Subcritical Limit Cycle in Airfoil Aeroelastic System with Freeplay: Prediction and Mechanism
Author:
Affiliation:
1. Sun Yat-sen University, 510275 Guangzhou, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference34 articles.
1. Nonlinear aeroelastic analysis of airfoils: bifurcation and chaos
2. Nonlinear Aeroelasticity and Unsteady Aerodynamics
3. Parametric Flutter Margin Method for Aeroservoelastic Stability Analysis
4. Aircraft Control Surface and Store Freeplay-Induced Vibrations in Aeroelastic Stability Envelope
5. Multi-fractality in aeroelastic response as a precursor to flutter
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