Hostname: page-component-78c5997874-ndw9j Total loading time: 0 Render date: 2024-11-10T07:28:56.941Z Has data issue: false hasContentIssue false

Noise generation by a low-Mach-number jet

Published online by Cambridge University Press:  20 April 2006

John Laufer
Affiliation:
Department of Aerospace Engineering, University of Southern California, Los Angeles, CA 90089-1454
Ta-Chun Yen
Affiliation:
Department of Aerospace Engineering, University of Southern California, Los Angeles, CA 90089-1454 Present address: Beijing University, Beijing, People's Republic of China.

Abstract

Using a ‘clean’ jet facility the relationship between the jet flow and its radiation field was studied experimentally in the Mach-number range 0.05 < Mj < 0.20 and a Reynolds-number range 6 × 104 < ReD < 2.3 × 105. The various acoustic source parameters such as strength, frequency and Mach number were varied systematically, and the far-field pressure measured simultaneously. On the basis of these measurements the nature of the sources in the initial shear layer could be characterized. The principal results, equally valid for unexcited and excited jets, are as follows: the acoustic sources are not convected but are located within a confined volume fixed with respect to the nozzle even though they are being generated by moving disturbances in the jet; they are associated with the nonlinear saturation of the unstable wave amplitudes of the shear layer occurring at the vortex-pairing locations; the radiation intensity varies nonlinearly with the source strength and is highly directional, exponential in character.

Type
Research Article
Copyright
© 1983 Cambridge University Press

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

Bechert, D. & Pfizenmaier, E. 1975 On the amplification of broadband jet noise by pure tone excitation J. Sound Vib. 43, 581587.Google Scholar
Browand, F. K. & Laufer, J. 1975 The role of large scale structures in the initial development of circular jets. In Proc. 4th Biennial Symp. on Turbulence in Liquids, University of Missouri (ed. J. L. Zakin & G. K. Patterson), pp. 333344. Science Press.
Brown, G. L. & Roshko, A. 1974 On density effects and large structures in turbulent mixing layers J. Fluid Mech. 64, 775816.Google Scholar
Crighton, D. G. 1975 Basic principles of aerodynamic noise generation Prog. Aerospace Sci. 16, 3196.Google Scholar
Crow, S. C. 1972 Acoustic gain of a turbulent jet. Bull. Am. Phys. Soc., paper IE.6.Google Scholar
Crow, S. C. & Champagne, F. H. 1971 Orderly structure in jet turbulence J. Fluid Mech. 48, 547591.Google Scholar
Ffowcs Williams, J. E. & Kempton, A. J. 1978 The noise from the large scale structure of a jet J. Fluid Mech. 84, 673694.Google Scholar
Ho, C. M. & Huang, L. S. 1982 Subharmonics and vortex merging in mixing layers J. Fluid Mech. 119, 443473.Google Scholar
Hurdle, P. M. & Meecham, W. C. 1974 Investigation of the aerodynamic noise generating region of a jet engine by means of the simple source fluid dilatation model J. Acoust. Soc. Am. 56, 17081721.Google Scholar
Kibens, V. 1980 Discrete noise spectrum generated by an acoustically excited jet AIAA J. 18, 434441.Google Scholar
Laufer, J. 1974 On the mechanism of noise generation by turbulence. Omaggio a Carlo Ferrari, pp. 451464. Libreria Editrice Universitaria Levrotto & Bella, Torino.
Laufer, J. 1981 Instability and turbulence in jets. In Transition and Turbulence (ed. R. E. Meyer), pp. 6376. Academic.
Laufer, J. & Monkewitz, P. 1980 On turbulent jet flows: a new perspective. AIAA Paper 80–0962.Google Scholar
Laufer, J. & Zhang, J-X. 1983 Unsteady aspects of a low Mach number jet Phys. Fluids 26, 17401750.Google Scholar
Lighthill, M. J. 1952 On sound generated aerodynamically. I. General Theory Proc. R. Soc. Lond. A211, 564587.Google Scholar
Michalke, A. 1971 Instabilität eines kompressiblen runden Freistrahls unter Berücksichtigung des Einflusses der Strahlgrenzschichtdicke Z. Flugwiss. 19, 319328.Google Scholar
Moore, C. J. 1977 The role of shear-layer instability waves in jet exhaust noise J. Fluid Mech. 80, 321367.Google Scholar
Moore, C. J. 1978 The effect of shear layer instability on jet exhaust noise. In Structure and Mechanisms of Turbulence II (ed. H. Fiedler). Lecture Notes in Physics, vol. 76, pp. 254264. Springer.
Winant, C. D. & Browand, F. K. 1974 Vortex pairing: the mechanism of turbulent mixing-layer growth at moderate Reynolds number. J. Fluid Mech. 63, 237255.Google Scholar