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Section 6.3  Principal Stresses and the Maximum Shear Stress               245

                           y
                              σ
                               y                                          σ
                   (a)                                     (b)             y
                                                                              τ
                                  τ xy                                         xy
                                                    y
                                        σ
                                         x                                         σ x
                         σ                x        z      x             σ z
                          z
                  z


                                        (c)
                                                   θ
                                                     τ            y '  y
                                          σ               σ
                                           x                               x '
                                                                   θ
                                                    σ z                    x
                                                                     z
                                              τ
                                               xy
                                                   σ
                                                    y

             Figure 6.7 State of generalized plane stress where two components of shear stress are zero.

            with τ yz = τ zx = 0, we obtain σ 1 and σ 2 from Eq. 6.7 or from Mohr’s circle, and the third principal
            normal stress turns out to be σ 3 = σ z . Also, since ordinary plane stress is simply a special case
            of generalized plane stress where σ z = 0, the third principal normal stress in this case is simply
            σ 3 = σ z = 0.


            6.3 PRINCIPAL STRESSES AND THE MAXIMUM SHEAR STRESS

            Consider any state of stress on an x-y-z coordinate system, as in Fig. 6.1. There is, in all cases,
            an equivalent representation on a new coordinate system of principal axes, 1-2-3, where no shear
            stresses are present, as illustrated by Fig. 6.8(a). The three normal stresses for the 1-2-3 coordinate
            system are principal normal stresses, σ 1 , σ 2 , and σ 3 . Of these, one is the maximum normal stress
            acting on any plane, another is the minimum normal stress acting on any plane, and the remaining
            one has an intermediate value.
               For x-y plane stress or generalized plane stress, the values of σ 1 and σ 2 and their directions
            may be found, as described in the previous section of this chapter, by using Eqs. 6.6 and 6.7. In
            Fig. 6.4, the directions of σ 1 and σ 2 are the 1-2 axes, with these directions being determined by the
            θ n rotation from the original x-y axes. Further, the 3-axis is the z-axis, with σ 3 = σ z .
               However, for the general three-dimensional case, the 1-2-3 axes are unique directions that may
            all differ from the original x-y-z directions. The general procedure for finding σ 1 , σ 2 , and σ 3 and
            the corresponding 1-2-3 axes will be considered in the next section of this chapter. However, before
            proceeding with this somewhat advanced topic, it is useful to consider principal shear stresses and
            the maximum shear stress, and also to revisit plane stress.
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