Damping effects of rubber layer in laminated composite circular plate during forced vibration

dc.contributor.authorBaltaci, Aysun
dc.contributor.authorSarikanat, Mehmet
dc.contributor.authorYildiz, Hasan
dc.contributor.editorInan, E
dc.contributor.editorKiris, A
dc.date.accessioned2019-10-27T19:39:41Z
dc.date.available2019-10-27T19:39:41Z
dc.date.issued2007
dc.departmentEge Üniversitesien_US
dc.description7th International Conference on Vibration Problems (ICOVP 2005) -- SEP 05-09, 2005 -- Isik Univ, Sile Campus, Istanbul, TURKEYen_US
dc.description.abstractIn this study, the effects of the location of the rubber between composite layers which is located to supply damping on the vibration frequency of laminated composite circular plates having different fiber directions are investigated by using the finite element method. The laminated composite circular plate having free outer edge is manufatured as having a central hole. Hybrid composite circular plate is clamped at the inner edge and subjected to transverse impuls load on a location at the outer edge. The best location of the rubber layer in terms of the damping capability are determined by using finite element analysis.en_US
dc.identifier.endpage+en_US
dc.identifier.isbn978-1-4020-5400-6
dc.identifier.issn0930-8989
dc.identifier.startpage63en_US
dc.identifier.urihttps://hdl.handle.net/11454/40193
dc.identifier.volume111en_US
dc.identifier.wosWOS:000246655700012en_US
dc.identifier.wosqualityN/Aen_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.language.isoenen_US
dc.publisherSpringeren_US
dc.relation.ispartofVibration Problems Icovp 2005en_US
dc.relation.ispartofseriesSpringer Proceedings in Physics
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectdampingen_US
dc.subjectforced vibrationen_US
dc.subjectcomposite circular plateen_US
dc.titleDamping effects of rubber layer in laminated composite circular plate during forced vibrationen_US
dc.typeConference Objecten_US

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