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Fan noise reduction achieved by removing tip flow irregularities behind the rotor - forward arc test configurationsThe noise source caused by the interaction of the rotor tip flow irregularities (vortices and velocity defects) with the downstream stator vanes was studied. Fan flow was removed behind a 0.508 meter (20 in.) diameter model turbofan through an outer wall slot between the rotor and stator. Noise measurements were made with far-field microphones positioned in an arc about the fan inlet and with a pressure transducer in the duct behind the stator. Little tone noise reduction was observed in the forward arc during flow removal; possibly because the rotor-stator interaction noise did not propagate upstream through the rotor. Noise reductions were maded in the duct behind the stator and the largest decrease occurred with the first increment of flow removal. This result indicates that the rotor tip flow irregularity-stator interaction is as important a noise producing mechanism as the normally considered rotor wake-stator interaction.
Document ID
19840015167
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dittmar, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Woodward, R. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Mackinnon, M. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Acoustics
Report/Patent Number
NASA-TM-83616
E-2047
NAS 1.15:83616
Report Number: NASA-TM-83616
Report Number: E-2047
Report Number: NAS 1.15:83616
Meeting Information
Meeting: Meeting of the Acoustical Soc. of Am.
Location: Norfolk, VA
Country: United States
Start Date: May 7, 1984
End Date: May 10, 1984
Accession Number
84N23235
Funding Number(s)
PROJECT: RTOP 505-31-3B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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