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contributor authorNikhil Garg
contributor authorKarkhanis Rahul Sanjay
contributor authorRosalin Sahoo
contributor authorP. R. Maiti
contributor authorB. N. Singh
date accessioned2022-01-30T21:40:50Z
date available2022-01-30T21:40:50Z
date issued9/1/2020 12:00:00 AM
identifier other%28ASCE%29AS.1943-5525.0001177.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4268653
description abstractIn the present work, the hygro-thermomechanical response on the static characteristics of symmetric and antisymmetric laminated composite and sandwich plates is obtained using the recently developed inverse hyperbolic zigzag theory (IHZZT). The framework of IHZZT inculcates the shear strain shape function assuming a nonlinear distribution of transverse shear stresses. It satisfies the necessary conditions of interlaminar stress continuity at the layer interfaces as well as the condition of zero transverse shear stresses at the top and bottom surfaces of the plates. The theory has seven unknown field variables, which are layer-independent. The displacement-based finite-element approach is employed, using the eight-noded isoparametric serendipity element, accounting for the C0 continuity. A number of numerical examples are solved considering the effect of temperature, moisture concentration, span-thickness ratio, aspect ratio, boundary conditions, loading conditions, and variations in the number of layers. The results obtained in terms of deflections and stresses are validated with the exact results and results available in the existing literature. A few new results are produced here to establish a benchmark study for future research.
publisherASCE
titleAssessment of Inverse Hyperbolic Zigzag Theory for Hygro-Thermomechanical Analysis of Laminated Composite and Sandwich Plates
typeJournal Paper
journal volume33
journal issue5
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0001177
page16
treeJournal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 005
contenttypeFulltext


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