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Noise generated by quiet engine fans. 3: Fan CA family of fans designed with low noise features was acoustically evaluated, and noise results are documented for a 1.6-pressure-ratio, 472-m/sec (155-ft/sec) tip speed fan. The fan is described and some aerodynamic operating data are given. Far field noise around the fan was measured over a range of operating conditions for a variety of configurations having different arrangements of sound absorbing material in the flow ducts. Complete results of 1.3 octave band analysis of the data are presented in tabular form. Included also are acoustic power spectra and sideline perceived noise levels. Representative 1/3 octave band data are presented graphically, and sample graphs of continuous narrow band spectra are also provided.
Document ID
19760011046
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Montegan, F. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Schaefer, J. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Schmiedlin, R. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-8530
NASA-TM-X-3360
Report Number: E-8530
Report Number: NASA-TM-X-3360
Accession Number
76N18134
Funding Number(s)
PROJECT: RTOP 505-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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