Analysis of supersonic combustors with swept ramp injectors

Journal of Propulsion and Power

Volumn 13, Issue 2, 1997, Pages 327-328

  Baurle, R A ^a,b,c,d   Alexopoulos, G A ^a,b,d   Hassan, H A ^a,b,d  

^a NORTH CAROLINA STATE UNIVERSITY   (United States)

^b Mechanical and Aerospace Engineering   (United States)

^c Taitech Inc   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CALCULATIONS; COMPUTATIONAL FLUID DYNAMICS; FLOW VISUALIZATION; HEAT TRANSFER; MATHEMATICAL MODELS; PRANDTL NUMBER; PROBABILITY DENSITY FUNCTION; SUPERSONIC FLOW; TURBULENCE;

SCHMIDT NUMBER; SUPERSONIC COMBUSTORS; SWEPT RAMP INJECTORS; TURBULENCE CHEMISTRY INTERACTIONS;

COMBUSTORS;

EID: 0031101741     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.7643     Document Type: Article

References (7)

1. Stouffer, S. D., Baker, N. R., Capriotti, D. P., and Northam, G. B., "Effects of Wall Ramp Angle on Combustion and Heat Transfer During Mach 2.7 Direct Connect Testing of a Scramjet Combustor," AIAA Paper 93-0609, Jan. 1993.
2. Stouffer, S. D., Vandsburger, U., and Northam, G. B., "Comparison of Wall Mixing Concepts for Scramjet Combustors," AIAA Paper 94-0587, Jan. 1994.
3. Eklund, D. R., and Stouffer, S. D., "A Numerical and Experimental Study of a Supersonic Combustor Employing Swept Ramp Fuel Injectors," AIAA Paper 94-2819, June 1994.
4. Wilcox, D. C., "Turbulence and Transition Modeling for High Speed Flows," NASA CR 191473, April 1993.
5. Baurle, R. A., Alexopoulos, G. A., and Hassan, H. A., "Analysis of Supersonic Combustors with Swept Ramp Injectors," AIAA Paper 95-2413, July 1995.
6. Zhang, H. S., Speziale, C. G., and Lai, Y. G., "A Near Wall Two-Equation Model for Compressible Turbulent Flows," AIAA Paper 92-0442, Jan. 1992.
7. Warren, E. S., Harris, J. E., and Hassan, H. A., "A Transition Model for High Speed Flows," AIAA Paper 94-1851, June 1994.