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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 10 11 12 13 14 Next > Last >>
DF101 11 2.055 43.51 1.216 0.006
DF102 11 2.365 43.52 1.338 0.0054
DF103 11.16 2.181 44.98 1.166 0.0069
ENG.COR 12.42 0 0 1.013 0.0084
EPPLER 1200 16.93 3.48 40.77 1.818 0.0072
Coordinates
XUpper YUpper XLower YLower
0.11 0.45 0.11 0.45
0.65 1.23 0.48 -0.77
1.64 2.11 1.51 -1.35
3.08 3.05 2.99 -1.89
4.98 3.97 4.88 -2.4
7.31 4.83 7.19 -2.85
10.06 5.58 9.94 -3.22
13.21 6.21 13.13 -3.48
16.72 6.72 16.76 -3.61
20.56 7.11 20.78 -3.63
24.71 7.4 25.16 -3.55
29.13 7.58 29.83 -3.4
33.77 7.65 34.76 -3.21
38.58 7.61 39.88 -2.99
43.51 7.44 45.16 -2.75
48.52 7.15 50.53 -2.5
53.55 6.76 55.93 -2.23
58.57 6.28 61.3 -1.95
63.53 5.73 66.54 -1.69
68.38 5.13 71.62 -1.44
73.07 4.48 76.45 -1.22
77.56 3.81 80.99 -1
81.78 3.12 85.17 -0.79
85.7 2.45 88.92 -0.59
89.25 1.82 92.2 -0.39
92.38 1.26 94.94 -0.23
95.03 0.79 97.13 -0.11
97.16 0.44 98.72 -0.05
99.68 0.05 99.68 -0.02
100 0 100 0
V 1.0