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Finite Element Simulation of a Gust Response of an Ultralight 2-DOF Airfoil

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F14%3A00430087" target="_blank" >RIV/61388998:_____/14:00430087 - isvavai.cz</a>

  • Alternative codes found

    RIV/68407700:21220/14:00222866

  • Result on the web

    <a href="http://dx.doi.org/10.1115/PVP2014-28390" target="_blank" >http://dx.doi.org/10.1115/PVP2014-28390</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1115/PVP2014-28390" target="_blank" >10.1115/PVP2014-28390</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Finite Element Simulation of a Gust Response of an Ultralight 2-DOF Airfoil

  • Original language description

    Flexibly supported two-degrees of freedom (2-DOF) airfoil in two-dimensional (2D) incompressible viscous turbulent flow subjected to a gust (sudden change of flow conditions) is considered. The structure vibration is described by two nonlinear ordinary differential equations of motion for large vibration amplitudes. The flow is modeled by Reynolds averaged Navier-Stokes equations (RANS) and by k ?w turbulence model. The numerical simulation consists of the finite element (FE) solution of the RANS equations and the equations for the turbulent viscosity. This is coupled with the equations of motion for the airfoil by a strong coupling procedure. The time dependent computational domain and a moving grid are taken into account with the aid of the arbitraryLagrangian-Eulerian formulation. In order to avoid spurious numerical oscillations, the SUPG and div-div stabilizations are applied. The solution of the ordinary differential equations is carried out by the Runge-Kutta method. The result

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    BI - Acoustics and oscillation

  • OECD FORD branch

Result continuities

  • Project

    <a href="/en/project/GAP101%2F11%2F0207" target="_blank" >GAP101/11/0207: Coupled problems of fluid and solid mechanics - nonlinear aeroelasticity</a><br>

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2014

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    Proceedings of the ASME 2014 Pressure Vessels & Piping Conference

  • ISBN

    978-0-7918-4601-8

  • ISSN

  • e-ISSN

  • Number of pages

    10

  • Pages from-to

  • Publisher name

    ASME

  • Place of publication

    Anaheim

  • Event location

    Anaheim, California

  • Event date

    Jul 20, 2014

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article