Study of Active Rotor Control for In-Plane Rotor Noise Reduction-Reference-Cited by-同舟云学术

Study of Active Rotor Control for In-Plane Rotor Noise Reduction

Published:2019-01 Issue:1 Volume:56 Page:179-190
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Yang Tianxiao¹,Brentner Kenneth S.²,Corle Ethan²,Schmitz Sven²

Affiliation:

1. Aero Engine Academy of China, 101304 Beijing, People’s Republic of China

2. The Pennsylvania State University, University Park, Pennsylvania 16802

Funder

U.S. Government

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034873

Reference16 articles.

1. Helicopter Noise Prediction: The Current Status and Future Direction

2. Helicopter Thickness Noise Reduction Possibilities Through Active On-Blade Acoustic Control

3. Reduced In-Plane, Low-Frequency Noise of an Active Flap Rotor

4. Fundamental Experimental Studies Supporting On-Blade Tip Air Blowing Control of In-Plane Rotor Harmonic Noise

5. SargentD. C. “Active Jet Acoustic Control of Low Frequency, In-Plane Helicopter Harmonic Noise,” Ph.D. Dissertation, Dept. of Aerospace Engineering, Univ. of Maryland, College Park, MD, 2012.

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