Development of a single degree of freedom perforate impedance model under grazing flow and high SPL

Author:

Murray Paul1,Astley R. Jeremy1

Affiliation:

1. University of Southampton

Publisher

American Institute of Aeronautics and Astronautics

Reference20 articles.

1. Rice, E.J. "A Model for the Acoustic Impedance of a Perforated Plate Liner with Multiple Frequency Excitation", NASATM X-67950,1971.

2. Rice, E.J. "A model forthepressureexcitationspectrumand acousticimpedance ofsound absorbersin thepresence of grazingflow".AIAA-73-995, 1973.

3. Heidelberg, L.J., Rice, E.J. and Homyak, L. "Experimentalevaluation ofaspinning modeacoustic treatment design concept foraircraft inlets". NASA TP-1613, 1980.

4. Kooi, J.W., and Sarin, S.L. "An Experimental Study of the Acoustic Impedance of Helmholtz Resonator Arrays Under aTurbulent BoundaryLayer",AIAA-81-1998, 1981.

5. Zandbergen, T., Laan, J.N., Zeemans, H.J., and Sarin, S.L. "In-Flight Acoustic Measurements in the EngineIntakeof aFokkerF28 Aircraft", AIAA-83-0677,1983.

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