NACA 63A008

      x      y
      (per cent c)
     
      0      0
      0.5    0.658
      0.75   0.791
      1.25   1.003
      2.5    1.391
      5      1.930
      7.5    2.332
     10      2.656
     15      3.155
     20      3.515
     25      3.766
     30      3.926
     35      3.995
     40      3.978
     45      3.878
     50      3.705
     55      3.468
     60      3.176
     65      2.837
     70      2.457
     75      2.055
     80      1.647
     85      1.240
     90      0.833
     95      0.425
    100      0.018

    L.E. radius 0.473 per cent c
    T.E. radius 0.020 per cent c

    NACA 63A008 Basic Thickness Form

    Source: Abbott, Doenhoff: Theory of Wing Sections, page 342, 2nd Edition, Dover Book, New York, USA, 1959.