Hostname: page-component-cd9895bd7-jkksz Total loading time: 0 Render date: 2024-12-19T05:47:06.296Z Has data issue: false hasContentIssue false

Sound generated by instability waves of supersonic flows. Part 1. Two-dimensional mixing layers

Published online by Cambridge University Press:  20 April 2006

Christopher K. W. Tam
Affiliation:
Department of Mathematics, Florida State University, Tallahassee, Florida 32306
Dale E. Burton
Affiliation:
Department of Mathematics, Florida State University, Tallahassee, Florida 32306

Abstract

The problem of acoustic radiation generated by a spatially growing instability wave of a supersonic two-dimensional mixing layer is studied. It is shown that at high supersonic Mach numbers the classical locally parallel-flow hydrodynamic stability theory as well as the more recent theories based on the method of multiple scales (e.g. Saric & Nayfeh 1975; Crighton & Gaster 1976; Plaschko 1979; Tam & Morris 1980) would fail to give even a first-order instability wave solution. Physically, at these high flow speeds the radiated sound field is no longer an insignificant part of the total phenomenon. The disturbances associated with the flow-instability process now extend from the mixing layer all the way to the far field. The problem is therefore global in nature. Methods of solution which are predicated on local approximations such as the classical locally parallel-flow hydrodynamic-stability theory or the method of multiple scales are hence inappropriate and inapplicable. A global solution based on the method of matched asymptotic expansions is constructed. The outer solution is valid outside the mixing layer. It provides a mathematical description of the radiated acoustic field and the pressure near field. The near field in this case consists of both the acoustic and the hydrodynamic (non-propagating) fluctuation components. The inner solution is valid inside and in the immediate vicinity of the mixing layer. Physically it represents the instability wave of the flow. Matching is carried out according to the intermediate matching principle of Van Dyke (1975) and Cole (1968). Matching terms to order unity gives the basic instability-wave solution. Matching terms to the next order gives the instability- and acoustic-wave amplitude equation. For low-Mach-number flows it is found that the present results agree with the multiple-scales solution of Tam & Morris (1980).

Type
Research Article
Copyright
© 1984 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Bishop, K. A., FFOWCS WILLIAMS, J. E. & Smith, W. 1971 On the noise sources of the unsuppressed high speed jet J. Fluid Mech. 50, 2131.Google Scholar
Blumen, W. 1970 Shear layer instability of an inviscid compressible fluid J. Fluid Mech. 40, 769781.Google Scholar
Blumen, W. 1971 Jet flow instability of an inviscid compressible fluid J. Fluid Mech. 46, 737747.Google Scholar
Boyce, W. E. & Diprima, R. C. 1977 Elementary Differential Equations. Wiley.
Chan, Y. Y. & Westley, R. 1973 Directional acoustic radiation generated by spatial jet instability Can. Aero. and Space Inst. Trans. 6, 3641.Google Scholar
Cole, J. D. 1968 Perturbation Methods in Applied Mathematics. Blaisdell.
Crighton, D. B. & Gaster, M. 1976 Stability of slowly divergent jet flows J. Fluid Mech. 77, 397413.Google Scholar
Dingle, R. B. 1973 Asymptotic Expansions: Their Derivation and Interpretation. Academic.
Eggers, J. M. 1966 Velocity profile and eddy viscosity distributions downstream of a Mach 2.2 nozzle exhausting to quiescent air. NASA TN D-3601.Google Scholar
Garg, V. K. & Round, G. F. 1978 Nonparallel effects on the stability of jet flows. Trans ASME E: J. Appl. Mech. 45, 717722.
Hill, W. G. & Page, R. H. 1969 Initial development of turbulent compressible free shear layers. Trans. ASME D: J. Basic Engng 91, 6773.
Kaplun, S. 1967 In Fluid Mechanics and Singular Perturbations (ed. P. A. Lagerstrom, L. N. Howard & C. S. Liu). Academic.
Lau, J. C. 1981 Effects of exit Mach number and temperature on mean-flow and turbulence characteristics in round jets J. Fluid Mech. 105, 193218.Google Scholar
Lau, J. C., Morris, P. J. & Fisher, M. J. 1979 Turbulence measurements in subsonic and supersonic jets using a laser velocimeter J. Fluid Mech. 93, 127.Google Scholar
Lees, L. & Lin, C. C. 1946 Investigation of the stability of the laminar boundary layer in a compressible fluid. NACA Tech. Note 1115.Google Scholar
Lees, L. & Reshotko, E. 1962 Stability of the compressible laminar boundary layer J. Fluid Mech. 12, 555590.Google Scholar
Liepmann, H. W. & Laufer, J. 1947 Investigations of free turbulent mixing. NACA Tech. Note 1257.Google Scholar
Lin, C. C. 1953 On the stability of laminar mixing region between two parallel streams in a gas. NACA Tech. Note 2887.Google Scholar
Mack, L. M. 1965 Computation of the stability of the laminar compressible boundary layer. In Methods in Computational Physics, vol. 4 (ed. B. Alder), pp. 247299. Academic.
Mack, L. M. 1975 Linear stability theory and the problem of supersonic boundary-layer transition AIAA J. 13, 279289.Google Scholar
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, 7395.Google Scholar
Mclaughlin, D. K., Morrison, G. L. & Troutt, T. R. 1977 Reynolds number dependence in supersonic jet noise AIAA J. 15, 526532.Google Scholar
Morris, P. J. 1977 Flow characteristics of the large-scale wave-like structure of a supersonic round jet J. Sound Vib. 53, 223244.Google Scholar
Morris, P. J. 1981 Stability of a two-dimensional jet AIAA J. 19, 857862.Google Scholar
Nayfeh, A. H. 1973 Perturbation Methods. Wiley-Interscience.
Plaschko, P. 1979 Helical instabilities of slowly divergent jets J. Fluid Mech. 92, 209215.Google Scholar
Reshotko, E. 1976 Boundary layer stability and transition Ann. Rev. Fluid Mech. 8, 311349.Google Scholar
Saric, W. S. & Nayfeh, A. H. 1975 Nonparallel stability of boundary layer flows Phys. Fluids 18, 945950.Google Scholar
Saric, W. S. & Nayfeh, A. H. 1977 Nonparallel stability of boundary layers with pressure gradients and suction. AGARD CP-224, pp. 6.16.21.Google Scholar
Sedel'Nikov, T. K. 1967 The frequency spectrum of the noise of a supersonic jet. Phys. Aero. Noise. Nauka. (Transl. 1969 NASA TTF-538, pp. 71–75.)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. 1972 On the noise of a nearly ideally expanded supersonic jet J. Fluid Mech. 51, 6995.Google Scholar
Tam, C. K. W. 1975 Supersonic jet noise generated by large-scale disturbances J. Sound Vib. 38, 5179.Google Scholar
Tam, C. K. W. & Burton, D. E. 1984 Sound generated by instability waves of supersonic flows. Part 2. Axisymmetric jets J. Fluid Mech. 138, 273295.Google Scholar
Tam, C. K. W. & Morris, P. J. 1980 The radiation of sound by the instability waves of a compressible plane turbulent shear layer J. Fluid Mech. 98, 349381.Google Scholar
Troutt, T. R. 1978 Measurements on the flow and acoustic properties of a moderate Reynolds number supersonic jet. Ph.D. thesis, Oklahoma State University.
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, 123156.Google Scholar
Van Dyke, M. 1975 Perturbation Methods in Fluid Mechanics. Parabolic.
Whitham, G. B. 1974 Linear and Nonlinear Waves. Wiley-Interscience.