A simple model for low-frequency unsteadiness in shock-induced separation

Journal of Fluid Mechanics

Volumn 629, Issue , 2009, Pages 87-108

  Piponniau, S ^a   Dussauge, J P ^a   Debieve J F ^a   Dupont, Pierre ^a  

^a AIX MARSEILLE UNIVERSITÉ   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; SHOCK WAVES; VELOCITY MEASUREMENT;

AERODYNAMIC PARAMETERS; BOUNDARY LAYER INTERACTION; FLUID ENTRAINMENT; LOW-FREQUENCY MOTION; OBLIQUE SHOCK WAVES; PARTICLE IMAGE VELOCIMETRIES; SHOCK INDUCED SEPARATION; SIMPLE MODELING;

FLOW SEPARATION;

AERODYNAMICS; AIR BUBBLE; CONTRACTION; ENTRAINMENT; EXPERIMENTAL STUDY; FLUID FLOW; NUMERICAL MODEL; PARAMETERIZATION; SEPARATION; TURBULENT BOUNDARY LAYER; UNSTEADY FLOW;

EID: 67650888935     PISSN: 00221120     EISSN: 14697645     Source Type: Journal    
DOI: 10.1017/S0022112009006417     Document Type: Article

References (39)

1. ADRIAN, R. J., MEINHART, C. D. S. & TOMKINS, C. D. 2000 Vortex organization in the outer region of the turbulent boundary layer. J. Fluid Mech. 422, 1-53.
2. BERESH, S. J., CLEMENS, N. T. & DOLLING, D. S. 2002 Relationship between upstream turbulent boundary layer velocity fluctuations and separation shock unsteadiness. AIAA J. 40 (12), 2412-2422.
3. BROWAND, F. K. & TROUTT, T. R. 1985 The turbulent mixing layer: geometry of large vortices. J. Fluid Mech. 158, 489-509.
4. BROWN, G. L. & ROSHKO, A. 1974 On density effects and large structures in turbulent mixing layers. J. Fluid Mech. 64, 775-781.
5. CHERRY, N. J., HILLIER, R. & LATOUR, M. E. M. 1984 Unsteady measurements in a separated and reattaching flow. J. Fluid Mech. 144, 13-46.
6. DANDOIS, J., GARNIER, E. & SAGAUT, P. 2007 Numerical simulation of active separation control by synthetic jet. J. Fluid. Mech. 574 25-58.
7. DEBIÈVE, J. F. & DUPONT, P. 2007 Dependence between shock and separation bubble in a shock wave/boundary layer interaction. In IUTAM Symp. on Unsteady Separated Flows and Their Control, Corfu, Greece.
8. DEBIÈVE, J. F. & LACHARME, J. P. 1985 A shock wave/free turbulence interaction. In IUTAM Symp. on Turbulent Shear-Layer/ Shock-Wave Interaction, Palaiseau, France.
9. DELERY, J. & MARVIN, J. G. 1986 Shock wave-boundary layer interactions. Tech Rep. NATO. AGARDOgraph n°280.
10. DOLLING, D. S. 2001 Fifty years of shock-wave/boundary-layer interaction research: What next? AIAA J. 39 (8), 1517-1531.
11. DOLLING, D. S. & BRUSNIAK, L. 1989 Separation shock motion in fin, cylinder, and compression ramp-induced turbulent interactions. AIAA J. 27 (6), 734-742.
12. DUPONT, P., HADDAD, C., ARDISSONE, J. P. & DEBIÈVE, J. F. 2005 Space and time organisation of a shock wave/turbulent boundary layer interaction. Aerosp. Sci. Technol. 9 (7), 561-572.
13. DUPONT, P., HADDAD, C. & DEBIÈVE, J. F. 2006 Space and time organization in a shock induced boundary layer. J. Fluid Mech. 559, 255-277.
14. DUPONT, P., PIPONNIAU, S., SIDORENKO, A. & DEBIÈVE, J. F. 2008 Investigation of an oblique shock reflection with separation by PIV measurements. AIAA J. 46 (6).
15. DUSSAUGE, J. P., DUPONT, P. & DEBIÈVE, J. F. 2006 Unsteadiness in shock wave boundary layer interaction with separation. Aeros. Sci. Technol. 10, 85-91.
16. ELENA, M., TEDESCHI, G. & GOUIN, H. 1999 Motion of tracer particles in supersonic flows. Exp. Fluids 26 (4), 288-296.
17. ERENGIL, M. E. & DOLLING, D. S. 1991a Correlation of separation shock motion with pressure fluctuations in the incoming boundary layer. AIAA J. 29 (11), 1868-1877.
18. ERENGIL, M. E. & DOLLING, D. S. 1991b Unsteady wave structure near separation in a Mach 5 compression ramp interaction. AIAA J. 29 (5), 728-735.
19. GANAPATHISUBRAMANI, B., CLEMENS, N. T. & DOLLING, D. S. 2006 Large-scale motions in a supersonic turbulent boundary layer. J. Fluid Mech. 556, 271-282.
20. GANAPATHISUBRAMANI, B., CLEMENS, N. T. & DOLLING, D. S. 2007a Effects of upstream boundary layer on the unsteadiness of shock-induced separation. J. Fluid Mech. 585, 369-394.
21. GANAPATHISUBRAMANI, B., CLEMENS, N. T. & DOLLING, D. S. 2007b Effects of upstream coherent structures on low-frequency motion of shock-induced turbulent separation. In 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada.
22. GARNIER, E. & SAGAUT, P. 2002 Large eddy simulation of shock/ boundary layer interaction. AIAA J. 40 (10), 1935-1944.
23. HUMBLE, R. A., ELSINGA, G. E., SCARANO, F. & VAN OUDHEUSDEN, B. W. 2007 Investigation of the instantaneous 3D flow organization of a shock-wave/turbulent boundary layer interaction using tomographic PIV. Paper 2007-4112. AIAA.
24. KIM, K. C. & ADRIAN, R. J. 1999 Very large-scale motion in the outer layer. Phys. Fluids 11, 417-422.
25. KIYA, M. & SASMU, K. 1983 Structure of a turbulent separation bubble. J. Fluid Mech. 137, 83-113.
26. DE MARTEL, E., GARNIER, E. & SAGAUT, P. 2007 Large eddy simulation of impinging shock wave/turbulent boundary layer interaction at M = 2.3. In IUTAM Symp. on Unsteady Separated Flows and their Control Corfu, Greece.
27. PAPAMOSCHOU, D. & ROSHKO, A. 1988 The compressible turbulent shear layer: An experimental study. J. Fluid Mech. 197, 453-477.
28. PIROZZPLI, S. & GRASSO, F. 2006 Direct numerical simulation of impinging shock wave/turbulent boundary layer interaction at M = 2.25. Phys. Fluids 18, 065113. 1-17.
29. RINGUETTE, M. J. & SMITS, A. J. 2007 Wall-pressure measurements in a Mach 3 shock-wave turbulent boundary layer interaction at a DNS-accessible Reynolds number. In 37th AIAA Fluid Dynamics Conf. and Exhibit, Miami, Florida.
30. RINGUETTE, M. J., WU, M. & MARTIN, M. P. 2008 Coherent structures in direct numerical simulation of turbulent boundary layers at Mach 3. J. Fluid Mech. 594, 59-69.
31. SAMIMY, M. & LELE, S. K. 1991 Motion of particles with inertia in a compressible free shear layer. Phys. Fluids A 3, 1915-1923.
32. SIMPSON, R. L. 1989 Turbulent boundary-layer separation. Annu. Rev. Fluid Mech. 21, 205-234.
33. SMITS, A. J. & DUSSAUGE, J. P. 2006 Turbulent Shear Layers in Supersonic Flow, 2nd edn. AIP Press.
34. SOUVEREIN, L., VAN OUDHEUSDEN, B. W., SCARANO, F. & DUPONT, P. 2008 Unsteadiness characterisation in a shock wave turbulent boundary layer interaction through dual-PIV. In 38th Fluid Dynamics Conf. and Exhibit, Seattle, Washington.
35. THOMAS, F. O., PUTMAN, C. M. & CHU, H. C. 1994 On the mechanism of unsteady shock oscillation in shock wave/turbulent boundary layer interaction. Exp. Fluids 18, 69-81.
36. TOUBER, E. & SANDHAM, N. D. 2008 Oblique shock impinging on a turbulent boundary layer: Low-frequency mechanisms. In 38th AIAA Fluid Dynamics Conf., Seattle, Washington.
37. WU, M. & MARTIN, M. P. 2007 Direct numerical simulation of supersonic turbulent boundary layer over a compression ramp. AIAA J. 45 (4), 879-889.
38. WU, M. & MARTIN, M. P. 2008 Analysis of shock motion in shock wave and turbulent boundary layer interaction using direct numerical simulation data. J. Fluid Mech. 594, 71-83.
39. WU, M. & MILES, R. B. 2001 Megahertz visualization of compression-corner shock structures. AIAA J. 39 (8), 1542-1546.