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Computation of Sound Radiation in an AxisymmetricSupersonic Jet
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 Title & Authors
Computation of Sound Radiation in an AxisymmetricSupersonic Jet
Kim, Yong-Seok; Lee, Duck-Joo;
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An axisymmetric supersonic jet is simulated at a Mach number 2.1 and a Reynolds numberof 70000 to identify the mechanism of Mach wave generation and radiation from the jet. In orderto provide the near-field radiated sound directly and resolve the large-scale vortices highly.high-resolution essentially non-oscillatory(ENO) scheme, which is one of the ComputationalAeroAcoustics(CAA) techniques, is newly employed. Perfectly expanded supersonic jet is selectedas a target to see pure shear layer growth and Mach wave radiation without effect of change injet cross section due to expansion or shock wave generated at nozzle exit. The sound field ishighly directional and dominated by Mach waves generated near the end of potential core. Thenear field sound pressure levels as well as the aerodynamic properties of the jet, such asmean-flow parameters are in fare agreement with experimental data.
 Cited by
Tam, C. K. W., 'Supersonic Jet Noise', Annu. Rev. Fluid Mech., Vol. 27, 1995, pp. 17-43 crossref(new window)

Tam, C. K. W., and Burton, D.E., 'Sound Generated by Instability Waves of Supersonic Flows, Part 2: Axisymmetric jets', Journal of Fluid Mechanics, Vol. 138, 1984, pp. 273-295 crossref(new window)

Tam, C. K. W., and Chen, P., 'Turbulent Mixing Noise from Supersonic Jets'. AIAA Journal, Vol. 32, No. 9, 1994, pp. 1774-1780 crossref(new window)

J. T. C. Liu, 'Developing large-scale wavelike eddies and the near jet noise field', Journal of Fluid Mechanics, Vol. 62, 1974, pp. 437-464 crossref(new window)

D. K. McLaughlin, G. L. Morrison and T. R. Troutt, 'Experiments on the instability waves in a supersonic jet and their acoustic radiation', Journal of Fluid Mechanics, Vol. 69, 1975, pp. 73-95 crossref(new window)

G. L. Morrison and D. K. McLaughlin, 'Noise Generation by Instabilities in Low Reynolds Number Supersonic Jets', Journal of Sound and Vibration. Vol. 65, No. 2, 1979, pp. 177-191 crossref(new window)

Nakamura, Y. and Yamaguchi, H., 'Compressible Jet and Its Sound Emission', Computational Fluid Dynamics JOURNAL. Vol. 8, No. 2, 1999, pp. 250-256

M. J. Lighthill, 'On sound Generated Aerodynamically, I. General theory', Proceedings of the Royal Society London, Ser. A211, 1952, pp. 564-587

T. R. Troutt and D. K. McLaughlin, 'Experiments on the Flow and Acoustic Properties of a Moderate-Reynolds-Number Supersonic Jet', Journal of Fluid Mechanics, Vol. 116, 1982, pp. 123-156 crossref(new window)

Mitchell, B. E., Lele, S. K., and Moin. P., 'Direct Computation of Mach Wave Radiation in an Axisymmetric Supersonic Jet', AIAA Journal, Vol. 35, No. 10, 1997, pp. 1574-1580 crossref(new window)

Mitchell, B. E., Lele, S. K., and Moin, P., 'Direct Computation of the Sound Generated by Vortex Pairing in an Axisymmetric Jet', Journal of Fluid Mechanics, Vol. 383, 1999, pp. 113-142 crossref(new window)

Freund, J. B., Lele, S.K. and Moin, P., 'Direct Simulation of A Mach 1.92 Jet and ItsSound Field', AIAA/CEAS Paper 98-2291, 1998

Freund, J. B., 'Acoustic Sources In A Turbulent Jet : A Direct Numencal Simulation Study', AIAA/CEAS Paper 99-1858, 1999

R. R. Mankbadi, M. E. Hayer, and L. A. Povinelli, 'Structure of Supersonic Jet Flow and Its Radiated Sound', AIAA Journal. Vol. 32, No. 5, 1994, pp. 897-906 crossref(new window)

C. Bogey, C. Bailly and D. Juve. 'Computation of the Sound Radiated by a 3-D Jet Using Large Eddy Simulation', AIAA Paper 2000-2009, June 2000

W. Zhao, S. H. Frankel and L. Mongeau, 'Large Eddy Simulation of Sound Radiation from a Subsonic Turbulent Jet,' AIAA Paper 2000-2078, June 2000

Hoffmann, K. A., 'Computational Fluid Dynamics for Engineers', Engineering Education System, Vol. 2, pp. 25-28

Harten, A., 'High Resolution Schemes for Hyperbolic Conservation Laws', Journal of Computational Physics, Vol. 49, No. 3. 1983, pp. 357-393 crossref(new window)

Kim, Y. S. and Lee, D. J., 'Numerical Analysis of Internal Combustion Engine Intake Noise with a Moving piston and a Valve', Journal of Sound and Vibration, Vol. 241, No. 5, 2001, pp. 895-912 crossref(new window)

Kim, Y. S., and D. J. Lee, 'Computation of Shock-Sound Interaction Using Finite Volume Essentially Nonoscillatory Scheme'. AIAA Journal, Vol. 40, No 6, 2002, pp. 1239-1240 crossref(new window)

C. K. W. Tam, 'Advances in Numerical Boundary Conditions for Computational Aeroacoustics', AIAA Paper 97-1774, 1997, pp. 1-16

Thompson, K. W., 'Time Dependent Boundary Conditions for Hyperbolic Systems', Journal of Computational Physics, Vol. 68, 1987, pp.1-24 crossref(new window)

Thompson, K. W., 'Time Dependent Boundary Conditions for Hyperbolic Systems II', Journal of Computational Physics, Vol. 89, 1990, pp. 439-461 crossref(new window)

Poinsot, T. J. and Lele, S. K., 'Boundary Conditions for Direct Simulations of Compressible Viscous Flow', Journal of Computational Physics. Vol. 101, 1992, pp. 104-129 crossref(new window)