Počet záznamů: 1  

Numerical Simulation of Airfoil Vibrations Induced by Turbulent Flow

  1. 1.
    SYSNO ASEP0437115
    Druh ASEPJ - Článek v odborném periodiku
    Zařazení RIVJ - Článek v odborném periodiku
    Poddruh JČlánek ve WOS
    NázevNumerical Simulation of Airfoil Vibrations Induced by Turbulent Flow
    Tvůrce(i) Feistauer, M. (CZ)
    Horáček, Jaromír (UT-L) RID, ORCID
    Sváček, P. (CZ)
    Zdroj.dok.Communications in Computational Physics. - : Global Science Press - ISSN 1815-2406
    Roč. 17, č. 1 (2015), s. 146-188
    Poč.str.43 s.
    Forma vydáníTištěná - P
    Jazyk dok.eng - angličtina
    Země vyd.CN - Čína
    Klíč. slovafluid-structure interaction ; flow induced vibrations ; turbulence models ; finite element method
    Vědní obor RIVBI - Akustika a kmity
    CEPGAP101/11/0207 GA ČR - Grantová agentura ČR
    Institucionální podporaUT-L - RVO:61388998
    UT WOS000353692300006
    EID SCOPUS84925788899
    DOI10.4208/cicp.181213.230514a
    AnotaceThe subject of the paper is the numerical simulation of the interaction of two-dimensional incompressible viscous flow and a vibrating airfoil with large amplitudes. The airfoil with three degrees of freedom performs rotation around an elastic axis, oscillations in the vertical direction and rotation of a flap. The numerical simulation consists of the finite element solution of the Reynolds averaged Navier-Stokes equations combined with Spalart-Allmaras or κ–ω turbulence models, coupled with a system of nonlinear ordinary differential equations describing the airfoil motion with consideration of large amplitudes. The time-dependent computational domain and approximation on a moving grid are treated by the Arbitrary Lagrangian-Eulerian formulation of the flow equations. Due to large values of the involved Reynolds numbers an application of a suitable stabilization of the finite element discretization is employed. The developed method is used for the computation of flow-induced oscillations of the airfoil near the flutter instability, when the displacements of the airfoil are large, up to ±40 degrees in rotation. The paper contains the comparison of the numerical results obtained by both turbulence models.
    PracovištěÚstav termomechaniky
    KontaktMarie Kajprová, kajprova@it.cas.cz, Tel.: 266 053 154 ; Jana Lahovská, jaja@it.cas.cz, Tel.: 266 053 823
    Rok sběru2016
Počet záznamů: 1  

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