Hypersonic Flow Control Using Surface Plasma Actuator

2008 ◽  
Vol 24 (5) ◽  
pp. 923-934 ◽  
Author(s):  
J. S. Shang ◽  
R. L. Kimmel ◽  
J. Menart ◽  
S. T. Surzhikov
Keyword(s):  
Flow Control ◽  
Hypersonic Flow ◽  
Plasma Actuator ◽  
Surface Plasma

Plasma Actuator for Hypersonic Flow Control

2005 ◽  
Author(s):  
Joseph Shang ◽  
Roger Kimmel ◽  
James Menart ◽  
John Hayes
Keyword(s):  
Flow Control ◽  
Hypersonic Flow ◽  
Plasma Actuator

Experimental Study of Flow Control Over a Standard Road Vehicle Using Plasma Actuator

2020 ◽  
Vol 22 (4) ◽  
pp. 1047-1060
Author(s):  
S. Shadmani ◽  
S. M. Mousavi Nainiyan ◽  
R. Ghasemiasl ◽  
M. Mirzaei ◽  
S. G. Pouryoussefi
Keyword(s):  
Flow Control ◽  
Pressure Distribution ◽  
Drag Force ◽  
Separated Flow ◽  
Plasma Actuator ◽  
Road Vehicle ◽  
Slant Angle ◽  
Total Drag ◽  
Slant Surface ◽  
Ahmed Body

AbstractAhmed Body is a standard and simplified shape of a road vehicle that's rear part has an important role in flow structure and it's drag force. In this paper flow control around the Ahmed body with the rear slant angle of 25° studied by using the plasma actuator system situated in middle of the rear slant surface. Experiments conducted in a wind tunnel in two free stream velocities of U = 10m/s and U = 20m/s using steady and unsteady excitations. Pressure distribution and total drag force were measured and smoke flow visualization carried out in this study. The results showed that at U = 10m/s using plasma actuator suppress the separated flow over the rear slant slightly and be effective on pressure distribution. Also, total drag force reduces in steady and unsteady excitations for 3.65% and 2.44%, respectively. At U = 20m/s, using plasma actuator had no serious effect on the pressure distribution and total drag force.

Magnetoaerodynamic Actuator for Hypersonic Flow Control

AIAA Journal ◽  
2005 ◽  
Vol 43 (8) ◽  
pp. 1633-1652 ◽  
Author(s):  
J. S. Shang ◽  
Sergey T. Surzhikov
Keyword(s):  
Flow Control ◽  
Hypersonic Flow

scholarly journals Wing flow control using pulse thermal plasma actuator

2018 ◽  
Author(s):  
A. A. Kornyakov ◽  
A. V. Voevodin ◽  
D. A. Petrov ◽  
A. S. Petrov ◽  
G. G. Soudakov
Keyword(s):  
Flow Control ◽  
Thermal Plasma ◽  
Plasma Actuator
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