Résumé:
The objective of this memory of magister's was the numerical modeling by a
finite element method the adhesive joint of two laminated composite plates using an
epoxy adhesive. The commercial software ABAQUS was used for modeling. Several
cases have been traited with include the effect of crack length and its angle
orientation on the stresses and strains, the second case concerns the influence of the
adhesive thickness on the stress states and deformations, the third is devoted to the
influence of plate thickness on the J integral, stress and strain. The numerical results
provided by the software Abaqus were then represented graphically both for the
stress, strain, and the integral J. These results were compared with those in the
literature.
