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                       404                                Fracture Mechanics: Fundamentals and Applications


































                       FIGURE 9.11 Comparison of J estimates from the EPRI handbook with the deep crack formula for a center-
                       cracked panel.


                                                                                                   *
                       time-dependent creep deformation (Chapter 4). He expressed the creep crack driving force C  as
                       a function of a parameter that he called  reference  stress. Several years later,  Ainsworth [29]
                       combined the reference stress concept with the EPRI J estimation procedure to introduce a new
                       fracture assessment methodology that is more versatile than the original EPRI approach.
                          The EPRI equations for fully plastic J, Equation (9.29) and Equation (9.32), assume that the
                       material’s stress-plastic strain curve follows a simple power law. Many materials, however, have flow
                       behavior that deviates considerably from a power law. For example, most low carbon steels exhibit
                       a plateau in the flow curve immediately after yielding. Applying Equation (9.29) or Equation (9.32)
                       to such a material, results in significant errors. Ainsworth [29] modified the EPRI relationships to
                       reflect more closely the flow behavior of real materials. He defined a reference stress as follows:
                                                        σ  ref  = (/  o  σ  o                    (9.42)
                                                              PP )
                       He further defined the reference strain as the total axial strain when the material is loaded to a
                       uniaxial stress of s . Substituting these definitions into Equation (9.29) gives
                                      ref
                                                                  σε   
                                                   J       b =  h   ε  − σ  ref  o             (9.43)
                                                    pl
                                                         ref
                                                               ref  σ o 
                                                             1
                       For materials that obey a power law, Equation (9.43) agrees precisely with Equation (9.29), but
                       the former is more general, in that it is applicable to all types of stress-strain behavior.
                          Equation (9.43) still contains h , the geometry factor that depends on the power-law-hardening
                                                   1
                       exponent n. Ainsworth proposed redefining P  for a given configuration to produce another constant
                                                           o
                       h ′  that is insensitive to n. He noticed, however, that even without the modification of P , h  was
                                                                                               o
                        1
                                                                                                 1
                       relatively insensitive to n except at high n values (low-hardening materials). Ainsworth believed
                       that accurate estimates of h  were less crucial for high n values because at that time, the strip-yield
                                            1
                       failure assessment diagram (Section 9.4.1) was considered adequate for low-hardening materials.
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