Eigenvalue analysis for predicting the onset of multiple subcritical limit cycles of an airfoil with a control surface

DOI10.1007/S11071-020-06172-7zbMath1516.74105OpenAlexW3119537587MaRDI QIDQ6166399

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Publication date: 2 August 2023

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11071-020-06172-7

zbMATH Keywords

airfoilaeroelasticgeneralized Jacobian matrixfreeplay control surfacesubcritical limit cycle

Mathematics Subject Classification ID

Spectral and related methods applied to problems in solid mechanics (74S25) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Cites Work

• Unnamed Item
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• Bifurcations of non-smooth systems
• Homotopy analysis method for limit cycle flutter of airfoils
• Bifurcation phenomena in non-smooth dynamical systems
• A reduced-order cyclic method for computation of limit cycles
• The secondary bifurcation of an aeroelastic airfoil motion: effect of high harmonics
• APPLICATION OF THE CENTRE MANIFOLD THEORY IN NON-LINEAR AEROELASTICITY
• Bifurcations in Nonsmooth Dynamical Systems
• The flutter of an airfoil with cubic structural and aerodynamic non-linearities

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