Wind Tunnel Results Showing Rotor Vibratory Loads Reduction Using Higher Harmonic Blade Pitch-Reference-Cited by-同舟云学术

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Wind Tunnel Results Showing Rotor Vibratory Loads Reduction Using Higher Harmonic Blade Pitch

Published:1983-01-01 Issue:1 Volume:28 Page:10-15
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Hammond C. E.

Publisher

American Helicopter Society

Cited by 32 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. Active Twist Control of Smart Helicopter Rotor - A Survey;Journal of Aerospace Sciences and Technologies;2023-08-11

2. Controlled Aerodynamic Loads at Low Angles of Attack using Fluidic Actuation;AIAA Scitech 2019 Forum;2019-01-06

3. Pressure feedback-based blade–vortex interaction noise controller for helicopter rotors;International Journal of Aeroacoustics;2018-04

4. Adaptive control of tonal disturbance in mechanical systems with nonlinear damping;Journal of Vibration and Control;2016-08-09

5. Introduction;Smart Helicopter Rotors;2015-12-16

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