NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Pusher propeller noise directivity and trendsThe effects of pylon wake interaction on far-field propeller noise are studied using a model scale SR-2 propeller in a low-speed anechoic wind tunnel. The variation in the pusher noise penalty with axial angle theta and circumferential angle phi is compared to that of the tractor noise penalty; and the former exhibits minima occurring in the propeller plane and maxima occurring toward the propeller axis. The magnitude of the pusher installation noise penalty decreased with in increase in shaft horsepower and tip Mach number. Directivity comparisons revealed that both a noise reduction and a directivity pattern change resulted when the pylon was moved farther from the propeller. Noise emerging from the wake interaction was distinguished from that of the propeller by means of a modal decomposition.
Document ID
19860060682
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Block, P. J. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1986
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 86-1929
Accession Number
86A45420
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available