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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 15 16 17 18 19 Next > Last >>
NACA 664-221 20.98 44.97 1.119 50 1.434 0.008
NACA 663-418 17.98 44.94 2.216 50 1.394 0.0076
NACA 663-218 17.97 44.97 1.117 50 1.166 0.0073
NACA 662-415 14.99 44.95 2.217 50 0.751 0.0001
NACA 662-215 14.98 44.98 1.109 50 0.915 0.0002
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 1 0.1 -0.5
0.2 1.25 0.2 -0.8
0.37 1.57 0.63 -1.47
0.61 1.87 0.89 -1.73
1.1 2.34 1.41 -2.13
2.32 3.23 2.68 -2.85
4.8 4.58 5.2 -3.95
7.29 5.65 7.71 -4.81
9.79 6.57 10.21 -5.53
14.8 8.04 15.2 -6.69
19.82 9.17 20.19 -7.58
24.84 10.05 25.16 -8.26
29.87 10.71 30.13 -8.77
34.9 11.18 35.1 -9.12
39.93 11.48 40.07 -9.34
44.97 11.6 45.03 -9.4
50 11.54 50 -9.33
55.03 11.28 54.97 -9.09
60.06 10.76 59.94 -8.62
65.09 9.82 64.91 -7.76
70.1 8.58 69.9 -6.64
75.11 7.15 74.89 -5.36
80.11 5.59 79.89 -4
85.09 4 84.91 -2.65
90.07 2.44 89.93 -1.41
95.03 1.03 94.97 -0.4
100 0 100 0
X Y
1 0
0.9503 0.0103
0.9007 0.0244
0.8509 0.04
0.8011 0.0559
0.7511 0.0715
0.701 0.0858
0.6509 0.0982
0.6006 0.1076
0.5503 0.1128
0.5 0.1154
0.4497 0.116
0.3993 0.1148
0.349 0.1118
0.2987 0.1071
0.2484 0.1005
0.1982 0.0917
0.148 0.0804
0.0979 0.0657
0.0729 0.0565
0.048 0.0458
0.0232 0.0323
0.011 0.0234
0.0061 0.0187
0.0037 0.0157
0.002 0.0125
0.001 0.01
0 0
0 0
0.001 -0.005
0.002 -0.008
0.0063 -0.0147
0.0089 -0.0173
0.0141 -0.0213
0.0268 -0.0285
0.052 -0.0395
0.0771 -0.0481
0.1021 -0.0553
0.152 -0.0669
0.2019 -0.0758
0.2516 -0.0826
0.3013 -0.0877
0.351 -0.0912
0.4007 -0.0934
0.4503 -0.094
0.5 -0.0933
0.5497 -0.0909
0.5994 -0.0862
0.6491 -0.0776
0.699 -0.0664
0.7489 -0.0536
0.7989 -0.04
0.8491 -0.0265
0.8993 -0.0141
0.9497 -0.004
1 0
X Y
100 0
95.03 1.03
90.07 2.44
85.09 4
80.11 5.59
75.11 7.15
70.1 8.58
65.09 9.82
60.06 10.76
55.03 11.28
50 11.54
44.97 11.6
39.93 11.48
34.9 11.18
29.87 10.71
24.84 10.05
19.82 9.17
14.8 8.04
9.79 6.57
7.29 5.65
4.8 4.58
2.32 3.23
1.1 2.34
0.61 1.87
0.37 1.57
0.2 1.25
0.1 1
0 0
0 0
0.1 -0.5
0.2 -0.8
0.63 -1.47
0.89 -1.73
1.41 -2.13
2.68 -2.85
5.2 -3.95
7.71 -4.81
10.21 -5.53
15.2 -6.69
20.19 -7.58
25.16 -8.26
30.13 -8.77
35.1 -9.12
40.07 -9.34
45.03 -9.4
50 -9.33
54.97 -9.09
59.94 -8.62
64.91 -7.76
69.9 -6.64
74.89 -5.36
79.89 -4
84.91 -2.65
89.93 -1.41
94.97 -0.4
100 0
V 1.1