Investigation of joining methods of honeycomb composite panels used in structural elements of aircraft cabin units

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dc.contributor.authorErhal, Aslan Kahraman
dc.contributor.authorKılınçarslan, Sena Kabave
dc.contributor.authorKorkmaz, Şeyma
dc.contributor.authorÇetin, M. Hüseyin
dc.date.accessioned2024-09-29T16:32:20Z
dc.date.available2024-09-29T16:32:20Z
dc.date.issued2021
dc.departmentKarabük Üniversitesien_US
dc.description.abstractThe design, material selection, manufacture and assembly of aircraft structural elements are critical issues in the aviation industry. This study aims to optimize the selection of joining methods of aircraft honeycomb panels by considering strength, cost, and weight parameters. Accordingly, panel type, panel thickness and joining methods were determined as input parameters, and fracture force, displacement, cost, and weight as output parameters. Tenon-mortise, double-sided bracket, single-sided bracket, and extrusion methods were investigated for L and T-type panels. Panel thicknesses were determined as 10 mm and 22 mm according to standards. Tensile test and finite element analysis were applied to the samples to examine their mechanical behavior. The weight and cost of the panels were determined by the process analysis. The obtained findings were optimized according to multi-criteria decision making and response surface analysis methods. In the optimization model, maximization of tensile strength and minimization of displacement, cost and weight was determined as the target function. At the end of the study, the optimum thickness value for both types of panels was determined as 22 mm, and the optimum joining method was tenon-mortise.en_US
dc.identifier.endpage117en_US
dc.identifier.issn1304-0448
dc.identifier.issue1en_US
dc.identifier.startpage99en_US
dc.identifier.trdizinid485035en_US
dc.identifier.urihttps://search.trdizin.gov.tr/tr/yayin/detay/485035
dc.identifier.urihttps://hdl.handle.net/20.500.14619/11558
dc.identifier.volume14en_US
dc.indekslendigikaynakTR-Dizinen_US
dc.language.isoenen_US
dc.relation.ispartofHavacılık ve Uzay Teknolojileri Dergisien_US
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.titleInvestigation of joining methods of honeycomb composite panels used in structural elements of aircraft cabin unitsen_US
dc.typeArticleen_US

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