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Detailed noise measurements on the SR-7A propeller: Tone behavior with helical tip Mach numberDetailed noise measurements were taken on the SR-7A propeller to investigate the behavior of the noise with helical tip Mach number and then to level off as Mach number was increased further. This behavior was further investigated by obtaining detailed pressure-time histories of data. The pressure-time histories indicate that a portion of the primary pressure pulse is progressively cancelled by a secondary pulse which results in the noise leveling off as the helical tip Mach number is increased. This second pulse appears to originate on the same blade as the primary pulse and is in some way connected to the blade itself. This leaves open the possibility of redesigning the blade to improve the cancellation; thereby, the propeller noise is reduced.
Document ID
19920007487
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dittmar, James H.
(NASA Lewis Research Center Cleveland, OH, United States)
Hall, David G.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Subject Category
Acoustics
Report/Patent Number
NAS 1.15:105206
NASA-TM-105206
E-6519
Report Number: NAS 1.15:105206
Report Number: NASA-TM-105206
Report Number: E-6519
Accession Number
92N16705
Funding Number(s)
PROJECT: RTOP 535-03-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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