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CFD simulation of flow-induced vibration of an elastically supported airfoil

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24220%2F16%3A00003882" target="_blank" >RIV/46747885:24220/16:00003882 - isvavai.cz</a>

  • Result on the web

    <a href="https://doi.org/10.1051/epjconf/201611402105" target="_blank" >https://doi.org/10.1051/epjconf/201611402105</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1051/epjconf/201611402105" target="_blank" >10.1051/epjconf/201611402105</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    CFD simulation of flow-induced vibration of an elastically supported airfoil

  • Original language description

    © 2016 Owned by the authors, published by EDP Sciences.Flow-induced vibration of lifting or control surfaces in aircraft may lead to catastrophic consequences. Under certain circumstances, the interaction between the airflow and the elastic structure may lead to instability with energy transferred from the airflow to the structure and with exponentially increasing amplitudes of the structure. In the current work, a CFD simulation of an elastically supported NACA0015 airfoil with two degrees of freedom (pitch and plunge) coupled with 2D incompressible airflow is presented. The geometry of the airfoil, mass, moment of inertia, location of the centroid, linear and torsional stiffness was matched to properties of a physical airfoil model used for wind-tunnel measurements. The simulations were run within the OpenFOAM computational package. The results of the CFD simulations were compared with the experimental data.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Result continuities

  • Project

    <a href="/en/project/GA13-10527S" target="_blank" >GA13-10527S: Subsonic flutter analysis of elastically supported airfoils using interferometry and CFD</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2016

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    EPJ Web of Conferences

  • ISBN

  • ISSN

    2101-6275

  • e-ISSN

  • Number of pages

    7

  • Pages from-to

    ""

  • Publisher name

    EDP Sciences

  • Place of publication

    Les Ulis, France

  • Event location

    Praha

  • Event date

    Jan 1, 2015

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article