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Initial postbuckling response of an unsymmetrically laminated rectangular plateIt was shown that anisotropic plates can have unstable postbuckling behavior resulting in potential imperfection sensitivity. The degree of instability for rectangular, simply-supported, cross-ply laminated plates is quantified. The analysis is based on asymptotic Koiter-type expansion of postbuckling response. The degree of postbuckling instability is quantified in terms of the reduction in load carrying capacity in the immediate postbuckling range. For graphite-epoxy plates it is found that this measure of instability is very small. Only a low aspect ratio plate with a high degree of anisotropy can have any significant reduction in its buckling load.
Document ID
19920023342
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Haftka, Raphael T.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Johnson, Eric R.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1990
Publication Information
Publication: NASA. Langley Research Center, Eighth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Part 2
Subject Category
Composite Materials
Accession Number
92N32586
Funding Number(s)
CONTRACT_GRANT: NAG1-537
CONTRACT_GRANT: NAG1-168
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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