NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A Damage Model for the Simulation of Delamination in Advanced Composites under Variable-Mode LoadingA 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.
Document ID
20080014292
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Turon, A.
(Girona Univ. Girona, Spain)
Camanho, P. P.
(Porto Univ. Portugal)
Costa, J.
(Girona Univ. Girona, Spain)
Davila, C. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2006
Publication Information
Publication: Mechanics of Materials
Volume: 38
Issue: 11
Subject Category
Composite Materials
Funding Number(s)
OTHER: 23-719-20-40-10
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available