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350                  c. CAL~ R. CITARELLA AND M PERRELLA


             Three dimensional simulation: theoretical aspects and results.
             Surface crack solutions are widely used  in applications of fracture mechanics to fatigue and
            monotonic loading.  A  semi-elliptical  surface crack  lying  perpendicular to  the  surface and
             subject to applied stresses with no  shear component parallel to the crack, experience mode I
             conditions  around  its  edge,  as  in  the  problem  presented  in  the  following. Generally this
             orientation is the critical one, also in mixed mode conditions if the fatigue crack threshold  is
             governed by (AG I)W, where G is the energy release rate.


             The dual boundary element method. BEASY uses dual elements for 3D crack growth analysis.
             The dual boundary element method (DBEM) incorporates two independent boundary integral
             equations: the  displacement equation  applied  at  the  collocation point  on  one  of  the  crack
             surfaces and the traction equation on the other surface. Application of the DBEM to three-
             dimensional crack growth analysis has been presented in [ 1 1-1 31.
             In the absence of body force, the displacement boundary equation can be written as:

                    cIJ(xI).u,(xI)+ ~~,(x~,x).u,(x').(rr(x) lu,(.',x).t,(x').~(x)
                                                =
                               r                  r
             where iJ denote Cartesian components, r, (x 'J) and Uv(x 'J) represent the Kelvin traction and

             displacement fundamental solutions at a boundary point x, respectively. The symbol   stands
             for the Cauchy principal value integral.
               Assuming  continuity of both  strains and  traction at x' on  a  smooth boundary,  the  stress
             components  G,, are given by:






             where Tkv (x 'J) and uk,(x 'J) contain derivatives of z,  (x f) and uv(x 'T), respectively.
               The symbol   stands for the Hadamard principal value integral. The traction components 6

             are given by:






             where n, (x ') denotes the component of outward unit normal to the boundary at x '.
             Equations (2) and (4)  constitute the basis of DBEM. A more complete description is given in
             u11.
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