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contributor authorT. Y. Kam
contributor authorR. R. Chang
date accessioned2017-05-08T23:41:13Z
date available2017-05-08T23:41:13Z
date copyrightMarch, 1993
date issued1993
identifier issn0195-0738
identifier otherJERTD2-26448#41_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111854
description abstractA shear deformable finite element is developed for the analysis of thick laminated composite plates. The finite element formulation is based on Mindlin’s plate theory in which shear correction factors are derived from the exact expressions for orthotropic materials. The element is used to solve a variety of problems on deflection, stress distribution, natural frequency and buckling of laminated composite plates. The effects of material properties, plate aspect ratio, length-to-thickness ratio, number of layers and lamination angle on the mechanical behaviors of laminated composite plates are investigated. Optimal lamination arrangements of layers for laminated composite plates of particular applications are determined.
publisherThe American Society of Mechanical Engineers (ASME)
titleFinite Element Analysis of Shear Deformable Laminated Composite Plates
typeJournal Paper
journal volume115
journal issue1
journal titleJournal of Energy Resources Technology
identifier doi10.1115/1.2905968
journal fristpage41
journal lastpage46
identifier eissn1528-8994
keywordsComposite materials
keywordsShear (Mechanics)
keywordsFinite element analysis
keywordsPlates (structures)
keywordsLaminations
keywordsThickness
keywordsBuckling
keywordsDeflection
keywordsMechanical behavior
keywordsStress concentration AND Materials properties
treeJournal of Energy Resources Technology:;1993:;volume( 115 ):;issue: 001
contenttypeFulltext


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