Direct numerical simulations of roughness-induced transition in supersonic boundary layers

Journal of Fluid Mechanics

Volumn 693, Issue , 2012, Pages 28-56

  Muppidi, Suman ^a   Mahesh, Krishnan ^a  

^a UNIVERSITY OF MINNESOTA   (United States)

Author keywords

boundary layer stability; compressible boundary layers; high speed flow

Indexed keywords

ACOUSTIC STREAMING; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; DIRECT NUMERICAL SIMULATION; NUMERICAL MODELS; SHEAR FLOW; SUPERSONIC AIRCRAFT; SURFACE ROUGHNESS; TRANSPORT PROPERTIES; TURBULENCE; TURBULENT FLOW; VORTEX FLOW; WALL FLOW;

BOUNDARY LAYER STABILITIES; COMPRESSIBLE BOUNDARY LAYERS; FLAT PLATE BOUNDARY LAYERS; HIGH SPEED FLOWS; LAMINAR TO TURBULENT TRANSITIONS; SUPERSONIC BOUNDARY LAYER; TRANSITION TO TURBULENCE; TURBULENT BOUNDARY LAYERS;

LAMINAR BOUNDARY LAYER;

COMPRESSIBLE FLOW; FLOW STABILITY; LAMINAR-TURBULENT TRANSITION; NUMERICAL MODEL; SURFACE ROUGHNESS; TURBULENT BOUNDARY LAYER; VORTEX FLOW;

EID: 84858693484     PISSN: 00221120     EISSN: 14697645     Source Type: Journal    
DOI: 10.1017/jfm.2011.417     Document Type: Article

References (47)

1. ACARLAR, M. S. & SMITH, C. R. 1987 A study of hairpin vortices in a laminar boundary layer. Part 1. J. Fluid Mech. 175, 1-42.
2. BERRY, S. A., HAMILTON, H. H. II & WURSTER, K. E. 2006 Effect of computational method on discrete roughness correlations for shuttle orbiter. J. Spacecr. Rockets 43 (4), 842-852. (Pubitemid 44299739)
3. BERRY, S. A. & HORVATH, T. J. 2007 Discrete roughness transition for hypersonic flight vehicles. AIAA Paper 2007-0307.
4. BERRY, S. A., HORVATH, T. J., HOLLIS, B. R., THOMPSON, R. A. & HAMILTON, H. H. II 2001 X-33 hypersonic boundary-layer transition. J. Spacecr. Rockets 38 (5), 646-657. (Pubitemid 33046931)
5. BOOKEY, P. B., WYCKHAM, C., SMITS, A. J. & MARTIN, M. P. 2005 New experimental data of STBLI at DNS/LES accessible Reynolds numbers. AIAA Paper 2005-309.
6. CHOUDHARI, M. & FISCHER, P. 2005 Roughness-induced transient growth AIAA Paper 2005-4765.
7. CHOUDHARI, M., LI, F., WU, M., CHANG, C. L., EDWARDS, J., KEGERISE, M. & KING, R. 2010 Laminar-turbulent transition behind discrete roughness elements in a high-speed boundary layer. AIAA Paper 2010-1575.
8. CORKE, T. C., BAR-SEVER, A. & MORKOVIN, M. V. 1986 Experiments on transition enhancement by distributed roughness. Phys. Fluids 29 (10), 3199-3213.
9. EKOTO, I. W., BOWERSOX, R. D. W., BEUTNER, T. & GOSS, L. 2008 Supersonic boundary layers with periodic surface roughness. AIAA. J. 46 (2), 486-497. (Pubitemid 351683014)
10. ELENA, M., LACHARME, J. & GAVIGLIO, J. 1985 Comparison of hot-wire and laser Doppler anemometry methods in supersonic turbulent boundary layers. In Proceedings of the International Symposium on Laser Anemometry. (ed. A. Dybb & P. A. Pfund). ASME.
11. ERGIN, F. G. & WHITE, E. B. 2006 Unsteady and transitional flows behind roughness elements. AIAA J. 44 (11), 2504-2514. (Pubitemid 44788045)
12. FEDEROV, A. 2010 Transition and stability of high-speed boundary layers. Annu. Rev. Fluid Mech. 43, 79-95.
13. GATSKI, T. B. & ERLEBACHER, G. 2002 Numerical simulation of a spatially evolving supersonic turbulent boundary layer. NASA Tech. Memo. 211934.
14. GUARINI, S. E., MOSER, R. D., SHARIFF, K. & WRAY, A. 2000 Direct numerical simulation of a supersonic turbulent boundary layer at Mach 2.5. J. Fluid. Mech. 414, 1-33.
15. JIMENEZ, J. 2004 Turbulent flows over rough walls. Annu. Rev. Fluid Mech. 36, 173-196. (Pubitemid 38381909)
16. KLEBANOFF, P. 1955 Characteristics of turbulence in a boundary layer with zero pressure gradient. NASA Rep. 1247.
17. KLEBANOFF, P. S. & TIDSTROM, K. D. 1972 Mechanism by which a two-dimensional roughness element induces boundary-layer transition. Phys. Fluids 15 (7), 1173-1188.
18. LOGINOV, M. S., ADAMS, N. A. & ZHELTOVODOV, A. A. 2006 Large-eddy simulation of shock-wave/turbulent-boundary-layer interaction. J. Fluid. Mech. 565, 135-169. (Pubitemid 44489600)
19. MASON, P. J. & MORTON, B. R. 1987 Trailing vortices in the wakes of surface-mounted obstacles. J. Fluid Mech. 175, 247-293. (Pubitemid 17532292)
20. MORKOVIN, M. V., RESHOTKO, E. & HERBERT, T. 1994 Transition in open flow systems: a reassessment. Bull. Am. Phys. Soc. 39, 1-31.
21. PARK, N. & MAHESH, K. 2007 Numerical and modelling issues in LES of compressible turbulent flows on unstructured grids. AIAA Paper 2007-722.
22. REDA, D. C 2002 Review and synthesis of roughness-dominated transition correlations for reentry applications. J. Spacecr. Rockets 39 (2), 161-167.
23. REDFORD, J. A., SANDHAM, N. D. & ROBERTS, G. T. 2010 Roughness-induced transition of compressible laminar boundary layers. In Proceedings of the Seventh IUTAM Symposium on Laminar-Turbulent Transition, Stockholm, Sweden, 2009. (ed. P. Schlatter & D. S. Henningson). Seventh IUTAM Symposium on Laminar-Turbulent Transition, IUTAM Bookseries 18, pp. 337-342. Springer Science+ Business Media B.V.
24. RESHOTKO, E. 1976 Boundary-layer stability and transition. Annu. Rev. Fluid Mech. 8, 311-349.
25. RESHOTKO, E. 2001 Transient growth: a factor in bypass transition. Phys. Fluids 13 (5), 1067-1075. (Pubitemid 32449567)
26. RESHOTKO, E. 2007 Is Re =Me a meaningful transition criterion? AIAA Paper 2007-943.
27. RESHOTKO, E. 2008 Roughness-induced transition. Transient growth in 3-D and supersonic flow. In RTO-AVT/VKI Lectures Series, Advances in Laminar-Turbulent Transition Modelling VKI, Brussels, Belgium, June 2008.
28. RESHOTKO, E. & TUMIN, A. 2004 Role of transient growth in roughness-induced transition. AIAA J. 42 (4), 766-770.
29. RINGUETTE, M. J., BOOKEY, P. B., WYCKHAM, W. & SMITS, A. J. 2009 Experimental study of a Mach 3 compression ramp interaction at Re D 2400. AIAA J. 47, 373-385.
30. ROBERTS, S. K. & YARAS, M. I. 2005 Boundary-layer transition affected by surface roughness and free-stream turbulence. Trans. ASME: J. Fluids Engng 127, 449-457. (Pubitemid 41048154)
31. SAHOO, D., PAPAGEORGE, M. & SMITS, A. J. 2010 PIV experiments on a rough-wall hypersonic turbulent boundary layer. AIAA Paper 2010-4471.
32. SARIC, W. S., REED, H. L. & WHITE, E. B. 2003 Stability and transition of three-dimensional boundary layers. Annu. Rev. Fluid Mech. 35, 413-440. (Pubitemid 37515241)
33. SCHLICHTING, H. T. 1963 Boundary Layer Theory. McGraw-Hill.
34. SCHNEIDER, S. P. 2008 Summary of hypersonic boundary-layer transition experiments on blunt bodies with roughness. J. Spacecr. Rockets 45 (6), 1090-1105.
35. SPALART, P. R. 1998 Direct simulation of a turbulent boundary layer up to Re D 1410. J. Fluid Mech. 187, 61-98.
36. STETSON, K. F. 1990 Comments on hypersonic boundary-layer transition. Wright Research and Development Center, WRDC-TR-90-3057.
37. TANI, I. 1969 Boundary layer transition. Annu. Rev. Fluid Mech. 1, 169-196.
38. TUMIN, A. & RESHOTKO, E. 2003 Optimal disturbances in compressible boundary layers. AIAA J. 41 (12), 2357-2363.
39. TUMIN, A. & RESHOTKO, E. 2004 The problem of boundary-layer flow encountering a three-dimensional hump revisited. AIAA Paper 2004-101.
40. VAN DRIEST, E. R. & BLUMER, C. B. 1962 Boundary layer transition at supersonic speeds - three dimensional roughness effects (spheres). J. Aerosp. Sci. 29, 909-916.
41. VAN DRIEST, E. R. & MCCAULEY, W. D. 1960 Measurements of the effect of two-dimensional and three-dimensional roughness elements on boundary layer transition. J. Aero. Sci. 27, 261-271.
42. WANG, X. & ZHONG, X. 2008 Receptivity of a hypersonic flat-plate boundary layer to three-dimensional surface roughness. Journal of Spacecr. Rockets 45 (6), 1165-1175.
43. WHITE, E. B. 2002 Transient growth of stationary disturbances in a flat plate boundary layer. Phys. Fluids 14 (12), 4429-4439. (Pubitemid 36111380)
44. WU, M. & MARTIN, M. P. 2007 Direct numerical simulation of supersonic turbulent boundary layer over a compression ramp. AIAA J. 45, 879-889. (Pubitemid 46643602)
45. WU, X. & MOIN, P. 2009 Direct numerical simulation of turbulence in a nominally zero-pressuregradient flat-plate boundary layer. J. Fluid Mech. 632, 5-41.
46. ZHELTOVODOV, A. A., TROFIMOV, V. M., SCHULEIN, E. & YAKOVLEV, V. N. 1990 An experimental documentation of supersonic turbulent flows in the vicinity of forward- and backward-facing ramps. Tech. Rep. 2030. Institute of Theoretical and Applied Mechanics, USSR Academy of Sciences, Novosibirsk.
47. ZHOU, J., ADRIAN, R. J., BALACHANDAR, S. & KENDALL, T. M. 1999 Mechanisms for generating coherent packets of hairpin vortices in channel flow. J. Fluid Mech. 387, 353-396.