Experimental study of causes of unsteadiness of shock-induced turbulent separation

AIAA Journal

Volumn 36, Issue 3, 1998, Pages 371-378

  Unalmis O H ^a,b   Dolling, D S ^a,b  

^a The University of Texas at Austin   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000106746     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.373     Document Type: Article

References (15)

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2. Gramann, R. A., and Dolling, D. S., "Dynamics of Separation and Reattachment in a Mach 5 Unswept Compression Ramp Flow," AIAA Paper 90-0380, Jan. 1990.
3. Erengil, M. E., and Dolling, D. S., "Correlation of Separation Shock Motion with Pressure Fluctuations in the Incoming Boundary Layer," AIAA Journal. Vol. 29, No. 11, 1991, pp. 1868-1877.
4. Erengil, M. E., and Dolling, D. S., "Unsteady Wave Structure near Separation in a Mach 5 Compression Ramp Interaction," AIAA Journal, Vol. 29, No. 5, 1991, pp. 728-735.
5. Erengil, M. E., and Dolling, D. S., "Physical Causes of Separation Shock Unsteadiness in Shock Wave/Turbulent Boundary-Layer Interactions," AIAA Paper 93-3134, July 1993.
6. McClure, W. B., "An Experimental Study of the Driving Mechanism and Control of the Unsteady Shock Induced Turbulent Separation in a Mach 5 Compression Corner Flow," Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Texas, Austin, TX, Aug. 1992.
7. Dolling, D. S., and Brusniak, L., "Separation Shock Motion in Fin, Cylinder, and Compression Ramp Induced Turbulent Interactions," AIAA Journal, Vol. 27, No. 6, 1989, pp. 734-742.
8. Ünalmis, Ö. H., and Dolling, D. S., "Decay of Wall Pressure Field and Structure of a Mach 5 Adiabatic Turbulent Boundary Layer," AIAA Paper 94-2363, June 1994.
9. Beresh, S. J., Clemens, N. T., Dolling, D. S., and Comninos, M. C., "Investigation of the Causes of Large Scale Unsteadiness of Shock-Induced Separated Flow Using Planar Laser Imaging," AIAA Paper 97-0064, Jan. 1997.
10. Marshall, T. A., and Dolling, D. S., "Spanwise Properties of the Unsteady Separation Shock in a Mach 5 Unswept Compression Ramp Interaction," AIAA Journal, Vol. 30, No. 8, 1992, pp. 2056-2065.
11. Spina, E. F., "Organized Structures in a Supersonic Turbulent Boundary Layer," Ph.D. Dissertation, Dept. of Mechanical and Aerospace Engineering, Princeton Univ., Princeton, NJ, Oct. 1988.
12. Ünalmis, Ö. H., "Structure of the Supersonic Turbulent Boundary Layer and Its Influence on Unsteady Separation," Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Texas, Austin, TX, Aug. 1995.
13. Brusniak, L., "Physics of Unsteady Blunt Fin-Induced Shock Wave/Turbulent Boundary Layer Interactions," Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Texas, Austin TX, May 1994.
14. Gramann, R. A., and Dolling, D. S., "A Preliminary Study of Turbulent Structures Associated with Unsteady Separation Shock Motion in a Mach 5 Compression Ramp Interaction," AIAA Paper 92-0744, Jan. 1992.
15. Chan, S. C., Clemens, N. T., and Dolling, D. S., "Flowfield Imaging of Unsteady, Separated Compression Ramp Interactions," AIAA Paper 95-2195, June 1995.