Airfoil generation using cst parameterization method in matlab

The following Matlab project contains the source code and Matlab examples used for airfoil generation using cst parameterization method. CST method is a powerful parameterization method because of its simplicity, robustness, and its ability to be generalized into various possible shapes of aerodynamic bodies.

The source code and files included in this project are listed in the project files section, please make sure whether the listed source code meet your needs there.

Project Files: 

File NameSize
CST_airfoil.m 1709
license.txt 1322