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Influence of mean-density gradient on small-scale turbulence noise
Author(s) -
Abbas Khavaran
Publication year - 2000
Publication title -
6th aeroacoustics conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2000-2059
Subject(s) - physics , jet noise , computational physics , turbulence , noise (video) , mach number , mechanics , jet (fluid) , mean flow , taylor microscale , multipole expansion , reynolds number , quantum mechanics , artificial intelligence , computer science , image (mathematics)
A physics-based methodology is described to predict jet-mixing noise due to small-scale turbulence. Both self- and shear-noise source teens of Lilley's equation are modeled and the far-field aerodynamic noise is expressed as an integral over the jet volume of the source multiplied by an appropriate Green's function which accounts for source convection and mean-flow refraction. Our primary interest here is to include transverse gradients of the mean density in the source modeling. It is shown that, in addition to the usual quadrupole type sources which scale to the fourth-power of the acoustic wave number, additional dipole and monopole sources are present that scale to lower powers of wave number. Various two-point correlations are modeled and an approximate solution to noise spectra due to multipole sources of various orders is developed. Mean flow and turbulence information is provided through RANS-k(epsilon) solution. Numerical results are presented for a subsonic jet at a range of temperatures and Mach numbers. Predictions indicated a decrease in high frequency noise with added heat, while changes in the low frequency noise depend on jet velocity and observer angle.

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