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Evaluation of a Multizone Impedance Eduction MethodA computational study is used to evaluate the PyCHE impedance eduction method developed at the NASA Langley Research Center. This method combines an aeroacoustic duct propagation code based on numerical solution to the convected Helmholtz equation with a global optimizer that uses the Differential Evolution algorithm. The efficacy of this method is evaluated with acoustic pressure data simulated to represent that measured with one-zone, two-zone, and three-zone liners mounted in the NASA Langley Grazing Flow Impedance Tube. The PyCHE method has a normalized impedance error of approximately 0.2 for (uniform) one-zone liners with a length of at least 5”, and produces quite reasonable results for liners as short as 2”. Whereas the impedance of the liner has an effect on eduction accuracy, the amount of attenuation is shown to be the dominant parameter. Similar results are observed for two-zone liners, for which the impedance of each zone is unique. The two-zone results also indicate it is more difficult to accurately educe resistance than reactance, and a zone length of at least 6” (slightly longer than for uniform liners) is needed to limit the normalized error to 0.2. The PyCHE method is also demonstrated to successfully educe the impedances for each zone of a three-zone liner. These results are sufficiently encouraging to warrant the continued usage of the PyCHE impedance eduction method for single and multizone liners.





Document ID
20200002606
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Jones, M. G.
(NASA Langley Research Center Hampton, VA, United States)
Nark, D. M.
(NASA Langley Research Center Hampton, VA, United States)
Watson, W. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 17, 2020
Publication Date
May 20, 2019
Subject Category
Acoustics
Report/Patent Number
NF1676L-31445
Report Number: NF1676L-31445
Meeting Information
Meeting: 2019 AIAA Aeroacoustics Conference
Location: Delft
Country: Netherlands
Start Date: May 20, 2019
End Date: May 24, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 081876.02.07.03.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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