Supersonic-inlet boundary-layer bleed flow

AIAA Journal

Volumn 34, Issue 4, 1996, Pages 778-785

  Harloff, Gary J ^a,b   Smith, Gregory E ^a,b  

^a AIAA ^*

^b NYMA Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0041499002     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13140     Document Type: Article

References (25)

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3. Cebeci, T., and Chang, K. C., "Calculation of Incompressible Rough-Wall Boundary Layer Flows," AIAA Journal, Vol. 16, No. 7, 1978, pp. 730, 731.
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7. Weir, L. J., NASA Lewis Research Center, Cleveland, OH, private communications, Sept. 1993.
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10. Benhachmi, D., Greber, I., and Hingst, W., "Experimental and Numerical Investigation of the Effect of Distributed Suction on Oblique Shock Wave/Turbulent Boundary Layer Interaction," NASA TM-101334, Aug. 1988.
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14. McLafferty, G., and Ranard, E., "Pressure Losses and Flow Coefficients of Slanted Perforations Discharging from Within a Simulated Supersonic Inlet," R-0920-1, United Aircraft Corp., 1958.
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16. Chyu, W. J., Rimlinger, M. J., and Shih, T. I-P., "Effects of Bleed-Hole Geometry and Plenum Pressure on Three-Dimensional Shock-Wave/Boundary-Layer/Bleed Interactions," AIAA Paper 93-3259, July 1993.
17. Hahn, T. O., and Shih, T. I-P., "Numerical Study of Shock-Wave/ Boundary-Layer Interactions with Bleed," AIAA Journal, Vol. 31, No. 5, 1993, pp. 869-876.
18. Davis, D. O., Willis, B., and Hingst, W., "Flowfield Measurements of Slot-Bleed/Oblique Shock-Wave Interaction," AIAA Paper 95-0032, Jan. 1995.
19. Bragg, S. L., "Effect of Compressibility on the Discharge Coefficient of Orifices and Convergent Nozzles," Journal of Mechanical Engineering Science, Vol. 2, No. 1, 1960, pp. 35-44.
20. Davis, D. O., Hingst, W. R., and Bodner, J. P., "Flow Coefficient Behavior for Isolated Normal and 20 Degree Boundary Layer Bleed Holes," NASA TM 106816, 1995.
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22. Smith, G. E., "Bleed Modeling," NASA Lewis Research Center, Workshop in Inlet Bleed Modeling, Sept. 1993.
23. Syberg, J., and Koncsek, J. L., "Bleed System Design Technology for Supersonic Inlets," AIAA Paper 72-1138, Nov. 1972.
24. Dennard, J. S., "A Transonic Investigation of the Mass-Flow and Pressure Recovery Characteristics of Several Types of Auxiliary Air Inlets," RM L57B07, NACA, 1957.
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