DC Field | Value | Language |
---|---|---|
dc.contributor.author | 김수환 | - |
dc.contributor.author | 권장혁 | - |
dc.date.accessioned | 2013-03-18T08:52:49Z | - |
dc.date.available | 2013-03-18T08:52:49Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2004-10 | - |
dc.identifier.citation | 2004년도 한국전산유체공학회 추계학술대회 , v., no., pp.187 - 191 | - |
dc.identifier.uri | http://hdl.handle.net/10203/146710 | - |
dc.description.abstract | The conventional reliability based design optimization(RBDO) methods require high computational cost compared with the deterministic design optimization(DO) methods. To overcome the computational inefficiency of RBDO, single loop methods have been proposed. These need less function calls than that of RBDO but much more than that of DO. In this study, the approximate reliability method is proposed that the computational requirement is nearly the same as DO and the reliability accuracy is good compared with that of RBDO. Using this method, the 3-D viscous aerodynamic shape design optimization with uncertainty is performed very efficiently. | - |
dc.language | KOR | - |
dc.publisher | 한국전산유체공학회 | - |
dc.title | 근사신뢰도기법을 이용한 효율적인 공력 형상 설계에 관한 연구 | - |
dc.title.alternative | Study of the Efficient Aerodynamic Shape Design Optimization Using the Approximate Reliability Method | - |
dc.type | Conference | - |
dc.type.rims | CONF | - |
dc.citation.beginningpage | 187 | - |
dc.citation.endingpage | 191 | - |
dc.citation.publicationname | 2004년도 한국전산유체공학회 추계학술대회 | - |
dc.identifier.conferencecountry | South Korea | - |
dc.identifier.conferencecountry | South Korea | - |
dc.contributor.localauthor | 권장혁 | - |
dc.contributor.nonIdAuthor | 김수환 | - |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.