Center for Composite Materials - University of Delaware

Example 3:
Sphere Impact on Elliptical Carbon/Epoxy Tube



Impact on aircraft structure with curved surfaces require modeling with unidirectional carbon/epoxy composites. Materials Sciences Corporation has developed a set of carbon/epoxy unidirectional composites and are in the process of optimizing the MAT162 modeling parameters. In conducting parametric simulations an edge clamped elliptical tube of length 500mm and major and minor axis of 254mm and 152mm, respectively, has been meshed with 5mm mesh everywhere except at the impact point where the mesh size is 2.5mm. A steel sphere of 20mm diameter has been impacted with a velocity vector [Vx, Vy, Vz] = [+25, +25, -100] m/s. Four sub-laminates of thickness 0.500mm is stacked in the sequence [+45/-45/+45/-45] to obtain the total thickness of 2mm. Each sub-laminate has one element through the thickness and has been assigned an unique part number with respective material orientation in defining 3 potential delamination plane.

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