On the dynamic stability of an elastically fixed high-drag airfoil under vortical parametric excitations


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Abstract

Conditions of dynamic instability at parametric resonance in an oscillatory system with three degrees of freedom, which models the motion of an elastically fixed high-drag airfoil under unsteady aerohydrodynamic loads due to the vortex trail separation, are obtained in the linear approximation.

About the authors

I. K. Marchevskii

Bauman Moscow State Technical University

Author for correspondence.
Email: iliamarchevsky@mail.ru
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005

G. A. Shcheglov

Bauman Moscow State Technical University

Email: iliamarchevsky@mail.ru
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005

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