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1656_C009.fm  Page 402  Monday, May 23, 2005  3:58 PM





                       402                                Fracture Mechanics: Fundamentals and Applications


                          Since Equation (9.31) gives an expression for the  P-∆  curve for a stationary crack, it is
                                                                        p
                       possible to compare J  estimates from Equation (9.29) and Equation (9.32) with Equation (9.35).
                                        pl
                       According to Equation (9.31), the P-∆  curve follows a power law, where the exponent is the
                                                       p
                       same as in the material’s true stress–true strain curve. The plastic energy absorbed by the specimen
                       is as follows:
                                            ∫ ∆ p Pd ∆  p  n  P∆ =  p

                                             0        n +1
                                                        n          P  n +1
                                                     =    P    aαε  h                          (9.36)
                                                      n  +1  o  o  3  P o 

                       Thus the plastic J is given by

                                                        n         a    P   n+1
                                                  J =     η  P ε α  h                          (9.37)
                                                   pl
                                                       n +1  po  o  b  3   P 
                                                                       o
                       Comparing Equation (9.29) and Equation (9.37) and solving for h  gives
                                                                             p
                                                                   2
                                                       η =  n +1 σ bh 1 3                       (9.38a)
                                                                 o
                                                                PWh
                                                             n
                                                         p
                                                                 o
                       Alternatively, if J  is given by Equation (9.34)
                                     pl
                                                                   2
                                                                 o
                                                       η =  n +1 σ bh 1 3                       (9.38b)
                                                         p
                                                             n
                                                                PWh
                                                                 o
                          Consider an edge-cracked bend specimen in plane strain. The EPRI fully plastic J solution for
                       this configuration is tabulated in Table A9.8. The reference load, assuming unit thickness and the
                       standard span of 4W, is given by
                                                            0 364σ b  2
                                                             .
                                                        P =    W  o                              (9.39)
                                                         o
                       Substituting Equation (9.39) into Equation (9.38a) gives


                                                     η =   1   n +1  W h 1                       (9.40)
                                                      p
                                                         0 364  n  a h
                                                          .
                                                                      3
                       Equation (9.40) is plotted in Figure 9.10 for n = 5 and n = 10. According to the equation that was
                       derived in Section 3.2.5, h  = 2. This derivation, however, is valid only for deep cracks, since it
                                             p
                       assumes that the ligament length b is the only relevant length dimension. Figure 9.10 indicates that
                       Equation (9.40) approaches the deep crack limit with increasing a/W. For n = 10, the deep crack
                       formula appears to be reasonably accurate beyond a/W~0.3. Note that the h  values computed from
                                                                                   p
                       Equation (9.40) for deep cracks fluctuate about an average of ~1.9, rather than the theoretical value
                       of 2.0. The deviations from the theoretical value for deep cracks may be indicative of numerical
                       errors in the h  and h  values.
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