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122                                   Mechanical Behaviour of Plastics
                       be expressed as

                                                                                    (2.80)

                       where y  is the surface energy per unit area.
                         Note that for a situation where the applied force does no work (Le. there is
                       no overall change in length of  the material) then  W = 0 and equation (2.80)
                       becomes                      au
                                                    -'Yz   aA                       (2.81)
                                                    aa
                         Now, for a through crack propagating in a sheet of material of thickness, B,
                       we may write
                                                    aA = 2Baa

                       So equation (2.80) becomes
                                                 a
                                                -(W - U) > 2yB                      (2.83)
                                                 aa
                         In the context of  fracture mechanics the term 2y is replaced by  the G,  so
                       that the condition for fracture is written as
                                                ia
                                                --(W  - U) > G,                     (2.84)
                                                Baa
                         G, is a material property which is referred to  as the toughness, critical
                       strain energy release rate or crack extension force. It is effectively the energy
                       required to increase the crack length by unit length in a piece of  material of
                       unit width. It has units of J/m2.
                         Equation  (2.84) may  be  converted into a  more practical form as follows.
                       Consider a piece of material of thickness, B, subjected to a force, F, as shown
                       in Fig. 2.63(a). The load-deflection graph is shown as line (i) in Fig. 2.63(b).
                       From this the elastic stored energy, U 1,  may be expressed as

                                                    U1 = ZFS                        (2.85)
                                                          1
                         If  the crack extends by a small amount aa then the stiffness of the material
                       changes and  there will be  a  small change in  both  load,  aF, and  deflection,
                       86. This is shown as line (ii) in Fig. 2.63(b). The elastic stored energy would
                       then be
                                              U2 = i(F + aF)(6 + 36)                (2.86)
                         From equations (2.85) and (2.86) the change in stored energy as a result of
                       the change in crack length 8~ would be given by
                                       au = u2 - u1 = $(Fad + 6aF + aFas)           (2.87)
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