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contributor authorC.-L. Tsai
contributor authorG. Yaniv
contributor authorI. M. Daniel
date accessioned2017-05-08T23:31:52Z
date available2017-05-08T23:31:52Z
date copyrightJune, 1990
date issued1990
identifier issn0021-8936
identifier otherJAMCAV-26321#383_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106471
description abstractThe torsional response of a composite laminate of rectangular cross-section was analyzed by the Mindlin-Reissner theory. The analysis takes into account separately the shear properties of each layer. A general closed-form relationship was derived between torque and angle of twist in terms of the geometric parameters and shear properties of the laminae. In the case of unidirectional laminates, relations can be expressed involving the three principal shear moduli, G 12 , G 13 , and G 23 . An experimental method was also developed for determining these moduli by measuring surface and edge strains with strain gages. Results for a typical graphite/epoxy composite show the validity of the usual assumption of transverse isotropy.
publisherThe American Society of Mechanical Engineers (ASME)
titleTorsional Response of Rectangular Composite Laminates
typeJournal Paper
journal volume57
journal issue2
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.2892001
journal fristpage383
journal lastpage387
identifier eissn1528-9036
keywordsComposite materials
keywordsLaminates
keywordsShear (Mechanics)
keywordsGraphite
keywordsIsotropy
keywordsStrain gages
keywordsEpoxy adhesives AND Torque
treeJournal of Applied Mechanics:;1990:;volume( 057 ):;issue: 002
contenttypeFulltext


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