoted by the unit MeV. The value of 28.3 MeV is more than two million times greater than the energy required to remove an orbital electron from an atom.
EXAMPLE 3 The Binding Energy of the Helium Nucleus, Revisited
The atomic mass of helium 42He is 4.0026 u, and the atomic mass of hy- drogen 11H is 1.0078 u. Using atomic mass units instead of kilograms, obtain the binding energy of the 42He nucleus.
Reasoning To determine the binding energy, we calculate the mass defect in atomic mass units and then use the fact that one atomic mass unit is equivalent to 931.5 MeV of energy. The mass of 4.0026 u for 42He includes the mass of the two electrons in the neutral helium atom. To calculate the mass defect, we must subtract 4.0026 u from the sum of the individual masses of the nucleons, including the mass of the electrons. As Figure 31.4 illustrates, the electron mass will be included if the masses of two hydrogen atoms are used in the calculation instead of the masses of two protons. The mass of a 11 H hydrogen atom is given in Table 31.1 as 1.0078 u, and the mass of a neutron as 1.0087 u.
Solution The sum of the individual masses is 2(1.0078 u) + 2(1.0087 u) = 4.0330 u
The mass defect is Δm = 4.0330 u − 4.0026 u = 0.0304 u. Since 1 u is equivalent to 931.5 MeV, the binding energy is
⏟⎵⏟⎵⏟
Two hydrogen atoms
⏟⎵⏟⎵⏟
Two neutrons
Binding energy = (0.0304 u)(931.5 MeV1 u ) = 28.3 MeV which matches the result obtained in Example 2.
FIGURE 31.4 Data tables usually give the mass of the neutral atom (including the orbital electrons) rather than the mass of the nucleus. When data from such tables are used to determine the mass defect of a nucleus, the mass of the orbital electrons must be taken into account, as this drawing illustrates for the 42He isotope of helium. See Example 3.
He42
H11 n 1 0
+ +Bindingenergy
Mass = 4.0026 u
+
+–
–
+
Mass = 4.0330 u
–
H11 n 1 0+
–
890 CHAPTER 31 Nuclear Physics and Radioactivity
To see how the nuclear binding energy varies from nucleus to nucleus, it is necessary to compare the binding energy for each nucleus on a per-nucleon basis. The graph in Figure 31.5 shows a plot in which the binding energy divided by the nucleon number A is plotted against the nucleon number itself. In the graph, the peak for the 42 He isotope of helium indicates that the 42 He nucleus is particularly stable. The binding energy per nucleon increases rapidly for nuclei with small masses and reaches a maximum of approximately 8.7 MeV/nucleon for a nucleon number of about A = 60. For greater nucleon numbers, the binding energy per nucleon decreases gradu- ally. Eventually, the binding energy per nucleon decreases enough so there is insuffi cient binding energy to hold the nucleus together. Nuclei more massive than the 83209 Bi nucleus of bismuth are unstable and hence radioactive.
Check Your Understanding
(The answers are given at the end of the book.) 5. Using Figure 31.5, rank the following nuclei in ascending order according to the binding energy per
nucleon (smallest fi rst): (a) Phosphorus 1531P (b) Cobalt 2759 Co (c) Tungsten 7484W (d) Thorium 90232 Th 6. The following table gives values for the mass defect Δm for four hypothetical nuclei: A, B, C, and D.
Which statement is true regarding the stability of these nuclei? (a) Nucleus D is the most stable, and nucleus A is the least stable. (b) Nucleus C is stable, whereas nuclei A, B, and D are not. (c) Nucleus A is the most stable, and nucleus D is not stable. (d) Nuclei A and B are stable, but nucleus B is more stable than nucleus A.
A B C D
Mass defect, Δm +6.0 × 10−29 kg +2.0 × 10−29 kg 0 kg −6.0 × 10−29 kg
31.4 Radioactivity When an unstable or radioactive nucleus disintegrates spontaneously, certain kinds of particles and/or high-energy photons are released. These particles and photons are collectively called “rays.” Three kinds of rays are produced by naturally occurring radioactivity: 𝞪 rays, 𝞫 rays, and 𝞬 rays. They are named according to the fi rst three letters of the Greek alphabet, alpha (α), beta (β), and gamma (𝛾), to indicate the extent of their ability to penetrate matter. α rays are the least penetrating, being blocked by a thin (≈0.01 mm) sheet of lead, whereas β rays penetrate lead to a much greater distance (≈0.1 mm). 𝛾 rays are the most penetrating and can pass through an appreciable thickness (≈100 mm) of lead.
FIGURE 31.5 A plot of binding energy per nucleon versus the nucleon number A.
0
10
8
6
B in
di ng
e ne
rg y
pe r
nu cl
eo n
(M eV
/n uc
le on
)
4
2
0 50 150 200 250
H21
H31
Li63
He42
C126
N147
O168
F199
P3115
K3919
Fe5626 As 75 33
Zr9040 Sn12050
Eu15363 Bi20983
U23892
100
Nucleon number A
31.4 Radioactivity 891
The nuclear disintegration process that produces α, β, and 𝛾 rays must obey the conservation laws of physics. These laws are called “conservation laws,” because each of them deals with a property that is conserved, in the sense that it does not change during a process. The following list shows the property with which each law deals:
1. Conservation of energy/mass (Sections 6.8 and 28.6) 2. Conservation of linear momentum (Section 7.2) 3. Conservation of angular momentum (Section 9.6) 4. Conservation of electric charge (Section 18.2) 5. Conservation of nucleon number (Section 31.4) We have studied the fi rst four of these laws in previous chapters, and to them we now add a fi fth, the conservation of nucleon number.
In all radioactive decay processes it has been observed that the number of nucleons (pro- tons plus neutrons) present before the decay is equal to the number of nucleons after the decay. Therefore, the number of nucleons is conserved during a nuclear disintegration. As ap- plied to the disintegration of a nucleus, the conservation laws require that the energy, electric charge, linear momentum, angular momentum, and nucleon number that a nucleus possesses must remain unchanged when it disintegrates into nuclear fragments and accompanying α, β, or 𝛾 rays.
The three types of radioactivity that occur naturally can be observed in a relatively simple experiment. A piece of radioactive material is placed at the bottom of a narrow hole in a lead cyl- inder. The cylinder is located within an evacuated chamber, as Interactive Figure 31.6 illustrates. A magnetic fi eld is directed perpendicular to the plane of the paper, and a photographic plate is positioned to the right of the hole. Three spots appear on the developed plate, which are associ- ated with the radioactivity of the nuclei in the material. Since moving particles are defl ected by a magnetic fi eld only when they are electrically charged, this experiment reveals that two types of radioactivity (α and β rays, as it turns out) consist of charged particles, whereas the third type (𝛾 rays) does not.
𝛼 Decay When a nucleus disintegrates and produces α rays, it is said to undergo 𝞪 decay. Experimental evidence shows that α rays consist of positively charged particles, each one being the 42He nucleus of helium. Thus, an α particle has a charge of +2e and a nucleon number of A = 4. Since the grouping of 2 protons and 2 neutrons in a 42He nucleus is particularly stable, as we have seen in connection with Figure 31.5, it is not surprising that an α particle can be ejected as a unit from a more massive unstable nucleus.
Animated Figure 31.7 shows the disintegration process for one example of α decay:
92 238 U 23490Th + 42He
Parent nucleus
(uranium)
Daughter nucleus
(thorium)
α particle (helium nucleus)
Lead cylinder
Magnetic field (into paper) Helium
nucleus
Gamma photon
Electron
Photographic plate
Radioactive material
Evacuated chamber
𝛾 𝛼
𝛽 −
+ +
INTERACTIVE FIGURE 31.6 α and β rays are defl ected by a magnetic fi eld and, therefore, consist of moving charged particles. γ rays are not defl ected by a magnetic fi eld and, consequently, must be uncharged.
U23892 Th 234
90
+ +
146
92
He42
+ + 144
90 2 2
Uranium parent
nucleus
Thorium daughter nucleus
particle (helium nucleus)
𝛼
ANIMATED FIGURE 31.7 α decay occurs when an unstable parent nucleus emits an α particle and in the process is converted into a diff erent, or daughter, nucleus.
892 CHAPTER 31 Nuclear Physics and Radioactivity
The original nucleus is referred to as the parent nucleus (P), and the nucleus remaining after disintegration is called the daughter nucleus (D). Upon emission of an α particle, the uranium 92 238 U parent is converted into the 90234 Th daughter, which is an isotope of thorium. The parent and daughter nuclei are diff erent, so α decay converts one element into another, a process known as transmutation.
Electric charge is conserved during α decay. In Animated Figure 31.7, for instance, 90 of the 92 protons in the uranium nucleus end up in the thorium nucleus, and the remaining 2 pro- tons are carried off by the α particle. The total number of 92, however, is the same before and after disintegration. α decay also conserves the number of nucleons, because the number is the same before (238) and after (234 + 4) disintegration. Consistent with the conservation of electric charge and nucleon number, the general form for α decay is
𝛼 Decay Z AP Z−2A−4 D + 24 He
Parent
nucleus Daughter nucleus
α particle (helium nucleus)
When a nucleus releases an α particle, the nucleus also releases energy. In fact, the energy released by radioactive decay is responsible, in part, for keeping the interior of the earth hot and, in some places, even molten. The following example shows how the conservation of mass/energy can be used to determine the amount of energy released in α decay.
EXAMPLE 4 𝛼 Decay and the Release of Energy
The atomic mass of uranium 238 92U is 238.0508 u, that of thorium 90234 Th is 234.0436 u, and that of an α particle 42He is 4.0026 u. Determine the energy released when α decay converts 92238 U into 90234 Th.
Reasoning Since energy is released during the decay, the combined mass of the 90234 Th daughter nucleus and the α particle is less than the mass of the 92238 U parent nucleus. The diff erence in mass is equivalent to the energy released. We will determine the diff erence in mass in atomic mass units and then use the fact that 1 u is equivalent to 931.5 MeV.
Solution The decay and the masses are shown below:
92 238 U 90234 Th + 42He
238.0508 u 234.0436 u 4.0026 u
238.0462 u
The decrease in mass, or mass defect for the decay process, is 238.0508 u − 238.0462 u = 0.0046 u. As usual, the masses are atomic masses and include the mass of the orbital electrons. But this causes no error here because the same total number of electrons is included for 92238 U, on the one hand, and for 90234 Th plus 42 He, on the other. Since 1 u is equivalent to 931.5 MeV, the released energy is
Released energy = (0.0046 u) (931.5 MeV1 u ) = 4.3 MeV
When α decay occurs as in Example 4, the energy released appears as kinetic energy of the recoiling 90234 Th nucleus and the α particle, except for a small portion carried away as a 𝛾 ray. Conceptual Example 5 discusses how the 90234 Th nucleus and the α particle share in the released energy.
CONCEPTUAL EXAMPLE 5 How Energy Is Shared During the α Decay of 23892U
Reasoning and Solution Kinetic energy depends on the mass m and speed υ of a particle, since KE = 12mυ2 (Equation 6.2). The 90234 Th nucleus has a much greater mass than the α particle, and since the kinetic energy is proportional to the mass, it is tempting to conclude that the 90234 Th nucleus has the greater kinetic energy. This conclusion is not correct,
In Example 4, the energy released by the α decay of 92238 U is found to be 4.3 MeV. Since this energy is carried away as kinetic energy of the recoiling 90234 Th nucleus and the α particle, it follows that KETh + KEα = 4.3 MeV. However, KETh and KEα are not equal. Which particle carries away more kinetic energy, the 90234 Th nucleus or the α particle?
31.4 Radioactivity 893
however, since it does not take into account the fact that the 90234 Th nuc- leus and the α particle have diff erent speeds after the decay. In fact, we expect the thorium nucleus to recoil with the smaller speed precisely because it has the greater mass. The decaying 92238 U is like a father and his young daughter on ice skates, pushing off against one another. The more massive father recoils with much less speed than the daughter. We can use the principle of conservation of linear momentum to verify our expectation.
As Section 7.2 discusses, the conservation principle states that the total linear momentum of an isolated system remains constant. An isolated system is one for which the vector sum of the external forces acting on the system is zero, and the decaying 92238 U nucleus fi ts this de- scription. It is stationary initially, and since momentum is mass times
velocity, its initial momentum is zero. In its fi nal form, the system consists of the 90234 Th nucleus and the α particle and has a fi nal total momentum of mThυTh + mαυα. According to momentum conservation, the initial and fi nal values of the total momentum of the system must be the same, so that mThυTh + mαυα = 0. Solving this equation for the velocity of the thorium nucleus, we fi nd that υTh = −mαυα/mTh. Since mTh is much greater than mα, we can see that the speed of the thorium nucleus is less than the speed of the α particle. Moreover, the kinetic energy depends on the square of the speed and only the fi rst power of the mass. As a result of its much greater speed, the α particle has the greater kinetic energy.
Related Homework: Problem 29
THE PHYSICS OF radioactivity and smoke detectors. One widely used application of α decay is in smoke detectors. Figure 31.8 illustrates how a smoke detector operates. Two small and parallel metal plates are separated by a distance of about one centimeter. A tiny amount of radioactive material at the center of one of the plates emits α particles, which collide with air molecules. During the collisions, the air molecules are ionized to form positive and negative ions. The voltage from a battery causes one plate to be positive and the other negative, so that each plate attracts ions of opposite charge. As a result there is a current in the circuit attached to the plates. The presence of smoke particles between the plates reduces the current, since the ions that collide with a smoke particle are usually neutralized. The drop in current that smoke particles cause is used to trigger an alarm.
𝛽 Decay The β rays in Interactive Figure 31.6 are defl ected by the magnetic fi eld in a direction opposite to that of the positively charged α rays. Consequently, these β rays, which are the most common kind, consist of negatively charged particles or β− particles. Experiment shows that β− particles are electrons. As an illustration of β− decay, consider the thorium 90234 Th nucleus, which decays by emitting a β− particle, as in Figure 31.9:
90 234 Th 91234 Pa + −1 0 e
Parent nucleus
(thorium)
Daughter nucleus
(protactinium)
β− particle (electron)
β− decay, like α decay, causes a transmutation of one element into another. In this case, thorium 90 234 Th is converted into protactinium 91234 Pa. The law of conservation of charge is obeyed, since the net number of positive charges is the same before (90) and after (91 − 1) the β− emission. The law of conservation of nucleon number is obeyed, since the nucleon number remains at A = 234. The general form for β− decay is
β− decay ZA P Z+1A D + 0−1 e
Parent
nucleus Daughter nucleus
β− particle (electron)
The electron emitted in β− decay does not actually exist within the parent nucleus and is not one of the orbital electrons. Instead, the electron is created when a neutron decays into a proton and an electron; when this occurs, the proton number of the parent nucleus increases from Z to Z + 1 and the nucleon number remains unchanged. The newly created electron is usually fast-moving and escapes from the atom, leaving behind a positively charged atom.
Example 6 illustrates that energy is released during β− decay, just as it is during α decay, and that the conservation of mass/energy applies.
Current
Battery
Radioactive material
particles
FIGURE 31.8 A smoke detector.
Th23490 Pa 234
91
+ +
144
90
e0–1
+ 143
91
Thorium parent
nucleus
Protactinium daughter nucleus
– particle (electron)
–
𝛽
FIGURE 31.9 β−decay occurs when a neu- tron in an unstable parent nucleus decays into a proton and an electron, the electron being emitted as the β− particle. In the process, the parent nucleus is transformed into the daughter nucleus.
894 CHAPTER 31 Nuclear Physics and Radioactivity
A second kind of β decay sometimes occurs.* In this process the particle emitted by the nucleus is a positron rather than an electron. A positron, also called a β+ particle, has the same mass as an electron but carries a charge of +e instead of −e. The disintegration process for β+ decay is
β+ decay ZA P Z−1 A D + +10 e
Parent
nucleus Daughter nucleus
β+ particle (positron)
The emitted positron does not exist within the nucleus but, rather, is created when a nuclear proton is transformed into a neutron. In the process, the proton number of the parent nucleus decreases from Z to Z − 1, and the nucleon number remains the same. As with β−decay, the laws of conservation of charge and nucleon number are obeyed, and there is a transmutation of one element into another.
𝛾 Decay The nucleus, like the orbital electrons, exists only in discrete energy states or levels. When a nucleus changes from an excited energy state (denoted by an asterisk*) to a lower energy state, a photon is emitted. The process is similar to the one discussed in Section 30.3 for the photon emission that leads to the hydrogen atom line spectrum. With nuclear energy levels, however, the photon has a much greater energy and is called a γ ray. The γ decay process is written as follows:
γ decay ZA P* ZA P + γ
Excited
energy state Lower
energy state γ ray
γ decay does not cause a transmutation of one element into another.
Medical Applications of Radioactivity BIO THE PHYSICS OF Gamma Knife radiosurgery. Gamma Knife radiosurgery is
becoming a very promising medical procedure for treating certain problems of the brain, including benign and cancerous tumors as well as blood vessel malformations. The procedure, which in- volves no knife at all, uses powerful, highly focused beams of γ rays aimed at the tumor or mal- formation. The γ rays are emitted by a radioactive cobalt-60 source. As Figure 31.10a illustrates, the patient wears a protective metal helmet that is perforated with many small holes. Part b of
EXAMPLE 6 β−Decay and the Release of Energy
When the 90234 Th nucleus of a thorium atom is converted into a 91234 Pa nucleus, the number of orbital electrons remains the same, so the res- ulting protactinium atom is missing one orbital electron. However, the given mass includes all 91 electrons of a neutral protactinium atom. In eff ect, then, the value of 234.043 30 u for 91234 Pa already includes the mass of the β− particle. The mass decrease that accompanies the β− decay is
234.043 59 u − 234.043 30 u = 0.000 29 u
Since 1 u is equivalent to 931.5 MeV, the released energy is
Released energy = (0.00029 u) (931.5 MeV1 u ) = 0.27 MeV This is the maximum kinetic energy that the emitted electron can have.
The atomic mass of thorium 90234 Th is 234.043 59 u, and the atomic mass of protactinium 91234 Pa is 234.043 30 u. Find the energy released when β− decay changes 90234 Th into 91234 Pa.
Reasoning To fi nd the energy released, we follow the usual procedure of determining how much the mass has decreased because of the decay and then calculating the equivalent energy.
Problem-Solving Insight In β−decay, be careful not to include the mass of the electron ( 0−1 e) twice. As discussed here, the atomic mass of the daughter atom ( 91234 Pa) already includes the mass of the emitted electron.
Solution The decay and the masses are shown below:
90 234 Th 91234Pa + 0−1 e
234.043 59 u 234.043 30 u
*A third kind of β decay also occurs in which a nucleus pulls in, or captures, one of the orbital electrons from outside the nucleus. The process is called electron capture, or K capture, since the electron normally comes from the innermost, or K, shell.
31.4 Radioactivity 895
the fi gure shows that the holes focus the γ rays to a single tiny target within the brain. The target tissue thus receives a very intense dose of radiation and is destroyed, while the surrounding healthy tissue is undamaged. Gamma Knife surgery is a noninvasive, painless, and bloodless pro- cedure that is often performed under local anesthesia. Hospital stays are 70 to 90% shorter than with conventional surgery, and patients often return to work within a few days.
BIO THE PHYSICS OF an exercise thallium heart scan. An exercise thallium heart scan is a test that uses radioactive thallium to produce images of the heart muscle. When combined with an exercise test, such as walking on a treadmill, the thallium scan helps identify regions of the heart that do not receive enough blood. The scan is especially useful in diagnosing the presence of blockages in the coronary arteries, which supply oxygen-rich blood to the heart muscle. During the test, a small amount of thallium is injected into a vein while the patient walks on a treadmill. The thallium attaches to the red blood cells and is carried throughout the body. The thallium enters the heart muscle by way of the coronary arteries and collects in heart-muscle cells that come into contact with the blood. The thallium isotope used, 81201Tl, emits γ rays, which a special camera records. Since the thallium reaches those regions of the heart that have an ad- equate blood supply, lesser amounts show up in areas where the blood fl ow has been reduced due to arterial blockages (see Figure 31.11). A second set of images is taken several hours later, while the patient is resting. These images help diff erentiate between regions of the heart that temporar- ily do not receive enough blood (the blood fl ow returns to normal after the exercise) and regions that are permanently damaged due to, for example, a previous heart attack (the blood fl ow does not return to normal).
BIO THE PHYSICS OF brachytherapy implants. The use of radioactive isotopes to deliver radiation to specifi c targets in the body is an important medical technique. In treating cancer, for example, the method of delivery should ideally apply a high dose of radiation to a ma- lignant tumor in order to kill it, while applying only a small (non-damaging) dose to healthy sur- rounding tissue. Brachytherapy implants off er such a delivery method. In this type of treatment, radioactive isotopes are formed into small seeds and implanted directly in the tumor according to a predesigned pattern. The energy and type of radiation emitted by the isotopes can be exploited to optimize a treatment design and minimize damage to healthy tissue. Seeds containing iridium 77 192 Ir are used to treat many cancers, and seeds containing iodine 53125 I and palladium 46103Pd are used for prostate cancer. Research has also indicated that brachytherapy implants may have an important role to play in the treatment of atherosclerosis, in which blood vessels become blocked with plaque. Such blockages are often treated using the technique of balloon angioplasty. With the aid of a catheter inserted into an occluded coronary artery, a balloon is infl ated to open the artery and place a stent (a metallic mesh that provides support for the arterial wall) at the site of the blockage. Sometimes the arterial wall is damaged in this process, and as it heals, the artery often becomes blocked again. Brachytherapy implants (using iridium 77192 Ir or phosphorus 1532 P, for instance) have been found to inhibit repeat blockages following angioplasty.
FIGURE 31.10 (a) In Gamma Knife radiosurgery, a protective metal helmet containing many small holes is placed on the patient’s head. (b) The holes focus the beams of 𝛾 rays to a tiny target within the brain.
Target
Helmet
(b)(a)
Gamma rays
FIGURE 31.11 An exercise thallium heart scan indicates regions of the heart that receive insuffi cient blood during exercise.
Insufficient blood
896 CHAPTER 31 Nuclear Physics and Radioactivity
Check Your Understanding
(The answers are given at the end of the book.) 7. Polonium
84 216 Po undergoes α decay to produce a daughter nucleus that itself undergoes β− decay. Which
one of the following nuclei is the one that ultimately results? (a) 82211 Pb (b) 81211 Tl (c) 81212 Tl (d) 83212 Bi (e) 82213 Pb
8. Uranium 92238 U decays into thorium 90234 Th by means of α decay, as Example 4 in the text discusses. Another possibility is that the 92238 U nucleus just emits a single proton instead of an α particle. This hypothetical decay scheme is shown below, along with the pertinent atomic masses:
92 238 U 91237 Pa + 11H
Uranium
238.050 78 u Protactinium 237.051 14 u
Proton 1.007 83 u
For a decay to be possible, it must bring the parent nucleus toward a more stable state by allowing the release of energy. Compare the total mass of the products of this hypothetical decay with the mass of 92 238 U and decide whether the emission of a single proton is possible for 92238 U.
31.5 The Neutrino When a β particle is emitted by a radioactive nucleus, energy is simultaneously released, as Example 6 illustrates. Experimentally, however, it is found that most β particles do not have enough kinetic energy to account for all the energy released. If a β particle carries away only part of the energy, where does the remainder go? The question puzzled physicists until 1930, when Wolfgang Pauli proposed that part of the energy is carried away by another particle that is emitted along with the β particle. This additional particle is called the neutrino, and its existence was verifi ed experimentally in 1956. The Greek letter nu (ν) is used to symbolize the neutrino. For instance, the β− decay of thorium 90234 Th (see Section 31.4) is more correctly written as
90 234 Th 91234 Pa + −10 e + ν
The bar above the ν is included because the neutrino emitted in this particular decay process is an antimatter neutrino, or antineutrino. A normal neutrino (ν without the bar) is emitted when β+ decay occurs.
The emission of neutrinos and β particles involves a force called the weak nuclear force because it is much weaker than the strong nuclear force. It is now known that the weak nuclear force and the electromagnetic force are two diff erent manifestations of a single, more funda- mental force, the electroweak force. The theory for the electroweak force was developed by Sheldon Glashow (1932– ), Abdus Salam (1926–1996), and Steven Weinberg (1933– ), who shared a Nobel Prize for their achievement in 1979. The electroweak force, the gravitational force, and the strong nuclear force are the three fundamental forces in nature.
The neutrino has zero electric charge and is extremely diffi cult to detect because it interacts very weakly with matter. For example, the average neutrino can penetrate one light-year of lead (about 9.5 × 1015 m) without interacting with it. Thus, even though trillions of neutrinos pass through our bodies every second, they have no eff ect. One of the major scientifi c questions of our time is whether neutrinos have mass. The question is important because neutrinos are so plentiful in the universe. Even a very small mass could account for a signifi cant portion of the mass in the universe and, possibly, could have an eff ect on the formation of galaxies.
Although difficult, it is possible to detect neutrinos. Figure 31.12 shows the Super- Kamiokande neutrino detector in Japan. It is located 915 m underground and consists of a steel cylindrical tank, ten stories tall, whose inner wall is lined with 11 000 photomultiplier tubes (see Section 31.9). The tank is fi lled with 12.5 million gallons of ultrapure water. Neut- rinos colliding with the water molecules produce light patterns that the photomultiplier tubes detect. In 1998 the Super-Kamiokande detector yielded the fi rst strong, but indirect, evidence that neutrinos do indeed have a small mass. (The mass of the electron neutrino is less than
31.6 Radioactive Decay and Activity 897
0.0004% of the mass of an electron.) This fi nding implies that neutrinos travel at less than the speed of light. If the neutrino’s mass were zero, like that of a photon, it would travel at the speed of light.
31.6 Radioactive Decay and Activity The question of which radioactive nucleus in a group of nuclei disintegrates at a given instant is decided like the winning numbers in a state lottery: individual disintegrations occur randomly. As time passes, the number N of parent nuclei decreases, as Figure 31.13 shows. This graph of N versus time indicates that the decrease occurs in a smooth fashion, with N approaching zero after enough time has passed. To help describe the graph, it is useful to defi ne the half- life T1/2 of a radioactive isotope as the time required for one-half of the nuclei present to disin- tegrate. For example, radium 22688 Ra has a half-life of 1600 years, because it takes this amount of time for one-half of a given quantity of this isotope to disintegrate. In another 1600 years, one-half of the remaining radium atoms will have disintegrated, leaving only one-fourth of the original number intact. In Figure 31.13, the number of nuclei present at time t = 0 s is N = N0, and the number present at t = T1/2 is N =
1 2 N0 . The number present at t = 2T1/2 is N =
1 4 N0 ,
and so on. The value of the half-life depends on the nature of the radioactive nucleus. Values ranging from a fraction of a second to billions of years have been found (see Table 31.2).
THE PHYSICS OF radioactive radon gas in houses. Radon 22286 Rn is a naturally oc- curring radioactive gas produced when radium 22688 Ra undergoes α decay. There is a nationwide concern about radon as a health hazard because radon in the soil is gaseous and can enter the basement of homes through cracks in the foundation. (It should be noted, however, that the mech- anism of indoor radon entry is not well understood and that entry via foundation cracks is likely only part of the story.) Once inside, the concentration of radon can rise markedly, depending on the type of housing construction and the concentration of radon in the surrounding soil. Radon gas decays into daughter nuclei that are also radioactive. The radioactive nuclei can attach to dust and smoke particles that can be inhaled, and they remain in the lungs to release tissue-damaging
FIGURE 31.13 The half-life T1/2 of a radio- active decay is the time in which one-half of the radioactive nuclei disintegrate.
0 0
N0
T1/2 2T1/2 Time, t
N um
be r
of r
ad io
ac ti
ve n
uc le
i, N
3T1/2 4T1/2
N0
N0
1– 2
1– 4
1– 8
N0
FIGURE 31.12 The Super-Kamiokande neutrino detector in Japan is an underground steel cylindrical tank with its inner wall lined with 11 000 photomultiplier tubes. It is fi lled with 12.5 million gallons of ultrapure water when operational. In this photograph it is partially full, and the technicians in the boat are inspecting the photomultiplier tubes.
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va to
ry , I
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R (I
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he U
ni ve
rs ity
o f T
ok yo
898 CHAPTER 31 Nuclear Physics and Radioactivity
radiation. Prolonged exposure to high levels of radon can lead to lung cancer. Since radon gas concentrations can be measured with inexpensive monitoring devices, it is recommended that all homes be tested for radon. Example 7 deals with the half-life of radon 22286Rn.
The activity of a radioactive sample is the number of disintegrations per second that occur. Each time a disintegration occurs, the number N of radioactive nuclei decreases. As a result, the activity can be obtained by dividing ΔN, the change in the number of nuclei, by Δt, the time interval during which the change takes place; the average activity over the time interval Δt is the magnitude of ΔN/Δt, or ∣∆N/∆t ∣. Since the decay of any individual nucleus is completely random, the number of disintegrations per second that occurs in a sample is proportional to the number of radioactive nuclei present, so that
∆N ∆t
= −λN (31.4)
where λ is a proportionality constant referred to as the decay constant. The minus sign is present in this equation because each disintegration decreases the number N of nuclei originally present.
The SI unit for activity is the becquerel (Bq), named after Antoine Becquerel (1852–1908). One becquerel is one disintegration per second. Activity is also measured using a unit called the curie (Ci), honoring Marie (1867–1934) and Pierre (1859–1906) Curie, the discoverers of radium and polonium. Historically, the curie was chosen as a unit because it is roughly the activity of one gram of pure radium. In terms of becquerels,
1 Ci = 3.70 × 1010 Bq
The activity of the radium put into the dial of a watch to make it glow in the dark is about 4 × 104 Bq, and the activity used in radiation therapy for cancer is approximately a billion times greater, or 4 × 1013 Bq.
TABLE 31.2 Some Half-Lives for Radioactive Decay
Isotope Half-Life Polonium 214 84Po 1.64 × 10−4 s
Krypton 8936 Kr 3.16 min
Radon 222 86Rn 3.83 d
Strontium 9038 Sr 29.1 yr
Radium 226 88Ra 1.6 × 103 yr
Carbon 14 6C 5.73 × 103 yr
Uranium 238 92U 4.47 × 109 yr
Indium 11549 In 4.41 × 1014 yr
EXAMPLE 7 The Radioactive Decay of Radon Gas
Suppose that 3.0 × 107 radon atoms are trapped in a basement at the time the basement is sealed against further entry of the gas. The half-life of radon is 3.83 days. How many radon atoms remain after 31 days?
Reasoning During each half-life, the number of radon atoms is reduced by a factor of two. Thus, for each half-life in the period of 31 days, we reduce the number of radon atoms present at the beginning of that half- life by a factor of two.
Solution In a period of 31 days there are (31 days)/(3.83 days) = 8.1 half-lives. In 8 half-lives the number of radon atoms is reduced by a factor of 28 = 256. Ignoring the diff erence between 8 and 8.1 half- lives, we fi nd that the number of atoms remaining after 31 days is (3.0 × 107)/256 = 1.2 × 105 .
31.6 Radioactive Decay and Activity 899
The mathematical expression for the graph of N versus t shown in Figure 31.13 can be ob- tained from Equation 31.4 with the aid of calculus. The result for the number N of radioactive nuclei present at time t is
N = N0 e−λt (31.5)
assuming that the number present at t = 0 s is N0. The exponential e has the value e = 2.718 . . . , and many calculators provide the value of ex. We can relate the half-life T1/2 of a radioactive nucleus to its decay constant λ in the following manner. By substituting N = 12N0 and t = T1/2 into Equation 31.5, we fi nd that 12 = e−λT1/ 2. Solving this equation for T1/2 reveals that
T1/2 = ln 2
λ =
0.693 λ
(31.6)
The following example illustrates the use of Equations 31.5 and 31.6.
Math Skills To obtain Equation 31.6, we take the natural logarithm of both sides of the equation 1 2 = e−λT1/ 2 , which gives
ln(12) = ln(e−λT1/2) According to Equation D-12 in Appendix D, the left side of this result is ln(12) = ln 1 − 1n 2. According to Equation D-9 in Appendix D, the right side is ln(e−λT1/2) = −λT1/2. Thus, we have
ln 1 − ln 2 = −λT1/2 However, since ln 1 = 0, this result becomes
ln 2 = λT1/2 or T1/2 = ln 2
λ (31.6)
EXAMPLE 8 The Activity of Radon 22286 Rn
As in Example 7, suppose that there are 3.0 × 107 radon atoms (T1/2 = 3.83 days or 3.31 × 105 s) trapped in a basement. (a) How many radon atoms remain after 31 days? Find the activity (b) just after the basement is sealed against further entry of radon and (c) 31 days later.
Reasoning The number N of radon atoms remaining after a time t is given by N = N0 e−λt (Equation 31.5), where N0 = 3.0 × 107 is the original number of atoms when t = 0 s and λ is the decay constant. The decay constant is related to the half-life T1/2 of the radon atoms by λ = 0.693/T1/2. The activity can be obtained from ΔN/Δt = −𝜆N (Equation 31.4).
Solution (a) The decay constant is
λ = 0.693 T1/2
= 0.693
3.83 days = 0.181 days−1 (31.6)
and the number N of radon atoms remaining after 31 days is
N = N0 e−λt = (3.0 × 107) e−(0.181 days −1)(31 days) = 1.1 × 105 (31.5)
This value is slightly less than that found in Example 7 because there we ignored the diff erence between 8.0 and 8.1 half-lives.
(b) The activity can be obtained from Equation 31.4, provided the decay constant is expressed in reciprocal seconds:
λ = 0.693 T1/2
= 0.693
3.31 × 105 s = 2.09 × 10−6 s−1 (31.6)
Thus, the number of disintegrations per second is
∆N ∆t
= −λN = −(2.09 × 10−6 s−1)(3.0 × 107) = −63 disintegrations/s (31.4)
The activity is the magnitude of ΔN/Δt, so initially Activity = 63 Bq .
(c) From part (a), the number of radioactive nuclei remaining at the end of 31 days is N = 1.1 × 105, and reasoning similar to that in part (b) reveals that Activity = 0.23 Bq .
Check Your Understanding
(The answers are given at the end of the book.) 9. The thallium 20881Tl nucleus is radioactive, with a half-life of 3.053 min. At a given instant, the activity of
a certain sample of thallium is 2400 Bq. Using the concept of a half-life, and without doing any written (Continued)
900 CHAPTER 31 Nuclear Physics and Radioactivity
calculations, determine whether the activity 9 minutes later is (a) a little less than 18 (2400 Bq) = 300 Bq, (b) a little more than 18 (2400 Bq) = 300 Bq, (c) a little less than
1 3 (2400 Bq) = 800 Bq, or (d) a little
more than 13 (2400 Bq) = 800 Bq.
10. The half-life of indium 115 49ln is 4.41 × 1014 yr. Thus, one-half of the nuclei in a sample of this isotope will decay in this time, which is very long. Is it possible for any single nucleus in the sample to decay after only one second?
11. Could two diff erent samples of the same radioactive element have diff erent activities?
31.7 Radioactive Dating THE PHYSICS OF radioactive dating. One important application of radioactivity is the determination of the age of archaeological or geological samples as in the case of the mummifi ed remains of Queen Hatshepsut (see Photo 31.1). If an object contains radioactive nuclei when it is formed, then the decay of these nuclei marks the passage of time like a clock, half of the nuc- lei disintegrating during each half-life. If the half-life is known, a measurement of the number of nuclei present today relative to the number present initially can give the age of the sample. According to Equation 31.4, the activity of a sample is proportional to the number of radioactive nuclei, so one way to obtain the age is to compare present activity with initial activity. A more accurate way is to determine the present number of radioactive nuclei with the aid of a mass spectrometer.
The present activity of a sample can be measured, but how is it possible to know what the original activity was, perhaps thousands of years ago? Radioactive dating methods entail certain assumptions that make it possible to estimate the original activity. For instance, the ra- diocarbon technique utilizes the 614 C isotope of carbon, which undergoes 𝛽− decay with a half- life of 5730 yr. This isotope is currently present in the earth’s atmosphere at an equilibrium concentration of about one atom for every 8.3 × 1011 atoms of normal carbon 612 C. It is of- ten assumed* that this value has remained constant over the years because 614 C is created when cosmic rays interact with the earth’s upper atmosphere, a production method that off sets the loss via 𝛽− decay. Moreover, nearly all living organisms ingest the equilibrium concentration of 6 14 C. However, once an organism dies, metabolism no longer sustains the input of 614 C, and 𝛽− decay causes half of the 614 C nuclei to disintegrate every 5730 years. Example 9 illustrates how to determine the 614 C activity of one gram of carbon in a living organism.
*The assumption that the 614C concentration has always been at its present equilibrium value has been evaluated by comparing 614C ages with ages determined by counting tree rings. More recently, ages determined using the radioactive decay of uranium 92238 U have been used for comparison. These comparisons indicate that the equilibrium value of the 6 14C concentration has indeed remained constant for the past 1000 years. However, from there back about 30 000 years, it appears that the 614C concentration in the atmosphere was larger than its present value by up to 40%. As a fi rst approximation we ignore such discrepancies.
The mummifi ed remains of Queen Hatshepsut, who ruled ancient Egypt from 1479 to 1458 BC. Radioactive dating is one of the techniques used to determine the age of such remains.
A FP
/G et
ty Im
ag es
31.7 Radioactive Dating 901
An organism that lived thousands of years ago presumably had an activity of about 0.23 Bq
per gram of carbon. When the organism died, the activity began decreasing. From a sample of the
remains, the current activity per gram of carbon can be measured and compared to the value of 0.23
Bq to determine the time that has transpired since death. This procedure is illustrated in Example 10.
EXAMPLE 9 146C Activity per Gram of Carbon in a Living Organism
(a) Determine the number of carbon 614 C atoms present for every gram of carbon 6
12 C in a living organism. Find (b) the decay constant and (c) the activity of this sample.
Reasoning The total number of carbon 612 C atoms in one gram of car- bon 6
12 C is equal to the corresponding number of moles times Avogadro’s
number (see Section 14.1). Since there is only one 6 14 C atom for every 8.3
× 1011 atoms of 6 12 C, the number of 6
12 C atoms is equal to the total number
of 6 12 C atoms divided by 8.3 × 1011. The decay constant 𝜆 for 614 C is 𝜆 =
0.693/T1/2, where T1/2 is the half-life. The activity is equal to the mag- nitude of ΔN/Δt, which is equal to the decay constant times the number of 6
14 C atoms present, according to Equation 31.4.
Solution (a) One gram of carbon 612 C (atomic mass = 12 u) is equival- ent to 1.0/12 mol. Since Avogadro’s number is 6.02 × 1023 atoms/mol and
since there is one 6 14 C atom for every 8.3 × 1011 atoms of 6
12 C, the number
of 6 14 C atoms is
Number of 6 14 C
atoms for every 1.0
grams of carbon 6 12 C
= (1.012 mol) (6.02 × 1023 atoms
mol ) ( 1
8.3 × 1011) = 6.0 × 1010 atoms
(b) Since the half-life of 614 C is 5730 yr (1.81 × 1011 s), the decay constant is
λ = 0.693
T1/2 =
0.693
1.81 × 10 11 s = 3.83 × 10−12 s−1 (31.6)
(c) Equation 31.4 indicates that ΔN/Δt = −𝜆N, so the magnitude of ΔN/Δt is 𝜆N.
Activity of 6 14 C for
every 1.0 gram of
carbon 6 12 C in a
living organism
= λN = (3.83 × 10−12 s−1)(6.0 × 1010 atoms) = 0.23 Bq
Analyzing Multiple-Concept Problems
EXAMPLE 10 The Ice Man
On September 19, 1991, German tourists in the Italian Alps found a
Stone-Age traveler, later dubbed the Ice Man, whose body had become
trapped in a glacier. Figure 31.14 shows the well-preserved remains, which were dated using the radiocarbon method. Material found with the
body had a 6 14C activity of about 0.121 Bq per gram of carbon. Find the
age of the Ice Man’s remains.
Reasoning In the radiocarbon method, the number of radioactive nuclei remaining at a given instant is related to the number present
initially, the time that has passed since the Ice Man died, and the decay
constant for 6 14C. Thus, to determine the age of the remains, we will
need information about the number of nuclei present when the body
was discovered and the number present initially, which is related to
the activity of the material found with the body and the initial activity.
To determine the age, we will also need the decay constant, obtainable
from the half-life of 6 14C.
Knowns and Unknowns We have the following data:
Description Symbol Value Comment Explicit Data Activity of material found with body A 0.121 Bq This is the activity per gram of carbon.
Implicit Data
Half-life of 6 14 C T1/2 5730 yr The radiocarbon dating method is specified.
Initial activity of material found with body A0 0.23 Bq This activity is assumed for one gram of carbon in a living organism.
Unknown Variable Age of Ice Man’s remains t ?
© S
o u th
T y ro
l M
u se
u m
o f
A rc
h ae
o lo
g y /
E u ra
c/ S
am ad
el li
/S ta
sc h it
z
FIGURE 31.14 The frozen remains of the Ice Man or “Oetzi,” as he also is called, were discovered in the ice of a glacier in the Italian Alps
in 1991. Radiocarbon dating has revealed his age.
902 CHAPTER 31 Nuclear Physics and Radioactivity
Modeling the Problem
STEP 1 Radioactive Decay The number N of radioactive nuclei present at a time t is
N = N0 e−λt (31.5)
where N0 is the number present initially at t = 0 s and 𝜆 is the decay constant for 614 C. Rearranging terms gives
N N0
= e−λt
Taking the natural logarithm of both sides of this result (see Appendix D), we fi nd that
ln ( NN0) = −λt Solving for t shows that the age of the Ice Man’s remains is given by Equation 1 at the right. To use this result, we need information about the ratio N/N0 and 𝜆. We deal with N/N0 in Step 2 and with 𝜆 in Step 3.
STEP 2 Activity The activity A is the number of disintegrations per second, or │∆N∆t │, where ΔN is the number of disintegrations that occur in the time interval Δt.
Noting that ∆N ∆t
= −λN according to Equation 31.4, we fi nd for the activity that
A =│∆N∆t │= ∣−λN ∣ = λN Using this expression, we have that
N N0
= λN λN0
= A A 0
The substitution of this result into Equation 1 is shown at the right. We turn now to Step 3, in order to evaluate the decay constant 𝜆.
STEP 3 Decay Constant The decay constant is related to the half-life T1/2 according to
λ = 0.693 T1/2
(31.6)
which we substitute into Equation 1, as shown at the right.
Solution Combining the results of each step algebraically, we fi nd that
t = −(1λ) ln ( N N0) = −(
1 λ) ln (
A A 0) = −(
1 0.693/T1/2) ln (
A A 0)
This result reveals that the age of the Ice Man’s remains is
t = −( T1/2
0.693) ln ( A A 0) = −(
5730 yr 0.693 ) ln (
0.121 Bq 0.23 Bq ) = 5300 yr
Note that this solution implies for the activity that
A = A0 e−λt
This can be seen by combining the result from Step 2 (N/N0 = A/A0) with Equation 31.5 (N = N0e−𝜆t).
Related Homework: Problems 47, 50
STEP 1 STEP 2 STEP 3
t = −(1λ) ln ( N N0) (1)
??
⏟
t = −(1λ) ln ( N N0) (1)
?
⏟
N N0
= A A 0
t = −(1λ) ln ( N N0) (1)
⏟
N N0
= A A 0
λ = 0.693 T1/2
t = −(1λ) ln ( N N0) (1)
⏟
N N0
= A A 0
λ = 0.693 T1/2
Radiocarbon dating is not the only radioactive dating method. For example, other methods utilize uranium 238 92U, potassium 40 19K, and lead 21082 Pb. For such methods to be useful, the half-life of the radioactive species must be neither too short nor too long relative to the age of the sample to be dated, as Conceptual Example 11 discusses.
31.8 Radioactive Decay Series 903
Check Your Understanding
(The answers are given at the end of the book.) 12. To which one or more of the following objects, each about 1000 yr old, can the radiocarbon dating
technique not be applied? (a) A wooden box (b) A gold statue (c) Some well-preserved animal fur 13. Suppose there were a greater number of carbon 614C atoms in a plant living 5000 yr ago than is currently
believed. When the seeds of this plant are tested using radiocarbon dating, is the age obtained too small or too large compared to the true age?
14. Review Conceptual Example 11 as an aid in answering this question. Tritium is an isotope of hydrogen and undergoes β− decay with a half-life of 12.33 yr. Like carbon 614C, tritium is produced in the atmo- sphere because of cosmic rays and can be used in a radioactive dating technique. Can tritium dating be used to determine a reliable date for a sample that is about 700 yr old?
31.8 Radioactive Decay Series When an unstable parent nucleus decays, the resulting daughter nucleus is sometimes also un- stable. If so, the daughter then decays and produces its own daughter, and so on, until a com- pletely stable nucleus is produced. This sequential decay of one nucleus after another is called a radioactive decay series. Examples 4–6 discuss the fi rst two steps of a series that begins with uranium 23892 U:
Uranium
U +23892
Protactinium
Pa23491
Thorium
Th23490 He 4 2
+ e01–
Furthermore, Examples 7 and 8 deal with radon 22286 Rn, which is formed down the line in the 23892 U radioactive decay series. Figure 31.15 shows the entire series. At several points, branches occur because more than one kind of decay is possible for an intermediate species. Ultimately, however, the series ends with lead 20682 Pb, which is stable.
CONCEPTUAL EXAMPLE 11 Dating a Bottle of Wine
A bottle of red wine is thought to have been sealed about 5 years ago. The wine contains a number of diff erent atoms, including carbon, oxygen, and hydrogen. Each of these has a radioactive isotope. The radioactive isotope of carbon is the familiar 614 C, with a half-life of 5730 yr. The radioactive isotope of oxygen is 15 8O and has a half-life of 122.2 s. The radioactive iso- tope of hydrogen, called tritium, is 3 1H; its half-life is 12.33 yr. The activ- ity of each of these isotopes is known at the time the bottle was sealed. However, only one of the isotopes is useful for determining the age of the wine accurately from a measurement of its current activity. Which is it? (a) 614 C (b) 15 8O (c) 3 1H
Reasoning To fi nd the age of the wine, it is necessary to determine the ratio of the current activity A to the initial activity A0 (see Example 10). If the age of the sample is very small relative to the half-life of the nuclei, relatively few of the nuclei would have decayed during the wine’s life, and the measured activity would have changed little from its initial value (A ≈ A0 ). To obtain an accurate age from such a small change would re- quire prohibitively precise measurements. On the other hand, if the age of the sample is many times greater than the half-life of the nuclei, virtually
all of the nuclei would have decayed, and the current activity would be so small (A ≈ 0) that it would be virtually impossible to detect.
Answer (a) is incorrect. The expected age of the wine is about 5 years. This period is only a tiny fraction of the 5730-yr half-life of 614 C. As a res- ult, relatively few of the 614 C nuclei would have decayed during the wine’s life, and the current activity would be nearly the same as the initial activity (A ≈ A0 ), thus requiring prohibitively precise measurements.
Answer (b) is incorrect. The 15 8O isotope is not very useful either, be- cause of its relatively short half-life of 122.2 s. During a 5-year period, so many half-lives of 122.2 s would have occurred that the current activity would be vanishingly small (A ≈ 0) and undetectable.
Answer (c) is correct. The only remaining option is the 3 1H isotope. The expected age of 5 yr is long enough relative to the half-life of 12.33 yr that a measurable change in activity will have occurred, but not so long that the current activity will have completely vanished for all practical purposes.
Related Homework: Check Your Understanding Question 14, Problem 49
904 CHAPTER 31 Nuclear Physics and Radioactivity
The 23892 U series and other such series are the only sources of some of the radioactive elements found in nature. Radium 22688 Ra, for instance, has a half-life of 1600 yr, which is short enough that all the 22688 Ra created when the earth was formed billions of years ago has now disappeared. The 238 92 U series provides a continuing supply of 22688 Ra, however.
Check Your Understanding
(The answer is given at the end of the book.) 15. Because of radioactive decay, one element can be transmuted into another. Thus, a container of uranium
238 92 U ultimately becomes a container of lead 20682 Pb, as Figure 31.15 indicates. Roughly, how long does
it take for 23892 U to transmute entirely into 20682 Pb? (a) Several decades (b) Several centuries (c) Thou- sands of years (d) Millions of years (e) Billions of years
31.9 Radiation Detectors THE PHYSICS OF radiation detectors. There are a number of devices that can be used to detect the particles and photons (γ rays) emitted when a radioactive nucleus decays. Such devices detect the ionization that these particles and photons cause as they pass through matter.
The most familiar detector is the Geiger counter, which Figure 31.16 illustrates. The Geiger counter consists of a gas-fi lled metal cylinder. The α, β, or γ rays enter the cylinder through a thin window at one end. γ rays can also penetrate directly through the metal. A wire electrode runs along the center of the tube and is kept at a high positive voltage (1000–3000 V) relative to the outer cylinder. When a high-energy particle or photon enters the cylinder, it collides with and ion- izes a gas molecule. The electron produced from the gas molecule accelerates toward the positive wire, ionizing other molecules in its path. Additional electrons are formed, and an avalanche of electrons rushes toward the wire, leading to a pulse of current through the resistor R. This pulse can be counted or made to produce a “click” in a loudspeaker. The number of counts or clicks is related to the number of disintegrations that produced the particles or photons.
238
234
230
226
222
218
214
210
206 80 81 82 83 84 85 86 87 88 89 90 91 92 Hg TI Pb Bi Po At Rn Fr Ra Ac Th Pa U
8.2 m 4.2 m FINISH Z
22 y 1.3 m
22 y
5.0 d
13 8 d
5.0 d 20
m 27 m 20 m
1.6 × 10–4 s
3.1 m
3.1 m
1.6
s
0.0 35
s
1.6 s 3.8
d
1.6 ×
10 3 y
7.5 ×
10 4 y
2.5 ×
10 5 y
24 d 6.7 h
𝛽 decay
𝛼 decay
STARTA
4.5 ×
10 9 y
FIGURE 31.15 The radio- active decay series that begins with uranium 23892 U and ends with lead 20682Pb. Half-lives are given in seconds (s), minutes (m), hours (h), days (d), or years (y). The inset in the upper left identifi es the type of decay that each nucleus undergoes.
High voltage
Window
High-energy particle or photon
Counting device
R
e– Gas molecule
Wire electrode
+ –
FIGURE 31.16 A Geiger counter.
31.9 Radiation Detectors 905
The scintillation counter is another important radiation detector. As Figure 31.17 indicates, this device consists of a scintillator mounted on a photomultiplier tube. Often the scintillator is a crystal (e.g., cesium iodide) containing a small amount of impurity (thallium), but plastic, liquid, and gaseous scintillators are also used. In response to ionizing radiation, the scintillator emits a fl ash of visible light. The photons of the fl ash then strike the photocathode of the photomultiplier tube. The photocathode is made of a material that emits electrons because of the photoelectric eff ect. These photoelectrons are then attracted to a special electrode kept at a voltage of about +100 V relative to the photocathode. The electrode is coated with a substance that emits several additional electrons for every electron striking it. The additional electrons are attracted to a second similar electrode (voltage = +200 V), where they generate even more electrons. Com- mercial photomultiplier tubes contain as many as 15 of these special electrodes, so photoelec- trons resulting from the light fl ash of the scintillator lead to a cascade of electrons and a pulse of current. As in a Geiger tube, the current pulses can be counted.
Ionizing radiation can also be detected with several types of semiconductor detectors. Such devices utilize n- and p-type materials (see Section 23.5), and their operation depends on the electrons and holes formed in the materials as a result of the radiation. One of the main advant- ages of semiconductor detectors is their ability to discriminate between two particles with only slightly diff erent energies.
A number of instruments provide a pictorial representation of the path that high-energy particles follow after they are emitted from unstable nuclei. In a cloud chamber, a gas is cooled just to the point at which it will condense into droplets, provided nucleating agents are available on which the droplets can form. When a high-energy particle, such as an α particle or a β particle, passes through the gas, the ions it leaves behind serve as nucleating agents, and droplets form along the path of the particle. A bubble chamber works in a similar fashion, except that it contains a liquid that is just at the point of boiling. Tiny bubbles form along the trail of a high-energy particle passing through the liquid. Paths revealed in a cloud or bubble chamber can be photographed to provide a permanent record of the event. Figure 31.18 shows a photograph of tracks in a cloud chamber. A photographic emulsion also can be used dir- ectly to produce a record of the path taken by a particle of ionizing radiation. Ions formed as the particle passes through the emulsion cause silver to be deposited along the track when the emulsion is developed.
Photoelectron
Photon
Photo- multiplier
tube
Photocathode (0 V)
High-energy particle
or photon Scintillator
+200 V
+400 V
Pulse output to counting device
+500 V
+300 V
+100 V
FIGURE 31.17 A scintillation counter.
Sc ie
nc e
So ur
ce
FIGURE 31.18 A photograph showing particle tracks in a cloud chamber.
EXAMPLE 12 BIO The Physics of 90Sr in the Bones
Calcium is an essential element in the human body for maintaining proper bone density. Strontium is chemically very similar to calcium, and 99% of strontium in the body is located in the bones. This typically does not cause health problems, if the strontium in the body is a non-radioactive stable isotope. However, if a person ingests a radioactive isotope of strontium,
like 90Sr, for example, then the isotope will settle in the bones and deliver harmful radiation to the nearby bone and marrow cells. This can lead to bone cancer and leukemia (Figure 31.19). If 90Sr undergoes β−decay with a half-life of 29.1 years, what percentage of the initial amount is still in the body after 50.0 years?
906 CHAPTER 31 Nuclear Physics and Radioactivity
Concept Summary 31.1 Nuclear Structure The nucleus of an atom consists of protons and neutrons, which are collectively referred to as nucleons. A neutron is an elec-
trically neutral particle whose mass is slightly larger than that of the proton.
The atomic number Z is the number of protons in the nucleus. The atomic mass number A (or nucleon number) is the total number of protons and neut- rons in the nucleus and is given by Equation 31.1, where N is the number of neutrons. For an element whose chemical symbol is X, the symbol for
the nucleus is AZ X. Nuclei that contain the same number of protons, but a
diff erent number of neutrons, are called isotopes. The approximate radius (in
meters) of a nucleus is given by Equation 31.2.
A = Z + N (31.1)
r ≈ (1.2 × 10−15 m) A1/3 (31.2)
31.2 The Strong Nuclear Force and the Stability of the Nucleus The strong nuclear force is the force of attraction between nucleons (protons and
neutrons) and is one of the three fundamental forces of nature. This force
balances the electrostatic force of repulsion between protons and holds the
nucleus together. The strong nuclear force has a very short range of action
and is almost independent of electric charge.
31.3 The Mass Defect of the Nucleus and Nuclear Binding Energy The binding energy of a nucleus is the energy required to separate the nucleus into
its constituent protons and neutrons. The binding energy is given by Equation
31.3, where Δm is the mass defect of the nucleus and c is the speed of light in a vacuum. The mass defect is the amount by which the sum of the individual
masses of the protons and neutrons exceeds the mass of the intact nucleus.
When specifying nuclear masses, it is customary to use the atomic mass unit (u).
One atomic mass unit has a mass of 1.6605 × 10−27 kg and is equivalent to
an energy of 931.5 MeV.
Binding energy = (∆m)c2 (31.3)
31.4 Radioactivity Unstable nuclei spontaneously decay by breaking apart or rearranging their internal structure in a process called radioactivity.
Naturally occurring radioactivity produces α, β, and γ rays. α rays consist of
positively charged particles, each particle being the 42He nucleus of helium.
The general form for α decay is
Z A P Z−2
A−4 D + 2 4 He
The most common kind of β ray consists of negatively charged particles, or β− particles, which are electrons. The general form for β− decay is
Z AP Z+1
A D + −1 0 e
β+ decay produces another kind of β ray, which consists of positively charged particles, or β+ particles. A β+ particle, also called a positron, has the same mass as an electron, but carries a charge of +e instead of −e.
If a radioactive parent nucleus disintegrates into a daughter nucleus that
has a diff erent atomic number, as occurs in α and β decay, one element has been converted into another element, the conversion being referred to as a
transmutation.
γ rays are high-energy photons emitted by a radioactive nucleus. The gen- eral form for γ decay is
Z A P* Z
A P + 𝛾
γ decay does not cause a transmutation of one element into another.
31.5 The Neutrino The neutrino is an electrically neutral particle that is emitted along with β particles and has a mass that is much, much smaller than the mass of an electron.
31.6 Radioactive Decay and Activity The half-life of a radioactive iso- tope is the time required for one-half of the nuclei present to disintegrate or
⏟⏟⏟ ⏟⏟⏟ ⏟⏟⏟ Parent
nucleus
Daughter
nucleus
α particle (helium nucleus)
⏟⏟⏟ Parent
nucleus
⏟⏟⏟ Daughter
nucleus
⏟⏟⏟ β− particle (electron)
⏟⏟⏟ Excited
energy state
⏟⏟⏟ Lower
energy state
⏟⏟⏟ 𝛾 ray
Reasoning We can use Equation 31.5 to calculate the ratio of remain- ing 90Sr atoms (N) to the original number (N0). To fi nd this ratio, we will need the decay constant (λ) for 90Sr, which is related to its half-life (T1/2) by Equation 31.6.
Solution Beginning with Equation 31.5, we have:
N = N0 e−λt ⇒ N N0
= e−λt.
To fi nd the decay constant, we use Equation 31.6:
λ = 0.693
T1/2 =
0.693
29.1 yr = 0.0238 yr−1.
Plugging this into the expression above, we can calculate the ratio of
remaining atoms:
N N0
= e−(0.0238 yr−1)(50.0 yr) = 0.304 = 30.4% .
The half-life of 90Sr is a signifi cant fraction of a typical lifespan. Thus,
even after 50 years, there is a considerable percentage of atoms remaining.
FIGURE 31.19 Cross-section of a human femur bone showing a malignant tumor known
as osteosarcoma. This is an aggressive form of
cancer that can result from 90Sr replacing Ca in
the bone.
C N
R I/
S ci
en ce
S o u rc
e
Focus on Concepts 907
decay. The activity is the number of disintegrations per second that occur. Activity is the magnitude of ΔN/Δt, where ΔN is the change in the number N of radioactive nuclei and Δt is the time interval during which the change occurs. In other words, activity is ∣∆N/∆t ∣. The SI unit for activity is the becquerel (Bq), one becquerel being one disintegration per second. Activity is sometimes also measured in a unit called the curie (Ci); 1 Ci = 3.70 × 1010 Bq.
∆ N ∆ t
= −λN (31.4)
Radioactive decay obeys Equation 31.4, where 𝜆 is the decay constant. This equation can be solved by the methods of integral calculus to show that N is given by Equation 31.5, where N0 is the original number of nuclei. The decay constant 𝜆 is related to the half-life T1/2 according to Equation 31.6.
N = N0e−λt (31.5)
λ = 0.693 T1/2
(31.6)
31.7 Radioactive Dating If an object contained radioactive nuclei when it was formed, then the decay of these nuclei can be used to determine the age of the object. One way to obtain the age is to relate the present activity A of an object to its initial activity A0, according to Equation 1, where 𝜆 is the decay constant and t is the age of the object. For radiocarbon dating that uses the 6 14C isotope of carbon, the initial activity is often assumed to be A0 = 0.23 Bq.
31.8 Radioactive Decay Series The sequential decay of one nucleus after another is called a radioactive decay series. A decay series starts with a radioactive nucleus and ends with a completely stable nucleus. Figure 31.15 illustrates one such series that begins with uranium 23892U and ends with lead 206 82Pb.
31.9 Radiation Detectors A number of devices are used to detect α and β particles as well as γ rays. These include the Geiger counter, the scintillation counter, semiconductor detectors, cloud and bubble chambers, and photo- graphic emulsions.
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 31.1 Nuclear Structure 1. An indium (In) nucleus contains 49 protons and 66 neutrons. Which one of the following symbols describes this nucleus? (a) 49115 In (b) 4966 In (c) 11566 In (d) 6649 In (e) 11549 In 2. The notation for a particular nucleus is 8537 Rb. In an electrically neutral atom, how many electrons are in orbit about this nucleus? (a) 37 + 85 = 122 (b) 85 (c) 37 (d) 85 − 37 = 48 (e) The number of electrons cannot be determined from the notation.
Section 31.3 The Mass Defect of the Nucleus and Nuclear Binding Energy 6. Suppose that we lived in a hypothetical world in which the mass of each proton and each neutron were exactly 1 u. In this world, the atomic mass of copper 6329 Cu is 62.5 u. What would be the mass defect for this nucleus? (a) 63 u (b) 29 u (c) 63 u − 29 u = 34 u (d) 0.5 u (e) 63 u + 29 u = 92 u
Section 31.4 Radioactivity 7. Which one or more of the three decay processes (α, β−, or γ) results in a new element? (a) α and β− (b) Only α (c) Only β− (d) β− and γ (e) Only γ 9. A nucleus can undergo α, β−, or γ decay. For each type of decay, is the radius of the daughter nucleus greater than, less than, or about the same as the radius of the parent nucleus?
𝜶 Decay 𝞫− Decay 𝞬 Decay
(a) Greater than Greater than About the same as
(b) Greater than Less than About the same as
(c) Less than About the same as Greater than
(d) Less than About the same as About the same as
(e) About the same as Less than Less than
Section 31.6 Radioactive Decay and Activity 13. Two samples contain diff erent radioactive isotopes. Is it possible for these samples to have the same activity? (a) Yes, if they have the same num- ber of nuclei but diff erent half-lives. (b) Yes, if they have diff erent numbers of nuclei and diff erent half-lives. (c) Yes, if they have diff erent numbers of nuclei but the same half-lives. (d) No, because they can have diff erent half- lives. (e) No, because they can have diff erent numbers of nuclei. 16. The drawing shows the activities of three radioactive samples. Rank the samples according to half-life, largest fi rst. (a) 2, 3, 1 (b) 1, 2, 3 (c) 3, 2, 1 (d) 1, 3, 2 (e) 3, 1,2
A ct
iv it
y
Time
1
2
3
QUESTION 16
Section 31.7 Radioactive Dating 18. The bones from an animal found at an archaeological dig have a 146 C activity of 0.10 Bq per gram of carbon. The half-life of the radioactive iso- tope 146 C is 5730 yr. Which one of the following best describes the age of the bones? (a) It is less than 2000 years. (b) It is between 2000 and 3000 years. (c) It is between 3000 and 4000 years. (d) It is between 4000 and 5000 years. (e) It is more than 5000 years.
Focus on Concepts
908 CHAPTER 31 Nuclear Physics and Radioactivity
Note to Instructors: Most of the homework problems in this chapter are available for assignment via WileyPLUS. See the Preface for additional details.
Note: The data given for atomic masses in these problems include the mass of the electrons orbiting the nucleus of the electrically neutral atom.
SSM Student Solutions Manual MMH Problem-solving help GO Guided Online Tutorial V-HINT Video Hints CHALK Chalkboard Videos
BIO Biomedical application E Easy M Medium H Hard
Section 31.1 Nuclear Structure, Section 31.2 The Strong Nuclear Force and the Stability of the Nucleus 1. E SSM For 208 82Pb fi nd (a) the net electrical charge of the nucleus, (b) the number of neutrons, (c) the number of nucleons, (d) the approximate radius of the nucleus, and (e) the nuclear density. 2. E A nucleus contains 18 protons and 22 neutrons. What is the radius of this nucleus?
3. E In each of the following cases, what element does the symbol X rep- resent and how many neutrons are in the nucleus? Use the periodic table on the inside of the back cover as needed. (a) 19578 X (b) 3216 X (c) 6329 X (d) 115 X (e) 23994 X 4. E By what factor does the nucleon number of a nucleus have to increase in order for the nuclear radius to double?
5. E SSM In electrically neutral atoms, how many (a) protons are in the uranium 23892 U nucleus, (b) neutrons are in the mercury 20280 Hg nucleus, and (c) electrons are in orbit about the niobium 9341 Nb nucleus? 6. E GO The largest stable nucleus has a nucleon number of 209, and the smallest has a nucleon number of 1. If each nucleus is assumed to be a sphere, what is the ratio (largest/smallest) of the surface areas of these spheres?
7. M GO The ratio rX/rT of the radius of an unknown nucleus AZX to the radius of a tritium nucleus 31T is
rX rT = 1.10. Both nuclei contain the same
number of neutrons. Identify the unknown nucleus in the form AZ X. Use the periodic table on the inside of the back cover as needed.
8. M V-HINT An unknown nucleus contains 70 neutrons and has twice the volume of the nickel 6028 Ni nucleus. Identify the unknown nucleus in the form A Z X. Use the periodic table on the inside of the back cover as needed.
9. H SSM Available in WileyPLUS. 10. H Available in WileyPLUS.
Section 31.3 The Mass Defect of the Nucleus and Nuclear Binding Energy (Note: The atomic mass for hydrogen 11H is 1.007 825 u; this includes the mass of one electron.)
11. E SSM Find the binding energy (in MeV) for lithium 73 Li (atomic mass = 7.016 003 u).
12. E The binding energy of a nucleus is 225.0 MeV. What is the mass defect of the nucleus in atomic mass units?
13. E Determine the mass defect (in atomic mass units) for (a) helium 32He, which has an atomic mass of 3.016 030 u, and (b) the isotope of hydrogen known as tritium 31T, which has an atomic mass of 3.016 050 u. (c) On the
basis of your answers to parts (a) and (b), state which nucleus requires more energy to disassemble it into its separate and stationary constituent nucleons. Give your reasoning.
14. E GO A 245-kg boulder is dropped into a mine shaft that is 3.0 × 103 m deep. During the boulder’s fall, the system consisting of the earth and the boulder loses a certain amount of gravitational potential energy. It would take an equal amount of energy to “free” the boulder from the shaft by rais- ing it back to the top, so this can be considered the system’s binding energy. (a) Determine the binding energy (in joules) of the earth–boulder system. (b) How much mass does the earth–boulder system lose when the boulder falls to the bottom of the shaft?
15. E CHALK For lead 20682Pb (atomic mass = 205.974 440 u) obtain (a) the mass defect in atomic mass units, (b) the binding energy (in MeV), and (c) the binding energy per nucleon (in MeV/nucleon). 16. M (a) Energy is required to separate a nucleus into its constituent nucleons, as Interactive Figure 31.3 indicates; this energy is the total bind- ing energy of the nucleus. In a similar way one can speak of the energy that binds a single nucleon to the remainder of the nucleus. For example, separ- ating nitrogen 14 7N into nitrogen 13 7N and a neutron takes energy equal to the binding energy of the neutron, as shown below:
14 7N + Energy 13 7 N + 10n
Find the energy (in MeV) that binds the neutron to the 14 7 N nucleus by con- sidering the mass of 13 7N (atomic mass = 13.005 738 u) and the mass of 10n (atomic mass = 1.008 665 u), as compared to the mass of 14 7 N (atomic mass = 14.003 074 u). (b) Similarly, one can speak of the energy that binds a single proton to the 14 7N nucleus:
14 7N + Energy 13 6 C + 11H
Following the procedure outlined in part (a), determine the energy (in MeV) that binds the proton (atomic mass = 1.007 825 u) to the 14 7N nucleus. The atomic mass of carbon 136 C is 13.003 355 u. (c) Which nucleon is more tightly bound, the neutron or the proton?
17. M SSM Two isotopes of a certain element have binding energies that diff er by 5.03 MeV. The isotope with the larger binding energy contains one more neutron than the other isotope. Find the diff erence in atomic mass between the two isotopes.
18. M GO A copper penny has a mass of 3.0 g. Determine the energy (in MeV) that would be required to break all the copper nuclei into their con- stituent protons and neutrons. Ignore the energy that binds the electrons to the nucleus and the energy that binds one atom to another in the structure of the metal. For simplicity, assume that all the copper nuclei are 6329 Cu (atomic mass = 62.939 598 u).
Section 31.4 Radioactivity 19. E SSM Write the β+ decay process for each of the following nuclei, being careful to include Z and A and the proper chemical symbol for each daughter nucleus: (a) 189 F (b) 158 O 20. E Write the β− decay process for carbon 146 C, including the chemical symbols as well as the values of Z and A for the parent and daughter nuclei and the β− particle. 21. E SSM Osmium 191 76Os (atomic mass = 190.960 920 u) is converted into iridium 191 77Ir (atomic mass = 190.960 584 u) via β− decay. What is the energy (in MeV) released in this process?
Problems
Problems 909
22. E Find the energy that is released when a nucleus of lead 21182 Pb (atomic mass = 210.988 735 u) undergoes β− decay to become bismuth 21183Bi (atomic mass = 210.987 255 u).
23. E Find the energy (in MeV) released when α decay converts radium 226 88 Ra (atomic mass = 226.025 40 u) into radon 22286 Rn (atomic mass =
222.017 57 u). The atomic mass of an α particle is 4.002 603 u. 24. E GO Lead 20782 Pb is a stable daughter nucleus that can result from either an α decay or a β− decay. Write the decay processes, including the chemical symbols and values for Z and A of the parent nuclei, for (a) the α decay and (b) the β− decay. 25. E In the form AZ X, identify the daughter nucleus that results when (a) plutonium 24294 Pu undergoes α decay, (b) sodium 2411 Na undergoes β− decay, and (c) nitrogen 137 N undergoes β+ decay. 26. E V-HINT When uranium 23592U decays, it emits (among other things) a 𝛾 ray that has a wavelength of 1.14 × 10−11 m. Determine the energy (in MeV) of this 𝛾 ray. 27. M CHALK MMH Polonium 21084 Po (atomic mass = 209.982 848 u) under- goes α decay. Assuming that all the released energy is in the form of kinetic energy of the α particle (atomic mass = 4.002 603 u) and ignoring the recoil of the daughter nucleus (lead 20682 Pb, 205.974 440 u), fi nd the speed of the α particle. Ignore relativistic eff ects.
28. M GO Radon 22086 Rn produces a daughter nucleus that is radioactive. The daughter, in turn, produces its own radioactive daughter, and so on. This pro- cess continues until lead 20882 Pb is reached. What are the total number Nα of α particles and the total number N𝛽 of β− particles that are generated in this series of radioactive decays?
29. M Review Conceptual Example 5 as background for this problem. The α decay of uranium 23892 U produces thorium 23490 Th (atomic mass = 234.0436 u). In Example 4, the energy released in this decay is determined to be 4.3 MeV. Determine how much of this energy is carried away by the recoil- ing 23490 Th daughter nucleus and how much by the α particle (atomic mass = 4.002 603 u). Assume that the energy of each particle is kinetic energy, and ignore the small amount of energy carried away by the 𝛾 ray that is also emit- ted. In addition, ignore relativistic eff ects.
30. H MMH An isotope of beryllium (atomic mass = 7.017 u) emits a 𝛾 ray and recoils with a speed of 2.19 × 104 m/s. Assuming that the beryllium nucleus is stationary to begin with, fi nd the wavelength of the 𝛾 ray. 31. H SSM Find the energy (in MeV) released when β+ decay converts sodium 2211 Na (atomic mass = 21.994 434 u) into neon 2210 Ne (atomic mass = 21.991 383 u). Notice that the atomic mass for 2211 Na includes the mass of 11 electrons, whereas the atomic mass for 2210 Ne includes the mass of only 10 electrons.
Section 31.6 Radioactive Decay and Activity 32. E In 9.0 days the number of radioactive nuclei decreases to one-eighth the number present initially. What is the half-life (in days) of the material?
33. E SSM Available in WileyPLUS. 34. E The 3215 P isotope of phosphorus has a half-life of 14.28 days. What is its decay constant in units of s−1?
35. E BIO Strontium 9038 Sr has a half-life of 29.1 yr. It is chemically sim- ilar to calcium, enters the body through the food chain, and collects in the bones. Consequently, 9038 Sr is a particularly serious health hazard. How long (in years) will it take for 99.9900% of the 9038 Sr released in a nuclear reactor accident to disappear?
36. E GO Two radioactive waste products from nuclear reactors are strontium 90 38 Sr (T1/2 = 29.1 yr) and cesium 13455 Cs (T1/2 = 2.06 yr). These two species are present initially in a ratio of N0,Sr /N0,Cs = 7.80 × 10−3. What is the ratio NSr /NCs fi fteen years later?
37. E SSM Available in WileyPLUS. 38. E BIO Iodine 13153 I is used in diagnostic and therapeutic techniques in the treatment of thyroid disorders. This isotope has a half-life of 8.04 days. What percentage of an initial sample of 13153 I remains after 30.0 days?
39. E SSM The number of radioactive nuclei present at the start of an ex- periment is 4.60 × 1015. The number present twenty days later is 8.14 × 1014. What is the half-life (in days) of the nuclei?
40. M Available in WileyPLUS. 41. M BIO A device used in radiation therapy for cancer contains 0.50 g of cobalt 6027 Co (59.933 819 u). The half-life of 6027 Co is 5.27 yr. Determine the activity of the radioactive material.
42. M GO A one-gram sample of radium 22488 Ra (atomic mass = 224.020 186 u, T1/2 = 3.66 days) contains 2.69 × 1021 nuclei and undergoes α decay to pro- duce radon 22086 Rn (atomic mass = 220.011 368 u). The atomic mass of an α particle is 4.002 603 u. The latent heat of fusion for water is 33.5 × 104 J/kg. With the energy released in 3.66 days, how many kilograms of ice could be melted at 0 °C?
43. M BIO V-HINT The isotope 19879 Au (atomic mass = 197.968 u) of gold has a half-life of 2.69 days and is used in cancer therapy. What mass (in grams) of this isotope is required to produce an activity of 315 Ci?
44. M GO Outside the nucleus, the neutron itself is radioactive and decays into a proton, an electron, and an antineutrino. The half-life of a neutron (mass = 1.675 × 10−27 kg) outside the nucleus is 10.4 min. On average, over what distance (in meters) would a beam of 5.00-eV neutrons travel before the number of neutrons decreased to 75.0% of its initial value?
45. M SSM Two radioactive nuclei A and B are present in equal numbers to begin with. Three days later, there are three times as many A nuclei as there are B nuclei. The half-life of species B is 1.50 days. Find the half-life of species A.
Section 31.7 Radioactive Dating 46. E A sample has a 146 C activity of 0.0061 Bq per gram of carbon. (a) Find the age of the sample, assuming that the activity per gram of carbon in a liv- ing organism has been constant at a value of 0.23 Bq. (b) Evidence suggests that the value of 0.23 Bq might have been as much as 40% larger. Repeat part (a), taking into account this 40% increase.
47. E SSM Review Multiple-Concept Example 10 for help in approaching this problem. An archaeological specimen containing 9.2 g of carbon has an activity of 1.6 Bq. How old (in years) is the specimen?
48. E CHALK GO The half-life for the α decay of uranium 238 92U is 4.47 × 109 yr. Determine the age (in years) of a rock specimen that contains 60.0% of its original number of 238 92U atoms.
49. E Available in WileyPLUS. 50. E GO Multiple-Concept Example 10 reviews most of the concepts that are needed to solve this problem. Material found with a mummy in the arid highlands of southern Peru has a 146 C activity per gram of carbon that is 78.5% of the activity present initially. How long ago (in years) did this indi- vidual die?
51. M SSM When any radioactive dating method is used, experimental error in the measurement of the sample’s activity leads to error in the estim- ated age. In an application of the radiocarbon dating technique to certain fossils, an activity of 0.100 Bq per gram of carbon is measured to within an accuracy of ±10.0%. Find the age of the fossils and the maximum error (in years) in the value obtained. Assume that there is no error in the 5730-year half-life of 146 C nor in the value of 0.23 Bq per gram of carbon in a living organism.
52. H Available in WileyPLUS.
910 CHAPTER 31 Nuclear Physics and Radioactivity
53. E V-HINT Available in WileyPLUS. 54. E GO In a nucleus, each proton experiences a repulsive electrostatic force from each of the other protons. In a nucleus of gold 19779 Au, what is the magnitude of the least possible electrostatic force of repulsion that one pro- ton can exert on another?
55. E V-HINT When a sample from a meteorite is analyzed, it is determined that 93.8% of the original mass of a certain radioactive isotope is still present. Based on this fi nding, the age of the meteorite is calculated to be 4.51 × 109 yr. What is the half-life (in yr) of the isotope used to date the meteorite?
56. E GO The β− decay of phosphorus 3215 P (atomic mass = 31.973 907 u) produces a daughter nucleus that is sulfur 3216 S (atomic mass = 31.972 070 u), a β− particle, and an antineutrino. The kinetic energy of the β− particle is 0.90 MeV. Find the maximum possible energy (in MeV) that the antineutrino could carry away.
57. E Complete the following decay processes by stating what the symbol X represents (X = α, β−, β+, or 𝛾): (a) 21182 Pb → 21183 Bi + X (c) 23190 Th* → 23190 Th + X (b) 116 C → 115 B + X (d) 21084 Po → 20682 Pb + X
58. M MMH Available in WileyPLUS. 59. M SSM Available in WileyPLUS. 60. M V-HINT A sample of ore containing radioactive strontium 9038 Sr has an activity of 6.0 × 105 Bq. The atomic mass of strontium is 89.908 u, and its half-life is 29.1 yr. How many grams of strontium are in the sample?
61. M Available in WileyPLUS. 62. M V-HINT In a radioactive decay series similar to that shown in Figure 31.15, thorium 22890 Th (atomic mass = 228.028 715 u) undergoes four suc- cessive α decays, producing a daughter nucleus. (a) Determine the symbol Z A X for the nucleus produced by four successive α decays of 22890 Th. (b) What is the total amount of energy (in MeV) released in this series of α decays? The mass of the daughter nucleus can be obtained by using the result of part (a) and consulting Appendix F at the back of the book. The mass of a single α particle is 4.002 603 u. 63. M GO SSM What is the wavelength (in vacuum) of the 0.186-MeV 𝛾-ray photon emitted by 226 88Ra?
Additional Problems
Radioactive decay obeys the conservation laws of physics, and we have studied fi ve of these. Two of them are particularly important in understanding the types of radioactivity that occur and the nuclear changes that accompany them. These are the conservation of electric charge and the conservation of nucleon number. Problem 64 emphasizes their importance and reviews how they are applied. Problem 65 explores how radioactive decay can be a source of energy in the form of heat.
64. M CHALK Thorium 228 90Th produces a daughter nucleus that is radioactive. The daughter, in turn, produces its own radioactive daughter, and so on. This process continues until bismuth 212 83Bi is reached. Concepts: (i) How many of the 90 protons in the thorium nucleus are carried off by the α particles? (ii) How many protons are left behind when the β− particles are emitted? (iii) How many of the 228 nucleons in the thorium nucleus are carried off by
the α particles? (iv) Does the departure of a β− particle alter the number of nucleons? Calculations: What are the total number Nα of α particles and the total number N𝛽 of β− particles that are generated in this series of radioactive decays?
65. M CHALK SSM A one-gram sample of thorium 22890 Th contains 2.64 × 1021 atoms and undergoes α decay with a half-life of 1.913 yr (1.677 × 104 h). Each disintegration releases an energy of 5.52 MeV (8.83 × 10−13 J). Assume that all of the energy is used to heat a 3.8-kg sample of water. Concepts: (i) How much heat Q is needed to raise the temperature of a mass m of water by ΔT degrees? (ii) The energy released by each disintegration is E. What is the total energy Etotal released by a number n of disintegrations? (iii) What is the number n of disintegrations that occur during a time t? Calculations: Find the change in temperature of the 3.8-kg sample of water that occurs in one hour.
Concepts and Calculations Problems
66. M A Radioisotope Thermoelectric Generator. You and your team are designing a thermoelectric generator that converts the thermal energy released during the decay of a radioactive material into electrical energy. Such devices are used in deep-space probes such as Voyager 1, which was launched in 1977. Its radioisotope thermoelectric generators are expected to function until the year 2025. The isotope that your team will use is 23894 Pu (atomic mass = 238.049553 u), which has a half-life of 87.7 years. (a) If 238 94 Pu undergoes alpha decay, what is the daughter nucleus? (b) Assuming
the daughter nucleus found in (a) has an atomic mass of 234.0409468 u, calculate the energy released in the decay in joules (the atomic weight of an alpha particle is 4.002603 u). (c) How many atoms are in one gram of 23894 Pu? (d) How many atoms in one gram of 23894 Pu decay after one year? (e) How much energy is released from one gram of 23894 Pu during one year? (f) What is the average power output of one gram during one year (in watts)?
67. M Radioactive Dating of a Mystery Object. In a science fi ction movie, a strange object is discovered buried deep in the ice of western Antarctica. It appears to be a radioisotope thermoelectric device from a spacecraft, the function of which is to convert thermal energy released in the decay of its radioactive contents into electrical energy. The radioactive material is iden- tifi ed as americium-241 (24195 Am), which has a half-life of 432 years. (a) If 241 95 Am undergoes alpha decay, what is its daughter nucleus? (b) What is the
activity you would expect for 1.00 g of 24195 Am (in Bq)? (c) In the movie, 1.00 g of material is extracted from the device, and the activity is measured to be 4.00 × 1010 Bq. Assuming the device was initially loaded with 100% 24195 Am, how old is the device? Express your answer in years.
Team Problems
LEARNING OBJECTIVES
Aft er reading this module, you should be able to...
32.1 Calculate biological eff ects of ionizing radiation.
32.2 Apply nuclear conservation laws to complete induced nuclear reactions.
32.3 Calculate the energy released in nuclear fission reactions.
32.4 Describe the basic components of nuclear reactors.
32.5 Calculate the energy released in nuclear fusion reactions.
32.6 Describe elementary particle theories leading to the standard model.
32.7 Use Hubble’s law to explain the age and size of the universe.
V A
L E
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CHAPTER 32
Ionizing Radiation, Nuclear Energy, and Elementary Particles
Elementary particles are the basic building blocks for all matter. They are studied by accelerating particles
such as protons to high speeds and crashing them together. The Large Hadron Collider is designed to do
just such a job. It consists of a large underground ring (diameter 8.6 km or 5.3 mi) and associated facilities
located beneath parts of France and Switzerland. High-speed protons travel in opposite directions in the
ring, and the elementary particles that result from the collisions between them are observed using specialized
detectors. This photograph shows the Compact Muon Solenoid detector for the Large Hadron Collider.
32.1 Biological Eff ects of Ionizing Radiation
BIO THE PHYSICS OF . . . the biological eff ects of ionizing radiation. Ionizing radiation consists of photons and/or moving particles that have suffi cient energy to knock an electron out of an atom or molecule, thus forming an ion. The
photons usually lie in the ultraviolet, X-ray, or 𝛾-ray regions of the electromagnetic spectrum (see Figure 24.9), whereas the moving particles can be the 𝛼 and 𝛽 particles emitted during radioactive decay. An energy of roughly 1 to 35 eV is needed to ionize
an atom or molecule, and the particles and 𝛾 rays emitted during nuclear disintegration often have energies of several million eV. Therefore, a single 𝛼 particle, 𝛽 particle, or 𝛾 ray can ionize thousands of molecules.
Nuclear radiation is potentially harmful to humans because the ionization it produces
can signifi cantly alter the structure of molecules within a living cell. The alterations can 911
912 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
lead to the death of the cell and even of the organism itself. Despite the potential hazards, however,
ionizing radiation is used in medicine for diagnostic and therapeutic purposes, such as locating
bone fractures and treating cancer. The hazards can be minimized only if the fundamentals of
radiation exposure, including dose units and the biological eff ects of radiation, are understood.
Exposure is a measure of the ionization produced in air by X-rays or 𝛾 rays, and it is defi ned in the following manner: A beam of X-rays or 𝛾 rays is sent through a mass m of dry air at stan- dard temperature and pressure (STP: 0 °C, 1 atm pressure). In passing through the air, the beam
produces positive ions whose total charge is q. Exposure is defi ned as the total charge per unit mass of air: exposure = q/m. The SI unit for exposure is coulombs per kilogram (C/kg). How- ever, the fi rst radiation unit to be defi ned was the roentgen (R), and it is still used today. With q expressed in coulombs (C) and m in kilograms (kg), the exposure in roentgens is given by
Exposure (in roentgens) = ( 12.58 × 10−4) q m (32.1)
Thus, when X-rays or 𝛾 rays produce an exposure of one roentgen, q = 2.58 × 10−4 C of positive charge are produced in m = 1 kg of dry air:
1R = 2.58 × 10−4 C/kg (dry air, at STP)
Since the concept of exposure is defi ned in terms of the ionizing abilities of X-rays and
𝛾 rays in air, it does not specify the eff ect of radiation on living tissue. For biological purposes, the absorbed dose is a more suitable quantity because it is the energy absorbed from the radiation per unit mass of absorbing material:
Absorbed dose = Energy absorbed
Mass of absorbing material (32.2)
The SI unit of absorbed dose is the gray (Gy), which is the unit of energy divided by the unit of mass: 1 Gy = 1 J/kg. Equation 32.2 is applicable to all types of radiation and absorbing media.
Another unit is often used for absorbed dose—namely, the rad (sometimes abbreviated rd). The word “rad” is an acronym for radiation absorbed dose. The rad and the gray are related by
1 rad = 0.01 gray
Example 1 deals with the gray and the rad as units for the absorbed dose.
Analyzing Multiple-Concept Problems
EXAMPLE 1 Absorbed Dose of 𝛾 Rays
Figure 32.1 shows 𝛾 rays being absorbed by water. What is the absorbed dose (in rads) of 𝛾 rays that will heat the water from 20.0 to 50.0 °C?
Reasoning When 𝛾 rays are absorbed by the water, they cause it to heat up. The absorbed dose of 𝛾 rays is the energy (heat) absorbed by the water divided by its mass. According to the discussion in Section 12.7, the heat
that must be absorbed by the water in order for its temperature to increase
by a given amount depends on the mass and specifi c heat capacity of the
water. We will use the concept of specifi c heat capacity to evaluate the
absorbed dose of 𝛾 rays.
Knowns and Unknowns The following table summarizes the given information:
Thermometer
raysγ
FIGURE 32.1 When the water absorbs the 𝛾 rays, its temperature rises.
Description Symbol Value Initial temperature of water T0 20.0 °C
Final temperature of water T 50.0 °C
Unknown Variable Absorbed dose of 𝛾 rays (in rads) Absorbed dose ?
32.1 Biological Eff ects of Ionizing Radiation 913
The amount of biological damage produced by ionizing radiation is diff erent for diff erent
kinds of radiation. For instance, a 1-rad dose of neutrons is far more likely to produce eye cata-
racts than a 1-rad dose of X-rays. To compare the damage caused by diff erent types of radiation,
the relative biological eff ectiveness (RBE) is used.* The relative biological eff ectiveness of a particular type of radiation is the ratio of the dose of 200-keV X-rays needed to produce a certain
biological eff ect to the dose of the radiation needed to produce the same biological eff ect:
Relative biological
eff ectiveness (RBE) =
The dose of 200-keV X-rays that
produces a certain biological effect
The dose of radiation that
produces the same biological effect
(32.3)
The RBE depends on the nature of the ionizing radiation and its energy, as well as on the
type of tissue being irradiated. Table 32.1 lists some typical RBE values for diff erent kinds of radiation, assuming that an “average” biological tissue is being irradiated. A value of RBE = 1
for 𝛾 rays and 𝛽− particles indicates that they produce the same biological damage as do 200-keV X-rays. The larger RBE values for protons, 𝛼 particles, and neutrons indicate that they cause sub- stantially more damage. The RBE is often used in conjunction with the absorbed dose to refl ect
the damage-producing character of the radiation. The product of the absorbed dose in rads (not in
grays) and the RBE is the biologically equivalent dose:
Biologically equivalent dose
(in rems) =
Absorbed dose
(in rads) × RBE (32.4)
The unit for the biologically equivalent dose is the rem, short for roentgen equivalent, man. Example 2 illustrates the use of the biologically equivalent dose.
Modeling the Problem
STEP 1 Absorbed Dose The absorbed dose of 𝛾 rays is the energy (heat) Q absorbed by the water divided by its mass m (see Equation 32.2), as indicated in the right column. Neither Q nor m is known. Both variables will be dealt with in Step 2.
STEP 2 Heat Needed to Increase the Temperature of the Water The heat Q that is needed to increase the temperature of a mass m of water by an amount ΔT is Q = cm ΔT (Equation 12.4), where c is the specifi c heat capacity of water. The change in temperature ΔT is equal to the higher temperature T minus the lower temperature T0, or ΔT = T − T0. Thus, the heat can be expressed as
Q = cm ∆T = cm (T − T0) (12.4)
This expression for the heat absorbed by the water can be substituted into Equation 32.2 for the
absorbed dose, as indicated in the right column. Note that the mass m of the water appears in both the numerator and denominator, so it can be eliminated algebraically.
Solution Algebraically combining the results of the two modeling steps gives
Absorbed dose = Q m
= cm (T − T0)
m = c(T − T0)
Taking the specifi c heat capacity c of water from Table 12.2, we fi nd that the absorbed dose of 𝛾 rays [expressed in grays (Gy)] is
Absorbed dose = c(T − T0) = [4186 J/ (kg · C°)](50.0 °C − 20.0 °C) = 1.26 × 105 Gy
The problem asks that the absorbed dose be expressed in rads, rather than in grays. To this end,
we note that 1 rad = 0.01 Gy, so
Absorbed dose = (1.26 × 10 5 Gy )( 1 rad 0.01 Gy ) = 1.26 × 107 rad Related Homework: Problems 7, 10, 50
STEP 1 STEP 2
Absorbed dose = Q m
(32.2)
?
Absorbed dose = Q m
(32.2)
Q = cm (T − T0) (12.4)
*The RBE is sometimes called the quality factor (QF).
TABLE 32.1
Relative Biological Effectiveness (RBE) for Various Types of Radiation
Type of Radiation RBE 200-keV X-rays 1
𝛾 rays 1
𝛽− particles (electrons) 1
Protons 10
𝛼 particles 10–20
Neutrons
Slow 2
Fast 10
914 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
Everyone is continually exposed to background radiation from natural sources, such as
cosmic rays (high-energy particles that come from outside the solar system), radioactive materials
in the environment, radioactive nuclei (primarily carbon 146C and potassium 40 19 K) within our own
bodies, and radon. Table 32.2 lists the average biologically equivalent doses received from these sources by a citizen in the United States. According to this table, radon is a major contributor to
the natural background radiation. Radon is an odorless radioactive gas and poses a health hazard
because, when inhaled, it can damage the lungs and cause cancer. Radon is found in soil and
rocks and enters houses via a mechanism that is not well understood. One possibility for indoor
radon entry is through cracks and crevices in the foundation. The amount of radon in the soil
varies greatly throughout the country, with some localities having signifi cant amounts and others
having virtually none. Accordingly, the dose that any individual receives can vary widely from
the average value of 207 mrem/yr given in Table 32.2 (1 mrem = 10−3 rem). In many houses, the entry of radon can be reduced signifi cantly by sealing the foundation against entry of the gas and
providing good ventilation so it does not accumulate.
To the natural background of radiation, a signifi cant amount of human-made radiation has
been added, mostly from medically related sources. Among these sources, CAT scanning (see
Section 30.7) is the major contributor, as Table 32.2 indicates. The eff ects of radiation on humans can be grouped into two categories, according to the time
span between initial exposure and the appearance of physiological symptoms: (1) short-term or
acute eff ects that appear within a matter of minutes, days, or weeks, and (2) long-term or latent
eff ects that appear years, decades, or even generations later.
Radiation sickness is the general term applied to the acute eff ects of radiation. Depending on the severity of the dose, a person with radiation sickness can exhibit nausea, vomiting, fever,
diarrhea, and loss of hair. Ultimately, death can occur. The severity of radiation sickness is related
to the dose received, and in the following discussion the biologically equivalent doses quoted
are whole-body, single doses. A dose less than 50 rem causes no short-term ill eff ects. A dose
between 50 and 300 rem brings on radiation sickness, the severity increasing with increasing
dosage. A whole-body dose in the range of 400–500 rem is classifi ed as an LD50 dose, meaning
that it is a lethal dose (LD) for about 50% of the people so exposed; death occurs within a few
months. Whole-body doses greater than 600 rem result in death for almost all individuals.
Long-term or latent eff ects of radiation may appear as a result of high-level brief exposure or
low-level exposure over a long period of time. Some long-term eff ects are hair loss, eye cataracts,
and various kinds of cancer. In addition, genetic defects caused by mutated genes may be passed
on from one generation to the next.
Because of the hazards of radiation, the federal government has established dose limits. The
permissible dose for an individual is defi ned as the dose, accumulated over a long period of time
or resulting from a single exposure, that carries negligible probability of a severe health hazard.
Federal standards (1991) state that an individual in the general population should not receive
more than 500 mrem of human-made radiation each year, exclusive of medical sources. A person exposed to radiation in the workplace (e.g., a radiation therapist) should not receive more than
5 rem per year from work-related sources.
EXAMPLE 2 Comparing Absorbed Doses of 𝛾 Rays and Neutrons
A biological tissue is irradiated with 𝛾 rays that have an RBE of 0.70. The absorbed dose of 𝛾 rays is 850 rad. The tissue is then exposed to neutrons whose RBE is 3.5. The biologically equivalent dose of the neutrons is the
same as that of the 𝛾 rays. What is the absorbed dose of neutrons?
Reasoning The biologically equivalent doses of the neutrons and the 𝛾 rays are the same. Therefore, the tissue damage produced in each case is the same. However, the RBE of the neutrons is larger than the RBE of
the 𝛾 rays by a factor of 3.5/0.70 = 5.0. Consequently, we will fi nd that the absorbed dose of the neutrons is only one-fi fth as great as that of the 𝛾 rays.
Solution According to Equation 32.4, the biologically equivalent dose is the product of the absorbed dose (in rads) and the RBE; it is the same
for the 𝛾 rays and the neutrons. Therefore, we have
Biologically
equivalent dose = (Absorbed dose)γ rays RBEγ rays
= (Absorbed dose)neutrons RBEneutrons
Solving for the absorbed dose of the neutrons gives
(Absorbed dose)neutrons = (Absorbed dose)γ rays ( RBEγ rays
RBE neutrons) = (850 rad) (0.703.5 ) = 170 rad
TABLE 32.2
Average Biologically Equivalent Doses of Radiation Received by a U. S. Citizena
Source of Radiation
Biologically Equivalent Dose (mrem/yr)b
Natural background radiation Cosmic rays 33
Radioactive earth
and air
21
Internal radioactive
nuclei
29
Inhaled radon 207
Human-made radiation Consumer products 13
CAT scanning 147
Routine medical/
dental diagnostics
33
Nuclear medicine 74
aNational Council on Radiation Protection and
Measurements, Report No. 160, “Ionizing Radiation
Exposure of the Population of the United States,” 2009. b1 mrem = 10−3 rem.
32.2 Induced Nuclear Reactions 915
Check Your Understanding
(The answers are given at the end of the book.) 1. Two diff erent types of radiation have the same RBE. Is it possible for these two types of radiation to
deliver diff erent biologically equivalent doses of radiation to a given tissue sample?
2. The damage-producing character of a given type of ionizing radiation depends on (a) only the RBE of the radiation, (b) only the absorbed dose of the radiation, (c) both the RBE and the absorbed dose of the radiation.
3. A person faces the possibility of receiving the following absorbed doses of ionizing radiation: 20 rad of 𝛾 rays (RBE = 1), 5 rad of neutrons (RBE = 10), and 2 rad of 𝛼 particles (RBE = 20). Rank the amount of biological damage that these possibilities will cause in decreasing order (greatest damage fi rst).
32.2 Induced Nuclear Reactions Section 31.4 discusses how a radioactive parent nucleus disintegrates spontaneously into a daugh-
ter nucleus. It is also possible to bring about, or induce, the disintegration of a stable nucleus by
striking it with another nucleus, an atomic or subatomic particle, or a 𝛾-ray photon. A nuclear reaction is said to occur whenever an incident nucleus, particle, or photon causes a change to occur in a target nucleus.
In 1919, Ernest Rutherford observed that when an 𝛼 particle strikes a nitrogen nucleus, an oxygen nucleus and a proton are produced. This nuclear reaction is written as
2 4 He + 7
14 N 178O + 1 1 H
Because the incident 𝛼 particle induces the transmutation of nitrogen into oxygen, this reaction is an example of an induced nuclear transmutation.
Nuclear reactions are often written in a shorthand form. For example, the reaction above
is designated by 147N (𝛼, p) 178O. The fi rst and last symbols represent the initial and fi nal nuclei, respectively. The symbols within the parentheses denote the incident 𝛼 particle (on the left) and the small emitted particle or proton p (on the right). Some other induced nuclear transmutations are listed below, together with the equivalent shorthand notations:
Nuclear Reaction Notation 1 0 n +
10 5 B →
7 3 Li +
4 2 He
10 5B (n, α) 73 Li
γ + 2512 Mg → 2411 Na + 11 H 1225 Mg (γ, p) 1124 Na
1 1 H + 13 6 C → 7
14 N + γ 613C ( p, γ) 714 N
Induced nuclear reactions, like the radioactive decay process discussed in Section 31.4, obey
the conservation laws of physics. Each of these laws deals with a property that does not change
during a process. The following list shows the property with which each law deals:
1. Conservation of energy/mass (Sections 6.8 and 28.6) 2. Conservation of linear momentum (Section 7.2) 3. Conservation of angular momentum (Section 9.6) 4. Conservation of electric charge (Section 18.2) 5. Conservation of nucleon number (Section 31.4) In particular, items 4 and 5 on this list indicate that both the total electric charge of the nucleons
and the number of nucleons in a nuclear reaction are conserved. The next example illustrates
how the conservation of total electric charge and number of nucleons can be used to identify the
nucleus produced in a reaction.
⏟⏟⏟ Oxygen
⏟⏟⏟ Proton, p
⏟⏟⏟ Nitrogen
(target)
⏟⏟⏟ Incident
𝛼 particle
916 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
Induced nuclear transmutations can be used to produce isotopes that are not found naturally.
In 1934, Enrico Fermi (1901–1954) suggested a method for producing elements with a higher
atomic number than uranium (Z = 92). These elements—neptunium (Z = 93), plutonium (Z = 94), americium (Z = 95), and so on—are known as transuranium elements, and none occurs natu- rally. They are created in a nuclear reaction between a suitably chosen lighter element and a small
incident particle, usually a neutron or an 𝛼 particle. For example, Figure 32.2 shows a reaction that produces plutonium from uranium. A neutron is captured by a uranium 92
239 U nucleus, produc-
ing 92 239 U and a 𝛾 ray. The 92239 U nucleus is radioactive and decays with a half-life of 23.5 min into
neptunium 93 239 Np. Neptunium is also radioactive and disintegrates with a half-life of 2.4 days into
plutonium 94 239 Pu. Plutonium is the fi nal product and has a half-life of 24 100 yr.
The neutrons that participate in nuclear reactions can have kinetic energies that cover a wide
range. In particular, those that have a kinetic energy of about 0.04 eV or less are called thermal neutrons. The name derives from the fact that such a relatively small kinetic energy is compa- rable to the average translational kinetic energy of a molecule in an ideal gas at room temperature.
Check Your Understanding
(The answers are given at the end of the book.) 4. Which one or more of the following nuclear reactions could possibly occur? (a) 157N (𝛼, 𝛾) 189 F.
(b) 146 C (p, n) 158 O (c) 147N (p, 𝛾) 158O (d) 158O (n, p) 136C 5. Why is each of the following reactions not allowed? (a) 6028 Ni (𝛼, p) 6229 Cu (b) 2713Al (n, n) 2813Al
(c) 3919 K (p, 𝛼) 3617 Cl
32.3 Nuclear Fission In 1939 four German scientists, Otto Hahn, Lise Meitner, Fritz Strassmann, and Otto Frisch, made
an important discovery that ushered in the atomic age. They found that a uranium nucleus, after
absorbing a neutron, splits into two fragments, each with a smaller mass than the original nucleus.
The splitting of a massive nucleus into two less massive fragments is known as nuclear fi ssion. Animated Figure 32.3 shows a fi ssion reaction in which a uranium 92235 U nucleus is split into
barium 14156Ba and krypton 92 36Kr nuclei. The reaction begins when 92
235 U absorbs a slowly moving
neutron, creating a “compound nucleus,” 92 236 U. The compound nucleus disintegrates quickly into
141 56Ba,
92 36Kr, and three neutrons according to the following reaction:
0 1 n + 92
235 U 92 236 U 56
141 Ba + 36 92 Kr + 310 n
Compound
nucleus
(unstable)
⏟⏟⏟ ⏟⏟⏟ Barium
⏟⏟⏟ Krypton
⏟⏟⏟ 3 neutrons
EXAMPLE 3 An Induced Nuclear Transmutation
An 𝛼 particle strikes an aluminum 2713 Al nucleus. As a result, an unknown nucleus Z
A X and a neutron 1 0 n are produced:
2 4 He + 2713Al
A Z X + 0
1 n
Identify the nucleus produced, including its atomic number Z (the number of protons) and its atomic mass number A (the number of nucleons).
Reasoning The total electric charge of the nucleons is conserved, so that we can set the total number of protons before the reaction equal to
the total number after the reaction. The total number of nucleons is also
conserved, so that we can set the total number before the reaction equal
to the total number after the reaction. These two conserved quantities will
allow us to identify the nucleus ZA X.
Solution The conservation of total electric charge and total number of nucleons leads to the equations listed below:
Conserved Quantity Before
Reaction After
Reaction Total electric charge (number of protons) 2 + 13 = Z + 0
Total number of nucleons 4 + 27 = A + 1
Solving these equations for Z and A gives Z = 15 and A = 30. Since Z = 15 identifi es the element as phosphorus (P), the nucleus produced is 15
30 P .
–
U23892 U 239
92
Np23993 e0–1
n10
Pu23994
+ +
+ +
–
e0–1
+ +
23.5 min
2.4 days
γ
γ
γ
FIGURE 32.2 An induced nuclear reaction is shown in which 23892 U is transmuted into the
transuranium element plutonium 23994 Pu.
32.3 Nuclear Fission 917
This reaction is only one of the many possible reactions that can occur when uranium fi ssions.
For example, another reaction is
0 1 n + 92
235 U 92 236 U 54
140 Xe + 38 94 Sr + 2 10 n
Some reactions produce as many as 5 neutrons; however, the average number produced per
fi ssion is 2.5.
When a neutron collides with and is absorbed by a uranium nucleus, the uranium nucleus
begins to vibrate and becomes distorted. The vibration continues until the distortion becomes so
severe that the attractive strong nuclear force can no longer balance the electrostatic repulsion
between the nuclear protons. At this point, the nucleus bursts apart into fragments, which carry
off energy, primarily in the form of kinetic energy. The energy carried off by the fragments is
enormous and was stored in the original nucleus mainly in the form of electric potential energy.
An average of roughly 200 MeV of energy is released per fi ssion. This energy is approximately
108 times greater than the energy released per molecule in an ordinary chemical reaction, such as
the combustion of gasoline or coal. Example 4 demonstrates how to estimate the energy released
during the fi ssion of a nucleus.
Compound
nucleus
(unstable)
⏟⏟⏟ ⏟⏟⏟ Xenon
⏟⏟⏟ Strontium
⏟⏟⏟ 2 neutrons
+ n10
Ba14156
Kr9236
U23692
U23592
n10
n10
n10
Compound nucleus
ANIMATED FIGURE 32.3 A slowly moving neutron causes the uranium nucleus 23592U to
fi ssion into barium 14156Ba, krypton 92 36 Kr, and
three neutrons.
EXAMPLE 4 The Energy Released During Nuclear Fission
Estimate the amount of energy released when a massive nucleus (A = 240) fi ssions.
Reasoning Figure 31.5 shows that the binding energy of a nucleus with A = 240 is about 7.6 MeV per nucleon. We assume that this nucleus fi ssions into two fragments, each with A ≈ 120. According to Figure 31.5, the binding energy of the fragments increases to about
8.5 MeV per nucleon. Consequently, when a massive nucleus fi ssions,
there is a release of about 8.5 MeV − 7.6 MeV = 0.9 MeV of energy
per nucleon.
Solution Since there are 240 nucleons involved in the fi ssion process, the total energy released per fi ssion is approximately (0.9 MeV/nucleon)
(240 nucleons) ≈ 200 MeV .
Virtually all naturally occurring uranium is composed of two isotopes. These isotopes and
their natural abundances are 92 238 U (99.275%) and 92
235 U (0.720%). Although 92 238 U is by far the most
abundant isotope, the probability that it will capture a neutron and fi ssion is very small. For this
reason, 92 238 U is not the isotope of choice for generating nuclear energy. In contrast, the isotope 92
235 U
readily captures a neutron and fi ssions, provided the neutron is a thermal neutron (kinetic energy) ≈ 0.04 eV or less). The probability of a thermal neutron causing 92
235 U to fi ssion is about 500 times
greater than the probability for a neutron whose energy is relatively high—say, 1 MeV. Thermal
neutrons can also be used to fi ssion other nuclei, such as plutonium 94 239 Pu. Conceptual Example 5
deals with one of the reasons why thermal neutrons are useful for inducing nuclear fi ssion.
918 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
CONCEPTUAL EXAMPLE 5 Neutrons Versus Protons or Alpha Particles
A thermal neutron has a relatively small amount of kinetic energy but,
nevertheless, can penetrate a nucleus. To penetrate the same nucleus, would
a proton or an 𝛼 particle need (a) the same small amount of kinetic energy as the neutron needs, (b) a much larger amount of kinetic energy than the neutron needs, or (c) much less kinetic energy than the neutron needs?
Reasoning To penetrate a nucleus, a particle such as a neutron, a proton, or an 𝛼 particle must have enough kinetic energy to do the work of over- coming any repulsive force that it encounters. A repulsive force can arise
because protons in the nucleus are electrically charged. Since a neutron is
electrically neutral, however, it encounters no electrostatic force of repul-
sion as it approaches the nuclear protons, and, hence, needs relatively
little energy to reach the nucleus.
Answers (a) and (c) are incorrect. A proton and an 𝛼 particle each carry a positive charge, so that each would encounter an electrostatic
force of repulsion as it approached the nuclear protons, a force that a
thermal neutron does not encounter. These answers ignore the additional
kinetic energy that a proton or an 𝛼 particle would need to overcome the repulsion.
Answer (b) is correct. A proton and an 𝛼 particle, each being positively charged, would each require much more kinetic energy than a neutron
does, in order to overcome the electrostatic force of repulsion from the
nuclear protons. It is true that each would also experience the attractive
strong nuclear force from the nuclear protons and neutrons. However,
this force has an extremely short range of action and, therefore, would
come into play only after an impinging particle reached the target nucleus.
In comparison, the electrostatic force has a long range of action and is
encountered throughout the entire journey to the target.
Related Homework: Problem 45
The fact that the uranium fi ssion reaction releases 2.5 neutrons, on the average, makes it
possible for a self-sustaining series of fi ssions to occur. As Figure 32.4 illustrates, each neutron released can initiate another fi ssion event, resulting in the emission of still more neutrons, fol-
lowed by more fi ssions, and so on. A chain reaction is a series of nuclear fi ssions whereby some of the neutrons produced by each fi ssion cause additional fi ssions. During an uncontrolled chain
reaction, it would not be unusual for the number of fi ssions to increase a thousandfold within a
few millionths of a second. With an average energy of about 200 MeV being released per fi ssion,
an uncontrolled chain reaction can generate an incredible amount of energy in a very short time,
as happens in an atomic bomb (which is actually a nuclear bomb). By using a material that can absorb neutrons without fi ssioning, it is possible to limit the
number of neutrons in the environment of the fi ssile nuclei. In this way, a condition can be
established whereby each fi ssion event contributes, on average, only one neutron that fi ssions another nucleus (see Figure 32.5). Thus, the chain reaction and the rate of energy production are controlled. The controlled-fi ssion chain reaction is the principle behind nuclear reactors used in
the commercial generation of electric power.
U23592
n10
Legend
FIGURE 32.4 A chain reaction. For clarity, it is assumed that each fi ssion generates two
neutrons (2.5 neutrons are actually liberated
on the average). The fi ssion fragments are not
shown.
U23592
n10
Legend (Lost
neutron)
(Lost neutron)
(Lost neutron)
FIGURE 32.5 In a controlled chain reaction, only one neutron, on average, from each fi ssion
event causes another nucleus to fi ssion. The
“lost neutron” is absorbed by a material (not
shown) that does not fi ssion. As a result,
energy is released at a steady or controlled rate.
32.4 Nuclear Reactors 919
Check Your Understanding
(The answers are given at the end of the book.) 6. When the nucleus of a certain element absorbs a thermal neutron, fi ssion usually occurs, with the
production of nuclear fragments and a number N of neutrons. However, in a collection of atoms of this element, a small fraction of the thermal neutrons absorbed by the nuclei does not lead to fi ssion. For
which one of the following values of N can a self-sustaining chain reaction not be produced using this element? (a) N = 4 (b) N = 3 (c) N = 2 (d) N = 1
7. Thermal neutrons, thermal protons, and thermal electrons all have the same kinetic energy of about 0.04 eV. Rank the speeds of these particles in descending order (greatest speed fi rst).
8. Would a release of energy accompany the fi ssion of a nucleus of nucleon number 25 into two fragments of about equal mass? Consult Figure 31.5 as needed.
32.4 Nuclear Reactors THE PHYSICS OF . . . nuclear reactors. A nuclear reactor is a type of furnace in which energy is generated by a controlled-fi ssion chain reaction. The fi rst nuclear reactor was built by
Enrico Fermi in 1942, on the fl oor of a squash court under the west stands of Stagg Field at the
University of Chicago. Today, there are a number of kinds and sizes of reactors, and many have
the same three basic components: fuel elements, a neutron moderator, and control rods. Interactive Figure 32.6 illustrates these components.
The fuel elements contain the fi ssile fuel and, for example, may be thin rods about 1 cm in diameter. In a large power reactor there may be thousands of fuel elements placed close together,
and the entire region of fuel elements is known as the reactor core. Uranium 92235 U is a common reactor fuel. Since the natural abundance of this isotope is only about 0.7%, there are special
uranium-enrichment plants to increase the percentage. Most commercial reactors use uranium in
which the amount of 92 235 U has been enriched to about 3%.
Whereas neutrons with energies of about 0.04 eV (or less) readily fi ssion 92 235 U, the neutrons
released during the fi ssion process have signifi cantly greater energies of several MeV or so. Con-
sequently, a nuclear reactor must contain some type of material that will decrease or moderate the
speed of such energetic neutrons so they can readily fi ssion additional 92 235 U nuclei. The material that
slows down the neutrons is called a moderator. One commonly used moderator is water. When an energetic neutron leaves a fuel element, the neutron enters the surrounding water and collides with
water molecules. With each collision, the neutron loses an appreciable fraction of its energy and
slows down. Once slowed down to thermal energy by the moderator, a process that takes less than
10−3 s, the neutron is capable of initiating a fi ssion event upon reentering a fuel element.
If the output power from a reactor is to remain constant, only one neutron from each fi ssion
event must trigger a new fi ssion, as Figure 32.5 illustrates. When each fi ssion leads to one addi- tional fi ssion—no more or no less—the reactor is said to be critical. A reactor normally operates in a critical condition, because then it produces a steady output of energy. The reactor is subcriti- cal when, on average, the neutrons from each fi ssion trigger less than one subsequent fi ssion. In a subcritical reactor, the chain reaction is not self-sustaining and eventually dies out. When the
neutrons from each fi ssion trigger more than one additional fi ssion, the reactor is supercritical. During a supercritical condition, the energy released by a reactor increases. If left unchecked, the
increasing energy can lead to a partial or total meltdown of the reactor core, with the possible
release of radioactive material into the environment.
Clearly, a control mechanism is needed to keep the reactor in its normal, or critical, state.
This control is accomplished by a number of control rods that can be moved into and out of the reactor core (see Interactive Figure 32.6). The control rods contain an element, such as boron or cadmium, that readily absorbs neutrons without fi ssioning. If the reactor becomes supercritical,
the control rods are automatically moved farther into the core to absorb the excess neutrons caus-
ing the condition. In response, the reactor returns to its critical state. Conversely, if the reactor
becomes subcritical, the control rods are partially withdrawn from the core. Fewer neutrons are
absorbed, more neutrons are available for fi ssion, and the reactor again returns to its critical state.
Reactor core
Movable control rods
Hotter water out
Fuel elements
Cooler water
in Moderator
(water)
INTERACTIVE FIGURE 32.6 A nuclear reactor consists of fuel elements, control
rods, and a moderator (in this case, water).
920 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
Interactive Figure 32.7 illustrates a pressurized water reactor. In such a reactor, the heat generated within the fuel rods is carried away by water that surrounds the rods. To remove as
much heat as possible, the water temperature is allowed to rise to a high value (about 300 °C).
To prevent boiling, which occurs at 100 °C at 1 atmosphere of pressure, the water is pressurized
in excess of 150 atmospheres. The hot water is pumped through a heat exchanger, where heat is
transferred to water fl owing in a second, closed system. The heat transferred to the second system
produces steam that drives a turbine. The turbine is coupled to an electric generator, whose output
electric power is delivered to consumers via high-voltage transmission lines. After exiting the
turbine, the steam is condensed back into water that is returned to the heat exchanger.
32.5 Nuclear Fusion In Example 4 in Section 32.3, the plot of binding energy per nucleon in Figure 31.5 is used to
estimate the amount of energy released in the fi ssion process. As summarized in Figure 32.8, the massive nuclei at the right end of the curve have a binding energy of about 7.6 MeV per nucleon.
The less massive fi ssion fragments are near the center of the curve and have a binding energy of
approximately 8.5 MeV per nucleon. The energy released per nucleon by fi ssion is the diff erence
between these two values, or about 0.9 MeV per nucleon.
A glance at the far left end of the diagram in Figure 32.8 suggests another means of gener- ating energy. Two nuclei with very low mass and relatively small binding energies per nucleon
could be combined or “fused” into a single, more massive nucleus that has a greater binding
energy per nucleon. This process is called nuclear fusion. A substantial amount of energy can be released during a fusion reaction, as Example 6 shows for one possible reaction.
Pump
Water
Heat exchanger
Water out
Cool steam out
Turbine
Hot steam in
Electric generator
Condenser
Pump
Reactor
Pressurized water
INTERACTIVE FIGURE 32.7 Diagram of a nuclear power plant that uses a pressurized water reactor.
10
8
6
4
2
0
10
8
6
4
2
0
B in
di ng
e ne
rg y
pe r
nu cl
eo n,
M eV
0 50
Fusion Fission
100 150 200 250
Nucleon number A
FIGURE 32.8 When fi ssion occurs, a massive nucleus divides into two fragments whose binding energy per nucleon is greater than that of the original nucleus. When fusion occurs, two low-mass nuclei combine to
form a more massive nucleus whose binding energy per nucleon is greater than that of the original nuclei.
32.5 Nuclear Fusion 921
Because fusion reactions release so much energy, there is considerable interest in fusion
reactors, although to date no commercial units have been constructed. The diffi culties in building
a fusion reactor arise mainly because the two low-mass nuclei must be brought suffi ciently near
each other so that the short-range strong nuclear force can pull them together, leading to fusion.
However, each nucleus has a positive charge and repels the other electrically. For the nuclei to get
suffi ciently close in the presence of the repulsive electric force, they must have large kinetic ener-
gies, and hence large temperatures, to start with. For example, a temperature of around a hundred
million °C is needed to start the deuterium–tritium reaction discussed in Example 6.
Reactions that require such extremely high temperatures are called thermonuclear reactions. The most important thermonuclear reactions occur in stars, such as our own sun. The energy radi-
ated by the sun comes from deep within its core, where the temperature is high enough to initiate
the fusion process. One group of reactions thought to occur in the sun is the proton–proton cycle, which is a series of reactions whereby six protons form a helium nucleus, two positrons, two
𝛾 rays, two protons, and two neutrinos. The energy released by the proton–proton cycle is about 25 MeV (see Problem 38).
Human-made fusion reactions have been carried out in a fusion-type nuclear bomb—
commonly called a hydrogen bomb. In a hydrogen bomb, the fusion reaction is ignited by a fi s-
sion bomb using uranium or plutonium. The temperature produced by the fi ssion bomb is suffi -
ciently high to initiate a thermonuclear reaction where, for example, hydrogen isotopes are fused
into helium, releasing even more energy. For fusion to be useful as a commercial energy source,
the energy must be released in a steady, controlled manner—unlike the energy in a bomb. To
date, scientists have not succeeded in constructing a fusion device that produces more energy on
a continual basis than is expended in operating the device. A fusion device uses a high tempera-
ture to start a reaction, and under such a condition, all the atoms are completely ionized to form a
plasma (a gas composed of charged particles, like 21 H+ and e−). The problem is to confi ne the hot plasma for a long enough time so that collisions among the ions can lead to fusion.
Neutron n
Energy
Fusion
Helium He nucleus
2 4
0 1
Tritium H nucleus
(contains two neutrons)
1 3Deuterium H
nucleus (contains one
neutron)
1 2
Proton Neutron
FIGURE 32.9 Deuterium and tritium are fused together to form a helium nucleus (42 He).
The result is the release of an enormous
amount of energy, mainly carried by a single
high-energy neutron (10n).
EXAMPLE 6 The Energy Released During Nuclear Fusion
Two isotopes of hydrogen, 21 H (deuterium, D) and 3 1 H (tritium, T), fuse to
form 42He and a neutron according to the following reaction:
2 1H +
3 1H
4 2He +
1 0 n
Determine the energy that is released by this particular fusion reaction,
which is illustrated in Figure 32.9.
Reasoning Energy is released, so the total mass of the fi nal nuclei is less than the total mass of the initial nuclei. To determine the energy
released, we fi nd the amount (in atomic mass units u) by which the
total mass has decreased. Then, we use the fact that 1 u is equivalent to
931.5 MeV of energy, as determined in Section 31.3. This approach is the
same as that used in Section 31.4 for radioactive decay.
Solution The masses of the initial and fi nal nuclei in this reaction, as well as the mass of the neutron, are
Initial Masses Final Masses 2 1H 2.0141 u
4 2He 4.0026 u
3 1H 3.0161 u
1 0n 1.0087 u
Total: 5.0302 u Total: 5.0113 u
The decrease in mass, or the mass defect, is Δm = 5.0302 u − 5.0113 u = 0.0189 u. Since 1 u is equivalent to 931.5 MeV, the energy released is
Released energy = (0.0189 u)(931.5 MeV1 u ) = 17.6 MeV
The deuterium nucleus contains 2 nucleons, and the tritium nucleus
contains 3. Thus, there are 5 nucleons that participate in the fusion, so the
energy released per nucleon is about 3.5 MeV. This energy per nucleon
is greater than the energy released in a fi ssion process (≈0.9 MeV per
nucleon).
922 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
THE PHYSICS OF . . . magnetic confi nement and fusion. One ingenious method of confi ning the plasma is called magnetic confi nement because it uses a magnetic fi eld to contain and compress the charges in the plasma. Charges moving in the magnetic fi eld are subject to
magnetic forces. As the forces increase, the associated pressure builds, and the temperature rises.
The gas becomes a superheated plasma, ultimately fusing when the pressure and temperature are
high enough.
THE PHYSICS OF . . . inertial confi nement and fusion. Another type of confi nement scheme, known as inertial confi nement, is also being developed. Tiny, solid pellets of fuel are dropped into a container. As each pellet reaches the center of the container, a number of high-
intensity laser beams strike the pellet simultaneously. The heating causes the exterior of the pellet to
vaporize almost instantaneously. However, the inertia of the vaporized atoms keeps them from
expanding outward as fast as the vapor is being formed. As a result, high pressures, high densi-
ties, and high temperatures are achieved at the center of the pellet, thus causing fusion. A vari-
ant of inertial confi nement fusion, called “Z pinch,” is under development at Sandia National
Laboratories in New Mexico. This device would also implode tiny fuel pellets, but without using
lasers. Instead, scientists are using a cylindrical array of fi ne tungsten wires that are connected to
a gigantic capacitor. When the capacitor is discharged, a huge current is sent through the wires.
The heated wires vaporize almost instantly, generating a hot gas of ions, or plasma. The plasma
is driven inward upon itself by the huge magnetic fi eld produced by the current. The compressed
plasma becomes superhot and generates a gigantic X-ray pulse. This pulse, it is hoped, would
implode the solid fuel pellets to temperatures and pressures at which fusion would occur.
When compared to fi ssion, fusion has some attractive features as an energy source. As
we have seen in Example 6, fusion yields more energy per nucleon of fuel than fi ssion does.
Moreover, one type of fuel, 21 H (deuterium), is found in the waters of the oceans and is plenti-
ful, cheap, and relatively easy to separate from the common 11H isotope of hydrogen. Fissile
materials like naturally occurring uranium 92 235 U are much less available, and supplies could
be depleted within a century or two. However, the commercial use of fusion to provide cheap
energy remains in the future.
Check Your Understanding
(The answers are given at the end of the book.) 9. Which one or more of the following statements correctly describe diff erences between fi ssion and
fusion? (a) Fission involves the combining of low-mass nuclei to form a more massive nucleus, where- as fusion involves the splitting of a massive nucleus into less massive fragments. (b) Fission involves the splitting of a massive nucleus into less massive fragments, whereas fusion involves the combining
of low-mass nuclei to form a more massive nucleus. (c) More energy per nucleon is released when a fi ssion event occurs than when a fusion event occurs. (d) Less energy per nucleon is released when a fi ssion event occurs than when a fusion event occurs.
10. Which one or more of the following statements concerning fi ssion and fusion are true? (a) Both fi ssion and fusion reactions are characterized by a mass defect. (b) Both fi ssion and fusion reactions always obey the conservation laws of physics. (c) Both fi ssion and fusion take advantage of the fact that the binding energy per nucleon varies with the nucleon number of the nucleus.
11. Would the fusion of two nuclei, each with a nucleon number of 60, release energy? Consult Figure 32.8 as needed.
32.6 Elementary Particles
Setting the Stage By 1932 the electron, the proton, and the neutron had been discovered and were thought to be
nature’s three elementary particles, in the sense that they were the basic building blocks from which all matter is constructed. Experimental evidence obtained since then, however, shows that
several hundred additional particles exist, and scientists no longer believe that the proton and the
neutron are elementary particles.
32.6 Elementary Particles 923
Most of these new particles have masses greater than the electron’s mass, and many are
more massive than protons or neutrons. Most of the new particles are unstable and decay in times
between about 10−6 and 10−23 s.
Often, new particles are produced by accelerating protons or electrons to high energies and
letting them collide with a target nucleus. For example, Figure 32.10 shows a collision between an energetic proton and a stationary proton. If the incoming proton has suffi cient energy, the col-
lision produces an entirely new particle, the neutral pion (𝜋0). The 𝜋0 particle lives for only 8.4 × 10−17 s before it decays into two 𝛾-ray photons. Since the pion did not exist before the collision, it was created from part of the incident proton’s energy. Because a new particle such as the neutral
pion is often created from energy, it is customary to report the mass of the particle in terms of its
equivalent rest energy (see Equation 28.5). Often, energy units of MeV are used. For instance, detailed analyses of experiments reveal that the mass of the 𝜋0 particle is equivalent to a rest energy of 135.0 MeV. For comparison, the more massive proton has a rest energy of 938.3 MeV. Analyses
of experiments also provide the electric charge and other properties of particles created in high-
energy collisions. In the limited space available here, it is not possible to describe all the new par-
ticles that have been found. However, we will highlight some of the more signifi cant discoveries.
Neutrinos In 1930, Wolfgang Pauli suggested that a particle called the neutrino (now known as the “elec- tron neutrino”) should accompany the 𝛽 decay of a radioactive nucleus. As Section 31.5 dis- cusses, the neutrino has no electric charge, has a very small mass (a tiny fraction of the mass of
an electron), and travels at speeds approaching (but less than) the speed of light. Neutrinos were
fi nally discovered in 1956. Today, neutrinos are created in abundance in nuclear reactors and
particle accelerators and are thought to be plentiful in the universe.
Positrons and Antiparticles The year 1932 saw the discovery of the positron (a contraction for “positive electron”). The posi- tron has the same mass as the electron but carries an opposite charge of +e. A collision between a positron and an electron is likely to annihilate both particles, converting them into electromag-
netic energy in the form of 𝛾 rays. For this reason, positrons never coexist with ordinary matter for any appreciable length of time. The mutual annihilation of a positron and an electron lies at the
heart of an important medical diagnostic technique, as Conceptual Example 7 discusses.
Proton
+
Proton
+
After collisionBefore collision
Proton
+
Proton
+
π 0
FIGURE 32.10 When an energetic proton collides with a stationary proton, a neutral
pion (𝜋0) is produced. Part of the energy of the incident proton goes into creating the pion.
CONCEPTUAL EXAMPLE 7 BIO The Physics of PET Scanning
Certain radioactive isotopes decay by positron emission—for example,
oxygen 158O. In the medical diagnostic technique known as PET scanning
(positron emission tomography), such isotopes are injected into the body,
where they collect at specifi c sites. A positron (01 e) emitted by the decaying
isotope immediately encounters an electron ( 0−1e) in the body tissue, and
the resulting mutual annihilation produces two 𝛾-ray photons ( 01 e + 0−1 e → 𝛾 + 𝛾), which are detected by devices mounted on a ring around the patient. As Figure 32.11a shows, the two photons strike oppositely positioned de- tectors and, in so doing, reveal the line on which the annihilation occurred.
Such information leads to a computer-generated image that can be useful
in diagnosing abnormalities at the site where the radioactive isotope col-
lects (see Figure 32.12). Which conservation principle accounts for the fact that the photons strike oppositely positioned detectors, the principle of
conservation of (a) linear momentum or (b) energy?
Reasoning Momentum is a vector concept and, therefore, has a direc- tion. The momentum-conservation principle states that the total linear
momentum of an isolated system remains constant (see Section 7.2).
An isolated system is one on which no net external force acts. Energy
is not a vector concept and has no direction associated with it. The
energy-conservation principle states that energy can neither be created
nor destroyed, but can only be converted from one form to another (see
Section 6.8).
Answer (b) is incorrect. Energy is not a vector and has no direction associated with it. Therefore, it cannot, by itself, reveal the directional line
along which the 𝛾-ray photons were emitted.
Answer (a) is correct. The positron and the electron constitute an isolated system, so that momentum conservation applies. They do exert
electrostatic forces on one another, since they carry electric charges.
However, these forces are internal, not external, forces and cannot change
the total linear momentum of the two-particle system. The total photon
momentum, then, must equal the total momentum of the positron and the
electron, which is nearly zero, to the extent that these particles have much
less momentum than the photons do. With a total linear momentum of
zero, the momentum vectors of the photons must point in opposite direc-
tions. Thus, the two photons depart from the annihilation site heading
toward oppositely located detectors.
Related Homework: Problem 44
924 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
The positron is an example of an antiparticle, and after its discovery scientists came to real-
ize that for every type of particle there is a corresponding type of antiparticle. The antiparticle
is a form of matter that has the same mass as the particle but carries an opposite electric charge
(e.g., the electron–positron pair) or has a magnetic moment that is oriented in an opposite direc-
tion relative to the spin (e.g., the neutrino–antineutrino pair). A few electrically neutral particles,
like the photon and the neutral pion (𝜋0), are their own antiparticles.
Muons and Pions In 1937, the American physicists S. H. Neddermeyer (1907–1988) and C. D. Anderson (1905–
1991) discovered a new charged particle whose mass was about 207 times greater than the mass
of the electron. The particle is designated by the Greek letter 𝜇 (mu) and is known as a muon. There are two muons that have the same mass but opposite charge: the particle 𝜇− and its anti- particle 𝜇+. The 𝜇− muon has the same charge as the electron, whereas the 𝜇+ muon has the same charge as the positron. Both muons are unstable, and have a lifetime of 2.2 × 10−6 s. The 𝜇− muon
Responding detector
Responding detector
γ
γ
(a) (b)
FIGURE 32.11 (a) In positron emission tomography, or PET scanning, a radioactive isotope is injected into the body. The isotope decays by emitting a positron, which annihilates an electron in the body tissue,
producing two 𝛾-ray photons. These photons strike detectors mounted on opposite sides of a ring that surrounds the patient. (b) A patient undergoing a PET scan of the brain.
H an
k M
o rg
an /S
ci en
ce S
o u rc
e
M ed
ic al
I m
ag es
FIGURE 32.12 This PET scan of the lungs reveals pulmonary edema (see the white
rectangle), which is an abnormal accumulation
of fl uid.
32.6 Elementary Particles 925
decays into an electron (𝛽−), a muon neutrino (ν𝜇), and an electron antineutrino (νe) according to the following reaction:
μ− β− + νμ + νe The 𝜇+ muon decays into a positron (𝛽+), a muon antineutrino (νμ), and an electron neutrino (νe):
μ+ β+ + νμ + νe Muons interact with protons and neutrons via the weak nuclear force (see Section 31.5).
The Japanese physicist Hideki Yukawa (1907–1981) predicted in 1935 that pions exist, but they were not discovered until 1947. Pions come in three varieties: one that is positively charged,
the negatively charged antiparticle with the same mass, and the neutral pion, mentioned earlier,
which is its own antiparticle. The symbols for these pions are, respectively, 𝜋+, 𝜋−, and 𝜋0. The charged pions are unstable and have a lifetime of 2.6 × 10−8 s. The decay of a charged pion almost
always produces a muon:
π− μ− + νμ π+ μ+ + νμ
As mentioned earlier, the neutral pion 𝜋0 is also unstable and decays into two 𝛾-ray photons, the lifetime being 8.4 × 10−17 s. The pions are of great interest because, unlike the muons, the pions
interact with protons and neutrons via the strong nuclear force.
Classification of Particles It is useful to group the known particles into three families—the bosons, the leptons, and
the hadrons—as Table 32.3 summarizes. The boson family is composed of particles (all are types of bosons) that play central roles in nature’s three fundamental forces (see Section 4.6).
The photon is associated with the electromagnetic force, which is one manifestation of the
electroweak force. The W−, W+, and Z0 particles are associated with the weak nuclear force,
which is the other manifestation of the electroweak force. The gluons are associated with the
strong nuclear force, whereas the graviton is thought to be associated with the gravitational
force.
The lepton family consists of particles that interact by means of the weak nuclear force. Leptons can also exert gravitational and (if the leptons are charged) electromagnetic forces on
other particles. The four better-known leptons are the electron, the muon, the electron neutrino
νe, and the muon neutrino ν𝜇. Table 32.3 lists these particles together with their antiparticles. Two other leptons have also been discovered, the tau particle 𝜏 and its neutrino ν𝜏, bringing the number of particles in the lepton family to six.
The hadron family contains the particles that interact by means of both the strong nuclear force and the weak nuclear force. Hadrons can also interact by gravitational and electromagnetic forces, but at short distances (≤10−15 m) the strong nuclear force dominates. Among the hadrons
are the proton, the neutron, and the pions. As Table 32.3 indicates, most hadrons are short-lived. The hadrons are subdivided into two groups, the mesons and the baryons, for a reason that will be discussed in connection with the idea of quarks.
Quarks As more and more hadrons were discovered, it became clear that they were not all elementary
particles. The suggestion was made that the hadrons are made up of smaller, more elementary
particles called quarks. In 1963, a quark theory was advanced independently by M. Gell- Mann (1929– ) and G. Zweig (1937– ). The theory proposed that there are three quarks
and three corresponding antiquarks, and that hadrons are constructed from combinations of
these. Thus, the quarks are elevated to the status of elementary particles for the hadron family.
The particles in the lepton family are considered to be elementary, and as such they are not
composed of quarks.
The three quarks were named up (u), down (d), and strange (s), and were assumed to have, respectively, fractional charges of +
2 3e, −
1 3e, and −
1 3e. In other words, a quark possesses a charge
926 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
TABLE 32.3 Some Particles and Their Properties
Family Particle Particle Symbol
Antiparticle Symbol
Rest Energy (MeV) Lifetime (s)
Bosona Photon 𝛾 Selfb 0 Stable
W± W− W+ 8.04 × 104 3 × 10−25
Z0 Z0 Selfb 9.12 × 104 3 × 10−25
Gluonsc g — 0 —
Gravitonc — — 0 —
Lepton Electron e− or β− e+ or β+ 0.511 Stable
Muon μ− μ+ 105.7 2.2 × 10−6
Tau 𝜏− 𝜏+ 1777 2.9 × 10−13
Electron neutrino νe νe <2 × 10−6 Stable
Muon neutrino ν𝜇 νμ <0.19 Stable
Tau neutrino ν𝜏 ντ <18.2 Stable
Hadron
Mesons
Pion π+ π− 139.6 2.6 × 10−8
π0 Selfb 135.0 8.4 × 10−17
Kaon K+ K− 493.7 1.2 × 10−8
K 0 K 0 497.6 —d
Eta η0 Selfb 547.3 <10−18
Baryons
Proton p p 938.3 Stable
Neutron n n 939.6 886
Lambda Λ0 Λ 0 1116 2.6 × 10−10
Sigma Σ +
Σ − 1189 8.0 × 10 −11
Σ 0 Σ 0 1193 7.4 × 10 −20
Σ − Σ + 1197 1.5 × 10−10
Omega Ω− Ω+ 1672 8.2 × 10−11
aThe particles in this family are types of bosons that are associated with (or mediate) nature’s fundamental forces. bThe particle is its own antiparticle. cFree gluons and the graviton have not been observed experimentally. dThis particle and its antiparticle do not have definite lifetimes.
magnitude smaller than that of an electron, which has a charge of −e. Table 32.4 lists the symbols and electric charges of these quarks and the corresponding antiquarks. Experimentally, quarks
should be recognizable by their fractional charges, but in spite of an extensive search for them,
free quarks have never been found.
According to the original quark theory, the mesons are diff erent from the baryons, because
each meson consists of only two quarks—a quark and an antiquark—whereas a baryon contains
three quarks. For instance, the 𝜋− pion (a meson) is composed of a d quark and a u antiquark,
32.6 Elementary Particles 927
𝜋− = d + u, as Figure 32.13 shows. These two quarks combine to give the 𝜋− pion a net charge of −e. Similarly, the 𝜋+ pion is a combination of the d and u quarks, 𝜋+ = d + u. In contrast, protons and neutrons, being baryons, consist of three quarks. A proton contains the combination d + u + u, and a neutron contains the combination d + d + u (see Figure 32.13). These groups of three quarks give the correct charges for the proton and neutron.
The original quark model was extremely successful in predicting not only the correct charges
for the hadrons, but other properties as well. However, in 1974 a new particle, the J/ψ meson,
was discovered. This meson has a rest energy of 3097 MeV, much larger than the rest energies
of other known mesons. The existence of the J/ψ meson could be explained only if a new quark–
antiquark pair existed; this new quark was called charmed (c). With the discovery of more and more particles, it has been necessary to postulate a fi fth and a sixth quark; their names are top (t) and bottom (b), although some scientists prefer to call these quarks truth and beauty. Today, there is fi rm evidence for all six quarks, each with its corresponding antiquark. All of the hundreds of
known hadrons can be accounted for in terms of these six quarks and their antiquarks.
In addition to electric charge, quarks also have other properties. For example, each quark
possesses a characteristic called color, for which there are three possibilities: blue, green, or red. The corresponding possibilities for the antiquarks are antiblue, antigreen, and antired. The use
of the term “color” and the specifi c choices of blue, green, and red are arbitrary, for the visible
colors of the electromagnetic spectrum have nothing to do with quark properties. The quark
property of color, however, is important, because it brings the quark model into agreement with
the Pauli exclusion principle and enables the model to account for experimental observations that
are otherwise diffi cult to explain.
The Standard Model The various elementary particles that have been discovered can interact via one or more of the
following four forces: the gravitational force, the strong nuclear force, the weak nuclear force,
and the electromagnetic force. In particle physics, the phrase “the standard model” refers to the currently accepted explanation for the strong nuclear force, the weak nuclear force, and the elec-
tromagnetic force. In this model, the strong nuclear force between quarks is described in terms of
the concept of color, and the theory is referred to as quantum chromodynamics. According to the
standard model, the weak nuclear force and the electromagnetic force are separate manifestations
of a single, even more fundamental, force, referred to as the electroweak force, as we have seen
in Section 31.5.
In the standard model, our understanding of the building blocks of matter follows the
hierarchical pattern illustrated in Interactive Figure 32.14. Molecules, such as water (H2O) and glucose (C6H12O6), are composed of atoms. Each atom consists of a nucleus that is surrounded
by a cloud of electrons. The nucleus, in turn, is made up of protons and neutrons, which are
composed of quarks.
TABLE 32.4 Quarks and Antiquarks
Quarks Antiquarks
Name Symbol Charge Symbol Charge
Up u +23 e u − 2
3 e
Down d −13 e d + 1
3 e
Strange s −13 e s + 1
3 e
Charmed c +23 e c − 2
3 e
Top t +23 e t − 2
3 e
Bottom b −13 e b + 1
3 e
d
Mesons
− +
u
u
Baryons
Proton Neutron
d
u d
u
d
1–– 3
– e 1–– 3
– e 2–– 3
– e1–– 3
+ e 2–– 3
+ e
1–– 3
– e
1–– 3
– e 1–– 3
– e2–– 3
+ e 2–– 3
+ e
2–– 3
+ e
–ud – d
2–– 3
– e
ππ
FIGURE 32.13 According to the original quark model of hadrons, all mesons consist
of a quark and an antiquark, whereas baryons
contain three quarks.
928 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
Check Your Understanding
(The answers are given at the end of the book.) 12. Of the following particles, which ones are not composed of quarks and antiquarks? (a) A proton (b) An
electron (c) A neutron (d) A neutrino 13. The sigma-minus particle Σ − has a charge of −e. Which one of the following quark combinations
corresponds to this particle? (a) dds (b) ssu (c) uus
32.7 Cosmology Cosmology is the study of the structure and evolution of the universe. In this study, both the very large and the very small aspects of the universe are important. Astronomers, for example,
study stars located at enormous distances from the earth, up to billions of light-years away. In
contrast, particle physicists focus their eff orts on the very small elementary particles (10−18 m or
smaller) that comprise matter. The synergy between the work of astronomers and that of particle
physicists has led to signifi cant advances in our understanding of the universe. Central to that
understanding is the belief that the universe is expanding, and we begin by discussing the evi-
dence that justifi es this belief.
The Expanding Universe and the Big Bang THE PHYSICS OF . . . an expanding universe. The idea that the universe is expanding originated with the astronomer Edwin P. Hubble (1889–1953). He found that light reaching the
earth from distant galaxies is Doppler-shifted toward greater wavelengths—that is, toward the red
end of the visible spectrum. As Section 24.5 discusses, this type of Doppler shift results when
the observer and the source of the light are moving away from each other. The speed at which a
galaxy is receding from the earth can be determined from the measured Doppler shift in wave-
length. Hubble found that a galaxy located at a distance d from the earth recedes from the earth at a speed 𝜐 given by
Hubble’s law υ = Hd (32.5)
where H is a constant known as the Hubble parameter. In other words, the recession speed is proportional to the distance d, so that more distant galaxies are moving away from the earth at greater speeds. Equation 32.5 is referred to as Hubble’s law.
Hubble’s picture of an expanding universe does not mean that the earth is at the center of the
expansion. In fact, there is no literal center. Imagine a loaf of raisin bread expanding as it bakes.
Each raisin moves away from every other raisin, without any single one acting as a center for
the expansion. Galaxies in the universe behave in a similar fashion. Observers in other galaxies
would see distant galaxies moving away, just as we do.
THE PHYSICS OF . . . “dark energy.” Not only is the universe expanding, it is doing so at an accelerated rate, according to recent astronomical measurements of the brightness of
+
+
+
10–9 m 10–10 m 10–15 – 10–14 m 10–15 m Less than 10–18 m
Molecule Atom Nucleus Neutron (or proton) Quark
+ +
+ +
+ +
INTERACTIVE FIGURE 32.14 The current view of how matter is composed of basic units, starting with a molecule and ending with a quark. The approximate sizes of each unit are also listed.
32.7 Cosmology 929
supernovas, or exploding stars. To account for the accelerated rate, astronomers have postulated
that “dark energy” pervades the universe. The normal gravitational force between galaxies slows
the rate at which they are moving away from each other. The dark energy gives rise to a force that
counteracts gravity and pushes galaxies apart. As yet, little is known about dark energy.
Experimental measurements by astronomers indicate that an approximate value for the
Hubble parameter is
H = 0.022 m
s · light-year
The value for the Hubble parameter is believed to be accurate within 10%. Scientists are very
interested in obtaining an accurate value for H because it can be related to an age for the universe, as the next example illustrates.
EXAMPLE 8 An Age for the Universe
Determine an estimate of the age of the universe using Hubble’s law.
Reasoning Consider a galaxy currently located at a distance d from the earth. According to Hubble’s law, this galaxy is moving away from us at a
speed of υ = Hd. At an earlier time, therefore, this galaxy must have been closer. We can imagine, in fact, that in the remote past the separation dis-
tance was relatively small and that the universe originated at such a time.
To estimate the age of the universe, we calculate the time it has taken the
galaxy to recede to its present position. For this purpose, time is simply
distance divided by speed, or t = d/υ.
Solution Using Hubble’s law and the fact that a distance of 1 light-year is 9.46 × 1015 m, we estimate the age of the universe to be
t = d υ
= d
Hd =
1
H
t = 1
0.022 m
s · light-year
= 1
(0.022 ms · light-year) ( 1 light-year
9.46 × 1015 m) = 4.3 × 1017 s or 1.4 × 1010 yr
The idea presented in Example 8, that our galaxy and other galaxies in the universe were
very close together at some earlier instant in time, lies at the heart of the Big Bang theory. This theory postulates that the universe had a defi nite beginning in a cataclysmic event, sometimes
called the primeval fi reball. Dramatic evidence supporting the theory was discovered in 1965
by Arno A. Penzias (1933– ) and Robert W. Wilson (1936– ). Using a radio telescope, they
discovered that the earth is being bathed in weak electro-magnetic waves in the microwave region
of the spectrum (wavelength = 7.35 cm, see Figure 24.9). They observed that the intensity of these waves is the same, no matter where in the sky they pointed their telescope, and concluded
that the waves originated outside of our galaxy. This microwave background radiation, as it is
called, represents radiation left over from the Big Bang and is a kind of cosmic afterglow. Subse-
quent measurements have confi rmed the research of Penzias and Wilson and have shown that the
microwave radiation is consistent with a perfect blackbody (see Sections 13.3 and 29.2) radiat-
ing at a temperature of 2.7 K, in agreement with theoretical analysis of the Big Bang. In 1978,
Penzias and Wilson received a Nobel Prize for their discovery.
The Standard Model for the Evolution of the Universe Based on the recent experimental and theoretical research in particle physics, scientists have
proposed an evolutionary sequence of events following the Big Bang. This sequence is known as
the standard cosmological model and is illustrated in Figure 32.15. Immediately following the Big Bang, the temperature of the universe was incredibly high,
about 1032 K. During this initial period, the three fundamental forces (the gravitational force,
the strong nuclear force, and the electroweak force) all behaved as a single unifi ed force. Very
quickly, in about 10−43 s, the gravitational force took on a separate identity all its own, as
Figure 32.15 indicates. Meanwhile, the strong nuclear force and the electroweak force contin- ued to act as a single force, which is sometimes referred to as the GUT force. GUT stands for
the grand unifi ed theory that presumably would explain such a force. Slightly later, at about 10−35 s after the Big Bang, the GUT force separated into the strong nuclear force and the elec-
troweak force, the universe expanding and cooling somewhat to a temperature of roughly 1028 K
930 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
(see Figure 32.15). From this point on, the strong nuclear force behaved as we know it today, while the electroweak force maintained its identity. In this scenario, note that the weak nuclear
force and the electromagnetic force have not yet manifested themselves as separate entities.
The disappearance of the electroweak force and the appearance of the weak nuclear force and
the electromagnetic force eventually occurred at approximately 10−10 s after the Big Bang,
when the temperature of the expanding universe had cooled to about 1015 K.
From the Big Bang up until the strong nuclear force separated from the GUT force at a time
of 10−35 s, all particles of matter were similar, and there was no distinction between quarks and
leptons. After this time, quarks and leptons became distinguishable. Eventually the quarks and
antiquarks formed hadrons, such as protons and neutrons and their antiparticles. By a time of
10−4 s after the Big Bang, however, the temperature had cooled to approximately 1012 K, and the
hadrons had mostly disappeared. Protons and neutrons survived only as a very small fraction of
the total number of particles, the majority of which were leptons such as electrons, positrons, and
neutrinos. Like most of the hadrons before them, most of the electrons and positrons eventually
disappeared. However, they did leave behind a relatively small number of electrons to join the
small number of protons and neutrons at a time of about 3 min following the Big Bang. At this
time the temperature of the expanding universe had decreased to about 109 K, and small nuclei
such as that of helium began forming. Later, when the universe was about 500 000 years old and
the temperature had dropped to near 3000 K, hydrogen and helium atoms began forming. As the
temperature decreased further, stars and galaxies formed, and today we fi nd a temperature of 2.7 K
characterizing the cosmic background radiation of the universe.
GUT force Electroweakforce Electromagnetic force
Weak nuclear force
Strong nuclear force
Gravitational force
Temperature
Big Bang
Time
Unified force
1032 K
10–43s 3 min
3000 K
500 000 yr
2.7 K
Today
1028 K
10–35s
1015 K
10–10s
1012 K
10–4s
109 K
FIGURE 32.15 According to the standard cosmological model, the universe has evolved as illustrated here. In this model, the universe is presumed to have originated with a cataclysmic event known as the Big
Bang. The times shown are those following this event.
EXAMPLE 9 BIO The Energy Absorbed by a Body During a CT Scan
Consider a patient who receives a BED of 1.7 rem during a full-body CT
scan. If the RBE of the X-rays in this procedure is 0.90, how much energy
is absorbed by a patient with a mass of 82 kg?
Reasoning We can use Equation 32.4 to calculate the absorbed dose and then Equation 32.2 to calculate the energy absorbed by the
patient.
Solution From Equation 32.4, we have: Biologically equivalent dose
(in rems) =
Absorbed dose
(in rads) × RBE.
Rearranging, we fi nd:
Absorbed dose
(in rads) =
Biologically equivalent dose
(in rems)
RBE =
1.7 rem
0.90 = 1.9 rad.
In order to calculate the energy absorbed in joules, we need to convert
the absorbed dose to Gy: 1.9 rad = 0.019 Gy. Using Equation 32.2, we
calculate the energy absorbed:
Energy absorbed = (Absorbed dose) × (Mass of absorbing material)
= (0.019 Gy) × (82 kg) = 1.6 J
Concept Summary 931
Concept Summary 32.1 Biological Eff ects of Ionizing Radiation Ionizing radiation con- sists of photons and/or moving particles that have enough energy to ionize an
atom or molecule. Exposure is a measure of the ionization produced in air by
X-rays or 𝛾 rays. When a beam of X-rays or 𝛾 rays is sent through a mass m of dry air (0 °C, 1 atm pressure) and produces positive ions whose total charge
is q, the exposure in coulombs per kilogram (C/kg) is
Exposure (in coulombs per kilogram) = q m
With q in coulombs (C) and m in kilograms (kg), the exposure in roentgens is given by Equation 32.1.
Exposure
(in roentgens) = ( 12.58 × 10−4)
q m
(32.1)
The absorbed dose is the amount of energy absorbed from the radiation
per unit mass of absorbing material, as specifi ed by Equation 32.2. The SI
unit of absorbed dose is the gray (Gy); 1 Gy = 1 J/kg. However, the rad is
another unit that is often used: 1 rad = 0.01 Gy.
Absorbed dose = Energy absorbed
Mass of absorbing material (32.2)
The amount of biological damage produced by ionizing radiation is dif-
ferent for diff erent types of radiation. The relative biological eff ectiveness
(RBE) is the absorbed dose of 200-keV X-rays required to produce a certain
biological eff ect divided by the dose of a given type of radiation that pro-
duces the same biological eff ect, as given by Equation 32.3.
RBE =
The dose of 200-keV X-rays that
produces a certain biological effect
The dose of radiation that
produces the same biological effect
(32.3)
The biologically equivalent dose (in rems) is the product of the absorbed
dose (in rads) and the RBE, as shown in Equation 32.4.
Biologically equivalent dose
(in rems) =
Absorbed dose
(in rads) × RBE (32.4)
32.2 Induced Nuclear Reactions An induced nuclear reaction occurs whenever a target nucleus is struck by an incident nucleus, an atomic or
subatomic particle, or a 𝛾-ray photon and undergoes a change as a result. An induced nuclear transmutation is a reaction in which the target nucleus is
changed into a nucleus of a new element.
All nuclear reactions (induced or spontaneous) obey the conservation
laws of physics as they relate to mass/energy, electric charge, linear momen-
tum, angular momentum, and nucleon number.
Nuclear reactions are often written in a shorthand form, such as 147N
(𝛼, p) 178O. The fi rst and last symbols 147N and 178O denote, respectively, the initial and fi nal nuclei. The symbols within the parentheses denote the
incident 𝛼 particle (on the left) and the small emitted particle or proton p (on the right).
A thermal neutron is one that has a kinetic energy of about 0.04 eV.
32.3 Nuclear Fission Nuclear fi ssion occurs when a massive nucleus splits into two less massive fragments. Fission can be induced by the ab-
sorption of a thermal neutron. When a massive nucleus fi ssions, energy is
released because the binding energy per nucleon is greater for the fragments
than for the original nucleus. Neutrons are also released during nuclear
fi ssion. These neutrons can, in turn, induce other nuclei to fi ssion and lead to
a process known as a chain reaction. A chain reaction is said to be controlled
if each fi ssion event contributes, on average, only one neutron that fi ssions
another nucleus.
32.4 Nuclear Reactors A nuclear reactor is a device that generates energy by a controlled chain reaction. Many reactors in use today have
the same three basic components: fuel elements, a neutron moderator,
and control rods. The fuel elements contain the fi ssile fuel, and the entire
region of fuel elements is known as the reactor core. The neutron moderator
is a material (water, for example) that slows down the neutrons released in
a fi ssion event to thermal energies so they can initiate additional fi ssion
events. Control rods contain material that readily absorbs neutrons without
fi ssioning. They are used to keep the reactor in its normal, or critical, state,
in which each fi ssion event leads to one additional fi ssion, no more, no less.
The reactor is subcritical when, on average, the neutrons from each fi ssion
trigger less than one subsequent fi ssion. The reactor is supercritical when,
on average, the neutrons from each fi ssion trigger more than one additional
fi ssion.
32.5 Nuclear Fusion In a fusion process, two nuclei with smaller masses combine to form a single nucleus with a larger mass. Energy is
released by fusion when the binding energy per nucleon is greater for the
larger nucleus than for the smaller nuclei. Fusion reactions are said to be
thermonuclear because they require extremely high temperatures to proceed.
Current studies of nuclear fusion utilize either magnetic confi nement or
inertial confi nement to contain the fusing nuclei at the high temperatures
that are necessary.
32.6 Elementary Particles Subatomic particles are divided into three families: the boson family (which includes the photon), the lepton family
(which includes the electron), and the hadron family (which includes the
proton and the neutron). Elementary particles are the basic building blocks
of matter. All members of the boson and lepton families are elementary
particles.
The quark theory proposes that the hadrons are not elementary particles
but are composed of elementary particles called quarks. Currently, the hun-
dreds of hadrons can be accounted for in terms of six quarks (up, down,
strange, charmed, top, and bottom) and their antiquarks.
The standard model consists of two parts: (1) the currently accepted ex-
planation for the strong nuclear force in terms of the quark concept of “color”
and (2) the theory of the electroweak interaction.
32.7 Cosmology Cosmology is the study of the structure and evolution of the universe. Our universe is expanding. The speed υ at which a distant galaxy recedes from the earth is given by Hubble’s law (Equation 32.5),
where H = 0.022 m/(s · light-year) is called the Hubble parameter and d is the distance of the galaxy from the earth.
υ = Hd (32.5)
The Big Bang theory postulates that the universe had a defi nite be-
ginning in a cataclysmic event, sometimes called the primeval fi reball.
The radiation left over from this event is in the microwave region of the
electromagnetic spectrum, and it is consistent with a perfect blackbody
radiating at a temperature of 2.7 K, in agreement with theoretical analysis
of the Big Bang.
The standard cosmological model for the evolution of the universe is sum-
marized in Figure 32.15.
932 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
Note to Instructors: The numbering of the questions shown here refl ects the fact that they are only a representative subset of the total number that are available online. However, all of the questions are available for assignment via WileyPLUS.
Section 32.1 Biological Eff ects of Ionizing Radiation 1. Biologically equivalent doses are specifi ed in units called_______. (a) rads (b) grays (c) rems (d) J/kg (e) roentgens
Section 32.2 Induced Nuclear Reactions 4. Determine the unknown nuclear species AZ X in the following nuclear reaction:
A Z X +
14 7N
14 6C +
1 1H
(a) 21 H (b) 10 n (c) 𝛾 ray (d) 42 He
Section 32.3 Nuclear Fission 6. The fi ssion of 23592U can occur via many diff erent reactions. In general, they can be written as follows:
1 0 n +
235 92 U
AX ZX X +
AY ZY Y + η 10 n
where X and Y refer to the identities of the fi ssion fragments and η is the number of neutrons produced. Which one or more of the following state-
ments are true?
A. The compound nucleus that is formed to initiate the fi ssion process is the same, no matter what X and Y refer to.
B. The greater the number η of neutrons produced by the reaction, the smal- ler is the sum of the nucleon numbers AX and AY. C. The sum of the atomic numbers ZX and ZY is the same, no matter what X and Y refer to.
(a) A (b) A and B (c) A and C (d) B and C (e) A, B, and C
Section 32.5 Nuclear Fusion 9. In each of the following three nuclear fusion reactions, the masses of the nuclei are given beneath each nucleus. Rank the energy produced by each
reaction in descending order (greatest fi rst).
Reaction I 21 H + 2 1 H
3 2 He +
1 0 n
2.0141 u⏟ 2.0141 u⏟ 3.0160 u⏟ 1.0087 u⏟
Reaction II 32 He + 3 2 He
4 2 He +
1 1 H +
1 1 H
Reaction III 157 N + 1 1 H
12 6C +
4 2 He
(a) I, II, III (b) I, III, II (c) II, III, I (d) II, I, III (e) III, II, I
Section 32.6 Elementary Particles 10. The drawings show four possibilities for hadrons in the quark theory. In each of the possibilities, the symbols for the quarks are shown together with
the corresponding electric charges. Note that e stands for the magnitude of the charge on an electron. Which one shows the quark structure for an anti-
proton? (a) A (b) B (c) C (d) D
QUESTION 10
d
u
d u
d
u
2–– 3
–
–
– – e
2–– 3
+ e 2–– 3
+ e1–– 3
+ e 1–– 3
+ e
1–– 3
– e
A B
d
u
d u
d
u
2–– 3
+ e
2–– 3
– e 2–– 3
– e1–– 3
– e 1–– 3
– e
1–– 3
+ e
–
– –
C D
Section 32.7 Cosmology 11. Which one of the following statements is not accepted as a part of the current picture of the universe? (a) The universe is expanding. (b) Early in the history of the universe, there was only one fundamental force.
(c) The universe began with a cataclysmic event known as the Big Bang. (d) The weak electromagnetic radiation in the microwave region of the spectrum that bathes the earth provides evidence of the Big Bang theory.
(e) Hubble’s law indicates that a galaxy located at a distance d from the earth is moving away from the earth at a speed that is inversely propor-
tional to d.
3.0160 u⏟ 1.0078 u⏟4.0026 u⏟ 1.0078 u⏟3.0160 u⏟
15.0001 u⏟ 1.0078 u⏟ 12.0000 u⏟ 4.0026 u⏟
Focus on Concepts
Note to Instructors: Most of the homework problems in this chapter are avail- able for assignment via WileyPLUS. See the Preface for additional details.
SSM Student Solutions Manual
MMH Problem-solving help
GO Guided Online Tutorial
V-HINT Video Hints
CHALK Chalkboard Videos
BIO Biomedical application
E Easy
M Medium
H Hard
Section 32.1 Biological Eff ects of Ionizing Radiation 1. E SSM Neutrons (RBE = 2.0) and 𝛼 particles have the same biologically equivalent dose. However, the absorbed dose of the neutrons is six times the
absorbed dose of the 𝛼 particles. What is the RBE for the 𝛼 particles? 2. E What absorbed dose (in rads) of 𝛼 particles (RBE = 15) causes as much biological damage as a 60-rad dose of protons (RBE = 10)?
3. E BIO Over a full course of treatment, two diff erent tumors are to receive the same absorbed dose of therapeutic radiation. The smaller of the tumors
Problems
Problems 933
(mass = 0.12 kg) absorbs a total of 1.7 J of energy. (a) Determine the ab- sorbed dose, in Gy. (b) What is the total energy absorbed by the larger of the tumors (mass = 0.15 kg)?
4. E Over a year’s time, a person receives a biologically equivalent dose of 24 mrem (millirems) from cosmic rays, which consist primarily of high-
energy protons bombarding earth’s atmosphere from space. The relative bio-
logical eff ectiveness of protons is 10. (a) What is the person’s absorbed dose in rads? (b) The person absorbs 1.9 × 10−3 J of energy from cosmic rays in a year. What is the person’s mass?
5. E BIO GO SSM A beam of particles is directed at a 0.015-kg tumor. There are 1.6 × 1010 particles per second reaching the tumor, and the energy
of each particle is 4.0 MeV. The RBE for the radiation is 14. Find the biolo-
gically equivalent dose given to the tumor in 25 s.
6. E GO A 75-kg person is exposed to 45 mrem of 𝛼 particles (RBE = 12). How much energy (in joules) has this person absorbed?
7. E BIO Available in WileyPLUS. 8. E GO The biologically equivalent dose for a typical chest X-ray is 2.5 × 10−2 rem. The mass of the exposed tissue is 21 kg, and it absorbs 6.2 × 10−3 J
of energy. What is the relative biological eff ectiveness (RBE) for the radi-
ation on this particular type of tissue?
9. M BIO A 2.0-kg tumor is being irradiated by a radioactive source. The tumor receives an absorbed dose of 12 Gy in a time of 850 s. Each disinteg-
ration of the radioactive source produces a particle that enters the tumor and
delivers an energy of 0.40 MeV. What is the activity ΔN/Δt (see Section 31.6) of the radioactive source?
10. M V-HINT Available in WileyPLUS. 11. M CHALK SSM A beam of nuclei is used for cancer therapy. Each nucleus has an energy of 130 MeV, and the relative biological eff ectiveness (RBE) of
this type of radiation is 16. The beam is directed onto a 0.17-kg tumor, which
receives a biologically equivalent dose of 180 rem. How many nuclei are in
the beam?
Section 32.2 Induced Nuclear Reactions 12. E What is the atomic number Z, the atomic mass number A, and the element X in the reaction 105 B
(𝛼, p) AZX? 13. E SSM Write the equation for the reaction 178O (𝛾, 𝛼n) 126C. The notation “𝛼n” means that an 𝛼 particle and a neutron are produced by the reaction. 14. E GO For each of the nuclear reactions listed below, determine the unknown particle AZ X. Use the periodic table on the inside of the back cover
as needed.
(a) AZ X + 147N 11H + 178 O (c) 11H + 2713Al AZ X + 10n (b) 157 N + AZ X 126 C + 42He (d) 73Li + 11H 42He + AZ X 15. E A neutron causes 90232 Th to change according to the reaction
1 0 n +
232 90 Th
A Z X + γ
(a) Identify the unknown nucleus ZA X, giving its atomic mass number A, its atomic number Z, and the symbol X for the element. (b) The ZA X nucleus subsequently undergoes 𝛽− decay, and its daughter does too. Identify the fi nal nucleus, giving its atomic mass number, atomic number, and name.
16. E Write the reactions below in the shorthand form discussed in the text. (a) 42 He + 2713 Al 3015 P + 10 n (b) 11 H + 94 Be 63 Li + 42 He (c) 10 n + 5525 Mn 5625 Mn + γ 17. E SSM Complete the following nuclear reactions, assuming that the unknown quantity signifi ed by the question mark is a single entity:
(a) 3418 Ar (n, α)? (b) 8234 Se (?, n) 8235 Br (c) 5828 Ni (4018 Ar, ?) 5727 Co (d) ?(γ, α)168 O
18. M CHALK During a nuclear reaction, an unknown particle is absorbed by a copper 6329 Cu nucleus, and the reaction products are
62 29 Cu, a neutron,
and a proton. What are the name, atomic number, and nucleon number of
the nucleus formed temporarily when the copper 6329 Cu nucleus absorbs the
unknown particle?
19. M V-HINT Available in WileyPLUS.
Section 32.3 Nuclear Fission, Section 32.4 Nuclear Reactors 20. E Determine the atomic number Z, the atomic mass number A, and the element X for the unknown species AZX in the following reaction for the
fi ssion of uranium 92 235 U:
1 0 n +
235 92 U
133 51 Sb +
A Z X + 4
1 0 n
Consult the periodic table on the inside of the back cover of the text as needed.
21. E SSM When a 23592U (235.043 924 u) nucleus fi ssions, about 200 MeV of energy is released. What is the ratio of this energy to the rest energy of the
uranium nucleus?
22. E How many neutrons are produced when 92235 U fi ssions in the following way? 10 n +
235 92U →
132 50Sn +
101 42Mo + neutrons
23. E Neutrons released by a fi ssion reaction must be slowed by collisions with the moderator nuclei before the neutrons can cause further fi ssions. Sup-
pose a 1.5-MeV neutron leaves each collision with 65% of its incident energy.
How many collisions are required to reduce the neutron’s energy to at least
0.040 eV, which is the energy of a thermal neutron?
24. E V-HINT The energy released by each fi ssion within the core of a nuclear reactor is 2.0 × 102 MeV. The number of fi ssions occurring each
second is 2.0 × 1019. Determine the power (in watts) that the reactor generates.
25. E Uranium 23592U fi ssions into two fragments plus three neutrons: 1 0 n +
235 92U → (2 fragments) + 3
1 0 n. The mass of a neutron is 1.008 665 u and
the mass of 23592U is 235.043 924 u. If 225.0 MeV of energy is released, what
is the total mass of the two fragments?
26. M GO When 1.0 kg of coal is burned, approximately 3.0 × 107 J of energy is released. If the energy released during each 23592 U fi ssion is 2.0 ×
102 MeV, how many kilograms of coal must be burned to produce the same
energy as 1.0 kg of 23592 U?
27. M SSM Available in WileyPLUS. 28. M GO The water that cools a reactor core enters the reactor at 216 °C and leaves at 287 °C. (The water is pressurized, so it does not turn to steam.)
The core is generating 5.6 × 109 W of power. Assume that the specifi c
heat capacity of water is 4420 J/(kg · C°) over the temperature range stated above, and fi nd the mass of water that passes through the core each second.
29. H SSM A nuclear power plant is 25% effi cient, meaning that only 25% of the power it generates goes into producing electricity. The remaining 75%
is wasted as heat. The plant generates 8.0 × 108 watts of electric power. If
each fi ssion releases 2.0 × 102 MeV of energy, how many kilograms of 23592U
are fi ssioned per year?
30. H Available in WileyPLUS.
Section 32.5 Nuclear Fusion 31. E Two deuterium atoms (21 H) react to produce tritium (31 H) and hydro- gen (11 H) according to the following fusion reaction:
2 1 H +
2 1 H
3 1 H +
1 1 H
What is the energy (in MeV) released by this deuterium–deuterium reaction?
3.016 050 u⏟⏟2.014 102 u ⏟2.014 102 u ⏟1.007 825 u
934 CHAPTER 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
32. E GO In one type of fusion reaction a proton fuses with a neutron to form a deuterium nucleus:
1 1 H +
1 0 n
2 1 H + γ
The masses are 11 H (1.0078 u), 1 0 n (1.0087 u), and
2 1 H (2.0141 u). The 𝛾-ray
photon is massless. How much energy (in MeV) is released by this reaction?
33. E MMH The fusion of two deuterium nuclei (12 H, mass = 2.0141 u) can yield a helium nucleus ( 2
3 He, mass = 3.0160 u) and a neutron ( 0 1 n, mass =
1.0087 u). What is the energy (in MeV) released in this reaction?
34. E V-HINT Tritium (31 H) is a rare isotope of hydrogen that can be pro- duced by the following fusion reaction:
1 Z X + 1
AY 31 H + γ
(a) Determine the atomic mass number A, the atomic number Z, and the names X and Y of the unknown particles. (b) Using the masses given in the reaction, determine how much energy (in MeV) is released by this reaction.
35. M CHALK SSM One proposed fusion reaction combines lithium 63 Li (6.015 u) with deuterium 21 H (2.014 u) to give helium
4 2 He (4.003 u):
2 1 H +
6 3 Li → 2
4 2 He. How many kilograms of lithium would be needed to sup-
ply the energy needs of one household for a year, estimated to be 3.8 × 1010 J?
36. M GO In Example 6 it was determined that 17.6 MeV of energy is released when the following fusion reaction occurs:
2 1 H +
3 1 H
4 2 He +
1 0 n
Ignore relativistic eff ects and determine the kinetic energies of the neutron
and the 𝛼 particle.
37. M Deuterium ( 21 H) is an attractive fuel for fusion reactions because it is abundant in the oceans, where about 0.015% of the hydrogen atoms in the
water (H2O) are deuterium atoms. (a) How many deuterium atoms are there in one kilogram of water? (b) If each deuterium nucleus produces about 7.2 MeV in a fusion reaction, how many kilograms of water would be needed to supply
the energy needs of the United States for one year, estimated to be 1.1 × 1020 J?
38. H Available in WileyPLUS.
3.0161 u⏟⏟1.0087 u ⏟2.0141 u
4.0026 u⏟⏟2.0141 u ⏟3.0161 u ⏟1.0087 u
Section 32.6 Elementary Particles 39. E The main decay mode for the negative pion is π− → μ− + νμ. Find the energy (in MeV) released in this decay. Consult Table 32.3 for rest energies and assume that the rest energy for νμ is ≈ 0 MeV. 40. E V-HINT A neutral pion 𝜋0 (rest energy = 135.0 MeV) produced in a high-energy particle experiment moves at a speed of 0.780 c. After a very short time, it decays into two 𝛾-ray photons. One of the 𝛾-ray photons has an energy of 192 MeV. What is the energy (in MeV) of the second 𝛾-ray photon? Take relativistic eff ects into account.
41. E Available in WileyPLUS. 42. E GO In addition to its rest energy, a moving proton (pʹ ) has kinetic energy. This proton collides with a stationary proton (p), and the reaction forms a stationary neutron (n), a stationary proton (p), and a stationary pion (𝜋+), according to the following reaction: p′ + p → n + p + 𝜋+. The rest energy of each proton is 938.3 MeV, and the rest energy of the neutron is
939.6 MeV. The rest energy of the pion is 139.6 MeV. What is the kinetic
energy (in MeV) of the moving proton?
43. E SSM Suppose a neutrino is created and has an energy of 35 MeV. (a) Assuming the neutrino, like the photon, has no mass and travels at the speed of light, fi nd the momentum of the neutrino. (b) Determine the de Broglie wavelength of the neutrino.
44. M GO Review Conceptual Example 7 as background for this problem. An electron and its antiparticle annihilate each other, producing two 𝛾-ray photons. The kinetic energies of the particles are negligible. Determine the
magnitude of the momentum of each photon.
45. M Review Conceptual Example 5 as background for this problem. An energetic proton is fi red at a stationary proton. For the reaction to produce
new particles, the two protons must approach each other to within a distance
of about 8.0 × 10−15 m. The moving proton must have a suffi cient speed to
overcome the repulsive Coulomb force. What must be the minimum initial
kinetic energy (in MeV) of the proton?
46. E GO Someone stands near a radioactive source and receives doses of the following types of radiation: 𝛾 rays (20 mrad, RBE = 1), electrons (30 mrad, RBE = 1), protons (5 mrad, RBE = 10), and slow neutrons (5 mrad,
RBE = 2). Rank the types of radiation, highest fi rst, as to which produces the
largest biologically equivalent dose.
47. E SSM Available in WileyPLUS. 48. E Identify the unknown species AZX in the following nuclear reaction: 22 11 Na (d, 𝛼) AZX. Here, d stands for the deuterium isotope 21 H of hydrogen. 49. E GO MMH What energy (in MeV) is released by the following fi ssion reaction?
1 0 n +
235 92U
140 54 Xe +
94 38 Sr + 2
1 0 n
50. M V-HINT Multiple-Concept Example 1 discusses some of the physics principles that are used to solve this problem. What absorbed dose (in rads) of 𝛾 rays is required to change a block of ice at 0.0 °C into steam at 100.0 °C?
51. M SSM Imagine that your car is powered by a fusion engine in which the following reaction occurs: 3 21 H →
4 2 He +
1 1 H +
1 0 n. The masses are
2 1 H
139.922 u⏟⏟1.009 u ⏟235.044 u ⏟93.915 u ⏟2(1.009 u)
(2.0141 u), 42 He (4.0026 u), 1 1 H (1.0078 u), and
1 0 n (1.0087 u). The engine
uses 6.1 × 10−6 kg of deuterium 21 H fuel. If one gallon of gasoline produces
2.1 × 109 J of energy, how many gallons of gasoline would have to be burned
to equal the energy released by all the deuterium fuel?
52. M GO The energy consumed in one year in the United States is about 1.1 × 1020 J. With each 23592U fi ssion, about 2.0 × 10
2 MeV of energy is re-
leased. How many kilograms of 23592U would be needed to generate this energy
if all the nuclei fi ssioned?
53. M (a) If each fi ssion reaction of a 23592U nucleus releases about 2.0 × 102 MeV of energy, determine the energy (in joules) released by the com-
plete fi ssioning of 1.0 gram of 23592U. (b) How many grams of 23592U would be consumed in one year to supply the energy needs of a household that uses
30.0 kWh of energy per day, on the average?
54. H One kilogram of dry air at STP conditions is exposed to 1.0 R of X-rays. One roentgen is defi ned by Equation 32.1. An equivalent defi n-
ition can be based on the fact that an exposure of one roentgen deposits
8.3 × 10−3 J of energy per kilogram of dry air. Using the two defi nitions and
assuming that all ions produced are singly charged, determine the average
energy (in eV) needed to produce one ion in air.
Additional Problems
Team Problems 935
When considering the biological eff ects of ionizing radiation, the concept of
biologically equivalent dose is especially important. Its importance lies in
the fact that the biologically equivalent dose incorporates both the amount of
energy per unit mass that is absorbed and the eff ectiveness of a particular
type of radiation in producing a certain biological eff ect. Problem 55 exam-
ines this concept and also reviews the notions of power (Section 6.7) and
intensity (Section 16.7) of a wave. Problem 56 illustrates the decay of a
particle into two photons, and provides a review of the principles of conser-
vation of energy and conservation of momentum.
55. M CHALK SSM A patient is being given a chest X-ray. The X-ray beam is turned on for 0.20 s, and its intensity is 0.40 W/m2. The area of the chest
being exposed is 0.072 m2, and the radiation is absorbed by 3.6 kg of tissue.
The relative biological eff ectiveness (RBE) of the X-ray for this tissue is 1.1.
Concepts: (i) How is the power of the beam related to the beam intensity?
(ii) How is the energy absorbed by the tissue related to the power of the beam? (iii) What is the absorbed dose? (iv) How is the biologically equival- ent dose related to the absorbed dose? Calculation: Calculate the biologically equivalent dose received by the patient.
56. M CHALK The 𝜋0 meson is a particle that has a rest energy of 135.0 MeV (see Table 32.3). It lives for a very short time and then decays into two 𝛾-ray photons: 𝜋0 → 𝛾 + 𝛾. Suppose that one of the 𝛾-ray photons travels along the +x axis. Concepts: (i) How is the energy E of each 𝛾-ray photon related to the rest energy E0 of the 𝜋0 particle? (ii) How can the frequency and wavelength of a photon be determined from its energy? (iii) How is the total linear mo-
mentum of the photons related to the momentum of the 𝜋0 particle, and what is the momentum of each particle? Calculations: If the 𝜋0 is at rest when it decays, fi nd (a) the energy (in MeV), (b) the frequency and wavelength, and (c) the momentum of each 𝛾-ray photon.
Concepts and Calculations Problems
57. M A Rough Measure of Exposure. You and your team are designing a crude device to estimate radiation exposure. The device consists of a set
of parallel plates with a large voltage across them. The circular plates have
a radius of 3.50 cm and are separated by distance of 1.00 cm. The region
between the plates is fi lled with dry air at standard temperature and pressure
(STP: T = 0°, P = 1). A cubic meter of dry air at STP has a mass of 1.29 kg. When radiation ionizes an air molecule, the stripped electron is accelerated
by the electric fi eld between the plates and is registered as a current. When
the device is located near a particularly strong source, it registers a current
of 1.30 × 10−9 A. What is the exposure between the plates after 5.00 s (in
roentgens)?
58. M A Hypothetical Fusion Reactor. You and your team are tasked with evaluating the following deuterium-deuterium fusion reaction for use in a
future fusion power reactor:
2 1 H +
2 1 H
3 1 H +
1 1 H
(a) What is the energy released in this reaction (in joules)? (b) How many reactions per second would be required to run a 5000 MW reactor? (c) What mass of deuterium (in kg) would be needed to run the reactor for a year with
a power output of 5000 MW?
3.016 050 u⏟⏟2.014 102 u ⏟2.014 102 u ⏟1.007 825 u
Team Problems
A-1
In science, very large and very small decimal numbers are conveniently
expressed in terms of powers of ten, some of which are listed below:
103 = 10 × 10 × 10 = 1000 10−3 = 1
10 × 10 × 10
= 0.001
102 = 10 × 10 = 100 10−2 = 1
10 × 10 = 0.01
101 = 10 10−1 = 1
10 = 0.1
100 = 1
Using powers of ten, we can write the radius of the earth in the following
way, for example:
Earth radius = 6 380 000 m = 6.38 × 106 m
The factor of ten raised to the sixth power is ten multiplied by itself six
times, or one million, so the earth’s radius is 6.38 million meters. Al-
ternatively, the factor of ten raised to the sixth power indicates that the
decimal point in the term 6.38 is to be moved six places to the right to obtain the radius as a number without powers of ten.
For numbers less than one, negative powers of ten are used. For
instance, the Bohr radius of the hydrogen atom is
Bohr radius = 0.000 000 000 0529 m = 5.29 × 10 −11 m
The factor of ten raised to the minus eleventh power indicates that the
decimal point in the term 5.29 is to be moved eleven places to the left to obtain the radius as a number without powers of ten. Numbers expressed
with the aid of powers of ten are said to be in scientifi c notation. Calculations that involve the multiplication and division of powers
of ten are carried out as in the following examples:
(2.0 × 106)(3.5 × 103) = (2.0 × 3.5) × 106+3 = 7.0 × 109
9.0 × 107
2.0 × 104 = (9.02.0) × 107 × 10−4
= (9.02.0) × 107−4 = 4.5 × 103 The general rules for such calculations are
1
10 n = 10 −n (A-1)
10n × 10m = 10n+m (Exponents added) (A-2)
10 n
10 m = 10 n−m (Exponents subtracted) (A-3)
where n and m are any positive or negative number. Scientifi c notation is convenient because of the ease with which it
can be used in calculations. Moreover, scientifi c notation provides a
convenient way to express the significant figures in a number, as
Appendix B discusses.
Appendix A Powers of Ten and Scientific Notation
The number of signifi cant fi gures in a number is the number of digits whose values are known with certainty. For instance, a person’s height
is measured to be 1.78 m, with the measurement error being in the third
decimal place. All three digits are known with certainty, so that the num-
ber contains three signifi cant fi gures. If a zero is given as the last digit
to the right of the decimal point, the zero is presumed to be signifi cant.
Thus, the number 1.780 m contains four signifi cant fi gures. As another
example, consider a distance of 1500 m. This number contains only two
signifi cant fi gures, the one and the fi ve. The zeros immediately to the left
of the unexpressed decimal point are not counted as signifi cant fi gures.
However, zeros located between signifi cant fi gures are signifi cant, so a
distance of 1502 m contains four signifi cant fi gures.
Scientifi c notation is particularly convenient from the point of view
of signifi cant fi gures. Suppose it is known that a certain distance is fi fteen
hundred meters, to four signifi cant fi gures. Writing the number as 1500 m
presents a problem because it implies that only two signifi cant fi gures are
known. In contrast, the scientifi c notation of 1.500 × 103 m has the advan-
tage of indicating that the distance is known to four signifi cant fi gures.
When two or more numbers are used in a calculation, the number of
signifi cant fi gures in the answer is limited by the number of signifi cant
fi gures in the original data. For instance, a rectangular garden with sides
of 9.8 m and 17.1 m has an area of (9.8 m)(17.1 m). A calculator gives
167.58 m2 for this product. However, one of the original lengths is known
only to two signifi cant fi gures, so the fi nal answer is limited to only two
signifi cant fi gures and should be rounded off to 170 m2. In general, when numbers are multiplied or divided, the number of signifi cant fi gures in the fi nal answer equals the smallest number of signifi cant fi gures in any of the original factors.
The number of signifi cant fi gures in the answer to an addition or a
subtraction is also limited by the original data. Consider the total distance
along a biker’s trail that consists of three segments with the distances
shown as follows:
2.5 km
11 km
5.26 km
Total 18.76 km
The distance of 11 km contains no signifi cant fi gures to the right of the
decimal point. Therefore, neither does the sum of the three distances,
and the total distance should not be reported as 18.76 km. Instead, the
answer is rounded off to 19 km. In general, when numbers are added or subtracted, the last signifi cant fi gure in the answer occurs in the last column (counting from left to right) containing a number that results from a combination of digits that are all signifi cant. In the answer of 18.76 km, the eight is the sum of 2 + 1 + 5, each digit being signifi cant.
However, the seven is the sum of 5 + 0 + 2, and the zero is not signifi cant,
since it comes from the 11-km distance, which contains no signifi cant
fi gures to the right of the decimal point.
Appendix B Significant Figures
A-2 Appendixes
C.1 Proportions and Equations Physics deals with physical variables and the relations between them.
Typically, variables are represented by the letters of the English and
Greek alphabets. Sometimes, the relation between variables is expressed
as a proportion or inverse proportion. Other times, however, it is more
convenient or necessary to express the relation by means of an equation,
which is governed by the rules of algebra.
If two variables are directly proportional and one of them dou- bles, then the other variable also doubles. Similarly, if one variable is
reduced to one-half its original value, then the other is also reduced to
one-half its original value. In general, if x is directly proportional to y, then increasing or decreasing one variable by a given factor causes the other variable to change in the same way by the same factor. This
kind of relation is expressed as x ∝ y, where the symbol ∝ means “is proportional to.”
Since the proportional variables x and y always increase and de- crease by the same factor, the ratio of x to y must have a constant value, or x/y = k, where k is a constant, independent of the values for x and y. Consequently, a proportionality such as x ∝ y can also be expressed in the form of an equation: x = ky. The constant k is referred to as a propor- tionality constant.
If two variables are inversely proportional and one of them in- creases by a given factor, then the other decreases by the same factor. An
inverse proportion is written as x ∝ 1/y. This kind of proportionality is equivalent to the following equation: xy = k, where k is a proportionality constant, independent of x and y.
C.2 Solving Equations Some of the variables in an equation typically have known values, and
some do not. It is often necessary to solve the equation so that a variable
whose value is unknown is expressed in terms of the known quantities.
In the process of solving an equation, it is permissible to manipulate the equation in any way, as long as a change made on one side of the equals sign is also made on the other side. For example, consider the equation 𝜐 = 𝜐0 + at. Suppose values for 𝜐, 𝜐0, and a are available, and the value of t is required. To solve the equation for t, we begin by subtracting 𝜐0 from both sides:
𝜐 = υ0 + at −𝜐0 = −𝜐0 𝜐 − 𝜐0 = at Next, we divide both sides of 𝜐 − 𝜐0 = at by the quantity a:
υ − υ0
a =
at a
= (1) t
On the right side, the a in the numerator divided by the a in the denominator equals one, so that
t = υ − υ0
a It is always possible to check the correctness of the algebraic ma-
nipulations performed in solving an equation by substituting the answer
back into the original equation. In the previous example, we substitute the
answer for t into 𝜐 = 𝜐0 + at:
υ = υ0 + a ( υ − υ0
a ) = υ0 + (υ − υ0) = υ The result 𝜐 = 𝜐 implies that our algebraic manipulations were done correctly.
Algebraic manipulations other than addition, subtraction, multi-
plication, and division may play a role in solving an equation. The
same basic rule applies, however: Whatever is done to the left side
of an equation must also be done to the right side. As another example,
suppose it is necessary to express 𝜐0 in terms of 𝜐, a, and x, where 𝜐2 = 𝜐02 + 2ax. By subtracting 2ax from both sides, we isolate 𝜐02 on the right:
𝜐2 = 𝜐02 + 2ax −2ax = −2ax 𝜐2 − 2ax = 𝜐02
To solve for 𝜐0, we take the positive and negative square root of both sides of 𝜐2 − 2ax = 𝜐02:
υ0 = ± √υ 2 − 2ax
C.3 Simultaneous Equations When more than one variable in a single equation is unknown, additional
equations are needed if solutions are to be found for all of the unknown
quantities. Thus, the equation 3x + 2y = 7 cannot be solved by itself to give unique values for both x and y. However, if x and y also (i.e., simulta- neously) obey the equation x − 3y = 6, then both unknowns can be found.
There are a number of methods by which such simultaneous equa-
tions can be solved. One method is to solve one equation for x in terms of y and substitute the result into the other equation to obtain an expression containing only the single unknown variable y. The equation x − 3y = 6, for instance, can be solved for x by adding 3y to each side, with the result that x = 6 + 3y. The substitution of this expression for x into the equation 3x + 2y = 7 is shown below:
3x + 2y = 7 3(6 + 3y) + 2y = 7 18 + 9y + 2y = 7
We fi nd, then, that 18 + 11y = 7, a result that can be solved for y:
18 + 11y = 7 −18 −18
11y = −11 Dividing both sides of this result by 11 shows that y = −1. The value of y = −1 can be substituted in either of the original equations to obtain a value for x:
x − 3y = 6 x − 3(−1) = 6 x + 3 = 6 −3 −3
x = 3
Appendix C Algebra
Appendix D Exponents and Logarithms A-3
C.4 The Quadratic Formula Equations occur in physics that include the square of a variable. Such
equations are said to be quadratic in that variable, and often can be put into the following form:
ax 2 + bx + c = 0 (C-1)
where a, b, and c are constants independent of x. This equation can be solved to give the quadratic formula, which is
x = −b ± √b2 − 4ac
2a (C-2)
The ± in the quadratic formula indicates that there are two solutions.
For instance, if 2x2 − 5x + 3 = 0, then a = 2, b = −5, and c = 3. The quadratic formula gives the two solutions as follows:
x = −b + √b2 − 4ac
2a
= −(−5) + √(−5)2 − 4(2)(3)
2(2)
= +5 + √1
4 =
3
2
x = −b − √b2 − 4ac
2a
= −(−5) − √(−5)2 − 4(2)(3)
2(2)
= +5 − √1
4 = 1
Solution 1: Plus sign
Solution 2: Minus sign
Appendix A discusses powers of ten, such as 103, which means ten mul-
tiplied by itself three times, or 10 × 10 × 10. The three is referred to as
an exponent. The use of exponents extends beyond powers of ten. In general, the term yn means the factor y is multiplied by itself n times. For example, y2, or y squared, is familiar and means y × y. Similarly, y5 means y × y × y × y × y.
The rules that govern algebraic manipulations of exponents are the
same as those given in Appendix A (see Equations A-1, A-2, and A-3)
for powers of ten:
1
y n = y −n (D-1)
y n y m = y n+m (Exponents added) (D-2)
y n y m
= y n−m (Exponents subtracted) (D-3)
To the three rules above we add two more that are useful. One of
these is
y n z n = ( yz)n (D-4)
The following example helps to clarify the reasoning behind this rule:
3252 = (3 × 3)(5 × 5) = (3 × 5)(3 × 5) = (3 × 5)2
The other additional rule is
( y n) m = y nm (Exponents multiplied) (D-5)
To see why this rule applies, consider the following example:
(52)3 = (52)(52)(52) = 52+2+2 = 52×3
Roots, such as a square root or a cube root, can be represented with
fractional exponents. For instance,
√y = y1/2 and 3√y = y1/3
In general, the nth root of y is given by
n√y = y1/n (D-6)
The rationale for Equation D-6 can be explained using the fact that
(yn)m = ynm. For instance, the fi fth root of y is the number that, when multiplied by itself fi ve times, gives back y. As shown below, the term y1/5
satisfi es this defi nition:
(y1/5)(y1/5)(y1/5)(y1/5)(y1/5) = (y1/5)5 = (y1/5)×5 = y
Logarithms are closely related to exponents. To see the connection
between the two, note that it is possible to express any number y as another number B raised to the exponent x. In other words,
y = B x (D-7)
The exponent x is called the logarithm of the number y. The number B is called the base number. One of two choices for the base number is usually used. If B = 10, the logarithm is known as the common logarithm, for which the notation “log” applies:
Common logarithm y = 10x or x = log y (D-8)
If B = e = 2.718 . . . , the logarithm is referred to as the natural logarithm, and the notation “ln” is used:
Natural logarithm y = ez or z = ln y (D-9)
The two kinds of logarithms are related by
ln y = 2.3026 log y (D-10)
Both kinds of logarithms are often given on calculators.
The logarithm of the product or quotient of two numbers A and C can be obtained from the logarithms of the individual numbers according
to the rules below. These rules are illustrated here for natural logarithms,
but they are the same for any kind of logarithm.
ln (AC ) = ln A + ln C (D-11)
ln ( A C ) = ln A − ln C (D-12) Thus, the logarithm of the product of two numbers is the sum of the
individual logarithms, and the logarithm of the quotient of two numbers
is the diff erence between the individual logarithms. Another useful rule
concerns the logarithm of a number A raised to an exponent n:
ln An = n ln A (D-13)
Rules D-11, D-12, and D-13 can be derived from the defi nition of the
logarithm and the rules governing exponents.
Appendix D Exponents and Logarithms
A-4 Appendixes
E.1 Geometry Angles Two angles are equal if
1. They are vertical angles (see Figure E1). 2. Their sides are parallel (see Figure E2).
3. Their sides are mutually perpendicular (see Figure E3).
Triangles 1. The sum of the angles of any triangle is 180° (see Figure E4).
2. A right triangle has one angle that is 90°. 3. An isosceles triangle has two sides that are equal. 4. An equilateral triangle has three sides that are equal. Each angle of an
equilateral triangle is 60°.
5. Two triangles are similar if two of their angles are equal (see Figure E5). The corresponding sides of similar triangles are proportional to each
other:
a1 a 2
= b1
b2 =
c1 c2
6. Two similar triangles are congruent if they can be placed on top of one another to make an exact fi t.
Circumferences, Areas, and Volumes of Some Common Shapes 1. Triangle of base b and altitude h (see Figure E6):
Area = 1
2 bh
2. Circle of radius r:
Circumference = 2πr Area = πr 2
3. Sphere of radius r:
Surface area = 4πr 2
Volume = 4
3πr 3
4. Right circular cylinder of radius r and height h (see Figure E7):
Surface area = 2πr 2 + 2πrh Volume = πr 2h
Appendix E Geometry and Trigonometry
FIGURE E1
θ
θ θ
θ
FIGURE E2
90°
90°
θ
θ
FIGURE E3
+ + = 180°γ
γ
β β
α
α
FIGURE E4
b2
c2
a2
b1
c1
a1
β
β
α
α
FIGURE E5
90°
h
b
FIGURE E6
h
r
FIGURE E7
Appendix F Selected Isotopes A-5
E.2 Trigonometry Basic Trigonometric Functions 1. For a right triangle, the sine, cosine, and tangent of an angle 𝜃 are
defi ned as follows (see Figure E8):
sin θ = Side opposite θ
Hypotenuse =
ho h
cos θ = Side adjacent θ
Hypotenuse =
ha h
tan θ = Side opposite θ
Side adjacent to θ =
ho ha
2. The secant (sec 𝜃), cosecant (csc 𝜃), and cotangent (cot 𝜃) of an angle 𝜃 are defi ned as follows:
sec θ = 1
cos θ csc θ =
1
sin θ cot θ =
1
tan θ
Triangles and Trigonometry 1. The Pythagorean theorem states that the square of the hypotenuse of
a right triangle is equal to the sum of the squares of the other two sides
(see Figure E8):
h2 = ho2 + ha 2
2. The law of cosines and the law of sines apply to any triangle, not just a right triangle, and they relate the angles and the lengths of the sides
(see Figure E9):
Law of cosines c 2 = a 2 + b 2 − 2ab cos γ
Law of sines a
sin α =
b sin β
= c
sin γ
Other Trigonometric Identities 1. sin(−𝜃) = −sin 𝜃 2. cos(−𝜃) = cos 𝜃 3. tan(−𝜃) = −tan 𝜃 4. (sin 𝜃)/(cos 𝜃) = tan 𝜃 5. sin2 𝜃 + cos2 𝜃 = 1 6. sin(𝛼 ± 𝛽) = sin 𝛼 cos 𝛽 ± cos 𝛼 sin 𝛽
If 𝛼 = 90°, sin(90° ± 𝛽) = cos 𝛽
If 𝛼 = 𝛽, sin 2𝛽 = 2 sin 𝛽 cos 𝛽
7. cos(𝛼 ± 𝛽) = cos 𝛼 cos 𝛽 ∓ sin 𝛼 sin 𝛽
If 𝛼 = 90°, cos(90° ± 𝛽) = ∓sin 𝛽
If 𝛼 = 𝛽, cos 2𝛽 = cos2 𝛽 − sin2 𝛽 = 1 − 2 sin2 𝛽
Appendix F Selected Isotopesa
aData for atomic masses are taken from Handbook of Chemistry and Physics, 66th ed., CRC Press, Boca Raton, FL. The masses are those for the neutral atom, including the Z electrons. Data for percent abundance, decay mode, and half-life are taken from E. Browne and R. Firestone, Table of Radioactive Isotopes, V. Shirley, Ed., Wiley, New York, 1986. 𝛼 = alpha particle emission, 𝛽− = negative beta emission, 𝛽+ = positron emission, 𝛾 = 𝛾-ray emission, EC = electron capture.
90°
ha
ho h
θ
FIGURE E8
a
b
c
γ
β
α
FIGURE E9
Atomic No. Z Element Symbol
Atomic Mass No. A
Atomic Mass (u)
% Abundance, or Decay Mode if Radioactive
Half-Life (if Radioactive)
0 (Neutron) n 1 1.008 665 𝛽− 10.37 min 1 Hydrogen
Deuterium
Tritium
H
D
T
1
2
3
1.007 825
2.014 102
3.016 050
99.985
0.015
𝛽− 12.33 yr 2 Helium He 3
4
3.016 030
4.002 603
0.000 138
≈100
3 Lithium Li 6
7
6.015 121
7.016 003
7.5
92.5
4 Beryllium Be 7
9
7.016 928
9.012 182
EC, 𝛾 100
53.29 days
5 Boron B 10
11
10.012 937
11.009 305
19.9
80.1
A-6 Appendixes
Appendix F Selected Isotopes (continued)
Atomic No. Z Element Symbol
Atomic Mass No. A
Atomic Mass (u)
% Abundance, or Decay Mode if Radioactive
Half-Life (if Radioactive)
6 Carbon C 11
12
13
14
11.011 432
12.000 000
13.003 355
14.003 241
𝛽+, EC 98.90
1.10
𝛽−
20.39 min
5730 yr
7 Nitrogen N 13
14
15
13.005 738
14.003 074
15.000 108
𝛽+, EC 99.634
0.366
9.965 min
8 Oxygen O 15
16
18
15.003 065
15.994 915
17.999 160
𝛽+, EC 99.762
0.200
122.2 s
9 Fluorine F 18
19
18.000 937
18.998 403
EC, 𝛽+ 100
1.8295 h
10 Neon Ne 20
22
19.992 435
21.991 383
90.51
9.22
11 Sodium Na 22
23
24
21.994 434
22.989 767
23.990 961
𝛽+, EC, 𝛾 100
𝛽−, 𝛾
2.602 yr
14.659 h
12 Magnesium Mg 24 23.985 042 78.99
13 Aluminum Al 27 26.981 539 100
14 Silicon Si 28
31
27.976 927
30.975 362
92.23
𝛽−, 𝛾 2.622 h 15 Phosphorus P 31
32
30.973 762
31.973 907
100
𝛽− 14.282 days 16 Sulfur S 32
35
31.972 070
34.969 031
95.02
𝛽− 87.51 days 17 Chlorine Cl 35
37
34.968 852
36.965 903
75.77
24.23
18 Argon Ar 40 39.962 384 99.600
19 Potassium K 39
40
38.963 707
39.963 999
93.2581
𝛽−, EC, 𝛾 1.277 × 109 yr 20 Calcium Ca 40 39.962 591 96.941
21 Scandium Sc 45 44.955 910 100
22 Titanium Ti 48 47.947 947 73.8
23 Vanadium V 51 50.943 962 99.750
24 Chromium Cr 52 51.940 509 83.789
25 Manganese Mn 55 54.938 047 100
26 Iron Fe 56 55.934 939 91.72
27 Cobalt Co 59
60
58.933 198
59.933 819
100
𝛽−, 𝛾 5.271 yr 28 Nickel Ni 58
60
57.935 346
59.930 788
68.27
26.10
29 Copper Cu 63
65
62.939 598
64.927 793
69.17
30.83
30 Zinc Zn 64
66
63.929 145
65.926 034
48.6
27.9
31 Gallium Ga 69 68.925 580 60.1
32 Germanium Ge 72
74
71.922 079
73.921 177
27.4
36.5
33 Arsenic As 75 74.921 594 100
34 Selenium Se 80 79.916 520 49.7
35 Bromine Br 79 78.918 336 50.69
Appendix F Selected Isotopes A-7
Appendix F Selected Isotopes (continued)
Atomic No. Z Element Symbol
Atomic Mass No. A
Atomic Mass (u)
% Abundance, or Decay Mode if Radioactive
Half-Life (if Radioactive)
36 Krypton Kr 84
89
92
83.911 507
88.917 640
91.926 270
57.0
𝛽−, 𝛾 𝛽−, 𝛾
3.16 min
1.840 s
37 Rubidium Rb 85 84.911 794 72.165
38 Strontium Sr 86
88
90
94
85.909 267
87.905 619
89.907 738
93.915 367
9.86
82.58
𝛽− 𝛽−, 𝛾
29.1 yr
1.235 s
39 Yttrium Y 89 88.905 849 100
40 Zirconium Zr 90 89.904 703 51.45
41 Niobium Nb 93 92.906 377 100
42 Molybdenum Mo 98 97.905 406 24.13
43 Technetium Tc 98 97.907 215 𝛽−, 𝛾 4.2 × 106 yr 44 Ruthenium Ru 102 101.904 348 31.6
45 Rhodium Rh 103 102.905 500 100
46 Palladium Pd 106 105.903 478 27.33
47 Silver Ag 107
109
106.905 092
108.904 757
51.839
48.161
48 Cadmium Cd 114 113.903 357 28.73
49 Indium In 115 114.903 880 95.7; 𝛽− 4.41 × 1014 yr 50 Tin Sn 120 119.902 200 32.59
51 Antimony Sb 121 120.903 821 57.3
52 Tellurium Te 130 129.906 229 38.8; 𝛽− 2.5 × 1021 yr 53 Iodine I 127
131
126.904 473
130.906 114
100
𝛽−, 𝛾 8.040 days 54 Xenon Xe 132
136
140
131.904 144
135.907 214
139.921 620
26.9
8.9
𝛽−, 𝛾 13.6 s 55 Cesium Cs 133
134
132.905 429
133.906 696
100
𝛽−, EC, 𝛾 2.062 yr 56 Barium Ba 137
138
141
136.905 812
137.905 232
140.914 363
11.23
71.70
𝛽−, 𝛾 18.27 min 57 Lanthanum La 139 138.906 346 99.91
58 Cerium Ce 140 139.905 433 88.48
59 Praseodymium Pr 141 140.907 647 100
60 Neodymium Nd 142 141.907 719 27.13
61 Promethium Pm 145 144.912 743 EC, 𝛼, 𝛾 17.7 yr 62 Samarium Sm 152 151.919 729 26.7
63 Europium Eu 153 152.921 225 52.2
64 Gadolinium Gd 158 157.924 099 24.84
65 Terbium Tb 159 158.925 342 100
66 Dysprosium Dy 164 163.929 171 28.2
67 Holmium Ho 165 164.930 319 100
68 Erbium Er 166 165.930 290 33.6
69 Thulium Tm 169 168.934 212 100
70 Ytterbium Yb 174 173.938 859 31.8
71 Lutetium Lu 175 174.940 770 97.41
72 Hafnium Hf 180 179.946 545 35.100
A-8 Appendixes
Appendix F Selected Isotopes (continued)
Atomic No. Z Element Symbol
Atomic Mass No. A
Atomic Mass (u)
% Abundance, or Decay Mode if Radioactive
Half-Life (if Radioactive)
73 Tantalum Ta 181 180.947 992 99.988
74 Tungsten (wolfram) W 184 183.950 928 30.67
75 Rhenium Re 187 186.955 744 62.60; 𝛽− 4.6 × 1010 yr 76 Osmium Os 191
192
190.960 920
191.961 467
𝛽−, 𝛾 41.0
15.4 days
77 Iridium Ir 191
193
190.960 584
192.962 917
37.3
62.7
78 Platinum Pt 195 194.964 766 33.8
79 Gold Au 197
198
196.966 543
197.968 217
100
𝛽−, 𝛾 2.6935 days 80 Mercury Hg 202 201.970 617 29.80
81 Thallium Tl 205
208
204.974 401
207.981 988
70.476
𝛽−, 𝛾 3.053 min 82 Lead Pb 206
207
208
210
211
212
214
205.974 440
206.975 872
207.976 627
209.984 163
210.988 735
211.991 871
213.999 798
24.1
22.1
52.4
𝛼, 𝛽−, 𝛾 𝛽−, 𝛾 𝛽−, 𝛾 𝛽−, 𝛾
22.3 yr
36.1 min
10.64 h
26.8 min
83 Bismuth Bi 209
211
212
208.980 374
210.987 255
211.991 255
100
𝛼, 𝛽−, 𝛾 𝛽−, 𝛼, 𝛾
2.14 min
1.0092 h
84 Polonium Po 210
212
214
216
209.982 848
211.988 842
213.995 176
216.001 889
𝛼, 𝛾 𝛼, 𝛾 𝛼, 𝛾 𝛼, 𝛾
138.376 days
45.1 s
163.69 𝜇s 150 ms
85 Astatine At 218 218.008 684 𝛼, 𝛽− 1.6 s 86 Radon Rn 220
222
220.011 368
222.017 570
𝛼, 𝛾 𝛼, 𝛾
55.6 s
3.825 days
87 Francium Fr 223 223.019 733 𝛼, 𝛽−, 𝛾 21.8 min 88 Radium Ra 224
226
228
224.020 186
226.025 402
228.031 064
𝛼, 𝛾 𝛼, 𝛾 𝛽−, 𝛾
3.66 days
1.6 × 103 yr
5.75 yr
89 Actinium Ac 227
228
227.027 750
228.031 015
𝛼, 𝛽−, 𝛾 𝛽−, 𝛾
21.77 yr
6.13 h
90 Thorium Th 228
231
232
234
228.028 715
231.036 298
232.038 054
234.043 593
𝛼, 𝛾 𝛽−, 𝛾
100; 𝛼, 𝛾 𝛽−, 𝛾
1.913 yr
1.0633 days
1.405 × 1010 yr
24.10 days
91 Protactinium Pa 231
234
237
231.035 880
234.043 303
237.051 140
𝛼, 𝛾 𝛽−, 𝛾 𝛽−, 𝛾
3.276 × 104 yr
6.70 h
8.7 min
92 Uranium U 232
233
235
236
238
239
232.037 130
233.039 628
235.043 924
236.045 562
238.050 784
239.054 289
𝛼, 𝛾 𝛼, 𝛾
0.7200; 𝛼, 𝛾 𝛼, 𝛾
99.2745; 𝛼, 𝛾 𝛽−, 𝛾
68.9 yr
1.592 × 105 yr
7.037 × 108 yr
2.342 × 107 yr
4.468 × 109 yr
23.47 min
93 Neptunium Np 239 239.052 933 𝛽−, 𝛾 2.355 days 94 Plutonium Pu 239
242
239.052 157
242.058 737
𝛼, 𝛾 𝛼, 𝛾
2.411 × 104 yr
3.763 × 105 yr
95 Americium Am 243 243.061 375 𝛼, 𝛾 7.380 × 103 yr
Appendix F Selected Isotopes A-9
Appendix F Selected Isotopes (continued)
Atomic No. Z Element Symbol
Atomic Mass No. A
Atomic Mass (u)
% Abundance, or Decay Mode if Radioactive
Half-Life (if Radioactive)
96 Curium Cm 245 245.065 483 𝛼, 𝛾 8.5 × 103 yr 97 Berkelium Bk 247 247.070 300 𝛼, 𝛾 1.38 × 103 yr 98 Californium Cf 249 249.074 844 𝛼, 𝛾 350.6 yr 99 Einsteinium Es 254 254.088 019 𝛼, 𝛾, 𝛽− 275.7 days 100 Fermium Fm 253 253.085 173 EC, 𝛼, 𝛾 3.00 days 101 Mendelevium Md 255 255.091 081 EC, 𝛼 27 min 102 Nobelium No 255 255.093 260 EC, 𝛼 3.1 min 103 Lawrencium Lr 257 257.099 480 𝛼, EC 646 ms 104 Rutherfordium Rf 261 261.108 690 𝛼 1.08 min 105 Dubnium Db 262 262.113 760 𝛼 34 s
A-10
Chapter 1 CYU 1: (a) Yes. (b) No.
CYU 2: No.
CYU 3: a, b, c, f
CYU 4: No.
CYU 5: b, d
CYU 6: (a) 11 m (b) 5 m
CYU 7: No.
CYU 8: Yes.
CYU 9: (a) The magnitude of B→ is equal to the magnitude of A→.
(b) The direction of B→ is opposite to the direction of A→ .
CYU 10: Vector A→ is perpendicular to vector B→.
CYU 11: Vector A→ points in the same direction as vector B→.
CYU 12: A→ and D→
CYU 13: (a) Ax is − and Ay is + (b) Bx is + and By is − (c) Rx is + and Ry is +
CYU 14: No.
CYU 15: Yes.
CYU 16: (a) Ax = 0 units and Ay = +12 units (b) Ax = −12 units and Ay = 0 units (c) Ax = 0 units and Ay = −12 units (d) Ax = +12 units and Ay = 0 units
CYU 17: No.
CYU 18: a
Chapter 2 CYU 1: 0 m
CYU 2: scalar quantity
CYU 3: No.
CYU 4: a
CYU 5: average velocity = 2.7 m/s due east, average speed = 8.0 m/s
CYU 6: Yes.
CYU 7: No.
CYU 8: c
CYU 9: zNo.
CYU 10: No.
CYU 11: the rifl e with the short barrel
CYU 12: 1.73 υ
CYU 13: a
CYU 14: b
CYU 15: b
CYU 16: b
Chapter 3 CYU 1: b
CYU 2: c
CYU 3: a and c
CYU 4: (a) Yes; when the object is at its highest point.
(b) No.
CYU 5: No.
CYU 6: b
CYU 7: (a) when the ball is at its highest point in the trajectory
(b) at the initial and fi nal positions of the motion
CYU 8: Yes.
CYU 9: Both bullets reach the ground at the same time.
CYU 10: (a) The displacement is greater for the stone thrown horizontally.
(b) The impact speed is greater for the stone thrown horizontally.
(c) The time of fl ight is the same for both stones.
CYU 11: No.
CYU 12: Ball A has the greater launch speed.
CYU 13: (a) +70 m/s (b) +30 m/s (c) +40 m/s (d) −60 m/s
CYU 14: No.
CYU 15: The two times are the same.
CYU 16: (a) The range toward the front is the same as the range toward the rear.
(b) The range toward the front is greater than the range toward the rear.
CYU 17: swimmer A
Chapter 4 CYU 1: b
CYU 2: c
CYU 3: d
CYU 4: No, because two or more forces can cancel each other, leading to a net force of zero.
CYU 5: c
CYU 6: a and d
CYU 7: b
CYU 8: Yes, because the ratio of the two weights depends only on the masses of the ob-
jects, which are the same on the earth
and on Mars.
CYU 9: a
CYU 10: d
CYU 11: No.
CYU 12: a
CYU 13: b
CYU 14: c
CYU 15: To pull, because the upward component of the pulling force reduces the normal
force and, therefore, also reduces the
force of kinetic friction acting on the sled.
CYU 16: 43°
CYU 17: c, a, b
CYU 18: a
CYU 19: a
CYU 20: b
CYU 21: d
CYU 22: No, because there must always be a ver- tical (upward) component of the tension
force in the rope to balance the weight
of the crate.
CYU 23: c
CYU 24: No, because the transfer described does not change the total mass being
pulled by the engine.
CYU 25: a
Chapter 5 CYU 1: (a) The velocity is due south and the
acceleration is due west.
(b) The velocity is due west and the acceleration is due north.
CYU 2: Yes, if you are going around a curve. CYU 3: the person at the equator CYU 4: a and b
Answers to Check Your Understanding
CYU 5: AB or DE, CD, BC
CYU 6: (a) 4r (b) 4r
CYU 7: No.
CYU 8: the same
CYU 9: edge of the turntable
CYU 10: car B
CYU 11: less than
CYU 12: (a) less than (b) equal to
CYU 13: (a) Yes. (b) Yes. (c) Yes. (d) Yes.
CYU 14: vertical
Chapter 6 CYU 1: b
CYU 2: d
CYU 3: d
CYU 4: a
CYU 5: No.
CYU 6: c
CYU 7: false
CYU 8: c
CYU 9: a
CYU 10: a, b, and c
CYU 11: b
CYU 12: d
CYU 13: b and d
CYU 14: e
CYU 15: c
CYU 16: a
CYU 17: No.
Chapter 7 CYU 1: No.
CYU 2: The total linear momentum is approx- imately zero because of the random
directions and random speeds of the
moving people.
CYU 3: (a) Yes. (b) No.
CYU 4: (a) No. (b) Yes.
CYU 5: b
CYU 6: (a) No. (b) The impulse of the thrust is equal in
magnitude and opposite in direction
to the impulse of the force due to air
resistance.
CYU 7: (a) No. (b) No.
CYU 8: equal to
CYU 9: Yes.
CYU 10: a
CYU 11: decrease
CYU 12: (a) No. (b) decrease
CYU 13: b, c, d
CYU 14: the cannonball
CYU 15: d
CYU 16: No. It is the total kinetic energy of the system that is the same before and after the collision.
CYU 17: c
CYU 18: nearer the heavier end
CYU 19: (a) zero (b) Yes, opposite to the motion of the
sunbather.
CYU 20: a
Chapter 8 CYU 1: Both axes lie in the plane of the paper.
One passes through point A and is parallel to the line BC. The other passes through point A and the midpoint of the line BC.
CYU 2: B, C, A
CYU 3: No. The instantaneous angular speed of each blade is the same, but the blades
are rotating in opposite directions.
CYU 4: c
CYU 5: 1.0 rev/s
CYU 6: b
CYU 7: Case A
CYU 8: a
CYU 9: at the north pole or at the south pole
CYU 10: c
CYU 11: 0.30 m
CYU 12: d
CYU 13: c
CYU 14: b
CYU 15: 8.0 m/s2
CYU 16: a
CYU 17: Among the many possible answers are the motions of a Frisbee through the air,
the earth in its orbit, a twirling baton
that has been thrown into the air, the
blades on a moving lawn mower cutting
the grass, and an ice skater performing a
quadruple jump.
Chapter 9 CYU 1: 0°, 45°, 90°
CYU 2: greater torque
CYU 3: (a) Yes, if the lever arm is very small. (b) Yes, if the lever arm is very large.
CYU 4: the box at the far right
CYU 5: (a) C (b) A (c) B
CYU 6: Additional forces are necessary.
CYU 7: a
CYU 8: b
CYU 9: Bob
CYU 10: A, B, C
CYU 11: axis B
CYU 12: (a) remains the same (b) remains the same
CYU 13: (a) remains the same (b) increases
CYU 14: (a) Both have the same translational speed.
(b) Both have the same translational speed.
CYU 15: axis B
CYU 16: solid sphere, solid cylinder, spherical shell, hoop
CYU 17: (a) decreases (b) remains the same
CYU 18: decrease
CYU 19: greater than
CYU 20: No.
Chapter 10 CYU 1: No, because the force of gravity acting
on the ball is constant, unlike the restor-
ing force of simple harmonic motion.
CYU 2: Both boxes experience the same net force due to the springs.
CYU 3: 180 N/m
Answers to Check Your Understanding A-11
A-12 Answers to Check Your Understanding
CYU 4: The spring stretches more when attached to the wall.
CYU 5: object II
CYU 6: at the position x = 0 m
CYU 7: The particle can cover the greater distance in the same time because at
larger amplitudes the maximum speed
is greater.
CYU 8: The same amount of energy is stored in both cases, since the elastic potential
energy is proportional to the square of
the displacement x.
CYU 9: b, c, a
CYU 10: The amplitude is unchanged. The frequency and maximum speed each
decrease by a factor of √2.
CYU 11: a
CYU 12: the simple-pendulum clock, because its period depends on the acceleration due
to gravity
CYU 13: Use a shoe and the shoe laces to make a simple pendulum whose period is related
to the magnitude g of the acceleration due to gravity (see Equations 10.5
and 10.16). Measure the period of your
pendulum and calculate g.
CYU 14: Yes, because for small angles the period of each person’s motion is the same.
CYU 15: Yes, because the frequency depends on the mass of the car and its occupants
(see Equations 10.6 and 10.11).
CYU 16: υ = d 2π√
k m
CYU 17: b
CYU 18: The rod with the square cross section is longer.
CYU 19: No, because the value of B given in Table 10.3 applies to solid aluminum,
not to a can that is mostly empty space.
CYU 20: No, because pressure involves a force that acts perpendicular to an area. In Equation 10.18 for shear deformation,
the force acts parallel, not perpendicu-
lar, to the area A (see Figure 10.29).
CYU 21: Face B experiences the largest stress, and face C experiences the smallest
stress.
Chapter 11 CYU 1: (a) outward (b) inward
CYU 2: b
CYU 3: a
CYU 4: (a) increase (b) decrease (c) remain constant
CYU 5: A noticeable amount of water will remain in the tank.
CYU 6: b
CYU 7: Yes; see Equation 11.4, in which P 2 is
the pressure at his wrist and P 1 is the
pressure above the water.
CYU 8: c
CYU 9: Both beams experience the same buoyant force.
CYU 10: (a) The readings are the same. (b) The fi nal reading is greater than
the initial reading.
CYU 11: No. You fl oat because the weight of the water you displace equals your weight.
Each weight is proportional to g, so its value makes no diff erence.
CYU 12: No. F B depends only on the weight of
the water she displaces, which doesn’t
change.
CYU 13: b
CYU 14: No.
CYU 15: d
CYU 16: c
CYU 17: e
CYU 18: c
CYU 19: c
CYU 20: b
CYU 21: a
CYU 22: c
Chapter 12 CYU 1: 178 °X
CYU 2: (a) No. (b) Yes. (c) No.
CYU 3: It decreases (see Equations 10.5 and 10.16).
CYU 4: With equal values for α, concrete and steel expand (contract) by the same
amount as the temperature increases
(decreases), thus minimizing problems
with thermal stress.
CYU 5: The bottom is bowed outward, because it acts like a bimetallic strip.
CYU 6: b and d
CYU 7: cooled
CYU 8: No. When the temperature changes, the change in volume of the cavity within
the glass would exactly compensate for
the change in volume of the mercury,
which would never rise or fall in the
capillary tube of the thermometer.
CYU 9: Less than. The buoyant force is equal to the weight of the displaced water (see
Section 11.6, Archimedes’ principle),
which is proportional to the water’s
density. Here, warmer water has a
smaller density than cooler water does
(see Figure 12.20).
CYU 10: a and b
CYU 11: the object with the smaller mass
CYU 12: c, b, d, a
CYU 13: Because heat is released when the water freezes at 0 °C (consistent with
the latent heat of fusion of water), and
this heat warms the blossoms.
CYU 14: c, a, b
CYU 15: No, because at sea level water boils at a higher temperature and the stove may
not generate enough heat.
CYU 16: Because water in an open pot boils at 100 °C, thus preventing the temperature
from rising further, whereas under the
elevated pressure in the autoclave water
has a boiling point above 100 °C.
CYU 17: Boiling water has a vapor pressure of one atmosphere, and the cool water
in the sealed jar has a lower vapor
pressure. The excess external pressure
creates a net force pushing on the lid,
making it hard to unscrew.
CYU 18: Under pressure in the sealed bottle, the soda has a freezing point lower
than normal (see Figure 12.35b). The outside temperature is not cold enough
to freeze it. When the bottle is opened,
the pressure on the liquid decreases to
one atmosphere, and the freezing point
rises to its normal value. The liquid is
now cold enough to freeze.
CYU 19: As the water vapor is removed, more forms in an attempt to reestablish equilib-
rium between liquid and vapor. When the
pumping is rapid, the required latent heat
is supplied mostly by the remaining liquid,
which cools and eventually freezes.
CYU 20: 100%
CYU 21: Yes. The dew points on the two nights could be diff erent, Tuesday’s being
higher than Monday’s due to a greater
partial pressure of water vapor in the
air on Tuesday than on Monday.
CYU 22: The air above the swimming pool probably has a greater partial pressure
of water vapor (due to ineffi cient hu-
midity control) and, therefore, a higher
dew point than that in the other room.
Evidently, the temperature at the inner
window-surfaces is below the dew point
of the room with the swimming pool but
above the dew point in the other room.
Chapter 13 CYU 1: a
CYU 2: b
CYU 3: the house with the snow on the roof
CYU 4: b
CYU 5: c
CYU 6: c
CYU 7: hollow, air-fi lled strands
CYU 8: c
CYU 9: b
CYU 10: forced convection
CYU 11: strip B
CYU 12: a
CYU 13: d
CYU 14: b
CYU 15: e
Chapter 14 CYU 1: Both have the same number of mole-
cules, but oxygen has the greater mass.
CYU 2: In general, the number of molecules would be diff erent. But they could be
the same, if the molecular masses of the
two types of molecules happen to be the
same.
CYU 3: 66.4%
CYU 4: The ideal gas law gives the pressure as P = nRT/V, where T and V are constant. The fan reduces n in the house and increases it in the attic, so pressure
decreases in the house and increases in the
attic. The fan has a harder job pushing air
out against the higher attic pressure.
CYU 5: The ideal gas law gives the gas pressure as P = nRT/V, where V and n are constant. As T increases, the pressure in- creases and could cause the can to burst.
CYU 6: The ideal gas law gives the gas pressure as P = nRT/V, where V and n are constant. As T increases, the pressure increases.
CYU 7: The ideal gas law gives the gas pressure as P = nRT/V, where T and n are constant. As V decreases due to the incoming tide, the pressure increases,
and your ears pop inward, as if you were
climbing down a mountain.
CYU 8: The ideal gas law gives the gas volume as V = nRT/P, where T and n are constant. As the pressure P decreases during the balloon’s ascent,
the volume increases. The balloon
would overinfl ate if not underinfl ated
to start with.
CYU 9: Boyle’s law gives the fi nal pressure in the bottle after the cork is pressed
in: Pf = Pi (Vi /Vf), where Vi /Vf is the volume of air above the wine before
the cork is pressed in divided by the
volume after the cork is pressed in.
This ratio is much larger for the full
bottle than for the half-full bottle, cre-
ating a pressure large enough to push
the cork out.
CYU 10: Xenon has the greatest and argon the smallest temperature.
CYU 11: less than, which follows directly from the impulse–momentum theorem
CYU 12: No. The average kinetic energy is pro- portional to the Kelvin, not the Celsius,
temperature.
CYU 13: It remains unchanged.
CYU 14: argon
CYU 15: υrms, new /υrms, initial = 0.707
CYU 16: L must be small and there must be many alveoli so that the total eff ective
area A is large.
CYU 17: c, a, b
Chapter 15 CYU 1: d
CYU 2: c
CYU 3: b
CYU 4: A → B: Q = + and W = + B → C: ∆U = + and W = 0
CYU 5: a
CYU 6: b
CYU 7: a
CYU 8: c
CYU 9: c
CYU 10: c
CYU 11: b
CYU 12: No, because Carnot’s principle only states that a reversible engine operating between
two temperatures is more effi cient than an
irreversible engine operating between the
same temperatures.
CYU 13: d
CYU 14: d
CYU 15: b
CYU 16: c
CYU 17: a
CYU 18: c
CYU 19: b
CYU 20: a
CYU 21: d
CYU 22: c and d
CYU 23: the popcorn that results from the kernels; a salad after it has been tossed;
a messy apartment
CYU 24: b
CYU 25: c
Chapter 16 CYU 1: c
CYU 2: No. The coil moves back and forth in simple harmonic motion.
CYU 3: The wavelength increases.
CYU 4: The person pulling on string B should pull harder to increase the tension in the string.
CYU 5: In Equation 16.2, the speed would be in- fi nitely large if m were zero, so it would take no time at all.
CYU 6: decrease
CYU 7: No, because the particles exhibit simple harmonic motion, in which the acceler-
ation is not always zero.
CYU 8: increase
CYU 9: a
CYU 10: No, because each particle executes simple harmonic motion as the wave passes by.
CYU 11: hot day
CYU 12: CO and N2 CYU 13: increase
CYU 14: Large outer ears intercept and direct more sound power into the auditory
system than smaller ones do.
CYU 15: No, because not all points on the surface are at the same distance from the source.
Answers to Check Your Understanding A-13
CYU 16: No, because it is the intensities I1 and I2 that add to give a total intensity Itotal. The intensity levels β1 and β2 do not add to give a total intensity level βtotal .
CYU 17: (a) 1/4 (b) 2
CYU 18: (a) f o is smaller than f
s , and f
o
decreases during the fall.
(b) f o is greater than f
s , and f
o increases
during the fall.
CYU 19: No, because the observed frequency is less than the source frequency, so
the car is moving away from him.
CYU 20: (a) greater in air (b) greater under water
CYU 21: No, because there is no relative motion of the cars.
CYU 22: (a) minus sign in both places (b) the truck driver
Chapter 17 CYU 1: (a) −3 cm
(b) −2 cm
CYU 2: No, because if the two sound waves have the same amplitude and
frequency, they might cancel in a way
analogous to that illustrated in Figure
17.2b and no sound will be heard.
CYU 3: b
CYU 4: c
CYU 5: a
CYU 6: d
CYU 7: a
CYU 8: c
CYU 9: b
CYU 10: d
CYU 11: (a) 4 (b) 3 (c) node (d) 110 Hz
CYU 12: b
CYU 13: d
CYU 14: b
CYU 15: (a) antinode (b) node (c) 14λ (d) lowered
CYU 16: b
CYU 17: c (14λ is the distance between an antinode and an adjacent node.)
CYU 18: a
Chapter 18 CYU 1: c
CYU 2: +3.2 × 10−13 C on object A and −3.2 × 10−13 C on object B
CYU 3: +1.6 × 10−13 C on object A and −3.2 × 10−13 C on object B
CYU 4: b and e
CYU 5: Yes, because the charge on the balloon will induce a slight charge of opposite
polarity in the surface of the ceiling,
analogous to that in Figure 18.8.
CYU 6: a
CYU 7: b
CYU 8: C, A, B
CYU 9: the electron, because, being less massive, it has the greater acceleration
CYU 10: No, because the force of the spring changes direction when the spring
is stretched compared to when it is
compressed, while the electrostatic force
does not have this characteristic.
CYU 11: d
CYU 12: 0 N/C
CYU 13: (a) corner C (b) negative (c) greater
CYU 14: a
CYU 15: (a) No. (b) No.
CYU 16: For rod A, the fi eld points perpendicularly away from the rod. For
rod B, it points parallel to the rod and
is directed from the positive toward the
negative half.
CYU 17: (a) false (b) false (c) true (d) false (e) false
CYU 18: d
CYU 19: The fl ux does not change, as long as the charge remains within the Gaussian
surface.
CYU 20: The same fl ux passes through each, since each encloses the same net charge.
CYU 21: (a) q1 and q2 (b) q1, q2, and q3
Chapter 19 CYU 1: (a) Yes.
(b) No.
(c) Yes. (d) Yes.
CYU 2: The work is the same in all three cases (see Equation 19.4).
CYU 3: The electron arrives at a plate fi rst.
CYU 4: a
CYU 5: b
CYU 6: c
CYU 7: a
CYU 8: d
CYU 9: (a) remains the same (b) decreases
CYU 10: the electron
CYU 11: (a) +2.0 V (b) 0 V (c) +2.0 V
CYU 12: The electric fi eld is zero.
CYU 13: b
CYU 14: a
CYU 15: c
CYU 16: (a) bottom of a valley (b) top of a mountain
CYU 17: (a) decreases (b) increases (c) increases (d) increases
CYU 18: (a) decreases (b) increases (c) remains the same (d) increases
Chapter 20 CYU 1: d
CYU 2: 0.50 A
CYU 3: b
CYU 4: a
CYU 5: b, d, and e
CYU 6: c (A value for the current is also needed.)
CYU 7: a
CYU 8: c
CYU 9: b and d
CYU 10: The 75-W bulb. See Equation 20.15c.
CYU 11: d
CYU 12: e
CYU 13: in parallel
CYU 14: b
A-14 Answers to Check Your Understanding
CYU 15: c
CYU 16: a, b, d, and e
CYU 17: There are two ways. One is to form two groups of two parallel resistors and then
connect the groups in series. The other is
to form two groups of two series resistors
and then connect the groups in parallel.
CYU 18: Junction rule: I1 + I3 = I2 Loop rule, loop ABCD: 3.0 V + 7.0 V + I3 R3 = I1 R1 Loop rule, loop BEFC: 5.0 V = I3 R3 + 7.0 V + I2 R2
CYU 19: c
CYU 20: b
CYU 21: ohm × farad = (volt /ampere)(coulomb/volt)
= coulomb/ampere
= coulomb/(coulomb/second)
= second
CYU 22: e
Chapter 21 CYU 1: c
CYU 2: d
CYU 3: (a) Yes. (b) No, because the particle could move
either parallel or anti-parallel to the
magnetic fi eld.
CYU 4: b
CYU 5: d
CYU 6: particle 3
CYU 7: b
CYU 8: c
CYU 9: b
CYU 10: c
CYU 11: (a) The direction of the magnetic force reverses.
(b) The direction of the magnetic force does not change.
CYU 12: B and D (a tie), A, C
CYU 13: a
CYU 14: (a) repelled (b) repelled
CYU 15: (a) attracted (b) repelled
CYU 16: c
CYU 17: a
CYU 18: Part a: There is a point to the right of both wires where the total magnetic
fi eld is zero. Part b: There is a point between the wires where the total mag-
netic fi eld is zero. This point is closer to
the wire carrying the current I 2 .
CYU 19: A, D, C, B CYU 20: d CYU 21: No, because aluminum is a non-
ferromagnetic material.
CYU 22: b
Chapter 22 CYU 1: No. With both the magnet and coil
moving at the same velocity with respect
to the earth, there is no relative motion
between the magnet and the coil, which is
needed for there to be an induced current
in the coil.
CYU 2: d
CYU 3: a
CYU 4: b
CYU 5: c
CYU 6: b
CYU 7: A lightning bolt is a large electric current that changes in time and, thus, produces a
magnetic fi eld that also changes in time.
When this changing fi eld passes through a
coil or loop of wire in an appliance, it can,
via Faraday’s law, create an induced emf,
which can lead to an induced current.
CYU 8: c
CYU 9: a and d
CYU 10: a
CYU 11: b
CYU 12: Answer 1: downward and decreasing Answer 2: upward and increasing
CYU 13: c
CYU 14: d
CYU 15: b
CYU 16: With the headlights off , the engine does not need to do the work of
keeping the battery charged.
CYU 17: a
CYU 18: c
CYU 19: b
CYU 20: b and d
Chapter 23 CYU 1: The ratio decreases by a factor of 3.
CYU 2: (a) the circuit containing the inductor (b) the circuit containing the resistor
CYU 3: less than
CYU 4: decreases
CYU 5: decreases
CYU 6: d
CYU 7: (a) increases (b) increases
CYU 8: a
CYU 9: (a) remains the same (b) decreases
CYU 10: in phase (see Equation 23.8, in which XL = XC)
CYU 11: (a) Yes. (b) Yes.
CYU 12: a
CYU 13: (a) left to right (b) left to right
Chapter 24 CYU 1: d
CYU 2: a
CYU 3: because, according to Faraday’s law of electromagnetic induction, the emf
depends on how rapidly the magnetic
fi eld of the wave is changing and this
is determined by the frequency of the
wave
CYU 4: e
CYU 5: d
CYU 6: b
CYU 7: No. The same Doppler change results when the star moves away from the
earth and when the earth moves away
from the star. Only the relative motion
between the star and the earth can be
detected.
CYU 8: B, A, C
CYU 9: Yes.
CYU 10: The light intensity that is not transmitted is absorbed by the polarizer
and the analyzer. The polarizer absorbs
one-half of the incident intensity, and
the analyzer absorbs four-tenths of the
incident intensity.
CYU 11: unpolarized: c horizontally polarized: b
vertically polarized: c
CYU 12: because the transmission axis of the Polaroid material is nearly horizontal,
in the same direction as the polarized
light refl ected from the lake
Answers to Check Your Understanding A-15
Chapter 25 CYU 1: 55°
CYU 2: Yes.
CYU 3: Yes.
CYU 4: finside = +0.30 m, foutside = −0.30 m
CYU 5: (a) concave (b) The sodium unit and engine are
located at the focal point of the
mirror.
CYU 6: Open the surface up to produce a more gently curving shape.
CYU 7: No.
CYU 8: (a) upright (b) upside down
CYU 9: (a) Yes, provided the object distance is greater than the focal length of the
mirror.
(b) It is not possible for a convex mirror to project an image directly onto a
screen.
CYU 10: (a) No. (b) No.
CYU 11: (a) The magnitude of the image distance becomes larger.
(b) The magnitude of the image height becomes larger.
CYU 12: (a) No. You can see yourself anywhere on the principal axis.
(b) You cannot see yourself when you are between the center of curvature
and the focal point of the mirror
because your image is behind you.
CYU 13: A, D, and E
CYU 14: The image will never be located beyond the focal point (behind the
mirror).
Chapter 26 CYU 1: slab B
CYU 2: liquid B
CYU 3: Yes. To see why, apply Snell’s law at the air–water interface and at the
water–glass interface.
CYU 4: the one fi lled with water
CYU 5: liquid A
CYU 6: c
CYU 7: b
CYU 8: a
CYU 9: c
CYU 10: The critical angle for a water–air interface is 48.8° (see Equation 26.4).
Any light emitted at an angle greater
than 48.8° with respect to the vertical
is incident on the surface at an angle
exceeding the critical angle. It is totally
internally refl ected and doesn’t exit the
water.
CYU 11: No. To see why, apply Snell’s law at both surfaces of the glass slab and use
Equation 26.4.
CYU 12: c (They are most eff ective when the angle of incidence is the Brewster
angle and the refl ected light is 100%
polarized.)
CYU 13: liquid A
CYU 14: a (Since n = 1.520 for red light and n = 1.538 for violet-colored light, the critical angle for total internal
refl ection is greater for red than for
violet-colored light.)
CYU 15: b
CYU 16: Yes.
CYU 17: a
CYU 18: the lens
CYU 19: converging lens, do = 12 f
CYU 20: d
CYU 21: the glasses of the farsighted person, since they use converging lenses
CYU 22: 13 cm
CYU 23: Light normally passes from air (n = 1.00) into the cornea (n = 1.38), at which time most of the eye’s
refraction of the light occurs. If water
(n = 1.33) replaces air, the similarity of the index of refraction of water to
that of the cornea reduces the eye’s
normal refraction and causes blurred
vision. Goggles preserve the air–cornea
boundary.
CYU 24: b
CYU 25: hawk, kestrel, eagle
CYU 26: a
CYU 27: 0.042 rad
CYU 28: b
CYU 29: the longer telescope
CYU 30: microscope
CYU 31: c, d, e, f
CYU 32: because chromatic aberration is related to the refraction of light and not to the
refl ection of light
Chapter 27 CYU 1: (a) constructive
(b) destructive (c) destructive
CYU 2: c
CYU 3: Yes.
CYU 4: a
CYU 5: (a) d 1 and 𝜆
2
(b) d 2 and 𝜆
1
CYU 6: (a) The pattern would be the same. (b) The positions of the light and dark
fringes would be interchanged.
CYU 7: No, because 𝜃 in Equations 27.1 and 27.2 approaches 90° as 𝜆 becomes larger
and larger.
CYU 8: b
CYU 9: c
CYU 10: enhances
CYU 11: (a) A and C (b) B
CYU 12: c
CYU 13: b
CYU 14: (a) broadens (b) contracts
CYU 15: a
CYU 16: c
CYU 17: a, c, b
CYU 18: Yes.
CYU 19: small f-number setting
CYU 20: (a) the maximum that is closer to the central maximum
(b) away from the central maximum
CYU 21: The distance between the bright fringes would decrease.
Chapter 28 CYU 1: d
CYU 2: a, b
CYU 3: C, B, A
CYU 4: No, because the term 𝜐2/c2 in Equations 28.1 and 28.2 would then be zero.
CYU 5: c
CYU 6: c, d
CYU 7: No, because the two diagonals are perpendicular, so that diagonal AC is
contracted, whereas diagonal BD is not
contracted.
A-16 Answers to Check Your Understanding
CYU 8: greatest mass: c, smallest mass: b
CYU 9: a, because then they have more electric potential energy (see Example 8 in
Chapter 19)
CYU 10: b, because the fully charged capacitor stores electric potential energy (see
Section 19.5)
CYU 11: a. The work is the change in kinetic energy, which is proportional to the
mass (see the work–energy theorem
in Section 6.2). The electron has the
smaller mass.
CYU 12: c
Chapter 29 CYU 1: No.
CYU 2: (a) red (b) violet
CYU 3: No.
CYU 4: b
CYU 5: a
CYU 6: (a) increases (b) increases (c) remains the same (d) remains the same
CYU 7: less than
CYU 8: c
CYU 9: a
CYU 10: No. Photon collisions would cause spinning in a direction from the shiny
side of a panel toward the black side.
CYU 11: decreases
CYU 12: b
CYU 13: decreases
CYU 14: b
Chapter 30 CYU 1: b
CYU 2: d
CYU 3: The absorption lines belong only to the Lyman series, since very few electrons
are present with n = 2 or n = 3.
CYU 4: No, because the location of the electron in a given quantum mechanical energy
state is uncertain.
CYU 5: when the electron is in the n = 1 state, because then the only possible value for
the orbital quantum number is ℓ = 0
CYU 6: (a) No, because the Bohr model uses the same quantum number n for the total energy and the orbital angular
momentum (see Equations 30.13
and 30.8).
(b) Yes, because quantum mechanics uses the quantum number n for the total energy but the quantum number
ℓ for the orbital angular momentum.
CYU 7: (a) Yes, because the Bohr model uses the same quantum number n for the orbital angular momentum and
the total energy (see Equations 30.8
and 30.13).
(b) No, because quantum mechanics uses the quantum number ℓ for
the orbital angular momentum but
the quantum number n for the total energy.
CYU 8: 1s2 2s2 2p6 3s2 3p6 4s2 3d10 4p6
CYU 9: (a) No. (b) Yes.
CYU 10: b
CYU 11: c
CYU 12: a
CYU 13: c
CYU 14: d
CYU 15: a
Chapter 31 CYU 1: c, d
CYU 2: a
CYU 3: No, because they could have diff erent numbers of protons (diff erent atomic
numbers).
CYU 4: Yes, because the total number A of nucleons could be the same, and it is the
value of A that determines the radius.
CYU 5: d, c, a, b
CYU 6: c
CYU 7: d
CYU 8: It is not possible, because the total mass of the decay products is greater than the
mass of the parent nucleus, 23892U, indic-
ating that energy would not be released.
CYU 9: b
CYU 10: Yes, because the decay of any single nucleus occurs randomly and can
happen at any moment.
CYU 11: Yes.
CYU 12: b, because the gold statue does not contain carbon atoms
CYU 13: too small
CYU 14: No, because in 700 years the activity of a sample would have decreased to
an immeasurably small fraction of its
initial value.
CYU 15: e
Chapter 32 CYU 1: Yes, if the absorbed dose of the radiation
is diff erent for each type of radiation
(see Equation 32.4).
CYU 2: c
CYU 3: neutrons, α particles, 𝛾 rays
CYU 4: c
CYU 5: (a) because it violates the conservation of nucleon number
(b) because it violates the conservation of nucleon number
(c) because it violates the conservation of electric charge
CYU 6: d
CYU 7: electrons, protons, neutrons
CYU 8: No, because the binding energy per nucleon is greater for the original
nucleus than for the two fragments, as
indicated in Figure 31.5.
CYU 9: b and d
CYU 10: a, b, and c
CYU 11: No, because the binding energy per nucleon is greater for the original
nuclei than for the nucleus resulting
from the fusion, as indicated in
Figure 32.8.
CYU 12: b and d
CYU 13: a
Answers to Check Your Understanding A-17
Chapter 1 1. 124 m2
3. 10 159 m
5. 0.75 m2/s
7. 2.0 magnums
9. 29.6 mL
11. [M]/[T]2
13. 80.1 km, 25.9° south of west
15. 0.25 m
17. 54.1 m
19. 35.3°
21. 1.2 × 102 m
23. (a) 551 newtons, 36.1° north of west (b) 551 newtons, 36.1° south of west
25. smallest magnitude: F1 →
+ F3 →
= 10.0 newtons,
due east; largest magnitude: F3 →
+ F4 →
= 70.0
newtons, due west
27. (a) 1200 m (b) 26° south of east
29. (a) 45.6 cm (b) 39.4 cm
31. (a) 5600 newtons (b) along the dashed line
33. (a) 78 newtons (b) 34°
35. (a) C→ has the largest x component. (b) B→ has the largest y component.
37. (a) 45° (b) 35° (c) 55°
39. 222 m, 55.8° below the −x axis
41. Vectors A→ and C→ are equal. Each has a mag- nitude of 100.0 m, and each is oriented at an
angle of 36.9° above the +x axis.
43. (a) 25.0° above the +x axis. (b) 34.8 newtons
45. 7.1 m, 9.9° north of east
47. 4790 newtons, 67.2° south of east
49. 0.90 km, 56° north of west
51. (a) 2.7 km (b) 6.0 × 101 degrees, north of east
53. 6.88 km, 26.9°
55. (a) 178 units (b) 164 units
57. (a) 64 m (b) 37° south of east
59. (a) 15.8 m/s (b) 6.37 m/s
61. (a) 147 km (b) 47.9 km
63. (a) 9.4 ft (b) 69°
65. (a) 10.4 units (b) 12.0 units
67. (a) 142 newtons, 67° south of east (b) 142 newtons, 67° north of west
69. x component: −288 units y component: +156 units
71. 20.4 m; 59.9°
73. (a) 2780 m (b) 37.0° south of west (c) 6.60°
Chapter 2 1. 9.1
3. 5 × 104 yr
5. (a) +8.0 m/s (b) −8.0 m/s (c) +2.0 × 101 m/s
7. 28 m
9. 52 m
11. (a) 2.67 × 104 m (b) 6.74 m/s, due north
13. 2.1 s
15. (a) 0 m/s2 (b) −14 m/s2
17. (a) 4.0 s (b) 4.0 s
19. (a) 18 m/s (b) 6.0 m/s (c) 6.0 m/s (d) 18 m/s
21. 8.18 m/s2
23. +8.0 m/s (Cycle A was initially traveling faster.)
25. (a) 1.5 m/s2 (b) 1.5 m/s2 (c) Car travels 76 m farther.
27. (a) 1.7 × 102 cm/s2 (b) 0.15 s
29. 3.1 m/s2, directed southward
31. −1.0 m/s2
33. 39.2 m
35. 52.8 m
37. 0.87 m/s2, in the same direction as the second car’s velocity
39. +25.7 m
41. 14 s
43. 44.1 m/s
45. d 1 = 0.018 m, d
2 = 0.071 m, d
3 = 0.16 m
47. 6.12 s
49. 1.08 s
51. (a) −7.9 m/s (b) 3.2 m
53. 1.1 s
55. −5.06 m
57. 0.767 m/s
59. (a) 3H (b) The answer to part (a) would be the same.
61. 0.40 s
63. −11 m/s
65. (a) positive for segments A and C, negative for segment B, zero for segment D
(b) +6.3 km/h for segment A, −3.8 km/h for segment B, +0.63 km/h for segment C, 0 km/h for segment D
67. 1.9 m/s2 for segment A, 0 m/s2 for segment B, 3.3 m/s2 for segment C
69. −8.3 km/h2
71. (a) 6.6 s (b) 5.3 m/s
73. (a) −9.80 m/s2 (The pebble is not decelerating.) (b) 5.7 m
75. 0.74 m/s
77. 2.3 min
79. +6.0 m/s2
81. 7.2 × 103 m
83. 73 s
85. 11.1 s
87. Car B wins by 0.22 s.
89. +62 m
91. (a) 80 m/s [at t = 2.0 s]; 160 m/s [at t = 4.0 s] (b) 80 m [at t = 2.0 s]; 320 m [at t = 4.0 s]
93. Your team needs to hike 3840 m 50.6° west of south to retrieve the drone.
Chapter 3 1. 2.8 m
3. 𝜐x = 11 m/s, vy = 13 m/s
5. 8.8 × 102 m
7. x = 75.3 km, y = 143 km
9. (a) 2.47 m/s2 (b) 2.24 m/s2
11. (a) 2.99 × 104 m/s (b) 2.69 × 104 m/s
13. 8.6 m/s
Answers to Odd-Numbered Problems
A-18
Answers to Odd-Numbered Problems A-19
15. (a) 2.8 m (b) 2.0 m
17. 9.4 mm
19. (a) 4.37 s (b) 93.5 m
21. 18 m/s
23. (a) 239 m/s, 57.1° with respect to the horizontal
(b) 239 m/s, 57.1° with respect to the horizontal
25. ax = 4.79 m/s2, ay = 7.59 m/s2
27. 30.0 m
29. 0.844 m
31. (a) 1.1 s (b) 1.3 s
33. 5.2 m
35. 33.2 m
37. (a) 1380 m (b) 66.0° below the horizontal
39. 56 m
41. 14.7 m/s
43. 42°
45. 21.9 m/s, 40.0° above the horizontal
47. 0.141° and 89.860°
49. D = 850 m, H = 31 m
51. 8.79 m/s, 81.5°
53. (a) 2.0 × 103 s (b) 1.8 × 103 m
55. (a) The answer is a drawing. (b) 38 m/s
57. 6.3 m/s, 18° north of east
59. (a) 41 m/s due east (b) 41 m/s due west
61. 2.3 m/s
63. 5.2 m/s, 52° west of south
65. 4.60 m/s
67. 5.4 m/s
69. (a) 1.78 s (b) 20.8 m/s
71. 14.1 m/s
73. 5.17 s
75. 14.9 m
77. 5.79 m/s
79. θ 1 = 28.1° and θ
2 = 67.7°
81. 11 m/s; 65°
83. 𝜐 0 = 44.7 m/s and θ = 77.6°
Chapter 4 1. 93 N
3. (a) +6 N (b) −24 N (c) −9.0 N
5. 32 N
7. 3560 N
9. (a) 3.6 N (b) 0.40 N
11. 30.9 m/s2, 27.2° above the +x axis
13. 10.3 m/s2, 21.9° above the horizontal
15. 1.20 m/s2, directed straight upward
17. 33 s
19. 18.4 N, 68° north of east
21. (a) 3.75 m/s2 (b) 2.4 × 102 N
23. (a) 5.1 × 10−6 N (b) 5.1 × 10−6 N
25. 9.6 × 10−9 N
27. 0.223 m/s2
29. (a) 5.67 × 10−5 N directed to the right (b) 3.49 × 10−5 N directed to the right (c) 9.16 × 10−5 N directed to the left
31. 1.76 × 1024 kg
33. 1.05
35. 178
37. x = +0.414 L
39. (a) 447 N (b) 241 N
41. (a) 0.97 (b) 0.82
43. (a) 1.6 × 104 N (b) 4.3 × 103 N
45. (a) 21.2 N (b) 23.8 N
47. (a) 390 N (b) 7.7 m/s, directed toward second base
49. 16.3 N
51. 68°
53. 1.00 × 102 N, 53.1° south of east
55. 11.6 N
57. 68 kg
59. 9.70 N
61. 62 N
63. 1.9 × 102 N
65. 0.141
67. 406 N
69. 0.29
71. 4290 N
73. 18.0 m/s2, 56.3° above the +x axis
75. (a) 1.0 × 102 N (b) 38 N
77. 160 N
79. 6.6 m/s
81. 2730 N
83. (a) 3.56 m/s2 (b) 281 N
85. 6.7 × 10−3 m/s2
87. 820 N
89. 8.7 s
91. (a) 13.7 N (b) 1.37 m/s2
93. 1.2 s
95. 120 N, directed straight upward
97. (a) 1.10 × 103 N (b) 931 N (c) 808 N
99. 39 N
101. 29 400 N
103. 1730 N, directed due west
105. (a) weight = 1.13 × 103 N, mass = 115 kg (b) weight = 0 N, mass = 115 kg
107. (a) 4.25 m/s2 (b) 1080 N
109. 141 N
111. (a) ∆TA = 0 N, ∆TB = −4.7 N, ∆TC = 0 N (b) ∆TA = 0 N, ∆TB = 0 N, ∆TC = +4.7 N
113. 0.78 m, 21° south of east
115. 4.4 s
117. (a) 0.60 m/s2 (b) 104 N (left string), 230 N (right string)
119. 1.65 m/s2, 34.6° above the x axis
121. 8000 N; −x direction
123. (a) 23.7° (b) 4.30 m/s2 (c) 9.21°
Chapter 5 1. 0.79 m/s2
3. 61°
5. 160 s
7. 6.9 m/s2
9. 332 m
11. 10 600 rev/min
13. (a) 1.2 × 104 N (b) 1.7 × 104 N
15. 22 m/s
17. 594 N
19. (a) 88 N (b) 181 N
21. 3500 N
23. (a) 3510 N (b) 14.9 m/s
25. 39°
27. 22 m/s
A-20 Answers to Odd-Numbered Problems
29. 2.12 × 106 N
31. 7690 m/s (satellite A), 7500 m/s (satellite B)
33. 1.33 × 104 m/s
35. 5.92 × 103 m/s
37. 12 m/s
39. (a) 4.65 × 1031 kg (b) 3.07 yr
41. (a) 1.70 × 103 N (b) 1.66 × 103 N
43. 17 m/s
45. 14 N (twelve o’clock), 18 N (six o’clock)
47. 21.0 m/s
49. 606 N
51. 3600
53. 1/27
55. 14.0 m/s
57. (a) 3.0 × 105 m/s2 (b) 3.1 × 104 g
59. 28°
61. 23 N (speed = 19.0 m/s), 77 N (speed = 38.0 m/s)
63. 25 m/s (automobile A); 18 m/s (automobile B)
65. (a) The fi gure shows three concentric cylinders where r
E > r
Mars > r
moon .
rmars rmoon
rE
(b) 115 m 49.7 m
300 m
(c) T = 34.8 s
Chapter 6 1. 2.2 × 103 J
3. −2.6 × 106 J (The work is negative because the retarding force points opposite to the truck’s
displacement.)
5. 42.8°
7. (a) More net work is done during the dive. (b) 6.8 × 107 J
9. 25°
11. 256 N
13. 2.5 × 107 J
15. 1450 kg
17. 3.2 × 103 J
19. (a) 3.1 × 103 J (b) 2.2 × 102 J
21. (a) −4.5 × 1011 J (b) 2.5 × 105 N
23. 1.4 × 1011 J
25. 18%
27. 5.4 × 102 J
29. 5.24 × 105 J
31. (a) 27 J (b) 36 J (c) 8.8 J (d) The change in gravitational potential
energy is −27 J = −W, where W is the work done by the weight.
33. (a) −3.0 × 104 J (b) The resistive force is not a conservative
force.
35. (a) −1086 J (b) The skater is 2.01 m below the starting
point.
37. 6.6 m/s
39. (a) 28.3 m/s (b) 28.3 m/s (c) 28.3 m/s
41. (a) 52.2 J (b) 48.8 m/s
43. 0.60 m
45. 1.7 m/s
47. 27.0 m/s
49. 18 m
51. (a) 16.5 m (b) 2.9 N
53. 5.3 m
55. −1.21 × 106 J
57. 2.4 m/s
59. 2450 N
61. 13.5 m
63. (a) 5.48 × 106 J (b) 1.31 × 103 nutritional calories
65. (a) 3.3 × 104 W (b) 5.1 × 104 W
67. (a) 1.0 × 104 W (b) 13 hp
69. 6.7 × 102 N
71. (a) Bow 1 requires more work. (b) 25 J
73. (a) 54% (b) 46%
75. 7.07 m/s
77. At h = 20.0 m: KE = 0 J, PE = 392 J, and E = 392 J
At h = 10.0 m: KE = 196 J, PE = 196 J, and E = 392 J
At h = 0 m: KE = 392 J, PE = 0 J, and E = 392 J
79. 1.20 × 104 J
81. 45 N
83. (a) 2.8 J (b) 35 N
85. 6.33 m
87. 3.40 × 102 N
89. +1470 J
91. (a) 479 m So it does have enough energy to lift the
elevator and passenger (without friction.)
(b) E grav
= mgh = (125 kg)(9.80 m/s2)(450 m) = 5.51 × 105 J and E
Net = 5.32 × 105 J.
Therefore, we see that E net
< E grav
, and the
elevator will NOT make it to the top when
including the given frictional force.
Chapter 7 1. 69 N, directed opposite to the skater’s velocity
3. 1.8 N, directed straight downward
5. ‒8.7 kg · m/s
7. (a) +2.2 × 103 N (b) +4.4 × 103 N
9. +5.1 × 107 kg · m/s
11. 6.7 m
13. 322 kg · m/s, 16° north of east
15. 344 N
17. (a) +7.5 kg · m/s (b) +3.3 m/s
19. (a) ‒1.5 m/s (b) +1.1 m/s
21. 4500 m/s, in the same direction the rocket had before the explosion
23. (a) ‒0.14 m/s (b) ‒7.1 × 10‒3 m/s
25. m 1 = 1.00 kg, m
2 = 1.00 kg
27. +547 m/s
Answers to Odd-Numbered Problems A-21
29. (a) 4.89 m/s (b) 1.22 m
31. +9.3 m/s
33. (a) ‒0.400 m/s (5.00-kg ball), +1.60 m/s (7.50-kg ball)
(b) +0.800 m/s (both balls)
35. 7.4%
37. +9.09 m/s
39. 0.062 kg
41. (a) 73° (b) 4.28 m/s
43. 2.175 × 10‒3
45. (a) 5.56 m/s (b) ‒2.83 m/s (1.50-kg ball),
+2.73 m/s (4.60-kg ball)
(c) 0.409 m (1.50-kg ball), 0.380 m (4.60-kg ball)
47. 8 bounces
49. (a) +1.0 m/s (b) +1.0 m/s (c) equal to
51. 1.51 × 1030 kg
53. 96 kg
55. (a) ‒0.432 m/s (b) +1.82 m/s
57. 9.6 ms
59. 6.46 × 10‒11 m
61. 2.54 × 10‒3 kg
63. 0.707
65. 0.097 m
67. (a) 1160 J; 580 kg · m/s (b) 1160 J; 140 kg · m/s 69. (a) 2.49 m/s (b) 3.3 × 10‒3 m/s (c) 3.00 m/s
Chapter 8 1. 21 rad
3. (a) +7.3 × 10‒5 rad/s (b) +2.0 × 10‒7 rad/s
5. 63.7 grad
7. (a) +0.75 rad/s2 (b) ‒0.75 rad/s2 (c) +1.0 rad/s2 (d) ‒2.0 rad/s2
9. 8.0 s
11. 128 s
13. 1200 s
15. 336 m/s
17. (a) 2.00 × 10‒2 s (b) 4.00 × 10‒2 s
19. 1.43 × 10‒1 m/s
21. 0.125 s
23. (a) 117 rad/s (b) 140 s
25. (a) 10.0 s (b) ‒2.00 rad/s2
27. +267 rad
29. 1.95 × 104 rad
31. 2.1 rev
33. 7.37 s
35. (a) 1500 rad/s (b) 4.2 × 10‒3 s
37. 0.18 m
39. 0.62 m
41. 4.63 m/s
43. (a) 3.61 rad/s (b) 6.53 rad/s2
45. (a) 9.00 m/s2 (b) radially inward toward the center of the
track
47. (a) 1.99 × 10‒7 rad/s (b) 2.98 × 104 m/s (c) 5.94 × 10‒3 m/s2, directed toward the
center of the orbit
49. 0.577
51. (a) 2.4 × 105 m/s (b) 5.3 × 1020 N
53. 8.71 rad/s2
55. 693 rad
57. (a) ‒1.4 rad/s2 (b) +33 rad
59. 2.10 × 106 rev
61. 974 rev
63. 1.47 rad/s
65. (a) 2.5 m/s2 (b) 3.1 m/s2
67. 157.3 rad/s
69. 22 rev/s
71. (a) 1.25 m/s (b) 7.98 rev/s
73. (a) 8 (b) 5
75. 25 rev
77. ‒485 rad
79. (a) 8.2 × 10‒2 rad/s (b) 2.6 m/s2 (c) 3.2 m/s2
81. (a) Referring to the fi gure, if Wheel 1 rotates clockwise, Wheel 3 rotates clockwise.
(b) 0.26 m/s 1.12 rad/s (c) Largest tangential speed occurs when the
wheel of the largest diameter is in the
drive-wheel position: 𝜐 = 0.59 m/s.
Chapter 9 1. 843 N
3. 2.1 × 102 N
5. (a) 13 500 N · m (b) 132 000 N · m
7. (a) FL (b) FL (c) FL
9. 43.7°
11. 1.03 m
13. (a) 2590 N (b) 2010 N
15. 1200 N, to the left
17. 24 m/s
19. (a) 1.60 × 105 N (b) 4.20 × 105 N
21. V = 170 N, P = 270 N, H = 210 N
23. 37.6°
25. (a) 2260 N (b) horizontal component: 1450 N
vertical component: 1450 N
27. (a) 1.6 × 104 N (b) 2.2 × 104 N
29. 1.7 m
31. 8.0 × 10‒4 N · m
33. 0.027 kg · m2
35. hoop: 0.20 N · m disk: 0.10 N · m
37. (a) 5.94 rad/s2 (b) 44.0 N
39. 0.060 kg · m2
A-22 Answers to Odd-Numbered Problems
41. 2.0 s
43. (a) system A: 229 kg · m2 system B: 321 kg · m2
(b) system A: ‒1270 N · m system B: 0 N · m
(c) system A: ‒27.7 rad/s system B: 0 rad/s
45. 0.78 N
47. 1700 N · m
49. (a) object 1: 12.0 m/s object 2: 9.00 m/s
object 3: 18.0 m/s
(b) 1.08 × 103 J (c) 60.0 kg · m2 (d) 1.08 × 103 J
51. 6.1 × 105 rev/min
53. 2/7
55. (a) 3.7 m (b) 7.0 m/s
57. 1.3 m/s
59. 4.4 kg · m2
61. 28 kg
63. 0.26 rad/s
65. 8%
67. 0.573 m
69. (a) 27 N · m (b) 34°
71. 5.0 kg
73. 0.50 rad/s2
75. 1400 N
77. 34 m/s
79. 51.4 N
81. 6.3 rad/s2; 5.00 × 103 N
83. 4.8 s (solid sphere); 8.0 s (spherical shell)
85. (a) 23.5 g’s (not safe) (b) A safe distance up the slope of the hill to
start the ride is l < 34.1 m.
Chapter 10 1. 237 N
3. 650 N/m
5. (a) 8.5 × 104 N/m (b) 290 N
7. 1.4 kg
9. 0.240 m
11. 2.29 × 10−3 m
13. (a) 0.407 m (b) 397 m
15. (a) 730 Hz (b) 13 m/s2
17. (a) −9.84 N (b) 10.5 rad/s (c) 1.26 m/s (d) 13.2 m/s2
19. 6.0 rad/s
21. 4.3 kg
23. (a) 2.66 Hz (b) 0.0350 m
25. −0.012 J
27. (a) 58.8 N/m (b) 11.4 rad/s
29. 4.8 cm
31. 14 m/s
33. 7.18 × 10−2 m
35. 0.50 m/s
37. 24.2 rad/s
39. (a) amplitude = 3.59 × 10−2 m frequency = 4.24 Hz
(b) amplitude = 5.08 × 10−2 m frequency = 4.24 Hz
41. 2.37 × 103 N/m
43. 0.40 s
45. (a) 3.5 rad/s (b) 2.0 × 10−2 J (c) 0.41 m/s
47. (a) 1.64 s (b) 1.64 s
49. 0.54 s
51. 5.2 × 10−4 m
53. 260 m
55. 2.9 × 10−2 m
57. (a) 4.9 × 106 N/m2 (b) 6.0 × 10−6 m
59. 1.6 × 105 N
61. 1.4 × 10−6
63. 6.6 × 104 N
65. 1.2 × 1011 N/m2
67. (a) 2.5 × 10−4 (b) 7.5 × 10−5 m
69. 1.0 × 10−3 m
71. 12 m
73. −4.4 × 10−5
75. (a) 0.450 m (b) 3.31 rad/s (c) 1.49 m/s
77. 61 kg
79. +0.50 m
81. 0.44 m/s
83. 140 N/m
85. 8.00
87. 2.08 m/s
89. 3.2 × 102 N/m
91. 66 Hz
93. (a) 0.15 m (b) 1.1 m/s (c) 0.85 s
95. (a) The total distance it will let you fall is 65.4 m. Since the distance from the cliff to
the beach is 140 ft = 42.7 m, the bungee
does NOT aff ord you a safe landing when
you hang from the very end.
(b) You should grab the unstretched bungee at a distance of 19.3 m from the end attached to
the rail. The deformation is 1.21 or 121%.
This is less than the deformation limit of the
bungee cord, so it should be okay!
Chapter 11 1. 8.3 × 103 lb
3. 317 m2
5. 7.0 ×10−2 m
7. 1.9 gal
9. 4240 s
11. 1.1 × 103 N
13. 24
15. 32 N
17. 2400 Pa
19. 0.95 N
21. 10.3 m
23. (a) 1.26 × 105 Pa (b) 19.4 m
25. 0.50 m
27. (a) 2.45 × 105 Pa (b) 1.73 × 105 Pa
29. 0.74 m
31. 2.3 × 108 N
33. 3.8 × 105 N
35. (a) 93.0 N (b) 94.9 N
37. 8.50 × 105 N · m
39. 108 N
41. 59 N
Answers to Odd-Numbered Problems A-23
43. 250 kg/m3
45. 390 kg/m3
47. 20
49. 0.20 m
51. 7.6 × 10−2 m
53. 5.28 × 10−2 m (inner), 6.20 × 10−2 m (outer)
55. 4.5 × 10−5 kg/s
57. (a) 0.18 m (b) 0.14 m
59. 2 × 109
61. 46 Pa (Air enters at B and exits at A.)
63. 1.92 × 105 N
65. 96 Pa
67. 3.0 × 105 Pa
69. (a) 14 m/s (b) 0.98 m3/s
71. 1.81 × 10−2 m3/s
73. 33 m/s
75. 7.78 m/s
77. 0.5 m/s
79. 1.19
81. 1.7 m
83. 2.25
85. 2.9 × 104 Pa 87. 4.89 m
89. 8750 N (The bed should not be purchased.)
91. 3.91 × 10−6 m3
93. 7.0 × 105 Pa
95. (a) 1.6 × 10−4 m3/s (b) 2.0 × 101 m/s
97. 7.9 × 10−4 m3
99. 31.3 rad/s
101. 78.4 gal/min
103. 1120 N
105. 55 Pa
107. 0.27 m (Father); 0.20 m (Daughter)
109. (a) 1.69 × 105 N/m (b) 73.5 m/s (c) 551 m
Chapter 12 1. (a) 56 F° (b) 31 K
3. (a) 102 °C (day), −173 °C (night) (b) 215 °F (day), −2.80 × 102 °F (night)
5. (a) −196 °C (b) −321 °F
7. 44.0 °C
9. T R = T
F + 459.67
11. 0.084 m
13. (a) The radius will be larger. (b) 0.0017
15. 1.7 × 10−5 (C°)−1
17. 5.8 m
19. 49 °C
21. 2.0027 s
23. 41 °C
25. 31.7 °C (arrangement A), 34.1 °C (arrangement B), 30.4 °C (arrangement C)
27. 26 °C
29. 2.5 × 10−7 m3
31. 3.1 × 10−3 m3
33. 7.3 × 10−6 m3
35. 0.33 gal
37. 1.2 × 10−6 m3
39. 45 atm
41. 6.9
43. 43.0 °C
45. 19 °C
47. 21.03 °C
49. 940 °C
51. 650 W
53. 4.4 × 103 N
55. 0.016 C°
57. 3.9 × 105 J
59. (a) 2.4 × 106 J (b) 5.3 C°
61. 9.49 × 10−3 kg
63. 0.16 kg
65. 64 °C
67. 2.6 × 10−3 kg
69. 1.9 × 104 J/kg
71. 3.50 × 102 m/s
73. (a) 3.0 × 1020 J (b) 2.7 years
75. 5.5
77. 87%
79. 2.8 × 105 J
81. 39%
83. 28%
85. 25 °C
87. 3.9 × 10−3 kg
89. 59 °C
91. 230 C°
93. 1.4 × 10−3 m
95. 0.223
97. 1.2 × 10−2 kg
99. 4.5 × 105 J
101. 32.1 °C
103. 9.89 × 10−2 m3
105. 18 C°; 6.0 C°; 2.8 C°
107. (a) 1750.00 rpm (b) 1749.50 rpm (c) We must adjust (increase) the angular
speed of the larger wheel to bring the
angular speed of the small wheel back
up to the 1750.0 rpm speed it had at the
higher temperature. In this case we need
35.010 rpm.
Chapter 13 1. 1.5 C°
3. 8.0 × 102 J/s
5. 12 J
7. 17
9. 287 °C
11. 85 J
13. (a) 2200 J (b) 0.26 C°
15. 103.3 °C
17. (a) 101.2 °C (b) 110.6 °C
19. 4.5
21. 5800 K
23. (a) 6.3 J/s (b) 4.8 J/s
25. 1.2 × 104 s
27. 275 W
29. (a) 67 W (b) 58 food Calories
31. 0.39 kg
A-24 Answers to Odd-Numbered Problems
33. 12
35. 2.0 × 10−3 m
37. 14.5 d
39. 0.70
41. 0.40 m
43. (a) 2.0 (b) 0.61
45. 7.30 × 103 W
47. (a) 1.5 × 105 s (smaller area) (b) 3.6 × 103 s (larger area)
49. (a) 2.79 J/s (b) 5.3 °C
Chapter 14 1. 1.07 × 10−22 kg
3. aluminum
5. 1.00 × 10−2 g
7. (a) 2.3 × 103 mol (b) 1.4 × 1027
9. 11
11. 1.1 g
13. (a) 201 mol (b) 1.21 × 105 Pa
15. 2.5 × 1021
17. 12
19. 2.2 kg/m3
21. 39
23. 0.205
25. 5.9 × 104 g
27. 1.02
29. 0.090%
31. 308 K
33. 1.6 × 10−15 kg
35. 3.9 × 105 J
37. (a) 46.3 m2/s2 (b) 40.1 m2/s2
39. 1.73
41. 2820 m
43. (a) −120 N (assuming the bullets travel in the + direction)
(b) 120 N (c) 4.0 × 105 Pa
45. 0.14 kg/m3
47. (a) 2.1 s (b) 1.6 × 10−5 s (c) because the diff usional path is zigzag and
not straight-line
49. 2.29 × 10−3 m2
51. (a) The answer is a derivation. (b) 31 s
53. 304 K
55. 925 K
57. 327 m/s
59. 67.0 m3
61. 343 m/s
63. 7.23 × 10−20 J
65. Nitrogen: υ rms
= 511 m/s;
Oxygen: υ rms
= 478 m/s
67. (a) 1.5 × 10−16 N (b) 3.8 × 10−17 Pa (c) 2.7 K
69. (a) The pressure of the gas in the cylinder at the surface is 1.84 × 106 Pa. This is equal
to 267 psi (a relatively high gas pressure).
Chapter 15 1. (a) +1.6 × 104 J (b) −4.2 × 104 J (c) −2.6 × 104 J
3. (a) −87 J (b) +87 J
5. (a) +1.2 × 105 J (b) 5.9 × 105 J
7. (a) −5.03 × 105 J (b) 1.20 × 102 nutritional Calories
9. 1.2 × 107 Pa
11. 3.0 × 105 Pa
13. (a) 3.0 × 103 J (b) Work is done by the system.
15. 0.24 m
17. 3.1 × 105 Pa
19. 4.99 × 10−6
21. (a) +5.0 × 103 J (b) −5.0 × 103 J
23. −4700 J
25. 1.81
27. 19.3
29. A to B: ΔU = 4990 J, W = 3320 J, Q = 8310 J B to C: ΔU = −4990 J, W = 0 J, Q = −4990 J C to D: ΔU = −2490 J, W = −1660 J,
Q = −4150 J D to A: ΔU = 2490 J, W = 0 J, Q = 2490 J
31. (a) −8.00 × 104 J (b) Heat fl ows out of the gas.
33. (a) 477 K (b) 323 K
35. (a) 1.1 × 104 J (b) 1.8 × 104 J
37. 45 K
39. (a) 1.40 × 102 K (b) 5.24 × 103 J (c) 2.33 × 103 Pa
41. 0.264 m
43. 2.38 × 104 J
45. (a) 4.6 × 105 J (b) 4.1 × 105 J
47. 65 J
49. 0.75
51. 256 K
53. (a) 1260 K (b) 1.74 × 104 J
55. 1090 K
57. lowering the temperature of the cold reservoir
59. 1.23
61. The answer is a proof.
63. 21
65. 13
67. 284 K
69. 275 K
71. 3.8 × 104 J
73. (a) 2.0 × 101 (b) 1.5 × 104 J
75. engine I: +0.4 J/K (irreversible, could exist) engine II: 0 J/K (reversible) engine
III: −1.0 J/K (irreversible, could not exist)
77. (a) 3.68 × 103 J/K (b) 1.82 × 104 J/K (c) The vaporization process creates more
disorder.
79. (a) +8.0 × 102 J/K (b) The entropy of the universe
increases.
81. (a) +1.74 J/K (b) 811 J (c) 546 J
83. (a) −2.1 × 102 K (b) decrease
85. 4.5 × 10−3 m3
87. (a) reversible (b) −125 J/K
89. 5.86 × 105 J
91. (a) 0 J (b) +2.1 × 103 J (c) −1.5 × 103 J
Answers to Odd-Numbered Problems A-25
93. (a) 24.4 J (b) 37.3 J/(mol · K)
95. 75 K
97. 44.3 s
99. e = e 1 + e
2 − e
1 e
2
101. 240 J (outdoor temperature of 273 K); 479 J (outdoor temperature of 252 K)
103. 332 K (Engine 1); 449 K (Engine 2)
105. (a) 1.41 × 105 Pa (b) 86.1 cm (c) 466 K
Chapter 16 1. 5.50 × 1014 Hz
3. (a) 10.0 s (b) 0.100 Hz (c) 32 m (d) 3.2 m/s (e) It is not possible to determine the
amplitude.
5. 0.25 m
7. 0.20 m/s
9. 5.0 × 101 s
11. (a) 1.09 m/s (b) 6.55 m
13. 8.68 × 10−3 kg/m
15. 7.7 m/s2
17. (a) 2.0 × 101 m/s (b) 1.4 × 101 m/s
19. (a) 2.0 m (wave A), 4.0 m (wave B) (b) 6.0 Hz (wave A), 3.0 Hz (wave B) (c) 19 m/s (wave A), 4.7 m/s (wave B)
21. m 1 = 28.7 kg, m
2 = 14.3 kg
23. 3.26 × 10−3 s
25. y = (0.37 m) sin[(8.2 rad/s)t + (0.68 m−1)x]
27. y = (0.35 m) sin[(88 rad/s)t − (17 m−1)x]
29. (a) 4.2 m/s (b) 0.35 m (c) y = (3.6 × 10−2 m) sin[(75 rad/s)t +
(18 m−1)x]
31. 110 m
33. 28.8 K
35. 1730 m/s
37. 690 rad/s
39. 61 m
41. (a) fi rst in metal, second in water, third in air (b) Second sound arrives 0.059 s later, and
third sound arrives 0.339 s later.
43. 650 m
45. tungsten
47. 8.0 × 105 m
49. 57% argon, 43% neon
51. 0.404 m
53. 6.5 W
55. 1.4 × 10−5 W/m2
57. 1.98%
59. 7.6 × 103 W/m2
61. 8.0 × 102 s
63. (a) 8.0 × 10−4 W/m2 (b) 89 dB
65. 6.0
67. −6.0 dB
69. 0.316 W/m2
71. 79 400
73. 0.84 s
75. 2.39 dB
77. 56 m/s
79. 1.054
81. 326 Hz
83. 22 m/s
85. 1.5 m/s2
87. (a) 1570 Hz (b) 1590 Hz
89. 3.02 × 10−6 W/m2
91. 2.06
93. 64 N
95. 1000
97. 78 cm
99. 3.4 m/s
101. 1.0 × 102
103. 2.6
105. (a) υ = √yg (b) 2.2 m/s at y = 0.50 m, 4.4 m/s at
y = 2.0 m
107. 153 N
109. 239 m/s
111. 719 Hz
113. (a) 2310 Hz (b) 1970 Hz
115. (a) 2004 m (b) 23.7 m/s (c) 83.2 s
Chapter 17 1. 8.42 m
3. The answer is a series of drawings.
5. (a) +13.3 mm (b) +48.8 mm
7. 3.89 m
9. 28 Hz and 42 Hz
11. 3.90 m, 1.55 m, 6.25 m
13. 16°
15. (a) 53.8° (b) 23.8°
17. 3.7°
19. 8 Hz
21. 437 Hz
23. 263 Hz
25. 8 Hz
27. 1.95 × 10−3 s
29. 171 N
31. 3.93 × 10−3 kg/m
33. (a) 180 m/s (b) 1.2 m (c) 150 Hz
35. 0.485
37. 0.077 m
39. 12 Hz
41. 3.0 × 103 Hz
43. 1.96 m
45. 0.35 m
47. (a) 3 (b) 0.57 m
49. 6.1 m
51. 0.557 m
53. 0.28 m
55. 5.06 m
57. 2.92
59. 1.10 × 102 Hz
61. (a) destructive interference (b) constructive interference
63. 20.8° and 53.1°
65. 8.0° (air), 37° (water)
67. (a) For the aluminum rod and f = 95.50 kHz we have 2.65 cm. For the aluminum rod
and f = 102.50 kHz we have 2.47 cm.
A-26 Answers to Odd-Numbered Problems
(b) For the titanium rod and f = 95.50 kHz we have 2.70 cm. For the titanium rod
and f = 102.50 kHz we have 2.52 cm.
Chapter 18 1. +3.04 × 10‒18 C
3. (a) ‒1.6 𝜇C (b) 1.0 × 1013 electrons
5. (a) +1.5q (b) +4q (c) +4q
7. (a) 3.35 × 1026 electrons (b) ‒5.36 × 107 C
9. 8 electrons
11. (a) 0.83 N (b) attractive
13. 1.8 × 10‒5 C
15. (a) the same algebraic signs, both positive or both negative
(b) 1.7 × 10‒16 C
17. (a) 4.56 × 10‒8 C (b) 3.25 × 10‒6 kg
19. 7.19 × 1023 m/s2
21. (a) 0.166 N directed along the +y axis (b) 111 m/s2 directed along the +y axis
23. 1.96 × 10‒17 J
25. ‒3.3 × 10‒6 C
27. (a) 15.4° (b) 0.813 N
29. 1.37
31. 1.8 N due east
33. 54 N/C
35. (a) 7700 N/C (b) 1300 N/C (c) 5500 N/C
37. 0.16 N · m
39. 6.5 × 103 N/C directed downward
41. 1.81 × 102 N/C in Figure 18.20a and 3.11 × 102 N/C in Figure 18.20b
43. 2.2 × 105 N/C directed along the ‒x axis
45. 3.9 × 106 N/C directed along the +y axis
47. +1.9 × 10‒2 m
49. 1.0 × 107 m/s
51. 61°
53. 3.25 × 10‒8 C
55. (a) 350 N · m2/C (b) 460 N · m2/C
57. 58°
59. The answer is a proof.
61. (a) The fl ux through the face in the x, z plane at y = 0 m is ‒6.0 × 101 N · m2/C. The fl ux through the face parallel to the x, z plane at y = 0.20 m is +6.0 × 101 N · m2/C. The fl ux through each of the remaining four
faces is zero.
(b) 0 N · m2/C
63. The answer is a drawing.
65. ‒q on the interior surface and +3q on the exterior surface
67. (a) 6.2 × 107 N/C directed along the ‒x axis (b) 2.9 × 108 N/C directed along the +x axis
69. 3.8 × 1012 electrons
71. ∣q 1 ∣ = 0.716 q and ∣q
2 ∣ = 0.0895 q
73. 2.5 × 104 N/C
75. 0.76
77. +3.9 × 104 m/s
79. (a) 7.56 × 104 N/C (along the +y axis) (b) 5.04 × 102 m/s2 (along the +y axis)
81. (a) 1.23 × 105 N/C (b) ‒1.94 × 105 N/C
Chapter 19 1. ‒2.1 × 10‒11 J
3. 1.1 × 10‒20 J
5. 67 hp
7. 19 m/s
9. 339 V
11. (a) 3.0 × 1010 J (b) 7.4 × 103 m/s (c) 7.2 × 104 kg
13. ‒4.05 × 104 V
15. 2.4
17. ‒9.4 × 103 V
19. +7.8 × 106 V
21. ‒3.1 × 10‒6 C
23. ‒0.746 J
25. 1.53 × 10‒14 m
27. 0.0342 m
29. 1.41 × 10‒2 m
31. 1.1 m
33. 8.8 × 106 V/m
35. 3.5 × 104 V
37. (a) 179 V (b) 143 V (c) 155 V
39. (a) 0 V/m (b) 1.0 × 101 V/m (c) 5.0 V/m
41. (a) 0 V (b) +290 V (c) ‒290 V
43. 1.1 × 103 V
45. (a) 33 J (b) 8500 W
47. 5.3
49. (a) 1.3 × 10‒12 C (b) 8.1 × 106 ions
51. 52 V
53. 7.7 V decrease
55. 2.77 × 106 m/s
57. 2 × 10‒8 F
59. +38 V
61. 5.40 × 10‒5 C
63. 0.032 m
65. 1.3 × 10‒4 C
67. The answer is a proof.
69. 2.8
71. 0 N/C; V = 170 V
73. (a) 3657 capacitors (b) 398 capacitors
Chapter 20 1. (a) 3.6 × 10‒2 C (b) 2.3 × 1017 electrons
3. 1.3 × 106 J
5. (a) 1.5 × 10‒11 A (b) 4.7 × 107 ions 7. 16 Ω
9. (a) 4.7 × 1013 protons (b) 17 C°
11. 0.12 Ω
13. 0.0050 (C°)‒1
15. 1.64
17. 9.3%
19. 70
21. 39.5 °C
23. 6.0 × 102 W
25. $5.9 × 106
Answers to Odd-Numbered Problems A-27
27. 8.9 h
29. 3.1 × 10‒4 m
31. 250 °C
33. (a) 786 W (b) 1572 W
35. 150 W
37. 21 V
39. (a) 50.0 Hz (b) 2.40 × 102 Ω (c) 60.0 W
41. (a) 145 Ω (b) 74 V
43. 32 Ω
45. 9.0 V
47. (a) 15.5 V (b) 14.2 W
49. (a) 35 Ω (b) 5.0 × 101 Ω
51. 288 Ω (50.0-W fi lament) and 144 Ω (100.0-W fi lament)
53. (a) 65.0 Ω (b) 38.8 Ω (c) 1.25 W (d) 2.09 W
55. (a) 4.57 A (b) 1450 W
57. 190 Ω
59. 0.00116 Ω
61. 3.58 × 10‒8 m2
63. 9.2 A
65. 4.6 Ω
67. 42 Ω
69. 6.00 Ω, 0.545 Ω, 3.67 Ω, 2.75 Ω, 2.20 Ω, 1.50 Ω, 1.33 Ω, 0.833 Ω
71. 25 Ω
73. 30 bulbs
75. 12.0 V
77. 24.0 V
79. (a) 0.38 A (b) 2.0 × 101 V (c) Point B is at the higher potential.
81. 0.73 A to the left
83. 6.0 A (left to right) in the 2.0-Ω resistor, 2.0 A (left to right) in the 8.0-Ω resistor
85. 1.82 A (downward) in the 4.00-Ω resistor
87. 5.01 A
89. 30.0 V
91. 820 Ω and 8.00 × 10‒3 A
93. 9.0 V
95. 18 𝜇F
97. 2.0 𝜇F
99. The answer is a proof.
101. 11 V
103. 4.1 × 10‒7 F
105. 1.2 × 10‒2 s
107. 0.29 s
109. 36 𝜇F
111. 82 Ω
113. ‒34.6 °C
115. 0.0835 Ω
117. (a) 0.750 A (b) 2.11 A
119. (a) 1.2 Ω (b) 110 V
121. 189 Ω
123. C 0
125. I1 = 23 A; I2 = 1
3 A; I3 = 1.0 A
127. (a) R = 12 Ω (b) Four 47-Ω resistors in parallel have an
equivalent resistance of 11.8 Ω, within
10% of the required 12 Ω.
Chapter 21 1. 5.9 × 1012 m/s2
3. 4.1 × 10‒3 m/s
5. 58°
7. 1.1 × 10‒2 N
9. 1.3 × 10‒10 N, directed out of the page
11. (a) due south (b) 2.55 × 1014 m/s2
13. 0.14 T
15. (a) negative (b) 2.7 × 10‒3 kg
17. 0.338 T
19. (a) 1.08 × 107 m/s (b) 7.60 × 10‒12 N (c) 0.102 m
21. 1.63 × 10‒2 m
23. 0.16 T
25. 8.7 × 10‒3 s
27. (a) 4.4 × 10‒3 N (b) 1.7 × 10‒4 C
29. 9.6 × 104 m/s
31. 5.1 × 10‒5 T
33. 3.4 × 10‒3 T
35. 2.7 m
37. (a) 0 N (side AB), 24.2 N (side BC, directed perpendicularly out of the paper), 24.2 N
(side AC, directed perpendicularly into the paper)
(b) 0 N
39. 44°
41. 14 A
43. 2.2 A
45. 4.19 × 10‒3 N · m
47. 1.27
49. (a) 170 N · m (b) 35° angle increases
51. 8.3 N
53. (a) downward (b) 3.1 × 10‒4 T
55. 2.8 × 104 turns/m
57. 3.8 × 10‒5 T
59. (a) 4.3 × 10‒5 T (b) 5.3 × 10‒5 T
61. 8.6 A in a direction opposite to the current in the inner coil
63. between the wires and 0.800 m from wire 1
65. 1.04 × 10‒2 T
67. 320 A
69. (a) 1.1 × 10‒5 T (b) 4.4 × 10‒6 T
71. The answer is a proof.
73. 19.7°
75. 0.062 m
77. 0.19 N
79. 1.7 × 10‒3 N
81. (a) 0° (b) 0.29 m
83. 0.030 m
85. 1.2 × 10‒5 A · m2
87. ‒1.06 × 10‒4 N
89. (a) 2.1 × 107 m/s (b) 1.85 cm (c) direction (d) 6.5 × 10‒3 T
A-28 Answers to Odd-Numbered Problems
Chapter 22 1. (a) 3.7 × 10‒5 T (b) East end is positive.
3. 7800 V
5. rod A: emf = 0 V; rod B: emf = 1.6 V, with end 2 being positive; rod C: emf = 0 V
7. 25 m/s
9. 250 m
11. 0.70
13. 70.5°
15. 2.2 × 10‒3 Wb
17. both triangular ends: 0 Wb; bottom surface: 0 Wb; 1.2 m × 0.30 m surface: 0.090 Wb;
1.2 × 0.50 m surface: 0.090 Wb
19. 0.25 V
21. 8.6 × 10‒5 T
23. (a) 0.38 V (b) 0.43 m2/s
25. 0.14 V
27. (a) 3.6 × 10‒3 V (b) The area of the loop must be shrunk at a
rate of 2.0 × 10‒3 m2/s.
29. ‒0.84 A
31. 2100 rad/s
33. When the loop is viewed from above, the external magnetic fi eld is directed toward the
viewer.
35. (a) clockwise in loop A (b) counterclockwise in loop B
37. There is no induced current.
39. (a) location I: x → y → z location II: z → y → x
(b) location I: z → y → x location II: x → y → z
41. 0.150 m
43. 3.0 × 105
45. 38 m
47. 15.4 V
49. 1.5 × 109 J
51. 2.5 × 10–2 H
53. 1.4 V
55. 220 turns
57. 0.033 m
59. M = 𝜇 0 𝜋N
1 N
2 R2
2 /(2R
1 )
61. 1.0 × 101 W
63. 0.25
65. 0.20 A
67. (a) 7.0 × 105 W (b) 7.0 × 101 W
69. The answer is a proof.
71. (a) 12 V (b) 670 Hz
73. (a) clockwise (b) clockwise
75. 0.86 A
77. 0.050 V
79. 6.6 × 10–2 J
81. 1.6 × 10–5 A
83. ‒1.6 × 10‒3 V
85. (a) 0.040 s (b) 160 rad/s (c) 65 V (d) ‒49 V
87. (a) 534 V (b) 378 V (c) 0.066 T (d) N
p :N
s = 3.44:1
Chapter 23 1. 9470 Hz
3. 36 Ω
5. 2.7 × 10‒6 F
7. (a) 6.4 × 10‒6 F (b) 9.0 × 10‒4 C
9. 0.44 A
11. 24.6 Ω
13. 176 mH
15. (a) 1.11 × 104 Hz (b) 6.83 × 10‒9 F (c) 6.30 × 103 Ω (d) 7.00 × 102 Ω
17. 83.9 V
19. (a) 0.925 A (b) 31.8°
21. (a) 359 Ω (b) 51.3°
23. 38 V
25. 270 Hz
27. (a) 29.0 V (b) ‒0.263 A
29. 76 Ω
31. 2.7 × 10‒5 H
33. (a) 352 Hz (b) 15.5 A
35. 0.81 W
37. (a) 1.3 × 10‒3 H (b) 8.7 × 10‒6 F
39. 8 additional capacitors
41. 2.4%
43. 5.00 × 10‒2 s
45. resistor: 10.5 V, capacitor: 19.0 V, inductor: 29.6 V
47. 8.0 × 101 Hz
49. 0.075 A
51. (a) 2.94 × 10‒3 H (b) 4.84 Ω (c) 0.163
53. 4.2 kHz
55. 0.094 W
57. (a) 363 Hz (b) For capacitors in parallel and inductors
in series, we have 181 kHz; For the capa-
citors in series and inductors in parallel,
we have 725 kHz; For capacitors and in-
ductors both in parallel, we have 363 kHz
(c) (0.88 nF) ≤ C var
≤ (14.1 nF)
Chapter 24 1. 2.73 × 1012 m
3. 4.1 × 1016 m
5. (a) 2.4 × 109 Hz (b) 0.063 m
7. 11.118 m
9. 4.4 × 108 Hz
11. 1.93 × 1012
13. 4.500 × 107 Hz
15. 6.4 × 1018 m
17. 1.3 × 106 m
19. 42.3 m/s
21. 8.75 × 105 times
23. (a) 6.81 × 105 N/C (b) 2.27 × 10‒3 T
25. 0.07 N/C
27. 1.7 × 1011 W
29. 3.93 × 1026 W
31. 920 W
Answers to Odd-Numbered Problems A-29
33. (a) 2.1 × 104 W/m2 (b) 1.1 × 102 W (c) 18 s
35. (a) receding (b) 3.1 × 106 m/s
37. (a) 6.175 × 1014 Hz (b) 6.159 × 1014 Hz
39. (a) 0.55 W/m2 (b) 3.7 × 10‒2 W/m2
41. 21.5°
43. 14 W/m2
45. 206 W/m2
47. 20 analyzers
49. (a) 473 nm (b) 606 nm
51. 1.5 × 10‒4 H
53. (a) 183 N/C (b) 6.10 × 10‒7 T
55. increased by an additional 9.3°
57. The answers are in graphical form.
59. 6.25 × 10‒9 J
61. 5600 W
63. 2.1 × 103 Hz
65. (a) 4.0 W/m2 (b) 6.0 W/m2
67. (a) 500 W/m2 (b) 8.52 W/m2 (c) ‒1.5°, clockwise
+1.5°, counterclockwise
Chapter 25 1. Image 1: x = ‒2.0 m, y = +1.0 m Image 2: x = +2.0 m, y = ‒1.0 m Image 3: x = +2.0 m, y = +1.0 m
3. 7.2 m
5. 55°
7. only the arrow A
9. (a) 0.0670° (b) 7 m
11. (a) 70.6° (b) 62.1°
13. The image is 6.0 cm behind the mirror.
15. (a) The image is 28 cm behind the mirror. (b) The image is 7.6 cm tall.
17. (a) The image is 20.0 cm behind the mirror. (b) The image is 6.0 cm tall.
19. 22 cm
21. (a) 290 cm (b) ‒8.9 cm (c) upside down.
23. 9.62 cm, concave
25. (a) ‒4.3 m (b) 0.39
27. (a) convex (b) 24.0 cm
29. 42.0 cm
31. (a) 82 m (b) 11 m
33. 56 cm
35. (a) 1.07 × 105 m (b) 1420 m/s
37. 14 cm
39. (a) 0.91 m (b) 0.85 m
41. (a) R (b) ‒1 (c) inverted
43. 1.2 m/s pointing in the ‒x direction
45. ‒3
47. 1.73
49. 18 cm (m = ‒2); 6.0 cm (m = +2)
51. 44.6 m
Chapter 26 1. 2.0 × 10‒11 s
3. 1.66 × 108 m/s
5. ethyl alcohol
7. 1.82
9. case (a) 46° case (b) 50° (Drawing wrongly shows an angle
of refraction greater than 55°.)
case (c) 69° case (d) 0° (Drawing wrongly shows an angle
of refraction greater than 0°.)
11. 0.9°
13. 1.92 × 108 m/s
15. 2.46 × 108 m/s
17. 1.65
19. 2.7 m
21. 1.19 mm
23. The answer is a derivation.
25. 3.23 cm
27. 65.1° (The ray of light will not enter the water.)
29. (a) 1.50 (b) 1.27
31. (a) point B (b) point A
33. 1.35
35. 0.813
37. 1.52
39. 25.0°
41. (a) 60.1° (b) 1.74
43. 0.86°
45. 0.35°
47. 52.7° (red), 56.2° (violet)
49. d i = 18 cm
51. (a) ‒0.00625 m (b) ‒0.0271 m
53. (a) 3.78 m (b) width = 8.40 × 102 mm
height = 1.26 × 103 mm
55. 2.8
57. (a) 204 cm (b) real (c) ‒17.1 cm
59. (a) 4.52 × 10‒4 m (b) 6.12 × 10‒2 m
61. 48 cm
63. +35 cm and +90.5 cm
65. ‒5.6 cm
67. ‒12 cm
69. (a) 4.00 cm to the left of the diverging lens (b) ‒0.167 (c) virtual (d) inverted (e) smaller
71. (a) 18.1 cm (b) real (c) inverted
73. (a) +0.600 (b) +2.00
75. ‒9.2 m
77. 28.0 cm
79. ‒0.20 diopters (right eye), ‒0.15 diopters (left eye)
A-30 Answers to Odd-Numbered Problems
81. (a) ‒4.5 m (b) 0.50 m
83. 18
85. (a) 6.88 cm (b) 3.63
87. 13.7 cm
89. 15.4
91. 0.81 cm
93. 0.86 cm
95. (a) ‒30.0 (b) 4.27 cm (c) ‒4.57
97. 1.1 m
99. ‒260
101. (a) ‒194 (b) ‒7.8 × 10‒5 m (c) 1.94 × 106 m
103. (a) 1.482 m (b) 0.018 m
105. (a) d i = ‒75 cm, m = +2.5
(b) d i = ‒75.0 cm, m = +2.50
107. 1.51
109. 0.023 m
111. 4.8 × 10‒3 rad
113. 38.7°
115. (a) 35.2 cm (b) 32.9 cm
117. (a) ‒24 cm (b) 6.0 mm
119. (a) converging lens (b) 2 f (c) 2 f
121. (a) 11.8 cm (b) 47.8 cm
123. ‒181
125. (a) 22.4 cm (b) 28.4 cm
127. (a) 36.0 cm (b) ‒4.00 mm (c) ‒26.0 cm (d) ‒35.5 cm (e) 5.46 mm
129. (a) Diverging lens (b) f = ‒621.0 cm (c) ‒0.161 diopters
Chapter 27 1. (a) 11° (b) 22°
(c) 34° (d) 48°
3. (a) Destructive interference occurs. (b) 3.25 m and 0.75 m from one of the
sources
5. 4.9 × 10−7 m
7. 6 (version A), 4 (version B)
9. 0.0248 m
11. 487 nm
13. 102 nm
15. 6.12 × 10−7 m
17. 1.18
19. 115 nm
21. 0.0256 m
23. (a) 1.1° (b) 3.0 × 10−5 m
25. (a) 0.21° (b) 22°
27. 0.576 m
29. 3.18 cm
31. 8
33. 5.6 × 1017 m
35. 1.0 × 104 m
37. (a) 9.7 mm (b) The hunter’s claim is not reasonable.
39. 2.3 m
41. (a) 1.22 𝜆 (b) shorter wavelength
43. 644 nm
45. 630 nm
47. 4.0 × 10−6 m
49. 640 nm and 480 nm
51. (a) violet light: 𝜃 = 7.9° red light: 𝜃 = 13°
(b) violet light: 𝜃 = 16° red light: 𝜃 = 26°
(c) violet light: 𝜃 = 24° red light: 𝜃 = 41°
(d) The second and third orders overlap.
53. (a) 2 (b) m
B = 4, m
A = 2 and m
B = 6, m
A = 3
55. 571 nm
57. 6.0 × 10−5 m
59. 1.9 mm
61. 0.75
63. 2.0 × 10−5 m
65. 1.95 m
67. 2.9 m
69. (a) 3.79° (b) 0.48 mm
Chapter 28 1. (a) 4.9 × 10−9 s (b) 1.5 m
3. 0.999 95c
5. 2.28 s
7. 16
9. 2.60 × 108 m/s
11. 8.1 km
13. 1.3
15. 40.2°
17. 3.0 m × 1.3 m
19. 7.5 × 10−19 kg · m/s
21. 1.0 m
23. −2.0 m/s
25. 5.0 × 10−13 J
27. 5.3 × 106 mi
29. (a) 1.0 (b) 6.6
31. 1.1 × 1024 kg/s
33. 1.3 × 107 kg · m/s
35. 0.31c
37. +0.80c
39. These answers assume that the direction of the cruiser, the ions, and the laser light is the
positive direction.
(a) +c (b) +0.994c (c) +0.200c (d) +0.194c
41. (a) 2.82 × 108 m/s (b) 1.8 × 10−16 kg · m/s
43. 4.0 light-years
45. 72 h
47. 42 m
49. (a) 4.3 years (b) the twin traveling at 0.500c
51. (a) m a = 6.64 × 10−27 kg;
m b = 6.64 × 10−27 kg;
m c = 33.2 × 10−27 kg
(b) KE a = 5.98 × 10−10 J;
KE b = 17.9 × 10−10 J;
KE c = 5.98 × 10−10 J
Answers to Odd-Numbered Problems A-31
53. (a) 56.6 yr (b) 0.12 min = 7.1 s (c) 0.014:1
Chapter 29 1. (a) 1.63 × 10−7 m (b) 1.84 × 1015 Hz (c) ultraviolet region
3. 6.3 eV
5. 310 nm
7. 1.26 eV
9. 73 photons/s
11. 162 nm
13. (a) 7760 N/C (b) 2.59 × 10−5 T
15. (a) 1.0 × 1013 Hz (b) infrared region
17. 75°
19. 4.755 × 10−24 kg · m/s
21. 9.50 × 10−17 m
23. 3.22 × 106 m/s
25. 1 × 10−18 m
27. (a) 4.50 × 10−36 m/s (b) 7.05 × 1027 years
29. 7.38 × 10−11 m
31. 1.9 × 10−10 m
33. 1.10 × 103 m/s
35. 6.01 × 10−11 m
37. (a) 2.1 × 10−35 kg · m/s (b) 4.7 × 10−34 m/s (c) 2.3 × 10−5 m/s
39. 8.3 × 10−6 m/s
41. 8.0%
43. 1.41 × 103 m/s
45. 7.77 × 10−13 J
47. 𝜆 A
= 2.75 × 10−7 m and
𝜆 B = 3.35 × 10−7 m
49. 1.86 × 104 V
51. (a) 5.0 × 1018 photons/s (b) 4.4 W/m2
53. 42.8
55. (a) 2.00 × 10−11 m (b) 3.80 kV
Chapter 30 1. (a) 6.2 × 10−31 m3 (b) 4 × 10−45 m3 (c) 7 × 10−13%
3. 2 mi
5. 7.3 × 10−14 m
7. n = 3
9. 16
11. 1.98 × 10−19 J
13. 6.56 × 10−7 m and 1.22 × 10−7 m
15. −13.6 eV, −3.40 eV, and −1.51 eV
17. n i = 6 and n
f = 2
19. The answer is a proof.
21. (a) 𝜐n = (2𝜋ke2Z)/(nh) (b) 2.19 × 106 m/s (c) 1.09 × 106 m/s (d) Yes.
23. (a) −1.51 eV (b) 2.58 × 10−34 J · s (c) 2.11 × 10−34 J · s
25. −0.378 eV
27. 1.732
29. −0.544 eV, −0.378 eV, and −0.278 eV
31. (a)
(b)
33. 50
35. (a) not allowed (b) allowed (c) not allowed (d) allowed (e) not allowed
37. carbon (Z = 6)
39. 6.83 × 10−11 m
41. Z = 32 (germanium, Ge)
43. 21 600 V
45. 1.9 × 1017 photons
47. 3.98 × 1014 photons
49. 2.2 × 1016 photons
51. 1s2 2s2 2p6 3s2 3p6 4s2 3d10 4p6 5s2 4d10
53.
55. (a) 7458 nm (b) 2279 nm (c) infrared region
57. (a) Bohr model: L = h/(2𝜋), quantum mechanics: L = 0 J · s
(b) Bohr model: L = 3h/(2𝜋), quantum mechanics: L = 0 J · s, L = √2h /(2π), and L = √6h /(2π)
59. 6 ≤ n i ≤ 19
61. 30.39 nm
63. (a) 8028 V (b) 1.545 × 10−10 m
65. (a) 11.4 keV (b) 11.4 kV (c) 1.09 × 10−10 m (d) 8.02 keV (e) 5.30 × 10−10 m
Chapter 31 1. (a) +1.31 × 10−17 C (b) 126 (c) 208 (d) 7.1 × 10−15 m (e) 2.3 × 1017 kg/m3
3. (a) 117 neutrons, platinum (Pt) (b) 16 neutrons, sulfur (S) (c) 34 neutrons, copper (Cu) (d) 6 neutrons, boron (B) (e) 145 neutrons, plutonium (Pu)
n ℓ mℓ ms 2 0 0 1/2
2 0 0 −1/2
n ℓ mℓ ms 2 1 1 1/2
2 1 1 −1/2
2 1 0 1/2
2 1 0 −1/2
2 1 −1 1/2
2 1 −1 −1/2
n ℓ mℓ ms 4 3 3 1/2
4 3 3 −1/2
4 3 2 1/2
4 3 2 −1/2
4 3 1 1/2
4 3 1 −1/2
4 3 0 1/2
4 3 0 −1/2
4 3 −1 1/2
4 3 −1 −1/2
4 3 −2 1/2
4 3 −2 −1/2
4 3 −3 1/2
4 3 −3 −1/2
A-32 Answers to Odd-Numbered Problems
5. (a) 92 protons (b) 122 neutrons (c) 41 electrons
7. 42 He
9. 9.4 × 103 m
11. 39.25 MeV
13. (a) 0.008 285 u (b) 0.009 105 u (c) More energy must be supplied to 31 T than
to helium 32 He.
15. (a) 1.741 670 u (b) 1622 MeV (c) 7.87 MeV/nucleon
17. 1.003 27 u
19. (a) 189 F → 188 O + 0+1 e (b) 158O → 157N + 0+ 1 e
21. 0.313 MeV
23. 4.87 MeV
25. (a) 23892 U (b) 2412Mg (c) 136 C
27. 1.61 × 107 m/s
29. 0.072 MeV (thorium atom) and 4.2 MeV (alpha particle)
31. 1.82 MeV
33. f = 1/16
35. 387 yr
37. 146 disintegrations/min
39. 8.00 days
41. 2.1 × 1013 Bq
43. 1.29 × 10−3 g
45. 7.23 days
47. 2.2 × 103 yr
49. (a) 0.999 (b) 1.36 × 10−9 (c) 0.755
51. age = 6900 yr, maximum error = 900 yr
53. 2.28 × 10−28 kg
55. 4.88 × 1010 yr
57. (a) 𝛽 − (b) 𝛽+ (c) 𝛾 (d) α
59. 4 782 969 electrons
61. 21284 Po
63. 6.68 × 10−12 m
65. 6.1 C°
67. (a) 23793 Np (b) 1.27 × 1011 Bq (c) 720.6 yr
Chapter 32 1. 12
3. (a) 14 Gy (b) 2.1 J
5. 2.4 × 104 rem
7. 5.0 × 10−4 C°
9. 4.4 × 1011 s−1
11. 9.2 × 108 nuclei
13. γ + 178O 126C + 42 He + 10 n
15. (a) A = 233, Z = 90, thorium 23390 Th (b) A = 233, Z = 92, uranium 23392U
17. (a) sulfur 3116 S (b) proton 11 H (c) potassium 4119 K (d) neon 2010 Ne
19. 13.6 MeV
21. 9.0 × 10−4
23. 41 collisions
25. 232.7851 u
27. 160 MeV
29. 1200 kg
31. 4.03 MeV
33. 3.3 MeV
35. 1.1 × 10−4 kg
37. (a) 1.0 × 1022 deuterium atoms (b) 9.6 × 109 kg
39. 33.9 MeV
41. (a) The K− particle does not contain u, c, or t quarks.
(b) The K− particle does not contain d , s, or b antiquarks.
43. (a) 1.9 × 10−20 kg · m/s (b) 3.5 × 10−14 m
45. 0.18 MeV
47. The three possibilities are (1) u, d, s; (2) u, d, b; (3) u, s, b.
49. 184 MeV
51. 1.0 gal
53. (a) 8.2 × 1010 J (b) 0.48 g
55. 0.18 rem
57. 0.507 R
A A (ampere), 552 Å (angstrom), 690 Aberrations, lenses, 765–766
concept focus, 769 concept summary, 768
Absolute pressure, 297 Absolute zero, 328–329, 417, 425 Absolute zero point, 329 Absorbed dose, 912–915 Absorption, 860 Absorption lines in sun’s spectrum, 861 ac (alternating current). See Alternating current (ac) Acceleration
action and reaction forces, 87 angular, 203–205 average, 31–33, 47, 56 centripetal, 122–125 centripetal acceleration and tangential acceleration,
210–213, 215, 216, 219 concept summary, 47–48 deceleration vs. negative acceleration, 37 due to gravity, 41 freely falling bodies, 43–44 increasing velocity, 32 instantaneous, 31–32, 56 loudspeakers, 601 nonequilibrium applications of Newton’s laws of
motion, 109 one-dimensional, 34–36, 41–47 rotational vs. translational, 241 simple harmonic motion and reference
circles, 264 two-dimensional, 55–59, 72, 74–75 units, 86 work, and static frictional force, 146
Accommodation, 758 Achilles tendon, 225 Acoustic Remote Control team problem, 488 Action potential, 542 Action-at-a-distance forces, 80 Activity, radioactive decay, 897–900
concept focus, 907 concept summary, 906–907 problems, 909
Addition of electric fields, 502 of vectors, 10–12, 15–18 of velocities, 824
Adhesion, 497–498 Adiabatic expansion or compression, 409–410 Adiabatic process, 406, 410 Adiabatic walls, 401–402 Age of universe, 929 Air conditioners, 417–420
concept focus, 427 concept summary, 426 problems, 430
Air wedges, thin-film interference, 785–786 Airplanes
angular acceleration of engines, 205 banked turns, 129 overloaded cargo planes, 232–233
sound barrier, 433 wings, 312
Algebra, A-2–3 Alnico (aluminum– nickel–cobalt), 613 alpha (α) decay, 891–893 alpha (α) rays, 890–891 Alpha particles
vs. neutrons, 918 Alternating current (ac), 552, 559–562
capacitors and capacitive reactance, 661–663 concept focus, 581, 679–680 concept summary, 580, 678–679 inductors and inductive reactance, 664–665 problems, 584, 680–683 RCL circuits, 665–670 resonance, 670–672 semiconductor devices, 672–678 transformers, 649–651
Alternating current (ac) generator, 643 AM and FM radio reception, 686–691 Ammeters, 574–575 Ampere (A), 552 Ampère’s law, 612–613
concept summary, 617 problems, 622–623
Amplitude, 435 pressure amplitude of sound waves, 441–442
Analyzers, 698–699 Anderson, C. D., 924 Angel Falls, 3 Angle of declination, compasses, 592 Angle of dip, magnetic fields, 592 Angle of incidence, 712 Angle of reflection, 712 Angles, A-4 angstrom (Å), 690 Angular acceleration, 203–205
concept focus, 216 concept summary, 215 problems, 216–218
Angular displacement, 200–203 concept focus, 216 concept summary, 215 problems, 216–218
Angular magnification, 761 astronomical telescopes, 764–765 compound microscopes, 763 concept focus, 769 concept summary, 768 magnifying glasses, 761–763 problems, 774
Angular momentum, 244–246 concept focus, 248 concept summary, 247 problems, 253
Angular size, 761 Angular variables
tangential variables, 208–210, 215, 216, 219 vector nature of, 214–215
Angular velocity, 203–205 concept focus, 216 concept summary, 215 problems, 216–218
Antennas, electromagnetic waves, 685–686 Antinodes, 474 Antiparticles, 923–924 Antiquarks, 927 Antiscalding device, 332–333 Apparent depth, 736–737 Apparent weight, 94–95 Arbitrary vectors, 12 Archery
bow stabilizers, 240 compound bows, 165–166
Archimedes’ principle, 300–305 concept focus, 318 concept summary, 317 problems, 321–322
Areas, A-4 Arthroscopic surgery, 744 Artificial gravity, 133–135
concept summary, 138 problems, 141
Astronauts artificial gravity, 133–135 body mass measurement device, 265–266 time measurement, 811–812
Astronomical telescopes, 764–765 Astronomy
Doppler effect, 696 electromagnetic spectrum, 690 supernovas, 691
Atmospheric pressure, 292, 297, 312 Atomic clock, 2 Atomic mass number, 886 Atomic mass scale, 380 Atomic mass unit, 380, 889 Atomic number, 885 Atoms, 489–490
binding energy, 888–890 Bohr model of hydrogen atom, 496–497, 857–861 concept focus, 879–880 concept summaries, 878–879 electrically neutral, 490 ground states, 866–868 holography, 876–878 impurity atoms, doping, 673 lasers. See Lasers line spectra, 855–856, 859 mass defect of nucleus, 888–890 neutrons, 885 nuclear atom, 853–855 nuclear structure, 885–887 Pauli exclusion principle and periodic table,
866–868 plum-pudding model, 853–854 positron, 894 problems, 880–884 quantum mechanical picture of hydrogen, 862–866 radioactivity. See Radioactivity Rutherford scattering, 853–855 strong nuclear force, and stability of nucleus,
887–888 X-rays, 868–872
Aurora borealis, 590 Automatic coffee maker, 335
Index
I-1
I-2 Index
Automobiles automatic trailer brakes, 87 banked curves, 129 batteries, 571 centripetal force, 126–127, cruise control, 626 Daytona International Speedway, 129 electrical systems, 573 engine efficiency, 413–414 engines, replacing, 104 forced convection, 363 headlights, 718 head-up displays (HUDs), 721 hydraulic car lift, 299–300 intersections, 70 passenger-side mirrors, 722 pushing a stalled car, 86 radiators, 338 raindrops on windows, 70 rolling motion, 213 rollovers, 233–235 seat belts, 82, 110 shock absorber, 273 tire traction, 96 trailers, 107 windshield wipers, 578
The Avengers, 1 Average acceleration, 31–33, 47, 56 Average angular velocity, 203–205 Average energy density, 693 Average power, 163 Average speed, 28–29 Average velocity, 29, 56 Avogadro’s number, 380–382
concept focus, 396 concept summary, 395 problems, 397
Axis of rotation, 200–201 inertia, 238
B Back emf, 645–646 Balmer series, 856–860 Banked curves, 129
concept focus, 138 concept summary, 137 problems, 140
Baryons, 925–926 Base SI units, 2–3 Base number, A-3 Baseball, impulse and momentum,
176–177 Baseballs, and de Broglie wavelength, 843 Bathroom scales, 670 Batteries
automobiles, 571 electric power, 557–558 electromotive force, 551–553 internal resistance, 570–571 terminal voltage, 570
Battery indicator, 303 Bay of Fundy, 274–275 Beat frequency, 473 Beats, 473–474
concept focus, 483 concept summary, 482 problems, 485
Becquerel, Antoine, 888 Beer bubbles, 385
Bernoulli’s equation, 309–314 concept focus, 318 concept summary, 317 problems, 322–323
beta (β) decay, 893–894 beta (β) rays, 890–891 Betelgeuse, 372 Bicycles, average velocity, 46 Big Bang theory, 929 Bike generator, 643–644
Generator Bike team problem, 660 Billiards, conservation of linear momentum, 181 Bimetallic strip, 334–335 Binding energy, nuclear, 888–890
concept focus, 907 concept summary, 906 problems, 908
Biologically equivalent dose, 913–914 Biomedical applications of electric potential
differences, 541–543 Blackbody, 371 Blackbody radiation and Planck’s constant, 833–834
concept focus, 849 concept summary, 849
Black holes, 131–132 Blenders, 207 Blood
clogged artery, 308 Doppler flow meter, 455 as fraction of body weight, 290 pressure, 296, 298 splatters, 72
Blue Angels, 27 BMI (body mass index), 4–5 Boats, relative velocity, 69 Bobsled tracks, 127 Body mass index (BMI), 4–5 Body mass measurement device, 265–266 Body-fat scales, 670 Bohr model of hydrogen atom, 496–497, 857–861
concept focus, 879 concept summary, 879 de Broglie’s explanation of angular momentum of
electron, 861–862 energies and radii of the Bohr orbits, 857–859 energy level diagrams, 859 line spectra of hydrogen, 859 problems, 881 vs. quantum mechanics, 864
Bohr radius, 858 Boiling, 343, 348
saving energy, 344 Boltzmann’s constant, 384 Bones
compression, 276 mechanical properties, 280 structure, 276
Boson family of particles, 925–926 Bow and arrow
bow stabilizers, 240 compound bows, 165–166
Boyle’s law, 385–387 Brachytherapy implants, 895 Brackett series for atomic hydrogen, 860 Brain, heat, 351 Bremsstrahlung, 870 Brewster angle, 745 Brewster’s law, 745 Bridge expansion joints, 333
Brownian motion, 391 Bubble chamber, 905
particle tracks, 598 Bubbles
beer bubbles, 385 thin-film interference, 784
Bulk modulus, 278 Bullets
collisions, 187–188 Energy of a Bullet Dissipated by Plywood team
problem, 222 projectile motion, 63–64
Bungee Cord Escape team problem, 288 Buoyant force, 300–305 Bursting water pipes, 339 Butterflies, and polarized light, 702
C C (coulomb), 489–490 Calculators, 552 Calorie, 341–342 Calorimetry, 342 Cameras, 751, 837–838
electronic flashes, 540 real images, 753
Capacitance, 537–539 parallel plate capacitors, 538–539 RCL circuits, 665–670
Capacitive reactance, 661–663 concept focus, 679 concept summary, 678 problems, 680
Capacitors, 537–541 ac circuits, 661–663 capacitance, 537–539 concept focus, 545 concept summary, 544 dielectrics, 537–539 energy storage, 540 equivalent, 576 in series and in parallel, 575–577 limiting behaviors of, 669 parallel plate. See Parallel plate capacitors problems, 548 RC (resistor–capacitor circuits), 577–579 relation between charge and potential
difference, 537 Capturing solar energy with mirrors, 718 Car lift, 299–300 Carbon dating, 900–902 Care package, projectile motion, 61–63 Cargo planes, overloaded, 232–233 Carnot’s principle/Carnot engine, 414–417
concept focus, 427 concept summary, 426 problems, 430
CAT scans, 853, 871–872 Cataract surgery, 445 Cavendish, Henry, 89 Cavitron ultrasonic surgical aspirator
(CUSA), 455 CCDs (charge-coupled devices), 837–838 CD (compact discs)
physics of, 798–799 use of interference, 798–799, 805
Celsius temperature scale, 326–328 Center of gravity, 231–235
concept summary, 246–247 problems, 249–251
Index I-3
Center of mass, 189–192 concept focus, 194 concept summary, 192 problems, 197 velocity, 190
centi (c), 3 Centrifuges, 214–215 Centripetal acceleration, 122–125
concept focus, 138 concept summary, 137 problems, 139 and tangential acceleration, 210–213, 215, 216, 219
Centripetal force, 125–128 artificial gravity, 135 Bohr model of hydrogen atom, 497 concept focus, 138 concept summary, 137 problems, 140 satellites in circular orbits, 130–133 vertical circular motion, 136–137
cg (center of gravity), 231 Chadwick, James, 885 Chain reactions, nuclear fission, 918 Characteristic X-rays, 870 Charge-coupled devices (CCDs), 837–838 Charge density, 504 Charge distribution, 510 Charged objects, and electric force, 490–492
concept focus, 516 concept summary, 516 problems, 517–518
Charged particles circular trajectory in magnetic fields, 596–597 electric vs. magnetic fields, 595–596 magnetic fields, 595–599 magnetic force, 594
Charges in a plane, 498–499 Charges on a line, 498 Charging by contact, 493–495
concept focus, 517 concept summary, 516
Charging by induction, 493–495 concept focus, 517 concept summary, 516 problems, 517
Charles’ law, 388 Chemical energy, and conservation of
energy, 164 Chemicals, detecting and measuring, 266 Chromatic aberration, 766 Circle of least confusion, 765 Circles, reference, 261–267
concept focus, 281 concept summary, 280 problems, 283–284
Circuits. See Electric circuits Circular motion. See Uniform circular motion Circular openings, waves, 471 Circular trajectory of charged particles, 596–597 Circumferences, A-4 Circus performers, 93 Clocks
atomic clock, 2 pendulums, 271
Clogged artery, 308 Clothes dryers, 579, 636 Clothing
dressing warmly, 365 summer clothing, 371
Cloud chamber, 905 Cochlear implants, 688 Coefficient of kinetic friction, 99 Coefficient of linear expansion, 331–332 Coefficient of performance, 419 Coefficient of static friction, 96–97 Coefficient of volume expansion, 337–338 Coffee maker, 335 Coherent sources, 467, 778 Coin tosses, free falling bodies, 43–44 Cold reservoir, 413 Colinear displacement vectors, 10 Collisions
concept focus, 193–194 concept summary, 192 elastic vs. inelastic, 184–188 one dimension, 184–189 problems, 196–197 two dimensions, 189
Colonoscope, 743–744 Color Doppler ultrasound, 456 Color, quarks, 927 Common logarithm, A-3 Communications Jammer team problem, 683 Compact discs (CDs)
physics of, 798–799 use of interference, 798–799, 805
Compasses, 591–592 Completely inelastic collision, 184 Complex sound waves, 481–482
concept summary, 483 problems, 486–487
Components definition of, 13 Newton’s second law of motion, 85–86 vectors, 13–18
Compound bow, 165–166 Compound microscope, 763
concept summary, 768 problems, 774
Compression, 275–276 adiabatic, 409–410 isothermal, 408–409
Compton effect, 840–842 concept focus, 850 concept summary, 849 problems, 851
Compton wavelength of the electron, 841 Computers
display monitors, 610 keyboards, 539 producing computer chips using
photolithography, 790 random-access memory (RAM) chips, 537
Concave mirrors, 716–719. See also Mirrors formation of images, 719–721 mirror equation and magnification equation,
722–724 virtual images, 724
Condensation, 440 Condense, 343 Conduction, 363–370
concept focus, 375–376 concept summary, 375 neurons, 541–542 problems, 376–378
Conductors, 493 concept focus, 517 concept summary, 516
electric fields, 508–510 problems, 518–520 superconductors, 557
Conductors, motional emf, 627–631 Confining plasma, 922 Conservation of energy, 164, 167, 528–529, 630 Constructive interference, 777 Contact, charging by, 493–494 Contact lenses, 760 Control rods, 919 Conservation of angular momentum, 244 Conservation of linear momentum, 180–184
concept focus, 193 concept summary, 192 problems, 195–196
Conservation of mechanical energy, 157–161 concept focus, 167 concept summary, 167 problems, 169–170
Conservative vs. nonconservative forces, 155–157 concept focus, 167 concept summary, 166 problems, 169
Constant force, 144–147 concept focus, 167 concept summary, 166 problems, 168
Constant loudness, 455 Constant-volume gas thermometer, 328 Constructive interference, 466–470
concept focus, 483 concept summary, 482 problems, 484
Convection, 360–363, 375 Conventional current, 553 Converging lens, 748–749
image formation, 750–751 ray diagrams and ray tracing, 749–750
Conversion of units, 3–5 Convex mirrors, 716, 718–719. See also Mirrors
formation of images, 721–722 mirror equation and magnification equation, 724–727 vs. plane mirrors, 724 virtual images, 724
Coordinate systems, 808 Copiers/computer printers, 513–515 Corotron, 514 Cosine (cos), 6–8, A-5 Cosmology, 928–930
Big Bang Theory, 928–929 concept focus, 932 concept summary, 931 standard model, 929–930
Coulomb (C), 489–490 Coulomb’s Law, 495–500
concept focus, 517 concept summary, 516 problems, 518–519
Counter emf, 645 Countertorque, and electrical energy generation,
644–645 Crab Nebula, electromagnetic spectrum, 690 Crack-the-whip ice-skating stunt, 208–210 Crick, Francis, 800 Critical angle, 739–740 Critical temperature, 557 Crossed polarizers/analyzers, 699–700 Crossing a River team problem, 325 Crude Thermometer team problem, 359
I-4 Index
Crude Thickness Monitor team problem, 807 Cruise control, 626 CT scans, 930 Current-carrying coils
net force exerted by current-carrying wire, 607 torque, 602–604
Current-produced magnetic fields, 605–612 concept focus, 618 concept summary, 617 long straight wire, 605–607 loop of wire, 607–609 problems, 621–622 solenoid, 609
Currents, 551–553 alternating current (ac). See Alternating current (ac) concept focus, 581 concept summary, 580 conventional current, 553 induced, 625–627 magnetic fields, 600–602 magnetic force on moving charge, 605–606 measurement of, 574–575 physiological effects of, 579–580 problems, 582–583 RCL circuits, 667–668 torque on current-carrying coil, 602–604
Curveballs, 312 CUSA (cavitron ultrasonic surgical aspirator), 455 Cycles, waves, 435 Cylinders
expanding, 336–337 rolling, 243
D d (deci), 3 da (deka), 3 Damped harmonic motion, 273–274
concept focus, 282 concept summary, 281
Dark energy, 928–929 Daughter nucleus, 892 Daytona International Speedway, 131 dc (direct current), 552
electric motor, 604 dc galvanometer, 574–575 de Broglie, Louis, 843 de Broglie’s explanation of Bohr’s assumption about
angular momentum, 861–862 concept summary, 879
de Broglie wavelength, 843–845 concept focus, 850 concept summary, 849 problems, 851
Deadly Virus team problem, 54 Decay constant, 898 Decay, radioactive, 891–896
concept focus, 907 concept summary, 906–907 half-lives, 897–900 problems, 909 radioactive decay series, 903–904 radon, 898–899
Deceleration, 37 deci (d), 3 Decibels, 448–450
concept focus, 458 concept summary, 457 problems, 462
Declination, compasses, 592
Decreasing velocity, 33 Deepwater Horizon oil spill, 361 Defibrillator, 540, 543 Deflection plates, inkjet printers, 515 Dehumidifier, 351 deka (da), 3 Density, nuclear, 887 Derived units, 3 Destructive interference, 466–470, 778
concept focus, 483 concept summary, 482 problems, 484
Detecting and measuring small amounts of chemicals, 266
Deuterium–tritium reaction, 921 Dewar flask, 374 Diamond Ring Solution team problem, 379 Diamonds, sparkles, 741 Diathermal walls, 401–402 Dielectric constant, 538 Dielectrics, 537–539
concept focus, 545 concept summary, 544 problems, 548
Difference, sound frequencies, 473 Diffraction, 470–473, 787–791
concept focus, 483, 802 concept summary, 482, 801 Electron Diffraction team problem, 852 problems, 485, 804 resolving power, 791–796 single-slit, 790 X-ray diffraction, 799–800
Diffraction grating, 796–798 concept focus, 802 concept summary, 801 problems, 805
Diffuse reflection, 713 Diffusion, 392–395
concept focus, 396–397 concept summary, 396 problems, 399
Digital cameras, 837–838 Digital movie projectors, 713 Digital satellite system TV, 132 Digital video discs (DVDs)
physics of, 798 use of interference, 798–799, 805
Dimensional analysis, 5–6 Dimensions, 5 Diodes, 673–675 Diopter, 760 Dipole moment, 506 Direct current (dc), 552
electric motor, 604 Directly proportional, A-2 Discus throwers, 211 Disorder, 423–424 Dispersion of light, 746–748
concept focus, 769 concept summary, 767 problems, 772
Displacement, 27–28 average velocity, 29 concept summary, 47 equations of kinematics, 34–41, 56–60 of light, by transparent material, 738 Newton’s second law of motion, 86 one-dimensional, 27–28
rotational vs. translational, 241 simple harmonic motion and reference circles,
261–262 two-dimensional, 55–56, 72, 74–75
Displacement vectors, 10–12, 14 Display monitors, 610 Distance, dimensional analysis, 5 Distribution of molecular speeds, 388–389 Diverging lens, 748–749
image formation, 751–752 ray diagrams and ray tracing, 749–750 virtual images, 754
Docking a Spaceship team problem, 199 Door-closing unit, 267 Doping, 673 Doppler effect, 450
concept focus, 458 concept summary, 457 problems, 462–463 sound, 450–454
Doppler effect, and electromagnetic waves, 704 astronomy, 696 concept focus, 705 concept summary, 704 electromagnetic waves, 695–697 problems, 707
Doppler flow meter, 455 Doppler shift, 451 Doppler ultrasound, 456 Double-slit interference, light waves, 779–782
concept focus, 802 concept summary, 801 problems, 803
Downhill skiing, 150–151 Driven harmonic motion, 274–275
concept focus, 282 concept summary, 281
Driving force, 274 Drug delivery systems, diffusion, 393 Dryera, 579, 636 DVDs (digital video discs)
physics of, 798 use of interference, 798–799, 805
Dye-sublimation printer, 346 Dynamics, 27
E Eagle eye, compared to human eye, 793–795 Ears/hearing
Fletcher–Munson curves, 455, 482 loss of hearing, 481–482 noise-canceling headphones, 467–468 sensitivity, 455–456 threshold of hearing, 447–449, 455, 482
Ebonite rod, 490–491, 493–494, 500 ECG (electrocardiogram), 543 Eclipses (solar), 202 EEG (electroencephalogram), 543 Efficiency, heat engines, 413–414
thermal pollution, 416–417 Efflux speed, 313 Einstein, Albert, 164, 391, 810
special relativity, 809–810, 819 EKG (electrocardiogram), 543 Elastic collisions, 184–188 Elastic deformation, 275–279
concept focus, 282 concept summary, 281 problems, 285–286
Index I-5
Elastic potential energy, 267–268 Electric charges. See also Electric fields; Electric forces
charge distribution, 510 definition of, 489 law of conservation of electric charge, 491 point charges. See point charges test charges, 500–501
Electric circuits alternating current (ac), 559–562 capacitors in series and in parallel, 575–577 concept focus, 581 concept summary, 580–581 current and voltage measurement, 574–575 electric power, 557–559 electromotive force and current, 551–553 grounding, 579 internal resistance, 570–571 Kirchhoff rules, 571–574 Ohm’s law, 553–554 parallel wiring, 565–568 partially in series/partially in parallel, 569–570 problems, 582–589 RC circuits, 577–579 resistance and resistivity, 554–557 safety, 579–580 series wiring, 562–565
Electric current, 551–553 Electric dipole, 506 Electric field lines, 505–508
concept focus, 517 concept summary, 516 problems, 519–520
Electric fields, 500–505 adding, 502 concept focus, 517 concept summary, 516 copiers/computer printers, 513–515 equipotential surfaces, 534–537 Gauss’ law, 510–513 inside conductors, 508–510 lines of force, 505–508 parallel plate capacitors, 504–505, 512 particle motion vs. magnetic fields, 595–596 point charges, 502–504 problems, 519–522 symmetry, 504 test charges, 500–501
Electric flux, 510–513 Electric forces
adhesion, 497–498 charged objects, 490–492 charging by contact and induction, 493–495 concept focus, 516–517 concept summary, 516 conductors and insulators, 493 Coulomb’s Law, 495–500 definition of, 491 electronic ink, 491, 492 law of conservation of electric charge, 491 origin of electricity, 489–490 point charges, 495–498 problems, 517–522
Electric generators, 641–646 back emf generated by electric motor, 645–646 concept focus, 654 concept summary, 652 electrical energy and countertorque, 644–645 problems, 657–658 production of emf, 641–644
Electric guitars, 625 pickups, 640
Electric motors, 604 back emf generation, 645–646 operating, 645
Electric potential, 523–530 concept focus, 544–545 concept summary, 544 conservation of energy, 528–529 of point charges, 530–534 problems, 546–550
Electric potential difference, 524–530 biomedical applications, 541–543 concept focus, 544–545 concept summary, 544 conservation of energy, 528–529 point charges, 530–534 problems, 546–547
Electric potential energy, 523–530 concept focus, 544–545 concept summary, 544 conservation of energy, 528–529 problems, 546–550
Electric power, 557–559 concept focus, 581–582 concept summary, 580 loudspeakers, 561 problems, 583
Electric stove, 556 Electrical circuits
alternating current (ac). See Alternating current (ac) impedance in RCL circuits, 665–667 power factor, 667
Electrical conductors, 493–494 concept focus, 517 concept summary, 516 problems, 518
Electrical energy and conservation of energy, 164 and countertorque, 644–645
Electrical extension cords, 555, 561–562 Electrical grounding, 579 Electrical insulators, 493–494
concept focus, 517 concept summary, 516 problems, 518
Electrical resistance thermometers, 329 Electrically neutral atoms, 490 Electrocardiogram (ECG or EKG), 543 Electroencephalogram (EEG), 543 Electroencephalography, 543 Electromagnetic induction
concept focus, 653 concept summary, 652–653 energy stored in inductors, 648 Faraday’s law, 634–637 generators, 641–646 induced emf and induced current, 625–627 Lenz’s law, 637–640 magnetic flux, 631–634 motional emf, 627–631 mutual inductance and self-inductance, 646–648 problems, 654–660 sound reproduction, 640–641 transformers, 649–651
Electromagnetic spectrum, 689–691 concept focus, 705 concept summary, 704 problems, 706
Electromagnetic waves, 684–686, 688–689 antennas, 685–686 concept focus, 704–705 concept summary, 704 Doppler effect, 695–697 electromagnetic spectrum, 689–691 energy carried by, 692–695 frequency, 686 intensity, 693–695 polarization, 697–703 power, 694–695 problems, 705–710 speed, 686 speed of light, 691–692 wavelength, 689–691 X-rays. See X-rays
Electromagnetism, 605 magnetic levitation, 615
Electromotive force. See emf (electromotive force) Electron capture, 894 Electron Diffraction team problem, 852 Electron Evaporator team problem, 624 Electron Gun team problem, 522 Electron volt (eV), 527–528 Electronic flashes, cameras, 540 Electronic ink, 491–492 Electrons, 489–490
angular momentum, in Bohr model, 861 breathing in, 848 coulombs, 490 Compton wavelength of the electron, 841 de Broglie wavelength, 843 high speed electrons, 818, 821 maximum speed of photoelectrons, 836–837 shells, 866 X-rays, 869
Electroreception, 515 Electroretinogram (ERG), 543 Electroretinography, 543
concept focus, 545 Electrostatic force, 491 Electrostatic Positioner team problem, 522 Electroweak force, 88, 896 Elementary particles, 922–928
antiparticles, 923–924 baryons, 925–926 bosons, 925–926 classification of particles, 925 concept focus, 932 concept summary, 931 hadrons, 925–926 leptons, 925–926 mesons, 925–926 muons, 924–925 neutrinos, 923 pions, 924–925 positrons, 923–924 problems, 934 quarks, 925–927 the standard model, 927–928
Elevators, 94–95 Makeshift Elevator problem, 174
Elliptical orbits, 245 Emergency Replacement Glasses team problem, 776 emf (electromotive force), 551–553, 626
back emf generated by electric motor, 645–646 concept focus, 581 concept summary, 580 determining polarity of induced emf, 638
I-6 Index
emf (electromotive force) (Continued ) Faraday’s law, 634–637 induced emf, 625–627 induction by a changing magnetic field, 635 induction in a rotating coil, 635 Lenz’s law, 637–640 magnetic flux, 631–632 motional emf, 627–631 problems, 582–583 produced by moving copper ring, 639 produced by moving magnet, 638 production of emf by generator, 641–644
Emission lines, 860 Emissivity, 372 Endoscopy, 743 Energy
average energy density of sunlight, 693 availability for doing work, 422 concept focus, 167–168 concept summaries, 166–167 conservation of energy, 164, 167, 630 conservation of mechanical energy, 157–161 conservative vs. nonconservative forces, 155–157 dark energy, 928–929 electric potential. See Electric potential energy electromagnetic waves, 692–695 flashlights, 558 golf ball, energy equivalent, 819 gravitational potential energy, 153–155 internal, 339–340 kinetic, 147–153 mass and energy equivalence, 819–824, 827–830 monatomic ideal gas, 391 nonconservative forces and work–energy theorem,
161–162 nuclear. See Nuclear energy nuclear binding energy, 888–890 photons, 834 power, 162–164 problems, 168–174 quantization, 834 rest energy, 819–820 rotational work and energy, 241–244, 247, 248,
252–253 simple harmonic motion, 267–270, 280–281, 282,
284–285 stored in inductors, 648 total energy, 819 total mechanical energy, 157–161
Energy density, 540, 648 Energy level diagrams, 859 Energy of a Bullet Dissipated by Plywood team
problem, 222 Engagement ring, heated, 336 Engines
Carnot engine, 414–417 heat engines, 413
Entropy, 420–424 concept focus, 427 concept summary, 426 problems, 430–431 second law of thermodynamics, 422
EPE. See Electric potential energy Equation of continuity, 307–309
concept focus, 318 concept summary, 317 problems, 322
Equations, A-2 Equations of kinematics
one dimension, 34–41, 47–48, 49–54 rotational, 205–208, 215, 216, 218 two dimensions, 56–60, 73, 75
Equilibrium between phases of matter, 347–349, 352, 353, 357 at constant velocity, 105 definition of, 102 and Newton’s second law of motion, 102–105 rigid objects, 4, 227–231, 246, 247, 249–251 thermal, 402 uniform circular motion, 127
Equilibrium vapor pressure, 347 Equipotential surfaces, 534–537
concept summary, 544 problems, 547–548
Equivalent capacitor, 576 Equivalent resistance, 562–563 ERG (electroretinogram), 543 Errors, checking for, 6 eV (electron volt), 527–528 Evaporate, 343 Evaporative cooling of human body, 349 Events, special relativity, 808–809
concept focus, 827 concept summary, 827
Exactly in phase, 466 Exactly out of phase, 467 Excited states, atoms, 859 Exercise
hot joggers, 340 staying cool, 375
Exercise thallium heart scan, 895 Expanding universe, 928 Expansion
adiabatic, 409–410 cylinders, 336–337 holes, 335–337 isothermal, 408–409 linear thermal, 330–337 volume thermal, 337–339
Expansion joint, 333 Exponents, A-3 Exposure, 912 Extension cords, 555–562 External forces, 84 Eyepiece, 756 Eyes. See also Human eye
LASIK eye surgery, 875 PRK eye surgery, 875 pupils of predators vs prey, 800
F f (femto), 3 F (force), 92 Fahrenheit temperature scale, 326–327 Far point, eyes, 758 Faraday, Michael, 634 Faraday’s law of electromagnetic induction,
634–637, 664 concept focus, 653 concept summary, 652 mutual inductance, 646–647 problems, 655–656 self-induction, 648
Farsightedness, 759–760 Fermi, Enrico, 916 Ferromagnetism/ferromagnetic materials, 613 Fetal oxygen monitors, 675 Fiber optics, 742–744
Fick’s law of diffusion, 394 Film projector, 751 Final velocity, 59
one dimension, 39, 40, 53 two dimensions, 57, 59, 63
Fingerprints, detecting, 614 Fireworks
nonconservative forces, 162 sound intensity, 447
First law of thermodynamics, 402–404 concept focus, 426–427 concept summary, 425 problems, 427
Fission, 916–919 concept focus, 932 concept summary, 931 problems, 933
Fixed axis, rotational motion about (Newton’s second law), 236–241
concept focus, 248 concept summary, 247 problems, 251–252
Fixing a Radio team problem, 589 Flashlights, 554, 558 Fletcher–Munson curves, 455, 482 Flow, 305–306
concept summary, 317 viscous flow, 314–317
Fluids Archimedes’ principle, 300–305 Bernoulli’s equation, 309–314 concept focus, 318 concept summaries, 317 equation of continuity, 307–309 isobaric expansion of water, 405 mass density, 28, 290 motion/flow, 305–306 Pascal’s principle, 298–300 pressure, 291–292 pressure and depth in static fluid, 293–297 pressure gauges, 297–298 problems, 319–325 specific heat capacity, 340 speed of sound, 445 viscosity, 306 viscous flow, 314
Flute, 479 Flux
electric, 510–513 magnetic flux, 631–634
Focal length, 718 lenses, 748 mirrors, 716, 719
Focal point lenses, 748 mirrors, 716, 718–719
Fog formation, 350 Football, projectile motion, 64–65 Force, 80–81
accelerations produced by action and reaction forces, 87
action-at-a-distance forces, 80 artificial gravity, 136 buoyant, 300–305 centripetal, 128–133, 136-137 concept focus, 112 concept summaries, 111–112 conservative vs. nonconservative forces, 155–157 constant, 144–147
Index I-7
driving, 274 electrical/electrostatic. See Electric forces external forces, 84 free-body diagrams, 86 gravitational force, 88–91 GUT (grand unified theory), 929 ideal, 306 internal forces, 84 lines of force, 505 loudspeakers, 601 magnetic, 592–595, 605–606 Newton’s first law of motion, 81–82 Newton’s second law of motion, 84–86, 100 Newton’s third law of motion, 86–88 noncontact forces, 80 normal force, 92–95, 100 problems, 114–120 restoring force of an ideal spring, 259–260 rigid objects, 223–226 static and kinetic friction, 95–101 swimmers, 292 tension, 101–102 types of, 88 units, 86 work done by constant force, 144–147, 166,
167, 168 work done by variable force, 164–166,
167, 172 Forced convection, 362–363 Fosbury Flop, 191–192 Foucault, Jean, 691 Four-resistor circuit, 569 Fraunhofer lines, 861 Free-body diagrams, 86, 95 Free-fall, 41 Freely falling bodies, 41–45
concept focus, 48 concept summary, 48 problems, 51
Freeze, 343 Freight trains. See Trains Frequency
driving force, 274 electromagnetic waves, 686 natural, 274 simple harmonic motion, 262 sound waves, 440–441 of vibration, 264–266 waves, 435
Frictional forces (friction), 95–101 concept focus, 113 concept summary, 112 problems, 115–116
Fringe field, 615 Frisch, Otto, 916 Fuel elements, nuclear reactors, 919 Full-length mirrors, 714 Full-wave rectifier circuits, 675 Function of state, 404 Functions (trigonometric), 6–8 Fundamental forces, 88 Fuse, 343 Fusion, 920–922
concept focus, 932 concept summary, 931 Hypothetical Fusion Reactor team
problem, 935 problems, 933–934
Fusion curve, 349
G G (universal gravitational constant), 89 Galilei, Galileo, 1 Galvanometers, 574–575
concept summary, 581 problems, 587
gamma (g) decay, 894 gamma (g) rays, 890–891
absorbed dose, 912–914 Gamma Knife radiosurgery, 894–895 Garage door openers, 838 Garden hose, 308 Gas Dosing Device team problem, 400 Gas Lift team problem, 432 Gases
Boltzmann’s constant, 384 Charles’ law, 388 diffusion, 392–395 ideal gas, 383–388 kinetic theory of gases, 388–392 Maxwell speed distribution, 389–390 monatomic ideal gas, 391 specific heat capacity, 341 speed of sound, 442–445 universal gas constant, 384
Gasoline, thin-film interference, 782–783 Gauge pressure, 297 Gauss’ law, 510–513
concept focus, 517 concept summary, 516 problems, 520
Gaussian surface, 510–513 Geiger counter, 904 Gell-Mann, M., 925 Gemstones, 382 Generator bike, 643–644 Generator Bike team problem, 660 Generators, 641–646
back emf generated by electric motor, 645–646 concept focus, 654 concept summary, 652 electrical energy and countertorque, 644–645 problems, 657–658 production of emf, 641–644
Geometry, A-4 GeV (one billion electron volts), 528 giga (G), 3 Glashow, Sheldon, 88, 896 Global Positioning System (GPS), 131
special relativity, 813 Golf ball, energy equivalent, 819 Goodyear airship, 303 GPS (Global Positioning System)
special relativity, 813 Gram-mole, 381 Grand unified theory (GUT) force, 929 Graphical analysis of velocity and acceleration, 45–47 Grating spectroscope, 798 Gravitational force, 88–91
concept focus, 111–113 problems, 115 satellites in circular orbits, 130–133
Gravitational potential energy, 153–155 concept summary, 166 problems, 169 total mechanical energy, 157–161
Gravity artificial, 133–135, 138, 141 center of, 231–235, 246–247, 249–251
conservative vs. nonconservative forces, 155–157 freely falling bodies, 41–45 g-suits, 137 universal gravitational constant, 89, 91, 130 weight, 90–91 and work, 153–155
Greenhouse effect, 692 Ground fault interrupter, 636 Ground state, atoms, 859, 866–868 Grounding, 579 g-suits, 139 Guitar
frets, 477–478 playing, 476–477 strings, 437
GUT (grand unified theory) force, 929 Gymnasts
average angular velocity, 204 trampolines, 154
H H (henry), 647 Hadron family of particles, 925–926 Hafele J. C., 814 Hahn, Otto, 916 Half-length mirrors, 714 Half-life, 897–900
radioactive dating, 900–903 Half-wave rectifier, 675 Halogen cooktop stove, 374 Harmonics, 474 Head mirror, 727 Head-up displays (HUDs), automobiles, 721 Hearing, 455–456
Fletcher–Munson curves, 455, 482 loss of, 481–482 noise-canceling headphones, 467–468 threshold of hearing, 447–449,
455, 482 Heart pacemakers, 578, 580 Heat. See also Heat engines; Heat pumps;
Heat transfer concept focus, 352 concept summaries, 352 definition of, 339 equilibrium between phases of matter, 347–349 humidity, 350–351 internal energy, 339–340 linear thermal expansion, 330–337 mechanical equivalent of heat, 342 phase change, latent heat, 343–346 problems, 353–359 second law of thermodynamics, 412–413 temperature change, specific heat capacity,
340–343 temperature scales, 326–329 thermometers, 329–330 units, 341–342 volume thermal expansion, 337–339
Heat engines, 413 Carnot’s principle/Carnot engine, 414–417 concept focus, 427 concept summary, 426 efficiency, 416–417 problems, 429–430
Heat pumps, 417–420 concept focus, 427 concept summary, 426 problems, 430
I-8 Index
Heat transfer applications of, 373–375 concept focus, 375–376 concept summaries, 375 conduction, 363–370 convection, 360–363 heating and cooling by convection, 361–362 in human body, 366 problems, 376–379 radiation, 370–373
Heating element, electric stove, 556 hecto (h), 3 Heisenberg uncertainty principle, 845–848, 865–866
concept focus, 850 concept summary, 849 problems, 851–852
Heisenberg, Werner, 844 Helicopters
relative velocity, 68 tangential speeds and tangential
accelerations, 209 Turbo-shaft Helicopter team problem, 710
Helium, binding energy of nucleus, 888–889 henry (H), 647 Henry, Joseph, 634 HIFU (high-intensity focused ultrasound), 455 High jumpers, 191–192 High-Performance Engine team problem, 432 High-tech clothing, 344–345 Hinges, 224–225 Hole expansion, 335–336 Holography, 876–878 Hooke’s law
restoring force of ideal spring, 259–260, 264, 270 stress and strain, 279–280, 281, 282, 285–286
Hoover Dam, 294 Hope diamond, 382 Hot air balloons, thermodynamics, 401–402 Hot joggers, 340 Hot reservoir, 413 Hot showers, 341 Household plumbing, 311 Hubble parameter, 928–929 Hubble, Edwin P., 928 Hubble Space Telescope
Doppler effect, 697 locating black holes, 131–132 physics of, 130 temperature regulation, 374 weight of, 90
Hubble’s law, 928–929 HUDs (head-up displays), automobiles, 721 Hughes-Fulford, Millie, 265 Human bones, 93
compression, 276 mechanical properties, 280 structure, 276
Human eye, 756–761 anatomy, 756–757 compared to eagle eye, 793–795 concept focus, 769 concept summary, 767 corrective surgery, 875 farsightedness, 759–760 infant vision, 766 nearsightedness, 758–759 optics, 757–758 problems, 773–774 refractive power of lens (diopters), 760
Humidity, 350–351 concept focus, 353 concept summary, 352 problems, 357
Huygens’ principle, 787–789, 791 Hydraulic car lift, 299–300 Hydrogen
Bohr model, 496–497, 857–861 Brackett series, 860 line spectra, 859 line spectrum, 856 quantum mechanical picture of, 862–866 uncertainty principle, 865–866
Hyperopic, 759 Hyperopic vision, 759–760 Hypothetical Fusion Reactor team problem, 935
I IC (integrated circuit) chips, 677 Ice cold lemonade, 345 Ice formation and aquatic life, 338–339 Ice hockey, Newton’s first law of motion, 81 Ice Man, 901–902 Ice skaters, conservation of linear momentum,
182–183 Iced-up refrigerator, 369 Ideal gas law, 383–388
concept focus, 396 concept summary, 395–396 kinetic theory of gases, 388–392 problems, 397
Ideal gasses first law of thermodynamics, 404 monatomic, 391, 411–412 speed of sound, 442 thermal processes, 408–411
Ideal fluid, 306 Ideal spring, 257–261
concept focus, 281 concept summary, 280 problems, 282–283
Identifying Unknown Metals team problem, 852 Image point, 716 IMAX 3-D movies, 699–700 Impedance in RCL circuits, 665–667 Impedance plethysmography, 555–556 Implantable medical devices, 651–652 Impulse
center of mass, 189–192 collisions in one dimension, 184–189 collisions in two dimensions, 189 concept focus, 193–194 concept summaries, 192 conservation of linear momentum, 180–184 definition of, 176 problems, 194–199
Impulse–momentum theorem, 175–179 concept focus, 193 concept summary, 192 problems, 194
Impurity atoms, 673 Increasing velocity, 32 Index of refraction, 733–734
concept summary, 767 problems, 769–770
Indirect Cooling with Liquid Nitrogen team problem, 379
Induced current, 625–627 concept summary, 652
Induced emf, 625–627 concept summary, 652
Induced magnetic field, 637 Induced magnetism, 613–614 Induced nuclear reactions, 915–916
concept focus, 932 concept summary, 931 problems, 933
Induced nuclear transmutation, 915–916 Inductance, 647
RCL circuits, 665–670 Induction, charging by, 493–495
concept focus, 517 concept summary, 516 mutual induction, 646 problems, 517 self-induction, 647
Induction stove, 636–637 Inductive reactance, 664–665
concept focus, 679 concept summary, 678 problems, 680
Inductors, 648 ac circuits, 664–665 limiting behaviors of, 669
Inelastic collisions, 184–188 Inertia
axis of rotation, 238 definition of, 82 and mass, 81–82 moment of inertia I of the body, 237 moment of inertia of the particle, 236 rotational vs. translational, 241
Inertial confinement, 922 Inertial reference frames, 82, 808–809
concept focus, 827 concept summary, 827
Infrasonic sound waves, 441 Initial velocity
one dimension, 53 two dimensions, 57
Inkjet printers, 515 Instantaneous acceleration, 31–32, 56 Instantaneous angular acceleration, 205 Instantaneous angular speed, 204 Instantaneous angular velocity, 204 Instantaneous speed, 30 Instantaneous velocity, 30
slope of tangent line, 46 two dimensions, 56
Insulation, 367–368 rating (R values), 373–374
Insulators, 493 concept focus, 517 concept summary, 516 problems, 518
Integrated circuit (IC) chips, 677 Intensity of electromagnetic waves, 693–695 Intensity of sound waves, 446–448
concept focus, 458 concept summary, 457 decibels, 448–450 problems, 461
Interference of light waves CDs and DVDs, 798–799 concept focus, 802 concept summaries, 801 constructive interference, 777 destructive interference, 778
Index I-9
diffraction, 787–791 diffraction grating, 796–798 Michelson interferometer, 786–787 principle of linear superposition, 777–779 problems, 803–807 resolving power, 791–796 thin-film, 782–786 X-ray diffraction, 799–800 Young’s double-slit experiment, 779–782
Interference of sound waves, 466–470 concept focus, 483 concept summary, 482 problems, 484
Intermittent windshield wipers, 578 Internal energy, 339–340
concept summary, 352 problems, 355–356
Internal forces, 84 Internal resistance, 570–571
concept focus, 582 concept summary, 581 problems, 586
Inverse trigonometric functions, 7 Inversely proportional, A-2 Inversion layer, 362 Ion propulsion drive, 149 Ionization energy, 859 Ionizing radiation, 911–915
concept summary, 932–933 problems, 932–933
Ions, mass spectrometers, 599–600 Irreversible process, 420–422 Isobaric process, 404–406, 410 Isochoric process, 406, 410 Isotherm, 385 Isothermal expansion or compression, 408–409 Isothermal process, 406, 410 Isotope Separator team problem, 624 Isotopes, 886, A-5–A-8
uranium, 917
J Jell-O, shear modulus, 277 joule (J), 145, 342 Joule, James, 342 Joysticks, 565 Junction rule, 571–574
K k (spring constant), 258 K capture, 894 Kα characteristic X-ray for platinum, 870 Keating, R. E., 814 Kelvin temperature scale, 328–329
concept focus, 352 concept summary, 352 problems, 353–354
Kepler’s second law of planetary motion, 245 Keratometers, 725 Keyboards, computers, 539 kilo (k), 3 kilocalorie, 341–342 kilogram (kg), 2 Kinematics, 27
one dimension. See Kinematics (one dimension) two dimensions. See Kinematics (two dimensions) rotational. See Rotational kinematics
Kinematics (one dimension), 34–41 acceleration, 31–36
concept focus, 48 concept summaries, 47–48 constant acceleration, 34–36 displacement, 27–28 equations, 37–41 freely falling bodies, 41–45 graphical analysis of velocity and acceleration,
45–47 problems, 49–54 speed and velocity, 28–30
Kinematics (two dimensions), 56–60 acceleration, 57–59 concept summary, 72–73 displacement, 55–56 equations, 56–60 problems, 74–79 projectile motion, 60–67 relative velocity, 68–72
Kinetic energy, 147–148 figure skaters, 246 relation to total energy, 820 rotational vs. translational, 241 total mechanical energy, 157–161 work–energy theorem, 147–153, 166
Kinetic friction, 95–101 concept focus, 113 concept summary, 112 problems, 115–116
Kinetic theory of gases, 388–392 concept focus, 396 concept summary, 396 problems, 398
Kingda Ka roller coaster, 160, 161 Kirchhoff rules, 571–574
concept focus, 582 concept summary, 581 problems, 586–587
L Laser altimeter, 874 Laser lithotripsy, 878 Laser printers, 514–515 Laser scalpel, 703 Lasers, 872–876
concept focus, 880 concept summary, 879 holography, 876–878 laser beam speed, 825–826 medical applications, 874–876 problems, 882
LASIK eye surgery, 875 Latent heat, 343–346
concept focus, 353 concept summary, 352 problems, 356–357
Latent heat of fusion, 344 Latent heat of sublimation, 344 Latent heat of vaporization, 344 Law of conservation of electric charge, 491 Law of conservation of mechanical energy.
See Conservation of mechanical energy Law of cosines, A-5 Law of reflection, 712 Law of sines, A-5 LCDs (liquid crystal displays), 701 Leaves, water loss, 394 LEDs (light-emitting diodes), 675 Lemonade (ice cold), 345 Lemur warming up, 371
Length contraction, 815–817 concept focus, 828 concept summary, 827 problems, 829
Length, meter (m), 2 Lenses, 748–756
aberrations, 765–766, 768–769 concept focus, 769 concept summaries, 767 converging, 748–750 diverging, 748–750 Emergency Replacement Glasses team problem, 776 formation of images, 749–752 human eye, 756–758 in combination, 755–756 infant vision, 766 problems, 772–773 ray diagrams and ray tracing, 749–750 resolving power, 791–796 sign conventions, 753 thin-lens and magnification equations, 752–755
Lenz’s law, 637–640 concept focus, 653 concept summary, 652 problems, 656–657
Lepton family of particles, 925–926 Lever arms, 224 Light
average energy density of sunlight, 693 Compton effect, 840–842 dispersion (prisms and rainbows), 746–748 interference of waves. See Interference of
light waves particle (corpuscular) theory, 782 photoelectric effect, 834–839 polarization. See Polarization polarized light in nature, 702 reflection. See Reflection of light refraction. See Refraction of light speed. See Speed of light wave interference. See Interference of light waves wave nature of. See Wave nature of light wavelengths for visible light, 690
Light-Beam Metronome team problem, 288 Light bulbs, 559, 562
flashlight, 554 operating with motional emf, 628–630 photons, 834–835 three-way, 568
Light-emitting diodes (LEDs), 675 Line of action, 224 Line spectra, 855–856
concept summary, 878 hydrogen, 859 problems, 881
Linear expansion, 330 Linear momentum. See also Momentum
conservation of linear momentum, 180–184, 192, 193, 195–196
definition of, 176 Linear superposition, 465–467, 777–779
concept focus, 483, 802 concept summary, 482, 801 problems, 484, 803
Linear thermal expansion, 330–337 bimetallic strip, 334–335 concept focus, 352–353 concept summary, 352 expansion of holes, 335–337
I-10 Index
Linear thermal expansion (Continued ) normal solids, 330–332 problems, 354–355 thermal stress, 333–334
Linearly polarized waves, 697–698 Liquid crystal displays (LCDs), 701 Liquid Nitrogen team problem, 379 Liquids. See Fluids Lithium ionization, 859 Lithotripsy, 878 Logarithms, A-3 Long Trip team problem, 831 Longitudinal sound waves, 439–440 Longitudinal standing waves, 478–480
concept focus, 484 concept summary, 482–483 problems, 486–487
Longitudinal waves, 434 Loop rule, 571–574 Loop-the-loop motorcycle stunt, 137 Lost Drone team problem, 54 Loudness, 442 Loudspeakers
diaphragm, 263–264, 439–440 electric power, 561 force and acceleration, 601 physics of, 471–472 sound wave interference, 468–469 wiring, 469–470
Lungs energy in, 395 oxygen, 384
Lyman series, 856–860 Lynx paws, 292
M Maglev (magnetically levitated) trains, 615 Magnetic confinement, 922 Magnetic domain, 613 Magnetic fields, 590–592
Ampère’s law, 612–613 angle of dip, 592 circular trajectory of charged particles, 596–597 compasses, 591–592 concept focus, 617–618 concept summary, 616–617 current-produced, 605–612 definition of, 593 emf induced by a changing magnetic field, 635 finding magnetic field, 608 force exerted on moving charge, 592–595, 605–606 force on currents, 600–602 fringe fields, 615 mass spectrometers, 599–600 motion of charged particle, 595–599 navigation in animals, 592 northern lights (aurora borealis), 590 particle tracks in bubble chamber, 598 problems, 618–624 Right-Hand Rule No. 1 (RHR-1), 593 Right-Hand Rule No. 2 (RHR-2), 605 torque on current-carrying coil, 602–604 velocity selectors, 595–596
Magnetic fingerprint powder, 614 Magnetic flux, 631–634
concept focus, 653 concept summary, 652 Faraday’s law, 634–637 general expression for, 632–633
graphical interpretation, 634 Lenz’s law, 637–640 motional emf, 631–632 problems, 655
Magnetic force, 592–595 charged particles, 594 circular trajectory of charged particles, 596–597 concept summary, 616 currents, 600–602 force and acceleration in loudspeakers, 601 moving charges, 592–593, 605–606
Magnetic materials, 613–616 concept summary, 617 ferromagnetic, 613 induced magnetism, 613–614 maglev (magnetically levitated) trains, 615 magnetic tape recording, 614–615
Magnetic moment, current-carrying coil, 603 Magnetic resonance imaging (MRI), 609–610, 616 Magnetic tape recording, 614–615 Magneto-optic Device team problem, 710 Magnification equation, 722–727, 752–755
concept focus, 729 concept summary, 728, 767 problems, 772–773, 730–731
Magnifying glasses, 751, 761–763 concept focus, 769 concept summary, 768 problems, 774
Magnifying power, 761 Makeshift Elevator team problem, 174 Makeup mirrors, 721 Malus’ law, 698–702 Mars rover, 80 Mass, 80–81
atomic mass number, 886 atomic mass unit, 889 center of mass, 189–192, 192, 194, 197 concept focus, 112 concept summaries, 111–112 definition of, 82 dimensional analysis, 5 inertia, 81–82 kilogram (kg), 2 mass and energy equivalence, 819–824, 827–830 massless spring, 822 molecular, 380–382 Newton’s first law of motion, 81–82 Newton’s second law of motion, 84–86, 100 Newton’s third law of motion, 86–88 problems, 114–120 relation between mass and weight, 91 sun, 821 units, 86
Mass defect of nucleus, 888–890 concept focus, 907 concept summary, 906 problems, 908
Mass density, 28, 290 concept summary, 317 problems, 319
Mass spectrometers, 599–600 concept summary, 617 problems, 619
Mathematical concepts dimensional analysis, 5–6 problem solving, 3–6 trigonometry, 6–8 units, 1–6
Mathematical description of a wave, 439 concept focus, 458 concept summary, 457 problems, 460
Matter phases, 343–349 wave nature, 843–845
Maximum possible force, magnetic fields, 592 Maxwell, James Clerk, 2, 88, 684, 685, 691 Maxwell speed distribution curves, 389–390 Mechanical energy
conservation, 157–161, 167, 169–170 transforming chemical into mechanical energy, 164
Mechanical equivalent of heat, 342 Mechanics, 27 Medical diagnostic techniques, 542–543 mega (M), 3 Meitner, Lise, 916 Melt, 343 Mercury vapor street lamps, 855 Mesons, 925–926 Metals, Identifying Unknown Metals team
problem, 852 Metastable, 873 meter (m), 2 MeV (one million electron volts), 528 Michelson, A. A., 810 Michelson, Albert, 691 Michelson interferometer, 786–787
concept summary, 801 micro (μ), 3 Micromirrors, 713 Microphones, 641 Microscopes
compound microscope, 763 lenses in combination, 755–756 scanning electron microscope (SEM), 832
Microwave ovens, 692 milli (m), 3 Mirror equation, 722–727
concept focus, 729 concept summary, 728 problems, 730–731
Mirrors angle of reflection/angle of incidence, 712 capturing solar energy, 718 concept focus, 728–729 concept summary, 728 focal length, 716, 718–719 focal point, 716 full-length vs. half-length, 714 head mirror, 727 image formation by plane mirrors, 713–715 image formation by spherical mirrors, 719–722 keratometers, 725 micromirrors, 713 mirror equation and magnification equation,
722–727 multiple reflections, 714–715 parabolic mirrors, 718 principle of reversibility, 720 problems, 729–732 real images, 714, 716, 720 reflection of light, 712–713 speed of light measurement, 691 spherical mirrors, 716, 718–722 virtual images, 714, 721, 724 wave front and rays, 711–712
Moderators, nuclear reactors, 919
Index I-11
Molar specific heat capacity, 411 Mole, 380–382
concept focus, 396 concept summary, 395 problems, 397
Molecular mass, 380–382 concept focus, 396 concept summary, 395 problems, 397
Molecular speeds, distribution of, 388–389 Moment of inertia
of the body, 237 of the particle, 236
Momentum angular, 244–246, 247, 248, 253 angular momentum of electron, in Bohr model,
861–862 center of mass, 189–192 collisions in one dimension, 184–189 collisions in two dimensions, 189 concept focus, 193–194 concept summaries, 192 conservation of linear momentum, 180–184 impulse–momentum theorem, 175–180, 192,
193, 194 photons, and Compton effect, 840–842 problems, 194–199 relation with total energy, 823 relativistic momentum, 817–818 rotational vs. translational, 241
Monatomic ideal gas, 391, 412 Monitors, 610 Moon rover, 91 Morley, E. W., 810 Motion, Newton’s laws. See Newton’s laws
of motion Motional emf, 627–631
concept focus, 653 concept summary, 652 and electrical energy, 628–630 magnetic flux, 631–632 operating a light bulb, 628–630 problems, 654
Motorcycles applications of equations of kinematics, 39 conservation of mechanical energy, 159 loop-the-loop stunt, 137 Motorcycle Jump team problem, 79
Moving charges, magnetic fields, 592–594, 605–606 Moving light advertisements, 263 MRI (magnetic resonance imaging), 609–610, 616 Multiplying vectors, 11 Muons, 924–925
confirmation of time dilation, 814 Musical instruments
guitar, 437, 476–478 tuning, 474 wind instruments, 479
Mutual inductance, 646–647 concept focus, 654 concept summary, 652 problems, 658
Mutual induction, 646 Myopic vision, 758–759 Mysterious Underwater Object team problem, 464
N n (nano), 3 N (newton), 90
Natural convection, 362 Natural frequency, 274, 476 Natural logarithm, A-3 Navigation in animals, earth’s magnetic field, 592 Navstar Global Positioning System (GPS), 131 Near field, 685 Near point, eyes, 758 Nearsightedness, 758–759 Neddermeyer, S. H., 924 Negative acceleration, 37 Neon signs, 855 Net magnetic field, 608 Neurons, conduction in, 541–542 Neutrino, 896, 923
concept summary, 906 Neutron, 885 Neutrons, 489–490
vs. protons or alpha particles, 918 Newton (N), 90 Newton, Isaac, 1, 81
particle (corpuscular) theory of light, 782 Newton’s first law of motion, 81–82
and uniform circular motion, 125 Newton’s law of inertia, inertial reference
frames, 808 Newton’s law of universal gravitation, 88–91 Newton’s laws of motion, 81–88
concept focus, 112 concept summaries, 111–112 equilibrium applications, 102–105 inertial reference frames, 82 nonequilibrium applications, 106–111 problems, 114–120
Newton’s rings, 785 Newton’s second law of motion, 84–86, 100,
236–241 concept focus, 248 concept summary, 247 frequency of vibration, 264–265 impulse and momentum, 176 problems, 251–252 vector nature, 85–86
Newton’s third law of motion, 86–88 NEXRAD, 453 NMR (Nuclear Magnetic Resonance), 678 Nodes, 474 Noise-canceling headphones, 467–468 Nonconservative forces, 161–162
concept focus, 167 concept summary, 166–167 problems, 168–171
Nonconservative vs. conservative forces, 155–157 concept focus, 167 concept summary, 166 problems, 169
Noncontact forces, 80 Nonequilibrium, and Newton’s second law of
motion, 106–111 Nonfundamental forces, 88 Nonuniform circular motion, 210 Normal force, 92–95, 100
centripetal force, 125 concept focus, 112–113 definition of, 92 problems, 115
North magnetic pole, 590 Northern lights, 590 npn transistors, 676 n-type semiconductors, 673–674
Nuclear atom, 853–855 concept summary, 878 problems, 880
Nuclear binding energy, 888–890 concept focus, 907 concept summary, 906 problems, 908
Nuclear density, 887 Nuclear energy, 915–922
concept focus, 932 concept summary, 931 induced nuclear reactions, 915–916 nuclear fission, 916–919 nuclear fusion, 920–922 nuclear reactors, 919–920 problems, 933–935
Nuclear fission, 916–919 concept focus, 932 concept summary, 931 problems, 933
Nuclear fusion, 920–922 concept focus, 932 concept summary, 931 Hypothetical Fusion Reactor team problem, 935 problems, 933–934
Nuclear Magnetic Resonance (NMR), 678 Nuclear physics
concept focus, 907 concept summaries, 906 mass defect, and binding energy, 888–890 nuclear structure, 885–887 problems, 908, 910 radioactivity. See Radioactivity strong nuclear force, and stability of nucleus,
887–888 Nuclear reactions, 915–916 Nuclear reactors, 919–920
concept summary, 931 problems, 933
Nuclear structure, 885–887 concept focus, 907 concept summary, 906 problems, 908
Nucleon number, 886 Nucleons, 885
O Objective, 756 Ocular, 756 Oersted, Hans Christian, 605 Ohm’s law, 553–554
concept focus, 581 concept summary, 580 problems, 582–583
One-dimensional kinematics acceleration, 31–36 concept focus, 48 concept summaries, 47–48 displacement, 27–28 freely falling bodies, 41–45 graphical analysis of velocity and acceleration,
45–47 problems, 49–54 speed and velocity, 28–30
Optical fibers, 742–744 Optical instruments
astronomical telescope, 764–765 compound microscope, 763 lenses. See Lenses
I-12 Index
Optical instruments (Continued ) magnifying glasses, 761–763 microscopes, 755–756, 763 resolving power, 791–796 telescopes, 764–765
Optical Monochromator team problem, 807 Optical Spectrometer team problem, 776 Orbital quantum number, 863, 868 Orbits, satellites
circular, 130–133 apparent weightlessness and artificial gravity,
133–135 elliptical, 245 Hubble Space Telescope, 130
Order to disorder, 423–424 Ovens, microwave, 692 Overdamped motion, 274 Overtones, 475 Oxygen in lungs, 384
P Pacemakers, 578, 580 Parabolic mirrors, 718 Parallel capacitors, 575–577
problems, 582, 587 summary, 581
Parallel plate capacitors, 504–505 capacitance, 538–539 deflection plates, 515 electric fields, 512 equipotential surfaces, 535–536
Parallel wiring, 565–568 circuits wired partially in series/partially in parallel,
569–570 concept focus, 582 concept summary, 581 problems, 584–586
Paraxial light rays, 718–719 Parent nucleus, 892 Partial pressure, 350 Particle (corpuscular) theory of light, 782 Particle tracks in bubble chamber, 598 Particles
alpha particles, vs. neutrons, 918 antiparticles, 923–924 blackbody radiation and Planck’s constant,
833–834 classification of, 925 concept focus, 849–850 concept summaries, 849 de Broglie wavelength, 843–845 Heisenberg uncertainty principle, 845–848 moment of inertia of the particle, 236 photon momentum and Compton effect,
840–842 photons and photoelectric effect,
834–839 problems, 850–852 speed, 438 wave function of, 844 wave–particle duality, 832–833
pascal (Pa), 278 Pascal’s principle, 298–300
concept summary, 317 problems, 321
Paschen series, 856, 860 Passenger-side automobile mirrors, 722 Pauli, Wolfgang, 866
neutrinos, 896, 923
Pauli exclusion principle, 866–868 concept focus, 880 concept summary, 879 problems, 882
PCM (phase-change material), 345 PDAs (personal digital assistants), 564–565 PEG (personal energy generator), 642 Pendulum, 270–273
concept focus, 282 concept summary, 281 problems, 285
Penzias, Arno A., 929 Perfect blackbody, 371 Period T, 121, 262, 435 Periodic table, and Pauli exclusion principle, 866–868 Periodic waves, 435–436
concept focus, 457 concept summary, 456–457 problems, 458–459
Permeability of free space, 605 Permittivity of free space, 495 Perpendicular displacement vectors, 10 Personal digital assistants (PDAs), 564–565 Personal energy generator (PEG), 642 PET scans, 923–924 Phase-change material (PCM), 345 Photodynamic therapy, 875–876 Photoelectric effect, 834–839
concept focus, 849 concept summary, 849 problems, 850–851 silver surface, 835
Photoelectrons, 834 Photoevaporation and star formation, 838–839 Photographic emulsion, 905 Photolithography, 790 Photons, 834
Compton effect, 840–842 photoelectric effect, 834–851 spontaneous and stimulated emission, 872
Physical pendulum, 271–272 Physics, 1–6
nature of, 1–2 problem solving, 3–6 scalars and vectors, 8–18 trigonometry, 6–8 units, 2–6
Physiological effects of current, 579–580 pico (p), 3 Pile driver, 155 Pions, 924–925 Pitch, 441 Pixel, 491 Planck’s constant, 833–834, 848
concept focus, 849 concept summary, 849
Plane mirrors. See also Mirrors angle of reflection/angle of incidence, 712 concept focus, 729 concept summary, 728 vs. convex mirrors, 724 full-length vs. half-length, 714 image formation, 713–715 law of reflection, 712 multiple reflections, 714–715 problems, 729–730
Plane waves, 712 Plant leaves, water loss, 394 Plasma, 921
Plethysmography, 555–556 Plum-pudding model of atoms, 853–854 Plumbing, 311 p-n junction diodes, 673–675 pnp transistors, 676–677 Pocket calculator, 552 Point charges, 495–500
electric fields, 502–504 electric potential difference, 530–544 exertion of force on each other, 495–497 forces due to two or more other point charges,
498–499 Gaussian surfaces, 510–513
Polarization, 697–703 concept focus, 705, 769 concept summary, 704, 767 crossed polarizers/analyzers, 699–700 linearly polarized waves, 697–698 Malus’ law, 698–702 polarized light in nature, 702 problems, 707–708, 771–772 refraction of light, 745–746
Polarizers, 698–699 Polaroid sunglasses, 699, 702 Population inversion, 873 Port-wine stain removal, 875 Positrons, 894, 923–924 Postulates of special relativity, 809–811
concept summary, 827 Potential difference
capacitors, 537 Potential energy
electric, 523–530, 544. See also Electric potential Potential gradient, 535 Power, 162–164
concept focus, 168 concept summary, 167 electric power, 557–559 electromagnetic waves, 694–695 flashlights, 558 problems, 172 RCL circuits, 668–669 series circuits, 563–564 sound waves, 446
Power factor, 667 Power supplies, 675 Powers of ten, A-1 Prefixes, multiples of 10, 3 Pressure, 278, 291–292
concept summary, 317 depth in a static fluid, 293–297, 317, 318, 320 gauges, 297–298, 317, 320 problems, 319 standard temperature and pressure (STP), 384
Pressure amplitude, sound waves, 441–442 Pressure cuff, 556 Pressure–volume graph, 407 Principal axis of a mirror, 716 Principal fringes/principal maxima, 796–797 Principle of conservation of angular momentum, 244 Principle of conservation of linear momentum, 180–184
concept focus, 193 concept summary, 192 problems, 195–196
Principle of conservation of mechanical energy, 158 Principle of linear superposition, 465–467, 777–779
concept focus, 483, 802 concept summary, 482, 801 problems, 484, 803
Index I-13
Principle of reversibility, 720 Printers, 513–515 Prisms, 741–742, 746–748
concept focus, 769 concept summary, 767 problems, 772
PRK eye surgery, 875 Problem solving, 3–6 Projectile motion, 60–67
concept focus, 73–74 problems, 75–76
Projectors, 751 Proper length, 816 Proper time interval, 813 Proportionality constant, A-2 Proportions, A-2 Proton Gun team problem, 550 Proton–proton cycle, 921 Protons, 489–490
motion in magnetic field, 597 vs. neutrons, 918
p-type semiconductors, 673–674 Pulling a suitcase, 145 Pumping water, 296 Punch bowl temperature, 345–346 Pure tone, 440 Pyroelectric ear thermometer, 690 Pythagorean theorem, 8, A-5
final velocity, 59 vector components, 14 time dilation, 812
Q Quadratic formula, A-3 Quantization of energy, 834 Quantum mechanical picture of hydrogen,
862–866 Quantum mechanics, 844
vs. Bohr model, 864 Quantum number, 862–863, 868 Quarks, 925–927 Quasi-static, 404
R R values, insulation rating, 373–374 Radar, NEXRAD, 453 Radian (rad), 201 Radiation, 370–373
concept focus, 376 concept summary, 375 problems, 378 Stefan–Boltzmann law, 372
Radiation detectors, 904–906 concept summary, 907
Radiation field, 685 Radiation sickness, 914 Radiators, automobiles, 338 Radio reception, 688 Radio waves, 436
AM and FM reception, 686, 691 Radioactive dating, 900–903
concept focus, 907 concept summary, 907 problems, 909
Radioactive Dating of a Mystery Object team problem, 910
Radioactive decay series, 903–904 concept summary, 907
Radioactivity, 890–906
concept focus, 907 concept summaries, 906–907 decay, 891–904 ionizing radiation, 911–915 neutrino, 896 problems, 908–910 smoke detectors, 893
Radioisotope Thermoelectric Generator team problem, 910
Radios Communications Jammer team problem, 683 Fixing a Radio team problem, 589 tank circuits, 681
Radius of Curvature of a Partial Sphere team problem, 732
Radon, 914 radioactive decay and activity, 898–899 radon gas in houses, 897
Rafts, Newton’s second law of motion, 85–86 Rain
on car windows, 70 impulse and momentum, 179–180
Rainbows, 746–748 concept focus, 769 concept summary, 767 problems, 772
Random-access memory (RAM) chips, 537 Rarefaction, 440–441 Ray diagrams, 749–750
thin-lens and magnification equations, 754 Ray tracing, 719, 749–750
concave mirrors, 719–721 converging and diverging lenses, 750 convex mirrors, 721–722
Rayleigh criterion, 792, 794 Rays
light, 711–712 paraxial rays, 718
RBE (relative biological effectiveness), 913 RC (resistor–capacitor) circuits, 577–579
concept focus, 582 concept summary, 581 problems, 587–588
RCL circuits, 667–670 concept focus, 679 concept summary, 678–679 current, 667–668 impedance, 665–667 problems, 680–681 Reconfigurable RCL Circuit team problem, 683 resonance, 670–672 voltages and power, 668–669
Real images cameras, 753 mirrors, 714, 716, 720
Reconfigurable RCL Circuit team problem, 683 Reconfiguring a Transformer team problem, 660 Rectifier circuits, 675 Reference circles, 261–266
concept focus, 281 concept summary, 280 problems, 283–284
Reference frames, 808 Reflected sound, 448 Reflection of light, 712–713
angle of reflection/angle of incidence, 712 concept focus, 728–729 concept summary, 728 full-length vs. half-length mirrors, 714
image formation by plane mirrors, 713–715 image formation by spherical mirrors, 719–722 law of reflection, 712 mirror equation and magnification equation,
722–726, 727 multiple reflections, 714–715 parabolic mirrors, 718 polarization, 745–746 problems, 729–732 real images, 714, 716, 720 spherical mirrors, 716, 718–722 total internal reflection, 739–744 virtual images, 714, 721, 724 wave front and rays, 711–712
Refraction of light, 733 angular magnification of magnifying glasses,
761–763 compound microscope, 763 concept focus, 768–769 concept summaries, 767–768 definition of, 733 dispersion of light (prisms and rainbows), 746–748 human eye, 756–761 index of refraction, 733–734 Lens aberrations, 765–766 lens and magnification equations, 752–755 lenses, 748–756 lenses in combination, 755–756 polarization, 745–746 problems, 769–776 Snell’s law, 734–739 telescopes, 764–765 total internal reflection, 739–744
Refractive index, 733 Refractive power, 760 Refrigeration process, 417 Refrigerators, 417–420
concept focus, 427 concept summary, 426 problems, 430
Refueling lost internal energy, 425 Reinertsen, Sarah, 257 Relative biological effectiveness (RBE), 913 Relative humidity, 350 Relative speed, 696 Relative velocity, 68–72
concept focus, 74 concept summary, 73 problems, 77
Relativistic addition of velocities, 824–826 concept focus, 828 concept summary, 827 problems, 829–830
Relativistic momentum, 817–818 concept focus, 828 concept summary, 827 problems, 829
Relativity. See Special relativity Relativity Postulate, 809–811 Remote Control team problem, 488 Remote stereo speakers, 567 Resistance, 553–557
concept focus, 581 concept summary, 580 equivalent resistance, 562–563 internal resistance, 570–571 Ohm’s law, 553–554 problems, 583 RCL circuits, 665–670
I-14 Index
Resistive Heater team problem, 589 Resistivity, 554–557
concept focus, 581 concept summary, 580 problems, 583 temperature coefficient of resistivity, 556
Resistor circuits both series and parallel connections, 569–570 parallel connections, 565–568 series connections, 562–565
Resistor–capacitor (RC) circuits, 577–579 concept focus, 582 concept summary, 581 problems, 587–588
Resistors, 553 four-resistor circuit, 569 parallel wiring, 566 series wiring, 562–563 shunt, 574
Resolving power, 791–796 concept focus, 802 concept summary, 801 problems, 804–805
Resolving vectors into components, 13–15 Resonance, 274–275
concept focus, 282 concept summary, 281
Resonance in RCL circuits, 670–672 concept focus, 679–680 concept summary, 679 problems, 681
Rest energy, 819–820 Resting membrane potential, 541 Restoring force of an ideal spring, 259–260 Resultant vectors, 10 Reversible processes, 414–415, 421 Ride Inside a Tractor Tire team problem, 256 Right triangles, 6, 15, 17
Pythagorean theorem. See Pythagorean theorem Right-hand rule, 214
Right-Hand Rule No. 1 (RHR-1), 593 Right-Hand Rule No. 2 (RHR-2), 605
Rigid objects center of gravity, 231–235, 246–247, 249, 250–251 concept focus, 247 concept summary, 246 forces and torques on, 1–4 in equilibrium, 226–231, 246, 247, 249–251 Newton’s second law for rotation about fixed
axes, 237 problems, 248–249
Rock climbing, 98–99 Roentgen, Wilhelm K., 868 Roller coasters
closed path, 156 nonconservative forces, 161 physics of, 160
Rolling cylinders, 243 Rolling motion, 213–214
concept focus, 216 concept summary, 215 problems, 220
Rollovers, 233–235 Rope
swings, 159 tension, 102
Rosser Reeves ruby, 382 Rotational dynamics
angular momentum, 244–246
center of gravity, 231–235 concept focus, 247 concept summary, 246–247 forces and torques on rigid objects, 223–226 Newton’s law for motion about fixed axes,
236–241 problems, 248–256 rigid objects in equilibrium, 226–231 rotational work and energy, 241–244
Rotational kinematics angular variables and tangential variables, 208–210 angular velocity and angular acceleration, 203–205 centripetal acceleration and tangential acceleration,
210–213 concept focus, 216 concept summaries, 215 equations of, 205–208, 215, 216, 218 problems, 216–222 rolling motion, 213–214 rotational motion and angular displacement,
200–203, 215, 216, 216–218 vector nature of angular variables, 214–215
Rotational kinetic energy, 241–244 concept focus, 248 concept summary, 247 problems, 252–253
Rotational work, 241–244 concept focus, 248 concept summary, 247 problems, 252–253
Rough Measure of Exposure team problem, 935
Rutherford, Ernest, 853 Rutherford scattering, 853–855
concept summary, 878 problems, 880
Rydberg constant, 856
S Safe electrical grounding, 579 Salam, Abdus, 88, 896 Satellite TV, 132 Satellites
elliptical orbits, 245 temperature regulation, 374
Satellites in circular orbits, 130–133 apparent weightlessness and artificial gravity,
133–135 concept focus, 138–139 concept summary, 137–138 problems, 141
Saturated vapor, 350 Saws, torque of electric saw motors, 238 Scaffolds, 110 Scalar quantity, 8 Scalars, 8–18
components, 13 notation, 9 vs. vectors, 9
Scales bathroom scales, 670 body-fat scales, 670
Scanning electron microscope (SEM), 832 Schrödinger, Erwin, 844 Scientific notation, A-1 Scintillation counter, 905 Scuba diving, 385–387 Seatbelts, 110 Second (s), 2
Second law of thermodynamics, 412–413 Carnot’s principle, 414–417 concept summary, 426 entropy, 422 refrigerators, air conditioners, and heat
pumps, 419 Secondary fringes/secondary maxima, 796 Self-inductance, 647
concept focus, 654 concept summary, 652 problems, 658
Self-induction, 647–648 SEM (scanning electron microscope), 832 Semiconductor detectors, 905 Semiconductor devices, 672–678
concept summary, 679 diodes, 673–675 solar cells, 676 transistors, 676–677
Semiconductors forward bias, 674 n-type, 673–674 p-type, 673–674
Series capacitors, 575–577 concept focus, 582 concept summary, 581 problems, 587
Series RCL combination, 666 Series wiring, 562–565, 569–570
concept focus, 582 concept summary, 580–581 problems, 584–586
Setting Safety Parameters team problem, 464 Shaving mirrors, 721 Shear deformation, 277–278 Shear modulus, 277–278 Shell, 866 Shielding electronic circuits, 508–510 Shock absorber, 273 Shunt resistors, 574 SI units, 2 Sidewalk buckling, 332 sigma (Σ), 84 Sign conventions, lenses, 753 Significant figures, A-1 Silicon crystals, p-type semiconductors, 673 Silver surface, photoelectric effect, 835 Simple harmonic motion
acceleration, 264 concept focus, 281–282 concept summaries, 280–281 damped harmonic motion, 273–274 displacement, 261–262 driven harmonic motion and resonance, 274–275 energy, 267–270 frequency of vibration, 264–266 Hooke’s law, 259–260 ideal spring, 257–261 pendulum, 270–273 problems, 282–288 reference circles, 261–266 velocity, 262–263
Simple pendulum, 270–271 Simple Spectrometer team problem, 883–884 Simultaneous equations, A-2 Sine (sin), 6–8 Sines, A-5 Single-slit diffraction, 790 Single slits, waves, 471
Index I-15
Skaters axis of rotation, 201 conservation of linear momentum, 182–183 crack-the-whip, 208–210 rotational kinetic energy, 246 spinning, 244–245
Skiers, 97–98, 150–151 Sledding, 99
bobsled tracks, 127 Sledding Contest problem, 174
Slide projector, 751 Slope, 45
average acceleration, 47 tangent line, 46
Smoke detectors, 893 Smugglers team problem, 256 Snell’s law of refraction, 734–739
apparent depth, 736–737 concept focus, 768 concept summary, 767 derivation of, 738–739 displacement of light by transparent
material, 738 problems, 770–771
Solar cells, 676 Solar eclipse, 202 Solar sails, 841–842 Solenoids, 609 Solids
heat and phase change, 343 specific heat capacity, 340 speed of sound, 445
Solving equations, A-2 Sonar, 444 Sound
application in medicine, 454–455 concept focus, 458 concept summaries, 457 decibels, 448–450 Doppler effect, 450–454 intensity, 446–448 intensity level, 448 lightning and thunder, 444–445 loudness, 442 loudspeaker diaphragm, 263–264, 439–440 nature of, 439–442 pitch, 441 problems, 460–464 reflected, 448 reproduction via electromagnetic
induction, 640–641 sensitivity of human ears, 455–456 sonar, 444 speed of sound, 442–446
Sound barrier, 433 Sound waves, 439–441
beats, 473–474 complex, 481–482 concept focus, 483 concept summaries, 482 diffraction, 470–473 frequency, 440–441 infrasonic, 441 intensity, 446–448 interference, 466–470 longitudinal, 439–440 longitudinal standing waves, 478–480 pressure amplitude, 441–442 problems, 484–488
transverse standing waves, 474–478 tuning forks, 473 ultrasonic, 441
South magnetic pole, 590 Space
astronomical telescopes, 764–765 black holes, 131–132 determining size of stars, 372
Space Shuttle, 177, 326 Space travel and special relativity, 813–814, 826
length contraction, 815–816 Spacecraft. See also Satellites; Satellites in
circular orbits apparent weightlessness and artificial gravity,
133–135 contraction of, 816 Deep Space 1 space probe, 149 displacement, two dimensions, 58 Docking a Spaceship team problem, 199 retrorockets, 38 solar sails, 841–842 Spaceship Malfunction team problem, 199 velocity, two dimensions, 57–59
Speakers loudspeakers. See Loudspeakers stereo speakers, 567
Special relativity concept focus, 827–828 concept summaries, 827 events and inertial reference frames, 808–809 length contraction, 815–817 mass and energy equivalence, 819–824 postulates, 809–811 problems, 828–831 relativistic addition of velocities, 824–826 relativistic momentum, 817–818 time dilation, 811–815
Specific heat capacity, 340–343, 411–412 concept focus, 353 concept summaries, 352, 426 molar, 411 problems, 355–356, 429
Spectra, line, 855–856, 859 Spectrometer team problem, 883–884 Spectrum analyzer, 481 Specular reflection, 712 Speed
average speed, 28–29 average velocity, 29 centripetal force, 125–127 concept summary, 47 dimensional analysis, 5 electromagnetic waves, 686 instantaneous speed, 30 instantaneous velocity, 30 laser beams, 825–826 maximum speed of photoelectrons, 836–837 one-dimensional, 28–30 relative speed, 696 waves, 436–438, 457, 458, 459–460
Speed of light, 691–692 concept summary, 704 in a vacuum, 686 in a vacuum as ultimate speed, 823 problems, 706
Speed-of-Light Postulate, 809–811 Speed of sound, 442–446
concept focus, 458 concept summary, 457
problems, 460–461 sound barrier, 433
Spherical aberration, 765 mirrors, 718
Spherical mirrors, 716, 718–722. See also Mirrors concept focus, 729 concept summary, 728 focal length, 716, 718 focal point, 716 image formation, 719–722 mirror equation and magnification equation,
722–727 mirrors, 719 problems, 730
Sphygmomanometer, 298 Spin quantum number, 863 Spontaneous emission, 872 Spray cans, 348 Spring constant, 258 Spring Gun team problem, 325 Springs. See also Simple harmonic motion
body mass measurement device, 265–266 door-closing unit, 267 elastic deformation, 275–279 Hooke’s law, 259–260, 264, 265, 270–280 ideal spring, 257–261, 280, 281, 282–283 shock absorber, 273
Sprinters, average acceleration, 47 Standard cosmological model, 929–930 The standard model, 927–928 Standard temperature and pressure (STP), 384 Standing waves
longitudinal, 478–480 transverse, 474–478
Star formation, and photoevaporation, 838–839 Stars, determining size, 372 State of a system, thermodynamics, 401 State-of-charge battery indicator, 303 Static friction, 95–101
centripetal force, 126 concept focus, 113 concept summary, 112 problems, 115–116
Static stability factor, 233 Stationary orbits/stationary states, 857 Steady flow, 305–306 Steam burns, 344 Stefan–Boltzmann law of radiation, 372 Step-down transformer, 650 Stimulated emission, 872 Storing Wind Energy team problem, 550 Stoves
electric stove, 556 induction stove, 636–637
STP (standard temperature and pressure), 384 Strain, 279 Strassmann, Fritz, 916 Streamline flow, 306 Streamlines, 306 Stress, 279
thermal, 333–334 Stress and strain
elastic deformation, 275–279, 281, 282, 285–286 Hooke’s law, 279–280, 281, 282, 285–286
Stretching, 275–276 Strings, waves
concept focus, 458 concept summary, 457 problems, 459–460
I-16 Index
Strong nuclear force, 88, 887–888, 925, 927, 929, 930
concept summary, 906 problems, 908
Strontium in bones, 905–906 Stuck on a Ledge team problem, 120 Sublimes, 343 Submerged Machine team problem, 359 Subshell, 866 Subtraction, vectors, 11–12 Sun
absorption lines in spectrum, 861 mass, 821 proton–proton cycle, 921
Sunglasses polarization, 699, 702 Sunlight, average energy density, 693 Super Thruster team problem, 831 Super-Kamiokande neutrino detector, 896–897 Superconductors, 557 Supernovas, 691 Supertankers, 106–107 Surfaces, coefficient of static friction, 97 Surgical implants, 276 Surroundings, thermodynamics, 401 Swimmers, force, 292 Swimming holes, 295 Swimming raft, 302 Symmetry
electric fields, 504 free-falling bodies, 44–45
Synchronous communications satellites, 202 Synchronous satellites. See Satellites; Satellites in
circular orbits Systems, thermodynamics, 401
T Tangent (tan), 6–8
slope, 46 Tangential acceleration, 210–213
concept focus, 216 concept summary, 215 problems, 219
Tangential variables, and angular variables, 208–210 concept focus, 216 concept summary, 215 problems, 219
Tank circuit, 681 Tape recording, 614–615 Tape-deck playback heads, 640–641 Tarpaulins, 311 Telescopes, 764–765
concept focus, 769 concept summary, 768 problems, 774
Television reception, 686, 688 screens, 610–611
Temperature absolute zero point, 329 change, specific heat capacity, 340–343 concept focus, 352 concept summaries, 352 critical temperature, 557 equilibrium between phases of matter, 347–349 humidity, 350–351 inversion layer, 362 linear thermal expansion, 330–337 problems, 353–359 pyroelectric ear thermometer, 690
satellites, 374 single particles, 390–391 standard temperature and pressure (STP), 384 thermometers, 329–330 volume thermal expansion, 337–339 windchill factor, 363
Temperature coefficient of resistivity, 556 Temperature scales, 326–328
Celsius, 326–327 concept summary, 352 conversions, 327–328 Fahrenheit, 326–327 Kelvin, 328–329 problems, 353–354 thermometers, 329–330
TENS (transcutaneous electrical nerve stimulation), 670
Tension force, 101–102 concept focus, 112–113 problems, 116
tera (T), 3 Terminal voltage, 570 Test charges, 500–501 Thermal conductors, 364–365, 369 Thermal equilibrium, 402 Thermal expansion
linear, 330–337 volume, 337–339
Thermal insulators, 364–365, 369 Thermal neutrons, 916 Thermal pollution, 417 Thermal processes, 404–408
adiabatic, 406, 410 concept focus, 427 concept summary, 425–426 isobaric, 405–406, 410 isochoric, 406, 410 isothermal, 406, 410 problems, 428–429 using an ideal gas, 408–411
Thermal stress, 333–334 Thermals, 362 Thermocouple, 329 Thermodynamics, 401
Carnot’s principle/Carnot engine, 414–417
concept focus, 426–427 concept summaries, 425–426 entropy, 420–424 first law, 402–404 heat engines, 413 problems, 427–432 refrigerators, air conditioners, and heat pumps,
417–420 second law, 412–413 specific heat capacities, 411–412 systems and their surroundings, 401–402, 425 thermal processes, 404–408 thermal processes using an ideal gas, 408–411 third law, 425 zeroth law, 402
Thermogram/thermography, 330 Thermometers, 329–330
concept summary, 352 problems, 353–354 pyroelectric ear thermometer, 690
Thermometric property, 329 Thermonuclear reactions, 921 Thermos bottle, 374
theta (θ), 6 Thickness Monitor team problem, 807 Thin-film interference, 782–786
concept focus, 802 concept summary, 801 problems, 803–804
Thin-lens equation, 752–755 concept summary, 767 problems, 772–773
Third law of thermodynamics, 425, 426 Thomson, Joseph J., 853 Three Wheels team problem, 222 Three-beam tracking method, compact discs, 799 Three-way light bulb, 568 Threshold of hearing, 447–449, 455, 482 Throwing stones, projectile motion, 66–67 Thunderstorms, 444–445 Tides, Bay of Fundy, 274–275 Time
atomic clock, 2 equations of kinematics, 34–41 freely falling bodies, 43 second (s), 2
Time dilation, 811–815 concept summary, 827 problems, 828–829 proper time interval, 813 space travel, 813–814 verification of, 814
Tire pressure gauge, 258 Tire-balancing machine, 122 TMS (transcranial magnetic stimulation), 647 Torque, 224
countertorque, and electrical energy generation, 644–645
current-carrying coil, 602–604, 617–618, 621 electric saw motors, 238 rigid objects, 224–226, 246, 247, 248–249
Torricelli’s theorem, 313 Total energy, 819
relation with momentum, 823 Total energy density of electromagnetic waves, 692 Total internal reflection, 739–744
concept focus, 768 concept summary, 767 problems, 771
Total mechanical energy, 157–161 Total solar eclipse, 202 Touch-tone telephone, 440–441 Towing
supertankers, 106–107 trailers, 107
Towing a Detector team problem, 120 Tracking beams, CDs, 799 Traction
foot injuries, 103 tires, 96
Trailers, 87, 107 Trains
conservation of linear momentum, 181–182 magnetically levitated, 615 relative velocity, 68 sound, 451
Trampolines, 154 Transcranial magnetic stimulation (TMS), 647 Transcutaneous electrical nerve stimulation
(TENS), 670 Transformers, 649–651
concept focus, 654
Index I-17
concept summary, 653 problems, 658 Reconfiguring a Transformer team problem, 660
Transistors, 676–677 Translational motion, 224 Transmission axis, 698 Transmutation, 892 Transparent slab, displacement of light by, 738 Transrapid maglev, 615 Transverse standing wave pattern, 474 Transverse standing waves, 474–478
concept focus, 483 concept summary, 482 problems, 486
Transverse waves, 434 guitar strings, 437 speed, 437
Trapeze acts, 130 Triangles, A-5
Pythagorean theorem. See Pythagorean theorem right, 6, 15, 17 slope of tangent line, 46
Trigonometry, 6–8, A-4–A-5 functions, 6–8 problems, 21
Tunable Inclined Plane team problem, 488 Tuning forks, 473 Tuning musical instruments, 474 Turbo-shaft Helicopter team problem, 710 Turbulent flow, 305–306 Turntable, simple harmonic motion,
261–262, 264 Two-dimensional kinematics
equations of kinematics for constant acceleration, 57–59
displacement, velocity, and acceleration, 55–56 projectile motion, 60–67 relative velocity, 68–72
U Ultrasonic imaging, 454–455 Ultrasonic ruler, 443–444 Ultrasonic sound waves, 441 Ultrasound, 454–456 Uncertainty principle, 865–866 Underdamped motion, 274 Underwater Gas Piston team problem, 400 Unidentified Flying Object team problem, 732 Uniform circular motion, 121–122
artificial gravity, 133–135 banked curves, 129 centripetal acceleration, 122–125 centripetal acceleration and tangential acceleration,
210–213 centripetal force, 127–128 concept focus, 138–139 concept summary, 137–138 definition of, 121 equilibrium, 127 problems, 139–143 satellites in circular orbits, 131–133, 137,
138, 141 vertical, 136, 138, 139, 141
Units, 2–6 concept summary, 19 conversion, 3–5 dimensional analysis, 5–6 problems, 21 role in problem solving, 3–6
Universal gas constant, 384 Universal gravitational constant, 89, 91, 130 Unsaturated vapor, 350 Unsteady flow, 305 Uranium isotopes, 917
V Vacuum, speed of light, 686 Van de Graaff generator, 489 Vapor pressure curve, 347 Vaporization curve, 347 Variable force, 166
concept summary, 167 problems, 172
Variables, angular and tangential, 208–210
Vector quantity, 9 Vectors, 8–18
addition, 10–12, 15–18 angular variables, 214–215 components, 12–18 concept summaries, 19–20 multiplication, 11 Newton’s second law of motion, 85–86 notation, 9 problems, 22–26 vs. scalars, 9 subtraction, 11–12 uniform circular motion, 122
Velocity and acceleration, 32–33 angular, 203–205 average speed, 28–29 average velocity, 29, 56 center of mass, 191 concept summary, 47 equations of kinematics, 34–41, 56–60 equilibrium at constant velocity, 105 final, 39–40, 53, 57, 59, 63 freely falling bodies, 42 initial, 53, 57 instantaneous, 30, 56 one-dimensional, 28–34, 45–47 relative, 68–72 relativistic addition of velocities, 824–826 rotational vs. translational, 241 simple harmonic motion and reference circles,
262–263 two-dimensional, 55–56, 62–63, 68–72,
74–75 Velocity selectors, 595–596 Velocity-addition formula, 824 Vertical circular motion, 136–137
concept focus, 139 concept summary, 138 problems, 141
Virtual images diverging lens, 754 mirrors, 714, 721, 724
Viscosity, 306 Viscous flow, 314–317
concept focus, 318 concept summary, 317 problems, 323
Volt, 527 Voltage
measurement of, 574–575 RCL circuits, 668–669 terminal voltage, 570
Voltmeters, 574–575 concept summary, 581 problems, 587
Volume, A-4 Volume deformation and bulk modulus, 278 Volume thermal expansion, 337–339
concept focus, 353 concept summary, 352 problems, 355
W Walking, physics of, 101 Water. See also Fluids
boiling, 344, 348 bursting water pipes, 339 water loss from plant leaves, 394
Water Balloon Battle team problem, 79 Water skiers, 108 Waterfall team problem, 26 Watson, James, 800 Wave fronts, 711–712
concept focus, 728 concept summary, 728
Wave nature of light. See Interference of light waves
Wave–particle duality, 832–833 concept summary, 849
Wavelength, 435–436 electromagnetic waves, 689–691 visible light, 690
Waves AM and FM radio reception, 686, 691 beats, 473–474 blackbody radiation and Planck’s constant,
833–834 concept focus, 457, 483, 849–850 concept summaries, 456–457, 482, 849 de Broglie wavelength and wave nature of matter,
843–845 diffraction, 470–473 guitar strings, 437 Heisenberg uncertainty principle, 845–848 interference of sound waves, 466–470 lightning and thunder, 444–445 linear polarization, 697–698 longitudinal, 434 longitudinal standing waves, 478–480 mathematical description, 439, 457 nature of, 433–435 periodic, 435–436 photon momentum and Compton effect, 840–842 photons and photoelectric effect, 834–839 plane waves, 712 principle of linear superposition, 465–466 problems, 458–464, 484–488, 850–852 radio waves, 436 sound. See Sound waves speed, 436–438 transverse, 434 transverse standing waves, 474–478 wave function of particles, 844 wave–particle duality, 832–833
Weather Monitor team problem, 26 Weight, 90–91
apparent weight, 94–95 definition of, 90 relation between mass and weight, 91
Weight lifting, 146 weight W, 92
I-18 Index
Weightlessness and artificial gravity, 133–135 concept summary, 138 problems, 141
Weinberg, Steven, 88, 896 Wheelchair, 239 Wilson, Robert W., 929 Wind Energy team problem, 550 Wind instruments, 479 Windchill factor, 363 Windshield wipers, 578 Wireless capsule endoscopy, 688 Wireless implantable medical devices, 651–652 Wiring
circuits wired partially in series/partially in parallel, 569–570
concept focus, 582 concept summary, 580–581 parallel wiring, 565–568 problems, 584–586 series wiring, 562–565
Wood-burning stoves, Stefan–Boltzmann law, 372–373 Work
area under a pressure–volume graph, 407 concept focus, 167–168 concept summaries, 166–167 conservation of mechanical energy, 157–161 constant force, 144–147
definition of, 146 electric potential, 525 energy available for doing work, 422 gravitational potential energy, 153–155 kinetic energy and work–energy theorem, 147–153 nonconservative vs. conservative forces, 155–157 nonconservative forces and work–energy theorem,
161–162 power, 162–164 problems, 168–174 rotational vs. translational, 241 rotational work and energy, 241–244, 247,
248, 252–253 variable force, 164–166
Work function, 835 Work–energy theorem, 147–153
concept focus, 167 concept summary, 166 conservation of mechanical energy,
157–161 kinetic energy, 147–153 nonconservative forces, 161–162 problems, 168–169
X X-ray diffraction, 799–800
concept summary, 801
X-rays, 868–872 concept focus, 880 concept summary, 879 electrons, 869 Kα characteristic X-ray for platinum, 870 problems, 882 X-ray tube, 870
Xerography, 513–514
Y Young’s double-slit experiment, 779–782
concept focus, 802 concept summary, 801 electron version, 844 problems, 803
Young’s Modulus, 275–276 Yukawa, Hideki, 925
Z Zeeman effect, 863 Zero, absolute, 328–329, 417, 425 Zeroth law of thermodynamics, 402, 425 Zweig, G., 925
WILEY END USER LICENSE AGREEMENT Go to www.wiley.com/go/eula to access Wiley’s ebook EULA.
- Cover
- Title Page
- Copyright
- About the Authors
- Brief Contents
- Contents
- Acknowledgments
- 1 Introduction and Mathematical Concepts
- 1.1 The Nature of Physics
- 1.2 Units
- 1.3 The Role of Units in Problem Solving
- 1.4 Trigonometry
- 1.5 Scalars and Vectors
- 1.6 Vector Addition and Subtraction
- 1.7 The Components of a Vector
- 1.8 Addition of Vectors by Means of Components
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 2 Kinematics in One Dimension
- 2.1 Displacement
- 2.2 Speed and Velocity
- 2.3 Acceleration
- 2.4 Equations of Kinematics for Constant Acceleration
- 2.5 Applications of the Equations of Kinematics
- 2.6 Freely Falling Bodies
- 2.7 Graphical Analysis of Velocity and Acceleration
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 3 Kinematics in Two Dimensions
- 3.1 Displacement, Velocity, and Acceleration
- 3.2 Equations of Kinematics in Two Dimensions
- 3.3 Projectile Motion
- 3.4 Relative Velocity
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 4 Forces and Newton’s Laws of Motion
- 4.1 The Concepts of Force and Mass
- 4.2 Newton’s First Law of Motion
- 4.3 Newton’s Second Law of Motion
- 4.4 The Vector Nature of Newton’s Second Law of Motion
- 4.5 Newton’s Third Law of Motion
- 4.6 Types of Forces: An Overview
- 4.7 The Gravitational Force
- 4.8 The Normal Force
- 4.9 Static and Kinetic Frictional Forces
- 4.10 The Tension Force
- 4.11 Equilibrium Applications of Newton’s Laws of Motion
- 4.12 Nonequilibrium Applications of Newton’s Laws of Motion
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 5 Dynamics of Uniform Circular Motion
- 5.1 Uniform Circular Motion
- 5.2 Centripetal Acceleration
- 5.3 Centripetal Force
- 5.4 Banked Curves
- 5.5 Satellites in Circular Orbits
- 5.6 Apparent Weightlessness and Artificial Gravity
- 5.7 *Vertical Circular Motion
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 6 Work and Energy
- 6.1 Work Done by a Constant Force
- 6.2 The Work–Energy Theorem and Kinetic Energy
- 6.3 Gravitational Potential Energy
- 6.4 Conservative Versus Nonconservative Forces
- 6.5 The Conservation of Mechanical Energy
- 6.6 Nonconservative Forces and the Work–Energy Theorem
- 6.7 Power
- 6.8 Other Forms of Energy and the Conservation of Energy
- 6.9 Work Done by a Variable Force
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 7 Impulse and Momentum
- 7.1 The Impulse–Momentum Theorem
- 7.2 The Principle of Conservation of Linear Momentum
- 7.3 Collisions in One Dimension
- 7.4 Collisions in Two Dimensions
- 7.5 Center of Mass
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 8 Rotational Kinematics
- 8.1 Rotational Motion and Angular Displacement
- 8.2 Angular Velocity and Angular Acceleration
- 8.3 The Equations of Rotational Kinematics
- 8.4 Angular Variables and Tangential Variables
- 8.5 Centripetal Acceleration and Tangential Acceleration
- 8.6 Rolling Motion
- 8.7 *The Vector Nature of Angular Variables
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 9 Rotational Dynamics
- 9.1 The Action of Forces and Torques on Rigid Objects
- 9.2 Rigid Objects in Equilibrium
- 9.3 Center of Gravity
- 9.4 Newton’s Second Law for Rotational Motion About a Fixed Axis
- 9.5 Rotational Work and Energy
- 9.6 Angular Momentum
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 10 Simple Harmonic Motion and Elasticity
- 10.1 The Ideal Spring and Simple Harmonic Motion
- 10.2 Simple Harmonic Motion and the Reference Circle
- 10.3 Energy and Simple Harmonic Motion
- 10.4 The Pendulum
- 10.5 Damped Harmonic Motion
- 10.6 Driven Harmonic Motion and Resonance
- 10.7 Elastic Deformation
- 10.8 Stress, Strain, and Hooke’s Law
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 11 Fluids
- 11.1 Mass Density
- 11.2 Pressure
- 11.3 Pressure and Depth in a Static Fluid
- 11.4 Pressure Gauges
- 11.5 Pascal’s Principle
- 11.6 Archimedes’ Principle
- 11.7 Fluids in Motion
- 11.8 The Equation of Continuity
- 11.9 Bernoulli’s Equation
- 11.10 Applications of Bernoulli’s Equation
- 11.11 *Viscous Flow
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 12 Temperature and Heat
- 12.1 Common Temperature Scales
- 12.2 The Kelvin Temperature Scale
- 12.3 Thermometers
- 12.4 Linear Thermal Expansion
- 12.5 Volume Thermal Expansion
- 12.6 Heat and Internal Energy
- 12.7 Heat and Temperature Change: Specific Heat Capacity
- 12.8 Heat and Phase Change: Latent Heat
- 12.9 *Equilibrium Between Phases of Matter
- 12.10 *Humidity
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 13 The Transfer of Heat
- 13.1 Convection
- 13.2 Conduction
- 13.3 Radiation
- 13.4 Applications
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 14 The Ideal Gas Law and Kinetic Theory
- 14.1 Molecular Mass, the Mole, and Avogadro’s Number
- 14.2 The Ideal Gas Law
- 14.3 Kinetic Theory of Gases
- 14.4 *Diffusion
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 15 Thermodynamics
- 15.1 Thermodynamic Systems and Their Surroundings
- 15.2 The Zeroth Law of Thermodynamics
- 15.3 The First Law of Thermodynamics
- 15.4 Thermal Processes
- 15.5 Thermal Processes Using an Ideal Gas
- 15.6 Specific Heat Capacities
- 15.7 The Second Law of Thermodynamics
- 15.8 Heat Engines
- 15.9 Carnot’s Principle and the Carnot Engine
- 15.10 Refrigerators, Air Conditioners, and Heat Pumps
- 15.11 Entropy
- 15.12 The Third Law of Thermodynamics
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 16 Waves and Sound
- 16.1 The Nature of Waves
- 16.2 Periodic Waves
- 16.3 The Speed of a Wave on a String
- 16.4 *The Mathematical Description of a Wave
- 16.5 The Nature of Sound
- 16.6 The Speed of Sound
- 16.7 Sound Intensity
- 16.8 Decibels
- 16.9 The Doppler Effect
- 16.10 Applications of Sound in Medicine
- 16.11 *The Sensitivity of the Human Ear
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 17 The Principle of Linear Superposition and Interference Phenomena
- 17.1 The Principle of Linear Superposition
- 17.2 Constructive and Destructive Interference of Sound Waves
- 17.3 Diffraction
- 17.4 Beats
- 17.5 Transverse Standing Waves
- 17.6 Longitudinal Standing Waves
- 17.7 *Complex Sound Waves
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 18 Electric Forces and Electric Fields
- 18.1 The Origin of Electricity
- 18.2 Charged Objects and the Electric Force
- 18.3 Conductors and Insulators
- 18.4 Charging by Contact and by Induction
- 18.5 Coulomb’s Law
- 18.6 The Electric Field
- 18.7 Electric Field Lines
- 18.8 The Electric Field Inside a Conductor: Shielding
- 18.9 Gauss’ Law
- 18.10 *Copiers and Computer Printers
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 19 Electric Potential Energy and the Electric Potential
- 19.1 Potential Energy
- 19.2 The Electric Potential Difference
- 19.3 The Electric Potential Difference Created by Point Charges
- 19.4 Equipotential Surfaces and Their Relation to the Electric Field
- 19.5 Capacitors and Dielectrics
- 19.6 *Biomedical Applications of Electric Potential Differences
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 20 Electric Circuits
- 20.1 Electromotive Force and Current
- 20.2 Ohm’s Law
- 20.3 Resistance and Resistivity
- 20.4 Electric Power
- 20.5 Alternating Current
- 20.6 Series Wiring
- 20.7 Parallel Wiring
- 20.8 Circuits Wired Partially in Series and Partially in Parallel
- 20.9 Internal Resistance
- 20.10 Kirchhoff's Rules
- 20.11 The Measurement of Current and Voltage
- 20.12 Capacitors in Series and in Parallel
- 20.13 RC Circuits
- 20.14 Safety and the Physiological Effects of Current
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 21 Magnetic Forces and Magnetic Fields
- 21.1 Magnetic Fields
- 21.2 The Force That a Magnetic Field Exerts on a Moving Charge
- 21.3 The Motion of a Charged Particle in a Magnetic Field
- 21.4 The Mass Spectrometer
- 21.5 The Force on a Current in a Magnetic Field
- 21.6 The Torque on a Current-Carrying Coil
- 21.7 Magnetic Fields Produced by Currents
- 21.8 Ampère’s Law
- 21.9 Magnetic Materials
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 22 Electromagnetic Induction
- 22.1 Induced Emf and Induced Current
- 22.2 Motional Emf
- 22.3 Magnetic Flux
- 22.4 Faraday’s Law of Electromagnetic Induction
- 22.5 Lenz’s Law
- 22.6 *Applications of Electromagnetic Induction to the Reproduction of Sound
- 22.7 The Electric Generator
- 22.8 Mutual Inductance and Self-Inductance
- 22.9 Transformers
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 23 Alternating Current Circuits
- 23.1 Capacitors and Capacitive Reactance
- 23.2 Inductors and Inductive Reactance
- 23.3 Circuits Containing Resistance, Capacitance, and Inductance
- 23.4 Resonance in Electric Circuits
- 23.5 Semiconductor Devices
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 24 Electromagnetic Waves
- 24.1 The Nature of Electromagnetic Waves
- 24.2 The Electromagnetic Spectrum
- 24.3 The Speed of Light
- 24.4 The Energy Carried by Electromagnetic Waves
- 24.5 The Doppler Effect and Electromagnetic Waves
- 24.6 Polarization
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 25 The Reflection of Light: Mirrors
- 25.1 Wave Fronts and Rays
- 25.2 The Reflection of Light
- 25.3 The Formation of Images by a Plane Mirror
- 25.4 Spherical Mirrors
- 25.5 The Formation of Images by Spherical Mirrors
- 25.6 The Mirror Equation and the Magnification Equation
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 26 The Refraction of Light: Lenses and Optical Instruments
- 26.1 The Index of Refraction
- 26.2 Snell’s Law and the Refraction of Light
- 26.3 Total Internal Reflection
- 26.4 Polarization and the Reflection and Refraction of Light
- 26.5 The Dispersion of Light: Prisms and Rainbows
- 26.6 Lenses
- 26.7 The Formation of Images by Lenses
- 26.8 The Thin-Lens Equation and the Magnification Equation
- 26.9 Lenses in Combination
- 26.10 The Human Eye
- 26.11 Angular Magnification and the Magnifying Glass
- 26.12 The Compound Microscope
- 26.13 The Telescope
- 26.14 Lens Aberrations
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 27 Interference and the Wave Nature of Light
- 27.1 The Principle of Linear Superposition
- 27.2 Young’s Double-Slit Experiment
- 27.3 Thin-Film Interference
- 27.4 The Michelson Interferometer
- 27.5 Diffraction
- 27.6 Resolving Power
- 27.7 The Diffraction Grating
- 27.8 *Compact Discs, Digital Video Discs, and the Use of Interference
- 27.9 X-Ray Diffraction
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 28 Special Relativity
- 28.1 Events and Inertial Reference Frames
- 28.2 The Postulates of Special Relativity
- 28.3 The Relativity of Time: Time Dilation
- 28.4 The Relativity of Length: Length Contraction
- 28.5 Relativistic Momentum
- 28.6 The Equivalence of Mass and Energy
- 28.7 The Relativistic Addition of Velocities
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 29 Particles and Waves
- 29.1 The Wave–Particle Duality
- 29.2 Blackbody Radiation and Planck’s Constant
- 29.3 Photons and the Photoelectric Effect
- 29.4 The Momentum of a Photon and the Compton Effect
- 29.5 The De Broglie Wavelength and the Wave Nature of Matter
- 29.6 The Heisenberg Uncertainty Principle
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 30 The Nature of the Atom
- 30.1 Rutherford Scattering and the Nuclear Atom
- 30.2 Line Spectra
- 30.3 The Bohr Model of the Hydrogen Atom
- 30.4 De Broglie’s Explanation of Bohr’s Assumption About Angular Momentum
- 30.5 The Quantum Mechanical Picture of the Hydrogen Atom
- 30.6 The Pauli Exclusion Principle and the Periodic Table of the Elements
- 30.7 X-Rays
- 30.8 The Laser
- 30.9 *Medical Applications of the Laser
- 30.10 *Holography
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 31 Nuclear Physics and Radioactivity
- 31.1 Nuclear Structure
- 31.2 The Strong Nuclear Force and the Stability of the Nucleus
- 31.3 The Mass Defect of the Nucleus and Nuclear Binding Energy
- 31.4 Radioactivity
- 31.5 The Neutrino
- 31.6 Radioactive Decay and Activity
- 31.7 Radioactive Dating
- 31.8 Radioactive Decay Series
- 31.9 Radiation Detectors
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- 32 Ionizing Radiation, Nuclear Energy, and Elementary Particles
- 32.1 Biological Effects of Ionizing Radiation
- 32.2 Induced Nuclear Reactions
- 32.3 Nuclear Fission
- 32.4 Nuclear Reactors
- 32.5 Nuclear Fusion
- 32.6 Elementary Particles
- 32.7 Cosmology
- Concept Summary
- Focus on Concepts
- Problems
- Additional Problems
- Concepts and Calculations Problems
- Team Problems
- Appendixes
- APPENDIX A Powers of Ten and Scientific Notation
- APPENDIX B Significant Figures
- APPENDIX C Algebra
- APPENDIX D Exponents and Logarithms
- APPENDIX E Geometry and Trigonometry
- APPENDIX F Selected Isotopes
- ANSWERS TO CHECK YOUR UNDERSTANDING
- ANSWERS TO ODD-NUMBERED PROBLEMS
- INDEX
- EULA
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- 2018-03-24T01:06:37+0000
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