Development of Advanced Aeroelastic Analysis System and Numerical Computation for Transonic/Supersonic Aircraft Design

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dc.contributor.authorLee, In-
dc.contributor.authorKwon, H. J.-
dc.contributor.authorKim, J. Y.-
dc.date.accessioned2008-07-31T05:51:17Z-
dc.date.available2008-07-31T05:51:17Z-
dc.date.created2012-02-06-
dc.date.issued2005-12-01-
dc.identifier.citationInternational Conference on Computational & Experimental Engineering and Sciences, v., no., pp. --
dc.identifier.urihttp://hdl.handle.net/10203/6730-
dc.description.sponsorshipThis work was supported through funding from Korea Aerospace Industry (KAI) and Agency for Defense Development (ADD). The authors acknowledge the support from the Long-Term Project for Basic Research.en
dc.languageENG-
dc.language.isoen_USen
dc.publisherICCES-
dc.titleDevelopment of Advanced Aeroelastic Analysis System and Numerical Computation for Transonic/Supersonic Aircraft Design-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationnameInternational Conference on Computational & Experimental Engineering and Sciences-
dc.identifier.conferencecountryIndia-
dc.identifier.conferencecountryIndia-
dc.contributor.localauthorLee, In-
dc.contributor.nonIdAuthorKwon, H. J.-
dc.contributor.nonIdAuthorKim, J. Y.-

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