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Basic rock fracture mechanics  143


                 Similarly, the crack tip displacement components can be obtained as
              follows (Eftis and Subramonian, 1978):

                                   2                         3
                                     1          q      q   2 q
                      u     K I  r 6  2         2      2    2  7
                              r  ffiffiffiffiffiffi  ðk   1Þcos   cos  sin
                          ¼        6                         7
                      v     G    2p 1           q     q    q  5
                                   4
                                      ðk þ 1Þsin   sin  cos 2
                                     2          2     2    2
                                        1          q     q    2 q
                                      2                         3
                                          ðk þ 1Þsin þ sin  cos
                                  r ffiffiffiffiffiffi
                               K II  r 6  2        2     2     2  7
                            þ         6                         7        (4.21)
                               G    2p 1           q      q    q  5
                                      4
                                         ð1   kÞcos þ cos   sin 2
                                        2          2      2    2
              where r is the radius started from the crack tip; k is expressed in terms of
              Poisson’s ratio n by k ¼ (3   4n) for plane strain and k ¼ (3   n)/(1 þ n)
              for idealized plane stress. The expression for stress hold provided 0 < (r/
              a) << 1, while for displacement 0   (r/a) << 1.
                 By detailed study of the infinite sheet with a flat crack subject to biaxial
              loads, it was shown that use of Eqs. (4.20) and (4.21) leads to predictions
              that are, in general, qualitatively as well as quantitatively incorrect (Eftis and
              Subramonian, 1978). They extended their previous work to treat the
              biaxially loaded infinite sheet with an inclined crack. The stress and
              displacement components in the immediate vicinity of the crack front are as
              follows (Eftis and Subramonian, 1978):


                      K I    q        q   3q     K II   q         q   3q
                s x ¼ p ffiffiffiffiffiffiffi cos  1   sin sin    p ffiffiffiffiffiffiffi sin  2 þ cos cos
                       2pr   2        2    2      2pr   2         2    2
                     þsð1   JÞcos 2 a

                      K I    q        q   3q     K II   q    q   3q
                s y ¼ p ffiffiffiffiffiffiffi cos  1 þ sin sin  þ p ffiffiffiffiffiffiffi sin cos cos
                       2pr   2        2    2      2pr   2    2    2

                       K I   q    q   3q    K II   q        q    3q
                s xy ¼ p ffiffiffiffiffiffiffi sin cos cos  þ p ffiffiffiffiffiffiffi cos  1   sin sin
                       2pr   2    2    2     2pr   2        2    2
                                                                         (4.22)
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