Noise Abatement Flight Procedure Design for Helicopter Approach based on Acoustic Mode
Author:
Affiliation:
1. National Key Laboratory of Helicopter Aeromechanics/Nanjing university of Aeronautics and Astronautics,, China
2. National Key Laboratory of Helicopter Aeromechanics/Nanjing university of Aeronautics and Astronautics, China
Publisher
ACM
Link
https://dl.acm.org/doi/pdf/10.1145/3669721.3674529
Reference22 articles.
1. B. Edwards, C. Cox, F. Worth, Revolutionary Concepts for Helicopter Noise Reduction — S.I.L.E.N.T. Program, Contract. (2002).
2. A STUDY OF THE ORIGIN AND MEANS OF REDUCING HELICOPTER NOISE
3. Flight-Path Management/Control Methodology to Reduce Helicopter Blade-Vortex Interaction Noise
4. Dynamic Replanning of Low Noise Rotorcraft Operations
5. Numerical optimization of helicopter rotor aerodynamic performance in hover
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