Flame-holding configurations for kerosene combustion in a Mach 1.8 airflow

Journal of Propulsion and Power

Volumn 14, Issue 4, 1998, Pages 456-461

  Owens, Michael G ^a,c   Tehranian, Sharam ^a,c   Segal, Corin ^a,c   Vinogradov, Viatcheslav A ^b,c  

^a UNIVERSITY OF FLORIDA   (United States)

^b CENTRAL INSTITUTE OF AVIATION MOTORS   (Russian Federation)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMBUSTION; FLAME RESEARCH; FUEL INJECTION; HYDROGEN; HYPERSONIC FLOW; KEROSENE;

AIR STAGNATION; MACH NUMBER; RECIRCULATION REGION;

RAMJET ENGINES;

EID: 0032118723     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5322     Document Type: Article

References (18)

1. Goltsev, V. F., Sverdlov, E. D., and Tulupov, Y. N., "Combustion of Methane Flame in High Velocity Air Flow with Recirculation Zone," Conference on Combustion and Flame, Alma-Ata, Russia, 1991.
2. Waltrup, P., "Liquid Fueled Supersonic Combustion Ramjets: A Research Perspective of the Past, Present and Future," Journal of Propulsion and Power, Vol. 3, No. 6, 1987, pp. 515-524.
3. Hunt, J. L., Johnston, P. J., and Cubbage, J. M., "Hypersonic Air-breathing Missile Concepts Under Study at Langley," AIAA Paper 82-0316, Jan. 1982.
4. Diskin, C. S., and Northam, G. B., "Evaluation of a Storable Fluorine Based Pilot for Scramjet," AIAA Paper 86-0372, Jan. 1986.
5. Bonghi, L., Dunlap, M. J., Owens, M. G., Young, C., and Segal, C., "Hydrogen Piloted Energy for Supersonic Combustion of Liquid Fuels," AIAA Paper 95-0730, Jan. 1995.
6. Peschke, W. T., "Transverse Liquid Injection into Air Cross-streams," Report on US/Russia Workshop, United Technology Research Center, 1993.
7. Vinogradov, V. A., and Prudnikov, A. G., "Injection of Liquid into the Strut Shadow at Supersonic Velocities," Society of Automotive Engineers Aerospace Atlantic Conf., Dayton, OH, April 1993 (SAE-931455).
8. Avrashkov, V., Baranovsky, S., and Levin, V., "Gasdynamic Features of Supersonic Kerosene Combustion in a Model Combustion Chamber," AIAA Paper 90-5268, Oct. 1990.
9. Kay, I. W., Peschke, W. T., and Guile, R. N., "Hydrocarbon-Fueled Scramjet Combustor Investigation," AIAA 90-2337, July 1990.
10. Vasiliev, V. I., Krasheninnikov, S. J., Stepanov, V. A., and Zakotenko, S. N., "Numerical Investigation of Mixing Augmentation Behind Oblique Shock Waves," AIAA Journal, Vol. 32, No. 2, 1994, pp. 311-316.
11. Vinogradov, V., "Review of Russian Hydrocarbon Fueled Scramjet Technology," Workshop on Russian Hypersonic Technologies, Applied Physics Lab./Johns Hopkins University, Rept. 700-720477-1-2, Baltimore, MD, Nov. 1997.
12. Vinogradov, V., Albegov, R., and Petrov, M. "Experimental Investigation of Hydrogen Burning and Heat Transfer in Annular Duct at Supersonic Velocity," International Council of the Aeronautical Sciences, 91-304, Sept. 1992.
13. Vinogradov, V., Grachev V., Petrov, M., and Shickman J., "Experimental investigation of 2-D Dual Mode Scramjet with Hydrogen Fuel at Mach 4-6," AIAA Paper 90-5269, Oct. 1990.
14. Segal, C., and Young, C. D., "Development of an Experimentally-Flexible Facility for Mixing-Combustion Interactions in Supersonic Flow," Journal of Energy Resources Technology, Vol. 118, No. 2, 1996, pp. 152-158.
15. Segal, C., Haj-Hariri, H., and McDaniel, J. C., "Effects of the Chemical Reaction Model on Calculations of Supersonic Combustion Flows, Journal of Propulsion and Power, Vol. 11, No. 3, 1995, pp. 565-568.
16. Papamoschou, D., and Roshko, A., "Observation of Supersonic Free Shear Layer," AIAA Paper 86-0162, Jan. 1986.
17. Baranovski, S. I., and Schetz, J. A., "Low Angle Injection into a Supersonic Flow," AIAA Journal, Vol. 18, No. 6, 1980, pp. 625-629.
18. Tomioka, S., Takahashi, S., Ujiie, Y., and Kono, M., "Interaction Between Mixing and Combustion of Slot-Injected Fuel in a Supersonic Combustor," AIAA Paper 95-2447, July 1995.