Penetration and spreading of liquid jets in an external-internal compression inlet

AIAA journal

Volumn 38, Issue 6, 2000, Pages 989-994

  Livingston, T ^a   Segal, C ^a   Schindler, M ^b   Vinogradov, V A ^c  

^a UNIVERSITY OF FLORIDA   (United States)

^b UNIVERSITY OF STUTTGART   (Germany)

^c CENTRAL INSTITUTE OF AVIATION MOTORS   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; COMBUSTION CHAMBERS; DROP BREAKUP; FLOW VISUALIZATION; FUEL INJECTION; HYPERSONIC FLOW; INTAKE SYSTEMS; LIGHT SCATTERING; SURFACE TENSION; VISCOSITY OF LIQUIDS;

COMPRESSION INLET; PARTIAL FUEL PREMIXING;

JET AIRCRAFT;

EID: 0033729895     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1082     Document Type: Article

References (23)

1. Northam, G. B., Greenberg, I., Byington, C. S., and Capriotti, D. P., "Evaluation of Parallel Injector Configurations for Mach 2 Combustion," Journal of Propulsion and Power, Vol. 8, No. 2, 1992, pp. 491-499.
2. Hartfield, R. J., Hollo, S. D., and McDaniel, J. C., "Experimental Investigation of a Swept Ramp Injector Using Laser-Induced Iodine Fluorescence," Journal of Propulsion and Power, Vol. 10, No. 1, 1994, pp. 129-135.
3. Riggins, D. W., McClinton, C. R., Rogers, R. C., and Bittner, R. D., "Investigation of Scramjet Strategies for High Mach Number Flows," Journal of Propulsion and Power, Vol. 11, No. 3, 1995, pp. 409-418.
4. Cox, S. K., Fuller, R. P., Schetz, J. A., and Walters, R. W., "Vortical Interaction Generated by an Injector Array to Enhance Mixing in Supersonic Flow," AIAA Paper 94-0708, Jan. 1994.
5. Fuller, R. P., Wu, P.-K., Nejad, A. S., and Schetz, J. A., "Fuel-Vortex Interaction for Enhanced Mixing in Supersonic Flow," AIAA Paper 96-2661, July 1996.
6. Swithenbank, J., and Chigier, N. A., "Vortex Mixing for Supersonic Combustion," Twelfth Symposium (International) on Combustion, Combustion Inst., Pittsburgh, PA, 1968, pp. 1153-1162.
7. Povinelli, L. A., and Ehlers, R. C., "Swirling Base Injection for Supersonic Combustion Ramjets," AIAA Journal, Vol. 10, No. 9, 1972, pp. 1243, 1244.
8. Marble, F. E., Hendricks, G. J., and Zukoski, E. E., "Progress Toward Shock Enhancement of Supersonic Combustion Processes," AIAA Paper 87-1880, June 1987.
9. Marble, F. E., Zukoski, E. E., Jacobs, J. W., Hendricks, G. J., and Waitz, I. A., "Shock Enhancement and Control of Hypersonic Mixing and Combustion," AIAA Paper 90-1891, July 1990.
10. Owens, M., Segal, C., and Auslender, A. H., "Effects of Mixing Schemes on Kerosene Combustion in a Supersonic Airstream," Journal of Propulsion and Power, Vol. 13, No. 4, 1997, pp. 525-531.
11. Heiser, W. H., Pratt, D. T., Daley, D. H., and Mehta, U. B., Hypersonic Airbreathing Propulsion, edited by J. S. Przewieniecki, AIAA Education Series, AIAA, Washington, DC, 1994, pp. 507-512.
12. Goltsev, V. F., Sverdlov, E. D., and Tulupov, Yu. N., "Combustion of Methane Flame in High Velocity Air Flow with Recirculation Zone," Proceedings of the 3rd All-Union Workshop on Flame Structure, Vol. 1, Siberian Branch of the Russian Academy of Science, Novosibirsk, Russia, 1991, pp. 147-151.
13. 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.
14. Hunt, J. L., Johnston, P. J., and Cubbage, J. M., "Hypersonic Airbreathing Missile Concepts Under Study at Langley," AIAA Paper 82-0316, Jan. 1982.
15. Diskin, C. S., and Northam, G. B., "Evaluation of a Storable Fluorine-Based Pilot for Scramjet," AIAA Paper 86-0372, Jan. 1986.
16. 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.
17. Vinogradov, V. A., and Prudnikov, A. G., "Injection of Liquid into the Strut Shadow at Supersonic Velocities," SAE Aerospace Atlantic Conf., Society of Automotive Engineers, SAE-931455, Dayton, OH, April 1993.
18. Kay, I. W., Peschke, W. T., and Guile, R. N., "Hydrocarbon-Fueled Scramjet Combustor Investigation," AIAA Paper 90-2337, July 1990.
19. Tretyakov, P. K., Fomin, V. M., and Yakovlev, V. I., "New Principles of Control of Aerophysical Processes. Research Development," Proceedings (Part 2) of the International Conference on the Methods of Aerophysical Research, Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, 1986, pp. 210-220.
20. Vasilev, V. I., Zakotenko, S. N., Krasheninnikov, S. J., and Stepanov, V. A., "Numerical Investigations of Mixing Augmentation Behind Oblique Shock Waves," AIAA Journal, Vol. 32, No. 2, 1994, pp. 311-316.
21. Vinogradov, V. A., Grachev, V., Petrov, M., and Sheechman, J., "Experimental Investigation of Two-Dimensional Dual Mode Scramjet with Hydrogen Fuel at Mach 4...6," AIAA Paper 90-5269, 1990.
22. Tillman, T. G., Patrick, W. P., and Patterson, R. W., "Enhanced Mixing of Supersonic Jets," Journal of Propulsion and Power, Vol. 7, No. 6, 1991, pp. 1006-1014.
23. Papamoschou, D., and Roshko, A., "Observation of Supersonic Free Shear Layer," AIAA Paper 86-0162, Jan. 1986.