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Analysis of multilayered composite cylinders under thermal loading

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dc.creator Akcay, IH
dc.creator KAYNAK, İDRİS
dc.date 2004-12-31T22:00:00Z
dc.date.accessioned 2020-10-06T11:24:51Z
dc.date.available 2020-10-06T11:24:51Z
dc.identifier d42fd338-c9a0-4f98-901b-b64ea419ee85
dc.identifier 10.1177/0731684405048840
dc.identifier https://avesis.sdu.edu.tr/publication/details/d42fd338-c9a0-4f98-901b-b64ea419ee85/oai
dc.identifier.uri http://acikerisim.sdu.edu.tr/xmlui/handle/123456789/72987
dc.description In this investigation, a failure analysis is performed on analytical expressions of multilayered filament wound structures (FWS) in composite cylinders for the plane-strain and closed-end condition cases, under internal pressure and uniform thermal loading. The multilayer filament wound composite pressure closed-end cylinders are oriented symmetrically and antisymmetrically. The mechanical properties of composite cylinders are investigated considering a glass-epoxy multilayered composite cylinder. The failure analysis is carried out on different orientations of the multilayered composite cylinders. The failure pressure is found to be high at increased temperatures for the plane-strain cases. It is nearly the same for the closed-end case.
dc.language eng
dc.rights info:eu-repo/semantics/closedAccess
dc.title Analysis of multilayered composite cylinders under thermal loading
dc.type info:eu-repo/semantics/article


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