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
- 김수환; 권장혁; 김진
- 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.
- Files in This Item
- There are no files associated with this item.
- Appears in
Collections - ETC > 1. Journal Articles
Items in ScholarWorks are protected by copyright, with all rights reserved, unless otherwise indicated.