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F1 2026 regulations first attempt to simulate with only two wings

Examining the theory of Circulation Theory of Lift

CFD analysis for an airfoil with a circle-segment upper surface and flat lower surface.

The main aim of this project is to better understand the aerodynamic flow around a NACA2412 airfoil.

To see if an airfoil can provide enough lift

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

A simulation regarding analysis of specific NACA airfoils under conditions of mainly Re 5e5 & M 0.1

The first project for my aerodynamics class. I am simulating the airfoil to obtain the coefficients of drag and lift.

Airfoil lift & drag determination & side wall frictional resistance

simulating the air foil shape of drone body

Examining side airfoil wall shear forces generated from adjacent moving wall

Simulating the airflow around a Cessna 172's slotted flaps at different angles

Study of the behavior of the NACA airfoil.

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

Wing analysis for two airfoils (N-22 and CH10). The wing will be used for the conceptual design for an UAV (for agricultural applications)

airfoil | SimScale Project Library | Page 1