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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 39 40 41 42 43 Next > Last >>
NACA M12 11.9 1.942 30 1.382 0.01
NACA M20 8.26 5.939 30 1.436 0.0096
NACA M6 12 2.142 30 1.34 0.0119
NACA6451.COR 13.94 2.651 51.68 1.258 0.0029
NASA/AMES A-01 10.25 1.368 15 1.159 0.0144
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
1.25 2.03 1.25 -1.64
2.5 2.86 2.5 -2.13
5 4.03 5 -2.71
7.5 4.9 7.5 -3.05
10 5.61 10 -3.29
15 6.66 15 -3.57
20 7.34 20 -3.76
30 8.01 30 -3.92
40 7.94 40 -3.88
50 7.35 50 -3.72
60 6.39 60 -3.38
70 5.12 70 -2.86
80 3.66 80 -2.15
90 2.07 90 -1.19
95 1.26 95 -0.62
100 0.4 100 0
V 1.0