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    Torsional Response of Rectangular Composite Laminates

    Source: Journal of Applied Mechanics:;1990:;volume( 057 ):;issue: 002::page 383
    Author:
    C.-L. Tsai
    ,
    G. Yaniv
    ,
    I. M. Daniel
    DOI: 10.1115/1.2892001
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The 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.
    keyword(s): Composite materials , Laminates , Shear (Mechanics) , Graphite , Isotropy , Strain gages , Epoxy adhesives AND Torque ,
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      Torsional Response of Rectangular Composite Laminates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/106471
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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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