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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

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