Visualization of Flow Separation and Control by Vortex Generators on an Single Flap in Landing Configuration

0351483 - ÚT 2011 RIV CZ eng C - Conference Paper (international conference)
Součková, Natálie - Kuklová, J. - Popelka, Lukáš - Matějka, Milan
Visualization of Flow Separation and Control by Vortex Generators on an Single Flap in Landing Configuration.
Proceedings of the International Conference Experimental Fluid Mechanics 2010. Liberec: Technical University of Liberec, 2010 - (Vít, T.; Dančová, P.), s. 1-12. ISBN 978-80-7372-670-6.
[Experimental Fluid Mechanics 2010. Liberec (CZ), 24.11.2010-26.11.2010]
R&D Projects: GA MŠMT(CZ) 1M06031; GA ČR GAP101/10/1230; GA ČR GA101/08/1112; GA ČR GA103/09/0977
Institutional research plan: CEZ:AV0Z20760514
Keywords : flow separation * vortex generators * visualization
Subject RIV: JU - Aeronautics, Aerodynamics, Aircrafts

This paper focuses on a suppression of the flow separation, which occurs on a deflected flap, by means of vortex generators (VG's). An airfoil NACA 63A421 with a simple flap and vane-type vortex generators were used. The investigation was carried out by using experimental and numerical methods. The data from the numerical simulation of the flapped airfoil without VG's control were used for the vortex generator design. Two sizes, two different shapes and various spacing of the vortex generators were tested. The flow past the airfoil was visualized through three methods, namely tuft filaments technique, oil and thermo camera visualization. The experiments were performed in closed circuit wind tunnels with closed and open test sections. The lift curves for both cases without and with vortex generators were acquired for a lift coefficient improvement determination. The improvement was achieved for several cases by means all of the applied methods.
Permanent Link: http://hdl.handle.net/11104/0191224