Decay of fluctuating wall-pressure field of Mach 5 turbulent boundary layer

AIAA journal

Volumn 37, Issue 9, 1999, Pages 1088-1096

  Ünalmis, Ö H ^a   Dolling, D S ^a  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CORRELATION METHODS; PRESSURE MEASUREMENT; TURBULENT FLOW; WIND TUNNELS;

MACH NUMBER; STROUHAL NUMBER;

BOUNDARY LAYER FLOW;

EID: 0033197440     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.837     Document Type: Article

References (28)

1. Chyu, W. J., and Hanly, R. D., "Power and Cross-Spectra and Space-Time Correlations of Surface Fluctuating Pressures at Mach Numbers between 1.6 and 2.5," AIAA Paper 68-77, Jan. 1968.
2. Owen, F. K., and Horstman, C. C., "On the Structure of Hypersonic Turbulent Boundary Layers," Journal of Fluid Mechanics, Vol. 53, Pt. 4, 1972, pp. 611-636.
3. Owen, F. K., Horstman, C. C., and Kussoy, M. I., "Mean and Fluctuating Flow Measurements of a Fully-Developed, Non-Adiabatic, Hypersonic Boundary Layer," Journal of Fluid Mechanics, Vol. 70, Pt. 2, 1975, pp. 393-413.
4. Smits, A. J., Spina, E. F., Alving, A. E., Smith, R. W., Fernando, E. M., and Donovan, J. F., "A Comparison of the Turbulence Structure of Subsonic and Supersonic Boundary Layers," Physics of Fluids A, Vol. 1, No. 11, 1989, pp. 1865-1875.
5. Spina, E. P., Smits, A. J., and Robinson, S. K., "The Physics of Supersonic Turbulent Boundary Layers," Annual Review of Fluid Mechanics, Vol. 26, 1994, pp. 287-319.
6. 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.
7. Settles, G. S., "An Experimental Study of Compressible Turbulent Boundary Layer Separation at High Reynolds Numbers," Ph.D. Dissertation, Dept. of Mechanical and Aerospace Engineering, Princeton Univ., Princeton, NJ, Sept. 1975.
8. Sun, C. C., and Childs, M. E., "A Modified Wall-Wake Velocity Profile for Turbulent Compressible Boundary Layers," Journal of Aircraft, Vol. 10, No. 6, 1973, pp. 381-383.
9. 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.
10. Alving, A. E., "Boundary Layer Relaxation from Convex Curvature," Ph.D. Dissertation, Dept. of Mechanical and Aerospace Engineering, Princeton Univ., Princeton, NJ, June 1988.
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. Robinson, S. K., "Space-Time Correlation Measurements in a Compressible Turbulent Boundary Layer," AIAA Paper 86-1130, May 1986.
13. Tran, T. T., "An Experimental Investigation of Unsteadiness in Swept Shock Wave/Turbulent Boundary Layer Interactions," Ph.D. Dissertation, Mechanical and Aerospace Engineering Dept., Princeton Univ., Princeton, NJ, March 1987.
14. Bull, M. K., "Wall-Pressure Fluctuations Associated with Subsonic Turbulent Boundary Layer Flow," Journal of Fluid Mechanics, Vol. 28, Pt. 4, 1967, pp. 719-754.
15. 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.
16. Ünalmis, Ö. H., and Dolling, D. S., "On the Possible Relationship Between Low Frequency Unsteadiness of Shock-Induced Separated Flow and Görtler Vortices," AIAA Paper 96-2002, June 1996.
17. Ünalmis, Ö. H., and Dolling, D. S., "Experimental Study of Causes of Unsteadiness of Shock-Induced Turbulent Separation," AIAA Journal, Vol. 36, No. 3, 1998, pp. 371-378.
18. Dolling, D. S., and Dussauge, J. P., "Fluctuating Wall-Pressure Measurements," A Survey of Measurements and Measuring Techniques in Rapidly Distorted Compressible Turbulent Boundary Layers, AGARDograph 315, AGARD, Nov. 1988, Chap. 8.
19. Schewe, G., "On the Structure and Resolution of Wall Pressure Fluctuations Associated with Turbulent Boundary Layer Flow," Journal of Fluid Mechanics, Vol. 134, 1983, pp. 311-328.
20. Kistler, A. L., and Chen, W. S., "The Fluctuating Pressure Field in a Supersonic Turbulent Boundary Layer," Jet Propulsion Lab., JPL-TR-32-277, California Inst. of Technology, Pasadena, CA, Aug. 1962.
21. Maestrello, L., "Radiation from and Panel Response to a Supersonic Turbulent Boundary Layer," Boeing Scientific Research Labs., D1-82-0719, Seattle, WA, Sept. 1968.
22. Speaker, W. V., and Ailman, C. M., "Spectra and Space-Time Correlations of the Fluctuating Pressures at a Wall Beneath a Supersonic Turbulent Boundary Layer Perturbed by Steps and Shock Waves," NASA CR-486, May 1966.
23. Debieve, J. F., "Etude d'une Interaction Turbulence - Onde de Choc," Ph.D. Dissertation, Institut de Mecanique Statistique de la Turbulence, Univ. Aix-Marseille II, Marseille, France, June 1983.
24. Tan, D. K. M., Tran, T. T., and Bogdonoff, S. M., "Surface Pressure Fluctuations in a Three Dimensional Shock Wave/Turbulent Boundary Layer Interaction," AIAA Paper 85-0125, Jan. 1985.
25. Muck, K. C., Dussauge, J. P., and Bogdonoff, S. M., "Structure of the Wall Pressure Fluctuations in a Shock-Induced Separated Flow," AIAA Paper 85-0179, Jan. 1985.
26. Dussauge, J. P., "The Relaxation of a 'Relaminarized' Turbulent Boundary Layer in Supersonic Flow," Proceedings of the 5th Turbulent Shear Flow Symposium, A86-30201 13-34, Cornell Univ., Ithaca, NY, 1985.
27. Bonnet, J. P., "Space-Time Correlations of Wall Pressure Fluctuations in Shock-Induced Separated Turbulent Flows," Physics of Fluids, Vol. 31, No. 10, 1988, pp. 2821-2833.
28. Willmarth, W. W., and Wooldridge, C. E., "Measurements of the Fluctuating Pressure at the Wall Beneath a Thick Boundary Layer," Journal of Fluid Mechanics, Vol. 14, Pt. 2, 1962, pp. 187-210.