Abstract
The damage tolerance of thick S-2 glass-fabric reinforced polyester, vinylester, and epoxy matrix composite panels subjected to ballistic impact loading has been examined. The damage shape and size was examined using ultrasonic NDE. After inspection of the damage, residual compression strength of the impacted panels was measured. The hand laid-up glass-polyester composite suffered from a large damage size, and low strength in compression after ballistic impact (CABI). The glass-vinylester and glass-epoxy panels manufactured using the SCRIMP process showed small damage sizes and high residual strengths. Through-thickness stitching of glass-vinylester and glass-epoxy panels was found to reduce the impact damage size, but the difference was quite small and did not translate into a substantial strength increase. The performance of panels with a ceramic tile bonded at the impact site was also examined. Model predictions of the CABI strength based on compression failure at the net section are compared to measured data, and implications for design of damage tolerant materials are discussed.
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