Numerical study of the rotor thickness noise reduction based on the concept of sound field cancellation-Reference-Cited by-同舟云学术

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Numerical study of the rotor thickness noise reduction based on the concept of sound field cancellation

Published:2022-03 Issue:3 Volume:35 Page:214-233
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

XIA Runze^ORCID,SHI Yongjie,LI Teng,XU Guohua

Funder

National Natural Science Foundation of China

Aeronautical Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference37 articles.

1. Helicopter noise prediction: The current status and future direction;Brentner;J Sound Vib,1994

2. ICCAIA, NASA, DLR, et al. Helicopter noise reduction technology status report [Internet]. Montreal, Canada: ICAO. Available from: [updated 2016 Apr 18; cited 2020 Oct 26].

3. Revolutionary concepts for helicopter noise reduction: SILENT Program;Edwards,2002

4. Passive design for reduction of high-speed impulsive rotor noise;Baeder;J Am Helicopter Soc,1998

5. Rotor blade-vortex interaction noise;Yu;Prog Aerosp Sci,2000

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1. Noise attenuation of frequency-modulated multi-rotor using sound field reproduction;Chinese Journal of Aeronautics;2023-07

2. An Experimental Study on Rotor Aerodynamic Noise Control Based on Active Flap Control;Aerospace;2023-01-27

3. A Dynamic RCS and Noise Prediction and Reduction Method of Coaxial Tilt-Rotor Aircraft Based on Phase Modulation;Sensors;2022-12-11

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