0383603 - ÚT 2013 RIV CZ eng A - Abstract
Váchová, J. - Luxa, Martin
Numerical and experimental investigation of inlet flow angle in a supersonic turbine cascade.
Computational mechanics 2012. Plzeň: University of West Bohemia, 2012 - (Adámek, V.; Zajíček, M.; Jonášová, A.). s. 1-2. ISBN 978-80-261-0157-4.
[Computational mechanics 2012 /28./. 12.11.2012-14.11.2012, Špičák]
R&D Projects: GA ČR(CZ) GAP101/10/1329
Institutional support: RVO:61388998
Keywords : tip section * supersonic cascade * CFD
Subject RIV: BK - Fluid Dynamics

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.
Permanent Link: http://hdl.handle.net/11104/0007227