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Sound propagation in segmented exhaust ducts - Theoretical predictions and comparison with measurementsSuppressions due to acoustic treatment in the annular exhaust duct of a model fan have been theoretically predicted and compared with measurements. The predictions are based on the modal analysis of sound propagation in a straight annular flow duct with segmented treatment. Measured values of the mode distribution of the fan noise source (fan-stator interaction source only) and the acoustic impedance of the treatment in the duct were used as input to the prediction program. The predicted suppressions (under the assumption of uniform flow in the duct) compared well with the measured in-duct suppression for all test conditions. The measurements were made in an anechoic chamber and the interaction modes generated in the fan spanned a cut-off ratio range from nearly one to seven.
Document ID
19830046798
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Joshi, M. C.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Kraft, R. E.
(Douglas Aircraft Co. Long Beach, CA, United States)
Fiske, G. H.
(General Electric Co. Schenectady, NY, United States)
Syed, A. A.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Motsinger, R. E.
(General Electric Co. Evendale, OH, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1983
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 83-0734
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aeroacoustics Conference
Location: Atlanta, GA
Start Date: April 11, 1983
End Date: April 13, 1983
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
83A28016
Funding Number(s)
CONTRACT_GRANT: NAS3-22766
Distribution Limits
Public
Copyright
Other

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