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Helicopter Blade-Vortex Interaction Noise Reduction by Active Rotor Control Technology.
Helicopter Blade-Vortex Interaction Noise Reduction by Active Rotor Control Technology.
1997
Yung H. Yu
B. Gmelin
W.R. Splettstößer
Jean Jacques Philippe
J. Prieur
Thomas F. Brooks
Keywords:
Noise reduction
Helicopter rotor
Aerospace engineering
Rotor (electric)
Vortex
Engineering
Correction
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