According to an embodiment disclosed herein, a gurney flap assembly includes an actuator, and a flexible body attaching to the actuator, the body having a downwardly depending flap for moving into and out of an airstream in a pressure side of a wing, wherein the flexible body flexes in reaction to motion of the actuator. This increases the lift force of the rotor blade, wing or aerofoil blade.
ACTIVE GURNEY FLAP
VOLET GURNEY ACTIF
16.06.2015
Patent
Elektronische Ressource
Englisch
Springer Verlag | 2017
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