유연 날개의 확률기반 최적 설계Reliability Based Design Optimization of the Flexible Wing
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 이재훈 | - |
| dc.contributor.author | 김수환 | - |
| dc.contributor.author | 권장혁 | - |
| dc.date.accessioned | 2013-03-18T19:52:20Z | - |
| dc.date.available | 2013-03-18T19:52:20Z | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.issued | 2005-04 | - |
| dc.identifier.citation | 2005년도 한국전산유체공학회 춘계학술대회, v., no., pp.187 - 190 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/151895 | - |
| dc.description.abstract | In this study, the reliablility based design optimization is peformed for an aircraft wing. The flexiblility of the wing was assumed by considering the interaction modeled by static aeroelasticity between aerodynamic forces and the structure. For a multidisciplinary design optimization the results of aerodynamic analysis and structural analysis were included in the optimization formulation. The First Order Reliability Method(FORM) was employed to consider the uncertainty of the designed points. | - |
| dc.language | KOR | - |
| dc.publisher | 한국전산유체공학회 | - |
| dc.title | 유연 날개의 확률기반 최적 설계 | - |
| dc.title.alternative | Reliability Based Design Optimization of the Flexible Wing | - |
| dc.type | Conference | - |
| dc.type.rims | CONF | - |
| dc.citation.beginningpage | 187 | - |
| dc.citation.endingpage | 190 | - |
| dc.citation.publicationname | 2005년도 한국전산유체공학회 춘계학술대회 | - |
| dc.identifier.conferencecountry | South Korea | - |
| dc.identifier.conferencecountry | South Korea | - |
| dc.contributor.localauthor | 권장혁 | - |
| dc.contributor.nonIdAuthor | 이재훈 | - |
| dc.contributor.nonIdAuthor | 김수환 | - |
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