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The excitation of Tollmien-Schlichting waves in low subsonic boundary layers by free-stream sound waves

Published online by Cambridge University Press:  20 April 2006

Christopher K. W. Tam
Affiliation:
Department of Mathematics and Computer Science, Florida State University, Tallahassee, Florida 32306

Abstract

The excitation of Tollmien-Schlichting waves in low subsonic flat-plate boundary layers by sound is investigated theoretically. The problem is formulated mathematically as an inhomogeneous boundary-value problem which is then solved by a Green's-function technique. It is found that the amplitude of the excited Tollmien-Schlichting wave satisfies an inhomogeneous first-order differential equation. The calculated wave amplitude according to this equation exhibits spatial oscillations in the region ahead of the lower branch neutral stable point of the boundary layer. This characteristic feature resembles that observed experimentally by Shapiro (1977). The theoretical value of the coupling constant between incident sound wave and excited Tollmien-Schlichting wave agrees favourably with measured data. Other predictions of the theory also seem to compare well with available experimental measurements.

Type
Research Article
Copyright
© 1981 Cambridge University Press

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References

Briggs, R. J. 1964 Electron-Stream Interaction with Plasmas. Massachusetts Institute of Technology Press.
Freymuth, P. 1966 On transition in a separated laminar boundary layer. J. Fluid Mech. 25, 683704.Google Scholar
Kachanov, Yu. S., Kozlov, V. V. & Levchenko, V. Ya. 1978 Occurrence of Tollmien—Schlichting waves in the boundary layer under the effect of external perturbations. Izv. Akad. Nauk S.S.S.R. Mekhanika Zhid. i Gaza (English translation Fluid Dyn.) 13, 704–711.
Kendall, J. M. 1975 Wind tunnel experiments relating to supersonic and hypersonic boundary layer transition. A.I.A.A. J. 13, 290299.Google Scholar
Knapp, C. F. & Roache, P. J. 1968 A combined visual and hot-wire anemometer investigation of boundary layer transition. A.I.A.A. J. 6, 2936.Google Scholar
Lin, C. C. 1966 Theory of Hydrodynamic Stability. Cambridge University Press.
Mack, L. M. 1975 Linear stability theory and the problem of supersonic boundary layer transition. A.I.A.A. J. 13, 278289.Google Scholar
Mack, L. M. 1977 Transition and laminar instability. JPL Publication 77–15.
Michalke, A. 1965 On spatially growing disturbances in an inviscid shear layer. J. Fluid Mech. 23, 521544.Google Scholar
Reshotko, E. 1976 Boundary layer stability and transition. Ann. Rev. Fluid Mech. 8, 311349.Google Scholar
Scott, M. R. & Watts, H. A. 1977 Computational solutions of linear two-point boundary value problems via orthonormalization. SIAM J. Numer. Anal. 14, 4070.Google Scholar
Shapiro, P. 1977 The influence of sound upon laminar boundary layer instability. Acoustics and Vibration Lab. Rep. no. 83458–83560–1. Massachusetts Institute of Technology.Google Scholar
Spangler, J. G. & Wells, C. S. 1968 Effect of free stream disturbances on boundary layer transition. A.I.A.A. J. 6, 543547.Google Scholar
Tam, C. K. W. 1971 Directional acoustic radiation from a supersonic jet generated by shear layer instability. J. Fluid Mech. 46, 757768.Google Scholar
Tam, C. K. W. 1978 Excitation of instability waves in a two-dimensional shear layer by sound. J. Fluid Mech. 89, 357371.Google Scholar
Thomas, A. S. W. & Lekoudis, S. G. 1978 Sound and Tollmien—Schlichting waves in a Blasius boundary layer. Phys. Fluids 21, 21122113.Google Scholar
Wygnanski, I., Haritonidis, J. H. & Kaplan, R. E. 1979 On a Tollmien—Schlichting wave packet produced by a turbulent spot. J. Fluid Mech. 92, 505528.Google Scholar