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Broadband Fan Noise Prediction System for Turbofan EnginesPratt & Whitney has developed a Broadband Fan Noise Prediction System (BFaNS) for turbofan engines. This system computes the noise generated by turbulence impinging on the leading edges of the fan and fan exit guide vane, and noise generated by boundary-layer turbulence passing over the fan trailing edge. BFaNS has been validated on three fan rigs that were tested during the NASA Advanced Subsonic Technology Program (AST). The predicted noise spectra agreed well with measured data. The predicted effects of fan speed, vane count, and vane sweep also agreed well with measurements. The noise prediction system consists of two computer programs: Setup_BFaNS and BFaNS. Setup_BFaNS converts user-specified geometry and flow-field information into a BFaNS input file. From this input file, BFaNS computes the inlet and aft broadband sound power spectra generated by the fan and FEGV. The output file from BFaNS contains the inlet, aft and total sound power spectra from each noise source. This report is the first volume of a three-volume set documenting the Broadband Fan Noise Prediction System: Volume 1: Setup_BFaNS User s Manual and Developer s Guide; Volume 2: BFaNS User's Manual and Developer s Guide; and Volume 3: Validation and Test Cases. The present volume begins with an overview of the Broadband Fan Noise Prediction System, followed by step-by-step instructions for installing and running Setup_BFaNS. It concludes with technical documentation of the Setup_BFaNS computer program.
Document ID
20110003464
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Morin, Bruce L.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
August 25, 2013
Publication Date
November 1, 2010
Subject Category
Acoustics
Report/Patent Number
E-17477-1
NASA/CR-2010-216898/VOL1
Funding Number(s)
CONTRACT_GRANT: NAS3-27727
WBS: WBS 561581.02.08.03.18.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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