In this study Virtual testing was performed using both Abaqus/Standard and Abaqus/Explicit, using a dedicated user-defined material model developed at Fokker Landing Gear. In this material model the composite constituents (fibers and resin) are modelled as separate materials with their own specific material and failure behavior. The crucial interaction between the fibers and resin is accounted for using a new analytical approach. Damage between plies is accounted for using cohesive surfaces.
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