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Effects of inflow distortion profiles on fan tone noise calculated using a 3-D theoryCalculations of the fan tone acoustic power and modal structure generated by complex distortions in axial inflow velocity are presented. The model used treats the rotor as a rotating three-dimensional cascade and calculates the acoustic field from the distortion-produced dipole distribution on the blades including noncompact source effects. Radial and circumferential distortion shapes are synthesized from Fourier-Bessel components representing individual distortion modes. The relation between individual distortion modes and the generated acoustic modes is examined for particular distortion cases. Comparisons between theoretical and experimental results for distortions produced by wakes from upstream radial rods show that the analysis is a good predictor of acoustic power dependence on disturbance strength.
Document ID
19790042898
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kobayshi, H.
(NASA Lewis Research Center Cleveland, Ohio; National Aerospace Laboratory, Tokyo, Japan)
Groeneweg, J. F.
(NASA Lewis Research Center Turbomachinery Noise Section, Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 79-0577
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aeroacoustics Conference
Location: Seattle, WA
Start Date: March 12, 1979
End Date: March 14, 1979
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
79A26911
Distribution Limits
Public
Copyright
Other

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