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Computational Simulation of Composite Structural FatigueProgressive damage and fracture of composite structures subjected to monotonically increasing static, tension-tension cyclic, pressurization, and flexural cyclic loading are evaluated via computational simulation. Constituent material properties, stress and strain limits are scaled up to the structure level to evaluate the overall damage and fracture propagation for composites. Damage initiation, growth, accumulation, and propagation to fracture due to monotonically increasing static and cyclic loads are included in the simulations. Results show the number of cycles to failure at different temperatures and the damage progression sequence during different degradation stages. 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
20050161949
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Minnetyan, Levon
(Clarkson Univ. Potsdam, NY, United States)
Chamis, Christos C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
February 1, 2005
Subject Category
Composite Materials
Report/Patent Number
NASA/CR-2005-213573
E-15018
Report Number: NASA/CR-2005-213573
Report Number: E-15018
Funding Number(s)
CONTRACT_GRANT: NAG3-2609
WBS: WBS 22-066-30-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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