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Effect of Various Boundary Conditions on the Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Flat Profile

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    0511865 - ÚT 2020 RIV CZ eng C - Conference Paper (international conference)
    Musil, Josef - Příhoda, Jaromír - Fürst, J.
    Effect of Various Boundary Conditions on the Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Flat Profile.
    Proceedings of Computational mechanics 2019. Plzeň: University of West Bohemia, 2019 - (Adámek, V.; Jonášová, A.; Plánička, S.; Zajíček, M.), s. 133-134. ISBN 978-80-261-0889-4.
    [Conference with international participation Computational mechanics 2019. Srní (CZ), 04.11.2019-06.11.2019]
    R&D Projects: GA TA ČR TH02020057
    Institutional support: RVO:61388998
    Keywords : turbine cascade * transition model * shock wave-boundary layer interaction
    OECD category: Applied mechanics

    Permanent Link: http://hdl.handle.net/11104/0304531
     
Number of the records: 1  

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