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데이터베이스 기반 유전 알고리즘을 이용한 효율적인 에어포일 형상 최적화에 대한 연구Study on the Airfoil Shape Design Optimization Using Database based Genetic Algorithms

Other Titles
Study on the Airfoil Shape Design Optimization Using Database based Genetic Algorithms
Authors
김수환권장혁김진
Issue Date
20-1월-2007
Publisher
한국마린엔지니어링학회
Keywords
Design optimization; Genetic algorithm; Response surface modeling; Moving least squares method; CFD
Citation
한국마린엔지니어링학회지, v.31, no.1, pp 58 - 66
Pages
9
Journal Title
한국마린엔지니어링학회지
Volume
31
Number
1
Start Page
58
End Page
66
URI
https://www.kriso.re.kr/sciwatch/handle/2021.sw.kriso/1475
Abstract
Genetic 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.
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