Method of controlling deflection of wing flaps on glider, involves varying relative flap extension with degree of deployment

摘要

The method of controlling the deflection of the wing flaps on a glider or motor glider has both flaps extending in the same direction. In dependence on the value of the flap extension, the difference between the individual deflections can be varied. The alteration of the flap extensions can reduce laminar depression effects. Claims include a control and an aircraft using the method.