Wind Tunnel Test of the SMART Active Flap Rotor-Reference-Cited by-同舟云学术

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Wind Tunnel Test of the SMART Active Flap Rotor

Published:2018 Issue: Volume: Page:
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Straub Friedrich K.,Anand Vaidyanathan R.,Lau Benton H.,Birchette Terrence S.

Publisher

American Helicopter Society

Cited by 25 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. Simultaneous Vibration Reduction and Performance Improvement of Helicopter Rotor Using Individual Blade Pitch Control with Multiple Harmonic Inputs;International Journal of Aeronautical and Space Sciences;2024-05-10

2. Investigation of Smart Nano Rotor with Continuous Trailing Edge Flap Driven by Electroactive Polymer;Lecture Notes in Electrical Engineering;2024

3. A directly coil-actuated cyclic pitch control based rotor: Design, modeling, and analysis;Aerospace Science and Technology;2023-09

4. Modeling and experimental study on orientation dynamics of a Mars rotorcraft with swashplate mechanism;Aerospace Science and Technology;2023-07

5. Open-Loop Simulation of Active Vibration Control of Electrically Controlled Rotor;Machines;2023-02-06

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