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A Computing Method for Sound Propagation Through a Nonuniform Jet StreamUnderstanding the principles of jet noise propagation is an essential ingredient of systematic noise reduction research. High speed computer methods offer a unique potential for dealing with complex real life physical systems whereas analytical solutions are restricted to sophisticated idealized models. The classical formulation of sound propagation through a jet flow was found to be inadequate for computer solutions and a more suitable approach was needed. Previous investigations selected the phase and amplitude of the acoustic pressure as dependent variables requiring the solution of a system of nonlinear algebraic equations. The nonlinearities complicated both the analysis and the computation. A reformulation of the convective wave equation in terms of a new set of dependent variables is developed with a special emphasis on its suitability for numerical solutions on fast computers. The technique is very attractive because the resulting equations are linear in nonwaving variables. The computer solution to such a linear system of algebraic equations may be obtained by well-defined and direct means which are conservative of computer time and storage space. Typical examples are illustrated and computational results are compared with available numerical and experimental data.
Document ID
19750002287
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Padula, S. L.
(NASA Langley Research Center Hampton, VA, United States)
Liu, C. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-X-71941
Report Number: NASA-TM-X-71941
Accession Number
75N10359
Funding Number(s)
PROJECT: RTOP 505-03-12-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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