Disclosed is an airfoil having a leading edge and a trailing edge as well as a suction side and a pressure side, the suction side comprising an injector slot towards the leading edge. There may be at least one additional slot towards the trailing edge. The airfoil may be configured for an aircraft. Also disclosed is a method of operating an aircraft using such airfoil.
AIRFOIL WITH AUGMENTED LIFT
2023-06-22
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |