Low velocity impact modeling in composite laminates capturing permanent indentation

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On cohesive element parameters and delamination modelling (2019, unknown): “5 × 10(4) Sun [65] IM7/8552 Impact 60/90 60/90 McElroy [87] IM7/8552 Impact 129/93 129/93 Bouvet [88] T700/M21 Impact 50/90 50/90 10(6) Hongkarnjanakul [41] T700/M21 Impact 60/110 60/110 Abir [42] T700/M21 Impact 75/150 75/150 10(6) Zhi [73] Hexcel 913C Impact 60/105/105 10(6) Su [39] IM7/8552 OHC 6”
Validation of low velocity impact modelling on different stacking sequences of CFRP laminates and influence of fibre failure (2013, methodology): “For FE modelling, an alternative method is to dissipate the energy release rate of fibre failure spreading over the volume finite element such as the modelling of [8] [1] [13] [12] [11].”
Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates (2015, unknown): “[11] and Hongkarnjanakul et al.”
Experimental and numerical studies on the impact response of damage-tolerant hybrid unidirectional/woven carbon-fibre reinforced composite laminates (2018, unknown): “These specimens were subsequently scanned using a C-scan system to obtain damage maps [7,8,24,31].”
Failure analysis of CFRP laminates subjected to compression after impact: FE simulation using discrete interface elements (2013, background): “The proof of the relevance of this modeling type has already been shown in previous works of the authors [24], and in the literature [32].”