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icon Wing Profile


Use the NACA Chart below to make a profile of the wing upper and lower surface:

Upper SurfaceLower Surface
StationOrdinate StationOrdinate
0000
0.4310.8670.569-0.767
0.6731.0560.827-0.916
1.1631.3541.337-1.140
2.4011.8842.559-1.512
4.8902.6565.110-2.024
7.3873.2487.613-2.400
9.8873.76310.113-2.702
14.8944.51415.106-3.168
19.9055.09720.095-3.505
24.9195.53325.081-3.743
29.9345.83630.066-3.892
34.9516.01035.049-3.950
39.9686.05940.032-3.917
44.9855.93845.015-3.748
50.0005.68950.000-3.483
55.0145.33354.987-3.143
60.0254.89159.975-2.749
65.0334.37564.967-2.315
70.0383.79969.962-1.855
75.0403.17674.960-1.386
80.0382.51879.962-0.926
85.0331.84984.968-0.503
90.0241.18880.977-0.154
95.0120.56494.9880.068
100.000100.000
NACA 64-210:
  • Stations and ordinates given in per cent of air foil chord.
  • L.E. radius: 0.720
  • Slope radius through L.E.: 0.084

Offered by Geson.

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