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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 27 28 29 30 31 Next > Last >>
NACA 0010 9.97 0 0 0.877 0.0016
NACA 0009 8.97 0 0 0.871 0.0065
NACA 0008 7.98 0 0 0.765 0.0064
MILEY 12.86 5.132 35.03 1.43 0.005
MH62 9.29 1.409 37.15 0.919 0.0056
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.25 0.7 0.25 -0.7
0.5 0.95 0.5 -0.95
1 1.4 1 -1.4
1.25 1.58 1.25 -1.58
2.5 2.18 2.5 -2.18
5 2.96 5 -2.96
7.5 3.5 7.5 -3.5
10 3.9 10 -3.9
15 4.46 15 -4.46
20 4.78 20 -4.78
25 4.95 25 -4.95
30 5 30 -5
40 4.84 40 -4.84
50 4.41 50 -4.41
60 3.8 60 -3.8
70 3.05 70 -3.05
80 2.19 80 -2.19
90 1.21 90 -1.21
100 0.11 100 -0.11
V 1.0