Mechanical analysis of composite plates adhesively joined with different single-lap techniques under bending loading

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dc.authoridSÜLÜ, İsmail Yasin/0000-0002-2648-6294
dc.authorwosidSÜLÜ, İsmail Yasin/ABH-1342-2020
dc.contributor.authorSulu, Ismail Yasin
dc.date.accessioned2024-08-04T20:54:43Z
dc.date.available2024-08-04T20:54:43Z
dc.date.issued2023
dc.departmentİnönü Üniversitesien_US
dc.description.abstractIn this study, composite plates adhesively joined using single-lap joint without intermediated material (SLJ) and intermediated material (IM-SLJ) subject to bending loading were investigated via finite element analysis. DP 410 type adhesive was used. Composite parts and intermediate material were preferred as T700 carbon/epoxy. Numerical analyses were carried out using ANSYS 14.5 software package, in which the finite element method was taken into account. Failure situations for adhesive and composites were examined by the von-Mises failure criteria and the Tsai-wu failure criteria, respectively. Firstly, the failure loads for each parameter situation were determined. The equivalent stresses of the critical stress lines on adhesive layers were examined and critical stresses line were determined for length and width of adhesive layers. Shear, normal, and von-Mises stresses were investigated at obtained failure load for each parameter of SLJ and IM-SLJ. The von-Mises on the critical stress lines were compared for different overlap width and length of SLJ and IM-SLJ. The effects of joint techniques, orientation angles, and overlap dimensional were investigated on adhesive layer, and joint techniques were compared about advantages. A different study from the literature was carried out to compare the mechanical behavior of SLJ and IM-SLJ joining techniques.en_US
dc.identifier.doi10.1515/mt-2023-0137
dc.identifier.endpage1905en_US
dc.identifier.issn0025-5300
dc.identifier.issn2195-8572
dc.identifier.issue12en_US
dc.identifier.scopus2-s2.0-85172685351en_US
dc.identifier.scopusqualityQ2en_US
dc.identifier.startpage1890en_US
dc.identifier.urihttps://doi.org/10.1515/mt-2023-0137
dc.identifier.urihttps://hdl.handle.net/11616/101594
dc.identifier.volume65en_US
dc.identifier.wosWOS:001068714300001en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherWalter De Gruyter Gmbhen_US
dc.relation.ispartofMaterials Testingen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectjoint designen_US
dc.subjectfinite element analysisen_US
dc.subjectsingle-lap jointen_US
dc.subjectadhesiveen_US
dc.subjectorientation anglesen_US
dc.subjectstress analysisen_US
dc.titleMechanical analysis of composite plates adhesively joined with different single-lap techniques under bending loadingen_US
dc.typeArticleen_US

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