Impact and compression after impact experimental study of a composite laminate with a cork thermal shield

By Sandrine Petit, C. Bouvet, A. Bergerot, J. Barrau. 2007

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Low velocity impact modeling in composite laminates capturing permanent indentation (2012, unknown): “Impact damage in laminate with UD reinforcement: (a) different damage types [7], (b) damage photographs [5], and (c) diagram of the principle of interaction between intra- and inter-laminar damage [11].”
Low velocity impact modelling in laminate composite panels with discrete interface elements (2009, methodology): “Among the numerous experimental investigations in the literature (Aoki et al., 2006; Davies and Olsson, 2004; Petit et al., 2007; Kwon and Sankar, 1993 . . .), Aboissiere’s work (2002, 2003) was used to set this model because of the following interests: Firstly, the main stacking sequence used in…”
Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates (2015, background): “CAI tests were also performed to investigate the residual strength of a composite laminate with a cork thermal shield [15] , assess the effectivenss of self-healing composites in recovering CAI strength [16] and compare the influence of matrix toughness using thermoset and thermoplastic resins on CA”
Failure analysis of CFRP laminates subjected to compression after impact: FE simulation using discrete interface elements (2013, background): “A significant number of studies about the impact behavior of composite laminates are available in the literature, both experimentally [1,5,6] and numerically [1,7,8].”