Simulation of Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Strong Shock-Wave/Boundary Layer Interaction

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SYSNO	0495984
Title	Simulation of Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Strong Shock-Wave/Boundary Layer Interaction
Author(s)	Straka, P. (CZ) Příhoda, Jaromír (UT-L)_{RID, ORCID} Luxa, Martin (UT-L)_{RID, ORCID}
Source Title	Computational Mechanics 2018 - Book of extended abstracts. S. 123-124. - Plzeň : University of West Bohemia, Plzeň, 2018 / Adámek V. ; Jonášová A.
Conference	Conference with international participation Computational Mechanics 2018 /34./, 31.10.2018 - 02.11.2018, Srní
Document Type	Abstrakt
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/11104/0289917

Number of the records: 1