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    Discussion: “Zeroth-Order Shear Deformation Theory for Laminated Composite Plates” (Ray, M. C., 2003 ASME J. Appl. Mech., 70, pp. 374–380)

    Source: Journal of Applied Mechanics:;2004:;volume( 071 ):;issue: 004::page 594
    Author:
    S. Kapuria
    ,
    P. C. Dumir
    DOI: 10.1115/1.1769415
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is the contention of the authors that the “zeroth-order” shear deformation theory presented by Ray 1 is mathematically equivalent to Reddy’s third order theory 2. The notation of Ref. 1 is used herein. Ray’s approximations for the in-plane displacements u=u0−zw,x+3z2h−2z3h3 Qxλx, v=v0−zw,y+3z2h−2z3h3 QyλyDisplay Formulaare identical to those of the Reddy’s theory, 2, with Display Formulaψx+w,x=3Qx2hλx, ψy+w,y=3Qy2hλy.Hence the equations of motion and boundary conditions of Ray’s theory are mathematically equivalent to those of the dynamic version of Reddy’s theory. This is established explicitly by comparing the governing equations of the two theories.
    keyword(s): Composite materials , Plates (structures) AND Shear deformation ,
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      Discussion: “Zeroth-Order Shear Deformation Theory for Laminated Composite Plates” (Ray, M. C., 2003 ASME J. Appl. Mech., 70, pp. 374–380)

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    http://yetl.yabesh.ir/yetl1/handle/yetl/129469
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    contributor authorS. Kapuria
    contributor authorP. C. Dumir
    date accessioned2017-05-09T00:12:04Z
    date available2017-05-09T00:12:04Z
    date copyrightJuly, 2004
    date issued2004
    identifier issn0021-8936
    identifier otherJAMCAV-26580#594_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129469
    description abstractIt is the contention of the authors that the “zeroth-order” shear deformation theory presented by Ray 1 is mathematically equivalent to Reddy’s third order theory 2. The notation of Ref. 1 is used herein. Ray’s approximations for the in-plane displacements u=u0−zw,x+3z2h−2z3h3 Qxλx, v=v0−zw,y+3z2h−2z3h3 QyλyDisplay Formulaare identical to those of the Reddy’s theory, 2, with Display Formulaψx+w,x=3Qx2hλx, ψy+w,y=3Qy2hλy.Hence the equations of motion and boundary conditions of Ray’s theory are mathematically equivalent to those of the dynamic version of Reddy’s theory. This is established explicitly by comparing the governing equations of the two theories.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDiscussion: “Zeroth-Order Shear Deformation Theory for Laminated Composite Plates” (Ray, M. C., 2003 ASME J. Appl. Mech., 70, pp. 374–380)
    typeJournal Paper
    journal volume71
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.1769415
    journal fristpage594
    journal lastpage595
    identifier eissn1528-9036
    keywordsComposite materials
    keywordsPlates (structures) AND Shear deformation
    treeJournal of Applied Mechanics:;2004:;volume( 071 ):;issue: 004
    contenttypeFulltext
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