This MATLAB live code tool can be used to morph any given airfoil with user-defined flap and slat settings, this is more interactive. There is also a matlab code file, just import the file to the location of the code file and use the correct file name to import the NACA airfoil file. Two types of flaps and slats can be generated using this tool - Hinged and Continuous

1. The airfoil file should be in the (*.dat) extension
2. Add the input airfoil file location in the FileName variable with extension.
3. The Contour signifies if the Flap or Slat is going to be hinged or continuous.
   Illustration:

   Hinged	Continuous

4. The users have three options to switch between Flap modification, Slat modification or both combined.
5. The input data requires the hinge position in terms of Chord percentage and Thickness percentage depending on the type of modification.
6. You can rename the output file name but it should be in the (*.dat) extension.