A COMPUTATIONAL METHOD FOR DAMAGE INTENSITY PREDICTION IN A LAMINATED COMPOSITE STRUCTURE

The present study describes the basic principles of a general damage computational approach for laminates and demonstrates this approach's prediction capabilities in simulating the complete fracture phenomenon in the case of several tests, both with and without delamination. In this paper, the Damage Mechanics approach is applied in order to solve delamination problems, such as the propagation of an initiated crack, the onset of delamination near edges, and the growth of delamination around holes. For the M55J/M18 carbon/epoxy material, numerical simulations are presented and then compared with experimental results. Pierre Ladevèze, Olivier Allix, Bernard Douchin, and David Lévêque 2

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