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                       Elastic-Plastic Fracture  Mechanics                                         115













































                       FIGURE 3.13 Schematic of early experimental measurements of J, performed by Landes and Begley. Taken
                       from Begley, J.A. and Landes, J.D., ‘‘The J-Integral as a Fracture Criterion.’’ ASTM STP 514, American
                       Society for Testing and Materials, Philadelphia, PA, 1972, pp. 1–20; Landes,  J.D.  and  Begley,  J.A.,  ‘‘The
                       Effect of Specimen Geometry on J Ic .’’ ASTM STP 514, American Society for Testing and Materials, Phila-
                       delphia, PA, 1972, pp. 24–29.

                       A much better method for determining J numerically is outlined in Chapter 12. More practical
                       experimental approaches are developed below and are explored further in Chapter 7.
                          Landes and Begley [11, 12], who were among the first to measure J experimentally, invoked
                       the energy release rate definition of J (Equation (3.11)). Figure 3.13 schematically illustrates their
                       approach. They obtained a series of test specimens of the same size, geometry, and material and
                                                    3
                       introduced cracks of various lengths.  They deformed each specimen and plotted load vs. displace-
                       ment (Figure 3.13(a)). The area under a given curve is equal to U, the energy absorbed by the
                       specimen. Landes and Begley plotted  U vs. crack length at various fixed displacements
                       (Fig. 3.13(b)). For an edge-cracked specimen of thickness B, the J integral is given by


                                                        J =−  1    ∂ U                       (3.25)
                                                             B ∂   ∆
                                                               
                                                                 a
                       Thus J can be computed by determining the slope of the tangent to the curves in Figure 3.13(b).
                       Applying Equation (3.25) leads to Figure 3.13(c), a plot of J vs. displacement at various crack

                       3  See Chapter 7 for a description of fatigue-precracking procedures for test specimens.
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