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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 52 53 54 55 56
AG 10 10 6.443 32.1 1.798 0.015
A18 (original) 7.33 3.939 45 1.1 0.0069
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.02 0.642 0.02 -0.077
0.07 0.85 0.07 -0.63
0.158 1.191 0.158 -0.79
0.288 1.514 0.288 -1.076
0.465 1.877 0.465 -1.325
0.701 2.33 0.701 -1.414
1.016 2.817 1.016 -1.595
1.438 3.404 1.438 -1.674
1.997 4.056 1.997 -1.779
2.703 4.782 2.703 -1.769
3.543 5.515 3.543 -1.728
4.487 6.227 4.487 -1.623
5.502 6.886 5.502 -1.479
6.566 7.487 6.566 -1.296
7.669 8.026 7.669 -1.094
9.96 8.94 9.96 -0.649
11.139 9.318 11.139 -0.431
12.336 9.649 12.336 -0.214
13.545 9.941 13.545 0.007
14.769 10.189 14.769 0.21
15.999 10.4 15.999 0.405
17.233 10.579 17.233 0.596
18.469 10.725 18.469 0.772
19.707 10.841 19.707 0.939
20.945 10.933 20.945 1.101
22.183 11.002 22.183 1.257
23.422 11.046 23.422 1.395
24.661 11.071 24.661 1.527
25.9 11.077 25.9 1.644
28.379 11.04 28.379 1.847
29.619 11.003 29.619 1.943
30.859 10.951 30.859 2.022
32.1 10.887 32.1 2.091
33.34 10.814 33.34 2.15
34.581 10.732 34.581 2.204
35.823 10.64 35.823 2.245
37.065 10.541 37.065 2.279
38.308 10.435 38.308 2.303
39.552 10.321 39.552 2.318
40.796 10.202 40.796 2.325
42.042 10.076 42.042 2.323
43.287 9.945 43.287 2.315
44.534 9.808 44.534 2.299
45.781 9.667 45.781 2.277
47.029 9.519 47.029 2.247
48.278 9.368 48.278 2.213
49.528 9.211 49.528 2.172
50.778 9.05 50.778 2.127
52.03 8.883 52.03 2.078
53.282 8.713 53.282 2.026
54.535 8.538 54.535 1.97
55.789 8.359 55.789 1.912
57.044 8.177 57.044 1.853
58.299 7.991 58.299 1.792
59.555 7.8 59.555 1.729
60.812 7.606 60.812 1.666
62.07 7.409 62.07 1.603
63.328 7.21 63.328 1.54
64.587 7.009 64.587 1.477
65.846 6.803 65.846 1.414
67.105 6.595 67.105 1.351
68.364 6.384 68.364 1.286
69.624 6.169 69.624 1.219
70.884 5.95 70.884 1.152
72.144 5.729 72.144 1.083
73.404 5.505 73.404 1.014
74.664 5.278 74.664 0.945
75.924 5.048 75.924 0.874
77.183 4.816 77.183 0.803
78.443 4.581 78.443 0.731
79.702 4.343 79.702 0.658
80.961 4.104 80.961 0.585
82.221 3.861 82.221 0.511
83.481 3.617 83.481 0.436
84.741 3.368 84.741 0.36
86.001 3.118 86.001 0.283
87.262 2.864 87.262 0.205
88.523 2.608 88.523 0.128
89.785 2.348 89.785 0.049
91.048 2.086 91.048 -0.03
92.311 1.82 92.311 -0.111
93.574 1.552 93.574 -0.193
94.835 1.282 94.835 -0.275
96.091 1.01 96.091 -0.357
97.328 0.739 97.328 -0.438
98.495 0.481 98.495 -0.517
99.485 0.26 99.485 -0.585
99.997 0.145 99.997 -0.62
V 1.0