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Turbine noise generation and suppressionAn analytical method for the prediction of turbine generated noise is discussed. The method links the duct acoustic modes with the turbomachinery aerodynamics. The results of the analysis are compared with turbine component and engine results. Component data on the effects of the variation of axial spacing between blade rows on turbine aerodynamics and acoustics are presented. The results of an experimental evaluation of the relative importance of turbine noise on highly suppressed bypass turbofans are discussed. The development of high temperature acoustic treatment and its application to high bypass turbofans are presented.
Document ID
19740030548
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Benzakein, M. J.
Smith, E. B.
(General Electric Co. Cincinnati, Ohio, United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
ASME PAPER 73-WA/GT-7
Report Number: ASME PAPER 73-WA/GT-7
Meeting Information
Meeting: Winter Annual Meeting
Location: Detroit, MI
Start Date: November 11, 1973
End Date: November 15, 1973
Sponsors: American Society of Mechanical Engineers
Accession Number
74A13298
Funding Number(s)
CONTRACT_GRANT: DOT-FA-SS71-13
CONTRACT_GRANT: DOT-FA72WA-3023
CONTRACT_GRANT: NAS3-12430
Distribution Limits
Public
Copyright
Other

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