write mechanics of material lab (Torsion Tests of Metal specimens lab & Concrete lab)
UNIVERSITY OF NEW ORLEANS
MECHANICS OF MATERIALS LAB
LAB REPORT
Torsion Test
Objective:
The objective of this lab was to determine and draw the torsion vs. angle of twist and shear stress vs. shear-strain diagrams for steel and aluminum specimens tested. Also, to calculate the shear modulus for the steel and aluminum specimens.
Equipment:
Tinius Olsen Torsion tester
Steel rod specimen
Aluminum rod specimen
Ruler
Micrometer
Theory:
Where:
= the shear stress (psi)
T = torsion (in-lb)
= distance from axis of shaft to
where the stress is acting (in)
J = polar moment of inertia with
respect to the longitudinal axis (in4)
Where:
= shear strain (rad)
= distance from axis of shaft to
where the stress is acting (in)
L = length of the metal specimen (in)
= angle of twist (rad)
Where:
G = modulus of rigidity (psi)
L = length of the metal specimen (in)
= angle of twist (radians)
T = torsion (in-lb)
J = polar moment of inertia with
respect to the longitudinal axis (in4)
= maximum shear strain (radians)
= the shear stress (psi)
Procedure:
Place the rod in the Tinius Olsen Torsion Tester and secure each end in machine. Start applying twisting load on the specimen. Record the torque (in-lb.) on the specimen at various points during the experiment according to how many degrees the specimen has been twisted. Repeat this process for each specimen.
Data:
|
Steel |
||||
|
Line |
φ (degees) |
T (in-lb) |
τ (psi) |
γ (radians) |
|
1 |
0 |
0 |
0.000 |
0.0000 |
|
2 |
1 |
60 |
596.831 |
0.0012 |
|
3 |
2 |
250 |
2486.796 |
0.0023 |
|
4 |
3 |
610 |
6067.782 |
0.0035 |
|
5 |
4 |
770 |
7659.332 |
0.0047 |
|
6 |
5 |
770 |
7659.332 |
0.0058 |
|
7 |
6 |
880 |
8753.522 |
0.0070 |
|
8 |
8 |
1110 |
11041.374 |
0.0093 |
|
9 |
10 |
1390 |
13826.586 |
0.0116 |
|
10 |
12 |
1780 |
17705.987 |
0.0140 |
|
11 |
15 |
2270 |
22580.108 |
0.0175 |
|
12 |
20 |
2930 |
29145.249 |
0.0233 |
|
13 |
30 |
3000 |
29841.552 |
0.0349 |
|
14 |
45 |
3030 |
30139.967 |
0.0524 |
|
15 |
60 |
3230 |
32129.404 |
0.0698 |
|
16 |
90 |
3700 |
36804.581 |
0.1047 |
|
17 |
120 |
4050 |
40286.095 |
0.1396 |
|
18 |
180 |
4550 |
45259.687 |
0.2094 |
|
19 |
270 |
5030 |
50034.335 |
0.3142 |
|
20 |
360 |
5340 |
53117.962 |
0.4189 |
|
21 |
450 |
5550 |
55206.871 |
0.5236 |
|
22 |
540 |
5720 |
56897.892 |
0.6283 |
|
23 |
630 |
5870 |
58389.970 |
0.7330 |
|
24 |
720 |
5970 |
59384.688 |
0.8378 |
|
Max |
800 |
6120 |
60876.766 |
0.9308 |
|
Aluminum |
||||
|
Line |
φ (degees) |
T (in-lb) |
τ (psi) |
γ (radians) |
|
1 |
0 |
0 |
0.000 |
0.000 |
|
2 |
1 |
150 |
1492.078 |
0.001 |
|
3 |
2 |
350 |
3481.514 |
0.002 |
|
4 |
3 |
530 |
5272.007 |
0.003 |
|
5 |
4 |
720 |
7161.972 |
0.005 |
|
6 |
5 |
890 |
8852.994 |
0.006 |
|
7 |
6 |
1070 |
10643.487 |
0.007 |
|
8 |
8 |
1400 |
13926.058 |
0.009 |
|
9 |
10 |
1740 |
17308.100 |
0.012 |
|
10 |
12 |
2020 |
20093.312 |
0.014 |
|
11 |
15 |
2250 |
22381.164 |
0.017 |
|
12 |
20 |
2390 |
23773.770 |
0.023 |
|
13 |
30 |
2490 |
24768.488 |
0.035 |
|
14 |
45 |
2570 |
25564.263 |
0.052 |
|
15 |
60 |
2630 |
26161.094 |
0.070 |
|
16 |
90 |
2730 |
27155.812 |
0.105 |
|
17 |
120 |
2790 |
27752.643 |
0.140 |
|
18 |
180 |
2860 |
28448.946 |
0.209 |
|
19 |
270 |
2890 |
28747.362 |
0.314 |
|
20 |
360 |
2900 |
28846.83344 |
0.419 |
|
21 |
450 |
2910 |
28946.30527 |
0.524 |
|
22 |
540 |
2920 |
29045.77711 |
0.628 |
|
23 |
630 |
2930 |
29145.24895 |
0.733 |
|
24 |
720 |
2950 |
29344.19263 |
0.838 |
|
25 |
900 |
2960 |
29443.66447 |
1.047 |
|
26 |
1080 |
2980 |
29642.60815 |
1.257 |
|
27 |
1170 |
3000 |
29841.55183 |
1.361 |
|
28 |
1260 |
3010 |
29941.02367 |
1.466 |
|
Max |
1335 |
30020 |
298614.462 |
1.553 |
Discussion and Conclusion
After conducting the torsion test for both the aluminum and the steel specimens, the values for the modulus of rigidity for each specimen was found to be for the aluminum and for the steel specimen. These results are conflicting with the standard modulus of rigidity for aluminum and steel (based on the table of typical properties of materials used in engineering found in Appendix B of the book used in Mechanics of Materials course) being 11.2 x 106 psi for steel and 4 x 106 psi for aluminum. We also noticed that there was a slippage while twisting the steel specimen at the angles 4 and 5 because we got the same T value for both. These results could be fixed by making sure that the torsion tester machine is perfectly calibrated and that the manual rotation of the machine is being done accurately.
Steel calculation:
Then do the same process for Aluminum.
Torsion vs Angle of Twist (Aluminum)
0.0 1.0 2.0 3.0 4.0 5.0 6.0 8.0 10.0 12.0 15.0 20.0 30.0 45.0 60.0 90.0 120.0 180.0 270.0 0.0 150.0 350.0 530.0 720.0 890.0 1070.0 1400.0 1740.0 2020.0 2250.0 2390.0 2490.0 2570.0 2630.0 2730.0 2790.0 2860.0 2890.0Angle of twist (degrees)
Torsion (in-lb)
Shear Stress vs. Shear Strain (Aluminum)
0.0 0.00116355283466289 0.00232710566932577 0.00349065850398866 0.00465421133865154 0.00581776417331443 0.00698131700797732 0.00930842267730309 0.0116355283466289 0.0139626340159546 0.0174532925199433 0.0232710566932577 0.0349065850398866 0.0523598775598299 0.0698131700797732 0.10471975511966 0.139626340159546 0.20943951023932 0.314159265358979 0.0 1492.077591486518 3481.51438013521 5272.007489919029 7161.972439135286 8852.993709486675 10643.4868192705 13926.05752054083 17308.10006124361 20093.31156535175 22381.16387229777 23773.76962435185 24768.4880186762 25564.26273413567 26161.09377073028 27155.81216505463 27752.64320164924 28448.94607767628 28747.36159597358Shear Strain (rad)
Shear Stress (psi)
Torsion vs Angle of Twist (Steel)
0.0 1.0 2.0 3.0 4.0 5.0 6.0 8.0 10.0 12.0 15.0 20.0 30.0 45.0 60.0 90.0 120.0 180.0 270.0 360.0 450.0 540.0 630.0 720.0 800.0 0.0 60.0 250.0 610.0 770.0 770.0 880.0 1110.0 1390.0 1780.0 2270.0 2930.0 3000.0 3030.0 3230.0 3700.0 4050.0 4550.0 5030.0 5340.0 5550.0 5720.0 5870.0 5970.0 6120.0Angle of twist (degrees)
Torsion (in-lb)
Shear Stress vs. Shear Strain (Steel)
0.0 0.00116355283466289 0.00232710566932577 0.00349065850398866 0.00465421133865154 0.00581776417331443 0.00698131700797732 0.00930842267730309 0.0116355283466289 0.0139626340159546 0.0174532925199433 0.0232710566932577 0.0349065850398866 0.0523598775598299 0.0698131700797732 0.10471975511966 0.139626340159546 0.20943951023932 0.314159265358979 0.418879020478639 0.523598775598299 0.628318530717959 0.733038285837618 0.837758040957278 0.930842267730309 0.0 596.8310365946072 2486.795985810863 6067.782205378506 7659.33163629746 7659.33163629746 8753.52187005424 11041.37417700023 13826.5856811084 17705.98741897335 22580.10755116264 29145.24895370332 29841.55182973036 30139.96734802767 32129.40413667636 36804.58059000077 40286.09497013599 45259.68694175772 50034.33523451457 53117.96225692004 55206.87088500117 56897.89215535255 58389.96974683907 59384.68814116342 60876.76573264992Shear Strain (rad)
Shear Stress (psi)