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Optimization of suppression for two-element treatment liners for turbomachinery exhaust ductsSound wave propagation in a soft-walled rectangular duct with steady uniform flow was investigated at exhaust conditions, incorporating the solution equations for sound wave propagation in a rectangular duct with multiple longitudinal wall treatment segments. Modal analysis was employed to find the solution equations and to study the effectiveness of a uniform and of a two-sectional liner in attenuating sound power in a treated rectangular duct without flow (M = 0) and with uniform flow of Mach 0.3. Two-segment liners were shown to increase the attenuation of sound as compared to a uniform liner. The predicted sound attenuation was compared with measured laboratory results for an optimized two-segment suppressor. Good correlation was obtained between the measured and predicted suppressions when practical variations in the modal content and impedance were taken into account. Two parametric studies were also completed.
Document ID
19760017907
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Motsinger, R. E.
(General Electric Co. Cincinnati, OH, United States)
Kraft, R. E.
(General Electric Co. Cincinnati, OH, United States)
Zwick, J. W.
(General Electric Co. Cincinnati, OH, United States)
Vukelich, S. I.
(General Electric Co. Cincinnati, OH, United States)
Minner, G. L.
(General Electric Co. Cincinnati, OH, United States)
Baumeister, K. J.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Acoustics
Report/Patent Number
R76AEG256
NASA-CR-134997
Report Number: R76AEG256
Report Number: NASA-CR-134997
Accession Number
76N24995
Funding Number(s)
CONTRACT_GRANT: NAS3-18555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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