Experimental investigation of supersonic gaseous injection into a supersonic freestream

AIAA Journal

Volumn 34, Issue 2, 1996, Pages 317-323

  McCann, Gregory J ^a,b   Bowersox, Rodney D W ^a,b  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

FLOW VISUALIZATION; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; SCHLIEREN SYSTEMS; STRESS CONCENTRATION; THREE DIMENSIONAL; TURBULENT FLOW;

SUPERSONIC FREESTREAM; SUPERSONIC GASEOUS INJECTION; TURBULENCE MODELLING;

SUPERSONIC AERODYNAMICS;

EID: 0030080322     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13066     Document Type: Article

References (18)

1. Fuller, E., Mays, R., Thomas, R., and Schetz, J., "Mixing Studies of Helium in Air at High Supersonic Speeds," AIAA Journal, Vol. 30, No. 9, 1992, pp. 2234-2243.
2. Mays, R., Thomas, R., and Schetz, J., "Low Angle Injection into a Supersonic Flow," AIAA Paper 89-2461, July 1989.
3. Schetz, J., Thomas, R., and Billig, F., "Mixing of Transverse Jets and Wall Jets in Supersonic Flow," Separated Flows and Jets, edited by V. V. Koslow and A. V. Dovgal, Springer-Verlag, Berlin, 1991, pp. 807-837.
4. McClinton, C., "The Effects of Injection Angle on the Interaction Between Sonic Secondary Jets and a Supersonic Free Stream," NASA TN-6669, Feb. 1972.
5. Papomoschou, D., and Roshko, A., "The Compressible Turbulent Shear Layer: An Experimental Study," Journal of Fluid Mechanics, Vol. 197, 1988, pp. 453-477.
6. Bowersox, R., and Schetz, J., "Compressible Turbulence Measurements in a High-Speed High Reynolds Number Mixing Layer," AIAA Journal, Vol. 32, No. 4, 1994, pp. 758-764.
7. Bowersox, R., "Thermal Anemometry," Handbook of Fluid Dynamics and Fluid Machinery,.edited by J. Schetz and A. Fuhs, Wiley, New York (to be published).
8. Volluz, R., Handbook of Supersonic Aerodynamics, Section 20, Wind Tunnel Instrumentation and Operation, Vol. 6, Ordance Aerophysics Lab., NAVORD Rept. 1488, Daingerfield, TX, 1961.
9. Anon., Hot-Wire/Hot-Film Anemometry Probes and Accessories, TSI Incorporated, St. Paul, MN, 1989.
10. Kovasznay, L., "The Hot-Wire Anemometer in Supersonic Flow," Journal of the Aeronautical Sciences, Vol. 17, Sept. 1950, pp. 565-584.
11. Spangenberg, W., "Heat-Loss Characteristics of Hot-Wire Anemometers at Various Densities in Transonic and Supersonic Flow," NACA TN 3381, May 1955.
12. Kistler, A., "Fluctuation Measurements in a Supersonic Turbulent Boundary Layer," Physics of Fluids, Vol. 2, No. 3, 1959, pp. 290-296.
13. Schetz, J., Injection and Mixing in Turbulent Flow, Vol. 68, Progress in Astronautics and Aeronautics, AIAA, New York, 1980.
14. Abramovich, G., Theory of Turbulent Jets, MIT Press, Cambridge, MA, 1963.
15. Kim., S.-W., and Benson, T., "Fluid Flow in a Row of Jets in Crossflow - A Numerical Study," AIAA Journal, Vol. 31, No. 5, 1993, pp. 806-811.
16. Cox, S., Fuller, R., Schetz, J., and Walters, R., "Vortical Interactions Generated by an Injector Array to Enhance Mixing in Supersonic Flow," AIAA Paper 94-0708, Jan. 1994.
17. Miller, R., Dotter, J., Bowersox, R., and Buter, T., "Compressible Turbulence Measurements in Supersonic Boundary Layers with Favorable and Adverse Pressure Gradients," Joint ASME/AIAA Second Symposium on Transitional and Turbulent Compressible Flows, Fed.-Vol. 224, 1995, pp. 193-200.
18. Morkovin, M., "Effects of High Acceleration on a Turbulent Supersonic Shear Layer," Proceedings of the Heat Transfer and Fluid Mechanics Institute, Vol. 4, 1955, pp. 1-17.