About the effects of an oscillating miniflap upon the wake on an airfoil, all immersed in turbulent flow

The present research analyzes the asymmetry in the rolling up shear layers behind the blunt trailing edge of an airfoil 4412 with a miniflap acting as active flow control device and its wake organization. Experimental investigations relating the asymmetry of the vortex flow in the near wake region,...

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Veröffentlicht in:	Journal of physics. Conference series 2011-12, Vol.318 (6), p.062005-8
Hauptverfasser:	S, Delnero J, J, Marañón Di Leo, J, Colman, M, Camocardi, M, García Sainz, F, Muñoz
Format:	Artikel
Sprache:	eng
Schlagworte:	Active control Aerodynamics Airfoils Asymmetry Computational fluid dynamics Control equipment Flow control Fluid dynamics Fluid flow Near wakes Physics Rotation Shear layers Statistical methods Suction Trailing edges Turbulence Turbulent flow Vortices
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