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Experimental Data on High-Speed Flow Past the Root Blade Cascade
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SYSNO ASEP 0361182 Document Type C - Proceedings Paper (int. conf.) R&D Document Type Conference Paper Title Experimental Data on High-Speed Flow Past the Root Blade Cascade Author(s) Šimurda, David (UT-L) RID, ORCID
Luxa, Martin (UT-L) RID, ORCID
Synáč, J. (CZ)
Šafařík, P. (CZ)Source Title Současné trendy při návrhu a výpočtu turbostrojů. - Praha : Technologické inovační centrum ČKD Praha, 2011 / Moštěk M. - ISBN 978-80-254-9934-4 Pages s. 119-124 Number of pages 6 s. Action Current Trends in Design and Computation of Turbomachinery 2011 Event date 31.05.2011-02.06.2011 VEvent location Praha Country CZ - Czech Republic Event type EUR Language eng - English Country CZ - Czech Republic Keywords high speed aerodynamics ; blade cascades ; transonic flow Subject RIV BK - Fluid Dynamics R&D Projects IAA200760801 GA AV ČR - Academy of Sciences of the Czech Republic (AV ČR) GAP101/10/1329 GA ČR - Czech Science Foundation (CSF) CEZ AV0Z20760514 - UT-L (2005-2011) Annotation The paper deals with experimental results of high-speed aerodynamic research on a blade cascade. The blade cascade represents root section of the last stage rotor blades of large output steam turbine. Basic aerodynamic characteristics of the blade cascade are presented together with photographs of flow fields in the range of transonic flow regimes. Results are analysed and discussed to provide a new knowledge on design and operation of the last rotor at the region of the blade root. 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 2012
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