Validation of Goodrich Perforate Liner Impedance Model Using NASA Langley Test Data

Author:

Yu Jia1,Ruiz Marta1,Kwan Hwa-Wan1

Affiliation:

1. Goodrich Aerostructures Group

Publisher

American Institute of Aeronautics and Astronautics

Reference10 articles.

1. J. Yu and H.W. Kwan, R. E. Kraft, "Acoustic Treatment Impedance Models For High Frequencies", AIAA-97-1653,1997.

2. The acoustic impendance of perforates at medium and high sound pressure levels

3. Acoustic impedance of small, circular orifices in thin plates

4. J. Yu andH.W. Kwan,S. Chiou, "MicroperforatePlateAcousticPropertyEvaluation",AIAA-99-1880,1999.

5. H.W. Kwan, J. Yu, A. Abeysinghe, E. Chien, "A review of acoustic treatment design for aircraft engine noise reduction",IN06_284.Inter-Noise-December2006,Honolulu,Hawai,USA.

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