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1656_C004.fm  Page 209  Thursday, April 21, 2005  5:38 PM





                       Dynamic and Time-Dependent Fracture                                         209


                       where the subscripts + and − correspond to the upper and lower crack surfaces, respectively. The
                       following functions satisfy the boundary conditions and lead to integrable strain energy density
                       and finite displacement at the crack tip:
                                                         C           −2β C
                                                 Fz   =    Gz    =      2                       (A4.11)
                                                  ′′()
                                                             ′′( )
                                                    1    z     2    + (  2 )1 β  z
                                                          1            2   2
                       where  C is a constant. Making the substitution  z  r  e=  i 1 θ  and  z  r  e=  i 2 θ  leads to the following
                                                                1  1        2   2
                       expressions for the Mode I crack-tip stress fields:
                                       Kt() 1 + β 2             θ       4 β   β r   θ   r  
                                  σ  =   I      2      β + (  2  β −  2 )  12  cos  1  −  1 2  cos  2    (A4.12a)
                                    xx
                                         2 πrD t()     1  2    2    r 1  1 + β 2 2   2   r 2   
                                         Kt() 1 + β 2         θ       4 β   β r    θ   r  
                                    σ =   I      2   −+ (  β )1  2  cos  1  +  1 2  cos  2    (A4.12b)
                                      yy
                                          2 πrD t()     2    2   r 1  1 + β 2 2   2    r 2   

                                              Kt()  β    β ( 2  2     θ + )1  r    θ     r  
                                         τ =    I    1    2  sin  1   − sin  2                (A4.12c)
                                                        t
                                           xy
                                                πr 2  D  ()      2   r 1   2    r 2  
                       where
                                                     Dt() =    − 4ββ  ( 12  +  2 2 )1 β  2


                       Equation (A4.12) reduces to the quasistatic relationship (Table 2.1) when V = 0.
                          Craggs [25] and Freund [10] obtained the following relationship between K (t) and the energy
                                                                                       I
                       release rate for crack propagation at a constant speed:

                                                                2
                                                              K (1 −ν 2 )
                                                               I
                                                      G = AV()                                  (A4.13)
                                                                  E
                       for plane strain, where

                                                               V β
                                                                 2
                                                      AV() =       1
                                                            ( −ν ) cD t)
                                                                  2
                                                             1
                                                                    (
                                                                  2
                       It can be shown that  lim  A = 1 , and Equation (A4.13) reduces to the quasistatic result. Equation
                                          V→0
                       (A4.13) can be derived by substituting the dynamic crack-tip solution (Equation (A4.12) and the
                       corresponding relationships for strain and displacement) into the generalized contour integral given
                       by Equation (4.26).
                          The derivation that led to Equation (A4.12) implies that Equation (A4.13) is a general rela-
                       tionship that applies to accelerating cracks as well as constant speed cracks.
                       A4.2  DERIVATION OF THE GENERALIZED ENERGY RELEASE RATE

                       Equation (4.26) will now be derived. The approach closely follows that of Moran and Shih [11],
                       who applied a general balance law to derive a variety of contour integrals, including the energy
                       release rate. Other authors [8–10] have derived equivalent expressions using slightly different
                       approaches.
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