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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 32 33 34 35 36 Next > Last >>
NACA 63-206 5.99 1.108 50 0.62 0.0052
NACA 63-209 8.99 1.11 50 0.756 0.006
NACA 63-210 9.98 1.11 50 0.961 0.0061
NACA 632-215 14.97 1.114 50 0.998 0.0052
NACA 632-415 14.98 2.213 50 1.268 0.0028
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.2 0.4 0.2 -0.3
0.46 0.55 0.54 -0.45
0.7 0.68 0.8 -0.54
1.2 0.88 1.3 -0.66
2.44 1.24 2.56 -0.87
4.93 1.78 5.07 -1.14
7.43 2.19 7.57 -1.34
9.93 2.53 10.07 -1.49
14.93 3.06 15.07 -1.71
19.94 3.45 20.06 -1.86
29.96 3.93 30.04 -1.98
34.97 4.03 35.03 -1.97
39.98 4.04 40.02 -1.9
44.99 3.97 45.01 -1.78
50 3.83 50 -1.62
55.01 3.61 54.99 -1.42
60.02 3.34 59.99 -1.2
65.02 3.01 64.98 -0.95
70.02 2.64 69.98 -0.7
75.02 2.24 74.93 -0.48
80.02 1.8 79.98 -0.21
85.02 1.36 84.98 -0.01
90.01 0.9 89.99 0.13
95.01 0.45 94.99 0.18
100 0 100 0
V 1.0