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contributor authorK. K. Shukla
contributor authorY. Nath
date accessioned2017-05-09T00:06:36Z
date available2017-05-09T00:06:36Z
date copyrightSeptember, 2002
date issued2002
identifier issn0021-8936
identifier otherJAMCAV-26543#684_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126249
description abstractThis paper deals with the nonlinear dynamic buckling of laminated composite rectangular plates subjected to uniform time-dependent in-plane temperature-induced loading. The dynamic post-buckling deflection response is obtained and dynamic critical temperatures are estimated. The nonlinear governing equations of motion are solved analytically using fast Chebyshev series technique. The numerical results for CCCC, CCCS, CCSS, CSCS, CSSS and SSSS boundary conditions are presented.
publisherThe American Society of Mechanical Engineers (ASME)
titleBuckling of Laminated Composite Rectangular Plates Under Transient Thermal Loading
typeJournal Paper
journal volume69
journal issue5
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.1485755
journal fristpage684
journal lastpage692
identifier eissn1528-9036
keywordsTemperature
keywordsComposite materials
keywordsPlates (structures)
keywordsBuckling
keywordsDisplacement
keywordsDeflection
keywordsBoundary-value problems AND Equations of motion
treeJournal of Applied Mechanics:;2002:;volume( 069 ):;issue: 005
contenttypeFulltext


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