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Impedance Eduction in a Duct Using the Linearized Euler EquationsAn impedance eduction technique that is based upon a numerical solution to the linearized Euler equations coupled with the minimization of an objective function is presented. The linearized Euler equations are solved numerically using a cubic finite element method and the minimum of the objective function is obtained via a gradient based optimizer. The mean flow is allowed to have a gradient in two coordinate directions and the impedance of the liner may vary arbitrarily over the liner surface. A new regularized wall impedance boundary condition presented by Rienstra which contains the effects of the mean boundary layer thickness is implemented. Impedances are educed for a perforate over honeycomb liner using test data acquired in the Langley Grazing Flow Impedance Tube. The impedance of the liner is educed both with an upstream source and a downstream source. The method is validated by comparing the educed impedance to a benchmark method. The primary conclusion of the study is that the impedances educed for upstream and downstream sources are not well matched and that the primary effect of the boundary thickness is to reduce the resistance of the liner.
Document ID
20190027217
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Watson, Willie R.
(NASA Langley Research Center Hampton, VA, United States)
Jones, Michael G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
July 11, 2019
Publication Date
June 25, 2018
Subject Category
Air Transportation And Safety
Report/Patent Number
NF1676L-28628
Meeting Information
Meeting: AIAA Aviation Forum 2018
Location: Atlanta, GA
Country: United States
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Public Use Permitted.
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