How can I write code for plotting modified airfoil surface?

I have a project about modified 2D NACA2415 airfoil. I will modify upper surface and then analyze it on ANSYS. But, firstly ı need the points of modified naca airfoil. What can ı do for coding of new naca airfoil?

Answer 1

[Parsa]

Hi Merve

Please take a look at the link below.

NACA 4 digit Airfoil Generator - File Exchange - MATLAB Central (mathworks.com)