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Nonlinear temperature dependent failure analysis of finite width composite laminatesA quasi-three dimensional, nonlinear elastic finite element stress analysis of finite width composite laminates including curing stresses is presented. Cross-ply, angle-ply, and two quasi-isotropic graphite/epoxy laminates are studied. Curing stresses are calculated using temperature dependent elastic properties that are input as percent retention curves, and stresses due to mechanical loading in the form of an axial strain are calculated using tangent modulii obtained by Ramberg-Osgood parameters. It is shown that curing stresses and stresses due to tensile loading are significant as edge effects in all types of laminate studies. The tensor polynomial failure criterion is used to predict the initiation of failure. The mode of failure is predicted by examining individual stress contributions to the tensor polynomial.
Document ID
19800013922
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nagarkar, A. P.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Herakovich, C. T.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
August 10, 2013
Publication Date
December 1, 1979
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-162868
VPI-E-79-36
Report Number: NASA-CR-162868
Report Number: VPI-E-79-36
Accession Number
80N22409
Funding Number(s)
CONTRACT_GRANT: NSG-1250
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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