Composite materials are widely used in both the defense and commercial sectors for various applications. Many of these applications present the possibility of the composite material being subjected to high-velocity impacts, where the strain rates can be on the order of 106 s-1 or more and the pressures are often in the tens of GPa. The work presented in this paper expands upon previous work for the same materials where the impacts were normal to the composite material [1] by considering the non-ideal condition of oblique impacts that are more likely to occur in regular use.

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