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Aerodynamic Research on the Tip Sections of a Long Turbine Blade
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SYSNO ASEP 0309407 Document Type C - Proceedings Paper (int. conf.) R&D Document Type Conference Paper Title Aerodynamic Research on the Tip Sections of a Long Turbine Blade Title Aerodynamický výzkum špičkového řezu dlouhé turbínové lopatky Author(s) Šimurda, David (UT-L) RID, ORCID
Luxa, Martin (UT-L) RID, ORCID
Synáč, J. (CZ)
Šafařík, Pavel (UT-L) RID, ORCIDSource Title Proceedings of ASME Turbo Expo 2008 : Power for Land, Sea and Air. - Berlín : ASME, 2008 - ISBN 0-7918-3824-2 Pages s. 1-8 Number of pages 8 s. Publication form DVD - DVD Action ASME Turbo Expo 2008 Event date 09.06.2008-13.06.2008 VEvent location Berlin Country DE - Germany Event type WRD Language eng - English Country DE - Germany Keywords transsonic flow ; tip blade section ; turbomachinery Subject RIV BK - Fluid Dynamics R&D Projects GA101/07/1508 GA ČR - Czech Science Foundation (CSF) ME08025 GA MŠMT - Ministry of Education, Youth and Sports (MEYS) CEZ AV0Z20760514 - UT-L (2005-2011) UT WOS 000262646900084 Annotation This paper reports on results of high-speed aerodynamic research on a blade cascade. The blade cascade represents the tip section of the last stage rotor blades of a large output steam turbine. The aerodynamics characteristics of the blade cascade are presented together with flow field photographs in a range of transonic and supersonic velocities. 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 2009
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