An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil

Console to simulate airflow around an airfoil based on RANS approach

Analyse any airfoil from UIUC database in xfoil and obtain results.

This project models airflow around an airfoil to generate a pressure map for approximating the wing's lift. It involves refining the airfoil shape, utilizing cubic spline interpolation and integration methods.

Computes aerodynamical coefficients related to the flow around an airfoil.

This is an application to convert exported polars from XFLR5 to Excel, automatically