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Circumferentially segmented duct lines optimized for axisymmetric and standing wave sourcesOptimum and off-optimum properties of circumferentially segmented duct liners are compared with those of uniform liners to identify any potential benefits of circumferentially segmented liners. High- and low-order spinning-mode sources are considered in the study. The solution for the segmented liner is obtained by a multimodal expansion of the segmented-liner eigenmodes in terms of a series of hardwall duct models. The coefficients in the hard-wall series are obtained by using Galerkin's method. Results show that for some frequencies and duct lengths, circumferentially segmented liners scatter energy equally between a higher and lower order circumferential wave number. Studies for higher order spinning-mode sources show that an optimized segmented liner with a hard-wall/soft-wal admittance variation representing an optimum configuration gives better performance than an optimized uniform liner. Overall, the greatest benefit of the segmented liner over the uniform liner occurs under off-optimum conditions. The optimized segmented liner gives more effective broadband performance than the optimized uniform liner.
Document ID
19820026314
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Watson, W. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Acoustics
Report/Patent Number
NASA-TP-2075
L-15316
NAS 1.60:2075
Report Number: NASA-TP-2075
Report Number: L-15316
Report Number: NAS 1.60:2075
Accession Number
82N34190
Funding Number(s)
PROJECT: RTOP 505-32-03-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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