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contributor authorY. R. Wang
contributor authorT.-W. Chou
date accessioned2017-05-08T23:40:33Z
date available2017-05-08T23:40:33Z
date copyrightJune, 1993
date issued1993
identifier issn0021-8936
identifier otherJAMCAV-26349#560_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111472
description abstractThe first-order perturbation analysis of the three-dimensional transient interlaminar thermal stresses of a symmetric composite laminate has been performed in this paper. Numerical results for a four-layer angle-ply laminate have shown that the first-order analysis was necessary for the solution of thick laminate (thickness-to-width ratio ε ≥ 0.02).
publisherThe American Society of Mechanical Engineers (ASME)
titleFirst-Order Perturbation Analysis of Transient Interlaminar Thermal Stress in Composites
typeJournal Paper
journal volume60
journal issue2
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.2900832
journal fristpage560
journal lastpage563
identifier eissn1528-9036
keywordsComposite materials
keywordsThermal stresses
keywordsLaminates AND Thickness
treeJournal of Applied Mechanics:;1993:;volume( 060 ):;issue: 002
contenttypeFulltext


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