유한요소법에 의한 복합적층 원통쉘의 좌굴해석Buckling Analysis of Laminated Composite Cylindrical Shell by the Finite Element Method

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dc.contributor.author고대우ko
dc.contributor.author홍창선ko
dc.date.accessioned2013-02-25T16:13:56Z-
dc.date.available2013-02-25T16:13:56Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued1984-04-
dc.identifier.citation한국항공우주학회지, v.12, no.1, pp.85 - 94-
dc.identifier.issn1225-1348-
dc.identifier.urihttp://hdl.handle.net/10203/63462-
dc.languageKorean-
dc.publisher한국항공우주학회-
dc.title유한요소법에 의한 복합적층 원통쉘의 좌굴해석-
dc.title.alternativeBuckling Analysis of Laminated Composite Cylindrical Shell by the Finite Element Method-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume12-
dc.citation.issue1-
dc.citation.beginningpage85-
dc.citation.endingpage94-
dc.citation.publicationname한국항공우주학회지-
dc.contributor.localauthor홍창선-
dc.contributor.nonIdAuthor고대우-
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AE-Journal Papers(저널논문)
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