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데이터베이스 기반 유전 알고리즘을 이용한 효율적인 에어포일 형상 최적화에 대한 연구

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dc.contributor.author김수환-
dc.contributor.author권장혁-
dc.contributor.author김진-
dc.date.accessioned2021-08-03T06:42:11Z-
dc.date.available2021-08-03T06:42:11Z-
dc.date.issued2007-01-20-
dc.identifier.urihttps://www.kriso.re.kr/sciwatch/handle/2021.sw.kriso/1475-
dc.description.abstractGenetic Algorithms(GA) have some difficulties in practical applications because of too many function evaluations. To overcome these limitations, an approximated modeling method such as Response Surface Modeling(RSM) is coupled to GAs. Original RSM method predicts linear or convex problems well but it is not good for highly nonlinear problems cause of the average effect of the least square method(LSM). So the locally approximated methods, so called as moving least squares method(MLSM) have been used to reduce the error of LSM. In this study, the efficient evolutionary GAs tightly coupled with RSM with MLSM are constructed and then a 2-dimensional inviscid airfoil shape optimization is performed to show its efficiency.-
dc.format.extent9-
dc.language한국어-
dc.language.isoKOR-
dc.publisher한국마린엔지니어링학회-
dc.title데이터베이스 기반 유전 알고리즘을 이용한 효율적인 에어포일 형상 최적화에 대한 연구-
dc.title.alternativeStudy on the Airfoil Shape Design Optimization Using Database based Genetic Algorithms-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.bibliographicCitation한국마린엔지니어링학회지, v.31, no.1, pp 58 - 66-
dc.citation.title한국마린엔지니어링학회지-
dc.citation.volume31-
dc.citation.number1-
dc.citation.startPage58-
dc.citation.endPage66-
dc.description.isOpenAccessN-
dc.subject.keywordAuthorDesign optimization-
dc.subject.keywordAuthorGenetic algorithm-
dc.subject.keywordAuthorResponse surface modeling-
dc.subject.keywordAuthorMoving least squares method-
dc.subject.keywordAuthorCFD-
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