Original title: Simulation of Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Flat Profile
Authors: Musil, Josef ; Příhoda, Jaromír ; Fürst, J.
Document type: Papers
Conference/Event: Topical Problems of Fluid Mechanics 2019, Prague (CZ), 20190220
Year: 2019
Language: eng
Abstract: 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.
Keywords: CFD; supersonic tip-section blade cascade; transition modelling
Project no.: TH02020057 (CEP)
Funding provider: GA TA ČR
Host item entry: Proceedings of Topical Problems of Fluid Mechanics 2019, ISBN 978-80-87012-69-7, ISSN 2336-5781
Note: Související webová stránka: http://www.it.cas.cz/fm/im/im/proceedings/2019

Institution: Institute of Thermomechanics AS ČR (web)
Document availability information: Fulltext is available at the institute of the Academy of Sciences.
Original record: http://hdl.handle.net/11104/0298408

Permalink: http://www.nusl.cz/ntk/nusl-399114


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Research > Institutes ASCR > Institute of Thermomechanics
Conference materials > Papers
 Record created 2019-08-26, last modified 2021-11-24


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