Free vibration analysis of fiber metal laminated straight beam

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dc.authorid57204552000
dc.authorid53664642600
dc.authorid57204550621
dc.authorid57204546435
dc.contributor.authorMaraş S.
dc.contributor.authorYaman M.
dc.contributor.authorSansveren M.F.
dc.contributor.authorReyhan S.K.
dc.date.accessioned20.04.201910:49:12
dc.date.accessioned2019-04-20T21:43:10Z
dc.date.available20.04.201910:49:12
dc.date.available2019-04-20T21:43:10Z
dc.date.issued2018
dc.departmentBayburt Üniversitesien_US
dc.description.abstractIn recent years, studies on the development of new and advanced composite materials have been increasing. Among these new technological products, Fiber Metal Laminates (FML), and hybrid structures made of aluminium, carbon, glass or aramid fiber, are preferred especially in the aircraft industry due to their high performance. Therefore, free vibration analysis is necessary for the design process of such structures. In this study, the vibration characteristics of FML for clamped-free boundary conditions were investigated experimentally and numerically. Firstly, numerical results were obtained using Finite Element Method (FEM) and then these results were compared with the experimental results. It was seen that the numerical results were in good agreement with the experimental results. As the theoretical model was justified, the effects of various parameters such as number of layers, fiber orientations, and aluminium layer thickness on the in-plane vibration characteristics of the FML straight beam were analysed using FEM. Thus, most important parameters affecting the vibration characteristics of the hybrid structures were determined. © 2018 Sinan Maraş et al. published by De Gruyte.en_US
dc.identifier.doi10.1515/chem-2018-0101
dc.identifier.endpage948
dc.identifier.issn2391-5420
dc.identifier.issue1
dc.identifier.scopus2-s2.0-85056134061en_US
dc.identifier.scopusqualityQ2en_US
dc.identifier.startpage944
dc.identifier.urihttps://dx.doi.org/10.1515/chem-2018-0101
dc.identifier.urihttps://hdl.handle.net/20.500.12403/426
dc.identifier.volume16
dc.identifier.wosWOS:000449033200006en_US
dc.identifier.wosqualityQ3en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherDe Gruyter
dc.relation.ispartofOpen Chemistryen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectFiber Metal Laminates
dc.subjectFinite Element Method
dc.subjectHybrid Structures
dc.subjectLaminated Composite Straight Beam
dc.subjectVibration Analysis
dc.subjectFiber Metal Laminates
dc.subjectFinite Element Method
dc.subjectHybrid Structures
dc.subjectLaminated Composite Straight Beam
dc.subjectVibration Analysis
dc.titleFree vibration analysis of fiber metal laminated straight beamen_US
dc.typeArticleen_US

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