Numerical Study of Flap Side-Edge Vortex Based on the Combination of Zonal Detached Eddy Simulation and Lattice-Boltzmann Method-Reference-Cited by-同舟云学术

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Numerical Study of Flap Side-Edge Vortex Based on the Combination of Zonal Detached Eddy Simulation and Lattice-Boltzmann Method

Published:2024-05-30 Issue: Volume:60 Page:
ISSN:
Container-title:30th AIAA/CEAS Aeroacoustics Conference (2024)
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Author:

Husson Julien¹,Terracol Marc¹,Deck Sébastien¹

Affiliation:

1. ONERA Meudon

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3240

Reference37 articles.

1. Almost 40 Years of Airframe Noise Research: What Did We Achieve?

2. Gittens,A.,Hocquard,S.,deJuniac,A.,Liu,F.,andFanning,E."AviationBenefitReport,"ICAOTechnicalreport,2019. URL https://www.icao.int/sustainability/Documents/AVIATION-BENEFITS-2019-web.pdf.

3. Summary of the LAGOON Solutions from the Benchmark problems for Airframe Noise Computations-III Workshop

4. Sijtsma,P."Beamformingonmovingsources,"Tech.rep.,NationalAerospaceLaboratory(NLR),2006.

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