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Interlaminar shear stress effects on the postbuckling response of graphite-epoxy panelsThe objectives of the study are to assess the influence of shear flexibility on overall postbuckling response, and to examine transverse shear stress distributions in relation to panel failure. Nonlinear postbuckling results are obtained for finite element models based on classical laminated plate theory and first-order shear deformation theory. Good correlation between test and analysis is obtained. The results presented in this paper analytically substantiate the experimentally observed failure mode.
Document ID
19900046255
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Engelstad, S. P.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Reddy, J. N.
(Virginia Polytechnic Institute and State University Blacksburg, United States)
Knight, N. F., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Structural Mechanics
Accession Number
90A33310
Funding Number(s)
CONTRACT_GRANT: NAG1-1030
CONTRACT_GRANT: NAG1-1085
Distribution Limits
Public
Copyright
Other

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