Drag reduction by pulsed jets on strongly unstructured wake: towards the square back control - Archive ouverte HAL
Article Dans Une Revue International Journal of Aerodynamics Année : 2011

Drag reduction by pulsed jets on strongly unstructured wake: towards the square back control

Résumé

Experimental studies have been performed in a wind tunnel in order to control the flow separation on rear window of a generic vehicle shape (the Ahmed body with a scale of 0.7 and a slope angle of 35 degrees). The rear part of the geometry has been modified by replacing the sharp edge between roof and rear window by smooth curved surfaces. This model is equipped at the end of the roof with a strip of pulsed jets in order to control the flow with a velocity of 30 m.s−1. A 20% drag reduction has been obtained with a pulsed frequency at 500 Hz and a momentum coefficient Cµ = 2.75 10−3. This result confirms the interest in using pulsed jets in order to reduce aerodynamic drag and pollutant emission.
Fichier non déposé

Dates et versions

hal-00582525 , version 1 (01-04-2011)

Identifiants

Citer

Eric Bideaux, Pierre Bobillier, Elisabeth Fournier, Patrick Gilliéron, Mahmoud El Hajem, et al.. Drag reduction by pulsed jets on strongly unstructured wake: towards the square back control. International Journal of Aerodynamics, 2011, 1 (3/4), pp.282 - 298. ⟨10.1504/IJAD.2011.038846⟩. ⟨hal-00582525⟩
341 Consultations
0 Téléchargements

Altmetric

Partager

More