Abstract
The study of noise radiated from aero dynamically unsteady fluid flows was studied by Lighthill, who showed there exists an “acoustic analogy” whereby the exact fluid flow can be replaced by an equivalent distribution of acoustic quadrupole sources in which the sources may move but not the fluid. The problem posed by Lighthill was that although this “acoustic analogy” represented an exact solution of the Navier-Stokes equations for the density or pressure, in applications of engineering interest the flow field is rarely known to the exactness required to provide an accurate prediction of the radiated sound field, its acoustic power output, its intensity distribution with distance and direction, and its spectrum. Approximate models of the flow field for subsonic and supersonic jets at rest or moving at a uniform speed through a stationary atmosphere have been introduced into Lighthill’s “acoustic analogy” for the prediction of the radiated sound and to provide a comparison with experimental results. The difficulties in the applications of these models and the limitations in the success achieved with such models has been the subject of continuing study.
This paper gives a brief status report of the current position of the prediction methods used in the noise from jets, and comments on the available experimental data used to verify the accuracy of these models and procedures. Also discussed are the possible computational methods which could exploit current advances made in supercomputer technology in solving the Euler and Navier-Stokes equations for certain classes of flows and which would lead to the evaluation of the radiated sound field from such flows. The problems of computational domains containing embedded flows and their boundary conditions together with the resolution requirements are considered. Also considered are the advantages of the deployment of the “acoustic analogy” over the direct computation of the fluctating pressure and density fields within and external to the flow.
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References
Buckley, R. and Morfey, C. L., 1983. “Effects on jet mixing noise: Scaling laws predicted from flight simulation data,” AIAA 83–0748.
Crighton, D. G., 1981. “Acoustics as a branch of fluid mechanics,” J. Fluid Mech. 106, p. 261.
Crow, S. C., 1970. “Aerodynamic sound emission as a singular perturbation problem,” Stud. Appl. Math. XLIX, p. 1.
Ffowcs Williams, J. E., 1963. “The noise from turbulence at high speed,” Phil. Trans. Roy. Soc. (A) 255, p. 1061.
Fisher, M. J., Harper-Bourne, M., and Glegg, S. A. L., 1977. “Jet noise source location: The polar correlation method,” J. Sound Vibration 51, p. 1.
Goldstein, M. E., 1976. Aeroacoustics, McGraw-Hill Inc.
Guiraud, J. P., 1964. “Theorie du Bruit Ballistique,” ONERA Note Tech., p. 79.
Howe, M. S., 1975. “Contributions to the theory of aerodynamic sound with applications to excess jet noise and the theory of the flute,” J. Fluid Mech. 71, p. 4.
Hubbard, H. H., 1991. “Aeroacoustics of flight vehicles: Theory and practice. Vol. 1: Noise sources,” NASA Ref. Pub. 1258.
Landahl, M. T., 1967. “A wave-guide model for turbulent shear flow,” J. Fluid Mech. 29, p. 3.
Legendre, R., 1981. “Bruits emis par la turbulence,” ONERA Publ. 1981–3.
Lighthill, M. J., 1952. “On sound generated aerodynamically: I. General theory,” Proc. Roy. Soc. (A) 211, p. 1107.
Lighthill, M. J., 1954. “On sound generated aerodynamically: II. Turbulence as a source sound,” Proc. Roy. Soc. (A) 222, p. 1148.
Lighthill, M. J., 1962. “The Bakerian lecture, 1961: Sound generated aerodynamically,” Proc. Roy. Soc. (A) 267, p. 1329.
Lighthill, M. J., 1963. “Jet noise,” AIAA J. 1(7), pp. 1507–1517.
Lighthill, M. J., 1978. Waves in Fluids, C.U.P.
Lilley, G. M., 1958. “On the noise from air jets,” ARC 20376 (unpublished).
Lilley, G. M., Morris, P. J., and Tester, B. J., 1975. “On the theory of jet noise and its applications,” AIAA Progress in Astronautics and Aeronautics 37.
Mohring, W., 1983. “Problems in flow acoustics,” Reviews in Modern Physics 55, p. 3.
Morris, P. J., Giridharan, M. G., and Lilley, G. M., 1990. “On the turbulent mixing of compressible free shear layers,” Proc. Roy. Soc. (A) 431, p. 1882.
Phillips, O. M., 1960. “On the generation of sound by supersonic turbulent shear layers,” J. Fluid Mech. 9, p. 1.
Pridmore-Brown, D. C., 1958. “Sound propagation in a fluid flowing through an attenuating duct,” J. Fluid Mech. 4.
Ribner, H. S., 1964. “The generation of sound by turbulent jets,” Advances in Applied Mechanics 8, Academic Press.
Tester, B. J. and Fisher, M. J., 1981. “Engine noise source breakdown: Theory, simulation and results,” AIAA-81–2040.
Tester, B. J. and Morfey, C. L., 1976. “Developments in jet noise modelling-theoretical predictions with measured data,” J. Sound Vibration 46, p. 1.
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© 1993 Springer-Verlag New York, Inc.
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Lilley, G.M. (1993). On the Noise Radiated from a Turbulent High Speed Jet. In: Hardin, J.C., Hussaini, M.Y. (eds) Computational Aeroacoustics. ICASE/NASA LaRC Series. Springer, New York, NY. https://doi.org/10.1007/978-1-4613-8342-0_5
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DOI: https://doi.org/10.1007/978-1-4613-8342-0_5
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