Correlation of separation angles induced by glancing interactions

AIAA Journal

Volumn 34, Issue 10, 1996, Pages 2198-2200

  Koide, S ^a,c   Saida, N ^b,d   Ogata, R ^b,e  

^a JAPAN DEFENSE AGENCY   (Japan)

^b AOYAMA GAKUIN UNIVERSITY   (Japan)

^c Tech R and D Institute   (Japan)

^d Faculty of Natural Systems   (Japan)

^e Department of Mechanical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0006716282     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13375     Document Type: Article

References (8)

1. Lu, F. K., and Settles, G. S., " Mach Number Effects on Conical Surface Features of Swept Shock-Wave/Boundary-Layer Interactions," AIAA Journal, Vol. 28, No. 1, 1990, pp. 91-97.
2. Deng, X. Y., and Liao, J. H., "Correlation of Conical Interactions Induced by Sharp Fins and Semicones," AIAA Journal, Vol. 31, No. 5, 1993, pp. 962, 963.
3. Rodi, P. E., and Dolling, D. S., "An Experimental/Computational Study of Sharp Fin Induced Shock Wave/Turbulent Boundary Layer Interactions at Mach 5: Experimental Results," AIAA Paper 92-0749, Jan. 1992.
4. Avduyevskiy, V. S., and Gretsov, V. K., "Investigation of a Three-Dimensional Separated Flow Around Semicones Placed on a Plane Plate," NASA TTF-13578, July 1971.
5. Saida, N., Ooka, T., and Koide, S., "Interaction Between Shock Waves and Boundary Layer Induced by a Semicone Placed on a Flat Plate," Journal of the Japan Society for Aeronautical and Space Sciences, Vol. 33, No. 374, 1985, pp. 159-166 (in Japanese).
6. Saida, N., Ogata, R., and Koide, S., "Shock Wave/Boundary Layer Interactions Induced by a Rhombic Delta Fin," Proceedings of the Symposium on Shock Waves, edited by R. Yamane, Tokyo Inst. of Technology, Tokyo, Japan, 1996, pp. 51-54 (in Japanese).
7. Koide, S., Griesel, C. J. W., and Stollery, J. L., "Correlation of Shock Angles Caused by Rhombic Delta Wings," AIAA Journal, Vol. 34, No. 7, 1996, pp. 1529-1531.
8. Koide, S., Griesel, C. J. W., and Stollery, J. L., "Effects of Strakes on a Glancing Shock Wave/Turbulent Boundary-Layer Interaction," Journal of Aircraft, Vol. 32, No. 5, 1995, pp. 985-992.