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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Autores principales: Delnero, Juan Sebastián, Marañón Di Leo, Julio, Colman Lerner, Jorge León, Camocardi, Mauricio Ezequiel, García Saínz, Mariano Oscar, Muñoz, Federico
Formato: Articulo
Lenguaje:Inglés
Publicado: 2011
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Acceso en línea:http://sedici.unlp.edu.ar/handle/10915/84367
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