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1656_C003.fm  Page 151  Monday, May 23, 2005  5:42 PM





                       Elastic-Plastic Fracture  Mechanics                                         151









































                       FIGURE 3.45 Experimental data from Figure 3.28 corrected for constraint loss. Taken from Anderson, T.L.,
                       Stienstra, D.I.A., and Dodds, R.H., Jr., ‘‘A Theoretical Framework for Addressing Fracture in the Ductile-
                       Brittle Transition Region.’’ Fracture Mechanics, Vol. 24, ASTM STP 1207, American Society for Testing and
                       Materials, Philadelphia, PA (in press).

                       the case of two-parameter theory is mostly arbitrary, but the T stress has no physical meaning
                       under large-scale yielding conditions.
                          Just as plastic flow invalidates single-parameter fracture mechanics in many geometries, two-
                       parameter theories eventually break down with extensive deformation. If we look at the structure
                       of the crack-tip fields in the plastic zone, we can evaluate the range of validity of both single- and
                       two-parameter methodologies.
                          A number of investigators [39–43] have performed asymptotic analyses of the crack-tip fields
                       for elastic-plastic materials. These analyses utilize deformation plasticity and small-strain theory.
                       In the case of plane strain, these analyses assume incompressible strain. Consequently, asymptotic
                       analyses are not valid close to the crack tip (in the large-strain zone) nor remote from the crack
                       tip, where elastic strains are a significant fraction of the total strain. Despite these limitations,
                       asymptotic analysis provides insights into the range of validity of both single- and two-parameter
                       fracture theories.
                          In the case of a plane strain crack in a power-law-hardening material, asymptotic analysis leads
                       to the following power series:
                                                                   s k
                                                      ∞
                                                          
                                                                  
                                                              J
                                                  ij ∑
                                                 σ =    A k αεσ r    σ  ij k () (,  n)        (3.87)
                                                                        θ ˆ
                                                      k=1    o  o
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