Vibration Reduction on Helicopter Rotors Using Open-Loop Flow Control-Reference-Cited by-同舟云学术

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Vibration Reduction on Helicopter Rotors Using Open-Loop Flow Control

Published:2021-08-23 Issue: Volume: Page:1-16
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Patterson Ryan P.¹^ORCID,Friedmann Peretz P.¹

Affiliation:

1. University of Michigan, Ann Arbor, Michigan 48109-2140

Funder

U.S. Army Aviation Development Directorate, Combat Capabilities Development Command, Aviation and Missile Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060717

Reference34 articles.

1. On-Blade Control of Rotor Vibration, Noise, and Performance: Just Around the Corner? The 33rd Alexander Nikolsky Honorary Lecture

2. Simultaneous Vibration and Noise Reduction in Rotorcraft Using Aeroelastic Simulation

3. Trailing-Edge Flaps for Rotor Performance Enhancement and Vibration Reduction

4. Wind-Tunnel Testing of Rotor with Individually Controlled Trailing-Edge Flaps for Vibration Reduction

Cited by 2 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. Aerodynamics and vibration analysis of a helicopter rotor blade;Acta Mechanica;2024-02-27

2. Open-loop flow control design guided by the amplitude-frequency characteristics of the reduced-order model;Physics of Fluids;2023-12-01

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