Supersonic combustion models application in advanced propulsion concepts

15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2008, Pages

  Battista, Francesco ^a   Cutrone, Luigi ^a   Ranuzzi, Giuliano ^a   Borreca, Stefano ^b  

^a ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

^b ALSTOM   (France)

Author keywords

[No Author keywords available]

Indexed keywords

3D CODES; 3D FLOW; ADIABATIC FLAME TEMPERATURE; COMBUSTION PRO-CESS; COMPLEX APPLICATIONS; EXPERIMENTAL DATA; IGNITION DELAY TIME; KINETIC MECHANISM; MIXING PROCESS; PROPULSION CONCEPT; PROPULSION SYSTEM; SCRAMJET COMBUSTORS; SCRAMJET ENGINES; SUPERSONIC COMBUSTION; SUPERSONIC MIXING; TEST CASE; TRADE-OFF ANALYSIS; VALIDATION TEST; WIND TUNNEL MODELS;

COMBUSTORS; IGNITION; PROPULSION; THERMAL CONDUCTIVITY; WIND TUNNELS;

THREE DIMENSIONAL;

EID: 77958512904     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. LAPCAT Project Description of Work, Contract for Specific Target Research and Innovation Project, Annex I, April 2006.
2. Battista F., Cutrone L., Ranuzzi G., C3NS Solver for Supersonic Combustion Simulations: Final Report, LAPCAT 6.4.4 Deliverable, April 2008, CIRA-CF-08-0484.
3. Evans J. S. and Schexnayder C. J. J., Influence of Chemical Kinetics and Unmixedness on Burning in Supersonic Hydrogen Flames, AIAA Journal, Vol. 18, No. 2, 1980, pp. 188-193.
4. Drummond, J. P. and Rogers, R. C., A Numerical Model for Supersonic Reacting Mixing Layers, Computer Methods in Applied Mechanics and Engineering, Vol.64, 1987, pp. 39-60.
5. Marinov N.M., Westbrook C.K. and Pitz W.J., Detailed and Global Chemical Kinetics Model for Hydrogen, Lawrence Livermore National Laboratory.
6. Park C., Review of Chemical-Kinetic Problems of future NASA Missions, I: Earth Entries, Journal of Thermophysics and Heat Transfer, Vol.7, No. 3 1993.
7. Gordon, S., McBride, Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket performance, Incident and Reflected Shocks and Chapman-Jouguet Detonations, NASA Report SP-273, 1971.
8. Hirshfelder, Curtiss, Bird, Molecular Theory of Gases and Liquids, John Wiley and Sons, New York, 1954.
9. Borrelli S., Pandolfi M., An Upwind Formulation for the Numerical Prediction of Non Equilibrium Hypersonic Flows, 12th International Conference on Numerical Methods in Fluid Dynamics, Oxford, United Kingdom, 1990.
10. Bonifacio S., Borreca S., Ranuzzi G., and Salvatore V., SPREAD: a Scramjet PREliminary Aerothermodynamic Design Code, 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, Canberra, Australia, November 2006.
11. Jachimowski, C. J., An Analytical Study of the Hydrogen-Air Reaction Mechanism with Application to Scramjet Combustion, NASA TP-2791, Feb. 1988.
12. Rogers C.R., Schexnayder C.J.Jr., Chemical Kinetic Analysis of Hydrogen-Air Ignition And Reaction Times, NASA-TP-1856,1981.
13. Grasso F., and Magi V., Simulation of Transverse Gas Injection in Turbulent Supersonic Air Flows, AIAA Journal, Vol.33, No.1, 1995.
14. Drummond, J. P., and Weidner, E. H., Numerical Study of a Scramjet Engine FlowField, AIAA Journal, Vol. 20, No. 9, 1982, pp.1182-1187.
15. Ebrahimi H. B., An Overview of Computational FluidDynamics for Application to Advanced Propulsion Systems, AIAA 2002-5130.
16. Ebrahimi H. B., Validation Database for Propulsion Computational Fluif Dynamics, Journal of Spacecraft and Rockets, Vol.34, No.5, September-October 1997.
17. Burrow M., and Kurkov A. P., Analytical and Experimental Study of Supersonic Combustion of Hydrogen in a Vitiated Airstream, NASA-TMV-2828, September 1973.
18. Huber P.W., Schexnayder C. J. J., McClinton C.R., Criteria for Self-Ignition of Supersonic Hydrogen-Air Mixture, NASA TP 1457, 1979.
19. Von Lavante E., Zeitz D., and Kallenberg M., Numerical Simulation of Supersonic Airflow with Transverse Hydrogen Injection, AIAA Journal, Vol.17, No.6, 2001.
20. Grasso F., and Falconi D., High-Speed Turbulence Modeling of Shock-Wave/Boundary-Layer Interaction, AIAA Journal, Vol. 31, No. 7, July 1993.
21. Odam, J., and Paull, A., Internal Combustor Scramjet Pressure Measurements in the T4 Shock Tunnel, AIAA Paper 2002-5244.
22. Star B. J, Edwards J. R. Jr, Smart M.K, Baurle R.A, Numerical Simulation of Scramjet Combustion in a Shock Tunnel, AIAA Paper 2005-0428.