Study of a supersonic combustor employing swept ramp fuel injectors

Journal of Propulsion and Power

Volumn 13, Issue 6, 1997, Pages 697-704

  Eklund, Dean R ^a,d   Stouffer, Scott D ^b,d,e   Northam, G Burton ^c,d,f  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

^b VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

^d AIAA   (United States)

^e UNIVERSITY OF DAYTON   (United States)

^f Environmental Interactions Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGEBRA; COMPUTER AIDED ANALYSIS; FLOW VISUALIZATION; FUEL INJECTION; HEAT FLUX; MATHEMATICAL MODELS; MIXING; NAVIER STOKES EQUATIONS; RAMJET ENGINES; REACTION KINETICS; SUPERSONIC FLOW; TURBULENCE;

SCRAMJET COMBUSTORS; SOFTWARE PACKAGE SPARK; SWEPT RAMP FUEL INJECTORS;

COMBUSTORS;

EID: 0031275657     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5230     Document Type: Article

References (23)

1. Mays, R. B., Thomas, R. H., and Schetz, J. A., "Low Angle Injection into a Supersonic Flow," AIAA Paper 89-2461, July 1989.
2. Kraus, D. K., and Cutler, A. D., "Mixing Enhancement by the Use of Swirling Jets," AIAA Paper 93-3126, July 1993.
3. Gutmark, E., Schadow, K. C., and Wilson, K. J., "Noncircular Jet Dynamics in Supersonic Combustion," Journal of Propulsion and Power, Vol. 5, No. 5, 1989, pp. 529-533.
4. Haimovitch, Y., Gartenberg, E., Roberts, A. S., and Northam, G. B., "An Investigation of Wall Injectors for Supersonic Mixing Enhancement," AIAA Paper 94-2940, June 1994.
5. Zaman, K. B. M. Q., Reeder, M. F., and Samimy, M., "Supersonic Jet Mixing Enhancement by Delta-Tabs," AIAA Paper 92-3548, July 1992.
6. Menon, S, "Shock Waves for Enhanced Mixing in Scramjet Combustors," NASA CR-1028, Dec. 1989.
7. Northam, G. B., Greenberg, I., Byington, C. S., and Capriotti, D. P., "Evaluation of Parallel Injector Configurations for Mach 2 Combustion," Journal of Propulsion and Power, Vol. 8, No. 2, 1992, pp. 491-499.
8. Riggins, D. W., and McClinton, C. R., "A Computational Investigation of Flow Losses in a Supersonic Combustor," AIAA Paper 90-2093, July 1990.
9. Waitz, I. A., Marble, F. E., and Zukosi, E. E., "A Systematic Experimental and Computational Investigation of a Class of Contoured Wall Injectors," AIAA Paper 92-0625, Jan. 1992.
10. Davis, D. L., "Numerical Analysis of Techniques for Efficient Generation of Vorticity in Supersonic Flows," AIAA Paper 92-0828, Jan. 1992.
11. Donohue, J. M., McDaniel, J. C., and Haj-Hariri, H., "Experimental and Numerical Study of Swept Ramp Injection into a Supersonic Flowfield," AIAA Paper 93-2445, June 1993.
12. Stouffer, S. D., "The Effect of Flow Structure on the Combustion and Heat Transfer in a Scramjet Combustor," Ph.D. Dissertation, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 1995.
13. Eklund, D., and Stouffer, S., "A Numerical and Experimental Study of a Supersonic Combustor Employing Swept Ramp Fuel Injectors," AIAA Paper 94-2819, June 1994.
14. Drummond, J. P., A Two-Dimensional Numerical Simulation of a Supersonic, Chemically Reacting Mixing Layer," NASA TM-4055, Dec. 1988.
15. Carpenter, M. H., "Three Dimensional Computations of Cross-Flow Injection and Combustion in a Supersonic Flow," AIAA Paper 89-1870, June 1989.
16. Eklund, D. R., and Northam, G. B., A Numerical Study of the Effects of Geometry on the Performance of a Supersonic Combustor," AIAA Paper 92-0624, Jan. 1992.
17. Baldwin, B. S., and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-257, Jan. 1978.
18. Eggers, J. M., "Turbulent Mixing of Coaxial Compressible Hydrogen-Air Jets," NASA TN D-6487, Sept. 1971.
19. Eklund, D., Fletcher, D., Hartfield, R., McDaniel, J., Northam, G., Dancey, C., and Wang, J., "A Computational/Experimental Investigation of Staged Injection into a Mach 2 Flow," AIAA Journal, Vol. 32, No. 5, 1994, pp. 907-916.
20. Jachimowski, C. J., "An Analytical Study of the Hydrogen-Air Mechanism with Application to Scramjet Combustion," NASA TP 2791, Feb. 1988.
21. Jachimowski, C. J., "An Analysis of Combustion Studies in Shock Expansion Tunnels and Reflected Shock Tunnels," NASA TP-3224, July 1992.
22. Anderson, D. A., Tannehill, J. C., and Pletcher, R. H., Computational Fluid Mechanics and Heat Transfer, McGraw-Hill, New York, 1984, pp. 247-251.
23. White, J. A., "Elliptic Grid Generation with Orthogonality and Spacing Control on an Arbitrary Number of Boundaries," AIAA Paper 90-1568, June 1990.