Article ID Journal Published Year Pages File Type
253185 Composite Structures 2010 9 Pages PDF
Abstract

The low velocity impact behavior of three layer thermoplastic laminates consisting of woven glass fiber and polypropylene has been investigated for two different fiber volume configurations. Panels with configurations of 50/50 and 20/80 in the warp and fill directions were subjected to low velocity impact energies between 4 and 16 J using an instrumented dropping weight impact tower. Load vs. displacement plots showed the excellent energy absorbing capabilities exhibited by the woven composites. Both configurations dissipated approximately 75% of the 16 J incident impact energy. An energy-balance model was used to successfully predict the impact response of the woven thermoplastic composites. The impact damaged plates were tested under four point bend (4 PB) loading conditions. Results showed a reduction in flexural strength and modulus as the impact energy increased. A simple compression molding damage repair process was applied to the 16 J impacted composite plates. 4 PB testing of the repaired samples revealed a significant recovery in the flexural strength and modulus of the thermoplastic woven composite with both fiber configurations.

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Physical Sciences and Engineering Engineering Civil and Structural Engineering
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