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Modeling Quasi-Static and Fatigue-Driven Delamination MigrationAn approach was proposed and assessed for the high-fidelity modeling of progressive damage and failure in composite materials. It combines the Floating Node Method (FNM) and the Virtual Crack Closure Technique (VCCT) to represent multiple interacting failure mechanisms in a mesh-independent fashion. Delamination, matrix cracking, and migration were captured failure and migration criteria based on fracture mechanics. Quasi-static and fatigue loading were modeled within the same overall framework. The methodology proposed was illustrated by simulating the delamination migration test, showing good agreement with the available experimental data.
Document ID
20140016386
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
De Carvalho, N. V.
(National Inst. of Aerospace Hampton, VA, United States)
Ratcliffe, J. G.
(NASA Langley Research Center Hampton, VA, United States)
Chen, B. Y.
(Imperial Coll. of London London, United Kingdom)
Pinho, S. T.
(Imperial Coll. of London London, United Kingdom)
Baiz, P. M.
(Imperial Coll. of London London, United Kingdom)
Tay, T. E.
(National Univ. of Singapore Singapore)
Date Acquired
November 17, 2014
Publication Date
September 8, 2014
Subject Category
Composite Materials
Report/Patent Number
NF1676L-18069
Report Number: NF1676L-18069
Funding Number(s)
WBS: WBS 794072.02.07.03.03.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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