Airfoil Optimization by XFOIL Matlab

This MATLAB live code tool can morph any given airfoil file with user-defined flap and slat settings. There are two types of flaps and slats that can be generated - Hinged and Continuous

Polynomial Gridgeneration Wizard for crafting structured grids around airfoils with blunt trailing edges.

This repository makes use of the Vortex Panel Method to calculate the Lift, Drag and Pressure Coefficients of any airfoil at a specified Freestream Velocity, Chord Length and Angle of Attack by providing the X and Y coordinates of the airfoil in a .dat file.

GNU Octave Airfoil coordinates import function.

MATLAB script for defining a Kutta-Schukowki-airfoil and determining its pressure and velocity field

Fork of the original repository by Rafael Oliveira. Launch XFOIL from MATLAB

TSK fuzzy models for regression & classification in Matlab, using the Fuzzy Logic Toolbox.

Numerical and Analytical Flow Solution over Joukowski Aerofoil, Using O-grid Meshing Method and PSOR solving algorithm.

Analysis And Computation Of Aerodynamics Parameters of a 4-digit NACA Airfoil With Flaps Using The Discrete Vortex Method (DVM)