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Statements

Subject Item
n2:RIV%2F44555601%3A13420%2F12%3A43884542%21RIV13-MSM-13420___
rdf:type
n5:Vysledek skos:Concept
rdfs:seeAlso
http://ctn.cvut.cz/ap/index.php?year=2012&idissue=83
dcterms:description
This paper deals with a numerical solution of the interaction of two-dimensional (2-D) incompressible viscous flow and a vibrating profile NACA 0012 with large amplitudes. The laminar flow is described by the Navier-Stokes equations in the arbitrary Lagrangian-Eulerian form. The profile with two degrees of freedom (2-DOF) can rotate around its elastic axis and oscillate in the vertical direction. Its motion is described by a nonlinear system of two ordinary differential equations. Deformations of the computational domain due to the profile motion are treated by the arbitrary Lagrangian-Eulerian method. The finite volume method and the finite element method are applied, and the numerical results are compared. This paper deals with a numerical solution of the interaction of two-dimensional (2-D) incompressible viscous flow and a vibrating profile NACA 0012 with large amplitudes. The laminar flow is described by the Navier-Stokes equations in the arbitrary Lagrangian-Eulerian form. The profile with two degrees of freedom (2-DOF) can rotate around its elastic axis and oscillate in the vertical direction. Its motion is described by a nonlinear system of two ordinary differential equations. Deformations of the computational domain due to the profile motion are treated by the arbitrary Lagrangian-Eulerian method. The finite volume method and the finite element method are applied, and the numerical results are compared.
dcterms:title
Simulation of Free Airfoil Vibrations in Incompressible Viscous Flow - Comparison of FEM and FVM Simulation of Free Airfoil Vibrations in Incompressible Viscous Flow - Comparison of FEM and FVM
skos:prefLabel
Simulation of Free Airfoil Vibrations in Incompressible Viscous Flow - Comparison of FEM and FVM Simulation of Free Airfoil Vibrations in Incompressible Viscous Flow - Comparison of FEM and FVM
skos:notation
RIV/44555601:13420/12:43884542!RIV13-MSM-13420___
n5:predkladatel
n6:orjk%3A13420
n3:aktivita
n21:Z n21:I n21:P
n3:aktivity
I, P(GAP101/11/0207), P(GAP101/12/1271), Z(AV0Z20760514), Z(MSM6840770003)
n3:cisloPeriodika
6/2012
n3:dodaniDat
n16:2013
n3:domaciTvurceVysledku
n13:1116061
n3:druhVysledku
n4:J
n3:duvernostUdaju
n19:S
n3:entitaPredkladatele
n17:predkladatel
n3:idSjednocenehoVysledku
168007
n3:idVysledku
RIV/44555601:13420/12:43884542
n3:jazykVysledku
n14:eng
n3:klicovaSlova
arbitrary Lagrangian-Eulerian method, nonlinear aeroelasticity; finite element method; finite volume method; laminar flow
n3:klicoveSlovo
n15:laminar%20flow n15:arbitrary%20Lagrangian-Eulerian%20method n15:finite%20element%20method n15:finite%20volume%20method n15:nonlinear%20aeroelasticity
n3:kodStatuVydavatele
CZ - Česká republika
n3:kontrolniKodProRIV
[D0328BEB7156]
n3:nazevZdroje
Acta Polytechnica
n3:obor
n20:BK
n3:pocetDomacichTvurcuVysledku
1
n3:pocetTvurcuVysledku
4
n3:projekt
n12:GAP101%2F11%2F0207 n12:GAP101%2F12%2F1271
n3:rokUplatneniVysledku
n16:2012
n3:svazekPeriodika
52
n3:tvurceVysledku
Sváček, Petr Honzátko, Radek Horáček, Jaromír Kozel, Karel
n3:zamer
n9:MSM6840770003 n9:AV0Z20760514
s:issn
1210-2709
s:numberOfPages
11
n18:organizacniJednotka
13420