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                       Linear Elastic Fracture Mechanics                                            53



































                       FIGURE 2.23 Plot of stress intensity solutions from Table 2.4.



                          Although stress intensity solutions are given in a variety of forms, K can always be related to
                       the through crack (Figure 2.4) through the appropriate correction factor:

                                                       K  (  I II III)  ,,  Y  a= σπ             (2.47)

                       where
                         σ = characteristic stress
                         a = characteristic crack dimension
                         Y = dimensionless constant that depends on the geometry and the mode of loading




                       EXAMPLE 2.4

                         Show that the K I  solution for the single edge notched tensile panel reduces to Equation (2.42) when a << W.

                         Solution: All of the K I  expressions in Table 2.4 are of the form:

                                                             P      a 
                                                       K =  BW   f  w 
                                                         I

                         where
                              P = applied force
                              B = plate thickness
                           f(a/W) = dimensionless function
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