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Interaction of rotor tip flow irregularities with stator vanes as a noise sourceThe role of the interaction of rotor tip flow irregularities (vortices and velocity defects) with downstream stator vanes is discussed as a possible fan noise mechanism. This is accomplished by: (1) indicating some of the mothods of formation of these flow irregularities; (2) observing how they would behave with respect to known noise behavior; and (3) attempting to compare the strength of the rotor tip flow irregularity mechanism with the strength of the more common rotor wake-stator mechanism. The rotor tip flow irregularity-stator interaction is indicated as being a probable inflight noise source.
Document ID
19770025212
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dittmar, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-73706
Report Number: NASA-TM-73706
Meeting Information
Meeting: Aeroacoustics Conf.
Location: Atlanta
Start Date: October 3, 1977
End Date: October 5, 1977
Sponsors: AIAA
Accession Number
77N32156
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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