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NACA0012 - Angle of Attack - Parametric Study - Copy
16
0
Statistics
2 Geometries
3 Meshes
2 Simulation setups
7 Results
2 Geometries 3 Meshes 2 Simulation setups 7 ResultsAbout this project
Simple project studying NACA0012 symmetric airfoil under an angle of attack (aoa) range. The workflow utilizes the parametric capabilities of SimScale to study multiple design points/multiple aoa. Please check the following forum post for more information https://www.simscale.com/forum/t/parametric-angle-of-attack-aoa-study-for-airfoil-lift-and-drag-calculation/96408 - Copy
