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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 52 53 54 55 56 Next > Last >>
NACA 23018 17.96 1.835 15 1.275 0.0132
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 663-218 17.97 1.117 50 1.166 0.0073
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.3 2 0.3 -0.6
0.6 2.6 0.6 -1.1
1 3.5 1 -1.6
1.25 4.09 1.25 -1.83
2.5 5.29 2.5 -2.71
5 6.92 5 -3.8
7.5 8.01 7.5 -4.6
10 8.83 10 -5.22
15 9.86 15 -6.18
20 10.36 20 -6.86
25 10.56 25 -7.27
30 10.55 30 -7.47
40 10.04 40 -7.37
50 9.05 50 -6.81
60 7.75 60 -5.94
70 6.18 70 -4.82
80 4.4 80 -3.48
90 2.39 90 -1.94
95 1.32 95 -1.09
100 0.19 100 -0.19
V 1.0