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Validation of a Numerical Method for Determining Liner ImpedanceThis paper reports the initial results of a test series to evaluate a method for determining the normal incidence impedance of a locally reacting acoustically absorbing liner, located on the lower wall of a duct in a grazing incidence, multi-modal, non-progressive acoustic wave environment without flow. This initial evaluation is accomplished by testing the methods' ability to converge to the known normal incidence impedance of a solid steel plate, and to the normal incidence impedance of an absorbing test specimen whose impedance was measured in a conventional normal incidence tube. The method is shown to converge to the normal incident impedance values and thus to be an adequate tool for determining the impedance of specimens in a grazing incidence, multi-modal, nonprogressive acoustic wave environment for a broad range of source frequencies.
Document ID
20040110414
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Watson, Willie R.
(NASA Langley Research Center Hampton, VA, United States)
Jones, Michael G.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Tanner, Sharon E.
(NASA Langley Research Center Hampton, VA, United States)
Parrott, Tony L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1996
Subject Category
Aircraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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