Effects of plasma aerodynamic actuation on oblique shock wave in a cold supersonic flow

Journal of Physics D: Applied Physics

Volumn 42, Issue 16, 2009, Pages

  Wang, Jian ^a   Li, Yinghong ^a   Cheng, Bangqin ^a   Su, Changbing ^a   Song, Huimin ^a   Wu, Yun ^a  

^a AIR FORCE ENGINEERING UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

A-THERMAL; AERODYNAMIC ACTUATORS; ARC DISCHARGE; ARC DISCHARGE PLASMAS; FLOW DOWNSTREAM; INPUT VOLTAGES; MAGNETIC CONTROL; PLASMA ACTUATION; SCHLIEREN PHOTOGRAPHY; START POINT; STATIC MAGNETIC FIELDS; STATIC-PRESSURE RATIO; SUPERSONIC WIND TUNNEL; TEST CONDITION; THEORETICAL RESULT;

CAVITY RESONATORS; ELECTRIC DISCHARGES; GAS DYNAMICS; MAGNETIC FIELDS; PLASMA DIAGNOSTICS; PLASMA SHOCK WAVES; PLASMAS; SUPERSONIC AERODYNAMICS; SUPERSONIC FLOW; WIND TUNNELS;

WAVES;

EID: 70349087397     PISSN: 00223727     EISSN: 13616463     Source Type: Journal    
DOI: 10.1088/0022-3727/42/16/165503     Document Type: Article

References (15)

1. Meyer R, Palm P and Plonjes E 2001 The effect of a nonequilibrium RF discharge plasma on a conical shock wave in a M = 2.5 flow AIAA Paper no 2001-3059
2. Merriman S, Plonjes E and Palm P 2001 Shock wave control by nonequilibrium plasmas in cold supersonic gas flows AIAA J. 39 1547-52
3. Miles R B, Macheret S O and Martinelli L 2001 Plasma control of shock waves in aerodynamics and sonic boom mitigation AIAA Paper no 2001-3062
4. Macheret S O, Shneider M N and Zaidi S H 2003 Plasma and MHD control of oblique shocks ADA 434494
5. Macheret S O, Shneider M N and Miles R B 2003 Scramjet inlet control by off-body energy addition: a virtual cowl AIAA Paper no 2003-32
6. Shneider M N, Macheret S O and Miles R B 2003 Comparative analysis of MHD and plasma methods of scramjet inlet control AIAA Paper no 2003-170
7. Leonov S B, Yarantsev D A and Soloviev V R 2006 High-speed inlet customization by surface electric discharge AIAA Paper no 2006-403
8. Leonov S B, Bityurin V A and Yarantsev D A 2005 High-speed flow control due to interaction with electrical discharges AIAA Paper no 2005-3287
9. Leonov S B, Yarantsev D A and Isaenkov Y I 2005 Properties of filamentary electrical discharge in high-enthalpy flow AIAA Paper no 2005-159
10. Leonov S B 2005 Study of a structural plasma influence on characteristics of viscous friction and separated near-surface zone position under high-speed airflow ADA 433384
11. Kolesnichenko Y F, Brovkin V G and Leonov S B 2001 Investigation of AD-body interaction with microwave discharge region in supersonic flows AIAA Paper no 2001-0345
12. Bletzinger P, Ganguly B N and VanWie D M 2005 Plasmas in high speed aerodynamics J. Phys. D: Appl. Phys. 38 R33-57
13. Ganiev Y C, Gordeev V P and Krasilnikov A V 2000 Aerodynamic drag reduction by plasma and hot-gas injection J. Thermophys. Heat Transfer 14 10-17
14. Shang J S 2002 Plasma injection for hypersonic blunt-body drag reduction AIAA J. 40 1178-86
15. Guo Z Y and Zhao W H 1986 Arc and Thermal Plasmas (Beijing: Science Press) pp 141-57