Transverse jet mixing and combustion experiments in hypervelocity flows

Journal of Propulsion and Power

Volumn 12, Issue 1, 1996, Pages 186-192

  Bélanger, Jacques ^a,c   Hornung, Hans G ^b,c  

^a UNIVERSITY OF MINNESOTA   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; COMBUSTION; COMBUSTORS; ENTHALPY; HYDROGEN FUELS; MIXING; PRESSURE; RAMJET ENGINES; REYNOLDS NUMBER; SHOCK WAVES; TEMPERATURE; VELOCITY;

FREESTREAM VELOCITY; HYPERVELOCITY FLOWS; SCRAMJET PROPULSION SYSTEM; SHOCK TUNNEL; TRANSVERSE JET MIXING;

AERODYNAMICS;

EID: 0029679350     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.24009     Document Type: Article

References (10)

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2. Hornung, H. G., "Performance Data of the New Free Piston Shock Tunnel T5 at GALCIT," AIAA Paper 92-3943, July 1992.
3. Jacobs, P. A., Rogers, R. C., Weidner, E. H., and Bittner, R. D., "Flow Establishment in a Generic Scramjet Combustor," Journal of Propulsion and Power, Vol. 8, No. 4, 1992, pp. 890-899.
4. Rogers, R. C., and Weidner, E. H., "Scramjet Fuel-Air Mixing Establishment in a Pulse Facility," Journal of Propulsion and Power, Vol. 9, No. 1, 1993, pp. 127-133.
5. Bélanger, J., "Studies of Mixing and Combustion in Hypervelocity Flows with Hot Hydrogen Injection," Ph.D. Dissertation, California Inst. of Technology, Pasadena, CA, April 1993.
6. Germain, P., "The Boundary Layer on a Sharp Cone in High-Enthalpy Flow," Ph.D. Dissertation, California Inst. of Technology, Pasadena, CA, Nov. 1994.
7. He, Y., and Morgan, R. G., "Transition of Compressible High Enthalpy Boundary Layer Flow over a Flat Plate," 10th Australian Fluid Mechanics Conf., Univ. of Melbourne, Australia, Dec. 1989.
8. Riggins, D. W., McClinton, C. R., Rogers, R. C., and Bittner, R. D., "A Comparative Study of Scramjet Injection Strategies for High Mach Number Flows," AIAA Paper 92-3287, July 1992.
9. Dimotakis, P. E., and Hall, J. L., "A Simple Model for Finite Chemical Kinetics Analysis of Supersonic Turbulent Shear Layer Combustion," AIAA Paper 87-1879, June-July 1987.
10. Hermanson, J. C., and Dimotakis, P. E., "Effects of Heat Release in a Turbulent, Reacting Shear Layer," Journal of Fluid Mechanics, Vol. 199, Feb. 1989, pp. 333-375.