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contributor authorRosalin Sahoo
contributor authorB. N. Singh
date accessioned2017-05-08T22:08:41Z
date available2017-05-08T22:08:41Z
date copyrightJuly 2015
date issued2015
identifier other32949703.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/72235
description abstractThe present study deals with the dynamic stability behavior of laminated composite and sandwich plates subjected to in-plane static and periodic compressive loads based on a recently developed inverse hyperbolic zigzag theory by the authors. The present model satisfies the traction-free boundary conditions on the surfaces of the plate and interlaminar continuity conditions at the layer interfaces, thus obviating the need for a shear correction factor. An efficient
publisherAmerican Society of Civil Engineers
titleDynamic Instability of Laminated Composite and Sandwich Plates Using a New Inverse Hyperbolic Zigzag Theory
typeJournal Paper
journal volume28
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000440
treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 004
contenttypeFulltext


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