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The Detection of Radiated Modes from Ducted Fan EnginesThe bypass duct of an aircraft engine is a low-pass filter allowing some spinning modes to radiate outside the duct. The knowledge of the radiated modes can help in noise reduction, as well as the diagnosis of noise generation mechanisms inside the duct. We propose a nonintrusive technique using a circular microphone array outside the engine measuring the complex noise spectrum on an arc of a circle. The array is placed at various axial distances from the inlet or the exhaust of the engine. Using a model of noise radiation from the duct, an overdetermined system of linear equations is constructed for the complex amplitudes of the radial modes for a fixed circumferential mode. This system of linear equations is generally singular, indicating that the problem is illposed. Tikhonov regularization is employed to solve this system of equations for the unknown amplitudes of the radiated modes. An application of our mode detection technique using measured acoustic data from a circular microphone array is presented. We show that this technique can reliably detect radiated modes with the possible exception of modes very close to cut-off.
Document ID
20010049386
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Farassat, F.
(NASA Langley Research Center Hampton, VA United States)
Nark, Douglas M.
(NASA Langley Research Center Hampton, VA United States)
Thomas, Russell H.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA Paper 2001-2138
Meeting Information
Meeting: 7th AIAA/CEAS Aeroacoustics Conference
Location: Maastricht
Country: Netherlands
Start Date: May 28, 2001
End Date: May 30, 2001
Sponsors: American Inst. of Aeronautics and Astronautics, Confederation of European Aerospace Societies
Distribution Limits
Public
Copyright
Public Use Permitted.
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