Air high-enthalpy stagnation point heat flux calculation

Journal of Thermophysics and Heat Transfer

Volumn 12, Issue 4, 1998, Pages 608-610

  De Filippis, F ^a,b   Serpico, M ^a  

^a ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; CORRELATION METHODS; ENTHALPY; HYPERSONIC FLOW; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS;

AIR HIGH-ENTHALPY STAGNATION POINT HEAT FLUX; FAY-RIDDELL THEORY;

HEAT FLUX;

EID: 0032181347     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/2.6386     Document Type: Article

References (9)

1. Fay, J. A., and Riddell, F. R., "Theory of Stagnation Point Heat Transfer in Dissociated Air, Journal of the Aeronautical Sciences, Vol. 25, No. 2, 1992, pp. 73-85.
2. Winovich, W., and Carlson, W. C. A., "The 60-MW Shuttle Interaction Heating Facility," Proceedings of the 25th International Instrumentation Symposium, Instrument Society of America, ISA, Anaheim, CA, 1979.
3. Tran, H. K., and Rasky, D. J., "Thermal Response and Ablation Characteristics of Lightweight Ceramic Ablators," Journal of Spacecraft and Rockets, Vol. 31, No. 6, 1994, pp. 993-998.
4. Pandolfi, M., "On the Flux Difference Splitting Formulation," Notes on Numerical Fluid Mechanics, Vol. 24, Vieweg, Brunswick, Germany, 1989, pp. 466-481.
5. De Filippis, F., Serpico, M., Marini, M., Ravachol, M., and Tribot, J. P., "Comparison Between Numerical and Experimental Results on Different HERMES Elevon Shapes," Journal of Spacecracft and Rockets, Vol. 34, No. 3, 1997, pp. 272-278.
6. Serpico, M., Schettimo, A., Ciucci, A., Falconi, D., and Fabrizi, M., "VEGA Launcher Base Flow Prediction at Different Supersonic Mach Number," AIAA Paper 97-2302, June 1997.
7. Serpico, M., Monti, R., and Savino, R., "Heat Flux on Partially Catalytic Surfaces in Hypersonic Flows," Journal of Spacecracft and Rockets, Vol. 35, No. 1, 1998, pp. 9-15.
8. Rakich, J. V., Bailey, H. E., and Park, C., "Computation of Non-equilibrium, Supersonic Three-Dimensional Inviscid Flowfield over Blunt-Nosed Bodies," AIAA Journal, Vol. 21, No. 6, 1983, pp. 834-841.
9. Hirschfelder, J. O., Curtiss, C. F., and Bird, R. B., Molecular Theory of Gases and Liquids, 2nd ed., Wiley, New York, 1963, Chap. 7.