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1656_C02.fm  Page 59  Thursday, April 14, 2005  6:28 PM





                       Linear Elastic Fracture Mechanics                                            59


                       energy that accompanies an increment of crack extension; the latter quantity characterizes the
                       stresses, strains, and displacements near the crack tip. The energy release rate describes global
                       behavior, while K is a local parameter. For linear elastic materials, K and G are uniquely related.
                          For a through crack in an infinite plate subject to a uniform tensile stress (Figure 2.3), G and
                       K  are given by Equation (2.24) and Equation (2.41), respectively. Combining these two equations
                        I
                       leads to the following relationship between G and K  for plane stress:
                                                                 I
                                                               K  2
                                                           G =  I                                (2.54)
                                                               E
                                                                      2
                       For plane strain conditions, E must be replaced by E/(1 − ν ). To avoid writing separate expressions
                       for plane stress and plane strain, the following notation will be adopted throughout this book:
                                                     E  ′= E  for plane stress                  (2.55a)

                       and
                                                        E
                                                   E ′ =      for plane strain                  (2.55b)
                                                       1 − v 2
                       Thus the G-K  relationship for both plane stress and plane strain becomes
                                  I
                                                               K  2
                                                           G =  I                                (2.56)
                                                                ′ E
                          Since Equation (2.24) and Equation (2.41) apply only to a through crack in an infinite plate, we
                       have yet to prove that Equation (2.56) is a general relationship that applies to all configurations. Irwin [9]
                       performed a crack closure analysis that provides such a proof. Irwin’s analysis is presented below.
                          Consider a crack of initial length  a +∆a subject to Mode I loading, as illustrated in
                       Figure 2.28(a). It is convenient in this case to place the origin a distance ∆a behind the crack tip.
































                                                               FIGURE 2.28 Application of closure stresses which
                                                               shorten a crack by ∆a.
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