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dc.contributor.authorSayed A. Nassar
dc.contributor.authorDouglas Templeton
dc.contributor.authorJianghui Mao
dc.contributor.authorXianjie Yang
dc.date.accessioned2017-05-09T00:50:43Z
dc.date.available2017-05-09T00:50:43Z
dc.date.copyrightOctober, 2012
dc.date.issued2012
dc.identifier.issn0094-4289
dc.identifier.otherJEMTA8-926030#041004_1.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl/handle/yetl/148955
dc.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.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleA Damage Model for Adhesively Bonded Single-Lap Thick Composite Joints
dc.typeJournal Paper
dc.journal.volume134
dc.journal.issue4
dc.journal.titleJournal of Engineering Materials and Technology
dc.identifier.doi10.1115/1.4006821
dc.journal.fristpage41004
dc.identifier.eissn1528-8889
dc.keywordsDeformation
dc.keywordsComposite materials
dc.keywordsAdhesives
dc.keywordsStress
dc.keywordsShear (Mechanics)
dc.keywordsFailure
dc.keywordsThickness
dc.keywordsBonding AND Plasticity
dc.treeJournal of Engineering Materials and Technology:;2012:;volume( 134 ):;issue: 004
dc.contenttypeFulltext


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