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dc.contributor.authorOmidali, Mahdi
dc.contributor.authorKhedmati, Mohammad Reza
dc.contributor.authorHadipour Godarzi, Roholah
dc.coverage.spatialIranen_US
dc.date.accessioned2018-08-03T09:46:50Z
dc.date.available2018-08-03T09:46:50Z
dc.date.issued2017
dc.identifier.issn2008-8965
dc.identifier.urihttp://hdl.handle.net/1834/13486
dc.description.abstractA common way to join dissimilar materials in industrial applications is to use adhesives. Marine industries use this kind of joints for attaching main hull to superstructure of the ships. Most previous researches have focused on composite-composite joints, while a few of them are devoted to aluminum- sandwich panel joints. This study focuses on the numerical static strength analysis of a typical aluminum-sandwich panel T-joints and improving its strength through a novel design. The results of numerical analyses are in a good agreement with those of the experimental tests and confirm the accuracy of numerical analyses. In analyzing the adhesive between joint elements, contact elements and cohesive zone model (CZM) in ANSYS as well as nonlinear analysis is used. Results show that change in joint geometry considered in this paper, caused a 7.25% increase in vertical failure load of the joint. This increase in strength of joint attained in a situation that because of the merging of the joined parts, the process of construction became easier.en_US
dc.language.isofaen_US
dc.titleNumerical Investigation on Novel Method for Adhesively Bonded T-joint Between Aluminum and Sandwich Panelen_US
dc.typeJournal Contributionen_US
dc.bibliographicCitation.issue1en_US
dc.bibliographicCitation.titleJournal of Marine Science and Technologyen_US
dc.bibliographicCitation.volume16en_US
dc.description.statusPublisheden_US
dc.format.pagerangepp.122-134en_US
dc.subject.asfaInvestigationen_US
dc.subject.asfaMethoden_US
dc.subject.asfaAdhesivelyen_US
dc.subject.asfaAluminumen_US
dc.subject.asfaSandwich Panelen_US
dc.subject.asfaCZMen_US
dc.type.refereedRefereeden_US
refterms.dateFOA2021-01-30T18:48:39Z


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