Physics Lab report

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Physics 201 Fundamentals of Physics I Lab

FALL 2016

Name:

W # :

Section: Time: Date:

Lab partner:

Lab 3

I

Vector Addition

Purpose:

Procedure:

Data

Force #

m (g)

Magnitude of the force F (N)

Direction in o

1

70

0.686

0

2

50

0.49

140

3

65

0.637

70

Resultant Force FR

185

1.813

240

Analysis and discussion:

Finding the Resultant force FR =F1 + F2 + F3

i) Experimental

ii) Analytical or algebraic (analyze to components)

iii) Graphical

Conclusion

II

Projectile Motion

Parabolic Flight Path

Purpose:

Introduction:

Procedure:

Data

Calibrating the launcher (3rd notch)

t1

(s)

t2

(s)

t3

(s)

tavg

(s)

v0 = 1.5 / tavg (cm/s)

0.0025

0.0016

0.0016

θ0 = 30

y0 = (m)

x (m)

y1

(cm)

y2

(cm)

y3

(cm)

yavg

(m)

1.0

60

70

76

2.0

118

119

126

3.0

131

139

144

4.0

143

140

148

5.0

98

94

95

6.0

60

70

74

7

3

1

15

· Use Excel (or any other package of your choice) to plot x vs. y and fit the data points to a polynomial of order 2. Compare the coefficients obtained from fitting equation to their real values predicted by the path equation:

image1.wmf

2

00

22

0

0

(tan) ()

2 cos

g

yyxx

v

q

q

-

=++

· Test your understanding of the projectile motion equations:

Predicting the flight time parameters, path equation, etc, can you hit the monkey on the pendulum in the lab from a distance of around 3 meters? Set the pendulum in motion with reasonable amplitude.

· Measure the maximum height and compare to theory

image2.wmf

2

00

max

sin)

(

2

v

Hy

g

q

==

Data analysis:

Conclusion

III

Projectile Motion

Range Equation

Purpose:

Introduction:

Procedure:

Data

Calibrating the launcher; chose a suitable notch for this experiment

Notch number:

t1

(s)

t2

(s)

t3

(s)

tavg

(s)

v0 = 1.5 / tavg

(cm/s)

0.0039

0.0043

0.0040

θo

R1

(cm)

R2

(cm)

R3

(cm)

Ravg

(m)

sin(2θ)

10.0

91

92.5

94

20.0

122

166

119.5

30.0

154.5

153

147

45.0

179

179.5

178

55.0

172.5

173.5

176

The horizontal range equation is given by:

image3.wmf

2

0

0

)

() sin(2

v

g

R

q

=

In the current form, the relation between the range R along x and the angle of launch θ0 is not linear. However, we can linearize this relation by plotting R vs sin(2θ0), in other words, if you call y = R and x = sin(2θ0), the range equation adopts a straight line equation of the form y = a.x.

Use Excel (or any other package of your choice) to plot sin(2θ) vs. R and fit the data points to a straight line. Compare the slope obtained from fitted results to its real value predicted by the range equation

Data analysis:

Conclusion

Engineering/Physics Department

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