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Optimal one-section and two-section circular sound-absorbing duct liners for plane-wave and monopole sources without flowA discrete frequency study is made of the influence of source characteristics on the optimal properties of acoustically lined uniform and two section ducts. Two simplified sources, a plane wave and a monopole, are considered in some detail and over a greater frequency range than has been previously studied. Source and termination impedance effects are given limited examination. An example of a turbomachinery source and three associated source variants is also presented. Optimal liner designs based on modal theory approach the Cremer criterion at low frequencies and the geometric acoustics limit at high frequencies. Over an intermediate frequency range, optimal two section liners produced higher transmission losses than did the uniform configurations. Source distribution effects were found to have a significant effect on optimal liner design, but source and termination impedance effects appear to be relatively unimportant.
Document ID
19770008847
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Lester, H. C.
(NASA Langley Research Center Hampton, VA, United States)
Posey, J. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1976
Subject Category
Acoustics
Report/Patent Number
L-11039
NASA-TN-D-8348
Report Number: L-11039
Report Number: NASA-TN-D-8348
Accession Number
77N15790
Funding Number(s)
PROJECT: RTOP 505-03-11-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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