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Measurement of acoustic modes and wall impedance in a turbofan exhaust ductAcoustic measurements made with in-duct modal probes show how individual acoustic modes, as generated by fan/stator interaction, interact with a well-characterized liner. This measured attenuation provides a critical test for predicted attenuation as developed from the theoretical analysis of sound propagation in annular ducts with treatment and sheared flow. The primary investigations took place in the exhaust duct of a model fan mounted in an anechoic chamber. The results presented include induct attenuation, sound power attenuation as measured in the far field, and in-situ acoustic impedance measurements of the treated wall sections. Good theory/experiment agreement was found; the differences of treatment suppression between theory and measured values differed at most by 2.7 dB.
Document ID
19830046797
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fiske, G. H.
(General Electric Co. Schenectady, NY, United States)
Syed, A. A.
(General Electric Co. Schenectady, NY, United States)
Motsinger, R. E.
(General Electric Co., Aircraft Engine Group, Cincinnati OH, United States)
Joshi, M. C.
(General Electric Co. Schenectady, NY, United States)
Kraft, R. E.
(Douglas Aircraft Co. Long Beach, CA, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1983
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 83-0733
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
83A28015
Distribution Limits
Public
Copyright
Other

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