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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 6 7 8 9 10 Next > Last >>
AH 79-100 B 10.04 6.542 53.27 1.451 0.0072
AH21 6.99 1.766 55.23 0.963 0.0044
AMSOIL 11.62 1.93 39 1.412 0.0122
AQUILA 9.39 4.045 34.67 1.426 0.0051
AQUILA 9.3% Smoothed 9.38 4.049 34.667 1.421 0.0046
Coordinates
XUpper YUpper XLower YLower
0.11 -0.32 0.11 0.54
0.43 1.06 0.43 -0.62
0.96 1.68 0.96 -0.87
1.7 2.34 1.7 -1.01
2.65 3.04 2.65 -1.07
3.81 3.74 3.81 -1.08
5.16 4.46 5.16 -1.05
6.7 5.2 6.7 -0.99
8.43 5.94 8.43 -0.9
10.33 6.65 10.33 -0.79
12.41 7.34 12.41 -0.66
14.65 7.97 14.65 -0.52
17.03 8.58 17.03 -0.37
19.56 9.12 19.56 -0.19
22.22 9.61 22.22 -0.01
25 10.03 25 0.18
27.89 10.38 27.89 0.39
30.87 10.65 30.87 0.61
33.93 10.85 33.93 0.84
37.06 10.96 37.06 1.09
40.25 11.01 40.25 1.35
43.47 10.98 43.47 1.62
46.73 10.87 46.73 1.88
53.27 10.44 53.27 2.39
56.53 10.1 56.53 2.61
59.76 9.7 59.76 2.79
62.94 9.23 62.94 2.93
66.07 8.72 66.07 3.03
69.13 8.15 69.13 3.09
72.11 7.56 72.11 3.11
75 6.95 75 3.09
77.78 6.34 77.78 3.03
80.44 5.73 80.44 2.93
82.97 5.13 82.97 2.79
85.36 4.54 85.36 2.61
87.59 3.98 87.59 2.4
89.67 3.43 89.67 2.16
91.57 2.92 91.57 1.91
93.3 2.42 93.3 1.63
94.84 1.96 94.84 1.35
96.19 1.52 96.19 1.07
97.35 1.12 97.35 0.79
98.3 0.76 98.3 0.52
99.04 0.44 99.04 0.31
99.57 0.19 99.57 0.13
99.89 0.03 99.89 0.01
V 1.0