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Airfoil cascades with bistable separation control

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    0347821 - ÚT 2011 RIV GB eng C - Conference Paper (international conference)
    Tesař, Václav
    Airfoil cascades with bistable separation control.
    Advances in Fluid Mechanics VIII. Southampton: WIT Press, 2010 - (Rahman, M.; Brebbia, C.), s. 331-343. ISBN 978-1-84564-476-5. ISSN 1746-4471.
    [International Conference on Advances in Fluid Mechanics /8./. Carvoeiro (PT), 15.09.2010-17.09.2010]
    R&D Projects: GA ČR GA101/07/1499; GA AV ČR IAA200760705
    Institutional research plan: CEZ:AV0Z20760514
    Keywords : separation control * airfoil cascade * coanda effect
    Subject RIV: BK - Fluid Dynamics

    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.
    Permanent Link: http://hdl.handle.net/11104/0188508

     
     
Number of the records: 1  

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