Experimental studies of stability and transition in high-speed wakes

Journal of Fluid Mechanics

Volumn 392, Issue , 1999, Pages 1-26

  Lysenko, V I ^a  

^a KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW INTERACTIONS; LAMINAR FLOW; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS; TRANSITION FLOW; TURBULENT FLOW;

MACH NUMBER; SUPERSONIC WAKE; WAKE STABILITY;

WAKES;

EID: 0032631233     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112099004723     Document Type: Article

References (52)

1. BAGAEV, G. I., LEBIGA, V. A., PRIDANOV, V. G. & CHERNYH, V.V. 1972 A supersonic wind tunnel T-325 with low-degree turbulence. In Aerodynamic Researches, pp. 11-13. Novosibirsk (in Russian).
2. BEHRENS, W. 1968 Far wake behind cylinders at hypersonic speeds: II. Stability. AIAA J. 6, 225-232.
3. BEHRENS, W. & KO, D. R. S. 1971 Experimental stability studies in wakes of two-dimensional slender bodies at hypersonic speeds. AIAA J. 9, 851-857.
4. BEHRENS, W., LEWIS, J. E. & WEBB, W. H. 1971 Transition and turbulence phenomena in supersonic wakes of wedges. AIAA J. 9, 2083-2084.
5. CHEN, J. H., CANTWELL, B. J. & MANSOUR, N. N. 1990 The effect of Mach number on the stability of a plane supersonic wake. Phys. Fluids A 2, 984-1004.
6. DEMETRIADES, A. 1960 An experiment on the stability of hypersonic laminar boundary layers. J. Fluid Mech. 7, 385-396.
7. DEMETRIADES, A. 1964 Hot-wire measurements in the hypersonic wakes of slender bodies. AIAA J. 2, 245-250.
8. DEMETRIADES, A. 1978 Transition in two-dimensional wakes. AIAA J. 16, 587-591.
9. DEMETRIADES, A. 1990 Experiments on the free shear layer between two supersonic streams. AIAA Paper 90-710, 8p.
10. GERTSENSTEIN, S. YA. & KOSHKO, A. V. 1972 Stability of axis-symmetrical compressible in viscid wake. In Aerodynamics of Large Speeds, pp. 142-150. Moscow: Institute of the Mechanics of Moscow University (in Russian).
11. HEGDE, U. G. & ZINN, B. T. 1991 Vortical mode instability of shear layer with temperature and density gradients. AIAA J. 28, 1389-1396.
12. JACKSON, T. L. & GROSCH, C. E. 1988 Inviscid spatial stability of a compressible mixing layer. NASA-CR-181671; ICASE Rep. 2.
13. JACKSON, T. L. & GROSCH, C. E. 1989 Inviscid spatial stability of a compressible mixing layer. J. Fluid Mech. 208, 609-637.
14. JACKSON, T. L. & GROSCH, C. E. 1990a Absolute/convective instabilities and the convective Mach number in a compressible mixing layer. Phys. Fluids A 2, 949-954.
15. JACKSON, T. L. & GROSCH, C. E. 1990b Inviscid spatial stability of a compressible mixing layer. Part 2. The flame sheet model. J. Fluid Mech. 217, 391-420.
16. JACKSON, T. L. & GROSCH, C. E. 1991 Inviscid spatial stability of a compressible mixing layer. Part 3. Effect of thermodynamics. J. Fluid Mech. 224, 159-175.
17. KENDALL, J. M. 1967 Supersonic boundary layer stability experiments. Aerospace Rep. TR-0158(S3816-63)-1, vol. 2.
18. KIM, S. 1990 A new mixing length model for supersonic shear layers. AIAA Paper 90-18, 6p.
19. KOSINOV, A. D. & MASLOV, A. A. 1984 The development of the artificially caused disturbances in the supersonic boundary layer. Izv. Akad. Nauk SSSR, Mekh. Zhid. Gaza no. 5, 37-43 (in Russian).
20. KOSINOV, A. D., MASLOV, A. A., SEMIONOV, N. V. & SHEVELKOV, S. G. 1990a Wave structure of artificial disturbances in the supersonic boundary layer on a plate . Zh. Prikl. Mekh. Tekh. Fiz. no.2, 95-98 (in Russian).
21. KOSINOV, A. D., MASLOV, A. A. & SHEVELKOV, S. G. 1986 An experimental research on wave structure of the supersonic boundary layer (in Russian). Zh. Prikl. Mekh. Tekh. Fiz. no. 5, 107-112.
22. KOSINOV, A. D., MASLOV, A. A. & SHEVELKOV, S. G. 1989 Stability of a supersonic boundary layer after a fan of waves of rarity. Zh. Prikl. Mekh. Tekh. Fiz. no. 3, 113-117 (in Russian).
23. KOSINOV, A. D., MASLOV, A. A. & SHEVELKOV, S. G. 1990b Experiments on the stability of supersonic laminar boundary layers. J.Fluid Mech. 219, 621-633.
24. KOSINOV, A. D., MASLOV, A. A. & SHEVELKOV, S. G. 1990c An experimental research on development of harmonic disturbances in the boundary layer of a flat plate at Mach number M = 4. Izv. Akad. Nauk SSSR, Mekh. Zhid. Gaza no. 6, 54-58 (in Russian).
25. KOSINOV, A. D., SEMIONOV, N. V. & SHEVELKOV, S. G. 1994 Investigation of supersonic boundary layer stability and transition using controlled disturbances. In Methods of Aerophysical Research, Proc. 7th Intl Conference, Novosibirsk, vol. 2, pp. 159-166.
26. KOVENYA, V. M. & LEBEDEV, A. S. 1989 Numerical modeling of viscous separated flow in a near wake. Zh. Prikl. Mekh. Tekh. Fiz. no. 5, 53-59 (in Russian).
27. KUDRYAVTSEV, A. N. & SOLOVYOV, A. S. 1989 Stability of a shear layer of compressible gas. Zh. Prikl. Mekh. Tekh. Fiz. no. 6, 119-127 (in Russian).
28. KUDRYAVTSEV, A. N. & SOLOVYOV, A. S. 1991 Stability of a viscous compressible shear layer with temperature leap. Zh. Prikl. Mekh. Tekh. Fiz. no. 4, 88-95 (in Russian).
29. LAUFER, J. & VREBALOVICH, T. 1960 Stability and transition of a supersonic laminar boundary layer on an insulated flat plate. J. Fluid Mech. 9, 257-299.
30. LEES, L. 1964 Hypersonic wakes and trails. AIAA J. 2, 417-428.
31. LEES, L. & GOLD, H. 1964 Stability of laminar boundary layers and wakes at hypersonic speeds. Part 1. Stability of laminar wakes. In Fundamental Phenomena in Hypersonic Flow, no. 4, pp. 310-337. Cornell University Press.
32. LEGNER, H. H. & FINSON, M. I. 1977 Mach number dependence of laminar near-wake transition for slender cones. AIAA J. 15, 417-419.
33. LYKOUDIS, P. S. 1966 A review of hypersonic wake studies. AIAA J. 4, 577.
34. LYSENKO, V. I. 1993 High-speed boundary-layer stability and transition. Intl J. Mech. Sci. 35, 921-933.
35. LYSENKO, V. I., KOSINOV, A. D. & YERMOLAEV, YU. G. 1998 Development of artificial disturbances in the boundary layer on a plate and in the wake behind it at supersonic free-flow speed. In Proc. Third Intl Conf. on Fluid Mechanics, Beijing, pp. 201-206. Beijing Institute of Technology Press.
36. LYSENKO, V. I. & MASLOV, A. A. 1984 The effect of cooling on supersonic boundary-layer stability. J. Fluid Mech. 147, 39-52.
37. MACARAEG, M. G. & STREETT, C. L. 1989 New instability modes for bounded, free shear flows. Phys. Fluids A 1, 1305-1307.
38. MACK, L. M. 1965 The stability of the compressible laminar boundary layer according to a direct numerical solution. In Recent Developments in Boundary Layer Research, Part 1, AGARDograph 97, pp. 329-362.
39. MARTENS, S., KINZIE, K. W. & MCLAUGHLIN, D. K. 1994 Measurements of Kelvin-Helmholtz instabilities in a supersonic shear layer. AIAA J. 32, 1633-1639.
40. MCLAUGHLIN, D. K. 1971 Experimental investigation of the stability of the laminar supersonic cone wake. AIAA J. 9, 696-702.
41. MCLAUGHLIN, D. K., CARTER, J. E., FINSTON, M. & FORNEY, A. 1971 Experimental investigation of the mean flow of the laminar supersonic cone wake. AIAA J. 9, 479-484.
42. MCLAUGHLIN, D. K., MORRISON, G. L. & TROUTT, T. R. 1975 Experiments on the instability waves in a supersonic jet and their acoustic radiation. J. Fluid Mech. 69, 73-95.
43. MIHALEV, A. N. 1980 About influence of Reynolds number on the parameters of a near wake behind supersonic cones. In Physical-Gasdynamical Ballistic Researches, pp. 88-98. Nauka, Leningrad (in Russian).
44. PALLONE, A. J., ERDOS, J. & ECKERMAN, J. 1964 Hypersonic laminar wakes and transition studies. AIAA J. 2, 855-863.
45. PAPAGEORGIOU, D. T. 1991 The stability of two-dimensional wakes and shear layers at high Mach numbers. Phys. Fluids A 3, 793-802.
46. RAGAB, S. A. & WU, J. L. 1989a Linear instability waves in supersonic turbulent mixing layers. AIAA J. 27, 677-686.
47. RAGAB, S. A. & WU, J. L. 1989b Linear instabilities in two-dimensional compressible mixing layers. Phys. Fluids A 1 957-966.
48. REEVES, B. L. & LEES, L. 1965 Theory of laminar near wake of blunt bodies in hypersonic flow. AIAA J. 3, 2061.
49. ROSHKO, A. & FISHDON, U. 1969 About role of transition in a near wake. Mechanics, no. 6.
50. TROUTT, T. R. & MCLAUGHLIN, D. K. 1982 Experiments on the flow and acoustic properties of a moderate-Reynolds-number supersonic jet. J. Fluid Mech. 116, 123-156.
51. WEN, K.-S. 1964 Wake transition. AIAA J. 2, no. 5, 956.
52. ZHUANG, M., KUBOTA, T. & DIMOTAKIS, P. E. 1990 Instability of inviscid, compessible free shear layers. AIAA J. 28, 1728-1733.