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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 11 12 13 14 15 Next > Last >>
EPPLER 168 12.42 0 0 1.035 0.0073
EPPLER 169 14.37 0 0 1.146 0.0079
EPPLER 182 8.46 1.741 37.46 0.689 0.0033
EPPLER 184 8.31 1.146 36.76 0.7 0.005
EPPLER 193 MOD 11.86 4.147 39.98 1.429 0.0071
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.29 0.73 0.29 -0.73
1.1 1.55 1.1 -1.55
2.36 2.38 2.36 -2.38
4.07 3.18 4.07 -3.18
6.2 3.94 6.2 -3.94
8.73 4.62 8.73 -4.62
11.64 5.21 11.64 -5.21
14.92 5.67 14.92 -5.67
18.54 5.99 18.54 -5.99
22.49 6.17 22.49 -6.17
26.74 6.22 26.74 -6.22
31.26 6.13 31.26 -6.13
36.02 5.92 36.02 -5.92
40.97 5.6 40.97 -5.6
46.08 5.2 46.08 -5.2
51.28 4.72 51.28 -4.72
56.52 4.21 56.52 -4.21
61.74 3.67 61.74 -3.67
66.87 3.13 66.87 -3.13
71.85 2.61 71.85 -2.61
76.62 2.13 76.62 -2.13
81.09 1.69 81.09 -1.69
85.21 1.3 85.21 -1.3
88.91 0.97 88.91 -0.97
92.15 0.7 92.15 -0.7
94.86 0.47 94.86 -0.47
97.02 0.27 97.02 -0.27
98.63 0.1 98.63 -0.1
99.65 0.02 99.65 -0.02
100 0 100 0
V 1.0