Page 179 - T. Anderson-Fracture Mechanics - Fundamentals and Applns.-CRC (2005)
P. 179

1656_C003.fm  Page 159  Monday, May 23, 2005  5:42 PM





                       Elastic-Plastic Fracture  Mechanics                                         159


                       By applying the same assumptions as in Equation (A3.15) and Equation (A3.16), we obtain:

                                                  ∂w  =  ∂w  ∂ε ij  = σ  ∂  u i
                                                                       ∂ 
                                                   ∂a  ∂ε ij  ∂a  ij  ∂ x  j    a            (A3.24)
                                                                       ∂ 

                       Invoking the principle of virtual work gives

                                                 ∫  A′  σ ij  ∂     u ∂   dA = ∫  Γ ′  T i  u ∂ a ∂  i  ds  (A3.25)
                                                            i
                                                       x ∂
                                                            a ∂ 
                                                        j
                       which cancels with one of the terms in the line integral in Equation (A3.23), resulting in the
                       following:

                                                   dΠ  = ∫  T  u ∂  i  ds − ∫  ∂ w  dA
                                                   da   Γ′  i  x ∂  A′  x ∂                     (A3.26)

                       Applying the divergence theorem and multiplying both sides by –1 leads to

                                                                  u
                                                  dΠ            ∂ 
                                                 −    =   ∫  −  wn  T  i  ds
                                                                   x
                                                   da    ′ Γ  x  i  ∂ 
                                                                                               (A3.26a)
                                                                 ∂u
                                                     =     ∫   wdy −  T i  i  ds  
                                                         ′ Γ      ∂x  
                       since n  ds = dy. Therefore, the J contour integral is equal to the energy release rate for a linear or
                            x
                       nonlinear elastic material under quasistatic conditions.

                       A3.4 THE HRR SINGULARITY

                       Hutchinson [7] and Rice and Rosengren [8] independently evaluated the character of crack-tip
                       stress fields in the case of power-law-hardening materials. Hutchinson evaluated both plane stress
                       and plane strain, while Rice and Rosengren considered only plane-strain conditions. Both articles,
                       which were published in the same issue of the Journal of the Mec hanics and Physics of Solids ,
                       argued that stress times strain varies as 1/r near the crack tip, although only Hutchinson was able
                       to provide a mathematical proof of this relationship.
                          The Hutchinson analysis is outlined below. Some of the details are omitted for brevity. We
                       focus instead on his overall approach and the ramifications of this analysis.
                          Hutchinson began by defining a stress function Φ for the problem. The governing differential
                       equation for deformation plasticity theory for a plane problem in a Ramberg-Osgood material is
                       more complicated than the linear elastic case:

                                                                    α
                                                    ∆Φ +  4  Φ σ (, , ,, )  = γ  0              (A3.27)
                                                                rn
                                                               e
                       where the function  g differs for plane stress and plane strain. For the Mode I crack problem,
                       Hutchinson chose to represent Φ in terms of an asymptotic expansion in the following form:

                                                    Φ= C    r () θ  s  + C  r () θ  t  +       (A3.28)
                                                        1       2
   174   175   176   177   178   179   180   181   182   183   184