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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 20 21 22 23 24 Next > Last >>
MH 22 7.2 1.89 33.42 0.725 0.0048
MH 30 7.83 1.717 44.11 0.866 0.0039
MH 61 (10.28 %) 10.24 1.365 36.787 0.841 0.0041
MH16 12.13 1.544 53.33 0.888 0.0059
MH17 12.12 1.367 30.12 0.817 0.0062
Coordinates
XUpper YUpper XLower YLower
0.06 -0.18 0.06 -0.18
0.09 0.24 0.61 -0.57
0.68 0.79 1.68 -0.95
1.73 1.41 3.24 -1.3
3.22 2.06 5.3 -1.57
5.13 2.7 7.84 -1.77
7.45 3.3 10.85 -1.9
10.16 3.85 14.31 -1.97
13.26 4.34 18.19 -1.99
16.7 4.74 22.45 -1.96
20.47 5.04 27.03 -1.9
24.53 5.24 31.9 -1.82
28.86 5.33 36.98 -1.72
33.42 5.33 42.21 -1.62
38.17 5.23 47.54 -1.5
43.05 5.04 52.89 -1.38
48.02 4.76 58.22 -1.25
53.02 4.38 63.45 -1.13
58.06 3.89 68.54 -1
63.1 3.36 73.41 -0.88
68.07 2.83 78.01 -0.76
72.89 2.34 82.29 -0.65
77.49 1.87 86.19 -0.54
81.81 1.46 89.68 -0.44
85.79 1.09 92.71 -0.35
89.36 0.78 95.24 -0.25
92.48 0.53 97.26 -0.15
95.11 0.32 98.75 -0.06
97.2 0.17 99.68 -0.01
100 0 100 0
V 1.0