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Eigenvalue analysis for predicting the onset of multiple subcritical limit cycles of an airfoil with a control surface
Authors:Chen  Y M  Li  W L  Yan  B F  Liu  J K
Institution:1.Department of Mechanics, Sun Yat-sen University, No. 135 Xingang Road, Guangzhou, 510275, China
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Abstract:Nonlinear Dynamics - The aeroelastic system of an airfoil with a control surface usually encounters non-smooth nonlinearities such as freeplay. Freeplay can have a significant influence on...
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