DC plasma discharge effects on a Mach 5 flow between small plate electrodes

35th AIAA Plasmadynamics and Lasers Conference

Volumn , Issue , 2004, Pages

  Menart, J ^a   Henderson, S ^a   Shang, J ^a   Kimmel, R ^b   Hayes, J ^b  

^a Wright State University   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; ELECTRODES; LANGMUIR PROBES; MAGNETOHYDRODYNAMICS;

BOTTOM ELECTRODES; ELECTRICAL CONDUCTIVITY; LANGMUIR PROBE MEASUREMENTS; MEASURED PARAMETERS; PLASMA DISCHARGE; PLATE ELECTRODES; PROBE MEASUREMENTS; VERTICAL POSITIONS;

ELECTRIC DISCHARGES;

EID: 85085402408     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-2264     Document Type: Conference Paper

References (28)

1. Bityurin, V. A., Bocharov, A. N., Lineberry, J. T., and Suchomel, C., "Studies on MHD interaction in hypervelocity ionized air flow over aero-surfaces," AIAA 2003-4303, June 23-26, 2003.
2. Bobashev, S. V., Mende, N. P., Sakharov, V. A., Van Wie, D. M., "MHD control of the separation phenomenon in a supersonic xenon plasma flow. I." AIAA 2003-0168, January 6-9, 2003.
3. Clements, R. M. and Smy, P. R., "Electostatic-probe studies in a flame plasma," Journal of Applied Physics, Vol. 40, No. 11, 1969, p. 4553.
4. Clements, R. M. and Smy, P. R., "Ion current from a collision-dominated flowing plasma to a cylindrical electrode surrounded by a thin sheath," Journal of Applied Physics, Vol. 41, No. 9, 1970, p. 3745.
5. Exton, R., Balla, R., Shirinzadeh, B., Brauckmann, G., Hering, G., Kelliher, W., Fugitt, J., Lazard, C., and Khodataev, K., "On-board projection of a microwave plasma upstream of a Mach 6 bow shock," Physics of Pasmas, Vol. 8, p. 5013, 2001.
6. Henderson, S., Menart, J, Shang, J., Kimmel, R. and Hayes, J., "Data reduction analysis for a cylindrical, double Langmuir probe operating in a flowing plasma," AIAA 2004-340, January 5-8, 2004.
7. Huxley, L. and Crompton, R., The Diffusion and Drift of Electrons in Gases, Wiley, New York, 1974.
8. Knight, D., "Survey of aerodynamic flow control at high speed by energy deposition," AIAA 2003-0525, January 6-9, 2003.
9. Knight, D., "A selected survey of magnetogasdynamic local flow control at high speeds," AIAA 2004-1191, January 5-8, 2004.
10. Kimmel, R., Hayes, J., Menart, J., and Shang, J., "Effect of surface plasma discharges on boundary layers at Mach 5," AIAA 2004-0509, January 5-8, 2004.
11. Kuo, S. P. and Bivolaru, D., "A physical mechanism of the plasma effect on shock waves," AIAA 2003-0527, January 6-9, 2003.
12. Leonov, S., Bityurin, V., Savischenko, N., Yuriev, A., and Gromov, V., "Influence of surface electrical discharge on friction of plate in subsonic and transonic airflow," AIAA 2001-0640, 2001.
13. Leonov, S., Bityurin, V., Savelkin, K., and Yarantsev, D., "Effect of electrical discharge on separation processes and shocks position in supersonic airflow," AIAA 2002-0355, January 14-17, 2002.
14. Leonov, S, Bityurin, V., and Yarantsev, D. "The effect of plasma induced separation," AIAA 2003-3852, June 23-26, 2003.
15. Menart, J, Shang, J., Kimmel, R. and Hayes, J. "Effects of magnetic fields on plasma generated in a Mach 5 wind tunnel," AIAA 2003-14165, June 23-26, 2003a.
16. Menart, J, Shang, J.S., Henderson, S., Kurpik, A., Kimmel, R. and Hayes, J., "Survey of plasmas generated in a Mach 5 wind tunnel," AIAA 2003-1194, January 6-9, 2003b.
17. Menart, J., Shang, J., and Hayes, J., "Development of a Langmuir probe for plasma diagnostic work in high speed flow," AIAA paper 2001-2804, June 11-14, 2001.
18. Miles, R. B. "Flow control by energy addition into high-speed air," AIAA 2000-2324, June 19-22, 2000.
19. Palm, P., Meyer, R., Bezant, A., Adamovich, I., and Rich, J., "MHD effect on a supersonic weakly ionized flow," AIAA 2002-2246, May 20-23, 2002.
20. Shneider, M. N., Macheret, S. O., Zaidi, S. H., Girgis, I. G., Raizer, Y. P., and Miles, R. B., "Steady and unsteady flow control with energy addition," AIAA 2003-3862, June 23-26, 2003.
21. Shneider, M. N., Macheret, S. O., and Miles, R. B., "Nonequilibrium magnetohydrodynamic control of scramjet inlets," AIAA 2002-2251, May 20 - 23, 2002.
22. Shang, J. S., Hayes, J., and Menart, J., "Hypersonic flow over a blunt body with plasma injection," Journal of Spacecraft and Rockets, Vol. 35, p. 367, 2002.
23. Shang, J. S., Hayes, J., Menart, J., and Miller, J., "Blunt body in hypersonic electromagnetic flow field," Journal of Aircraft, Vol. 30, p. 314, 2003a.
24. Shang, J. S., Kimmel, R., Hayes, J., and Tyler, C., "Performance of a low density hypersonic magneto-aerodynamic facility," AIAA 2003-0329, January 6-9, 2003b.
25. Smy, P. R., "The use of Langmuir probes in the study of high pressure plasmas," Advances in Physics, Vol. 25, No. 5, 1976, p. 517-553.
26. Smy, P. R. and Noor, A. I., "High-pressure Langmuir probe in a weak flowing plasma or a plasma sheath," Journal of Applied Physics, Vol. 47, No. 4, 1976, p. 1327.
27. Staats, G. E., McGregor, W. K. Jr., Sprouse, J. A., and Fröhlich, J. P., "Magnetogasdynamic experiments conducted in a supersonic plasma arc tunnel," AIAA 2000-2566, June 19-22, 2000.
28. th International Conference on Methods in Aerophysical Research, Institute of Theroretical and Applied Mechanics, Russian Academy of Sciences, Siberian Division, Novosibirsk, Russia, p. 200, 1996.