Study of surface and volumetric heating effects in a Mach 5 flow

35th AIAA Plasmadynamics and Lasers Conference

Volumn , Issue , 2004, Pages

  Menart, J ^a   Henderson, S ^a   Atzbach, C ^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

ELECTRODES; FLOW FIELDS; HEAT CONDUCTION; MAGNETOHYDRODYNAMICS; THERMOCOUPLES;

COMPUTER MODELING; COPPER ELECTRODES; ELECTRICAL RESISTANCE HEATERS; HEAT TRANSFER CHARACTERISTICS; MEASURED TEMPERATURES; THERMAL CHARACTERISTICS; UNSTEADY HEAT CONDUCTION; VOLUMETRIC HEATING;

ELECTRIC DISCHARGES;

EID: 85087598235     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-2262     Document Type: Conference Paper

References (27)

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. Bracken, R. M., Hartley, C. S., Mann, G., Myrabo, L. N., Nagamatsu, H. T., and Shneider, M. N., " Experimental and computational parametric drag study of an " air spike" in hypersonic flow," AIAA 2002-3784 July 7-10, 2002.
4. Eckert, E. R. G., Engineering relations for heat transfer and friction in high-velocity laminar and turbulent boundary layer flow over surfaces with constant pressure and temperature, Transactions of ASME, Vol. 78, p. 1273, 1956.
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 Plasmas, Vol. 8, p. 5013, 2001.
6. Girgis, I., Shneider, M., Macheret, S., Brown, G., and Miles, R. B., " Creation of steering moments in supersonic flow by off-axis plasma heat addition," AIAA 2002-0129, January 14-17, 2002.
7. 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.
8. th edition, Wiley, New York, 1981.
9. Kimmel, R., Hayes, J., Menart, J., and Shang, J., " Effect of surface plasma discharges on boundary layers at Mach 5," AIAA 2004-509, January 5-8, 2004.
10. Knight, D., " Survey of aerodynamic flow control at high speed by energy deposition," AIAA 2003-0525, January 6-9, 2003.
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., 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.
13. Leonov, S, Bityurin, V., and Yarantsev, D. " The effect of plasma induced separation," AIAA 2003-3852, June 23-26, 2003.
14. 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, 2003.
15. 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.
16. Miles, R. B. " Flow control by energy addition into high-speed air," AIAA 2000-2324, June 19-22, 2000.
17. Miles, R. B., Martinelli, L., Macheret, S. O., Shneider, M. N., Girgis, I. G., Zaidi, S. H., and Mansfield, D. K., " Suppression of sonic boom by dynamic off-body energy addition and shape optimization," AIAA 2002-0150, January 14-17, 2002.
18. 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.
19. Patankar, S. V., Numerical Heat Transfer and Fluid Flow, Taylor & Francis, 1980.
20. Pletcher, R. H., " External flow forced convection," in Handbook of Single-Phase Convective Heat Transfer, Ed. by Kakac, S., Shah, R. K., and Aung, W., Wiley, New York, 1987.
21. 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.
22. Shneider, M. N., Macheret, S. O., and Miles, R. B., " Nonequilibrium magnetohydrodynamic control of scramjet inlets," AIAA 2002-2251, May 20 - 23, 2002.
23. 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.
24. 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
25. 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.
26. 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.
27. th International Conference on Methods in Aerophysical Research, Institute of Theoretical and Applied Mechanics, Russian Academy of Sciences, Siberian Division, Novosibirsk, Russia, p. 200, 1996.