Review of fuel pre-injection studies in a high speed airflow

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 16, Issue , 2006, Pages 12357-12370

  Vinogradov, Viacheslav A ^a,c,d   Shikhman, Yurii M ^a,c   Segal, Corin ^b,d  

^a CENTRAL INSTITUTE OF AVIATION MOTORS   (Russian Federation)

^b UNIVERSITY OF FLORIDA   (United States)

^c Department of Laboratory ^*  (Russian Federation)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FOSSIL FUELS; JET AIRCRAFT; ORGANIC COMPOUNDS; PROPULSION; SUPERSONIC FLOW;

AVIATION MOTORS; FLAME STABILITY; IMPULSE LOSSES;

FUEL INJECTION;

EID: 34250875011     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-1030     Document Type: Conference Paper

References (26)

1. Seiner, J.M., Dash, S.M., Kenzakovich, D.C., "Historical Survey on Enhanced Mixing in Scramjet Engines". AIAA Paper No. 99-4869, Nov. 1999.
2. Henry, J.R. and Anderson, G.Y., "Design considerations for the Airframe-lntegrated Scramjet", NASA TM X-2895, Dec. 1973.
3. "Investigations of the Low speed Fixed Geometry Supersonic Combustion Ramjet", General Applied Science Laboratories, AFAPL-TR-66-139, March 1967.
4. Vasiliev, V., Zakotenko, S.N., Krasheninnikov, S.Yu. and Stepanov, V.A. "Numerical Investigation of Mixing and Augmentation Behind Oblique Shock Waves", AIAA Journal, Vol. 32, No.2, 1994.
5. Sislian, J.P., Parent, B. «Hypervelocity Fuel/Air Mixing in a Shcramjet Inlet» Journal. of Propulsion and Power, Vol. 20, No. 2, March-April 2004, pp. 267-272.
6. Schwaitzentruber, I.E., Sislian, J.R., Parent, B. «Suppression of Premature Ignition in the Premixed Inlet Flow of a Shcramjet». Journal, of Propulsion and Power, Vol. 21, No. 1, January-February 2005, pp. 87-94.
7. Arai, T., Kasahara, J., Mukai, K., Sakima, F., "Experiments of Pre-Mixing Shock-Induced Combustion Scramjet with Forebody-Wall Fuel Injection". AIAA Paper No.2002-5243, Oct. 2002.
8. Star, J.B., Edwards, Jr.J., Smart, M.K., Baurle, R.A. "Numerical Simulation of Scrajet Combustion in a Shock Tunnel", AIAA Paper No. 2005-0428, Jan. 2005.
9. Vinogradov, V.A., Prudnikov, A.G., "Injection of Liquid into the Strut Shadow at Supersonic Velocities", SAE-931455, SAE Aerospace Atlantic Conference, Apr. 1993.
10. Golubev, A.G. Yagodkin, V.I. "Methods of Dispersity and Liquid Spray Droplet Concentration Definition by Using of Light Diffusion Integral Characteristics", Science Notes of CIAM, No.867, 1979 (in Russian).
11. Schetz, J.A. "Turbulent Flowfield. Mixing and Injection Process" Progress in Astronautics and Aeronautics, v.68, 1980
12. Northam, G.B., and Anderson, G.Y., "Supersonic Combustion Ramjet Research at Langley," AIAA Paper 86-0159, 1986.
13. Baranovski, S.I., and Schetz, J.A., "Effect of Injection Angle on Liquid Injection into Supersonic Flow," AIAA Paper 79-0383, 1979.
14. Northam, G.B., Capriotti, D.P., Byington, G.B., and Greenberg, I., "Evaluation of Parallel Injector Configurations for Mach 2 Combustion," Journal of Propulsion and Power, Vol. 8, No. 2, 1992, pp. 491-499.
15. Marble, F.E., Zukoski, E., Jacobs, J.W., Hendrics, G.J., and Waitz, I.A., "Shock Enhancement and Control of Hypersonic Mixing and Combustion " AIAA Paper 90-1981, 1990.
16. Vinogradov,V., Segal,C., Owens,M., and Mullargili,S., "Effect of Kerosene Preinjection on Combustion Flameholding in a Mach 1.6 Airflow". Journal of Propulsion & Power, Vol.17, No.3, pp.605-611, 2001.
17. Shikhman, Yu. M., Vinogradov, V.A., Yanovskiy, L.S., Stepanov,V.A., Shlyakotin, V.E., Pen'kov,S.N, "The Demonstrator of Technologies - Endothermic Hydrocarbon Fueled Dual Mode Scramjet." AIAA Paper 1787-2001, 2001.
18. Vinogradov, V.A., Shikhman, Yu.M., Albegov, R.V., Vedeshkin, G.K., Albegov, R.V., Vedeshkin, G.K., "Experimental Research of Pre-lnjected Methane Combustion in High Speed Airflow", AIAA Paper 2003-6940, 2003.
19. Heiser, W.H., Pratt, D.T., Daley, D.H. and Mehta, U.B., Hypersonic Airbreathing Propulsion, AIAA Education Series, AIAA, Washington, DC, 1994.
20. Buriko, Yu., Vinogradov, V., Goltsev, V. Waltrup, P. "Influence of Active Radical Concentration on Self-Ignition Delay of Hydrocarbon Fuel/Air Mixture". Journal of Propulsion & Power, v.18 # 5, Sept.-Oct., 2002, pp.1049-1058.
21. Livingston,T., Segal,C., Schindler,M. and Vinogradov,V.A., "Penetration and Spreading of Liquid Jets in an External-Internal Compression Inlet", AIAA Journal, Vol.38, No. 6, pp. 989-994, 2000.
22. Goldfeld, M., Starov, A., and Vinogradov, A. "Experimental Study of Scramjet Module". Journal of Propulsion and Power, v.17, #6, Nov.-Dec. 2001, pp. 1222-1226).
23. Guoskov, O.V., Kopchenov, V.I., Lomkov, K.E., Vinogradov, V.A., Waltrup, P.J. "Numerical Researches of Gaseous Fuel Pre-lnjection in Hypersonic 3-D Inlet". Journal of Propulsion and Power, Vol.17, No. 6, Nov.-Dec. 2001, pp.1162-1169.
24. Bezgin,L., Ganzhelo,A.N., Gouskov,O.V., Kopchenov.V.I., Laskin,J., Lomkov,K.E., "Numerical simulation of supersonic flows applied to scramjet duct". ISABE 95-7082, 1995, pp. 895-905.
25. Ogorodnikov, D.A., Vinogradov, V.A., Petrov, M.D., Shikhman, Yu.M, Stepanov, V.A. "Some Results of CIAM Scramjet Technology", AIAA Paper No. 99-4030, 1999.
26. th ISABE Conference, Vol.1, 1997, pp.374-384.