Wing Rock Due to Aerodynamic Hysteresis
Author:
Affiliation:
1. Naval Postgraduate School, Monterey, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58495
Reference9 articles.
1. Investigation of Nonlinear Motion Experienced on a Slender-Wing Research Aircraft
2. THE SQUARE PRISM AS AN AEROELASTIC NON-LINEAR OSCILLATOR
3. Analysis of Helicopter Rotor Blade Stall Flutter
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