Abstract
The effect of applying a Kutta-Joukowski condition at the edges of an absorbing strip which is generating noise in a turbulent fluid at low Mach numbers is examined. It is found that the presence of fluid flow attenuates the sound level in the shadow region of the absorbent screen. There is greater attenuation of the sound level in the trailing edge (wake present) situation than there is for the leading edge (no wake present) situation. Physical interpretation of the results is then discussed.
Similar content being viewed by others
References
D.S. Jones, Aerodynamic sound due to a source near a half-plane. J. Inst. Math. Appl.,9 (1972), 114.
R. Balasubramanyam, Aerodynamic sound due to a point source near a half-plane. IMA J. Appl. Math.,33, No. 1 (1984), 71.
S.W. Rienstra, Sound diffraction at a trailing edge. J. Fluid Mech.,108 (1981), 443.
A.D. Rawlins, Acoustic diffraction by an absorbing semi-infinite plane in a moving fluid, II. Proc. Roy. Soc. Edinb. Ser. A,75 (1975), 83.
P.M. Morse and K.U. Ingard, Encyclopedia of Physics, Acoustic I. Springer Verlag, Berlin, 1961.
D.S. Jones, The Theory of Electromagnetism. Pergamon, Oxford, 1964.
A.D. Rawlins, Acoustic diffraction by an absorbing semi-infinite half plane in a moving fluid. Proc. Roy. Soc. Edinb. Ser. A,72 (1974), 337.
B. Noble, Methods based on the Wiener-Hopf technique. Pergamon Press, London, 1958.
Author information
Authors and Affiliations
About this article
Cite this article
Asghar, S., Hayat, T. & Ayub, M. Scattering of sound near an absorbing strip. Japan J. Indust. Appl. Math. 15, 331–343 (1998). https://doi.org/10.1007/BF03167316
Received:
Revised:
Issue Date:
DOI: https://doi.org/10.1007/BF03167316