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Influence of blade characteristics on axial flow compressor noiseThis experimental study was initiated as a result of earlier theoretical work which found that changes in the spanwise circulation distribution can have a significant influence on noise generation for the single rotor and for rotor-stator combinations. The experimental results presented here clearly show that the rotor noise, and especially the rotor-stator interaction noise, is affected by the type of radial loading, i.e., type of twist. Other blade parameters tested for their influence on far-field noise include rotor solidity, spacing between rotor and stator for twisted and untwisted blades, blade thickness, and stator chord length; radial effects on cutoff were also investigated.
Document ID
19760055118
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lumsdaine, E.
(Tennessee Univ. Knoxville, TN, United States)
Cherng, J. G.
(Tennessee, University Knoxville, Tenn., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 76-570
Meeting Information
Meeting: Aero-Acoustics Conference
Location: Palo Alto, CA
Start Date: July 20, 1976
End Date: July 23, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A38084
Funding Number(s)
CONTRACT_GRANT: NGR-43-001-134
Distribution Limits
Public
Copyright
Other

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