Rotor Blade Flap‐Lag Stability in Turbulent Flows-Reference-Cited by-同舟云学术

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Rotor Blade Flap‐Lag Stability in Turbulent Flows

Published:1982-04-01 Issue:2 Volume:27 Page:51-57
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Prussing J. E.¹,Lin Y. K.¹

Affiliation:

1. Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, Ill.

Publisher

American Helicopter Society

Cited by 12 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. Flight Dynamics Modeling for a Small-Scale Flybarless Helicopter UAV;AIAA Atmospheric Flight Mechanics Conference;2011-06-14

2. Random binary (coalescence) flutter of a two-dimensional linear airfoil;Journal of Fluids and Structures;2003-08

3. Structurally Nonlinear Fluttering Airfoil in Turbulent Flow;AIAA Journal;2001-10

4. Response of a Nonrotating Rotor Blade to Lateral Turbulence Part I: Theory;Journal of Aircraft;1995-01

5. Almost sure stability of dynamical systems under combined harmonic and stochastic excitations;Journal of Sound and Vibration;1991-11

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