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1656_C008.fm  Page 379  Monday, May 23, 2005  5:59 PM





                       Fracture Testing of Nonmetals                                               379




























                       FIGURE 8.22 Comparison of stress-intensity factors in specimens with chevron and straight notches. Note
                       that K I  exhibits a minimum in the chevron-notched specimens.



                          The K  vs. crack length behavior of the chevron-notched specimen makes this specimen particu-
                               I
                       larly suitable for measuring the toughness in brittle materials. Consider a material in which the R
                       curve reaches a steady-state plateau soon after the crack initiates (Figure 8.23). The crack should
                       initiate at the tip of the chevron upon application of a small load, since the local K  is high. The crack
                                                                                       I
                       is stable at this point, because the driving force decreases rapidly with crack advance; thus additional
                       load is required to grow the crack further. The maximum load in the test, P , is achieved when the
                                                                                   M
                       crack grows to a , the crack length corresponding to the minimum in the K -a curve. At this point,
                                                                                   I
                                    m
                       the specimen will be unstable if the test is conducted in load control, but stable crack growth may be
                       possible beyond a  if the specimen is subject to crosshead control. The point of instability in the
                                     m
                       latter case depends on the compliance of the testing machine, as discussed in Section 2.5.

























                       FIGURE 8.23 Fracture toughness testing of a material with a flat R curve. The maximum load in the test
                       occurs when a = a m .
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