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1656_C004.fm  Page 204  Thursday, April 21, 2005  5:38 PM





                       204                                   Fracture Mechanics: Fundamentals and Applications


                       4.3.3 TRANSITION FROM LINEAR TO NONLINEAR BEHAVIOR

                       Typical polymers are linear viscoelastic at low stresses and nonlinear at high stresses. A specimen
                       that contains a crack may have a zone of nonlinearity at the crack tip, analogous to a plastic
                       zone, which is surrounded by linear viscoelastic material. The approach described in the previous
                       section applies only when one type of behavior (linear or nonlinear) dominates.
                          Schapery [61] has modified the J  concept to cover the transition from small-stress to large-
                                                     v
                       stress behavior. He introduced a modified constitutive equation, where the strain is given by the
                       sum of two hereditary integrals: one corresponding to linear viscoelastic strains and the other
                       describing nonlinear strains. For the latter term, he assumed power-law viscoelasticity. For the case
                       of uniaxial constant tensile stress σ  the creep strain in this modified model is given by
                                                   o
                                                               σ   n
                                                   t
                                                                        t
                                                  ε() =  E  R D  ()   o  D +  L   () σ o       (4.85)
                                                           t
                                                              σ ref 
                       where D and D  are the nonlinear and linear creep compliance, respectively, and σ  is a reference
                                   L
                                                                                         ref
                       stress.
                          At low stresses and short times, the second term in Equation (4.85) dominates, while the nonlinear
                       term dominates at high stresses or long times. In the case of a viscoelastic body with a stationary
                       crack at a fixed load, the nonlinear zone is initially small but normally increases with time, until the
                       behavior is predominantly nonlinear. Thus there is a direct analogy between the present case and the
                       transition from elastic to viscous behavior described in Section 4.2.
                          Close to the crack tip, but outside of the failure zone, the stresses are related to a pseudo-strain
                       through a power law:

                                                               σ    n
                                                          e
                                                         ε =    o                              (4.86)
                                                              σ ref 

                       In the region dominated by Equation (4.86), the stresses are characterized by J , regardless of whether
                                                                                   v
                       the global behavior is linear or nonlinear:

                                                                  1
                                                            J   n  +1
                                                  σ  ij  σ =  ref   v    σ  ˜ ij  θ n (, )     (4.87)
                                                           σ Ir
                                                            ref n 

                       If the global behavior is linear, there is a second singularity further away from the crack tip:
                                                             K
                                                       σ =     I  f  θ ()                        (4.88)
                                                         ij
                                                             2 πr  ij

                          Let us define a pseudo-strain tensor that, when inserted into the path-independent integral of
                       Equation (4.72), yields a value J . Also suppose that this pseudo-strain tensor is related to the stress
                                                L
                       tensor by means of linear and power-law pseudo-complementary strain energy density functions
                       (w  and w , respectively):
                               cn
                         cl
                                                           ∂
                                                      ε ij eL  =  ∂ σ ij  ( fw +  w )            (4.89)
                                                                 cn
                                                                     cl
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