Thermal Buckling Characteristics of Composite Conical Shell Structures

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dc.contributor.authorWoo, Ji-Hyeko
dc.contributor.authorRho, Jin-Hoko
dc.contributor.authorLee, Inko
dc.date.accessioned2008-07-14T06:28:34Z-
dc.date.available2008-07-14T06:28:34Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2007-11-
dc.identifier.citationKSAS INTERNATIONAL JOURNAL, v.8, no.2, pp.82 - 88-
dc.identifier.issn1229-9627-
dc.identifier.urihttp://hdl.handle.net/10203/5722-
dc.description.abstractThermal buckling and free vibration analyses of multi-laered composite conical shells based on a layerwise displacement theory are performed. The Donnells displacement-strain relationships of conical shell structure are applied. The natural frequencies are compared with the ones existing in the previous literature for laminated conical shells with several cone semi-vertex angles. Moreover, the thermal buckling behaviors of the laminated conical shell are investigated to consider the effect of the semi-vertex angle, subtended angle, and radius to thickness ratio on the structural stability.-
dc.description.sponsorshipThis study has been supported by the KARI under research and development of Korea Space Launch Vehicle Project. Authors are grateful for thier wupports.en
dc.languageEnglish-
dc.language.isoen_USen
dc.publisher한국항공우주학회-
dc.titleThermal Buckling Characteristics of Composite Conical Shell Structures-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume8-
dc.citation.issue2-
dc.citation.beginningpage82-
dc.citation.endingpage88-
dc.citation.publicationnameKSAS INTERNATIONAL JOURNAL-
dc.embargo.liftdate9999-12-31-
dc.embargo.terms9999-12-31-
dc.contributor.localauthorLee, In-
dc.contributor.nonIdAuthorWoo, Ji-Hye-
dc.contributor.nonIdAuthorRho, Jin-Ho-
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AE-Journal Papers(저널논문)
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