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                       58                                    Fracture Mechanics: Fundamentals and Applications
























                       FIGURE 2.27 Through crack configuration analyzed in Example 2.6: (a) definition of coordinate axes and
                       (b) arbitrary traction applied to crack faces.

                         If we apply a surface traction of ±p(x) on the crack faces, the Mode I stress intensity factor for the two
                         crack tips is as follows:
                                                K      =  1  ∫ 2 a  px()  x  dx
                                                  Ix=2 a)  π a  0     a 2  x −
                                                  (
                                                                       −
                                                 K    =   1  ∫ 2 a  px()  2 ax dx
                                                  Ix=0 )  π a  0      x
                                                   (


                          The weight function concept is not restricted to two-dimensional bodies, Mode I loading, or
                       isotropic elastic materials. In their early work on weight functions, Rice [15] extended the theory
                       to three dimensions, Bueckner [16] considered combined Mode I/II loading, and both allowed for
                       anisotropy in the elastic properties. Subsequent researchers [17–22] have shown that the theory
                       applies to all linear elastic bodies that contain an arbitrary number of cracks.
                          For mixed-mode problems, separate weight functions are required for each mode: h , h , and
                                                                                              I
                                                                                                 II
                       h . Since the stress intensity factors can vary along a three-dimensional crack front, the weight
                        III
                       functions also vary along the crack front. That is
                                                                 η
                                                         h  a  h =  a  x (, )                    (2.52)
                                                                i
                       where α( = 1, 2, 3) indicates the mode of loading and η is the crack front position.
                          Given that any loading configuration in a cracked body can be represented by equivalent crack-
                       face tractions, the general mixed-mode, three-dimensional formulation of the weight function
                       approach can be expressed in the following form:

                                                     K  a   ∫  T ()  i  hη  a  x=  i  d  S ( , ) η  (2.53)
                                                            S c
                       where T are the tractions assumed to act on the crack surface S .
                             i
                                                                          c
                          See Chapter 9 for examples of practical applications of weight functions.
                       2.7 RELATIONSHIP BETWEEN K AND G

                       Two parameters that describe the behavior of cracks have been introduced so far: the energy release
                       rate and the stress intensity factor. The former parameter quantifies the net change in potential
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