DC Field | Value | Language |
---|---|---|
dc.contributor.author | Kim, Eun-Ho | ko |
dc.contributor.author | Roh, Jin-Ho | ko |
dc.contributor.author | Yoo, Seung Jae | ko |
dc.contributor.author | Lee, In | ko |
dc.date.accessioned | 2008-07-14T06:44:34Z | - |
dc.date.available | 2008-07-14T06:44:34Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2006-11 | - |
dc.identifier.citation | KSAS INTERNATIONAL JOURNAL, v.7, no.2, pp.104 - 109 | - |
dc.identifier.issn | 2093-274X | - |
dc.identifier.uri | http://hdl.handle.net/10203/5728 | - |
dc.description.abstract | In 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.sponsorship | This study is supported by FVRC(Flight Vechicle Research Center) by Agency for Defense Development, Korea. Authors are grateful for their supports. | en |
dc.language | English | - |
dc.language.iso | en_US | en |
dc.publisher | 한국항공우주학회 | - |
dc.title | Equivalent Plate Modeling of the Wing-Box Structure with Control Surface | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 7 | - |
dc.citation.issue | 2 | - |
dc.citation.beginningpage | 104 | - |
dc.citation.endingpage | 109 | - |
dc.citation.publicationname | KSAS INTERNATIONAL JOURNAL | - |
dc.embargo.liftdate | 9999-12-31 | - |
dc.embargo.terms | 9999-12-31 | - |
dc.contributor.localauthor | Lee, In | - |
dc.contributor.nonIdAuthor | Kim, Eun-Ho | - |
dc.contributor.nonIdAuthor | Roh, Jin-Ho | - |
dc.contributor.nonIdAuthor | Yoo, Seung Jae | - |
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