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Statements

Subject Item
n2:RIV%2F68407700%3A21220%2F09%3A00156468%21RIV10-GA0-21220___
rdf:type
n22:Vysledek skos:Concept
dcterms:description
The subject of the paper is the numerical simulation of the interaction of two-dimensional incompressible viscous flow and a vibrating airfoil with large amplitudes. A solid airfoil with three degrees of freedom performs rotation around an elastic axis and oscillations in the vertical direction and rotation of a flap. The numerical simulation consists of the finite element solution of the Navier-Stokes equations coupled with a system of ordinary differential equations describing the airfoil motion. The time-dependent computational domain and a moving grid are treated by the Arbitrary Lagrangian-Eulerian formulation of the Navier-Stokes equations. High Reynolds numbers require the application of a suitable stabilization of the finite element discretization. The subject of the paper is the numerical simulation of the interaction of two-dimensional incompressible viscous flow and a vibrating airfoil with large amplitudes. A solid airfoil with three degrees of freedom performs rotation around an elastic axis and oscillations in the vertical direction and rotation of a flap. The numerical simulation consists of the finite element solution of the Navier-Stokes equations coupled with a system of ordinary differential equations describing the airfoil motion. The time-dependent computational domain and a moving grid are treated by the Arbitrary Lagrangian-Eulerian formulation of the Navier-Stokes equations. High Reynolds numbers require the application of a suitable stabilization of the finite element discretization.
dcterms:title
Nonlinear Interaction of Incompressible Flow and a Vibrating Airfoil with Three Degrees of Freedom Nonlinear Interaction of Incompressible Flow and a Vibrating Airfoil with Three Degrees of Freedom
skos:prefLabel
Nonlinear Interaction of Incompressible Flow and a Vibrating Airfoil with Three Degrees of Freedom Nonlinear Interaction of Incompressible Flow and a Vibrating Airfoil with Three Degrees of Freedom
skos:notation
RIV/68407700:21220/09:00156468!RIV10-GA0-21220___
n4:aktivita
n15:P n15:Z
n4:aktivity
P(GA201/08/0012), P(IAA200760613), Z(AV0Z20760514)
n4:dodaniDat
n7:2010
n4:domaciTvurceVysledku
n6:8416761
n4:druhVysledku
n11:D
n4:duvernostUdaju
n20:S
n4:entitaPredkladatele
n21:predkladatel
n4:idSjednocenehoVysledku
329713
n4:idVysledku
RIV/68407700:21220/09:00156468
n4:jazykVysledku
n10:eng
n4:klicovaSlova
aero-elasticity; flutter; Navier-Stokes equations; Arbitrary Lagrangian-Eulerian formulation; finite element method; stabilization for high Reynolds numbers
n4:klicoveSlovo
n5:aero-elasticity n5:flutter n5:Arbitrary%20Lagrangian-Eulerian%20formulation n5:stabilization%20for%20high%20Reynolds%20numbers n5:Navier-Stokes%20equations n5:finite%20element%20method
n4:kontrolniKodProRIV
[2878E5AE073D]
n4:mistoKonaniAkce
Podbanske
n4:mistoVydani
Bratislava
n4:nazevZdroje
Algoritmy 2009 Proceedings of Contributed Papers and Posters
n4:obor
n14:BK
n4:pocetDomacichTvurcuVysledku
1
n4:pocetTvurcuVysledku
4
n4:projekt
n13:IAA200760613 n13:GA201%2F08%2F0012
n4:rokUplatneniVysledku
n7:2009
n4:tvurceVysledku
Sváček, Petr
n4:typAkce
n12:WRD
n4:wos
000267157200027
n4:zahajeniAkce
2009-03-15+01:00
n4:zamer
n8:AV0Z20760514
s:numberOfPages
10
n17:hasPublisher
Slovenská technická univerzita v Bratislave. Stavebná fakulta
n16:isbn
978-80-227-3032-7
n18:organizacniJednotka
21220