Unstarted inlet for direct-connect combustor experiments in a shock tunnel

Journal of Propulsion and Power

Volumn 16, Issue 4, 2000, Pages 718-720

  Boyce, R R ^a,b   Paull, A ^a   Stalker, R J ^a  

^a UNIVERSITY OF QUEENSLAND   (Australia)

^b IMPERIAL COLLEGE LONDON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTORS; ENTHALPY; INTAKE SYSTEMS; NOZZLES; STEADY FLOW; STREAM FLOW; SUPERSONIC FLOW;

DIRECT CONNECT COMBUSTORS; SHOCK TUNNELS;

AIRCRAFT PROPULSION;

EID: 0034227905     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5633     Document Type: Article

References (7)

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2. Stalker, R. J., "Shock Tunnels for Real Gas Hypersonics," AGARD Conf., Aerodynamics of Hypersonic Lifting Vehicles, Symposium of the AGARD Fluid Dynamics Panel, AGARD CP428, Bristol, UK, 6-9 April 1987.
3. Masuya, G., Komuro, T., Murakami, A., Shinozaki, N., Nakamura, A., Murayama, M., and Ohwaki, K., "Ignition and Combustion Performance of Scramjet Combustors with Fuel Injection Struts," Journal of Propulsion and Power, Vol. 11, No. 2, 1995, pp. 301-307.
4. Korkegi, R. H., "Comparison of Shock-Induced Two- and Three-Dimensional Incipient Turbulent Separation," AIAA Journal, Vol. 13, No. 4, 1975, pp. 534, 535.
5. McIntosh, M. K., "Computer Program for the Numerical Calculation of Frozen and Equilibrium Conditions in Shock Tunnels," Dept. of Physics, Australian National Univ., ANU Internal Rept., Canberra, Australia, Sept. 1968.
6. Lordi, J. A., Mates, R. E., and Moselle, J. R., "Computer Program for the Numerical Solution of Nonequilibrium Expansions of Reacting Gas Mixtures," NASA CR-472, May 1966.
7. Skinner, K. A., and Stalker, R. J., "Mass Spectrometer Measurements of Test Gas Composition in a Shock Tunnel," AIAA Journal, Vol. 34, No. 1, 1996, pp. 203-205.