Investigation on a High-Frequency Controller for Rotor BVI Noise Alleviation

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At the most fundamental level, main rotor loading noise is caused by the harmonically-varying aerodynamic loads (acoustic pressures) exerted by the rotating blades on the air. Rotorcraft main rotor noise is therefore, in principle, a function of rotor control inputs, and thus the forces and moments required to achieve steady, or “trim”, flight equilibrium. In certain flight conditions, the ensu...

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ژورنال

عنوان ژورنال: The International Journal of Acoustics and Vibration

سال: 2016

ISSN: 1027-5851,2415-1408

DOI: 10.20855/ijav.2016.21.3416