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Liner Optimization Studies Using the Ducted Fan Noise Prediction Code TBIEM3DIn this paper we demonstrate the usefulness of the ducted fan noise prediction code TBIEM3D as a liner optimization design tool. Boundary conditions on the interior duct wall allow for hard walls or a locally reacting liner with axially segmented, circumferentially uniform impedance. Two liner optimization studies are considered in which farfield noise attenuation due to the presence of a liner is maximized by adjusting the liner impedance. In the first example, the dependence of optimal liner impedance on frequency and liner length is examined. Results show that both the optimal impedance and attenuation levels are significantly influenced by liner length and frequency. In the second example, TBIEM3D is used to compare radiated sound pressure levels between optimal and non-optimal liner cases at conditions designed to simulate take-off. It is shown that significant noise reduction is achieved for most of the sound field by selecting the optimal or near optimal liner impedance. Our results also indicate that there is relatively large region of the impedance plane over which optimal or near optimal liner behavior is attainable. This is an important conclusion for the designer since there are variations in liner characteristics due to manufacturing imprecisions.
Document ID
20040090461
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Dunn, M. H.
(Old Dominion Univ. Norfolk, VA, United States)
Farassat, F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1998
Subject Category
Acoustics
Report/Patent Number
AIAA Paper 98-2310
Meeting Information
Meeting: 4th AIAA/CEAS Aeroacoustics Conference
Location: Toulouse
Country: France
Start Date: June 2, 1998
End Date: June 4, 1998
Sponsors: National Oceanic and Atmospheric Administration, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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