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contributor authorJ. N. Reddy
date accessioned2017-05-08T23:16:54Z
date available2017-05-08T23:16:54Z
date copyrightDecember, 1984
date issued1984
identifier issn0021-8936
identifier otherJAMCAV-26244#745_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97909
description abstractA higher-order shear deformation theory of laminated composite plates is developed. The theory contains the same dependent unknowns as in the first-order shear deformation theory of Whitney and Pagano [6], but accounts for parabolic distribution of the transverse shear strains through the thickness of the plate. Exact closed-form solutions of symmetric cross-ply laminates are obtained and the results are compared with three-dimensional elasticity solutions and first-order shear deformation theory solutions. The present theory predicts the deflections and stresses more accurately when compared to the first-order theory.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Simple Higher-Order Theory for Laminated Composite Plates
typeJournal Paper
journal volume51
journal issue4
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3167719
journal fristpage745
journal lastpage752
identifier eissn1528-9036
keywordsComposite materials
keywordsPlates (structures)
keywordsShear deformation
keywordsThickness
keywordsDeflection
keywordsLaminates
keywordsStress
keywordsShear (Mechanics) AND Elasticity
treeJournal of Applied Mechanics:;1984:;volume( 051 ):;issue: 004
contenttypeFulltext


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