Investigation of vaporized kerosene injection in a supersonic model combustor

12th AIAA International Space Planes and Hypersonic Systems and Technologies

Volumn , Issue , 2003, Pages

  Yu, G ^a   Li, J G ^a   Zhao, Z ^a   Chang, X Y ^a   Sung, C J ^b  

^a INSTITUTE OF MECHANICS   (China)

^b Case Western Reserve University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EVAPORATION PROCESS; HEATING SYSTEM; INJECTION PRESSURES; INJECTION TEMPERATURE; KEROSENE INJECTION; MODEL COMBUSTOR; PREHEAT TEMPERATURE; SUPERSONIC COMBUSTORS;

COMBUSTORS; PREHEATING; TEMPERATURE MEASUREMENT; VAPORS;

KEROSENE;

EID: 84896693586     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Tishkoff, J.M, Drummond, J.P, Edwards, T, and Nejad, A.S.,"Future Direction of Supersonic Combustion Research: Air Force/NASA Workshop on Supersonic Combustion," AIAA Paper 97-1017, 1997.
2. Yu, G., Li, J.G., Chang, X.Y., Chen, L.H., and Sung, C.J., "Fuel Injection and Flame Stabilization in a Liquid-Kerosene-Fueled Supersonic Combustor," Journal of Propulsion and Power, Vol. 19, No. 5, 2003, pp. 885-893.
3. Yu G, Li, J.G., Yang, S.R., Yue, L.J., Chang, X.Y., Huang, Y., and Sung, C.J., "Characteristics of Kerosene Combustion in Supersonic Flow Using Effervescent Atomization," AIAA Paper 2002-5225, 2002.
4. th edition, CRC PRESS.