Closed-Loop Control Test of the NASA/Army/MIT Active Twist Rotor for Vibration Reduction-Reference-Cited by-同舟云学术

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Closed-Loop Control Test of the NASA/Army/MIT Active Twist Rotor for Vibration Reduction

Published:2005-04-01 Issue:2 Volume:50 Page:178-194
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Shin SangJoon,Cesnik Carlos E. S.,Hall Steven R.

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. Aeroelastic fluid dynamics assessment of performance and vibration on active twisting rotors;Aerospace Science and Technology;2024-08

2. New smart twisting active rotor (STAR): pretest predictions;CEAS Aeronautical Journal;2024-04-01

3. Vortex-Induced Stall on an Actively Twisted Highly Loaded Model Rotor Blade;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2023-09-23

4. Design and Simulation of the Linear Individual Blade Control Laws for Vibratory Loads Reduction in a Medium-size Rotorcraft;Transactions of the Korean Society for Noise and Vibration Engineering;2023-04-20

5. Numerical Analysis of HVAB and STAR Rotor Blades Using HMB3;AIAA SCITECH 2023 Forum;2023-01-19

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