Optical and pressure measurements in shock tunnel testing of a model scramjet combustor

Journal of Propulsion and Power

Volumn 13, Issue 3, 1997, Pages 388-394

  McIntyre, T J ^a,b,c   Houwing, A F P ^a,c   Palma, P C ^a,c   Rabbath, P A B ^a   Fox, J S ^a  

^a AUSTRALIAN NATIONAL UNIVERSITY   (Australia)

^b UNIVERSITY OF QUEENSLAND   (Australia)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CENTRAL STREAMWISE INJECTED PLANAR HYDROGEN JET; EMISSION IMAGES; LASER INDUCED FLUORESCENCE TECHNIQUE; SCRAMJET COMBUSTOR; SHADOWGRAPH; SHOCK TUNNEL TESTING;

COMBUSTION; DENSITY (OPTICAL); DUCTS; ENTHALPY; EQUIPMENT TESTING; FLUORESCENCE; IGNITION; LASER BEAM EFFECTS; PRESSURE MEASUREMENT; RAMJET ENGINES; SUPERSONIC FLOW; TEMPERATURE DISTRIBUTION;

COMBUSTORS;

EID: 0031145840     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5196     Document Type: Article

References (18)

1. Hall, J. L., Dimotakis, P. E., and Rosemann, H., "Experiments in Nonreacting Compressible Shear Layers," AIAA Journal, Vol. 31, No. 12, 1993, pp. 2247-2254.
2. Miller, M. F., "An Experimental Investigation of the Effect of Compressibility on a Turbulent Reacting Mixing Layer," Stanford Univ., High Temperature Gas Lab., Rept. T-299, Stanford, CA, 1994.
3. Quagliaroli, T. M., Laufer, G., Hollo, S. D., Krauss, R. H., Whitehurst, R. B., III, and McDaniel, J. C., Jr., "Planar KrF Laser-Induced OH Fluorescence Imaging in a Supersonic Combustion Tunnel," Journal of Propulsion and Power, Vol. 10, No. 3, 1994, pp. 377-381.
4. Allen, M. G., Parker, T. E., Reinecke, W. G., Legner, H. H., Foutter, R. R., Rawlins, W. T., and Davis, S. J., "Fluorescence Imaging of OH and NO in a Model Supersonic Combustor," AIAA Journal, Vol. 31, No. 3, 1993, pp. 505-512.
5. Casey, R. T., and Stalker, R. J., "Hydrogen Mixing and Combustion in a High-Enthalpy Hypersonic Stream," Shock Waves @ Marseille, Vol. 1, Springer-Verlag, 1995, pp. 321-326.
6. Bélanger, J., and Hornung, H., "Transverse Jet Mixing and Combustion Experiments in Hypervelocity Flows," Journal of Propulsion and Power, Vol. 12, No. 1, 1996, pp. 186-192.
7. Bakos, R., Tamagno, J., Trucco, R., Rizkalla, O., Chinitz, W., and Erdos, J. I., "Mixing and Combustion Studies Using Discrete Orifice Injection at Hypervelocity Flight Conditions," Journal of Propulsion and Power, Vol. 8, No. 6, 1992, pp. 1290-1296.
8. Paull, A., Stalker, R. J., and Mee, D. J., "Scramjet Thrust Measurement in a Shock Tunnel," Aeronautical Journal, Vol. 99, No. 984, 1995, pp. 161-163.
9. Stalker, R. J., "Development of a Hypervelocity Wind Tunnel," Aeronautical Journal of the Royal Aeronautical Society, Vol. 76, No. 738, 1972, pp. 374-384.
10. McIntosh, M. K., "Computer Program for the Numerical Calculation of Frozen and Equilibrium Conditions in Shock Tunnels," Australian National Univ., Canberra, Australia, 1968.
11. Vardavas, I., "Modelling Reactive Gas Flows Within Shock Tunnels," Australian Journal of Physics, Vol. 37, No. 2, 1984, pp. 157-161.
12. Seitzman, J. M., and Hanson, R. K., "Comparison of Excitation Techniques for Quantitative Fluorescence Imaging of Reacting Flows," AIAA Journal, Vol. 31, No. 3, 1993, pp. 513-519.
13. Crane, K. C. A., and Stalker, R. J., "Mass Spectrometric Analysis of Hypersonic Flows," Journal of Physics D, Vol. 10, No. 5, 1977, pp. 679-695.
14. McIntyre, T. J., Rabbath, P. A. B., and Houwing, A. F. P., "Imaging of Combustion Processes in a Supersonic Combustion Ramjet," The Second Pacific International Conf. on Aerospace Science and Technology (PICAST), Melbourne, Australia, March 1995.
15. McIntyre, T. J., Rabbath, P. A. B., and Houwing, A. F. P., "Imaging of Combustion Processes in a Supersonic Combustion Ramjet," 12th International Symposium on Air Breathing Engines, Vol. 2, 1995, pp. 1163-1171.
16. Davis, M. G., McGregor, W. K., and Mason, A. A., "OH Chemiluminescent Radiation from Lean Hydrogen-Oxygen Flames," Journal of Chemical Physics, Vol. 61, 1973, pp. 1352-1356.
17. Palma, P. C., Houwing, A. F. P., and Sandeman, R. J., "Absolute Intensity Measurements of Impurity Emissions in a Shock Tunnel and Their Consequences for Laser-Induced Fluorescence Measurements," Shock Waves, Vol. 3, No. 1, 1993, pp. 49-53.
18. Yip, B., Miller, M. F., Lozano, A., and Hanson, R. K., "A Combined OH/Acetone Planar Laser-Induced Fluorescence Technique for Visualizing Combustion Flows," Experiments in Fluids, Vol. 17, 1994, pp. 330-336.