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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 18 19 20 21 22 Next > Last >>
NACA 653-218 17.97 1.118 50 1.172 0.0034
NACA 652-415 14.98 2.218 50 1.248 0.0026
NACA 652-215 14.97 1.115 50 0.958 0.0054
NACA 65-218 17.95 1.123 50 1.399 0.0076
NACA 651-412 11.98 2.215 50 1.205 0.0025
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 1 0.1 -0.65
0.2 1.1 0.2 -0.85
0.39 1.38 0.61 -1.28
0.63 1.67 0.88 -1.53
1.11 2.12 1.39 -1.9
2.34 2.93 2.66 -2.56
7.31 5.15 7.69 -4.31
9.81 5.97 10.19 -4.94
14.82 7.28 15.18 -5.93
19.84 8.27 20.17 -6.68
24.86 9.02 25.14 -7.23
29.88 9.57 30.12 -7.62
34.91 9.92 35.09 -7.86
39.94 10.07 40.06 -7.93
44.97 10 45.03 -7.81
50 9.67 50 -7.47
55.03 9.1 54.97 -6.91
60.05 8.34 59.94 -6.2
65.06 7.43 64.94 -5.37
70.07 6.4 69.93 -4.4
75.08 5.29 74.92 -3.5
80.07 4.13 79.93 -2.54
85.06 2.97 84.94 -1.62
90.05 1.84 89.95 -0.8
95.02 0.81 94.98 -0.17
100 0 100 0
V 1.0