Failure analysis of two-dimensional carbon-epoxy composite plate pinned joint

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dc.contributor.authorAktas, A
dc.contributor.authorKarakuzu, R
dc.date.accessioned2020-06-25T17:34:38Z
dc.date.available2020-06-25T17:34:38Z
dc.date.issued1999
dc.departmentKırıkkale Üniversitesi
dc.descriptionKarakuzu, Ramazan/0000-0001-8149-4871
dc.description.abstractThe aim of this study is to investigate failure strength and failure mode of a mechanically fastened carbon-epoxy composite plate of arbitrary orientation. The failure load and the failure mode are analyzed numerically and experimentally. The numerical method includes two steps. First, the stress distribution in the plate is calculated by the use of finite-element method. Second, the failure load and the failure mode are predicted by means of Tsai-Hill and fiber tensile-compressive failure criteria. A computer program was developed which can be used to calculate the failure load, the failure mode, and the propagation of failure. The distance-to-diameter, E/D, and width-to-diameter, W/D, ratios in the plate are changed from 1 to 5 and 2 to 5, respectively. It is found that full bearing strength is developed when E/D and W/D ratios are equal to or greater than 4.en_US
dc.identifier.citationclosedAccessen_US
dc.identifier.doi10.1080/107594199305502
dc.identifier.endpage361en_US
dc.identifier.issn1075-9417
dc.identifier.issue4en_US
dc.identifier.startpage347en_US
dc.identifier.urihttps://doi.org/10.1080/107594199305502
dc.identifier.urihttps://hdl.handle.net/20.500.12587/2814
dc.identifier.volume6en_US
dc.identifier.wosWOS:000083524100005
dc.identifier.wosqualityQ2
dc.indekslendigikaynakWeb of Science
dc.language.isoen
dc.publisherTaylor & Francis Incen_US
dc.relation.ispartofMechanics Of Composite Materials And Structures
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.titleFailure analysis of two-dimensional carbon-epoxy composite plate pinned jointen_US
dc.typeArticle

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