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Single Mode Theory for Impedance Eduction in Large-Scale Ducts with Grazing FlowAn impedance eduction theory for a rigid wall duct containing an acoustic liner with an unknown impedance and uniform grazing flow is presented. The unique features of the theory are: 1) non-planar waves propagate in the hard wall sections of the duct, 2) input data consist solely of complex acoustic pressures acquired on a wall adjacent to the liner, and 3) multiple higher-order modes may exist in the direction perpendicular to the liner and the opposite rigid wall. The approach is to first measure the axial propagation constant of a dominant higher-order mode in the liner sample section. This axial propagation constant is then used in conjunction with a closed-form solution to a reduced form of the convected Helmholtz equation and the wall impedance boundary condition to educe the liner impedance. The theory is validated on a conventional liner whose impedance spectrum is educed in two flow ducts with different cross sections. For the frequencies and Mach numbers of interest, no higher-order modes propagate in the hard wall sections of the smaller duct. A benchmark method is used to educe the impedance spectrum in this duct. A dominant higher-order vertical mode propagates in the larger duct for similar test conditions, and the current theory is applied to educe the impedance spectrum. Results show that when the theory is applied to data acquired in the larger duct with a dominant higher-order vertical mode, the same impedance spectra is educed as that obtained in the small duct where only the plane wave mode is present and the benchmark method is used. This result holds for each higher-order vertical mode that is considered.
Document ID
20150000542
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Watson, Willie R.
(NASA Langley Research Center Hampton, VA, United States)
Gerhold, Carl H.
(NASA Langley Research Center Hampton, VA, United States)
Jones, Michael G.
(NASA Langley Research Center Hampton, VA, United States)
June, Jason C.
(Florida Univ. Gainesville, FL, United States)
Date Acquired
January 16, 2015
Publication Date
June 16, 2014
Subject Category
Acoustics
Aircraft Propulsion And Power
Report/Patent Number
NF1676L-17601
Meeting Information
Meeting: (AVIATION 2014) AIAA Aviation and Aeronautics Forum and Exposition
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 475122.02.07.03.0
Distribution Limits
Public
Copyright
Public Use Permitted.
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