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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
< Prev 1 2 3 4 5 Next > Last >>
NACA 4418 18 3.934 40 1.551 0.0104
NACA 663-418 17.98 2.216 50 1.394 0.0076
NACA 663-218 17.97 1.117 50 1.166 0.0073
NACA 653-218 17.97 1.118 50 1.172 0.0034
NACA 653-418 17.97 2.221 50 1.41 0.0082
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.25 1.4 0.25 -1.1
0.5 2.1 0.5 -1.4
1 3 1 -2
1.25 3.76 1.25 -2.11
2.5 5 2.5 -2.99
5 6.75 5 -4.06
7.5 8.06 7.5 -4.67
10 9.11 10 -5.06
15 10.66 15 -5.49
20 11.72 20 -5.56
25 12.4 25 -5.49
30 12.76 30 -5.26
40 12.7 40 -4.7
50 11.85 50 -4.02
60 10.44 60 -3.24
70 8.55 70 -2.45
80 6.22 80 -1.67
90 3.46 90 -0.93
95 1.89 95 -0.55
100 0.19 100 -0.19
V 1.0