Page 177 - T. Anderson-Fracture Mechanics - Fundamentals and Applns.-CRC (2005)
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1656_C003.fm  Page 157  Monday, May 23, 2005  5:42 PM





                       Elastic-Plastic Fracture  Mechanics                                         157


                       where A* is the area enclosed by Γ*. By invoking the definition of strain energy density given by
                       Equation (3.20), we can evaluate the first term in square brackets in Equation (A3.14):

                                                     ∂w  =  ∂w  ∂ε ij  = σ  ∂ε ij
                                                     ∂x   ∂ε ij  ∂ x  ij  ∂ x                   (A3.15)


                       Note that Equation (A3.15) applies only when w exhibits the properties of an elastic potential.
                       Applying the strain-displacement relationship (for small strains) to Equation (A3.15) gives


                                                                       ∂ 
                                                 ∂w  = σ     ∂   ∂u i  +  ∂  u j   
                                                     1
                                                                      
                                                 ∂x  2  ij   ∂x    ∂x  j    ∂  x i   
                                                                     x
                                                                        ∂ 
                                                         ∂  u                                  (A3.16)
                                                            ∂ 
                                                    = σ ij  ∂x j    x i 
                                                            ∂ 
                       since s  = s . Invoking the equilibrium condition:
                             ij
                                 ji
                                                           ∂σ ij
                                                           ∂x j  = 0                            (A3.17)

                       leads to

                                                      ∂   u ∂   ∂   u ∂ 
                                                                        i
                                                   σ  ij  x ∂  j     x  i  =  ∂ x ∂   j    σ  ij  x ∂    (A3.18)

                       which is identical to the second term in square brackets in Equation (A3.14). Thus the integrand
                       in Equation (A3.14) vanishes and J = 0 for any closed contour.
                          Consider now two arbitrary contours Γ  and Γ  around a crack tip, as illustrated in Figure A3.3.
                                                               2
                                                         1
                       If Γ  and Γ  are connected by segments along the crack face (Γ  and Γ ), a closed contour is formed.
                                                                        3
                          1
                               2
                                                                              4
                       The total J along the closed contour is equal to the sum of contributions from each segment:
                                                     J  J =  J +  J +  J +  =  0                (A3.19)
                                                         1   2  3   4


















                       FIGURE A3.3 Two arbitrary contours Γ 1  and Γ 2  around the tip of a crack. When these contours are connected
                       by Γ 3  and Γ 4 , a closed contour is formed, and the total J = 0.
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