한국전산유체공학회:학술대회논문집
- 한국전산유체공학회 2008년도 춘계학술대회논문집
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- Pages.130-133
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- 2008
Trust Region 기법을 이용한 공력 형상 최적설계
The Aerodynamic Shape Optimization with Trust Region Methods
- Lee, Jae-Hun (KAIST, Department of Aerospace of Engineering) ;
- Jung, Kyung-Jin (Agency for Defense Development) ;
- Kwon, Jang-Hyuk (KAIST, Department of Aerospace of Engineering)
- 발행 : 2008.03.26
초록
In this paper the trust region method is studied and applied in aerodynamic shape optimization. The trust region method is a gradient-based optimization method, but it is not as popular as other methods in engineering computations. Its theory will be explained for unconstrained optimization problems and a trust region subproblem will be solved with the dogleg method. After verifying the trust region method with analytical test problems, it is applied to aerodynamic shape design optimization and the performance of airfoil is improved successfully.