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Massive separation control analysis of the pulsed jet actuators effects

Published online by Cambridge University Press:  14 February 2014

P. Gillieron  and
A. Kourta
P. Gillieron*
Affiliation:
Chercheur indépendant 
A. Kourta
Affiliation:
Laboratoire PRISME, Université d’Orléans, France
*
a Corresponding author: rdmfa.pgillieron@orange.fr
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Abstract

The aerodynamic drag of simplified car geometry with small span and strongly separated wake can be reduced up 20% by using pulsed jet distributed along the rear window. Results show an enhancement of transversal wake size in the control region, a displacement of the mean positions of vortex wake structures, a decrease of velocities near the rear part and a reduction of vortex structure recirculation in the wake. These modifications produced by the control are analyzed, commented and model based on simple strategy to build efficient and suitable separation control strategy is proposed.

Keywords

Aerodynamiccontrolactuatorpulsed jetmodelingAérodynamiquecontrôleactionneurjets pulsésmodélisation
Type
Research Article
Information
Mechanics & Industry , Volume 14 , Issue 6 , 2013 , pp. 441 - 445
Copyright
© AFM, EDP Sciences 2014

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References

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