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Initial postbuckling response of anisotropic laminated rectangular platesIt has been shown that anisotropic plates can have unstable postbuckling behavior resulting in potential imperfection sensitivity. The present paper quantifies the degree of instability for rectangular, simply supported asymmetrically laminated plates. 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 unless the lamination asymmetry is very pronounced.
Document ID
19920051678
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johnson, Eric R.
(NASA Langley Research Center Hampton, VA, United States)
Haftka, Raphael T.
(Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 92-2284
Report Number: AIAA PAPER 92-2284
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Dallas, TX
Country: United States
Start Date: April 13, 1992
End Date: April 15, 1992
Accession Number
92A34302
Funding Number(s)
CONTRACT_GRANT: NAG1-537
CONTRACT_GRANT: NAG1-168
Distribution Limits
Public
Copyright
Other

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