Performance of Kumaresan and Tufts Algorithm in Liner Impedance Eduction with Flow
Author:
Affiliation:
1. Computational AeroSciences Branch, NASA Langley Research Center, Hampton, Virginia 23681-2199
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053705
Reference18 articles.
1. Design and Evaluation of Modifications to the NASA Langley Flow Impedance Tube
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3. A Finite Element Propagation Model for Extracting Normal Incidence Impedance in Nonprogressive Acoustic Wave Fields
4. Validation of an Impedance Eduction Method in Flow
5. Comparison of a Convected Helmholtz and Euler Model for Impedance Eduction in Flow
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