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                       310                                 Fracture Mechanics: Fundamentals and Applications






























                       FIGURE 7.13  Three types of load-displacement behavior in a K Ic  test.


                          When a precracked test specimen is loaded to failure, load and displacement are monitored.
                       Three types of load-displacement curves are shown in Figure 7.13. The critical load P  is defined
                                                                                            Q
                       in one of several ways, depending on the type of curve. One must construct a 5% secant line (i.e.,
                       a line from the origin with a slope equal to 95% of the initial elastic loading slope) to determine
                       P . In the case of Type I behavior, the load-displacement curve is smooth and it deviates slightly
                        5
                       from linearity before reaching a maximum load P max . This nonlinearity can be caused by plasticity,
                       subcritical crack growth, or both. For a Type I curve, P  = P . With a Type II curve, a small amount
                                                                  Q
                                                                       5
                       of unstable crack growth (i.e., a pop-in) occurs before the curve deviates from linearity by 5%. In
                       this case P  is defined at the pop-in. A specimen that exhibits Type III behavior fails completely
                               Q
                       before achieving 5% nonlinearity. In such cases, P  = P max .
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                          The crack length must be measured from the fracture surface. Since there is a tendency for the
                       crack depth to vary through the thickness, the crack length is defined as the average of three evenly
                       spaced measurements. Once P  and the crack length are determined, a provisional fracture tough-
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                       ness K  is computed from the following relationship:
                            Q
                                                             P
                                                             Q
                                                      K =  BW    fa W)                            (7.1)
                                                                  (/
                                                        Q
                       where f (a/W) is a dimensionless function of a/W. This function is given in polynomial form in the
                       E 399 standard for the four specimen types. Individual values of f (a/W) are also tabulated in ASTM
                       E 399. See Table 2.4 and Appendix 7 for K solutions for a variety of configurations.
                          The K  value computed from Equation (7.1) is a valid K  result only if all validity requirements
                               Q
                                                                      Ic
                       in the standard are met, including
                                                       045 ≤  .  / aW  ≤  055                    (7.2a)
                                                                   .
                                                                 K  2
                                                                  Q
                                                         ,
                                                        Ba ≥ 25   σ YS                       (7.2b)
                                                             .
                                                         P   ≤  . 110 P                          (7.2c)
                                                          max      Q
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