This code was made by students from Universitat Politècnica de Catalunya, Pau Ondoño, Miquel Tomàs, Pol Miguel, Pau Andrés and Biel Pujadas. The main objective of the project is to be able to use the TAT theory and the vortex circultaion method (DMV) to calcule the parameters of a 4-digit NACA airfoil with and without flap.
STATUS OF THE PROJECT: in development
Feel free to use this code for personal or comercial use.
Be aware: The results given by the program are aproximations and an error may be present in the results.