NACA airfoil shapes (4 digit series) can be calculated. 4 digit : NACA MPXX M:Max Camber(%) (M/100) P: Max camber position (%) (P/10) XX: Thickness (%) (XX/100)
The NACA airfoils are airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics (NACA). https://en.wikipedia.org/wiki/NACA_airfoil http://airfoiltools.com/search/index
