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This paper reports both experimental and numerical investigations on delamination mechanisms in [05, 905, 05] carbon fiber(CF)/poly(etheretherketone) (PEEK) laminate subjected to low‐velocity impact. It was found that the CF/PEEK composite exhibits the same damage mechanisms as epoxy‐based composites, but superior delamination resistance. For the crossply laminate, the impact delamination results from a Mode II interlaminar fracture process, and a close association exists between the interlaminar shear stress field and the delamination growth. The prediction of impact‐induced delamination sizes is discussed.
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Wang et al. (1991) studied this question.
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