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Find where the boundary layer starts separating from the upper surface of the wing profile

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

Basic aerofoil cross section, high cord swept wing. The goal of this project is to get laminar airflow over the wing.

Aerofoil in a different number of angle of attacks then measuring the drag coefficient of that wing.

this is a air flow simulation of a fictional aircraft

From Prandtl's 1933 paper on Bell lift distribution for minimizing the induced drag and recent works being published by NASA on PRANDTL D glider,  I decided to do a performance study and comparison of this type of lift distribution along with the conventional elliptic lift distribution,  that is to compare two wings with different lift distributions but with the same plan form area, taper ratio and aspect ratio

Study of ground effect on aerofoil lift at varying heights and free-stream conditions.

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