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Statements

Subject Item
n2:RIV%2F68407700%3A21220%2F09%3A00156612%21RIV10-GA0-21220___
rdf:type
n11:Vysledek skos:Concept
dcterms:description
In this paper the numerical approximation of a two dimensional aeroelastic problem is addressed, where nonlinear effects are considered. For the flow model we use the Navier-Stokes equations, spatially discretized by the FE method and stabilized with a modification of the Galerkin Least Squares (GLS) method. The motion of the computational domain is treated with the aid of the Arbitrary Lagrangian Eulerian (ALE) method. The structure model is considered as a solid body with two degrees of freedom (bending and torsion). The motion is described with the aid of a system of nonlinear differential equations and coupled with the flow model by the strongly coupled algorithm. In this paper the numerical approximation of a two dimensional aeroelastic problem is addressed, where nonlinear effects are considered. For the flow model we use the Navier-Stokes equations, spatially discretized by the FE method and stabilized with a modification of the Galerkin Least Squares (GLS) method. The motion of the computational domain is treated with the aid of the Arbitrary Lagrangian Eulerian (ALE) method. The structure model is considered as a solid body with two degrees of freedom (bending and torsion). The motion is described with the aid of a system of nonlinear differential equations and coupled with the flow model by the strongly coupled algorithm.
dcterms:title
Numerical Simulation of Aeroelastic Problems with Consideration of Nonlinear Effects Numerical Simulation of Aeroelastic Problems with Consideration of Nonlinear Effects
skos:prefLabel
Numerical Simulation of Aeroelastic Problems with Consideration of Nonlinear Effects Numerical Simulation of Aeroelastic Problems with Consideration of Nonlinear Effects
skos:notation
RIV/68407700:21220/09:00156612!RIV10-GA0-21220___
n3:aktivita
n7:Z n7:P
n3:aktivity
P(GA201/08/0012), Z(MSM6840770003)
n3:cisloPeriodika
1
n3:dodaniDat
n9:2010
n3:domaciTvurceVysledku
n14:8416761
n3:druhVysledku
n18:J
n3:duvernostUdaju
n10:S
n3:entitaPredkladatele
n8:predkladatel
n3:idSjednocenehoVysledku
330240
n3:idVysledku
RIV/68407700:21220/09:00156612
n3:jazykVysledku
n17:eng
n3:klicovaSlova
aeroelasticity; finite element method; Arbitrary Lagrangian Eulerian method
n3:klicoveSlovo
n12:finite%20element%20method n12:aeroelasticity n12:Arbitrary%20Lagrangian%20Eulerian%20method
n3:kodStatuVydavatele
CZ - Česká republika
n3:kontrolniKodProRIV
[B2C1D952F2E1]
n3:nazevZdroje
Engineering Mechanics
n3:obor
n19:BK
n3:pocetDomacichTvurcuVysledku
1
n3:pocetTvurcuVysledku
1
n3:projekt
n4:GA201%2F08%2F0012
n3:rokUplatneniVysledku
n9:2009
n3:svazekPeriodika
16
n3:tvurceVysledku
Sváček, Petr
n3:zamer
n15:MSM6840770003
s:issn
1802-1484
s:numberOfPages
16
n6:organizacniJednotka
21220