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- W796041605 abstract "An inverse method for the subsonic and transonic airfoil design was developed using the Euler equations. Two testcases were performed. One was a verification of the method using the supercritical airfoil of 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 flow regime. These testcases demonstrated the efficiency and the robustness of the design method in the present study." @default.
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- W796041605 date "1998-01-01" @default.
- W796041605 modified "2023-09-24" @default.
- W796041605 title "Subsonic/Transonic Airfoil Design Using an Inverse Method" @default.
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