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On the development of Mach waves radiated by small disturbances

Published online by Cambridge University Press:  28 March 2006

J. E. Ffowcs Williams
Affiliation:
Bolt Beranek and Newman Inc., 50 Moulton Street, Cambridge, Massachusetts Now at Imperial College, University of London.

Abstract

Mach wave radiation studies have, so far, been concentrated on the sound radiated to large distances from the flow. Then, both a turbulent eddy and the distance it may travel during its coherent life, appear small to the distant observer, so that the sound arrives from one direction. When that direction is the Mach angle, a Mach wave is heard. This paper deals with a different situation, where, although a turbulent eddy appears small, the distance it travels does not. Sound arriving at the observer then comes from different directions at different times in the eddy's life, so that Mach waves can only be radiated over a relatively small range, where the radiation angle corresponds to the Mach angle. In that range the far field equations no longer apply. It is shown that, whereas the distant field increases with the cube of convection Mach number, M, and inversely with the square of distance travelled, 1/r2, this particular near field is of a type where the mean square density, $\overline {\rho^2}$, has the proportionality $\overline {\rho^2} \sim \rho^{-2} {\frac {l^{3/2}}{r^{3/2}}}{\frac {M^{7/3}}{(M-1)^{1/2}}}$

Type
Research Article
Copyright
© 1965 Cambridge University Press

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References

Ffowcs Williams, J. E. 1963 The noise from turbulence convected at high speed. Phil. Trans. A, 255, 469.Google Scholar
Kistler, A. L. & Chen, W. S. 1963 A fluctuating pressure field in a supersonic turbulent boundary layer. J. Fluid Mech. 16, 1.Google Scholar
Laufer, J. 1961 Aerodynamic noise in supersonic wind tunnels. J. Aero. Sci. 28, 9.Google Scholar
Laufer, J. 1962 Sound radiation from a turbulent boundary layer. Proceedings of the Marseille Conference on Turbulence. Published as CNRS Report No. 108, Editions de Centre National de la Recherche Scientifique, 15, Quai Anatole-France, Paris (VII).
Laufer, J. 1964 Mechanism of noise generation in the turbulent boundary layer. AGARDograph with Ffowcs Williams, J. E. and Childress, S.
Lighthill, M. J. 1952 On sound generated aerodynamically: I, general theory. Proc. Roy. Soc. A, 221, 564.Google Scholar
Lighthill, M. J. 1963 Jet noise. A.I.A.A. Journal, 1, 1057.Google Scholar