Synthesis of Active Twist Controller for Rotor Blade–Vortex Interaction Noise Alleviation
Author:
Affiliation:
1. Roma Tre University, Rome, Italy
2. The National Research Council (CNR), Rome, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033330
Reference23 articles.
1. Rotor blade–vortex interaction noise
2. Simultaneous Vibration and Noise Reduction in Rotorcraft Using Aeroelastic Simulation
3. Reduction of helicopter blade-vortex interaction noise by active rotor control technology
4. Key Results From a Higher Harmonic Control Aeroacoustic Rotor Test (HART)
5. Closed loop IBC results from CH-53G flight tests
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2. Review of Control Technologies for Quiet Operations of Advanced Air-Mobility;Applied Sciences;2023-02-16
3. Impact of optimized variable rotor speed and active blade twist control on helicopter blade–vortex interaction noise and environmental impact;Journal of Fluids and Structures;2021-07
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