Nonlinear flutter characteristics of composite missile wing in transonic/low-supersonic flows

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dc.contributor.authorKim, DHko
dc.contributor.authorLee, Inko
dc.date.accessioned2008-07-18T08:35:24Z-
dc.date.available2008-07-18T08:35:24Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2002-
dc.identifier.citationJOURNAL OF AIRCRAFT, v.39, no.5, pp.889 - 892-
dc.identifier.issn0021-8669-
dc.identifier.urihttp://hdl.handle.net/10203/6113-
dc.description.sponsorshipThis work was supported through funding from the Korea Ministry of Science and Technology. The authors 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.subjectDIVERGENCE-
dc.titleNonlinear flutter characteristics of composite missile wing in transonic/low-supersonic flows-
dc.typeArticle-
dc.identifier.wosid000178565800020-
dc.identifier.scopusid2-s2.0-0036758052-
dc.type.rimsART-
dc.citation.volume39-
dc.citation.issue5-
dc.citation.beginningpage889-
dc.citation.endingpage892-
dc.citation.publicationnameJOURNAL OF AIRCRAFT-
dc.embargo.liftdate9999-12-31-
dc.embargo.terms9999-12-31-
dc.contributor.localauthorLee, In-
dc.contributor.nonIdAuthorKim, DH-
dc.type.journalArticleArticle-
dc.subject.keywordPlusDIVERGENCE-
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