한국전산유체공학회:학술대회논문집
- 2008.03a
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- Pages.227-228
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- 2008
DESIGN OF HIGH LIFT FLAP WITH OPTIMIZATION TECHNIQUE
최적화 기법을 이용한 고양력 플랩 설계
Abstract
In the present paper, fowler flap was optimized to maximize the lift with response surface method. Leading edge shape and the gap between main airfoil and flap, were optimized and the aerodynamic characteristics was improved considerably. The optimized flap has more rounded leading edge and bigger gap. Before angle of attack,
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