Stress analysis of adhesively bonded double strap joints with or without intermediate part subjected to tensile loading

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dc.authoridAYAZ, Yaşar/0000-0002-1089-0700
dc.authoridTEMİZ, ŞEMSETTİN/0000-0002-6737-3720
dc.authorwosidAYAZ, Yaşar/ABG-8694-2020
dc.authorwosidTEMİZ, ŞEMSETTİN/ABG-7809-2020
dc.contributor.authorCitila, Serif
dc.contributor.authorAyaz, Yasar
dc.contributor.authorTemiz, Semsettin
dc.date.accessioned2024-08-04T20:42:31Z
dc.date.available2024-08-04T20:42:31Z
dc.date.issued2017
dc.departmentİnönü Üniversitesien_US
dc.description.abstractAccidents in the industry, especially in the field of aerospace, are quite common. Damages like tears cracks and holes occur especially when small sand particles present in the airfield collide with the body and wings of an airplane during takeoff and landing. This torn, cracked, or pierced region should be repaired gently. Damaged parts are frequently small regions for which repair is more suitable than complete replacement as workmanship; cost and time are an important concept in today's world. A gap occurs between the patches if double-bonded patches are used in the repair of the damaged parts. In this study, the region between patches in a joint with and without intermediate parts was modeled and its effect on strength was examined numerically and experimentally. The effects of patch thickness, overlap length, adherent thickness, and gap length on the strength of the joints with and without intermediate part was compared. The results show that the intermediate part does not have any influence on the strength of the lap joint such that double strap joints without intermediate part have higher failure load. Additionally, it is seen that the failure load decreased with increasing patch thickness and increased with the thickness of the adherent.en_US
dc.identifier.doi10.1080/00218464.2015.1075885
dc.identifier.endpage356en_US
dc.identifier.issn0021-8464
dc.identifier.issn1545-5823
dc.identifier.issue5en_US
dc.identifier.scopus2-s2.0-84978160954en_US
dc.identifier.scopusqualityQ2en_US
dc.identifier.startpage343en_US
dc.identifier.urihttps://doi.org/10.1080/00218464.2015.1075885
dc.identifier.urihttps://hdl.handle.net/11616/97406
dc.identifier.volume93en_US
dc.identifier.wosWOS:000394681300001en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherTaylor & Francis Ltden_US
dc.relation.ispartofJournal of Adhesionen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectAdhesive materialsen_US
dc.subjectdouble strap jointen_US
dc.subjectfinite element analysisen_US
dc.subjectrepairen_US
dc.titleStress analysis of adhesively bonded double strap joints with or without intermediate part subjected to tensile loadingen_US
dc.typeArticleen_US

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