pressure_coefficient_contour.jpg size: 0.086946 MB
mesh.jpg size: 0.235971 MB
mach_number_contour.jpg size: 0.090609 MB
Cp_validation.png size: 0.050043 MB
mesh.jpg size: 0.235971 MB
mach_number_contour.jpg size: 0.090609 MB
Cp_validation.png size: 0.050043 MB
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Onera m6 wing transonic flow simulation
NoAI: This model, simulation, images, or project may not be utilized within datasets, during the developmental process, or as inputs for generative AI programs.
3D Flow over Onera M6 wing in Ansys Fluent. Airfoil data and problem description can be found here: https://www.grc.nasa.gov/www/wind/valid/m6wing/m6wing.html
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