An airfoil having a leading-edge and a trailing edge as well as a suction side and a pressure side is provided. The suction side including 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. A method of operating an aircraft using such airfoil is also provided.
AIRFOIL WITH AUGMENTED LIFT
SCHAUFEL MIT ERHÖHTEM AUFTRIEB
SURFACE PORTANTE À PORTANCE AUGMENTÉE
2023-10-25
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |