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College of Engineering(공과대학)School of Mechanical and Aerospace Engineering(기계항공공학부)Dept. of Aerospace Engineering(항공우주공학과)AE-Conference Papers(학술회의논문)

Aircraft Wing Flutter Characteristics Considering Control Surface and Actuator Nonlinearity in Subsonic and Supersonic Regions

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dc.contributor.authorLee, SJ-
dc.contributor.authorShin, WH-
dc.contributor.authorLee, In-
dc.date.accessioned2008-07-23T06:20:14Z-
dc.date.available2008-07-23T06:20:14Z-
dc.date.created2012-02-06-
dc.date.issued2007-08-08-
dc.identifier.citation007 Asia Pacific Vibration Conference, v., no., pp. --
dc.identifier.urihttp://hdl.handle.net/10203/6359-
dc.description.sponsorshipThis research was supported by the Agency for Defense Development (ADD) and Flight Vehicle Research Center(FVRC) in the Republic of Korea. This support is gratefully acknowledged.en
dc.languageENG-
dc.language.isoen_USen
dc.publisherAsia Pacific Vibration Conference (APVC)-
dc.titleAircraft Wing Flutter Characteristics Considering Control Surface and Actuator Nonlinearity in Subsonic and Supersonic Regions-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationname007 Asia Pacific Vibration Conference-
dc.identifier.conferencecountryJapan-
dc.identifier.conferencecountryJapan-
dc.contributor.localauthorLee, In-
dc.contributor.nonIdAuthorLee, SJ-
dc.contributor.nonIdAuthorShin, WH-
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AE-Conference Papers(학술회의논문)

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