DC Field | Value | Language |
---|---|---|
dc.contributor.author | 성춘호 | ko |
dc.contributor.author | 권장혁 | ko |
dc.date.accessioned | 2010-05-18T02:48:29Z | - |
dc.date.available | 2010-05-18T02:48:29Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2000-01 | - |
dc.identifier.citation | 한국항공우주학회지, v.28, no.4, pp.1 - 8 | - |
dc.identifier.issn | 1225-1348 | - |
dc.identifier.uri | http://hdl.handle.net/10203/18414 | - |
dc.description.abstract | An efficient aerodynamic design optimization method for 3-dimensional wing is developed. A gradients-based optimization is adopted to find optimum, and adjoint equations are used for sensitivity calculations. The computational efficiency is improved by using a tightly coupled approach with step size estimation, multigrid DADI flow analysis and parallel computing. To show the efficiency of present method, a drag minimization problem of ONERA M6 wing under transonic flow conditions is presented. | - |
dc.description.sponsorship | 본 연구는 과학기술부 특정연구과제 `신기술 설계기술 및 파손예방`의 일부 지원으로 수행되었음을 밝힌다. | en |
dc.language | Korean | - |
dc.language.iso | ko | en |
dc.publisher | 한국항공우주학회 | - |
dc.title | 병렬처리 기법을 이용한 3차원 날개의 공력 최적 설계 | - |
dc.title.alternative | Parallelized Aerodynamic Desing Optimization of 3-dimensional Wing | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 28 | - |
dc.citation.issue | 4 | - |
dc.citation.beginningpage | 1 | - |
dc.citation.endingpage | 8 | - |
dc.citation.publicationname | 한국항공우주학회지 | - |
dc.embargo.liftdate | 9999-12-31 | - |
dc.embargo.terms | 9999-12-31 | - |
dc.contributor.localauthor | 권장혁 | - |
dc.contributor.nonIdAuthor | 성춘호 | - |
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