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Improved NASA-ANOPP Noise Prediction Computer Code for Advanced Subsonic Propulsion Systems: Fan Suppression Model Development - Volume 2The Aircraft Noise Predication Program (ANOPP) is an industry-wide tool used to predict turbofan engine flyover noise in system noise optimization studies. Its goal is to provide the best currently available methods for source noise prediction. As part of a program to improve the Heidmann fan noise model, models for fan inlet and fan exhaust noise suppression estimation that are based on simple engine and acoustic geometry inputs have been developed. The models can be used to predict sound power level suppression and sound pressure level suppression at a position specified relative to the engine inlet.
Document ID
19970005047
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kontos, Karen B.
(General Electric Co. Cincinnati, OH United States)
Kraft, Robert E.
(General Electric Co. Cincinnati, OH United States)
Gliebe, Philip R.
(General Electric Co. Cincinnati, OH United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1996
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:202309
NASA-CR-202309
E-10595
Report Number: NAS 1.26:202309
Report Number: NASA-CR-202309
Report Number: E-10595
Accession Number
97N13033
Funding Number(s)
CONTRACT_GRANT: NAS3-26617
PROJECT: RTOP 538-08-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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