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Curved Duct Noise Prediction Using the Fast Scattering CodeResults of a study to validate the Fast Scattering Code (FSC) as a duct noise predictor, including the effects of curvature, finite impedance on the walls, and uniform background flow, are presented in this paper. Infinite duct theory was used to generate the modal content of the sound propagating within the duct. Liner effects were incorporated via a sound absorbing boundary condition on the scattering surfaces. Simulations for a rectangular duct of constant cross-sectional area have been compared to analytical solutions and experimental data. Comparisons with analytical results indicate that the code can properly calculate a given dominant mode for hardwall surfaces. Simulated acoustic behavior in the presence of lined walls (using hardwall duct modes as incident sound) is consistent with expected trends. Duct curvature was found to enhance weaker modes and reduce pressure amplitude. Agreement between simulated and experimental results for a straight duct with hard walls (no flow) was excellent.
Document ID
20070021693
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Dunn, M. H.
(NASA Langley Research Center Hampton, VA, United States)
Tinetti, Ana F.
(NASA Langley Research Center Hampton, VA, United States)
Farassat, F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 23, 2013
Publication Date
May 21, 2007
Subject Category
Acoustics
Report/Patent Number
AIAA 2007-3528
Report Number: AIAA 2007-3528
Meeting Information
Meeting: 13th AIAA/CEAS Aeroacoustics Conference
Location: Rome
Country: Italy
Start Date: May 21, 2007
End Date: May 23, 2007
Sponsors: American Inst. of Aeronautics and Astronautics, National Oceanic and Atmospheric Administration
Funding Number(s)
WBS: WBS 561581.02.08.07
Distribution Limits
Public
Copyright
Public Use Permitted.
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