A wing structure for an aircraft includes a stationary wing, a flap extendable so as to form an air flow path between the flap and the stationary wing, and at least one plasma actuator. The plasma actuator is configured to induce, while the flap is extended, air flow for suppressing or reducing separation of air on an upper surface of the flap including air flowing from a lower surface of the stationary wing to the upper surface of the flap via the flow path.
WING STRUCTURE, METHOD OF CONTROLLING WING STRUCTURE, AND AIRCRAFT
2019-10-31
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
WING STRUCTURE, METHOD OF CONTROLLING WING STRUCTURE, AND AIRCRAFT
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