Page 222 - Intro to Tensor Calculus
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                                            Figure 2.3-5. Stress distribution at a point


                                                                                    i
                   For i =1, 2, 3 we adopt the convention of sketching the components of ~ t in the positive directions if
                                               i
               the exterior normal to the surface x = constant also points in the positive direction. This gives rise to the
               figure 2.3-4 which illustrates the stress vectors acting upon an element of volume in rectangular Cartesian
                                                                                                  ij
                                            11
                                               22
               coordinates. The components σ ,σ ,σ 33  are called normal stresses while the components σ ,i 6= j are
               called shearing stresses. The equations (2.3.7) can be written in the more compact form using the indicial
               notation as
                                                    i
                                                         ij
                                                   ~ t = σ ˆ e j ,  i, j =1, 2, 3.                     (2.3.8)
                   If we know the stress distribution at three orthogonal interfaces at a point P in a solid body, we can then
               determine the stress at the point P with respect to any plane passing through the point P. With reference to
               the figure 2.3-5, consider an arbitrary plane passing through the point P which lies within the material body
                                                                                                 1
                                                                                                        2
               being considered. Construct the elemental tetrahedron with orthogonal axes parallel to the x = x, x = y
                    3
               and x = z axes. In this figure we have the following surface tractions:
                                                   − ~ t  1  on the surface 0BC
                                                   − ~ t  2  on the surface 0AC

                                                   − ~ t  3  on the surface 0AB
                                                   ~ t (n)  on the surface ABC

               The superscript parenthesis n is to remind you that this surface traction depends upon the orientation of
               the plane ABC which is determined by a unit normal vector having the direction cosines n 1 ,n 2 and n 3 .
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