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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 8 9 10 11 12 Next > Last >>
BOEING 707 .08 SPAN 11.43 0.227 6 0.918 0.0076
BOEING 737 ROOT AIRFOI 15.33 0.233 4.95 1.372 0.011
BOEING-VERTOL VR-1 10.95 1.542 43.33 1.121 0.0059
CLARK K 11.38 3.245 39.65 1.676 0.0066
CLARK V 11.6 3.355 50 1.617 0.0074
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.05 0.64 0.05 -0.46
0.1 0.84 0.1 -0.68
0.2 1.1 0.2 -0.95
0.4 1.4 0.4 -1.28
0.8 1.75 0.8 -1.62
1.2 2.09 1.2 -1.89
2 2.72 2 -2.41
3 3.26 3 -2.9
4 3.61 4 -3.22
5 3.87 5 -3.45
6 4.13 6 -3.68
8 4.54 8 -4.15
10 4.76 10 -4.61
12 4.91 12 -5.02
14 5 14 -5.37
16 5.04 16 -5.66
18 5.04 18 -5.91
20 5.05 20 -6.11
22 5.06 22 -6.26
24 5.02 24 -6.4
26 4.82 26 -6.59
28 4.56 28 -6.79
30 4.39 30 -6.89
32 4.3 32 -6.9
34 4.25 34 -6.83
36 4.22 36 -6.71
38 4.2 38 -6.54
40 4.16 40 -6.35
42 4.07 42 -6.15
44 3.95 44 -5.94
46 3.81 46 -5.74
48 3.66 48 -5.53
50 3.52 50 -5.32
52 3.39 52 -5.12
54 3.28 54 -4.92
56 3.17 56 -4.71
58 3.07 58 -4.51
60 2.96 60 -4.3
62 2.85 62 -4.09
64 2.73 64 -3.87
66 2.62 66 -3.65
68 2.5 68 -3.43
70 2.4 70 -3.2
72 2.3 72 -2.98
74 2.21 74 -2.76
76 2.11 76 -2.54
78 2.01 78 -2.33
80 1.91 80 -2.11
82 1.79 82 -1.91
84 1.65 84 -1.71
86 1.5 86 -1.5
88 1.33 88 -1.3
90 1.14 90 -1.09
92 0.94 92 -0.88
94 0.72 94 -0.66
96 0.48 96 -0.44
97 0.36 97 -0.33
98 0.24 98 -0.22
99 0.12 99 -0.11
100 0 100 0
V 1.0