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1656_C02.fm  Page 81  Thursday, April 14, 2005  6:28 PM





                       Linear Elastic Fracture Mechanics                                            81


















                                                               FIGURE 2.51 Typical propagation from an initial
                                                               crack that is not orthogonal to the applied normal
                                                               stress. The loading for the initial angled crack is a
                                                               combination of Mode I and Mode II, but the crack
                                                               tends to propagate normal to the applied stress, result-
                                                               ing in pure Mode I loading.


                       Figure 2.51 illustrates a more typical scenario for an angled crack. When fracture occurs, the crack
                       tends to propagate orthogonal to the applied normal stress; i.e., the mixed-mode crack becomes a
                       Mode I crack.
                          A propagating crack seeks the path of least resistance (or the path of maximum driving force)
                       and need not be confined to its initial plane. If the material is isotropic and homogeneous, the crack
                       will propagate in such a way as to maximize the energy release rate. What follows is an evaluation
                       of the energy release rate as a function of propagation direction in mixed-mode problems. Only
                       Mode I and Mode II are considered here, but the basic methodology can, in principle, be applied
                       to a more general case where all three modes are present. This analysis is based on similar work
                       in Refs. [34–36].


                       2.11.1 PROPAGATION OF AN ANGLED CRACK
                       We can generalize the angled through-thickness crack of Figure 2.18 to any planar crack oriented
                       90° − β from the applied normal stress. For uniaxial loading, the stress intensity factors for Mode I
                       and Mode II are given by

                                                        K  I  K =  I  ()  cos β                 (2.91a)
                                                                   2
                                                              0
                                                                   β
                                                       K  II  K =  I() 0  cos sinβ              (2.91b)
                       where K  is the Mode I stress intensity when β = 0. The crack-tip stress fields (in polar coordinates)
                             I(0)
                       for the Mode I portion of the loading are given by

                                               σ =     I  5  cos  θ K  −  1  cos   3 θ       (2.92a)
                                                         
                                                rr
                                                     2 πr  4     4    2   
                                                                2
                                               σ  =    I  3  cos  θ K  +  1  cos   3 θ       (2.92b)
                                                         
                                                θθ
                                                       r
                                                                2
                                                     2 π  4      4    2   
                                               τ  =    I  1  sin  θ K  +  1  sin   3 θ       (2.92c)
                                                         
                                                 θ r
                                                     2 πr  4     4    2   
                                                               2
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