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contributor authorIzhak Sheinman
contributor authorYeoshua Frostig
date accessioned2017-05-08T23:26:30Z
date available2017-05-08T23:26:30Z
date copyrightSeptember, 1988
date issued1988
identifier issn0021-8936
identifier otherJAMCAV-26297#635_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103494
description abstractAn analytical-numerical procedure is applied to investigate the post-buckling behavior of a composite laminated stiffened panel. The panel is modeled by plate elements for which the nonlinear equations are derived (via a variational principle) in terms of the lateral displacement and Airy stress function, and treated by resolving the variables into eigenfunctions in conjunction with a finite-difference scheme.
publisherThe American Society of Mechanical Engineers (ASME)
titlePost-Buckling Analysis of Stiffened Laminated Panel
typeJournal Paper
journal volume55
journal issue3
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3125841
journal fristpage635
journal lastpage640
identifier eissn1528-9036
keywordsBuckling
keywordsDisplacement
keywordsNonlinear equations
keywordsComposite materials
keywordsStress
keywordsVariational principles AND Eigenfunctions
treeJournal of Applied Mechanics:;1988:;volume( 055 ):;issue: 003
contenttypeFulltext


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