About: Influence of Flow Models in an Aeroelastic Problem: Comparison of a Turbulence Model with a Laminar Solution of the Navier - Stokes Equations     Goto   Sponge   NotDistinct   Permalink

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Description
  • The study deals with numerical approximation of a 2D aeroelastic problem. A fully coupled formulation of flow over a freely vibrating airfoil with two degrees of freedom for rotation and translation is considered. The flow is described by the incompressible Navier-Stokes equations written in Arbitrary Lagrangian-Eulerian (ALE) form or by the Reynolds averaged Navier-Stokes system. The flow is solved by the stabilized finite element method. The developed method is verified by experimental data and the numerical results obtained for laminar and turbulent models are compared.
  • The study deals with numerical approximation of a 2D aeroelastic problem. A fully coupled formulation of flow over a freely vibrating airfoil with two degrees of freedom for rotation and translation is considered. The flow is described by the incompressible Navier-Stokes equations written in Arbitrary Lagrangian-Eulerian (ALE) form or by the Reynolds averaged Navier-Stokes system. The flow is solved by the stabilized finite element method. The developed method is verified by experimental data and the numerical results obtained for laminar and turbulent models are compared. (en)
Title
  • Influence of Flow Models in an Aeroelastic Problem: Comparison of a Turbulence Model with a Laminar Solution of the Navier - Stokes Equations
  • Influence of Flow Models in an Aeroelastic Problem: Comparison of a Turbulence Model with a Laminar Solution of the Navier - Stokes Equations (en)
skos:prefLabel
  • Influence of Flow Models in an Aeroelastic Problem: Comparison of a Turbulence Model with a Laminar Solution of the Navier - Stokes Equations
  • Influence of Flow Models in an Aeroelastic Problem: Comparison of a Turbulence Model with a Laminar Solution of the Navier - Stokes Equations (en)
skos:notation
  • RIV/68407700:21220/08:00145770!RIV11-MSM-21220___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(IAA200760613), Z(AV0Z20760514), Z(MSM0021620839), Z(MSM6840770003)
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 372113
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21220/08:00145770
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Arbitrary Lagrangian-Eulerian formulation; aeroelasticity; finite element method (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [1A3E451C2EE5]
http://linked.open...v/mistoKonaniAkce
  • Praha
http://linked.open...i/riv/mistoVydani
  • Praha
http://linked.open...i/riv/nazevZdroje
  • Flow - Induced Vibration
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...vavai/riv/projekt
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Feistauer, Miloslav
  • Horáček, Jaromír
  • Sváček, Petr
http://linked.open...vavai/riv/typAkce
http://linked.open...ain/vavai/riv/wos
  • 000283472100083
http://linked.open.../riv/zahajeniAkce
http://linked.open...n/vavai/riv/zamer
number of pages
http://purl.org/ne...btex#hasPublisher
  • Ústav termomechaniky AV ČR
https://schema.org/isbn
  • 978-80-87012-12-3
http://localhost/t...ganizacniJednotka
  • 21220
is http://linked.open...avai/riv/vysledek of
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