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The acoustic experimental investigation of counterrotating propeller configurationsAn experimental study of scale counterrotating propellers operating in an anechoic facility has been conducted. Various configurations of counterrotation for equal numbers of blades per disk have been tested along with single-rotation propellers, underscoring the fundamental acoustic differences between single and counterrotation propeller operation. In addition it is shown that, as the loading on the counterrotating system is increased, the overall sound-pressure level is also increased in both the disk plane and axial direction.
Document ID
19870061486
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gazzaniga, John A.
(Sverdrup Technology, Inc. Arnold Air Force Station, TN, United States)
Date Acquired
August 13, 2013
Publication Date
April 1, 1987
Subject Category
Acoustics
Report/Patent Number
SAE PAPER 871031
Accession Number
87A48760
Funding Number(s)
CONTRACT_GRANT: NAG3-354
Distribution Limits
Public
Copyright
Other

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