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Modeling Sound Propagation Through Non-Axisymmetric Jets A method for computing the far-field adjoint Green's function of the generalized acoustic analogy equations under a locally parallel mean flow approximation is presented. The method is based on expanding the mean-flow-dependent coefficients in the governing equation and the scalar Green's function in truncated Fourier series in the azimuthal direction and a finite difference approximation in the radial direction in circular cylindrical coordinates. The combined spectral/finite difference method yields a highly banded system of algebraic equations that can be efficiently solved using a standard sparse system solver. The method is applied to test cases, with mean flow specified by analytical functions, corresponding to two noise reduction concepts of current interest: the offset jet and the fluid shield. Sample results for the Green's function are given for these two test cases and recommendations made as to the use of the method as part of a RANS-based jet noise prediction code.
Document ID
20140012697
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Leib, Stewart J.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 29, 2014
Publication Date
March 1, 2014
Subject Category
Acoustics
Aerodynamics
Report/Patent Number
NASA/CR-2014-218107
E-18827
Funding Number(s)
WBS: WBS 984754.02.07.03.17.06
CONTRACT_GRANT: NNC07BA13B
Distribution Limits
Public
Copyright
Public Use Permitted.
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