GitHub - riciadavinci/NACA-Aerofoil-Plotter-2D-: Python script to generate 2D Profiles of Airfoils from given coordinate files
Meridian Jorly - Department of Mechanical Engineering at Federal Institute of Science And Technology - Kaladi, Kerala, India | LinkedIn
![I made a 4 and 5 digit NACA airfoil aerodynamic properties calculator (This is a heavily updated version from the previous version) : r/desmos I made a 4 and 5 digit NACA airfoil aerodynamic properties calculator (This is a heavily updated version from the previous version) : r/desmos](https://i.redd.it/4cerrcysnjw61.png)