NASA NTRS · 20080014292
A Damage Model for the Simulation of Delamination in Advanced Composites under Variable-Mode Loading
Abstract
A thermodynamically consistent damage model is proposed for the simulation of progressive delamination in composite materials under variable-mode ratio. The model is formulated in the context of Damage Mechanics. A novel constitutive equation is developed to model the initiation and propagation of delamination. A delamination initiation criterion is proposed to assure that the formulation can account for changes in the loading mode in a thermodynamically consistent way. The formulation accounts for crack closure effects to avoid interfacial penetration of two adjacent layers after complete decohesion. The model is implemented in a finite element formulation, and the numerical predictions are compared with experimental results obtained in both composite test specimens and structural components.
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Turon, A., Camanho, P. P., Costa, J., Davila, C. G.. 2006-01-01. A Damage Model for the Simulation of Delamination in Advanced Composites under Variable-Mode Loading. https://ntrs.nasa.gov/citations/20080014292
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