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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

Testing simscale incompressible on a prop

The Project simulates the structural FEA of the airplane wing

Simulación del ala y empenaje de una aeronave

F1 style front wing for a home build biobased flak and seaweed epoxy based front wing for home project.

Run a baseline simulation with a tested geometry to lay groundwork for further simulations.

I took the Porsche 919 LMP model from another user in simscale and tweaked everything to be able to model the airflow over the vehicle