Experimental research on stability and transition in high-speed wakes Part 1. Research on the transition position in supersonic and hypersonic wakes, and the effects of temperature and other factors

Lysenko, V. I.

Artykuł - szczegóły

Tytuł artykułu

Experimental research on stability and transition in high-speed wakes Part 1. Research on the transition position in supersonic and hypersonic wakes, and the effects of temperature and other factors

Autorzy

Lysenko V. I.

Wybrane pełne teksty z tego czasopisma

http://et.ippt.gov.pl/

Identyfikatory

Warianty tytułu

Języki publikacji

Abstrakty

The development of disturbances in a supersonic wake (free viscous layer and regular wake) behind a flat plate, both in linear and in nonlinear phases of development was investigated. The influence of several factors (Mach and Reynolds numbers, temperature factor, thickness of a plate, length of its Stern) on the wake stability was studied.

Słowa kluczowe

supersonic wake stability transition experimental research

strumień naddźwiękowy stabilność przemiany badania doświadczalne

Wydawca

Instytut Podstawowych Problemów Techniki PAN

Czasopismo

Engineering Transactions

Rocznik

1998

Tom

Vol. 46, iss.3/4

Strony

243--250

Opis fizyczny

Bibliogr. 42 poz., rys.

Twórcy

autor

Lysenko V. I.

Russian Academy of Sciences, Institute of Theoretical and Applied Mechanics, gaponov@itam.nsc.ru

Bibliografia

1. A.N. MIHALRV, Influence of Reynolds number on the parameters of a near - make behind supersonic cones [in Russian], [in:] Physical-Gasdynamical Ballistic Researches, Nauka, Leningrad 1980, 88-98.
2. V.M. KOVENYA, A.S. LEBEDEV, Numerical modeling of viscous separated flow in a near -wake [in Russian], Zh. Prikl. Mekh. Tekh. Fiz., 5, 53-59, 1989.
3. V.I. LYSENKO, High-speed boundary-layer stability and transition, Int. J. Mech. Sci., 35, 11, 921-933, 1993.
4. V.I. LYSENKO, A.A. MASLOV, 77ie effect of cooling on supersonic boundary-layer stability, J. Fluid Mech., 147, 39-52, 1984.
5. W. BEHRENS, For make behind cylinders at hypersonic speeds: II. Stability, AIAA J., 6, 2, 225-232, 1968.
6. W. BEHRENS, D.R.S. KO, Experimental stability studies in wakes of two-dimensional slender bodies at hypersonic speeds, AIAA J., 9, 5, 851-857, 1971.
7. W. BEHRENS, J.E. LEWIS, W.H. WEBB, Transition and turbulence phenomena in supersonic wakes of wedges, AIAA J., 9, 10, 2083-2084, 1971.
8. A. DEMETRIADES, Hot-wire measurements in the hypersonic wakes of slender bodies, AIAA J., 2, 2, 245-250, 1964.
9. A. DEMETRIADES, Transition in two-dimensional wakes, AIAA J., 16, 6, 587-591, 1978.
10. A. DEMETRIADES, Experiments on the free shear layer between two supersonic streams, AIAA Paper, 710, 8p., 1990.
11. D.K. MCLAUGHLIN, Experimental investigation of the stability of the laminar supersonic cone wake, AIAA J., 9, 4, 696-702, 1971.
12. D.K. MCLAUGHLIN, J.E CARTER, M. FINSTON, A. FORNEY, Experimental investigation of the mean flow of the laminar supersonic cone wake, AIAA J., 9, 3, 479-484, 1971.
13. J. LAUFER, T. VREBALOVICH, Stability and transition of a supersonic laminar boundary layer on an insulated fiat plate, J.Fluid Mech., 9, pt.2, 257-299, 1960.
14. A. DEMETRIADES, An experiment on the stability of hypersonic laminar boundary layers, J. Fluid Mech., 7, 385-396, 1960.
15. J.M. KENDALL, Supersonic boundary layer stability experiments, Aerospace Rep.TR-0158 (S3816-63)-!, 2, 1967.
16. A.D. KOSINOV, A.A. MASLOV, The development of the artificially caused disturbances in the supersonic boundary layer [in Russian], Izv. Akad. Nauk SSSR, Mekh. Zhid. Gaza, 5, 37-43, 1984.
17. A.D. KOSINOV, A.A. MASLOV, S.G. SHEVELKOV, An experimental research of wave structure of the supersonic boundary layer [in Russian] Zh.Prikl.Mekh.Tekh.Fiz., 5, 107-112, 1986.
18. A.D. KOSINOV, A.A. MASLOV, S.G. SHEVELKOV, Stability of a supersonic boundary layer after a fan of waves of rarefaction [in Russian], Zh. Prikl. Mekh. Tekh. Fiz., 3, 113-117, 1989.
19. A.D. KOSINOV, A.A. MASLOV, N.V. SEMIONOV, S.G. SHEVELKOV, Wave structure of artificial disturbances in the supersonic boundary layer on a plate [in Russian], Zh. Prikl. Mekh. Tekh. Fiz., 2, 95-98, 1990.
20. A.D. KOSINOV, A.A. MASLOV, S.G. SHEVELKOV, Experiments on the stability of supersonic laminar boundary layers, J.Fluid Mech., 219, 621-633, 1990.
21. A.D. KOSINOV, N.V. SEMIONOV, S.G. SHEVELKOVG, Investigation of supersonic boundary layer stability and transition using controlled disturbances, [in:] Methods of Aerophysical Research, Proc. 7-th Intern. Conference, 2, 159-166, Novosibirsk 1994.
22. T.R. TROUTT, D.K. MCLAUGHLIN, Experiments on the flow and acoustic properties of a moderate Reynolds-number supersonic jet, J.Fluid Mech., 116, 123-156, 1982.
23. D.K. MCLAUGHLIN, G.L. MORRISON, T.R. TROUTT, Experiments on the instability waves in a supersonic jet and their acoustic radiation, J.Fluid Mech., 69, 73-95, 1975.
24. S. MARTENS, K.W. KINZIE, D.K. MCLAUGHLIN, Measurements of Kelvin-Helmholtz instabilities in a supersonic shear layer, AIAA J., 32, 8, 1633-1639, 1994.
25. K. -S. WEN, Wake transition, AIAA J., 2, 5, 956, 1964.
26. P.S. LYKOUDIS, A review of hypersonic make studies, AIAA J. 4, 4, 577, 1966.
27. H.H. LEGNER, M.I. FINSON, Mach number dependence of laminar near-wake transition for slender cones, AIAA J., 15, 3, 417-419, 1977.
28. A. ROSHKO, U. FISHDON, About the role of transition in a near wake, Mechanics, 6, 1969.
29. T.L. JACKSON, C.E. GROSCH, Inviscid spatial stability of a compressible miiing layer, NASA-CR-181671, ICASE Rep. 2, 1988.
30. T.L. JACKSON, C.E. GROSCH, Inuiscid spatial stability of a compressible miiing layer, J. Fluid Mech., 208, 609-637, 1989.
31. T.L. JACKSON, C.E. GROSCH, Absolute/convective instabilities and the convective Mach number in a compressible miiing layer, Phys.Fluids A, 2, 6, 949-954, 1990.
32. T.L. JACKSON, C.E. GROSCH, Inviscid spatial stability of a compressible miiing layer. Part 2. The flame sheet model, J. Fluid Mech., 217, 391-420, 1990.
33. T.L. JACKSON, C.E. GROSCH, Inviscid spatial stability of a compressible miiing layer. Part 3. Effect of thermodynamics, J. Fluid Mech., 224, 159-175, 1991.
34. S.A. RAGAB, J.L. WU, Linear instability waves in supersonic turbulent miiing layers, AIAA J., 27, 6, 677-686, 1989.
35. U.G. HEGDE, B.T. ZINN, Vortical modę instability of shear layer with temperaturę and density gradients, AIAA J., 28, 8, 1389-1396, 1991.
36. A.N. KUORYAVTSEV, A.S. SOLOVYOV, Stability of a shear layer of compressible gas [in Russian], Zh. Prikl. Mekh. Tekh. Fiz., 6, 119 -127, 1989.
37. A.N. KUDRYAVTSEV, A.S. SOLOVYOV, Stability of a viscous compressible shear layer with temperaturę leap [in Russian], Zn. Prikl. Mekh. Tekh. Fiz., 4, 88-95, 1991.
38. L. LEES, Hypersonic wakes and trails, AIAA J., 2, 3, 417-428, 1964.
39. L. LEES, H. GOLD, Stability of laminar boundary layers and wakes at hypersonic speeds. Part 1. Stability of laminar wakes, [in:] Fund. Phenom. in Hypersonic Flow, 4, 310-337, Cornell Univ. Press, Buffalo, N.Y. 1964.
40. S.A. RAGAB, J.L. WU, Linear instabilities in two-dimensional compressible mixing layers, Phys. Fluids A, 1, 957-966, 1989.
41. A.J. PALLONE, J. ERDOS, J. ECKERMAN, Hypersonic laminar wakes and transition studies, AIAA J., 2, 5, 855-863, 1964.
42. B.L. REEVES, L. LEES, Theory of laminar near wake of blunt bodies in hypersonic flow, AIAA J., 3, 11, 2061, 1965.

Typ dokumentu

Bibliografia

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