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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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SYSNO 0511865 Title Effect of Various Boundary Conditions on the Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Flat Profile Author(s) Musil, Josef (UT-L) ORCID
Příhoda, Jaromír (UT-L) RID, ORCID
Fürst, J. (CZ)Source Title Proceedings of Computational mechanics 2019. S. 133-134. - Plzeň : University of West Bohemia, 2019 / Adámek V. ; Jonášová A. ; Plánička S. ; Zajíček M. Conference Conference with international participation Computational mechanics 2019, 04.11.2019 - 06.11.2019, Srní Document Type Konferenční příspěvek (zahraniční konf.) Grant TH02020057 GA TA ČR - Technology Agency of the Czech Republic (TA ČR) Institutional support UT-L - RVO:61388998 Language eng Country CZ Keywords turbine cascade * transition model * shock wave-boundary layer interaction Permanent Link http://hdl.handle.net/11104/0304531
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