Lift and drag performances of an axisymmetric airfoil controlled by plasma actuator

A Dielectric Barrier Discharge (DBD) is mounted at the leading edge of a NACA 0015 airfoil model. The effects of steady and unsteady actuations on the lift and drag coefficients are investigated by time-averaged force measurements. Results demonstrate that the stall regime can be delayed of one or t...

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Veröffentlicht in:	Journal of electrostatics 2009-05, Vol.67 (2), p.133-139
Hauptverfasser:	Benard, N., Jolibois, J., Moreau, E.
Format:	Artikel
Sprache:	eng
Schlagworte:	DBD Engineering Sciences Flow separation control Fluid mechanics Fluids mechanics Mechanics Non-thermal plasma Periodic excitation Physics
Online-Zugang:	Volltext
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