patrykkulik/Panel-Code---NACA-4-digit
Script to output the lift coefficient for a given 4-digit NACA airfoil and the specified flow conditions, as well as to plot the airflow around the airfoil at a specified angle of attack
MATLAB
Script to output the lift coefficient for a given 4-digit NACA airfoil and the specified flow conditions, as well as to plot the airflow around the airfoil at a specified angle of attack
MATLAB