"Nonlinear Feedback of Incompressible Fluid and the Airfoil with Three Degrees of Freedom" . . "Sv\u00E1\u010Dek, Petr" . . "Hor\u00E1\u010Dek, Jarom\u00EDr" . . . . "978-80-87012-08-6" . . "[91496A6A8BC0]" . . "67;72" . "RIV/68407700:21220/07:02135877" . "Neline\u00E1rn\u00ED zp\u011Btn\u00E1 vazba mezi nestla\u010Ditelnou tekutinou a leteck\u00FDm nosn\u00EDkem se t\u0159emi stupni volnosti"@cs . "P(IAA200760613), S, Z(AV0Z20760514)" . . "1"^^ . . . "Nonlinear Feedback of Incompressible Fluid and the Airfoil with Three Degrees of Freedom" . "Feistauer, Miloslav" . "RIV/68407700:21220/07:02135877!RIV08-MSM-21220___" . "4"^^ . . "In this paper the incompressible viscous fluid flow is coupled with structure model with three degrees of freedom. The structure represents a flexibly supported rigid airfoil with control section. The motion equations are derived for large vibration amplitudes. Preliminary results for numerical simulation of flow-induced airfoil vibrations in a laminar incompressible flow are presented for the NACA profile 0012."@en . . "V tomto \u010Dl\u00E1nku je uva\u017Eov\u00E1n probl\u00E9m nestla\u010Diteln\u00E9ho vazk\u00E9ho proud\u011Bn\u00ED spojen\u00FD se strukturou popsanou pomoc\u00ED t\u0159\u00ED stup\u0148\u016F volnosti. Struktura reprezentuje v tomto p\u0159\u00EDpad\u011B pru\u017En\u011B uchycen\u00FD nosn\u00EDk s klapkou na odtokov\u00E9 \u010D\u00E1sti. Rovnice jsou uva\u017Eov\u00E1ny pro p\u0159\u00EDpad velk\u00FDch v\u00FDchylek. Jsou uvedeny p\u0159edb\u011B\u017En\u00E9 v\u00FDsledky pro profil NACA 0012 se t\u0159emi stupni volnosti."@cs . . . "437514" . "Proceedings Interaction and Feedbacks 2007" . "Praha" . "Nonlinear Feedback of Incompressible Fluid and the Airfoil with Three Degrees of Freedom"@en . "21220" . "In this paper the incompressible viscous fluid flow is coupled with structure model with three degrees of freedom. The structure represents a flexibly supported rigid airfoil with control section. The motion equations are derived for large vibration amplitudes. Preliminary results for numerical simulation of flow-induced airfoil vibrations in a laminar incompressible flow are presented for the NACA profile 0012." . "Nonlinear Feedback of Incompressible Fluid and the Airfoil with Three Degrees of Freedom"@en . "Praha" . "\u00DAstav termomechaniky AV \u010CR" . "Arbitrary Lagrangian Eulerian method; finite element method; incompressible fluid flow"@en . . "6"^^ . . . "R\u016F\u017Ei\u010Dka, M." . "Neline\u00E1rn\u00ED zp\u011Btn\u00E1 vazba mezi nestla\u010Ditelnou tekutinou a leteck\u00FDm nosn\u00EDkem se t\u0159emi stupni volnosti"@cs . . . "2007-11-27+01:00"^^ .