Experimental and numerical assessment of novel acoustic liners for aero-engine applications
Author:
Affiliation:
1. University of Southampton Faculty of Engineering and the Environment
2. Koninklijk Nederlands Lucht- en Ruimtevaartcentrum
3. Rolls-Royce Deutschland Ltd und Co KG
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2900
Reference25 articles.
1. Sugimoto,R.,Murray,P.,andAstley,R.“FoldedCavityLinersforTurbofanEngineIntakes,”AmericanInstituteofAeronautics andAstronautics,18thAIAA/CEASAeroacousticsConference,2012.
2. Schiller,N. H.,andJones,M. G.“SmearedImpedanceModel forVariableDepth Liners,”AmericanInstituteof Aeronautics andAstronautics,AIAA/CEASAeroacousticsConference,2018.
3. Effect of the acoustic boundary layer on the wave propagation in ducts
4. Effect of mean-velocity profile shapes on sound transmission through two-dimensional ducts
5. On the acoustic boundary condition in the presence of flow
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