Solution to Problem 204 Stress-strain Diagram
Problem 204
The following data were obtained during a tension test of an aluminum alloy. The initial diameter of the test specimen was 0.505 in. and the gage length was 2.0 in.
Load (lb) | Elongation (in.) | Load (lb) | Elongation (in.) |
0 | 0 | 14 000 | 0.020 |
2 310 | 0.00220 | 14 400 | 0.025 |
4 640 | 0.00440 | 14 500 | 0.060 |
6 950 | 0.00660 | 14 600 | 0.080 |
9 290 | 0.00880 | 14 800 | 0.100 |
11 600 | 0.0110 | 14 600 | 0.120 |
12 600 | 0.0150 | 13 600 | Fracture |
Plot the stress-strain diagram and determine the following mechanical properties: (a) proportional limit; (b) modulus of elasticity; (c) yield point; (d) yield strength at 0.2% offset; (e) ultimate strength; and (f) rupture strength.
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