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Multi-Functional Composite FatigueDamage and fracture of composites subjected to monotonically increasing static, tension-tension cyclic, pressurization, and flexural cyclic loading are evaluated via a recently developed composite mechanics code that allows the user to focus on composite response at infinitely small scales. Constituent material properties, stress and strain limits are scaled up to the laminate level to evaluate the overall damage and durability. Results show the number of cycles to failure at different temperatures. A procedure is outlined for use of computational simulation data in the assessment of damage tolerance, determination of sensitive parameters affecting fracture, and interpretation of results with insight for design decisions.
Document ID
20080034820
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Minnetyan, Levon
(Clarkson Univ. Potsdam, NY, United States)
Chamis, Christos C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
September 9, 2008
Subject Category
Composite Materials
Funding Number(s)
WBS: WBS 526282.03.02.02.04
Distribution Limits
Public
Copyright
Public Use Permitted.
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