A new passive boundary-layer control device

Journal of Aircraft

Volumn 14, Issue 7, 1977, Pages 654-660

  Sajben, M ^a   Chen, C P ^a   Kroutil, J C ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85003411168     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.58837     Document Type: Article

References (11)

1. Anon., “To Improve Control at the Stall,” The Aeroplane, Aug. 1934, pp. 256-257.
2. Moser, A., “Experimental Investigation of Wake/Boundary Layer Interaction and The Flow Control Rail,” McDonnell Douglas Report MDCQ0511, Dec. 1973.
3. Sajben, M., Kroutil, J. C., Sedrick, A. V., and Hoffman, G. H., “Experiments on Conical Diffusers with Distorted Inflow,” AIAA Paper 74-529, Palo Alto, Calif., 1974.
4. Sajben, M., Kroutil, J. C., and Sedrick, A. V., “Performance and Exit Distortion of Diffusers as Determined by Force Measurements,” McDonnell Douglas Research Laboratories, Paper MDRL 74-2, 1974.
5. Bower, W. W., “An Analytical Procedure for the Calculation of Attached and Separated Subsonic Diffuser Flows,” Journal of Aircraft, Vol. 13, Jan. 1976, pp. 49-56.
6. Sajben, M., Chen, C. P., and Kroutil, J. C., “Comparison of Conventional and Force-Based Distortion Index Measurements,” AIAA Journal, Vol. 14, Oct. 1976, pp. 1500-1501.
7. Farr, A. P., “Evaluation of F-15 Inlet Dynamic Distortion,” AIAA Paper 73-784, St. Louis, Mo., 1973.
8. Taylor, H. D., “Summary Report on Vortex Generators,” United Aircraft Corporation Rept. R-05280-9, 1950.
9. Valentine, E. F. and Carroll, R. B., “Effects of Some Primary Variables of Rectangular Vortex Generators on the Static-Pressure Rise Though a Short Diffuser,” NACA RM L52B13, 1952.
10. Senoo, Y. and Nishi, M., “Improvements of the Performance of Conical Diffusers by Vortex Generators,” Journal of Fluid Engineering, Vol. 96, Part 4, March 1974, pp. 4-10.
11. McDonald, A. T., Fox, R. W., and Van Dewoestine, R. V., Effect of Swirling Inlet Flow on Pressure Recovery in Diffusers, AIAA Journal, Vol. 9, Oct. 1971, pp. 2014-2018.