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Aircraft Noise Prediction Program (ANOPP) Fan Noise Prediction for Small EnginesThe Fan Noise Module of ANOPP is used to predict the broadband noise and pure tones for axial flow compressors or fans. The module, based on the method developed by M. F. Heidmann, uses empirical functions to predict fan noise spectra as a function of frequency and polar directivity. Previous studies have determined the need to modify the module to better correlate measurements of fan noise from engines in the 3000- to 6000-pound thrust class. Additional measurements made by AlliedSignal have confirmed the need to revise the ANOPP fan noise method for smaller engines. This report describes the revisions to the fan noise method which have been verified with measured data from three separate AlliedSignal fan engines. Comparisons of the revised prediction show a significant improvement in overall and spectral noise predictions.
Document ID
19960042711
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Hough, Joe W.
(Allied-Signal Corp. Phoenix, AZ United States)
Weir, Donald S.
(Allied-Signal Corp. Phoenix, AZ United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1996
Subject Category
Acoustics
Report/Patent Number
NASA-CR-198300
NAS 1.26-198300
Report Number: NASA-CR-198300
Report Number: NAS 1.26-198300
Accession Number
96N31662
Funding Number(s)
PROJECT: RTOP 538-03-11-01
CONTRACT_GRANT: NAS1-20102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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