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Simulation of Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Flat Profile

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    0503332 - ÚT 2020 RIV CZ eng C - Conference Paper (international conference)
    Musil, Josef - Příhoda, Jaromír - Fürst, J.
    Simulation of Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Flat Profile.
    Proceedings of Topical Problems of Fluid Mechanics 2019. Praha: Institute of Thermomechanics of the Czech Academy of Sciences, 2019, s. 169-174. ISBN 978-80-87012-69-7. ISSN 2336-5781.
    [Topical Problems of Fluid Mechanics 2019. Prague (CZ), 20.02.2019-22.02.2019]
    R&D Projects: GA TA ČR TH02020057
    Institutional support: RVO:61388998
    Keywords : supersonic tip-section blade cascade * CFD * transition modelling
    Subject RIV: BK - Fluid Dynamics
    OBOR OECD: Applied mechanics
    http://www.it.cas.cz/fm/im/im/proceedings/2019

    The contribution presents results of the numerical simulation of 2D compressible flow through the tip-section turbine blade cascade with a flat profile and the supersonic inlet. The simulation was carried out by the OpenFOAM code using the Favre-averaged NavierStokes equations completed by the two-equation SST turbulence model and the γ-Reθ bypass transition model. Predictions carried out for nominal conditions were focused particularly on the relation between the inlet flow angle and the inlet Mach number. Further, the effect of the shock-wave/boundary layer interaction on the skin friction coefficient was investigated. Numerical results were compared with experimental data.
    Permanent Link: http://hdl.handle.net/11104/0298408
     
Number of the records: 1