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

Equivalent Plate Modeling of the Wing-Box Structure with Control Surface

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dc.contributor.authorKim, Eun-Hoko
dc.contributor.authorRoh, Jin-Hoko
dc.contributor.authorYoo, Seung Jaeko
dc.contributor.authorLee, Inko
dc.date.accessioned2008-07-14T06:44:34Z-
dc.date.available2008-07-14T06:44:34Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2006-11-
dc.identifier.citationKSAS INTERNATIONAL JOURNAL, v.7, no.2, pp.104 - 109-
dc.identifier.issn2093-274X-
dc.identifier.urihttp://hdl.handle.net/10203/5728-
dc.description.abstractIn this study, the equivalent plate model is developed using a finite element method(FEM) based on the first order shear deformation theory(FSDT). The substructure synthesis method is used to consider the control surface. For the verification of the equivalent model, the results of free vibration analysis are compared with the ones of 3D wing structure modeled by using the MSC/NASTRAN.-
dc.description.sponsorshipThis study is supported by FVRC(Flight Vechicle Research Center) by Agency for Defense Development, Korea. Authors are grateful for their supports.en
dc.languageEnglish-
dc.language.isoen_USen
dc.publisher한국항공우주학회-
dc.titleEquivalent Plate Modeling of the Wing-Box Structure with Control Surface-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume7-
dc.citation.issue2-
dc.citation.beginningpage104-
dc.citation.endingpage109-
dc.citation.publicationnameKSAS INTERNATIONAL JOURNAL-
dc.embargo.liftdate9999-12-31-
dc.embargo.terms9999-12-31-
dc.contributor.localauthorLee, In-
dc.contributor.nonIdAuthorKim, Eun-Ho-
dc.contributor.nonIdAuthorRoh, Jin-Ho-
dc.contributor.nonIdAuthorYoo, Seung Jae-
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AE-Journal Papers(저널논문)
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