Aerodynamic Data for Tip Section of Rotor with 52 Titanium Blades 1375 mm Long

Number of the records: 1

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SYSNO ASEP	0432289
Document Type	K - Proceedings Paper (Czech conf.)
R&D Document Type	Conference Paper
Title	Aerodynamic Data for Tip Section of Rotor with 52 Titanium Blades 1375 mm Long
Author(s)	Luxa, Martin (UT-L)_{RID, ORCID} Synáč, J. (CZ) Šimurda, David (UT-L)_{RID, ORCID} Šafařík, Pavel (UT-L)_{RID, ORCID}
Source Title	Turbostroje 2014 - Sborník referátů. - Plzeň : ZČU Plzeň, 2014 - ISBN 978-80-260-6447-3
Number of pages	8 s.
Publication form	Medium - C
Action	Turbostroje 2014
Event date	24.09.2014-25.09.2014
VEvent location	Plzeň
Country	CZ - Czech Republic
Event type	CST
Language	eng - English
Country	CZ - Czech Republic
Keywords	supersonic flow ; long turbine rotor blade ; tip section
Subject RIV	BK - Fluid Dynamics
R&D Projects	TA03020277 GA TA ČR - Technology Agency of the Czech Republic (TA ČR)
Institutional support	UT-L - RVO:61388998
Annotation	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.
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	2015

Number of the records: 1