Progressive failure analysis of perforated aluminium/CFRP fibre metal laminates using a combined elastoplastic damage model and including delamination effects
In this work, a finite element (FE) model which includes in-ply and delamination damage effects is developed for progressive failure analyses of fibre–metal laminates (FMLs). The combined elastoplastic damage model recently developed by the authors is applied to represent the in-plane mechanical res...
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Veröffentlicht in: | Composite structures 2014-08, Vol.114, p.64-79 |
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Format: | Artikel |
Sprache: | eng |
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