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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 1 2 3 4 5 Next > Last >>
NACA 653-618 17.97 3.324 50 1.618 0.0085
NACA 23018 17.96 1.835 15 1.275 0.0132
NACA 2418 17.96 1.95 40 1.367 0.0128
NACA 65-218 17.95 1.123 50 1.399 0.0076
EPPLER 266 17.3 3.062 39.79 1.483 0.0066
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.172 1.446 0.828 -1.146
0.385 1.776 1.115 -1.356
0.839 2.293 1.661 -1.651
2.026 3.268 2.974 -2.152
4.462 4.776 5.538 -2.88
6.936 5.971 8.064 -3.427
9.431 6.978 10.569 -3.876
14.455 8.602 15.545 -4.564
19.506 9.848 20.494 -5.072
24.574 10.803 25.426 -5.433
29.652 11.504 30.348 -5.672
34.738 11.972 35.262 -5.792
39.826 12.21 40.174 -5.784
44.915 12.186 45.085 -5.616
50 11.877 50 -5.259
55.077 11.293 54.923 -4.723
60.141 10.479 59.859 -4.053
65.189 9.482 64.811 -3.302
70.219 8.338 69.781 -2.506
75.23 7.075 74.77 -1.705
80.22 5.719 79.78 -0.943
85.189 4.306 84.811 -0.268
90.138 2.863 89.862 0.239
95.068 1.433 94.932 0.463
100 0 100 0
V 1.0