Matlab based GUI to plot and generate data points for NACA airfoils.

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The standalone GUI plots and generates data points for four and five digit NACA Foils. Data points can be extracted as text, DAT or AUTO-CAD script files for convenient CAD modelling of 2D wing sections.

Features of the program include the ability to specify cosine or linear spacing of data points, specifying reflex to the airfoil and choosing the trailing edge to be either open or closed.

NacaFoil Web Site


  • Easy Visualization of Airfoil Sections
  • Convenient Generation of Data Point Files

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Additional Project Details

User Interface

Win32 (MS Windows)

Programming Language



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