초록

The optimum wing flow is thereby maintained more exactly. For transonic wings, the position and strength of compression shocks is also effectively controlled, which leads to a reduction of the direct shock induced separation.

대표청구항 ▼

[ We claim:] [1.] A method of optimizing an aerodynamic effect of an airfoil of an aircraft, wherein said airfoil has an adjustable camber that can be adjusted by actuating a camber motor system, wherein said method comprises:a) measuring with sensors a pressure distribution on said airfoil to provi

[ We claim:] [1.] A method of optimizing an aerodynamic effect of an airfoil of an aircraft, wherein said airfoil has an adjustable camber that can be adjusted by actuating a camber motor system, wherein said method comprises:a) measuring with sensors a pressure distribution on said airfoil to provide a plurality of measured pressure values;b) comparing said measured pressure values with corresponding stored optimal pressure reference values;c) forming differential values between said measured pressure values and said stored optimal pressure reference values;d) actuating said camber motor system to adjust said camber; ande) repeating said steps a) to d) until said differential values are approximately or exactly zero.