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                                                                                     Failures Resulting from Static Loading  257
                                       5–3     Repeat Prob. 5–1 for a bar of AISI 1030 hot-rolled steel and:
                                               (a) σ x = 25 kpsi, σ y = 15 kpsi
                                               (b) σ x = 15 kpsi, σ y =−15 kpsi
                                               (c) σ x = 20 kpsi, τ xy =−10 kpsi
                                               (d) σ x =−12 kpsi,σ y = 15 kpsi, τ xy =−9 kpsi
                                               (e) σ x =−24 kpsi, σ y =−24 kpsi,τ xy =−15 kpsi
                                       5–4     Repeat Prob. 5–1 for a bar of AISI 1015 cold-drawn steel with the following principal stresses
                                               obtained from Eq. (3–13):
                                               (a) σ A = 30 kpsi, σ B = 30 kpsi
                                               (b) σ A = 30 kpsi, σ B =−30 kpsi
                                               (c) σ A = 30 kpsi, σ B = 15 kpsi
                                               (d) σ A =−30 kpsi, σ B =−15 kpsi
                                               (e) σ A =−50 kpsi, σ B = 10 kpsi
                                       5–5     Repeat Prob. 5–1 by first plotting the failure loci in the σ A ,σ B plane to scale; then, for each stress
                                               state, plot the load line and by graphical measurement estimate the factors of safety.
                                       5–6     Repeat Prob. 5–3 by first plotting the failure loci in the σ A ,σ B plane to scale; then, for each stress
                                               state, plot the load line and by graphical measurement estimate the factors of safety.
                                    5–7 to     An AISI 1018 steel has a yield strength, S y = 295 MPa. Using the distortion-energy theory for
                                      5–11     the given state of plane stress, (a) determine the factor of safety, (b) plot the failure locus, the load
                                               line, and estimate the factor of safety by graphical measurement.


                                                Problem Number        S x (MPa)     S y (MPa)     T xy (MPa)
                                                      5–7                 75           −35             0
                                                      5–8               −100            30             0
                                                      5–9                 100            0           −25
                                                      5–10               −30           −65            40
                                                      5–11               −80            30           −10


                                      5–12     A ductile material has the properties S yt = 60 kpsi and S yc = 75 kpsi. Using the ductile Coulomb-
                                               Mohr theory, determine the factor of safety for the states of plane stress given in Prob. 5–3.
                                      5–13     Repeat Prob. 5–12 by first plotting the failure loci in the σ A , σ B plane to scale; then for each stress
                                               state, plot the load line and by graphical measurement estimate the factor of safety.
                                   5–14 to     An AISI 4142 steel Q&T at 800°F exhibits S yt = 235 kpsi, S yc = 285 kpsi, and ε f = 0.07. For
                                      5–18     the given state of plane stress, (a) determine the factor of safety, (b) plot the failure locus and the
                                               load line, and estimate the factor of safety by graphical measurement.


                                                Problem Number        S x (kpsi)    S y (kpsi)    T xy (kpsi)
                                                      5–14                150          −50             0
                                                      5–15              −150            50             0
                                                      5–16                125            0           −75
                                                      5–17               −80          −125            50
                                                      5–18                125           80           −75
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