Validation of a numerical method for extracting liner impedance-Reference-Cited by-同舟云学术

Validation of a numerical method for extracting liner impedance

Published:1996-03 Issue:3 Volume:34 Page:548-554
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Watson Willie R.¹,Jones Michael G.²,Tanner Sharon E.¹,Parrott Tony L.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681-0001

2. Lockheed Engineering and Sciences Company, Inc., Hampton, Virginia 23666

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.13102

Reference9 articles.

1. 3Phillips, B. "Effects of High Value Wave Amplitude and Mean Flow on a Helmholtz Resonator," NASA TMX-1582,1967.

2. 5Watson, W. R. "A Method for Determining Acoustic-Liner Admittance in a Rectangular Duct with Grazing Flow from Experimental Data," NASA TP-2310,1984.

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