Springback Behavior of Fiber Metal Laminates with Carbon Fiber-Reinforced Core in V-Bending Process

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dc.authoridtaskin, vedat/0000-0002-3013-2317;
dc.authorwosidtaskin, vedat/AAZ-2791-2021
dc.authorwosidışıktaş, ali/KIG-4362-2024
dc.contributor.authorIsiktas, Ali
dc.contributor.authorTaskin, Vedat
dc.date.accessioned2024-06-12T11:01:53Z
dc.date.available2024-06-12T11:01:53Z
dc.date.issued2020
dc.departmentTrakya Üniversitesien_US
dc.description.abstractFiber metal laminates (FMLs) are a kind of hybrid composite material that consist of metal sheets and fiber-reinforced composite layers. The use of FMLs has been particularly increasing in the production of aircraft bodies. However, the springback behavior that occurs during the formation of FML parts has a negative impact on the form of the final product. In the present study, FMLs were manufactured by combining aluminum 5754-H22 sheets and carbon fiber-reinforced plastic sheets by using adhesive. A set of experiments were performed to determine the effect of bending angle, face sheet thickness and core thickness on the springback behavior of FMLs. The results showed that the amount of springback in the FML specimen increased as the bending angle increased. It was found that when the thickness of the face sheet increased, the amount of springback in FML specimens was higher in all bending angles. In addition, the amount of springback in FML specimens decreased as core thickness increased.en_US
dc.description.sponsorshipResearch Fund of Trakya University [2017/185]en_US
dc.description.sponsorshipThis work was supported by the Research Fund of Trakya University. Project Number: 2017/185.en_US
dc.identifier.doi10.1007/s13369-020-04796-w
dc.identifier.endpage9366en_US
dc.identifier.issn2193-567X
dc.identifier.issn2191-4281
dc.identifier.issue11en_US
dc.identifier.scopus2-s2.0-85088292154en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage9357en_US
dc.identifier.urihttps://doi.org/10.1007/s13369-020-04796-w
dc.identifier.urihttps://hdl.handle.net/20.500.14551/21070
dc.identifier.volume45en_US
dc.identifier.wosWOS:000550656100006en_US
dc.identifier.wosqualityQ3en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherSpringer Heidelbergen_US
dc.relation.ispartofArabian Journal For Science And Engineeringen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectFiber Metal Laminate (FML)en_US
dc.subjectSpringbacken_US
dc.subjectV-Bendingen_US
dc.subjectBending Angleen_US
dc.subjectCarbon Fiberen_US
dc.subjectFinite-Elementen_US
dc.subjectBacken_US
dc.subjectFatigueen_US
dc.subjectSheeten_US
dc.subjectGlareen_US
dc.titleSpringback Behavior of Fiber Metal Laminates with Carbon Fiber-Reinforced Core in V-Bending Processen_US
dc.typeArticleen_US

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