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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 43 44 45 46 47 Next > Last >>
DF102 11 2.365 43.52 1.338 0.0054
DF101 11 2.055 43.51 1.216 0.006
DAE51 9.38 3.465 46.07 1.186 0.0078
CLARK YS 11.7 2.353 30 1.274 0.0055
CLARK YH 11.9 2.45 30 1.392 0.0095
Coordinates
XUpper YUpper XLower YLower
0 -0.09 0 -0.09
0.12 0.55 0.49 -0.77
0.66 1.43 1.52 -1.35
1.65 2.45 3 -1.89
3.09 3.51 4.89 -2.4
4.99 4.47 7.2 -2.85
7.32 5.27 9.95 -3.22
10.07 5.92 13.14 -3.48
13.22 6.43 16.76 -3.61
16.72 6.83 20.79 -3.63
20.57 7.14 25.17 -3.55
24.72 7.4 29.84 -3.4
29.13 7.58 34.77 -3.21
33.77 7.65 39.89 -2.99
38.58 7.61 45.17 -2.75
43.52 7.44 50.54 -2.5
48.53 7.15 55.94 -2.23
53.56 6.76 61.3 -1.95
58.57 6.28 66.55 -1.69
63.53 5.73 71.62 -1.44
68.38 5.13 76.46 -1.22
73.07 4.48 80.99 -1
77.56 3.81 85.17 -0.79
81.79 3.12 88.92 -0.59
85.7 2.45 92.2 -0.39
89.25 1.82 94.94 -0.23
92.38 1.26 97.13 -0.11
95.03 0.79 98.72 -0.05
97.16 0.44 99.68 -0.02
100 -0.01 100 -0.01
V 1.0