Method and apparatus for optimizing the aerodynamic effect of an

Aeronautics and astronautics – Aircraft control – Automatic

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Details

244203, 244213, 244219, 244 35A, 701 3, B64C 1316

Patent

active

058759980

ABSTRACT:
A method and an apparatus are provided for optimizing the aerodynamic effect of the airfoil of an aircraft by defined changes in camber. The method includes the following steps:

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