Open Fan Noise Confinement Effects in a Closed Wind-Tunnel: Numerical Methodology and Evaluation
Author:
Affiliation:
1. Office National d'Etudes et de Recherches Aerospatiales
2. Safran Aircraft Engines
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3071
Reference22 articles.
1. Mincu, D. C., Le Garrec, T., Péron, S., and Terracol, M. "Immersed boundary conditions for high order CAA solvers-Aeroacousticsinstallationeffectsassessment,"23rdAIAA/CEASAeroacousticsConference,2017.
2. Lorteau, M., Wiart, L., and Kopiev, V. "Numerical study, with experimental validation, of fan noise installation effects in Over-WingNacelleconfigurationusingtheImmersedBoundaryMethod,"25thAIAA/CEASAeroacousticsConference,2019.
3. Lorteau,M.,LeGarrec,T.,Daroukh,M.,andPolacsek,C."AcousticassessmentofBLIeffectsonAirbusNautiliusengine integrationconcept-partI:noiseradiation,"28thAIAA/CEASAeroacousticsConference,Vol.(2992),2022.
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