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Analysis of sound propagation in ducts using the wave envelope conceptA finite difference formulation is presented for sound propagation in a rectangular two-dimensional duct without steady flow for plane wave input. Before the difference equations are formulated, the governing Helmholtz equation is first transformed to a form whose solution does not oscillate along the length of the duct. This transformation reduces the required number of grid points by an order of magnitude, and the number of grid points becomes independent of the sound frequency. Physically, the transformed pressure represents the amplitude of the conventional sound wave. Example solutions are presented for sound propagation in a one-dimensional straight hard-wall duct and in a two-dimensional straight soft-wall duct without steady flow. The numerical solutions show evidence of the existence along the duct wall of a developing acoustic pressure diffusion boundary layer which is similar in nature to the conventional viscous flow boundary layer. In order to better illustrate this concept, the wave equation and boundary conditions are written such that the frequency no longer appears explicitly in them. The frequency effects in duct propagation can be visualized solely as an expansion and stretching of the suppressor duct.
Document ID
19740021541
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Baumeister, K. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1974
Subject Category
Fluid Mechanics
Report/Patent Number
E-7941
NASA-TN-D-7719
Report Number: E-7941
Report Number: NASA-TN-D-7719
Accession Number
74N29654
Funding Number(s)
PROJECT: RTOP 501-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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