Sensitivity of hydrocarbon combustion modeling for hypersonic missile design

Journal of Propulsion and Power

Volumn 19, Issue 1, 2003, Pages 89-97

  Starkey, Ryan P ^a   Lewis, Mark J ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT PROPULSION; FUEL INJECTION; GENETIC ALGORITHMS; HEAT FLUX; HYDROCARBONS; MATHEMATICAL MODELS; MISSILES; MIXING; OPTIMIZATION; PERTURBATION TECHNIQUES; SPECIFIC HEAT;

FUEL MASS FRACTION; FUEL MIXING EFFICIENCY; FUEL MIXING LENGTH; HYDROCARBON COMBUSTION MODELING; HYPERSONIC MISSILE DESIGN; VISCOUS LOSS;

COMBUSTORS;

EID: 0037278917     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.6084     Document Type: Article

References (29)

1. Starkey, R. R., and Lewis, M. J., "Critical Design Issues for Airbreathing Hypersonic Waverider Missiles," Journal of Spacecraft and Rockets, Vol. 38, No. 5, 2001, pp. 510-519.
2. Nonweiler, T. R. F., "Aerodynamic Problems of Manned Space Vehicles," Journal of the Royal Aeronautical Society, Vol. 63, Sept. 1959, pp. 521-528.
3. Center, K. B., Sobieczky, H., and Dougherty, F. C., "Interactive Design of Hypersonic Waverider Geometries," AIAA Paper 91-1697, June 1991.
4. Takashima, N., and Lewis, M. J., "Navier-Stokes Computation of a Viscous Optimized Waverider," AIAA Paper 92-0305, Jan, 1992.
5. Gillum, M. J., and Lewis, M. J., "Experimental Results on a Mach 14 Waverider with Blunt Leading Edges," Journal of Aircraft, Vol. 34, No. 3, 1997, pp. 296-303.
6. Starkey, R. P., and Lewis, M. J., "Simple Analytical Model for Parametric Studies of Hypersonic Waveriders," Journal of Spacecraft and Rockets, Vol. 36, No. 4, 1999, pp. 516-523.
7. Starkey, R. P., "A Parametric Study of L/D and Volumetric Efficiency Trade-Offs for Waverider Based Vehicles," M.S. Thesis, Dept. of Aerospace Engineering, Univ. of Maryland, College Park, June 1998.
8. Starkey, R. P., "Investigation of Air-Breathing, Hypersonic Missile Configurations Within External Box Constraints," Ph.D. Dissertation, Dept. of Aerospace Engineering, Univ. of Maryland, College Park, Oct. 2000.
9. Anderson, J. D., Modern Compressible Flow: with Historical Perspective, McGraw-Hill, New York, 1990.
10. Anderson, J. D., Hypersonic and High Temperature Gas Dynamics, McGraw-Hill, New York, 1989.
11. Taylor, G. I., and Maccoll, J. W., "The Air Pressure on a Cone Moving at High Speed," Proceedings of the Royal Society of London, Vol. 139, 1933, pp. 278-311.
12. White, F. M., Viscous Fluid Flow, 2nd ed., McGraw-Hill, New York, 1991.
13. Bowcutt, K., Anderson, J., and Capriotti, D., "The Viscous Optimized Hypersonic Waveriders," AIAA Paper 87-0272, 1987.
14. Waltrup, P. J., White, M. E., Zarlingo, F., and Gravlin, E. S., "History of U.S. Navy Ramjet, Scramjet, and Mixed-Cycle Propulsion Development," AIAA Paper 96-3152, 1996.
15. O'Brien, T., Starkey, R. P., and Lewis, M. J., "A Quasi-One-Dimensional High-Speed Engine Model with Finite-Rate Chemistry," Journal of Propulsiona and Power, Vol. 17, No. 6, 2001, pp. 1366-1374.
16. Shapiro, A. H., The Dynamics and Thermodynamics of Compressible Fluid Flow, Vol. 1, McGraw-Hill, New York, 1953.
17. Turns, S. R., An Introduction to Combustion, McGraw-Hill, New York, 1996.
18. O'Brien, T., and Lewis, M. J., "RBCC Engine-Airframe Integration on an Osculating Cone Waverider Vehicle," AIAA Paper 2000-3823, July 2000.
19. Billig, F. S., and Grenleski, S. E., "Heat Transfer in Supersonic Combustion Processes," Heat Transfer 1970, Vol. III, Elsevier, 1970.
20. Anderson, G. Y., and Gooderum, P. B., "Exploratory Tests of Two Strut Fuel Injectors for Supersonic Combustion," NASA TN D-7581, 1974.
21. Byrne, G. D., Hindmarch, A. C., and Brown, P. N., "VODPK: Variable-Coefficient Ordinary Differential Equation Solver with the Preconditioned Krylov Method GMRES for the Solution of Linear Systems," Lawrence Livermore National Lab., Livermore, CA, 1997.
22. Kee, R. J., Rupley, F. M., and Miller, J. A., "Chemkin-II: A Fortran Chemical Kinetics Package for the Analysis of Gas Phase Chemical Kinetics," SAND 89-8009B, Sandia National Labs., Livermore, CA, 1989.
23. Kundu, K. P., Penko, P. E., and Yang, S. L., "Reduced Reaction Mechanisms for Numerical Calculations in Combustion of Hydrocarbon Fuels," AIAA Paper 98-0803, Jan. 1998.
24. Chang, J. S., "Development of a Jet-A/Silane/Hydrogen Reaction Mechanism for Modeling a Scramjet Combustor," Scholarly Paper, Dept. of Aerospace Engineering, Univ. of Maryland, College Park, 1999.
25. Lewis, M. J., and Chang, J. S., "Joint Jet-A/Silane/Hydrogen Reaction Mechanism," Journal of Propulsion and Power, Vol. 16, No. 2, 2000, pp. 365-367.
26. Rogers, R. C., "Mixing of Hydrogen Injected from multiple Injectors Normal ot a Supersonic Airstream," NASA TN D-6476, 1971.
27. Goldberg, D. E., Genetic Algorithms in Search, Optimization, and Machine Learning, Addison Wesley Longman, Reading, MA, 1989.
28. Michalewicz, Z., Genetic Algorithms + Data Structures = Evolution Programs, Springer-Verlag, New York, 1996.
29. Geist, A., Beguelin, A., Dongarra, J., Jiang, W., Manchek, R., and Sunderam, V., PVM: Parrallel Virtual Machine-A User's Guide and Tutorial for Networked Parallel Computing, MIT Press, London, 1994.