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    A Laminated Plate Model of an Adhesive-Bonded Taper-Taper Joint Under Tension

    Source: Journal of Engineering Materials and Technology:;1997:;volume( 119 ):;issue: 004::page 408
    Author:
    Jack E. Helms
    ,
    Chihdar Yang
    ,
    Su-Seng Pang
    DOI: 10.1115/1.2812277
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analytical model of the strain and stress distributions in a taper-taper adhesive-bonded joint between two composite flat plates has been developed using first-order laminated plate theory. A correction for transverse shear deformation effects was included. The model was derived under the assumption of plane strain in the adherends and consists of eighteen first-order, linear, coupled ordinary differential equations with variable coefficients. The model was solved numerically using the Linear Shooting Method. Finite element models were also developed to verify the results of the analytical model using the COSMOS/M commercial software package.
    keyword(s): Adhesives , Tension , Universe , Composite materials , Stress , Differential equations , Computer software , Finite element model , Flat plates , Plane strain AND Shear deformation ,
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      A Laminated Plate Model of an Adhesive-Bonded Taper-Taper Joint Under Tension

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/118764
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    contributor authorJack E. Helms
    contributor authorChihdar Yang
    contributor authorSu-Seng Pang
    date accessioned2017-05-08T23:53:36Z
    date available2017-05-08T23:53:36Z
    date copyrightOctober, 1997
    date issued1997
    identifier issn0094-4289
    identifier otherJEMTA8-26988#408_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118764
    description abstractAn analytical model of the strain and stress distributions in a taper-taper adhesive-bonded joint between two composite flat plates has been developed using first-order laminated plate theory. A correction for transverse shear deformation effects was included. The model was derived under the assumption of plane strain in the adherends and consists of eighteen first-order, linear, coupled ordinary differential equations with variable coefficients. The model was solved numerically using the Linear Shooting Method. Finite element models were also developed to verify the results of the analytical model using the COSMOS/M commercial software package.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Laminated Plate Model of an Adhesive-Bonded Taper-Taper Joint Under Tension
    typeJournal Paper
    journal volume119
    journal issue4
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.2812277
    journal fristpage408
    journal lastpage414
    identifier eissn1528-8889
    keywordsAdhesives
    keywordsTension
    keywordsUniverse
    keywordsComposite materials
    keywordsStress
    keywordsDifferential equations
    keywordsComputer software
    keywordsFinite element model
    keywordsFlat plates
    keywordsPlane strain AND Shear deformation
    treeJournal of Engineering Materials and Technology:;1997:;volume( 119 ):;issue: 004
    contenttypeFulltext
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