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contributor authorC. T. Sun
date accessioned2017-05-09T01:36:03Z
date available2017-05-09T01:36:03Z
date copyrightMarch, 1973
date issued1973
identifier issn0021-8936
identifier otherJAMCAV-25974#193_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163573
description abstractPlate equations for the incremental deformation in composite plates with orthotropic constituent layers are derived according to Trefftz’s formulation for elastic bodies under initial stress. The plate theory thus derived includes the microdeformation which can account for the heterogeneity of the plate. Flexural wave propagation under initial stress and buckling of a simply supported rectangular composite plate are investigated. In a special case of harmonic wave propagation in a free composite plate dispersion curves predicted by the plate equations are compared with the exact curve. Good agreement is observed for the complete plate theory and Approximation I, while the adequacy of the other two sets of simplified equations, Approximations II and III, depends vitally on the ratio of the transverse shear rigidities of the constituent materials.
publisherThe American Society of Mechanical Engineers (ASME)
titleIncremental Deformations in Orthotropic Laminated Plates Under Initial Stress
typeJournal Paper
journal volume40
journal issue1
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3422924
journal fristpage193
journal lastpage200
identifier eissn1528-9036
keywordsDeformation
keywordsStress
keywordsPlates (structures)
keywordsComposite materials
keywordsEquations
keywordsApproximation
keywordsWave propagation
keywordsShear (Mechanics) AND Buckling
treeJournal of Applied Mechanics:;1973:;volume( 040 ):;issue: 001
contenttypeFulltext


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