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A new method for determining acoustic-liner admittance in a rectangular duct with grazing flow from experimental dataA method is developed for determining acoustic liner admittance in a rectangular duct with grazing flow. The axial propagation constant, cross mode order, and mean flow profile is measured. These measured data are then input into an analytical program which determines the unknown admittance value. The analytical program is based upon a finite element discretization of the acoustic field and a reposing of the unknown admittance value as a linear eigenvalue problem on the admittance value. Gaussian elimination is employed to solve this eigenvalue problem. The method used is extendable to grazing flows with boundary layers in both transverse directions of an impedance tube (or duct). Predicted admittance values are compared both with exact values that can be obtained for uniform mean flow profiles and with those from a Runge Kutta integration technique for cases involving a one dimensional boundary layer.
Document ID
19840019475
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Watson, W. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1984
Subject Category
Acoustics
Report/Patent Number
NAS 1.60:2310
NASA-TP-2310
L-15779
Report Number: NAS 1.60:2310
Report Number: NASA-TP-2310
Report Number: L-15779
Accession Number
84N27543
Funding Number(s)
PROJECT: RTOP 505-31-33-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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