During the last twenty years, composite materials have gained great popularity in many applications such as aerospace, naval and wind turbines. Despite their wide use, the behaviour of composite materials still needs to be thoroughly investigated, especially during and after failure. Only a deep knowledge of these phenomena could maximize the benefit achieved by their use. Many failure criteria have been published in the last thirty years. Among them, the three-dimensional criteria (considering also the out of plane stress) have received particular attention. The present work has focused on the implementation of threedimensional failure criteria (Puck and Hashin 3D) in the commercial Finite Element program ABAQUS, using a USDFLD subroutine.
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