Number of the records: 1
Airfoil cascades with bistable separation control
- 1.
SYSNO ASEP 0347821 Document Type C - Proceedings Paper (int. conf.) R&D Document Type Conference Paper Title Airfoil cascades with bistable separation control Author(s) Tesař, Václav (UT-L) RID Number of authors 1 Source Title Advances in Fluid Mechanics VIII. - Southampton : WIT Press, 2010 / Rahman M. ; Brebbia C.A. - ISSN 1746-4471 - ISBN 978-1-84564-476-5 Pages s. 331-343 Number of pages 13 s. Action International Conference on Advances in Fluid Mechanics /8./ Event date 15.09.2010-17.09.2010 VEvent location Carvoeiro Country PT - Portugal Event type WRD Language eng - English Country GB - United Kingdom Keywords separation control ; airfoil cascade ; coanda effect Subject RIV BK - Fluid Dynamics R&D Projects GA101/07/1499 GA ČR - Czech Science Foundation (CSF) IAA200760705 GA AV ČR - Academy of Sciences of the Czech Republic (AV ČR) CEZ AV0Z20760514 - UT-L (2005-2011) Annotation To accommodate varying flow rate and shaft speed conditions, the airfoilcascades in hydrodynamic machines should be variable. Author investigated blade separation control by jets issuing from stator bladesshaped so that the flow past them is switched by short control-jet pulses between two alternative stable regimes differing in the resultant exit flow angle. 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 2011
Number of the records: 1