Experimental Investigation of the Effects of Various Plasma Actuator Configurations on Lift and Drag Coefficients of a Circular Cylinder Including the Effects of Electrodes-Reference-Cited by-同舟云学术

Experimental Investigation of the Effects of Various Plasma Actuator Configurations on Lift and Drag Coefficients of a Circular Cylinder Including the Effects of Electrodes

Published:2012-06 Issue:3 Volume:25 Page:311-324
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

TABATABAEIAN Siavash,MIRZAEI Masoud,SADIGHZADEH Asghar,DAMIDEH Vahid,SHADARAM Abdollah

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference20 articles.

1. Steady control of laminar separation over airfoils with plasma sheet actuators;Sosa;Journal of Electrostatics,2006

2. Effect of a DC surface-corona discharge on a flat plate boundary layer for air flow velocity up to 25 m/s;Moreau;Journal of Electrostatics,2006

3. Stall control at high angle of attack with plasma sheet actuators;Sosa;Experiments in Fluids,2007

4. Font G I, Morgan W L. Plasma discharge in atmospheric pressure oxygen for boundary layer separation control. AIAA-2005-4632, 2005.

5. Visbal M R, Gaitonde D V, Roy S. Control of transitional and turbulent flows using plasma-based actuators. AIAA-2006-3230, 2006.

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