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Numerical spatial marching techniques for estimating duct attenuation and source pressure profilesA numerical method was developed that could predict the pressure distribution of a ducted source from far field pressure inputs. Using an initial value formulation, the two-dimensional homogeneous Helmholtz wave equation (no steady flow) was solved using explicit marching techniques. The Von Neumann method was used to develop relationships which describe how sound frequency and grid spacing effect numerical stability. At the present time, stability considerations limit the approach to high frequency sound. Sample calculations for both hard and soft wall ducts compare favorably to known boundary value solutions. In addition, assuming that reflections in the duct are small, this initial value approach was successfully used to determine the attenuation of a straight soft wall duct. Compared to conventional finite difference or finite element boundary value approaches, the numerical marching technique is orders of magnitude shorter in computation time and required computer storage and can be easily employed in problems involving high frequency sound.
Document ID
19780014386
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baumeister, K. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-78857
E-9586
Report Number: NASA-TM-78857
Report Number: E-9586
Meeting Information
Meeting: Meeting of the Acoust. Soc. of Am.
Location: Providence
Start Date: May 16, 1978
End Date: May 19, 1978
Accession Number
78N22329
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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