Effects of Inflow Conditions and Forcing on Subsonic Jet Flows and Noise.

Large-eddy simulations of a circular jet with a Mach number M = 0.9 and a Reynolds number ReD =4 × 10 5 are performed to investigate the effects of the inflow conditions on flow development and the sound field. Three parameters are varied in the jet inflow: the forcing amplitude, the shear-layer thickness, and the use of the first modes in the ring vortex excitation involving several azimuthal modes. The most significant modifications in the jet features are found in the latter case: When the first four azimuthal modes are removed from the forcing, the jet develops much more slowly with reduced turbulence intensities, and the jet is quieter. Moreover, links between the sound levels and the turbulence intensity peaks are observed. The downstream sound levels vary like the peak amplitudes of the centerline turbulence intensity, and the sideline sound levels vary like those of the fluctuating radial velocity in the shear layer.

[1]  Khairul Q. Zaman,et al.  Far-field noise of a subsonic jet under controlled excitation , 1985, Journal of Fluid Mechanics.

[2]  Lyle N. Long,et al.  Numerical Study of Nozzle Exit Condition Effects on Jet Development , 1998 .

[3]  S. Sarkar,et al.  Influence of Nozzle Conditions and Discrete Forcing on Turbulent Planar Jets , 2000 .

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

[5]  A. Michalke Survey on jet instability theory , 1984 .

[6]  Anjaneyulu Krothapalli,et al.  On the use of microjets to suppress turbulence in a Mach 0.9 axisymmetric jet , 2003, Journal of Fluid Mechanics.

[7]  J. Seiner,et al.  On the Two Components of Turbulent Mixing Noise from Supersonic Jets , 1996 .

[8]  Israel J Wygnanski,et al.  Some measurements in the self-preserving jet , 1969, Journal of Fluid Mechanics.

[9]  Geert Brethouwer,et al.  A numerical investigation on the effect of the inflow conditions on the self-similar region of a round jet , 1998 .

[10]  Chih-Ming Ho,et al.  Preferred modes and the spreading rates of jets , 1983 .

[11]  C. Bogey,et al.  A family of low dispersive and low dissipative explicit schemes for flow and noise computations , 2004 .

[12]  Erik Mollo-Christensen,et al.  Experiments on jet flows and jet noise far-field spectra and directivity patterns , 1964, Journal of Fluid Mechanics.

[13]  M. F. Zedan,et al.  Effects of the initial condition on the axisymmetric free shear layer: Effects of the initial momentum thickness , 1978 .

[14]  A. Hussain,et al.  Turbulence structure in the axisymmetric free mixing layer , 1980 .

[15]  Ganesh Raman,et al.  Mode spectra of natural disturbances in a circular jet and the effect of acoustic forcing , 1994 .

[16]  James Bridges,et al.  Roles of initial condition and vortex pairing in jet noise , 1987 .

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

[18]  P. A. Lush,et al.  Measurements of subsonic jet noise and comparison with theory , 1971, Journal of Fluid Mechanics.

[19]  R. A. Antonia,et al.  Effect of different initial conditions on a turbulent round free jet , 2002 .

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

[21]  Richard C. Jenkins,et al.  Effects of the Initial Boundary-Layer State on Turbulent Jet Mixing , 1976 .

[22]  D. G. Crighton,et al.  Acoustics as a branch of fluid mechanics , 1981, Journal of Fluid Mechanics.

[23]  Christophe Bailly,et al.  Decrease of the Effective Reynolds Number with Eddy-Viscosity Subgrid-Scale Modeling , 2005 .

[24]  Satish Narayanan,et al.  Aeroacoustic Characterization, Noise Reduction, and Dimensional Scaling Effects of High Subsonic Jets , 2001 .

[25]  C. Bogey Three-dimensional non-refrective boundary conditions for acoustic simulation : far field formulation and validation test cases , 2002 .

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

[27]  Khairul Q. Zaman,et al.  Flow field and near and far sound field of a subsonic jet , 1986 .

[28]  A. Hussain,et al.  Axisymmetric mixing layer: Influence of the initial and boundary conditions , 1979 .

[29]  L. Maestrello Two‐point correlations of sound pressure in the far‐field of a jet: experiment , 1976 .