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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

study of the aerodinamic behaibour of the NACA 0012 airfoil to compare whith the windtunel

To verify the setup to be used in analysing aerodynamic bodies

Analyse and compute the basic aerodynamic characteristics of a NACA0012 foil.

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