Nonlinear Airfoil Limit Cycle Analysis Using Continuation Method and Filtered Impulse Function
Author:
Affiliation:
1. National University of Singapore, Singapore 119077, Republic of Singapore
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference27 articles.
1. LIMIT CYCLE BEHAVIOR OF AN AIRFOIL WITH A CONTROL SURFACE
2. Report No. 496, general theory of aerodynamic instability and the mechanism of flutter
3. On the aeroelastic instability of two-dimensional panels in uniform incompressible flow
4. Limit Cycle Oscillations of a Cantilevered Wing in Low Subsonic Flow
5. Nonlinear Aeroelasticity
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3. Numerical Analysis of an Airfoil with Nonlinear Stiffness Using DTM;Iranian Journal of Science and Technology, Transactions of Mechanical Engineering;2023-02-21
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