Page 55 - T. Anderson-Fracture Mechanics - Fundamentals and Applns.-CRC (2005)
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1656_C02.fm  Page 35  Thursday, April 14, 2005  6:28 PM





                       Linear Elastic Fracture Mechanics                                            35


                       The term rate, as it is used in this context, does not refer to a derivative with respect to time; G is
                       the rate of change in potential energy with the crack area. Since G is obtained from the derivative
                       of a potential, it is also called the crack extension force or the crack driving force. According to
                       Equation (2.18a), the energy release rate for a wide plate in plane stress with a crack of length 2a
                       (Figure 2.3) is given by

                                                              πσ a
                                                                2
                                                          G =                                    (2.24)
                                                               E
                       Referring to the previous section, crack extension occurs when G reaches a critical value, i.e.,

                                                            dW
                                                        G =  c  dA S  =  2 w f                   (2.25)

                       where G  is a measure of the fracture toughness of the material.
                             c
                          The potential energy of an elastic body, Π, is defined as follows:
                                                          ∏= U  − F                              (2.26)

                       where U is the strain energy stored in the body and F is the work done by external forces.
                          Consider a cracked plate that is dead loaded, as illustrated in Figure 2.7. Since the load is fixed
                       at P, the structure is said to be load controlled. For this case

                                                           F   P =∆
                       and


                                                       U   ∫ ∆ P =  d  ∆  =  P∆
                                                           0       2

































                       FIGURE 2.7 Cracked plate at a fixed load P.
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