Název:
Comparison of Transonic Flows Through Two Tip-Section Turbine Blade Cascades with Different Flat Profiles
Autoři:
Musil, Josef ; Příhoda, Jaromír ; Fürst, J. ; Luxa, Martin ; Šimurda, David Typ dokumentu: Příspěvky z konference Konference/Akce: Topical Problems of Fluid Mechanics 2021, on-line (CZ), 20210217
Rok:
2021
Jazyk:
eng
Abstrakt: The contribution deals with numerical simulations of 2D compressible flow through two variants of the tip-section turbine blade cascade with a flat profile for the subsonic inlet. Simulations were realised by means of the OpenFOAM code using the γ-Reθ bypass transition model completed by the two-equation SST turbulence model. Predictions were focused particularly on the impact of the shock-wave/boundary-layer interaction on the flow structure in the inter-blade channel. Beside the effect of the inlet angle on the flow around the leading edge was studied. Numerical results were compared with optical and pressure experimental data.
Klíčová slova:
CFD; supersonic tip-section blade cascade; transition modelling Číslo projektu: LTAUSA19036 Poskytovatel projektu: GA MŠk Zdrojový dokument: Proceedings of Topical Problems of Fluid Mechanics 2021, ISBN 978-80-87012-76-5, ISSN 2336-5781