Application of a New Compressible Time Domain Aerodynamic Model to Vibration Reduction in Helicopters Using an Actively Controlled Flap-Reference-Cited by-同舟云学术

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Application of a New Compressible Time Domain Aerodynamic Model to Vibration Reduction in Helicopters Using an Actively Controlled Flap

Published:2001-01-01 Issue:1 Volume:46 Page:32-43
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Myrtle Timothy F.,Friedmann Peretz P.

Publisher

American Helicopter Society

Cited by 49 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. Vibration Reduction in Rotorcraft Using Closed-loop Active Flow Control;Journal of the American Helicopter Society;2022-07-01

2. Airfoil Dynamic Stall Model Suitable for Large Angle Deflection of a Trailing Edge Flap;Fluid Dynamics;2022-06

3. Vibration Reduction on Helicopter Rotors Using Open-Loop Flow Control;AIAA Journal;2021-08-23

4. Vibration Reduction on Helicopter Rotors Using Open Loop Flow Control;AIAA Scitech 2021 Forum;2021-01-04

5. Application of a CFD-Based Surrogate Approach for Active Flow Control Modeling;AIAA Scitech 2019 Forum;2019-01-06

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