Sonic Injection into a Mach 5.0 Freestream Through Diamond Orifices

Journal of Propulsion and Power

Volumn 20, Issue 2, 2004, Pages 280-287

  Bowersox, Rodney D W ^a,c   Fan, Huaiguo ^b,d   Lee, Daina ^b,d  

^a TEXAS A AND M UNIVERSITY   (United States)

^b UNIVERSITY OF ALABAMA   (United States)

^c Department of Aerospace Engineering ^*  (United States)

^d Aerospace Engineering and Mechanics   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMBUSTION; DIAMONDS; DISCHARGE (FLUID MECHANICS); FLOW VISUALIZATION; ORIFICES; REYNOLDS NUMBER;

DISCHARGE COEFFICIENT; SHADOWGRAPH PHOTOGRAPHY; SONIC INJECTION;

SUPERSONIC AERODYNAMICS;

EID: 1842787885     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.9254     Document Type: Article

References (24)

1. Beach, H., and Blankson, I., Jr., "Prospects for Future Hypersonic AirBreathing Vehicles," AIAA-91-5009, Dec. 1991.
2. Freeman, D. C., Jr., Reubush, D. E., McClinton, C. R., Rausch, V. L., and Crawford, J. F., "The NASA Hyper-X Program," 48th International Aeronautical Congress, NASA-97-48IAC-DCF, Turin, Italy, Oct. 1997.
3. Heiser, W., and Pratt, D., Hypersonic Airbreathing Propulsion, AIAA Education Series, AIAA, Washington DC, 1994, pp. 277-378.
4. Weber, R., and McKay, J., "Analysis of Ramjet Engines Using Supersonic Combustion," NACA TN-4386, Sept. 1958.
5. Riggins, D., McClinton, C., Rogers, R., and Bittner, R., "Investigation of Scramjet Injection Strategies for High Mach Number Flows," Journal of Propulsion and Power, Vol. 11, No. 3, 1995, pp. 409-418.
6. Schetz, J., Thomas, R., and Billig, F., "Mixing of Transverse Jets and Wall Jets Supersonic Flow," Separated Flows and Jets, edited by V. Kozlov and A Dovgal, Springer-Verlag, Berlin, 1991, pp. 807-835.
7. Wilson, M., Bowersox, R., and Glawe, D., "An Experimental Investigation of the Role of Downstream Ramps on a Supersonic Injection Plume," Journal of Propulsion and Power, Vol. 15, No. 3, 1998, pp. 432-439.
8. Zukowski, E., and Spaid, F., "Secondary Injection of Gases into a Supersonic Flow," AIAA Journal, Vol. 2, No. 10, 1964, pp. 1697-1705.
9. Schetz, J., and Billig, F., "Penetration of Gaseous Jets Injected into a Supersonic Stream," Journal of Spacecraft and Rockets, Vol. 3, No. 11, 1966, pp. 1658-1665.
10. Chenault, L., Beran, P., and Bowersox, R., "Second-Order Reynolds Stress Turbulence Modeling of Three-Dimensional Oblique Supersonic Injection," AIAA Journal, Vol. 37, No. 10, 1999, pp. 1257-1269.
11. McCann, G., and Bowersox, R., "Experimental Investigation of Supersonic Gaseous Injection into a Supersonic Freestream," AIAA Journal, Vol. 34, No. 2, 1996, pp. 317-323.
12. McClinton, C., "The Effects of Injection Angle on the Interaction Between Sonic Secondary Jets and a Supersonic Freestream," NASA TN D-6669, Feb. 1972.
13. Gruber, M., Nejad, A., Chen, T., and Dutton, C., "Mixing and Penetration Studies of Sonic Jets in a Mach 2 Freestream," Journal of Propulsion and Power, Vol. 11, No. 2, 1995, pp. 315-323.
14. Barber, M., Schetz, J., and Roe, L., "Normal Sonic Helium Injection Through a Wedge-Shaped Orifice into a Supersoni Flow," Journal of Propulsion and Power, Vol. 13, No. 2, 1997, pp. 257-263.
15. Fan, H., and Bowersox, R., "Gaseous Injection through Diamond Orifices at Various Incidence Angles into a Hypersonic Freestream," AIAA Paper 2001-1050, Jan. 2001.
16. Tomioka, S., Jacobsen, L., and Schetz, J., "Sonic Injection from Diamond-Shaped Orifices into a Supersonic Crossflow," Journal of Propulsion and Power, Vol. 19, No. 1, 2003, pp. 104-114.
17. Deissler, R., "Analysis of Turbulent Heat Transfer and Flow in the Entrance Region of Smooth Passages," NACA TN 3016, Oct. 1953.
18. Shames, I., Mechanics of Fluids, 4th ed., McGraw-Hill, New York, 2003, pp. 435, 436.
19. Bowersox, R., "Combined Laser Doppler Velocimetry and Cross-Wire Anemometry Analysis for Supersonic Turbulent Flow," AIAA Journal, Vol. 34, No. 11, 1996, pp. 2269-2275.
20. Anderson, J., Modern Compressible Flow, 2nd ed., McGraw-Hill, New York, 1990, pp. 294-306.
21. Volluz, R., Handbook of Supersonic Aerodynamics, Section 20, Wind Tunnel Instrumentation and Operation, Vol. 6, Ordnance Aerophysics Lab., NAVORD Rept. 1488, Daingerfield, TX, Jan. 1961.
22. Davis, J., GOSS, L., Crafton, J., and Dale, G., "Performance Characteristics and Methods of Application of Pressure Sensitive Paints," 8th Annual Pressure Sensitive Paint Workshop, NASA Langley Research Center, Langley, VA, Oct. 2000.
23. Billig, F., Orth, R., and Lasky, M., "A Unified Analysis of Gaseous Jet Penetration," AIAA Journal, Vol. 9, No. 6, 1971, pp. 1048-1058.
24. White, F., Viscous Fluid Flow, 2nd ed., McGraw-Hill, New York, 1991, pp. 543-556.