Progressive Failure Analysis of Reinforced-Adhesively Single-Lap Joint

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dc.contributor.authorTuran, Kadir
dc.contributor.authorPekbey, Yeliz
dc.date.accessioned2024-04-24T16:24:19Z
dc.date.available2024-04-24T16:24:19Z
dc.date.issued2015
dc.departmentDicle Üniversitesien_US
dc.description.abstractThe failure behavior of reinforced-adhesively single-lap joints was investigated experimentally and numerically. The reinforced adhesive was produced by mixing waste composite particles and an epoxy-based commercial adhesive. The single-lap joint was prepared with an adhesive and unidirectional fiber glass/epoxy composite plates with a (0 degrees/90 degrees)(3) stacking sequence. Three types of adhesive were used: an un-reinforced adhesive (ADH), an adhesive mixed with glass fiber-reinforced epoxy resin composite plate particles (GFRC), and an adhesive mixed with carbon fiber-reinforced epoxy resin composite plate particles (CFRC). The adhesive thickness (ta) and overlap length (lap) were 0.4, 0.8, 1.2, and 1.6 mm and 10, 20, 30, and 40 mm, respectively. Progressive failure analysis was performed with the ANSYS (TM) 11.0 finite element program using ANSYS (TM) parametric design language (APDL) code. In the numerical study, the failure loads of the composite and the adhesive were determined with the Hashin failure criteria and the Tresca failure criteria, respectively. The difference between the experimental and numerical studies ranged from 2% to 10%. The failure load of reinforced-adhesively single-lap joints was 1.3-22.8% higher than that of the un-reinforced adhesive.en_US
dc.description.sponsorshipDicle University Scientific Research Projects Unit [13-MF-109]en_US
dc.description.sponsorshipThis work was supported by the Dicle University Scientific Research Projects Unit [Grant Number 13-MF-109].en_US
dc.identifier.doi10.1080/00218464.2014.985379
dc.identifier.endpage977en_US
dc.identifier.issn0021-8464
dc.identifier.issn1545-5823
dc.identifier.issue12en_US
dc.identifier.scopus2-s2.0-84940367560
dc.identifier.scopusqualityQ2
dc.identifier.startpage962en_US
dc.identifier.urihttps://doi.org/10.1080/00218464.2014.985379
dc.identifier.urihttps://hdl.handle.net/11468/16647
dc.identifier.volume91en_US
dc.identifier.wosWOS:000359971500005
dc.identifier.wosqualityQ2
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoenen_US
dc.publisherTaylor & Francis Ltden_US
dc.relation.ispartofJournal of Adhesion
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectCompositesen_US
dc.subjectEpoxyen_US
dc.subjectMechanical Properties Of Adhesivesen_US
dc.subjectNumerical Analysisen_US
dc.titleProgressive Failure Analysis of Reinforced-Adhesively Single-Lap Jointen_US
dc.titleProgressive Failure Analysis of Reinforced-Adhesively Single-Lap Joint
dc.typeArticleen_US

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