Page 227 - T. Anderson-Fracture Mechanics - Fundamentals and Applns.-CRC (2005)
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1656_C004.fm  Page 207  Thursday, April 21, 2005  5:38 PM





                       Dynamic and Time-Dependent Fracture                                         207

















                                                               FIGURE A4.1 Definition of coordinate axes for a
                                                               rapidly propagating crack. The X, Y axes are fixed in
                                                               space and the x, y axes are attached to the crack tip.


                          Consider rapid crack propagation in a body subject to plane strain loading. Let us define a
                       fixed coordinate axis X-Y with an origin on the crack plane at a(t) = 0, as illustrated in Figure A4.1.
                       It is convenient at this point to introduce two displacement potentials, defined by

                                                   ∂ψ   ∂ψ           ∂ψ    ∂ψ
                                              u =  ∂ X  1  +  ∂ Y  2  ,  u =  ∂ Y  1  −  ∂ X  2  (A4.3)
                                               X
                                                                  Y
                       Substituting Equation (A4.3) into Equation (A4.2) leads to
                                                      ∂ ψ  2  1  +  ∂ ψ  2  1  =  1
                                                       ∂ X  2  ∂ Y  2  c  2  ψ ˙˙ 1             (A4.4a)
                                                                   1

                       and
                                                      ∂ ψ  2  2  +  ∂ ψ  2  2  =  1
                                                      ∂X  2  ∂Y  2  c  2  ψ ˙˙ 2                (A4.4b)
                                                                   2

                       since the wave speeds are given by
                                                        λ  + µ        µ
                                                     c =     ,    c =
                                                                   2
                                                      2
                                                     1    ρ        2  ρ
                       for plane strain. Thus ψ  and ψ  are the longitudinal and shear wave potentials, respectively. The
                                          1
                                                2
                       stresses can be written in terms of ψ  and ψ  by invoking Equation (A2.1) and Equation (A2.2):
                                                    1
                                                           2
                                                                ∂  2 ψ  ∂ 2 ψ  
                                              σ  XX  +  σ  YY  λ =  +  µ 2(  )    ∂ X  2 1  +  ∂ Y  2 1     (A4.5a)

                                                           ∂ 2 ψ  ∂ 2 ψ  ∂ 2 ψ 
                                                                            2
                                              σ  XX −  σ  YY  2 µ =     ∂ X  2 1  −  ∂ Y  2 1  + 2  X  Y ∂∂    (A4.5b)

                                                          ∂ 2 ψ  ∂ 2 ψ  ∂ 2 ψ 
                                                                           1
                                                  τ  XY  =  µ     ∂ Y  2 2  −  ∂ X  2 2  + 2  X  Y ∂∂    (A4.5c)
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