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STATIC STRESSSTRAIN RELATION           557
























                                       Y
                                             Figum 9.3. Stress at a point 0 in a plane f5j.


                                If any plane is taken within a solid body, as shown in Figure 9.3 along
                             the yz-plane, then the internal components of  stress may be resolved
                             into normal stress (on), which acts at a right angle to the plane, and
                             shear stress components, which act parallel to the plane (zxy  and zxz). If
                             the solid plane is taken along the xz-plane, the normal and shear stress
                             components at point  0 are zy., ow,zyz, and in the xy-plane the three
                             components are zm , zq, and 0,.  Therefore, nine components of stress
                             are required to fully define the forces acting on the cubic element shown
                             in Figure 9.1 The stress matrix is:







                             The notation Tij should be read as the “shear stress acting in the j direction
                             on a plane norma1 to the i axis.” By convention, the normal stresses o,,
                             ow, and oZ-or  for convenience ox, oY, and 0,-are    positive when
                             directed into the plane. If  the body is at equilibrium, then zq  = zyx,
                             T~ = ’tV, and 7% = zyz. In matrix operations it is convenient to express
                             the stress tensor as:








                                It is possible to show that there is one set of axes with respect to which
                             all shear stresses are zero and the normal stresses have their extreme
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