Numerical simulation of jet fuel heat transfer and deposition at supercritical pressure

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages

  Zhou, Ning ^a   Krishnan, Anantha ^a  

^a CFD RESEARCH CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; DEPOSITION; FUEL SYSTEMS; FUELS; HEAT TRANSFER; JET FUEL; PROPULSION; REYNOLDS NUMBER; SPECIFIC HEAT;

COMPUTATIONAL FLUID DYNAMICS CODES; FUEL DEPOSITION; HEAT TRANSFER MODEL; HIGH PERFORMANCE AIRCRAFTS; NUMERICAL RESULTS; REAL-FLUID PROPERTIES; REDUCED PRESSURE; SUPER-CRITICAL PRESSURES;

FIGHTER AIRCRAFT;

EID: 84962784397     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

1. Krishnan, A., Zhou, N. and Giridharan, M.G., “Transport Phenomena in Supercritical Fluids,” AIAA paper 95-2233.
2. Zhou, N. and Krishnan A., “Supercritical Heat Transfer in Aircraft Fuel Systems,” AIAA paper 95- 3032.
3. Zhou, N. and Krishnan, A., “A Numerical Model for Endothermic Fuel Flows with Heterogeneous Catalysis,” AIAA paper 96-0650.
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13. Krieger, J. Master Thesis, U. of Iowa, 1995.
14. Edwards, T. and Krieger J., “The Thermal Stability of Fuels at 480°C (900 F). Effect of Teat Time, Flow Rate, and Additives,” ASME 95-GT 68. Presented at the Int. Gas Turbine & Aeroengine Cong. & Expo., Houston, TX, June 5-8, 1995
15. Zhou, N. and Krishnan A., “Calibration of a Global Mechanism for Jet Fuel Deposition,” AIAA paper 96-3238.
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