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Chapter 4, Problem 4.7QP

An aluminum alloy bar with a rectangular cross section that has a width of 12.5 mm, thickness of 6.25 mm, and a gauge length of 50 mm was tested in tension to fracture according to ASTM E-8 method. The load and deformation data were as shown in Table P4.7. Using a spreadsheet program, obtain the following:

a. A plot of the stress–strain relationship. Label the axes and show units.

b. A plot of the linear portion of the stress–strain relationship. Determine the modulus of elasticity using the best fit approach.

c. Proportional limit.

d. Yield stress at an offset strain of 0.002 m/m.

e. Tangent modulus at a stress of 450 MPa.

f. Secant modulus at a stress of 450 MPa.

TABLE P4.7

Load (kN) L (mm) Load (kN) L (mm)
0 0 33.5 1.486
3.3 0.025 35.3 2.189
14.0 0.115 37.8 3.390
25.0 0.220 39.8 4.829
29.0 0.406 40.8 5.961
30.6 0.705 41.6 7.386
31.7 0.981 41.2 8.047
32.7 1.245    
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A cylindrical specimen of aluminum alloy having a diameter of 12.8 mm and a gauge length (lo) of 50.800 mm is pulled in tension. Use the load–elongation characteristics shown in the following table and answer the following questions. (10p) i- Convert the data as engineering stress (σ) versus engineering strain (ε). ii- Compute the modulus of elasticity (E) (with a precision of ±5000 MPa) iii- Determine the yield strength at a strain offset of 0.002 (σy) (with a precision of ±20 MPa) iv- Determine the tensile strength (TS) of this alloy.
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