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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 >>
NACA 6412 12.06 5.981 40 1.535 0.0075
NACA 6409 9.04 5.973 40 1.383 0
NACA 632-415 14.98 2.213 50 1.268 0.0028
NACA 632-215 14.97 1.114 50 0.998 0.0052
NACA 63-210 9.98 1.11 50 0.961 0.0061
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0.5 0.1 -0.2
0.2 0.8 0.2 -0.4
0.3 1 0.3 -0.45
0.4 1.2 0.4 -0.6
0.5 1.4 0.5 -0.7
1 2.05 1 -1
1.5 2.6 1.5 -1.3
2 3.15 2 -1.4
2.5 3.8 2.5 -1.64
5 5.36 5 -1.99
7.5 6.57 7.5 -2.05
10 7.58 10 -1.99
15 9.18 15 -1.67
20 10.34 20 -1.25
25 11.1 25 -0.82
30 11.65 30 -0.38
40 11.8 40 0.2
50 11.16 50 0.55
60 9.95 60 0.78
70 8.23 70 0.85
80 6.03 80 0.73
90 3.33 90 0.39
100 0 100 0
V 1.0