Original title: Aerodynamic Data for Tip Section of Rotor with 52 Titanium Blades 1375 mm Long
Authors: Luxa, Martin ; Synáč, J. ; Šimurda, David ; Šafařík, Pavel
Document type: Papers
Conference/Event: Turbostroje 2014, Plzeň (CZ), 2014-09-24 / 2014-09-25
Year: 2014
Language: eng
Abstract: The paper deals with aerodynamic experimental investigation of prismatic blade cascade,that represents the tip section of the rotor comprising of 52 titanium blades 1375mm long. This rotor is designed for the last stage of low pressure cylinder of a large output steam turbine. Investigated tip section is characterised by supersonic inlet, large stagger angle and supersonic outlet. Selected data from optical and pneumatic measurements are presented.
Keywords: long turbine rotor blade; supersonic flow; tip section
Project no.: TA03020277 (CEP)
Funding provider: GA TA ČR
Host item entry: Turbostroje 2014 - Sborník referátů, ISBN 978-80-260-6447-3

Institution: Institute of Thermomechanics AS ČR (web)
Document availability information: Fulltext is available at the institute of the Academy of Sciences.
Original record: http://hdl.handle.net/11104/0240309

Permalink: http://www.nusl.cz/ntk/nusl-180459


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Research > Institutes ASCR > Institute of Thermomechanics
Conference materials > Papers