Page 83 - T. Anderson-Fracture Mechanics - Fundamentals and Applns.-CRC (2005)
P. 83

1656_C02.fm  Page 63  Thursday, April 14, 2005  6:28 PM





                       Linear Elastic Fracture Mechanics                                            63


                       Elliptical and semielliptical flaws (Figure 2.20) also have an approximate closed-form plastic zone
                       correction, provided the flaw is small compared to the plate dimensions. In the case of the embedded
                       elliptical flaw, K  is given by
                                    eff

                                                      π a          a   2    / 14
                                              K eff  =  Q eff   sin 2  φ  + σ    c   cos ( )    (2.71)
                                                                         2
                                                                          φ ( )
                          where Q  is the effective flaw shape parameter defined as
                                 eff

                                                                   σ   2
                                                     Q  eff  Q =  −  0 212   σ YS            (2.72)
                                                              .

                          Equation (2.72) must be multiplied by a surface correction factor for a semielliptical surface
                       flaw (see Figure 2.20).
                          One interpretation of the Irwin plastic zone adjustment is that of an  effective  compliance.
                       Figure 2.30 compares the load-displacement behavior of a purely elastic cracked plate with that of
                       a cracked plate with a plastic zone at the tip. The load-displacement curve for the latter case deviates
                       from the purely elastic curve as the load increases. At a given load P, the displacement for the plate
                       with a plastic zone is greater than that of the elastic plate; referring to Figure 2.30, ∆  > ∆ . One
                                                                                                 1
                                                                                            2
                       can define an effective compliance as follows:
                                                                ∆
                                                           C =  P 2
                                                            eff

                          Therefore, a  in this instance can be viewed as the crack length that results in the compliance
                                    eff
                       C  in a purely elastic material.
                        eff
                          Finally, it should be noted that the author does not recommend using the Irwin plastic zone
                       adjustment for practical applications. It was presented here primarily to provide a historical context
                       to the development of both linear and nonlinear fracture mechanics. See Chapter 9 for recommended
                       approaches for handling plasticity effects.


























                       FIGURE 2.30 Definition of the effective compliance to account for crack-tip plasticity.
   78   79   80   81   82   83   84   85   86   87   88