DC Field | Value | Language |
---|---|---|
dc.contributor.author | Woo, Ji-Hye | ko |
dc.contributor.author | Rho, Jin-Ho | ko |
dc.contributor.author | Lee, In | ko |
dc.date.accessioned | 2008-07-14T06:28:34Z | - |
dc.date.available | 2008-07-14T06:28:34Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2007-11 | - |
dc.identifier.citation | KSAS INTERNATIONAL JOURNAL, v.8, no.2, pp.82 - 88 | - |
dc.identifier.issn | 1229-9627 | - |
dc.identifier.uri | http://hdl.handle.net/10203/5722 | - |
dc.description.abstract | Thermal 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.sponsorship | This 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.language | English | - |
dc.language.iso | en_US | en |
dc.publisher | 한국항공우주학회 | - |
dc.title | Thermal Buckling Characteristics of Composite Conical Shell Structures | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 8 | - |
dc.citation.issue | 2 | - |
dc.citation.beginningpage | 82 | - |
dc.citation.endingpage | 88 | - |
dc.citation.publicationname | KSAS INTERNATIONAL JOURNAL | - |
dc.embargo.liftdate | 9999-12-31 | - |
dc.embargo.terms | 9999-12-31 | - |
dc.contributor.localauthor | Lee, In | - |
dc.contributor.nonIdAuthor | Woo, Ji-Hye | - |
dc.contributor.nonIdAuthor | Rho, Jin-Ho | - |
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