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246                       Chapter 6  Review of Complex and Principal States of Stress and Strain


                                                3
                                        (a)                             3
                                                σ 3                  45°     (c)


                                                                  σ τ2
                                                             2
                                                        σ
                        3                                2                           2
                    45°                                                τ 2      σ
              (b)                           σ 1                                  2
              σ                 σ
               τ1
                        τ       τ1     1
                         1
                                                3                1   σ τ2
                                              σ      (d)
                                   2          3
                    σ 1



               1                    σ τ3      τ 3          45°  2
                                                   σ τ3

                                         1

            Figure 6.8 Principal normal stresses and principal axes (a), and principal shear stresses (b), (c),
            (d). In (b), rotation of the unit cube 45 about the axis of σ 1 gives the planes where τ 1 acts.
                                            ◦
            Similar rotation about σ 2 gives the τ 2 planes (c), and about σ 3 the τ 3 planes (d).




            6.3.1 Principal Shear Stresses and Maximum Shear Stress
            In Fig. 6.8(a), if the equivalent state of stress is found for a 45 rotation about any of the 1, 2, or 3
                                                              ◦
            axes, a shear stress is encountered that is the largest for any rotation about that axis. The three shear
            stresses that result are called the principal shear stresses, τ 1 , τ 2 , and τ 3 . These are each accompanied
            by normal stresses that are the same on the two shear planes, σ τ1 , σ τ2 , and σ τ3 , respectively. For
            the planes containing each pair of principal axes, 1-2, 2-3, and 3-1, we have a state of generalized
                                                                     ◦
            plane stress, so that relationships similar to Eq. 6.12 apply for each 45 rotation. Hence, the three
            principal shear stresses and the accompanying normal stresses are given by



                                 |σ 2 − σ 3 |     |σ 1 − σ 3 |     |σ 1 − σ 2 |
                            τ 1 =       ,    τ 2 =       ,    τ 3 =                   (6.18)
                                    2                2                2
                                  σ 2 + σ 3        σ 1 + σ 3        σ 1 + σ 2
                            σ τ1 =      ,    σ τ2 =       ,    σ τ3 =                 (6.19)
                                     2                2                2
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