Acoustic Investigation of the Transonic RAE 2822 Airfoil with Large-Eddy Simulation
Author:
Affiliation:
1. Universite de Sherbrooke Faculte de Genie
2. Ecole de technologie superieure
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2816
Reference18 articles.
1. Cook, P., Firmin, M., and McDonald, M. "Aerofoil RAE 2822: pressure distributions, and boundary layer and wake measurements," AGARDReportAR138,1977.
2. Numerical Simulation of Gurney Flap on RAE-2822 Supercritical Airfoil
3. An evaluation of RANS turbulence modelling for aerodynamic applications
4. Study of Delayed-Detached Eddy Simulation with Weakly Nonlinear Turbulence Model
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1. Numerical Study on Far-Field Noise Characteristic Generated by Wall-Mounted Swept Finite-Span Airfoil within Transonic Flow;Aerospace;2024-08-08
2. Shape Sensitivities of 2D Airfoils for Broadband Noise Reduction Using the Adjoint Method and Semi-Analytical Models;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
3. Broadband Noise of the Transonic RAE 2822 Airfoil;AIAA AVIATION 2023 Forum;2023-06-08
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