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.

Python package to compute the characteristics of an airplane or an airfoil based on simple flight mechanics equations.

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

Computational aerodynamics laboratory project implementing Hess-Smith panel method and Weissinger lifting-line theory for airfoil and wing analysis

Second aerospace project that analyzes airfoil

A comparative study of Deep Neural Network architectures for the high-accuracy prediction of pressure coefficients ($C_p$) in low Reynolds number airfoils, achieving a 97.58% correlation with XFoil CFD data.

A simple graphical interface for XFoil, with some extras!

🌬️ Analyze aerodynamic properties using panel methods and lifting-line theory, facilitating effective airfoil and wing design for aerospace applications.

Investigates NACA 2412 airfoil aerodynamics using ANSYS Fluent CFD and MATLAB. Analyzes lift/drag coefficients across AoA to identify stall angle. Uses ~120k quad mesh, k-omega SST model. MATLAB applies Thin Airfoil Theory. CFD captures post-stall behavior (~12°). Includes animations, residuals, Cl/Cd plots.