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Numerical simulation of aeroelastic problems

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F04%3A00103600" target="_blank" >RIV/61388998:_____/04:00103600 - isvavai.cz</a>

  • Result on the web

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Numerical simulation of aeroelastic problems

  • Original language description

    The interaction of two dimensional incompressible viscous laminar flow with a vibrating airfoil is studied.The airfoil can rotate and oscillate in vertical direction. The numerical simulation consists of discretization and stabilization of the Navier-Stokes equations for high Reynolds numbers. In order to take the grid motion into account the Arbitrary Lagrangian-Eulerian formulation of the Navier-Stokes equations is used.

  • Czech name

    Numerická simulace aeroelastických problémů

  • Czech description

    Tento článek se zabývá dvourozměrným nestlačitelným vazkým laminárním proudění okolo vibrujícího leteckého profilu, který se může otáčet okolo své elastické osy a posunovat ve vertikálním směru. Numerická simulace vyžaduje diskretizaci a stabilizaci Navierových-Stokesových rovnic pro vysoká Reynoldsova čísla. Vzhledem k deformaci sítě je využita Arbitrary Lagrangian-Eulerian formulace. The interaction of two dimensional incompressible viscous laminar flow with a vibrating airfoil is studied.The airfoilcan rotate and oscillate in vertical direction. The numerical simulation consists of discretization and stabilization of the Navier-Stokes equations for high Reynolds numbers. In order to take the grid motion into account the Arbitrary Lagrangian-Eulerian formulation of the Navier-Stokes equations is used.

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    BI - Acoustics and oscillation

  • OECD FORD branch

Result continuities

  • Project

    <a href="/en/project/GA101%2F02%2F0391" target="_blank" >GA101/02/0391: Numerical simulation and experimental research of aeroelasticity of aircrafts considering large displacements</a><br>

  • Continuities

    Z - Vyzkumny zamer (s odkazem do CEZ)

Others

  • Publication year

    2004

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    IC-SCCE 2004 : proceedings

  • ISBN

  • ISSN

  • e-ISSN

  • Number of pages

    8

  • Pages from-to

    1-8

  • Publisher name

    LFME, University of Patras

  • Place of publication

    Atény

  • Event location

    Atény

  • Event date

    Sep 8, 2004

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article