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Noise comparisons from full-scale fan tests at NASA Lewis Research CenterThe overall aero and acoutic design features of eight 6-foot-diameter, single stage fans tested in an outdoor acoustic facility are described. A correlation of the acoustic results for subsonic tip-speed fans showed the total sound power was proportional to the mechanical power imparted to the fan and the specific work performed on the air to within + or - 2 dB. The correlation was relatively insensitive to fan design variables over a broad range of operating conditions. Maximum perceived noise levels were generally proportional to the sound power levels with both noise levels exhibiting a relatively unique increase with fan pressure ratio when normalized by the delivered thrust.
Document ID
19730021936
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Heidmann, M. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Feiler, C. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Physics, General
Report/Patent Number
NASA-TM-X-68289
E-7637
Meeting Information
Meeting: Aero-Acoustics Conf
Location: Seattle, WA
Country: United States
Start Date: October 15, 1973
End Date: October 17, 1973
Sponsors: AIAA
Accession Number
73N30668
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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