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1656_C008.fm  Page 354  Monday, May 23, 2005  5:59 PM





                       354                                 Fracture Mechanics: Fundamentals and Applications


                          Let us examine the basis for applying K and J to viscoelastic materials, as well as the limitations
                       on these parameters.
                       8.1.1.1 K-Controlled Fracture

                       In linear viscoelastic materials, remote loads and local stresses obey the same relationships as in
                       the linear elastic case. Consequently, the stresses near the crack tip exhibit a 1/ r  singularity:

                                                             K
                                                       σ =    I  f  θ ()                          (8.1)
                                                         ij
                                                             2 π r  ij

                       and  K  is related to remote loads and geometry through the conventional linear elastic fracture
                            I
                       mechanics (LEFM) equations introduced in Chapter 2. The strains and displacements depend on
                       the viscoelastic properties, however. Therefore, the critical stress-intensity factor for a viscoelastic
                       material can be rate dependent; a K  value from a laboratory specimen is transferable to a structure
                                                   Ic
                       only if the local crack-tip strain histories of the two configurations are similar. Equation (8.1)
                       applies only when yielding and nonlinear viscoelasticity are confined to a small region surrounding
                       the crack tip.
                          Under plane strain linear viscoelastic conditions, K  is related to the viscoelastic J integral J ,
                                                                                                     v
                                                                   I
                       as follows [1]:
                                                              2
                                                            K 1(  −ν 2 )
                                                        J =   I  E R                              (8.2)
                                                         v

                       where E  is a reference modulus, which is sometimes defined as the short-time relaxation modulus.
                             R
                                                                       2
                          Figure 8.1 illustrates a growing crack at times t  and t  + t .  Linear viscoelastic material surrounds
                                                                   o
                                                              o
                                                                      ρ
                       a Dugdale strip-yield zone, which is small compared to specimen dimensions. Consider a point A,
                       which is at the leading edge of the yield zone at t  and is at the trailing edge at t  + t . The size of
                                                                                       o
                                                               o
                                                                                           ρ
                       the yield zone and the crack-tip-opening displacement (CTOD) can be approximated as follows
                       (see Chapter 2 and Chapter 3):
                                                             π  K  2
                                                         ρ =    Ic                              (8.3)
                                                          c
                                                             8    σ 
                                                                 cr
                       and
                                                               K  2
                                                         δ ≈    Ic                                (8.4)
                                                          c
                                                             σ Et ()
                                                                  ρ
                                                              cr
                       where σ  is the crazing stress. Assume that crack extension occurs at a constant CTOD. The time
                             cr
                       interval t  is given by
                              ρ
                                                               ρ
                                                           t =  c                                 (8.5)
                                                            ρ
                                                               a ˙

                       2  This derivation, which was adapted from Marshall et al. [8], is only heuristic and approximate. Schapery [9] performed
                       a more rigorous analysis that led to a result that differs slightly from Equation (8.9).
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