Using large eddy simulation to explore sound-source mechanisms in jets

Abstract This paper presents an analysis of data generated by means of large eddy simulation for a single-stream, isothermal Mach 0.9 jet. The acoustic field is decomposed into Fourier modes in the azimuthal direction, and filtered by means of a continuous wavelet transform in the temporal direction. This allows the identification of temporally localised, high-amplitude events in the radiated sound field for each of the azimuthal modes. Once these events have been localised, the flow field is analysed so as to determine their cause. Results show high-amplitude, intermittent sound radiation for azimuthal modes 0 and 1. The mode-0 radiation, which dominates low-angle emission, is found to result from the temporal modulation of a basic axisymmetric wave-packet structure within the flow. Similar intermittent activity, observed, again within the flow, for azimuthal mode 1 suggests a link between the modes 0 and 1 dynamics. Both the amplitude and spatial extent of the axisymmetric wave-packet are modulated, and the strongest axisymmetric propagative disturbances are found to radiate from the downstream end of the wave-packet at moments when the wave envelope becomes truncated. The observed behaviour is modelled using a line-source wave-packet ansatz which includes parameters that account for the said modulation. Inclusion of these parameters, which allow the wave-packet to “jitter” in a manner similar to that observed, leads to good quantitative agreement (accurate to within 1.5 dB), at low emission angles, with the acoustic field of the LES. This result is in contrast with results obtained using a time-averaged wave-packet (one which does not jitter), for which a 12 dB error is observed. This result shows that the said modulations are the salient source feature for the low-angle sound emission of the jet considered. Analysis of a longer time series shows the occurrence of several similar high-amplitude bursts in the axisymmetric mode of the acoustic pressure, and a calculation of the radiated sound for this longer time-series, again using the wave-packet ansatz , once again leads to good agreement with the LES (now accurate to within 1 dB).

[1]  C. Bogey,et al.  Noise Investigation of a High Subsonic, Moderate Reynolds Number Jet Using a Compressible Large Eddy Simulation , 2003 .

[2]  N. Sandham,et al.  Sound radiation from exponentially growing and decaying surface waves , 2006 .

[3]  James I. Hileman,et al.  Comparison of Noise Mechanisms in High and Low Reynolds Number High-Speed Jets , 2006 .

[4]  P. Moin,et al.  Boundary conditions for direct computation of aerodynamic sound generation , 1993 .

[5]  Christophe Bailly,et al.  Effects of Inflow Conditions and Forcing on Subsonic Jet Flows and Noise. , 2005 .

[6]  J. Hileman,et al.  Large-scale structure evolution and sound emission in high-speed jets: real-time visualization with simultaneous acoustic measurements , 2005, Journal of Fluid Mechanics.

[7]  D. G. Crighton,et al.  Basic principles of aerodynamic noise generation , 1975 .

[8]  Christophe Bailly,et al.  Computation of a high Reynolds number jet and its radiated noise using large eddy simulation based on explicit filtering , 2006 .

[9]  D. Bodony Aeroacoustic prediction of turbulent free shear flows , 2004 .

[10]  Tim Colonius,et al.  Temporal-Harmonic Specific POD Mode Extraction , 2008 .

[11]  Daniel Juvé,et al.  Intermittency of the noise emission in subsonic cold jets , 1980 .

[12]  M. Lighthill On sound generated aerodynamically I. General theory , 1952, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[13]  Eli Turkel,et al.  High order accurate solutions of viscous problems , 1993 .

[14]  Philip J. Morris,et al.  Measurements in subsonic and supersonic free jets using a laser velocimeter , 1979, Journal of Fluid Mechanics.

[15]  Luc Vervisch,et al.  Three-dimensional boundary conditions for direct and large-eddy simulation of compressible viscous flows , 2008, J. Comput. Phys..

[16]  Sanjiva K. Lele,et al.  On using large-eddy simulation for the prediction of noise from cold and heated turbulent jets , 2005 .

[17]  H. K. Tanna,et al.  An experimental study of jet noise part I: Turbulent mixing noise , 1977 .

[18]  Eli Turkel,et al.  Dissipative two-four methods for time-dependent problems , 1976 .

[19]  Phased Array Models of Shock-cell Noise Sources , 2005 .

[20]  James Bridges,et al.  Effect of Heat on Space-Time Correlations in Jets , 2013 .

[21]  C. Tinney,et al.  The near pressure field of co-axial subsonic jets , 2008, Journal of Fluid Mechanics.

[22]  J. Bendat,et al.  Random Data: Analysis and Measurement Procedures , 1971 .

[23]  Roberto Camussi,et al.  ACOUSTIC IDENTIFICATION OF COHERENT STRUCTURES IN A TURBULENT JET , 2003 .

[24]  Lars-Erik Eriksson,et al.  Investigation of an Isothermal Mach 0.75 Jet and its Radiated sound Using Large-Eddy Simulation and Kirchhoff Surface Integration , 2005 .

[25]  Mingjun Wei,et al.  Intermittent sound generation and its control in a free-shear flow , 2010 .

[26]  J. Freund Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9 , 2001, Journal of Fluid Mechanics.

[27]  J. Freund,et al.  A noise-controlled free shear flow , 2005, Journal of Fluid Mechanics.

[28]  M. Lesieur,et al.  Large-eddy simulation of transition to turbulence in a boundary layer developing spatially over a flat plate , 1996, Journal of Fluid Mechanics.

[29]  Favre filtering and macro-temperature in large-eddy simulations of compressible turbulence , 2001 .

[30]  Y. Gervais,et al.  Jittering wave-packet models for subsonic jet noise , 2010 .