Advanced Aeroelastic Computation of a Composite Curved Missile Fin Using Coupled Parallel Computing

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dc.contributor.authorOh, Il-Kwon-
dc.date.accessioned2013-03-18T10:43:29Z-
dc.date.available2013-03-18T10:43:29Z-
dc.date.created2012-02-06-
dc.date.issued2006-04-26-
dc.identifier.citationInternational Conference on Composite Materials & Nano-Structures 2006, v., no., pp.71 - 71-
dc.identifier.urihttp://hdl.handle.net/10203/147557-
dc.languageENG-
dc.titleAdvanced Aeroelastic Computation of a Composite Curved Missile Fin Using Coupled Parallel Computing-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.beginningpage71-
dc.citation.endingpage71-
dc.citation.publicationnameInternational Conference on Composite Materials & Nano-Structures 2006-
dc.identifier.conferencecountryMalaysia-
dc.identifier.conferencecountryMalaysia-
dc.contributor.localauthorOh, Il-Kwon-
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OSE-Conference Papers(학술회의논문)
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