Angle-of-attack effect on transonic/supersonic aeroelasticity of wing-box model

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dc.contributor.authorYoo, JHko
dc.contributor.authorKim, DHko
dc.contributor.authorLee, Inko
dc.date.accessioned2008-07-18T08:58:07Z-
dc.date.available2008-07-18T08:58:07Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2002-
dc.identifier.citationJOURNAL OF AIRCRAFT, v.39, no.5, pp.906 - 908-
dc.identifier.issn0021-8669-
dc.identifier.urihttp://hdl.handle.net/10203/6117-
dc.description.sponsorshipThis work was supported through funding from the Republic of Korea Ministry of Science and Technology.The authors would like to acknowledge the support (Subject 2000-N-NL-01-C-250) of the National Research Laboratory Program.en
dc.languageEnglish-
dc.language.isoen_USen
dc.publisherAMER INST AERONAUT ASTRONAUT-
dc.titleAngle-of-attack effect on transonic/supersonic aeroelasticity of wing-box model-
dc.typeArticle-
dc.identifier.wosid000178565800026-
dc.identifier.scopusid2-s2.0-0036756988-
dc.type.rimsART-
dc.citation.volume39-
dc.citation.issue5-
dc.citation.beginningpage906-
dc.citation.endingpage908-
dc.citation.publicationnameJOURNAL OF AIRCRAFT-
dc.embargo.liftdate9999-12-31-
dc.embargo.terms9999-12-31-
dc.contributor.localauthorLee, In-
dc.contributor.nonIdAuthorYoo, JH-
dc.contributor.nonIdAuthorKim, DH-
dc.type.journalArticleArticle-
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