Une methode simplifiee pour l'analyse du delaminage aupres d'un bord droit
Keywords:
laminates, damage, delamination, finite-elementsAbstract
A simplified method based upon damage mechanics for the delamination analysis of composites is presented. In the neighbourhood of a quasi-straight edge of a laminated structure, damage is taken concentrated on the interface between layers. The finite element code EDA, acting as a post-processor of an elastic laminate shell computation, allows the prediction of delamination onset and propagation. Numerical simulations of delamination are given and compared with experimental results from literature.
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