NACA 64A010

      x      y
      (per cent c)

      0      0
      0      0
      0.5    0.804
      0.75   0.969
      1.25   1.225
      2.5    1.688
      5      2.327
      7.5    2.905  (Typo in Abbott/Doenhoff, should read: 2.805)
     10      3.199
     15      3.813
     20      4.272
     25      4.606
     30      4.837
     35      4.968
     40      4.995
     45      4.894
     50      4.684
     55      4.388
     60      4.021
     65      3.597
     70      3.127
     75      2.623
     80      2.103
     85      1.582
     90      1.062
     95      0.541
    100      0.021

    L.E. radius 0.687 per cent c
    T.E. radius 0.023 per cent c

    NACA 64_3-018 Basic Thickness Form
	
    Source: Abbott, Doenhoff: Theory of Wing Sections, page 356, 2nd Edition, Dover Book, New York, USA, 1959.