Number of the records: 1
Aerodynamic Data for Tip Section of Rotor with 52 Titanium Blades 1375 mm Long
- 1.0432289 - ÚT 2015 RIV CZ eng K - Conference Paper (Czech conference)
Luxa, Martin - Synáč, J. - Šimurda, David - Šafařík, Pavel
Aerodynamic Data for Tip Section of Rotor with 52 Titanium Blades 1375 mm Long.
Turbostroje 2014 - Sborník referátů. Plzeň: ZČU Plzeň, 2014. ISBN 978-80-260-6447-3.
[Turbostroje 2014. Plzeň (CZ), 24.09.2014-25.09.2014]
R&D Projects: GA TA ČR(CZ) TA03020277
Institutional support: RVO:61388998
Keywords : supersonic flow * long turbine rotor blade * tip section
Subject RIV: BK - Fluid Dynamics
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.
Permanent Link: http://hdl.handle.net/11104/0240309
Number of the records: 1