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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 35 36 37 38 39 Next > Last >>
NACA 652-415 14.98 2.218 50 1.248 0.0026
NACA 653-218 17.97 1.118 50 1.172 0.0034
NACA 653-418 17.97 2.221 50 1.41 0.0082
NACA 653-618 17.97 3.324 50 1.618 0.0085
NACA 654-221 20.98 1.113 50 0.646 0.0123
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0.9 0.1 -0.3
0.2 1 0.2 -0.5
0.3 1.2 0.3 -0.7
0.31 1.21 0.69 -1.01
0.54 1.48 0.96 -1.2
1.02 1.9 1.48 -1.47
4.7 3.86 5.3 -2.6
7.18 4.79 7.82 -3.1
9.68 5.58 10.32 -3.51
14.7 6.84 15.3 -4.15
19.73 7.81 20.27 -4.63
24.76 8.55 25.24 -4.97
29.81 9.09 30.19 -5.21
34.85 9.46 35.15 -5.34
39.9 9.64 40.1 -5.36
44.95 9.62 45.05 -5.24
50 9.37 50 -4.96
55.04 8.91 54.96 -4.53
60.08 8.26 59.92 -3.98
65.11 7.46 64.89 -3.34
70.12 6.54 69.88 -2.65
75.13 5.53 74.87 -1.95
80.13 4.45 79.87 -1.26
85.11 3.32 84.89 -0.63
90.08 2.18 89.92 -0.11
95.04 1.06 94.96 0.21
100 0 100 0
V 1.0