Technical Notes: Reduction of Blade‐Vortex Interaction Noise Through Higher Harmonic Pitch Control-Reference-Cited by-同舟云学术

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Technical Notes: Reduction of Blade‐Vortex Interaction Noise Through Higher Harmonic Pitch Control

Published:1990-01-01 Issue:1 Volume:35 Page:86-91
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Brooks Thomas F.¹,Booth Earl R.¹,Jolly J. Ralph¹,Yeager William T.¹,Wilbur Matthew L.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Va.

Publisher

American Helicopter Society

Cited by 23 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Review of Control Technologies for Quiet Operations of Advanced Air-Mobility;Applied Sciences;2023-02-16

2. Active Noise Control of Multirotor Advanced Air Mobility Vehicles;Journal of the American Helicopter Society;2022

3. Fundamental investigation using active plasma control to reduce blade–vortex interaction noise;International Journal of Aeroacoustics;2021-11

4. Localized Individual Blade Root Pitch Control for Helicopter Blade—Vortex Interaction Noise Reduction;Journal of the American Helicopter Society;2010-07-01

5. Tip Vortex Control via a Tab Deflecting at Higher Harmonic Frequencies;AIAA Journal;2008-06

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