Hostname: page-component-5c6d5d7d68-vt8vv Total loading time: 0.001 Render date: 2024-08-18T16:21:26.797Z Has data issue: false hasContentIssue false

Acoustic near field of a transonic instability wave packet

Published online by Cambridge University Press:  19 April 2007

STÉPHANE LE DIZÈS
Affiliation:
Institut de Recherche sur les Phénomènes Hors Équilibre, CNRS, 49 rue F. Joliot-Curie, BP 146, F-13384 Marseille cedex 13, France
CHRISTOPHE MILLET
Affiliation:
Laboratoire de Géophysique, CEA, BP 12, 91680 Bruyères-le-Châtel, France

Abstract

We consider the problem of acoustic radiation generated by a spatial instability wave on a weakly developing shear flow. Assuming a local WKBJ approximation for the instability wave near its maximum, we compute the acoustic pressure field by using a Fourier transform along the streamwise direction. When the instability wave is close to transonic near its maximum amplitude, approximations for this pressure field are obtained by a steepest descent method. A branch cut and several saddle points are shown possibly to contribute to the approximation. A detailed analysis of these contributions is provided. The modifications of the acoustic field when we pass from subsonic to supersonic are examined. In particular, the superdirective character of the acoustic field of subsonic instability waves and the directivity pattern of supersonic waves are shown to be both compatible with our mathematical description and associated with a single saddle-point contribution.

The acoustic near field is also shown to possess a caustic around which a specific approximation is derived. In a large region of the physical space, the near field is composed of two saddle-point contributions. Close to the shear flow, one of these contributions degenerates into a branch-point contribution which always becomes dominant over the instability wave downstream of a location that is computed. An interesting phenomenon is observed in certain regions downstream of the maximum: the transverse behaviour of the instability wave has to be exponentially growing far from the shear layer to match the acoustic field. We demonstrate that this phenomenon neither requires a branch-point contribution nor a supersonic instability wave.

Type
Papers
Copyright
Copyright © Cambridge University Press 2007

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

REFERENCES

Arnold, V. I. 1978 The Mathematical Methods of Classical Mechanics. Springer.Google Scholar
Avital, E. J. & Sandham, N. D. 1997 A note on the structure of the acoustic field emitted by a wave packet. J. Sound Vib. 204, 533539.Google Scholar
Bender, C. M. & Orszag, S. A. 1978 Advanced Mathematical Methods for Scientists and Engineers. McGraw-Hill.Google Scholar
Colonius, T., Lele, S. K. & Moin, P. 1997 Sound generation in a mixing layer. J. Fluid Mech. 330, 375409.Google Scholar
Cooper, A. J. & Crighton, D. G. 2000 Global modes and superdirective acoustic radiation in low-speed axisymmetric jets. Eur. J. Mech. B\Fluids 19, 559574.CrossRefGoogle Scholar
Crighton, D. G. 1975 Basic principles of aerodynamic noise generation. Prog. Aerospace Sci. 16, 3196.Google Scholar
Crighton, D. G. & Huerre, P. 1990 Shear-layer pressure fluctuations and superdirective acoustic sources. J. Fluid Mech. 220, 355368.Google Scholar
Erdélyi, A. 1956 Asymptotic Expansions. Dover.Google Scholar
Freund, J. F. 2001 Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9. J. Fluid Mech. 438, 277305.Google Scholar
Goldstein, M. E. 1984 Aeroacoustics of turbulent jet flows. Annu. Rev. Fluid Mech. 16, 263295.CrossRefGoogle Scholar
Goldstein, M. E. & Leib, S. J. 2005 The role of instability waves in predicting jet noise. J. Fluid Mech. 525, 3772.CrossRefGoogle Scholar
Kravtzov, Y. A. & Orlov, Y. I. 1990 Geometrical Optics of Inhomogeneous Media, Springer series on wave phenomena, vol. 6. Springer.Google Scholar
Laufer, J. & Yen, T. C. 1983 Noise generation by a low-Mach-number jet. J. Fluid Mech. 134, 131.CrossRefGoogle Scholar
Lighthill, M. J. 1952 On sound generated aerodynamically. i: box General theory. Proc. Roy. Soc. Lond. 211, 564587.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.CrossRefGoogle Scholar
Malik, M. R. & Chang, C.-L. 2000 Nonparallel and nonlinear stability of supersonic jet flow. Comput. Fluids 29, 327365.CrossRefGoogle Scholar
Millet, C. & Casalis, G. 2004 Exponential-algebraic transition in the near-field of low supersonic jets. Eur. J. Mech. B Fluids 23, 367379.CrossRefGoogle Scholar
Mitchell, B. E., Lele, S. K. & Moin, P. 1997 Direct computation of Mach wave radiation in an axisymmetric supersonic jet. AIAA J. 35, 15741579.CrossRefGoogle Scholar
Mohseni, K., Colonius, T. & Freund, J. B. 2002 An evaluation of linear instability waves as sources of sound in a supersonic turbulent jet. Phys. Fluids 14, 35933600.Google Scholar
Morris, P. J. & Tam, C. K. W. 1977 Near and far field noise from large-scale instabilities of axisymmetric jets. AIAA Paper 77-1351.Google Scholar
Morris, P. J., Long, L. N., Bangalore, A. & Wang, Q. 1997 A parallel three-dimensional computational aeroacoustics method using nonlinear disturbance equations. J. Comput. Phys. 133, 5674.Google Scholar
Morrison, G. L. & McLaughlin, D. K. 1980 Instability process in low Reynolds number supersonic jets. AIAA J. 18, 793800.Google Scholar
Stromberg, J. L., McLaughlin, D. K. & Troutt, T. R. 1980 Flow field and acoustic properties of a Mach number 0.9 jet at low Reynolds number. J. Sound Vib. 72, 159176.Google Scholar
Tam, C. K. W. 1995 Supersonic jet noise. Annu. Rev. Fluid Mech. 27, 1743.Google Scholar
Tam, C. K. W. & Burton, D. E. 1984 a Sound generated by instability waves of supersonic flows. Part 1. Two dimensional mixing layers. J. Fluid Mech. 138, 249271.Google Scholar
Tam, C. K. W. & Burton, D. E. 1984 b Sound generated by instability waves of supersonic flows. Part 2. Axisymmetric jets. J. Fluid Mech. 138, 273295.CrossRefGoogle 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
Tam, C. K. W. & Chen, P. & Seiner, J. M. 1992 Relationship between instability waves and noise of high-speed jets. AIAA J. 30, 17471752.Google Scholar
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
Yu, J. C. & Dosanjh, D. S. 1971 Noise field of coaxial interacting supersonic jet flow. AIAA Paper 71–152.Google Scholar