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Source Methodology for Turbofan Noise Prediction (SOURCE3D Technical Documentation)This report provides the analytical documentation for the SOURCE3D Rotor Wake/Stator Interaction Code. It derives the equations for the rotor scattering coefficients and stator source vector and scattering coefficients that are needed for use in the TFANS (Theoretical Fan Noise Design/Prediction System). SOURCE3D treats the rotor and stator as isolated source elements. TFANS uses this information, along with scattering coefficients for inlet and exit elements, and provides complete noise solutions for turbofan engines. SOURCE3D is composed of a collection of FORTRAN programs that have been obtained by extending the approach of the earlier V072 Rotor Wake/Stator Interaction Code. Similar to V072, it treats the rotor and stator as a collection of blades and vanes having zero thickness and camber contained in an infinite, hardwall annular duct. SOURCE3D adds important features to the V072 capability-a rotor element, swirl flow and vorticity waves, actuator disks for flow turning, and combined rotor/actuator disk and stator/actuator disk elements. These items allow reflections from the rotor, frequency scattering, and mode trapping, thus providing more complete noise predictions than previously. The code has been thoroughly verified through comparison with D.B. Hanson's CUP2D two- dimensional code using a narrow annulus test case.
Document ID
19990028361
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Meyer, Harold D.
(United Technologies Corp. Windsor Locks, CT United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1999
Subject Category
Acoustics
Report/Patent Number
NASA/CR-1999-208877
E-11581
PWA-6420-104
NAS 1.26:208877
Report Number: NASA/CR-1999-208877
Report Number: E-11581
Report Number: PWA-6420-104
Report Number: NAS 1.26:208877
Funding Number(s)
PROJECT: RTOP 538-03-11
CONTRACT_GRANT: NAS3-26618
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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