Tangential injection from overlaid slots into a supersonic stream

Journal of Propulsion and Power

Volumn 13, Issue 1, 1997, Pages 59-63

  Lewis, David P ^a,b   Schetz, Joseph A ^a  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b BBN TECHNOLOGIES   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FUEL INJECTION; INTERFEROMETRY; INTERNAL COMBUSTION ENGINES; PRESSURE MEASUREMENT; PROPULSION; SCHLIEREN SYSTEMS; SUBSONIC FLOW; SUPERSONIC FLOW; WIND TUNNELS;

INTERFEROGRAMS; MACH NUMBER; MULTIPLE OVERLAID SLOTS; PRESSURE DISTRIBUTION; SUBSONIC INJECTION; SUPERSONIC AIRSTREAM; TANGENTIAL INJECTION;

SUPERSONIC AERODYNAMICS;

EID: 0030731842     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5150     Document Type: Article

References (13)

1. Schetz, J. A., Gilreath, H. E., Waltrup, P. J., and Lewis, D. P., "Research on Slot Injection into a Supersonic Air Stream," Dept. of Aerospace Engineering, Univ. of Maryland, Rept. 68-1, U.S. Air Force Aero Propulsion Lab., TR-68-97, Dayton, OH, 1968.
2. Visich, M., and Libby, P. A., "Experimental Investigation of Mixing of Mach Number 3.95 Stream in Presence of Wall," NASA TN D-247, 1960.
3. Goldstein, R. J., Eckert, E. R. G., Tsou, R. K., and Haji-Sheikh, A., "Film Cooling with Air and Helium Injection Through a Rearward-Facing Slot into a Supersonic Air Flow," AIAA Journal, Vol. 4, No. 6, 1966, pp. 981-985.
4. Peterson, J. B., Jr., McRee, D. I., Adcock, J. B., and Braslow, A. L., "Further Investigation of Effect of Air Injection Through Slots and Porous Surfaces on Flat-Plate Turbulent Skin Friction at Mach 3," NASA TN D-3311, 1966.
5. Schetz, J. A., and Gilreath, H. E., "Tangential Slot Injection in Supersonic Flow," AIAA Journal, Vol. 5, No. 12, 1967, pp. 2149-2154.
6. Howell, G. A., and Tatro, R. F., "Tangential Fluid Injection for Control of Shock-Boundary Layer Integration," AIAA Paper 66-656, June 1966.
7. Gilreath, H. E., "An Investigation of Gaseous Tangential Injection in Supersonic Flow," Ph.D. Dissertation, Univ. of Maryland, College Park, MD, 1968.
8. Cary, A. M., Jr., and Hefner, J. N., "Film Cooling Effectiveness in Hypersonic Turbulent Flow," AIAA Journal, Vol. 8, No. 11, 1970, pp. 2090, 2091.
9. Zakkay, V., Sakell, L., and Parthasarathy, K., "An Experimental Investigation of Supersonic Slot Cooling," Proceedings of the 1970 Heat Transfer and Fluid Mechanics Inst., edited by Turgut Sarpkaya, Stanford Univ. Press, Stanford, CA, 1970, pp. 88-103.
10. Gilreath, H., and Schetz, J. A., "Transition and Mixing in the Shear Layer Produced by Tangential Injection in Supersonic Flow," Journal of Basic Engineering, Dec. 1971, pp. 610-618.
11. Burrows, M. C., and Kurkov, A. P., "Supersonic Combustion of Hydrogen in a Vitiated Air Stream Using Stepped-Wall Injection," AIAA Paper 71-721, June 1971.
12. Hyde, C. R., Smith, B. R., Schetz, J. A., and Walker, D. A., "Turbulence Measurements for Heated Gas Slot Injection in Supersonic Flow," AIAA Journal, Vol. 28, No. 9, 1990, pp. 1605-1614.
13. Schetz, J. A., Billig, F. S., Favin, S., and Gilreath, H. E., "Effects of Pressure Mismatch on Slot Injection in Supersonic Flow," International Journal of Turbo and Jet Engines, Vol. 9, No. 2, 1992, pp. 135-146.