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contributor authorS. Kapuria
contributor authorP. C. Dumir
date accessioned2017-05-09T00:12:04Z
date available2017-05-09T00:12:04Z
date copyrightJuly, 2004
date issued2004
identifier issn0021-8936
identifier otherJAMCAV-26580#594_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129469
description abstractIt is the contention of the authors that the “zeroth-order” shear deformation theory presented by Ray 1 is mathematically equivalent to Reddy’s third order theory 2. The notation of Ref. 1 is used herein. Ray’s approximations for the in-plane displacements u=u0−zw,x+3z2h−2z3h3 Qxλx, v=v0−zw,y+3z2h−2z3h3 QyλyDisplay Formulaare identical to those of the Reddy’s theory, 2, with Display Formulaψx+w,x=3Qx2hλx, ψy+w,y=3Qy2hλy.Hence the equations of motion and boundary conditions of Ray’s theory are mathematically equivalent to those of the dynamic version of Reddy’s theory. This is established explicitly by comparing the governing equations of the two theories.
publisherThe American Society of Mechanical Engineers (ASME)
titleDiscussion: “Zeroth-Order Shear Deformation Theory for Laminated Composite Plates” (Ray, M. C., 2003 ASME J. Appl. Mech., 70, pp. 374–380)
typeJournal Paper
journal volume71
journal issue4
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.1769415
journal fristpage594
journal lastpage595
identifier eissn1528-9036
keywordsComposite materials
keywordsPlates (structures) AND Shear deformation
treeJournal of Applied Mechanics:;2004:;volume( 071 ):;issue: 004
contenttypeFulltext


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