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Section 7.8  Modified Mohr Fracture Criterion                               315


             Example 7.8
             A gray cast iron has a tensile strength of 214 MPa and a compressive strength of 770 MPa, where
             these values are averages from three tests of each type on a single batch of material. Also, in the
             compression tests, the fracture was observed to occur on a plane inclined to the direction of
                                            ◦
             loading by an angle averaging θ c = 37 .
                 (a) Assuming that the modified Mohr criterion applies, calculate m and σ i values for this
                    material.
                 (b) If a shaft of diameter 30 mm of this material is subjected to a torque of 500 N·m,
                    estimate the safety factor against fracture.
                 (c) What is the safety factor against fracture if a 100 kN compressive force is applied to the
                    shaft in addition to the torque?

                                                               ◦
             Solution  (a) The value of m can be obtained from θ c = 37 and Eqs. 7.43 and 7.47.
                                      ◦
                                                 ◦
                                φ = 90 − 2θ c = 16 ,  m = sin φ = 0.2756              Ans.

              To calculate σ i ,use σ uc = σ uc =−770 MPa, as well as σ ut = 214 MPa, with m in Eq. 7.62.
                                                  1 + m

                                   σ i =−|σ |+ σ ut     =−393.1MPa                    Ans.
                                          uc
                                                  1 − m
                 (b) The shear stress at the shaft surface due to a torque T is obtained from the shaft radius
             of r = 15 mm and expressions from Appendix A:

                                               Tr         πr 4
                                         τ xy =  ,    J =
                                               J           2
                                      2T    2(500,000 N·mm)
                                τ xy =    =                 = 94.31 MPa
                                      πr 3     π(15 mm) 3

             Noting that there is a state of plane stress with this τ xy and σ x = σ y = 0, the in-plane principal
             normal stresses from Eq. 6.7 are


                                                     2

                                 σ x + σ y   σ x − σ y
                                                          2
                         σ 1 ,σ 2 =     ±              + τ xy  = 94.31, −94.31 MPa
                                    2           2
             The third principal normal stress is σ 3 = 0.
                 We now have all of the quantities needed to obtain C 12 , C 23 , and C 31 from Eq. 7.58:
                             C 12 = 260.4,  C 23 = 94.31,  C 31 = 166.09 MPa

             These, along with the principal normal stresses, σ 1 , σ 2 , and σ 3 give the effective stresses and
             safety factors for the C–M and maximum normal stress components of the M-M failure criterion.
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