Nonlinear Flutter Analysis for Missile Fin with Actuator and Structural Nonlinearity

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dc.contributor.authorShin, W. H.-
dc.contributor.authorBae, J. S.-
dc.contributor.authorLee, In-
dc.date.accessioned2008-07-31T07:31:48Z-
dc.date.available2008-07-31T07:31:48Z-
dc.date.created2012-02-06-
dc.date.issued2005-10-
dc.identifier.citation2005 JSASS-KSAS Joint Symposium on Aerospace Engineering, v., no., pp. --
dc.identifier.urihttp://hdl.handle.net/10203/6738-
dc.description.sponsorshipThis research was supported by Agency for Defense Development(ADD) in the Republic of Korea. This support is gratefully acknowledged.en
dc.languageENG-
dc.language.isoen_USen
dc.publisherJSASS, KSAS-
dc.titleNonlinear Flutter Analysis for Missile Fin with Actuator and Structural Nonlinearity-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationname2005 JSASS-KSAS Joint Symposium on Aerospace Engineering-
dc.identifier.conferencecountryJapan-
dc.identifier.conferencecountryJapan-
dc.contributor.localauthorLee, In-
dc.contributor.nonIdAuthorShin, W. H.-
dc.contributor.nonIdAuthorBae, J. S.-

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