NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Aeroacoustic Analysis of Turbofan Noise GenerationThis report provides an updated version of analytical documentation for the V072 Rotor Wake/Stator Interaction Code. It presents the theoretical derivation of the equations used in the code and, where necessary, it documents the enhancements and changes made to the original code since its first release. V072 is a package of FORTRAN computer programs which calculate the in-duct acoustic modes excited by a fan/stator stage operating in a subsonic mean flow. Sound is generated by the stator vanes interacting with the mean wakes of the rotor blades. In this updated version, only the tonal noise produced at the blade passing frequency and its harmonics, is described. The broadband noise component analysis, which was part of the original report, is not included here. The code provides outputs of modal pressure and power amplitudes generated by the rotor-wake/stator interaction. The rotor/stator stage is modeled as an ensemble of blades and vanes of zero camber and thickness enclosed within an infinite hard-walled annular duct. The amplitude of each propagating mode is computed and summed to obtain the harmonics of sound power flux within the duct for both upstream and downstream propagating modes.
Document ID
19960021098
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Meyer, Harold D.
(United Technologies Corp. Windsor Locks, CT United States)
Envia, Edmane
(NYMA, Inc. Brook Park, OH United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:4715
E-10148
NASA-CR-4715
Accession Number
96N24573
Funding Number(s)
CONTRACT_GRANT: NAS3-26618
CONTRACT_GRANT: NAS3-27186
PROJECT: RTOP 538-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available