Development of a single degree of freedom micro-perforate impedance model under grazing flow and high SPL-Reference-Cited by-同舟云学术

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

Published:2016-05-27 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA/CEAS Aeroacoustics Conference
language:
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Author:

Murray Paul¹,Donnan Clark²,Richter Christoph³,Astley R. Jeremy¹

Affiliation:

1. University of Southampton

2. Bombardier Aerospace

3. Rolls-Royce Group plc

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2982

Reference20 articles.

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

2. 2Rice, E.J. "A model for the pressure excitationspectrumand acoustic impedance of sound absorbersinthe presence ofgrazing flow". AIAA-73-995, 1973.

3. 3Heidelberg,L.J.,Rice,E.J.andHomyak, L. "Experimental evaluationofaspinningmode acoustictreatmentdesign concept for aircraft inlets". NASATP-1613, 1980.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Further Investigation of Impedance Eduction in a Grazing Flow Duct Facility;AIAA Journal;2024-01

2. Impedance models for single and two degree of freedom linings and correlation with grazing flow duct testing;International Journal of Aeroacoustics;2021-06-20

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