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Counter-rotating propeller noise directivity and trendsThe effects of power loading on the far field noise spectra and directivity of counter-rotating propellers (CRP) were studied using a model scale SR-2 propeller in a low-speed anechoic wind tunnel. Approximately 264 far field noise measurements were obtained for each CRP configuration (pusher and tractor) and operating conditions covering from 30 to 140 deg to the flight direction and up to 340 deg circumferentially. Data indicated that the CRP tractor produced higher levels in the second and third harmonics which propagated axially; in effect, the noise exposure time increased over that of a single single-rotation propeller. The effects of pylon-to-propeller spacing, type of pylon attachment and reduced rear-blade row radius are considered and it is found that the 0.3 chord radial pylon produces less additional noise than the 0.1 chord radial pylon and that the 0.2 chord tangential pylon is the quietest pusher configuration.
Document ID
19860060680
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Block, P. J. W.
(NASA Langley Research Center Hampton, VA, United States)
Klatte, R. J.
(United Technologies Corp. Hamilton Standard Div., Windsor Locks, CT, United States)
Druez, P. M.
(Douglas Aircraft Co. Long Beach, CA, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1986
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 86-1927
Accession Number
86A45418
Distribution Limits
Public
Copyright
Other

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