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Microstructure Characterization   93


                 Where U is the elastic energy contained in the volume; F is the work performed by
              external force;  W is the energy for crack formation, and  S is the cracked surface.
               d                                 dW
                   −
                ( FU)  is the energy release rate and    is the crack resistance. If the material is
              dS                                 dS
              truly brittle like glass, the energy for crack growth is the surface energy to form the new
                                  dW
              fractured surface, and    γ − the surface energy for the material. If the volume
                                   dS
              change is further assumed to be negligible during the crack growth process, then:
                                              dS =  dS V                         (3-42)
                                                   v  0
                 Where S v is the specific damaged surface area and V 0 is the constant volume. There-
              fore, the following evolution equation for S v  holds.

                                            d
                                              ( FU)−  = V γ                      (3-43)
                                           dS          0
                                             v
              3.6.1.2 Damage Tensor
              The damage tensor s ij thus defined is widely used in CDM. The typical application can
              be found in the following equation (Murakami, 1988):
                                             −
                                             σ = M  σ                            (3-44)
                                              ij
                                                   ijkl  kl
                 Where s ij , s kl are the effective stress tensor and the Cauchy stress tensor respec-
              tively, while M ijkl  is a symmetric fourth rank tensor—the damage effect tensor. By using
              the vector formats of the tensors, Murakami (1988) showed that:
                                                      –1
                                             M = (I − j)                         (3-45)
                 Where I is the second-rank identity tensor, and j is the damage tensor.
                 Voyiadjis and Kattan (1999) derived an explicit relation between M and j. The di-
              agonalized form involves the terms of 1/(1 − j i ), and 1/(1 − j i )(1 − j j ) (i,j=1,2,3, i ≠ j).
              The averages of these terms and 1/(1 − j 1 )(1 − j 2 )(1 − j 3 ) may serve as empirical quan-
              tity to represent the state of damage. Voyiadjis and Kattan (1999) also introduced a term
             ϕ =  ϕ + ϕ + ϕ to represent the overall damage. This term was used to represent the
                       2
                   2
                           2
                   1   2   3
              damage states of the specimens obtained from the WesTrack project (Wang et al., 2001b).
              3.6.1.3 Spacing-Size Ratio
              The spacing between defects and the size of the defects are important variables in non-
              local damage theories. For modeling applications, the size of cracks or voids and the
              average spacing among the cracks offer two relevant parameters that are related to
              performance. Chudnovsky et al. (1987a, 1987b) developed a simple model addressing
              the interaction of two cracks, in which the two important model parameters are the
              spacing between the two crack tips and the sizes of the cracks. Figure 3.24 presents the
              configuration of two interacting cracks. The stress intensity (mode I) of the large crack
                                                  K  eff
                                                              eff
              is affected by the adjacent cracks. The ratio   1   (where  K is the effective stress inten-
                                                              1
                                                  K 0 1
              sity of a crack when subjected to the influence of the adjacent crack while K l  is the stress
                                                                            0
              intensity without the influence of adjacent cracks) decreases with the increase of l/d,
              which means, the larger the crack size and/or the smaller the spacing, the larger the
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