Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled Flap | ORKG Ask

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Alleviation of dynamic stall induced vibrations in helicopter rotors using actively controlled flaps.

Depailler, Gilles

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Alleviation of dynamic stall induced vibrations in helicopter rotors using actively controlled flaps.

Depailler, Gilles

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This work presents a treatment of the helicopter vibration reduction problem at high advance ratios,...

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Helicopters suffer from severe vibration levels compared to fixed-wing aircraft. The main source of ...