Power spectral density of subsonic jet noise

Abstract The scaling of the power scaling density (PSD) of the far field noise for subsonic, unheated, axisymmetric jets has been examined based on data obtained from the literature as well as from new experiments. It has been demonstrated that the PSD scales as the Strouhal number (StD) alone for most locations, except at shalloow angles (θ

[1]  Khairul Q. Zaman,et al.  Taylor hypothesis and large-scale coherent structures , 1981, Journal of Fluid Mechanics.

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

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

[4]  P. Deneuville,et al.  Jet noise amplification - A practically important problem , 1977 .

[5]  S. Crow,et al.  Orderly structure in jet turbulence , 1971, Journal of Fluid Mechanics.

[6]  F. Browand,et al.  The Roles of Large Scale Structures in the Initial Development of Circular Jets , 1975 .

[7]  Georges Elias,et al.  Coherent structures in the mixing zone of A subsonic hot free jet , 1978 .

[8]  Khairul Q. Zaman,et al.  Vortex pairing in a circular jet under controlled excitation. Part 2. Coherent structure dynamics , 1980, Journal of Fluid Mechanics.

[9]  R. Arndt,et al.  Jet noise at low Reynolds number , 1981 .

[10]  H. S. Ribner,et al.  “Basic” jet noise patterns after deletion of convection and refraction effects: Experiments vs. Theory , 1973 .

[11]  Helmut V. Fuchs,et al.  Coherent Structures in Jet Turbulence and Noise , 1977 .

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

[13]  B. Jubelin New experimental studies on jet noise amplification , 1980 .

[14]  H. S. Ribner,et al.  Perspectives on Jet Noise , 1981 .

[15]  R. Arndt,et al.  Jet noise at low Reynolds number , 1981 .

[16]  Helmut V. Fuchs,et al.  Experimental Evidence of Turbulent Source Coherence Affecting Jet Noise , 1978 .

[17]  H. K. Tanna,et al.  The influence of temperature on shock-free supersonic jet noise , 1975 .

[18]  H. Fuchs,et al.  Experimental evidence of turbulent source coherence effecting jet noise , 1977 .

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

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

[21]  Krishan K. Ahuja,et al.  An experimental study of subsonic jet noise and comparison with theory , 1973 .

[22]  Khairul Q. Zaman,et al.  The ‘preferred mode’ of the axisymmetric jet , 1981, Journal of Fluid Mechanics.

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

[24]  A. Michalke,et al.  Some remarks on source coherence affecting jet noise , 1983 .

[25]  R. Narasimha,et al.  Sound emission from jets at high subsonic velocities , 1960, Journal of Fluid Mechanics.

[26]  C. J. Moore The role of shear-layer instability waves in jet exhaust noise , 1977, Journal of Fluid Mechanics.

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

[28]  H. Fuchs,et al.  Turbulent source coherence and Helmholtz number as aerodynamic noise parameters , 1978 .

[29]  C. L. Morfey,et al.  Developments in jet noise modelling—theoretical predictions and comparisons with measured data , 1976 .

[30]  H. Bass,et al.  Atmospheric absorption of high frequency noise and application to fractional-octave bands , 1977 .

[31]  Christopher K. W. Tam,et al.  Tone-excited jet: Theory and experiments , 1982 .

[32]  E. Pfizenmaier,et al.  The amplification of broadband jet noise by pure tone excitation , 1976 .

[33]  E. Pfizenmaier,et al.  On the amplification of broad band jet noise by a pure tone excitation , 1975 .

[34]  Khairul Q. Zaman,et al.  Vortex pairing in a circular jet under controlled excitation. Part 1. General jet response , 1980, Journal of Fluid Mechanics.