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Effect of rotor-to-stator spacing on acoustic performance of a full-scale fan (QF-5) for turbofan enginesA study was made of the effect of increasing the fan rotor-to-stator spacing on the noise level of a full-scale, single-stage, 1.6-pressure-ratio fan. Noise data were obtained with axial spacing of 1.14, 1.65, and 2.27 rotor chord lengths. Over this spacing range, data indicate a reduction of 1.5 PNdb. Apparently, rotor-alone noise at the frequency at which the rotor-stator interaction noise was cut off limited the noise reduction for the QF-5 fan. It seems, however, that the reduction in sound power level with increases in spacing is potentially about 6 db over the range of spacing tested.
Document ID
19740025326
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Balombin, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Stakolich, E. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-3103
E-7879
Report Number: NASA-TM-X-3103
Report Number: E-7879
Accession Number
74N33439
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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