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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
< Prev 1 2 3 4 5 Next > Last >>
NACA 654-221 20.98 39.93 1.113 50 0.646 0.0123
MH52 9.01 35.04 0.076 0.19 0.675 0.0061
NACA 66-206 6 44.99 1.107 50 0.688 0.0003
EPPLER 182 8.46 32.84 1.741 37.46 0.689 0.0033
GOTTINGEN 532 12.49 25 4.84 40 0.697 0.006
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 1.1 0.1 -0.6
0.2 1.3 0.2 -0.9
0.3 1.6 0.3 -1.1
0.37 1.57 0.63 -1.47
1.09 2.4 1.41 -2.19
2.31 3.34 2.68 -2.96
4.79 4.78 5.21 -4.15
7.28 5.92 7.72 -5.07
9.78 6.87 10.22 -5.83
14.79 8.37 15.21 -7.02
19.81 9.51 20.19 -7.92
24.83 10.38 25.17 -8.59
29.87 11.01 30.14 -9.06
34.9 11.4 35.1 -9.34
39.93 11.57 40.07 -9.43
44.97 11.46 45.03 -9.43
50 11.06 50 -8.85
55.03 10.37 54.97 -8.18
60.05 9.46 59.95 -7.32
65.07 8.39 64.93 -6.33
70.08 7.2 69.92 -5.25
75.09 5.92 74.91 -4.13
80.08 4.6 79.92 -3
85.07 3.27 84.93 -1.92
90.05 2 89.95 -0.97
95.03 0.86 94.97 -0.23
100 0 100 0
X Y
1 0
0.9503 0.0086
0.9005 0.02
0.8507 0.0327
0.8008 0.046
0.7509 0.0592
0.7008 0.072
0.6507 0.0839
0.6005 0.0946
0.5503 0.1037
0.5 0.1106
0.4497 0.1146
0.3993 0.1157
0.349 0.114
0.2987 0.1101
0.2483 0.1038
0.1981 0.0951
0.1479 0.0837
0.0978 0.0687
0.0728 0.0592
0.0479 0.0478
0.0231 0.0334
0.0109 0.024
0.0037 0.0157
0.003 0.016
0.002 0.013
0.001 0.011
0 0
0 0
0.001 -0.006
0.002 -0.009
0.003 -0.011
0.0063 -0.0147
0.0141 -0.0219
0.0268 -0.0296
0.0521 -0.0415
0.0772 -0.0507
0.1022 -0.0583
0.1521 -0.0702
0.2019 -0.0792
0.2517 -0.0859
0.3014 -0.0906
0.351 -0.0934
0.4007 -0.0943
0.4503 -0.0943
0.5 -0.0885
0.5497 -0.0818
0.5995 -0.0732
0.6493 -0.0633
0.6992 -0.0525
0.7491 -0.0413
0.7992 -0.03
0.8493 -0.0192
0.8995 -0.0097
0.9497 -0.0023
1 0
X Y
100 0
95.03 0.86
90.05 2
85.07 3.27
80.08 4.6
75.09 5.92
70.08 7.2
65.07 8.39
60.05 9.46
55.03 10.37
50 11.06
44.97 11.46
39.93 11.57
34.9 11.4
29.87 11.01
24.83 10.38
19.81 9.51
14.79 8.37
9.78 6.87
7.28 5.92
4.79 4.78
2.31 3.34
1.09 2.4
0.37 1.57
0.3 1.6
0.2 1.3
0.1 1.1
0 0
0 0
0.1 -0.6
0.2 -0.9
0.3 -1.1
0.63 -1.47
1.41 -2.19
2.68 -2.96
5.21 -4.15
7.72 -5.07
10.22 -5.83
15.21 -7.02
20.19 -7.92
25.17 -8.59
30.14 -9.06
35.1 -9.34
40.07 -9.43
45.03 -9.43
50 -8.85
54.97 -8.18
59.95 -7.32
64.93 -6.33
69.92 -5.25
74.91 -4.13
79.92 -3
84.93 -1.92
89.95 -0.97
94.97 -0.23
100 0
V 1.1