Effect of resin and fibre properties on impact and compression after impact performance of CFRP

By D. Cartié, P. Irving. 2002

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Failure mechanisms and damage evolution of laminated composites under compression after impact (CAI): Experimental and numerical study (2018, background): “Comparing both layup configurations, the compressive strength reduction roughly scales linearly with the increasing delamination area, similar to the overall trend also reported by Cartie and Irving [12].”
Impact on composite structures (2004, methodology): “The delamination threshold load theoretically predicted by Davies and Robinson(1992) has been validated by numerous experimental studies, e.g. Davies et al(1994), Olsson et al(2000) and Cartié and Irving(2002).”
Improvement of low-velocity impact and compression-after-impact performance by z-fibre pinning (2006, background): “Given that E,ν, and GIIC are material constants, the critical impact force is proportional to the sample’s thickness at the order of t, which has been verified by experimental results [12-15].”
Damage in CFRPs due to low velocity impact at low temperature (2005, background): “The answers have led to a better understanding of the damage micromechanisms in impact loading conditions, related to the basic properties of resin, fibres, fibre matrix interfacing effects and the architecture of the laminate [2,3].”