한국전산유체공학회:학술대회논문집
- 1998.05a
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- Pages.61-66
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- 1998
Subsonic/Transonic Airfoil Design Using an Inverse Method
Inverse 기법을 이용한 아음속/천음속 익형 설계
- Published : 1998.05.01
Abstract
An inverse method for the subsonic and transonic airfoil design was developed using the Euler equations. Two testcases were performed. One was a design of the supercritical airfoil, aiming to be used for the Korean mid-sized (100 passengers class) transport aircraft. The other was the design of an airfoil showing a good cruising performance (L/D ratio) in the high subsonic/transonic flow regimes. These testcases demonstrated the efficiency and the robustness of the developed method.
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