On approximation of an aeroelastic problem in post-critical regimes

0356795 - ÚT 2012 RIV CZ eng C - Konferenční příspěvek (zahraniční konf.)
Sváček, P. - Horáček, Jaromír
On approximation of an aeroelastic problem in post-critical regimes.
Conference Topical Problems of Fluid Mechanics 2011. Prague: Institute of Thermomechanics AS CR, v. v. i., 2011 - (Příhoda, J.; Kozel, K.), s. 109-112. ISBN 978-80-87012-32-1.
[Topical problems of fluid mechanics 2011. Prague (CZ), 16.02.2011-17.02.2011]
Grant CEP: GA ČR(CZ) GAP101/11/0207
Výzkumný záměr: CEZ:AV0Z20760514
Klíčová slova: aeroelastcity * flutter * FEM
Kód oboru RIV: BI - Akustika a kmity

This paper focused on the mathematical modelling and the numerical approximation of interactions of a simplified problem of the two-dimensional flow and flexibly supported airfoil section with control section. The flow is modelled with the aid of the incompressible Navier-Stokes equations and for the approximation the stabilized finite element method is used. The structure motion is described with the aid of nonlinear ordinary differential equations. The time-dependent computational domain is taken into account by the Arbitrary Lagrangian-Eulerian method.
Trvalý link: http://hdl.handle.net/11104/0195225