Flow rate analyses and calibrations of kerosene cracking for supersonic combustion

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2005, Pages

  Fan, Xuejun ^a   Yu, Gong ^a,b   Li, JianGuo ^a,b  

^a INSTITUTE OF GEOLOGY AND GEOPHYSICS   (China)

^b Institute of Mechanics   (China)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; GAS CHROMATOGRAPHY; GASES; KEROSENE; MASS TRANSFER; NOZZLES; PROPULSION; RATE CONSTANTS;

AVERAGE MOLECULAR WEIGHT; CHEMICAL FORMULAE; HIGH TEMPERATURE; IDEAL GAS MIXTURES; SUPERCRITICAL CONDITION; SUPERSONIC COMBUSTION; TEMPERATURE DEPENDENCIES; THREE-COMPONENT MIXTURES;

FLOW RATE;

EID: 85088179181     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-3555     Document Type: Conference Paper

References (6)

1. Fan, X. J., Yu, G., Li, J. G., Zhang, X. Y., and Sung, C. J., "Performance of a Supersonic Model Combustor using Vaporized Kerosene Injection," AIAA Paper 2004-3485, Fort Lauderdale, Florida, July 11-14, 2004.
2. Edwards, T, "Liquid Fuel and Propellant for Aerospace Propulsion: 1903-2003," Journal of Propulsion and Power, Vol. 19, No. 6, 2003, pp.1089-1107.
3. Ely, J. F., and Huber, M. L., "NIST Standard Reference Database 4 - NIST Thermophysical Properties of Hydrocarbon Mixtures," National Inst, of Standards, Gaithersburg, MD, Feb. 1990.
4. Edwards, T., and Anderson, S., "Results of High Temperature JP-7 Thermal Cracking Assessment," AIAA Paper 93-0806, Reno, NV, Jan. 11-14, 1993.
5. Dagaut, P., "On the Kinetics of Hydrocarbon Oxidation from Natural Gas to Kerosene and Diesel Fuel," Phys. Chem. Chem. Phys., Vol. 4, 2002, pp. 2079-2094.
6. Daniau, E., Bouchez, M., Bounaceur, R., Battin-Leclerc, F., Marquaire, P. M., and Fournet, R., "Contribution to Scramjet Active Cooling Analysis Using N-Dodecane Decomposition Model as a Generic Endothermic Fuel," AIAA Paper 2003-6920, Norfolk, Virginia, Dec. 15-19, 2003.