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                       50                                    Fracture Mechanics: Fundamentals and Applications









































                       FIGURE 2.20 Stress concentration effects due to a through crack in finite and infinite width plates:  (a)
                       infinite plate and (b) finite plate.

                          One technique to approximate the finite width boundary condition is to assume a periodic array
                       of collinear cracks in an infinite plate (Figure 2.21). The Mode I stress intensity factor for this
                       situation is given by
                                                                         /
                                                  K  I    a = σπ  2 W  tan  π a    12       (2.45)
                                                            
                                                              π a   2 W  
                       The stress intensity approaches the infinite plate value as a/W approaches zero; K  is asymptotic
                                                                                          I
                       to a/W = 1.
                          More accurate solutions for a through crack in a finite plate have been obtained from finite-element
                       analysis; solutions of this type are usually fit to a polynomial expression. One such solution [12] is given by

                                                    π a   / 12      a   2    a   4 
                                        K  I   a = σπ   sec    1 − . 0 025  + . 0 06         (2.46)
                                                    2 W          W        w   

                       Figure 2.22 compares the finite width corrections in Equation (2.45) and Equation (2.46). The
                       secant term (without the polynomial term) in Equation (2.46) is also plotted. Equation (2.45) agrees
                       with the finite-element solution to within 7% for a/W < 0.6. The secant correction is much closer
                       to the finite element solution; the error is less than 2% for a/W < 0.9. Thus, the polynomial term
                       in Equation (2.46) contributes little and can be neglected in most cases.
                          Table 2.4 lists stress intensity solutions for several common configurations. These K  solutions
                                                                                              I
                       are plotted in Figure 2.23. Several handbooks devoted solely to stress intensity solutions have been
                       published [12–14].
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