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STRESS AND INFINITESIMAL STRAIN

                                        components of stress (  xx ,   yy ,   xy ) and the antiplane components (  zz ,   yz ,   zx ). In
                                        the particular case where the z direction is a principal axis, the antiplane shear stress
                                        components vanish. The plane geometric problem can then be analysed in terms of
                                        the plane components of stress, since the   zz , component is frequently neglected. A
                                        state of biaxial (or two-dimensional) stress at any point in the medium is defined by
                                        three components, in this case   xx ,   yy ,   xy .
                                          The stress transformation equations related to   ll ,   mm ,   lm in equation 2.22, for
                                        the biaxial state of stress, may be recast in the form
                                                         1
                                                                      1
                                                      ll = (  xx +   yy ) + (  xx −   yy ) cos 2  +   xy sin 2
                                                         2            2
                                                                      1
                                                         1
                                                     mm = (  xx +   yy ) − (  xx −   yy ) cos 2  −   xy sin 2   (2.23)
                                                         2            2
                                                                    1
                                                      lm =   xy cos 2  − (  xx −   yy ) sin 2
                                                                    2
                                          In establishing these equations, the x, y and l, m axes are taken to have the same
                                        sense of ‘handedness’, and the angle   is measured from the x to the l axis, in a sense
                                        that corresponds to the ‘handedness’ of the transformation. There is no inference
                                        of clockwise or anticlockwise rotation of axes in establishing these transformation
                                        equations. However, the way in which the order of the terms is specified in the
                                        equations, and related to the sense of measurement of the rotation angle  , should be
                                        examined closely.
                                          Consider now the determination of the magnitudes and orientations of the plane
                                        principal stresses for a plane problem in the x, y plane. In this case, the   zz ,   yz ,   zx
                                        stress components vanish, the third stress invariant vanishes, and the characteristic
                                        equation, 2.18, becomes

                                                           2
                                                           − (  xx +   yy )  p +   xx   yy −   2  = 0
                                                          p                          xy
                                          Solution of this quadratic equation yields the magnitudes of the plane principal
                                        stresses as

                                                                                          	 1/2
                                                            1              1        2   2
                                                        1,2 = (  xx +   yy ) ±  (  xx −   yy ) +     (2.24a)
                                                            2             4             xy
                                        The orientations of the respective principal stress axes are obtained by establishing
                                        the direction of the outward normal to a plane which is free of shear stress. Suppose
                                        ab, shown in Figure 2.5, represents such a plane. The outward normal to ab is Ol, and
                                        therefore defines the direction of a principal stress,   p . Considering static equilibrium
                                        of the element aOb under forces operating in the x direction:

                                                         p ab cos   −   xx ab cos   −   xy ab sin   = 0
                                        or

                                                                        p −   xx
                                                               tan   =
                                                                          xy
                                        i.e.
              Figure 2.5  Problem geometry for
              determination of plane principal                     = tan −1    p −   xx              (2.24b)
              stresses and their orientations.                                xy
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