Receptivity of hypersonic boundary layer to wall disturbances

Theoretical and Computational Fluid Dynamics

Volumn 15, Issue 4, 2002, Pages 231-254

  Fedorov, A V ^a   Khokhlov, A P ^a  

^a MOSCOW INSTITUTE OF PHYSICS AND TECHNOLOGY   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COOLING; NUMERICAL METHODS; THERMAL EFFECTS; WALL FLOW;

HYPERSONIC BOUNDARY LAYER; THEORETICAL ANALYSIS; WALL CONDITIONS; WALL DISTURBANCES;

HYPERSONIC FLOW;

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COOLING; HYPERSONIC FLOW; NUMERICAL METHODS; THERMAL EFFECTS; WALL FLOW;

BOUNDARY LAYER; NUMERICAL METHOD; VIBRATION; WALL;

EID: 23044530373     PISSN: 09354964     EISSN: 14322250     Source Type: Journal    
DOI: 10.1007/s001620100052     Document Type: Article

References (30)

1. Abramovitz, M., and Stegun, I.A. (1964). Handbook of Mathematical Functions. Applied Mathematics Series 55. National Bureau of Standards, Washington, DC.
2. Choudhari, M. (1994). Theoretical Prediction of Boundary-Layer Receptivity. AIAA Paper No. 94-2223.
3. Choudhari, M., and Streett, C. (1990). Boundary Layer Receptivity Phenomena in Three-Dimensional and High-Speed Boundary Layers. AIAA Paper No. 90-5258.
4. Fedorov, A.V. (1984). Excitation of Tollmien-Schlichting waves in boundary layer by periodic external forcing localized on body surface. Izv. Akad. Nauk. SSSR, Mekh. Zhidk. Gaza, 6, 36-41.
5. Fedorov, A.V., and Khokhlov, A.P. (1991). Excitation of unstble modes in a supersonic boundary layer by acoustic waves. Fluid Dynamics, 9, 456-467.
6. Fedorov, A.V., and Khokhlov, A.P. (1993). Excitation and evolution of unstable disturbances in supersonic boundary layer. Proceedings of the 1993 ASME Fluid Engineering Conference, Washington, DC, June 20-24, 1993, pp. 1-13. FED,- Vol. 151, Transitional and Turbulent Compressible Flows. ASME New York.
7. Fedorov, A.V., and Khokhlov, A.P. (2001). Prehistory of instability in a hypersonic boundary layer. Theoret. Comput. Fluid Dynamics, 14(6), 359-375.
8. Fedorov, A.V., and Tumin, A.M. (2001). Initial-Value Problem for Hypersonic Boundary Layer Flows. AIAA Paper No. 2001-2781.
9. Gaster, M. (1974). On the effects of boundary-layer growth on flow stability. J. Fluid Mech., 66, 465-480.
10. Gilev, V.M., and Kozlov, V.V. (1983). Excitation of Tollmien-Schlichting Waves by Vibrator in Boundary Layer. Preprint No. 19-83. ITAM SO AN SSSR, Novosibirsk.
11. Goldstein, M.E. (1983). The evolution of Tollmien-Schlichting waves near a leading edge. J. Fluid Mech., 127, 59-81.
12. Goldstein, M.E. (1985). Scattering of acoustic waves into Tollmein-Schlichting waves by small streamwise variation in surface geometry. J. Fluid Mech., 154, 509-529.
13. Hayes, W.D., and Probstein, R.F. (1959). Hypersonic Flow Theory. Academic Press, New York.
14. Hefner, J.N., and Bushnell, D.M. (1979). Application of Stability Theory to Laminar Flow Control. AIAA Paper No. 79-265.
15. Kendall, J.M. (1975). Wind tunnel experiments relating to supersonic and hypersonic boundary layer transition. AIAA J., 13(3), 290-299.
16. Kozlov, V.V, and Ryzhov, O.S. (1990). Receptivity of boundary layers: asymptotic theory and experiments. Proc. R. Soc. London, Ser. A 440, 341.
17. Mack, L.M. (1975). Linear stability theory and the problem of supersonic boundary-layer transition, AIAA J., 13(3), 278-289.
18. Malik, M., Zang, T., and Bushnell, D. (1990). Boundary Layer Transition in Hypersonic Flows. AIAA Paper No. 90-5232.
19. Maslov, A.A., Shiplyuk, A.A., Sidorenko, A.A., and Arnal, D. (2001). Leading-edge receptivity of a hypersonic boundary layer on a flat plate. J. Fluid Mech., 426, 73-94.
20. Nayfeh, A.H. (1980). Stability of three-dimensional boundary layer. AIAA J., 18(4), 406-416.
21. Reshotko, E. (1976) Boundary layer stability and control. Annu. Rev. Fluid Mech., 8, 311.
22. Ruban, A.I., (1984). On Tollmien-Schlichting waves generation by sound. Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, 6, 60-67
23. Skuratov, A.S., Fedorov, A.V., and Shogin, Yu.N. (1992). Analysis of flight and wind tunnel experimental data on the laminarturbulent transition of the boundary layer on sharp nosed cones with smooth and rough surface. In Methods of Investigation of Characteristics of Hypersonic Vehicles, pp. 171-172. Annual TsAGI's Workshop-School an "Fluid Dynamics", February 25-March 1. Zhukovski, Moscow Region.
24. Stetson, K.F., and Kimmel, R.L. (1992). The Hypersonic Boundary-Layer Stability, AIAA Paper No. 92-0737.
25. Tumin, A.M., and Fedorov, A.V. (1984). Excitation of instability waves by local vibrator in boundary layer. J. Prikl. Mekh. Tekh. Fiz., 6, 65-71.
26. Vladimirov, V.S. (1976). Equations of Mathematical Physics. Nauka, Moscow.
27. Wu, X. (1999). Generation of Tollmien-Schlichting waves by convecting gusts interacting with sound. J. Fluid Mech., 397, 285-316.
28. Zhigulev, V.N., and Fedorov, A.V. (1887). On boundary layer receptivity to acoustic disturbances. J. Prikl. Mekh. Tekh. Fiz., 6, 43-49.
29. Zhigulev, V.N., and Tumin, A.M. (1987). Onset of Turbulence. Nauka, Novosibirsk.
30. Zhong, X., and Ma, Y. (2001). Numerical Simulation of Receptivity and Stability of Nonequilibrium Reacting Hypersonic Boundary Layers. AIAA Paper No. 97-0755.