The strength of laminated fiber-reinforced composite materials depends on the combination of the orientations of the stacked plies with respect to the applied loads and the state of the bonding between adjacent plies. Prior work has focused on developing forming simulations using Abaqus to track fiber orientations as a stack of fabric plies conforms to the shape of a mold. Knowing the final fiber orientations, cured composite properties can be defined to model the behavior of a resin-infused solid structural composite part. In this paper, a failure criterion and damage properties are investigated to model delaminations in composite parts. Delaminations due to Mode I failure are studied by testing unidirectional coupon specimens.
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