Prediction of impact damage in composite plates

By J. Hou, Nik Petrinic, C. Ruiz, S. Hallett. 2000

460 citations recorded by the source corpus.

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Experimental and numerical analysis of normal and oblique ballistic impacts on thin carbon/epoxy woven laminates (2008, methodology): “The material model used for the carbon/epoxy woven laminate derives from the Chang Chang model [32], which has been used widely in the literature [30,33,34].”
Assessment of failure criteria and damage evolution methods for composite laminates under low-velocity impact (2019, methodology): “6 Tsai–Wu [8], Hashin [9], Hou [11,12] and Puck [13] criteria, combined with linear degradation models, are integrated and implemented using the VUMAT subroutine in ABAQUS and are validated against the experimental results reported by Hongkarnjanakul et al.”
A model to predict low-velocity impact response and damage in sandwich composites (2008, background): “account for nonlinear material behaviour can also be used to predict impact response of composite structures [12–14].”
Modelling of composite sandwich structures with honeycomb core subjected to high-velocity impact (2010, methodology): “The skins were modelled as laminates applying the Hou cri teria [13] for the prediction of the failure, and the honeycomb core was modelled reproducing the aluminium hexagonal cells.”