Mechanical analysis of hybrid structured aircraft wing ribs with different geometric gaps

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dc.contributor.authorAkdogan, Tumay Battal
dc.contributor.authorSulu, Ismail Yasin
dc.date.accessioned2024-08-04T20:56:13Z
dc.date.available2024-08-04T20:56:13Z
dc.date.issued2024
dc.departmentİnönü Üniversitesien_US
dc.description.abstractWing ribs, which play a critical role in aviation, are an important design element, especially for unmanned aerial vehicles. Aircraft wing ribs are structural elements that generally extend from the wing root to the tip, used to maintain the shape of the wing, provide aerodynamic stability and add durability to the wing surface. In this study, the wing root rib of the MQ-1B Predator unmanned aerial vehicle were modeled with cavities with different geometric structures and its mechanical behavior were examined. Wing rib structures were created from circular, elliptical, slot and beam geometry gaps. The hybrid structure was created by considering the combined use of Carbon-Kevlar-Aramid. In the hybrid structure, the thickness of each fiber layer was taken into account as 0.25 mm and the wing rib consisted of six layers. The effects of different fiber angles in hybrid composite structures were also examined. As a result of the analyses, equivalent stress (von-Mises stress) and total deformation results were examined.en_US
dc.identifier.doi10.1515/mt-2024-0033
dc.identifier.issn0025-5300
dc.identifier.issn2195-8572
dc.identifier.scopus2-s2.0-85198999511en_US
dc.identifier.scopusqualityQ2en_US
dc.identifier.urihttps://doi.org/10.1515/mt-2024-0033
dc.identifier.urihttps://hdl.handle.net/11616/102128
dc.identifier.wosWOS:001270127200001en_US
dc.identifier.wosqualityN/Aen_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.subjectcomposite materialen_US
dc.subjectaircraft wingen_US
dc.subjectfinite element methoden_US
dc.subjectstressen_US
dc.subjectdeformationen_US
dc.titleMechanical analysis of hybrid structured aircraft wing ribs with different geometric gapsen_US
dc.typeArticleen_US

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