Buckling analysis of laminated composite plates with a central hole in different geometric shapes

dc.authorid0000-0003-1898-1161en_US
dc.contributor.authorDeniz, Mehmet Emin
dc.date.accessioned2021-11-12T11:08:20Z
dc.date.available2021-11-12T11:08:20Z
dc.date.issued2017en_US
dc.departmentBatman Üniversitesi Mühendislik - Mimarlık Fakültesi Makine Mühendisliği Bölümüen_US
dc.description.abstractIn this study, the buckling behaviors of E-glass/epoxy composite plates with a central hole in different geometric shapes for different boundary conditions will be analyzed. For the analyzes, ratio between thickness and length of the specimen (L/t = 20, 30, 40, 50) and two different laminae orientation angles such as [0o /90o ] 4 and [(0o /90o )2] S parameters will be considered. The buckling behavior of laminated composite plates subjected to axial compressive load using a finite element method package program such as ANSYS will be analyzed. The analyzes will be carried out for three different boundary conditions: clamped-clamped support, clamped-fixed support and fixed-fixed support. Thus, the L/t ratio and laminae orientation angle effects on the buckling behavior of composite plates for different boundary conditions will be investigated. The obtained analyze results show that different L/t ratios and laminae orientation angles have significant effects on the buckling load of composite plates. In additon, the hole shape also affects the buckling loaden_US
dc.identifier.citationDeniz, M.E. (2017). Buckling analysis of laminated composite plates with a central hole in different geometric shapes. 8th International Advanced Technologies Symposium, 19-22 October 2017, Elazığ, Turkeyen_US
dc.identifier.urihttp://iats17.firat.edu.tr/
dc.identifier.urihttps://hdl.handle.net/20.500.12402/3968
dc.identifier.volume6en_US
dc.language.isotren_US
dc.publisherFırat Üniversitesien_US
dc.relation.journal8th International Advanced Technologies Symposium, 19-22 October 2017en_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.rightsAttribution-NonCommercial-ShareAlike 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/3.0/us/*
dc.subjectBuckling Loaden_US
dc.subjectLaminated Composite Plateen_US
dc.subjectBoundary Conditionen_US
dc.subjectBuckling Analysesen_US
dc.titleBuckling analysis of laminated composite plates with a central hole in different geometric shapesen_US
dc.title.alternativeFarklı geometrik şekillerde merkezi delik bulunan lamine kompozit plakaların burkulma analizien_US
dc.typeConference Objecten_US

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