The purpose of this paper consists in the implementation of a boundary element model for which the crack propagation is easily studied thanks to an automatic remeshing process. The traction singular quarter point element was used in order to improve the accuracy of the values of stress intensity factors. The Erdogan and Sih criterion allows us to determine the new growth direction after each step. Validity of this implement is demonstrated, with respect to experimental results, by the example of a holed plate. In this study, we can show the manner in which the crack may propagate when the distance between the initial crack's axis and the tangent hole is changed. Two distinct behaviours can be pointed out with respect to this distance : in some cases the crack may be simply deflected by the hole, and propagates across the plate until a complete fracture is reached. In other ones, the crack propagates toward and reaches the hole. In the framework of fatigue under cyclic loading, the manner in which growth rate is affected by the proximity of a hole is shown. INTRODUCTION The use of the Boundary Element Method for the solution of crack problems has been of interest to many investigators over recent years. However, for non-symetric problems where the two crack surfaces have the same geometrical coordinates, the direct application of this method leads to a singular system of equations. Some special techniques have been established to overcome this difficulty. The most general are the subregions method introduced by Blandford et al [1] and the dual bondary element method established by Portela et al [2]. In our study we have used the first method for the modelisation of the crack problems. We have shown [3] that the use of this method does not alter the automatization of crack propagation. Transactions on Engineering Sciences vol 6, © 1994 WIT Press, www.witpress.com, ISSN 1743-3533 376 Localized Damage THE BOUNDARY ELEMENT METHOD The boundary integral equation relates displacements i% and t< on the boundary F of an elastic homogeneous isotropic body. It can be written as : , Q)uj(Q)dT(Q) = f 0y (P, Q)ti(Q)dT(Q) (1) Jr In which the tensors T^ and Uij are the components number j of the tractions and displacements at Q due to a unit i direction load at P. The term Cij represents the behaviour of the singularity in Ty. When P is on a smoothpart of T, Cij = &,/2. Uj and tj denote components of the boundary displacement vector and the traction vector respectively. The boundary is now divided into N isoparametric elements. By using a collocation method, the system of equations is produced on the form : M {«}=[«]« (2) The matrices [A] and [J3] contain coefficients of either Tij and U . METHOD FOR THE CALCULATION OF STRESS INTENSITY FACTOR 'SIP' In order to evaluate correctly and accuratly the stress intensity factor, we have compared several methods like : the J Integral, Traction Singular Quarter Point Element (TSQP) and the Crack Opening Displacement method in which Kj is calculated for different formulations : Figure 1. Quarter point element /c = (3 — 4f/) for plane strain and =(3 — %/)/(! + %/) for plane stress In figure 2, we denote as follows : Quarter point elements and one-point displacement formula Quarter point elements and two point displacement formula Traction singular quarter-point elements and one-point displacement formula Traction singular quarter-point elements and two-point displacement formula Traction singular quarter-point elements and nodal value formula The extrapolation method of the displacement The crack size and the lenght of the element at crack tip KIUIS