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Sound radiation from a cylindrical duct. Part 2. Source modelling, nil-shielding directions, and the open-to-ducted transfer function

Published online by Cambridge University Press:  26 April 2006

C. J. Chapman
Affiliation:
Department of Mathematics, University of Keele, Keele, Staffordshire, ST5 5BG, UK

Abstract

This paper analyses the sound radiated from the front face of a hard-walled circular cylindrical duct in a subsonic mean flow when the duct contains acoustic sources typical of those in a ducted-fan aeroengine. Two main results are established for modes of any given frequency and circumferential order. The first result is that in certain easily calculated directions, called here the nil-shielding directions, the sound radiated by ducted sources is the same as the sound radiated by the corresponding open sources, i.e. by unducted sources of the same distribution and strength radiating into free space. Thus in these special directions the duct has no noise-shielding effect. The second result is that, in the Kirchhoff approximation, the sound radiated by the open sources in the nil-shielding directions determines the sound radiated by the ducted sources in all directions; i.e. the sound fields radiated by open and ducted sources are related by an open-to-ducted transfer function. This function is such that the sound radiated by the ducted sources is a linear combination of certain diffraction functions, in which the coefficients are given by the sound radiated by the open sources in the nil-shielding directions. The diffraction functions do not depend on the sources and are here calculated explicitly in terms of Bessel functions. The method used in the paper is Kirchhoff's approximation; within linear theory this gives the nil-shielding directions exactly, i.e. in agreement with the Wiener—Hopf solution, and gives the main beam of the radiated field, including the major side-lobes, to good accuracy. The results are relevant to the sound radiated into the forward arc by a ducted turbofan aeroengine.

Type
Research Article
Copyright
© 1996 Cambridge University Press

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References

Boyd, W. K., Kempton, A. J. & Morfey, C. L. 1984 Ray-theory predictions of the noise radiated from aeroengine ducts. AIAA Paper 84-2332.
Cargill, A. M. 1987 A note on high frequency duct radiation. Internal Rep., Rolls-Royce, Derby, England.Google Scholar
Chapman, C. J. 1994 Sound radiation from a cylindrical duct. Part 1. Ray structure of the duct modes and of the external field. J. Fluid Mech. 281, 293311.Google Scholar
Eversman, W. 1991 Theoretical models for duct acoustic propagation and radiation. In Aeroacoustics of Flight Vehicles: Theory and Practice. Volume 2: Noise Control ed. (H. H. Hubbard), pp. 101163. NASA Reference Publication 1258, vol.2.
Garrick, I. E. & Watkins, C. E. 1954 A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers. NACA Rep. 1198.Google Scholar
Garrick, M. E. 1976 Aeroacoustics. McGraw-Hill
Hanson, D. B. 1983 Compressible helicoidal surface theory for propeller aerodynamics and noise. AIAA J. 21, 881889.Google Scholar
Homicz, G. F. & Lordi, J. A. 1975 A note on the radiative directivity patterns of duct acoustic modes. J. Sound Vib. 41, 283290.Google Scholar
Hubbard, H. H., Lansing, D. L. & Runyan, H. L. 1971 A review of rotating blade noise technology. J. Sound Vib. 19, 227249.Google Scholar
Lansing, D. L. 1970 Exact solution for radiation of sound from a semi-infinite circular duct with application to fan and compressor noise. In Analytical Methods in Aircraft Aerodynamics, pp. 323334. NASA SP-228.
Lighthill, J. 1972 The fourth annual Fairey lecture: the propagation of sound through moving fluids. J. Sound Vib. 24, 471492.Google Scholar
Morse, P. M. 1981 Vibration and Sound. Acoustical Society of America, through the American Institute of Physics.
Morse, P. M. & Ingard, K. U. 1968 Theoretical Acoustics. McGraw-Hill
Myers, M. K. 1995 Boundary integral formulations for ducted fan radiation calculations. CEAS/AIAA Paper 95-076.
Myers, M. K. & Lan, J. H. 1993 Sound radiation from ducted rotating sources in uniform motion. AIAA Paper 93-4429.
Parry, A. B. & Crighton, D. G. 1989 Asymptotic theory of propeller noise - Part 1: Subsonic single-rotation propeller. AIAA J. 27, 11841190.Google Scholar
Peake, N. & Crighton, D. G. 1991 An asymptotic theory of near-field propeller acoustics. J. Fluid Mech. 232, 285301.Google Scholar
Rice, E. J., Heidmann, M. F. & Sofrin, T. G. 1979 Modal propagation angles in a cylindrical duct with flow and their relation to sound radiation. AIAA Paper 79-0183.
Schulten, J. B. H. M. 1988 Frequency-domain method for the computation of propeller acoustics. AIAA J. 26, 10271035.Google Scholar
Tyler, J. M. & Sofrin, T. G. 1962 Axial flow compressor noise studies. Trans. Soc. Automotive Engrs 70, 309332.Google Scholar
Weinstein, L. A. 1969 The Theory of Diffraction and the Factorization Method (Generalized Wiener-Hopf Technique). Golem.