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                 68   Mechanical Engineering Design
                                          Using the tabulated values of G and E in Table A–5, calculate Poisson’s ratio for steel, aluminum,
                                          beryllium copper, and gray cast iron. Determine the percent difference between the calculated
                                          values and the values tabulated in Table A–5.
                                   2–6    A specimen of steel having an initial diameter of 0.503 in was tested in tension using a gauge
                                          length of 2 in. The following data were obtained for the elastic and plastic states:


                                                 Elastic State              Plastic State
                                           Load P      Elongation       Load P      Area A i
                                             lbf           in             lbf         in 2
                                             1 000        0.0004          8 800      0.1984
                                             2 000        0.0006          9 200      0.1978
                                             3 000        0.0010          9 100      0.1963
                                             4 000        0.0013         13 200      0.1924
                                             7 000        0.0023         15 200      0.1875
                                             8 400        0.0028         17 000      0.1563
                                             8 800        0.0036         16 400      0.1307
                                             9 200        0.0089         14 800      0.1077


                                          Note that there is some overlap in the data.
                                          (a) Plot the engineering or nominal stress-strain diagram using two scales for the unit strain  ,
                                             one scale from zero to about 0.02 in/in and the other scale from zero to maximum strain.
                                          (b) From this diagram find the modulus of elasticity, the 0.2 percent offset yield strength, the ulti-
                                             mate strength, and the percent reduction in area.
                                          (c) Characterize the material as ductile or brittle. Explain your reasoning.
                                          (d) Identify a material specification from Table A–20 that has a reasonable match to the data.
                                   2–7    Compute the true stress and the logarithmic strain using the data of Prob. 2–6 and plot the results on
                                          log-log paper. Then find the plastic strength coefficient σ 0 and the strain-strengthening exponent m.
                                          Find also the yield strength and the ultimate strength after the specimen has had 20 percent cold work.
                                   2–8    The stress-strain data from a tensile test on a cast-iron specimen are
                                             Engineering
                                              stress, kpsi  5    10    16    19   26    32   40   46   49   54
                                           Engineering strain,  0.20  0.44  0.80  1.0  1.5  2.0  2.8  3.4  4.0  5.0
                                                 10  3  in/in
                                          Plot the stress-strain locus and find the 0.1 percent offset yield strength, and the tangent modulus
                                          of elasticity at zero stress and at 20 kpsi.
                                   2–9    A part made from annealed AISI 1018 steel undergoes a 20 percent cold-work operation.
                                          (a) Obtain the yield strength and ultimate strength before and after the cold-work operation.
                                             Determine the percent increase in each strength.
                                          (b) Determine the ratios of ultimate strength to yield strength before and after the cold-work
                                             operation. What does the result indicate about the change of ductility of the part?
                                 2–10     Repeat Prob. 2–9 for a part made from hot-rolled AISI 1212 steel.
                                 2–11     Repeat Prob. 2–9 for a part made from 2024-T4 aluminum alloy.
                                 2–12     A steel member has a Brinell of H B = 275. Estimate the ultimate strength of the steel in MPa.
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