Numerical and experimental investigation of inlet flow angle in a supersonic turbine cascade

Number of the records: 1

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SYSNO ASEP	0383603
Document Type	A - Abstract
R&D Document Type	Není vybrán druh dokumentu
Title	Numerical and experimental investigation of inlet flow angle in a supersonic turbine cascade
Author(s)	Váchová, J. (CZ) Luxa, Martin (UT-L)_{RID, ORCID}
Source Title	Computational mechanics 2012. - Plzeň : University of West Bohemia, 2012 / Adámek V. ; Zajíček M. ; Jonášová A. - ISBN 978-80-261-0157-4 S. 1-2
Number of pages	2 s.
Publication form	Medium - C
Action	Computational mechanics 2012 /28./
Event date	12.11.2012-14.11.2012
VEvent location	Špičák
Country	CZ - Czech Republic
Event type	EUR
Language	eng - English
Country	CZ - Czech Republic
Keywords	tip section ; supersonic cascade ; CFD
Subject RIV	BK - Fluid Dynamics
R&D Projects	GAP101/10/1329 GA ČR - Czech Science Foundation (CSF)
Institutional support	UT-L - RVO:61388998
Annotation	The paper presents one aspect of numerical and experimental investigation of a highly loaded supersonic cascade, which represents the tip section of rotor row in the last stage o steam turbines. It complements other papers, in which differences in the velocity inlet angle between CFD and experiment have been discussed.
Workplace	Institute of Thermomechanics
Contact	Marie Kajprová, kajprova@it.cas.cz, Tel.: 266 053 154 ; Jana Lahovská, jaja@it.cas.cz, Tel.: 266 053 823
Year of Publishing	2013

Number of the records: 1