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1656_C009.fm  Page 412  Monday, May 23, 2005  3:58 PM





                       412                                Fracture Mechanics: Fundamentals and Applications


                       The stress ratio for the component of interest can be defined as the ratio of the applied stress to
                       the collapse stress. Alternatively, the applied S  can be defined in terms of axial forces or moments.
                                                            r
                       If the assessment point with coordinates (S , K ) falls inside of the FAD curve, the analysis predicts
                                                            r
                                                         r
                       that the component is safe.
                         EXAMPLE 9.2

                         A middle tension (MT) panel (Figure 7.1(e)) 1 m wide and 25 mm thick with a 200 mm crack must
                         carry a 7.00 MN load. For the material K mat  = 200 MPa, m  s YS  = 350 MPa, and s TS  = 450 MPa. Use
                         the strip-yield FAD to determine whether or not this panel will fail.

                         Solution: We can take account of work hardening by assuming a flow stress that is the average of yield
                         and tensile strength. Thus s flow  = 400 MPa. The collapse load is then defined when the stress on the
                         remaining cross section reaches 400 MPa:
                                             P =  c          )(1 m  − (400 MPa  . 0 200 m ) 8 .00 MN
                                                                        = )( . 0 025 m
                         Therefore
                                                           .
                                                       S =  r  700 MN  =  0 875
                                                                   .
                                                           .
                                                          800 MN
                         The applied stress intensity can be estimated from Equation (2.46) (without the polynomial term):
                                                                  π
                                                                    0
                                              .
                                       K =   700 MN     π ( 0 100 m )sec  (.100 m   )  = 161 MPa m
                                                          .
                                                                  
                                        I
                                           (.  m )( 1 0  m )        100 m  
                                                                     .
                                                   .
                                           0 025
                         Thus
                                                         K =  r  161  =  0 805
                                                                 .
                                                            200
                         The point (0.875, 0.805) is plotted in Figure 9.17. Since this point falls outside of the failure assessment
                         diagram, the panel will fail before reaching 7 MN. Note that a collapse analysis or brittle fracture
                         analysis alone would have predicted a “safe” condition. The interaction of fracture and plastic collapse
                         causes failure in this case.
                          In 1976, the Central Electricity Generating Board (CEGB) in Great Britain incorporated the
                       strip-yield failure assessment into a fracture analysis methodology, which became known as the
                       R6 approach [31]. There have been several revisions of the R6 procedure over the years. The R6
                       approach is still based on the FAD methodology, but Equation (9.57) is no longer used. Section 9.4.2
                       and Section 9.4.3 describe the modern formulation of the FAD approach.
                       9.4.2 J-BASED FAD

                       Bloom [32] and Shih et al. [33] showed that a J-integral solution from the EPRI handbook could
                       be plotted in terms of a FAD. Of course, a more rigorous J solution based on elastic-plastic finite
                       element analysis can also be plotted as a FAD.
                          The failure assessment diagram is nothing more than an alternative method for plotting the
                       fracture driving force. The shape of the FAD curve is a function of plasticity effects. As described
                       above, the first FAD was derived from the strip-yield plastic zone correction, which assumes a
                       nonhardening material. A J solution merely provides a more accurate description of the FAD curve.
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