The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of test specimen was 0.505 inch and gauge length was 2.0 inch. Plot the stress strain diagram and determine (a) Proportional Limit (b) Modulus of Elasticity (c) Yield Stress at 0.2% offset (d) Ultimate Stress and (e) Nominal Rupture Stress. Load (Ib) Elongation (in.) Load (Ib) Elongation (in.) 14 000 0.020 2310 0.0022 14 400 0.025 4 640 0.0044 14 500 0.060 6950 0.0066 14 600 0.080 9 290 0.0088 14 800 0.100 11 600 0.0110 14 600 0.120 13 000 0.0150 13 600 Fracture
The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of test specimen was 0.505 inch and gauge length was 2.0 inch. Plot the stress strain diagram and determine (a) Proportional Limit (b) Modulus of Elasticity (c) Yield Stress at 0.2% offset (d) Ultimate Stress and (e) Nominal Rupture Stress. Load (Ib) Elongation (in.) Load (Ib) Elongation (in.) 14 000 0.020 2310 0.0022 14 400 0.025 4 640 0.0044 14 500 0.060 6950 0.0066 14 600 0.080 9 290 0.0088 14 800 0.100 11 600 0.0110 14 600 0.120 13 000 0.0150 13 600 Fracture
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of test
specimen was 0.505 inch and gauge length was 2.0 inch. Plot the stress strain diagram and determine
(a) Proportional Limit (b) Modulus of Elasticity (c) Yield Stress at 0.2% offset (d) Ultimate Stress and
(e) Nominal Rupture Stress.
Transcribed Image Text:The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of test
specimen was 0.505 inch and gauge length was 2.0 inch. Plot the stress strain diagram and determine
(a) Proportional Limit (b) Modulus of Elasticity (c) Yield Stress at 0.2% offset (d) Ultimate Stress and
(e) Nominal Rupture Stress.
Load (Ib)
Elongation (in.)
Load (Ib)
Elongation (in.)
14 000
0.020
2310
0.0022
14 400
0.025
4 640
0.0044
14 500
0.060
6950
0.0066
14 600
0.080
9 290
0.0088
14 800
0.100
11 600
0.0110
14 600
0.120
13 000
0.0150
13 600
Fracture
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