Multimodal characterisation of acoustic liners using the MAINE Flow facility
Author:
Affiliation:
1. Laboratoire d'Acoustique de l'Universite du Mains
2. Le Mans Technology Transfer Center - CTTM
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3082
Reference10 articles.
1. Aurégan,Y.,Leroux,M.,andPagneux,V.“Measurementoflinerimpedancewithflowbyaninversemethod,”10thAIAA/CEAS aeroacousticsconference,2004,p.2838.
2. Liner Impedance Eduction Under Shear Grazing Flow at a High Sound Pressure Level
3. Weng,C.,Schulz,A.,Ronneberger,D.,Enghardt,L.,andBake,F.“Impedanceeductioninthepresenceofturbulentshearflow usingthelinearizedNavier-Stokesequations,”23rdAIAA/CEASaeroacousticsconference,2017,p.3182.
4. Fundamental problems with the model of uniform flow over acoustic linings
5. Failure of the Ingard–Myers boundary condition for a lined duct: An experimental investigation
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1. Inverse Impedance Eduction of Liners in the MAINE Flow Facility: Flow Effects;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
2. Framework for Modal Based Assessment of Liner Structures;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
3. Shear flow effects in a 2D duct: Influence on wave propagation and direct impedance eduction;Journal of Sound and Vibration;2024-04
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