A model for the pressure excitation spectrum and acoustic impedance of sound absorbers in the presence of grazing flow

Author:

RICE E.1

Affiliation:

1. NASA, Lewis Research Center, V/STOL and Noise Div., Cleveland, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Acoustic Circulation Effects and the Nonlinear Impedance of Orifices

2. Acoustic Nonlinearity of an Orifice

3. Zlnn, E. T. "ATheoretical Study of Nonlinear mpinpr by Helmholtz Resonators," mper 69-481, 1569,AULA.

4. Rice, E. J. "AModel for the Acoustic Impedance of a Perforated Plate Linerwith Multiple reuancv Excitation," Presented at Acoustical - SO.~ m .Ineeting E=& et. 1971; l s oXASA m x-67950.

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3. Development of a single degree of freedom micro-perforate impedance model under grazing flow and high SPL;22nd AIAA/CEAS Aeroacoustics Conference;2016-05-27

4. A computational and experimental study of resonators in three dimensions;Journal of Sound and Vibration;2010-11

5. A Computational and Experimental Study of Resonators in Three Dimensions;15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference);2009-05-11

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