병렬처리 기법을 이용한 3차원 날개의 공력 최적 설계Parallelized Aerodynamic Desing Optimization of 3-dimensional Wing

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dc.contributor.author성춘호ko
dc.contributor.author권장혁ko
dc.date.accessioned2010-05-18T02:48:29Z-
dc.date.available2010-05-18T02:48:29Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2000-01-
dc.identifier.citation한국항공우주학회지, v.28, no.4, pp.1 - 8-
dc.identifier.issn1225-1348-
dc.identifier.urihttp://hdl.handle.net/10203/18414-
dc.description.abstractAn 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.sponsorship본 연구는 과학기술부 특정연구과제 `신기술 설계기술 및 파손예방`의 일부 지원으로 수행되었음을 밝힌다.en
dc.languageKorean-
dc.language.isokoen
dc.publisher한국항공우주학회-
dc.title병렬처리 기법을 이용한 3차원 날개의 공력 최적 설계-
dc.title.alternativeParallelized Aerodynamic Desing Optimization of 3-dimensional Wing-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume28-
dc.citation.issue4-
dc.citation.beginningpage1-
dc.citation.endingpage8-
dc.citation.publicationname한국항공우주학회지-
dc.embargo.liftdate9999-12-31-
dc.embargo.terms9999-12-31-
dc.contributor.localauthor권장혁-
dc.contributor.nonIdAuthor성춘호-
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AE-Journal Papers(저널논문)
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