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Influence of Mean-Density Gradient on Small-Scale Turbulence NoiseA 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.
Document ID
20000062459
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Khavaran, Abbas
(DYNACS Engineering Co., Inc. Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2000
Subject Category
Acoustics
Report/Patent Number
NASA/CR-2000-210226
NAS 1.26:210226
E-12346
AIAA Paper 2000-2059
Meeting Information
Meeting: Aeroacoustics
Location: Lahaina, HI
Country: United States
Start Date: June 12, 2000
End Date: June 14, 2000
Sponsors: Confederation of European Aerospace Societies, American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 523-90-43
CONTRACT_GRANT: NAS3-98008
Distribution Limits
Public
Copyright
Public Use Permitted.
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