NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Fan Noise SuppressionThe principal suppressor parameters and their relationships have been used to formulate a suppressor design methodology which has been applied to the design of several full-scale suppressors. Tests of these suppressors on several full-scale fans have demonstrated noise reductions of the order of 10 PNdB. The amount of suppression in several instances seems to have been limited by reaching noise floors that are not clearly at the estimated jet noise level but are not far above it. In addition to identifying noise floors, two other areas are considered. The first is attenuation by the fan exhaust suppressors, which seems in most cases to be less than that of the inlet. The second is the effectiveness of outer cowl treatment alone on multiple pure tones. This question relates to whether a high-speed fan can become as quiet as a low-speed fan without a substantial increase in the amount of treatment.
Document ID
19730003288
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Charles E Feiler
(Glenn Research Center Cleveland, United States)
John F Groeneweg
(Glenn Research Center Cleveland, United States)
Edward J Rice
(Glenn Research Center Cleveland, United States)
Edward B Smith
(General Electric Company)
R H Tucker
(The Boeing Company)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Publication Information
Publication: Aircraft Engine Noise Reduction
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft
Meeting Information
Meeting: Aircraft Engine Noise Reduction
Location: Cleveland, OH
Country: US
Start Date: May 16, 1972
End Date: May 17, 1972
Sponsors: National Aeronautics and Space Administration
Accession Number
73N12015
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available