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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 33 34 35 36 37 Next > Last >>
NACA 6409 9.04 5.973 40 1.383 0
NACA 6412 12.06 5.981 40 1.535 0.0075
NACA 64A210 9.97 1.325 49.99 0.558 0.0004
NACA 64A-312 11.95 1.554 51.68 1.059 0.009
NACA 64A410 9.96 2.115 51.68 1.065 0.0009
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0.3 0.1 -0.15
0.2 0.5 0.2 -0.2
0.3 0.7 0.3 -0.3
0.4 0.8 0.4 -0.4
0.5 1 0.5 -0.5
1 1.6 1 -0.7
1.5 2 1.5 -0.9
2 2.4 2 -1
2.5 2.96 2.5 -1.11
5 4.3 5 -1.18
7.5 5.42 7.5 -1.08
10 6.31 10 -0.88
15 7.78 15 -0.36
20 8.88 20 0.17
25 9.58 25 0.7
30 10.13 30 1.12
40 10.35 40 1.65
50 9.81 50 1.86
60 8.78 60 1.92
70 7.28 70 1.76
80 5.34 80 1.36
90 2.95 90 0.74
100 0 100 0
V 1.0