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The Prediction of Ducted Fan Engine Noise Via a Boundary Integral Equation MethodA computationally efficient Boundary Integral Equation Method (BIEM) for the prediction of ducted fan engine noise is presented. The key features of the BIEM are its versatility and the ability to compute rapidly any portion of the sound field without the need to compute the entire field. Governing equations for the BIEM are based on the assumptions that all acoustic processes are linear, generate spinning modes, and occur in a uniform flow field. An exterior boundary value problem (BVP) is defined that describes the scattering of incident sound by an engine duct with arbitrary profile. Boundary conditions on the duct walls are derived that allow for passive noise control treatment. The BVP is recast as a system of hypersingular boundary integral equations for the unknown duct surface quantities. BIEM solution methodology is demonstrated for the scattering of incident sound by a thin cylindrical duct with hard walls. Numerical studies are conducted for various engine parameters and continuous portions of the total pressure field are computed. Radiation and duct propagation results obtained are in agreement with the classical results of spinning mode theory for infinite ducts.
Document ID
19960023577
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
M H Dunn
(Old Dominion University Norfolk, Virginia, United States)
J Tweed
(Old Dominion University Norfolk, Virginia, United States)
F Farassat
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 17, 2013
Publication Date
May 6, 1996
Publication Information
Publication: Aeroacoustics Conference
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Acoustics
Report/Patent Number
NASA-TM-111586
NAS 1.15:111586
AIAA-96-1770
Meeting Information
Meeting: 2nd AIAA/CEAS Aeroacoustics Conference
Location: State College, PA
Country: US
Start Date: May 6, 1996
End Date: May 8, 1996
Sponsors: Council of European Aerospace Societies, American Institute of Aeronautics and Astronautics
Accession Number
96N26270
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
Boundary integral equation
Engine noise
Ducted fans
Uniform flow
Numerical integration
Mach numbers
Finite element method
Acoustic impedance
Singular value decomposition
Ducted propellers
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