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    A Damage Model for Adhesively Bonded Single-Lap Thick Composite Joints

    Source: Journal of Engineering Materials and Technology:;2012:;volume( 134 ):;issue: 004::page 41004
    Author:
    Sayed A. Nassar
    ,
    Douglas Templeton
    ,
    Jianghui Mao
    ,
    Xianjie Yang
    DOI: 10.1115/1.4006821
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A proposed damage model is used for investigating the deformation and interfacial failure behavior of an adhesively bonded single-lap thick joint made of S2 glass/SC-15 epoxy resin composite material. The bonding material is 3M Scotch-Weld Epoxy Adhesive DP405 Black. Continuum damage mechanics models are used to describe the damage initiation and final failure at or near the interface. The effect of adhesive overlap length, thickness, and plasticity on the interfacial shear and normal stresses is studied. Experimental and analytical data are used to validate the proposed damage models.
    keyword(s): Deformation , Composite materials , Adhesives , Stress , Shear (Mechanics) , Failure , Thickness , Bonding AND Plasticity ,
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      A Damage Model for Adhesively Bonded Single-Lap Thick Composite Joints

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/148955
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    • Journal of Engineering Materials and Technology

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    contributor authorSayed A. Nassar
    contributor authorDouglas Templeton
    contributor authorJianghui Mao
    contributor authorXianjie Yang
    date accessioned2017-05-09T00:50:43Z
    date available2017-05-09T00:50:43Z
    date copyrightOctober, 2012
    date issued2012
    identifier issn0094-4289
    identifier otherJEMTA8-926030#041004_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148955
    description abstractA proposed damage model is used for investigating the deformation and interfacial failure behavior of an adhesively bonded single-lap thick joint made of S2 glass/SC-15 epoxy resin composite material. The bonding material is 3M Scotch-Weld Epoxy Adhesive DP405 Black. Continuum damage mechanics models are used to describe the damage initiation and final failure at or near the interface. The effect of adhesive overlap length, thickness, and plasticity on the interfacial shear and normal stresses is studied. Experimental and analytical data are used to validate the proposed damage models.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Damage Model for Adhesively Bonded Single-Lap Thick Composite Joints
    typeJournal Paper
    journal volume134
    journal issue4
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.4006821
    journal fristpage41004
    identifier eissn1528-8889
    keywordsDeformation
    keywordsComposite materials
    keywordsAdhesives
    keywordsStress
    keywordsShear (Mechanics)
    keywordsFailure
    keywordsThickness
    keywordsBonding AND Plasticity
    treeJournal of Engineering Materials and Technology:;2012:;volume( 134 ):;issue: 004
    contenttypeFulltext
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