
Winfoil Airfoils - Total Number: 277
Coordinates
XUpper | YUpper | XLower | YLower |
---|---|---|---|
0 | 0.06 | 0 | 0.06 |
0.32 | 0.76 | 0.22 | -0.49 |
1.07 | 1.56 | 1.02 | -0.95 |
2.24 | 2.38 | 2.35 | -1.35 |
3.82 | 3.2 | 4.2 | -1.69 |
5.81 | 3.98 | 6.55 | -1.96 |
8.21 | 4.7 | 9.38 | -2.16 |
11 | 5.33 | 12.68 | -2.28 |
14.16 | 5.88 | 16.4 | -2.34 |
17.67 | 6.31 | 20.51 | -2.34 |
21.51 | 6.64 | 24.96 | -2.29 |
25.64 | 6.86 | 29.71 | -2.19 |
30.04 | 6.97 | 34.7 | -2.06 |
34.66 | 6.97 | 39.88 | -1.89 |
39.45 | 6.87 | 45.18 | -1.7 |
44.37 | 6.68 | 50.56 | -1.48 |
49.37 | 6.4 | 55.95 | -1.25 |
54.4 | 6.05 | 61.28 | -1.02 |
59.4 | 5.64 | 66.51 | -0.78 |
64.33 | 5.16 | 71.56 | -0.56 |
69.12 | 4.65 | 76.38 | -0.37 |
73.72 | 4.1 | 80.9 | -0.2 |
78.08 | 3.52 | 85.07 | -0.07 |
82.17 | 2.92 | 88.82 | 0.02 |
85.94 | 2.31 | 92.1 | 0.07 |
89.37 | 1.73 | 94.87 | 0.09 |
92.41 | 1.2 | 97.08 | 0.08 |
95.02 | 0.74 | 98.69 | 0.05 |
97.13 | 0.4 | 99.67 | 0.02 |
100 | 0 | 100 | 0 |
X | Y |
---|---|
1 | 0 |
0.9713 | 0.004 |
0.9502 | 0.0074 |
0.9241 | 0.012 |
0.8937 | 0.0173 |
0.8594 | 0.0231 |
0.8217 | 0.0292 |
0.7808 | 0.0352 |
0.7372 | 0.041 |
0.6912 | 0.0465 |
0.6433 | 0.0516 |
0.594 | 0.0564 |
0.544 | 0.0605 |
0.4937 | 0.064 |
0.4437 | 0.0668 |
0.3945 | 0.0687 |
0.3466 | 0.0697 |
0.3004 | 0.0697 |
0.2564 | 0.0686 |
0.2151 | 0.0664 |
0.1767 | 0.0631 |
0.1416 | 0.0588 |
0.11 | 0.0533 |
0.0821 | 0.047 |
0.0581 | 0.0398 |
0.0382 | 0.032 |
0.0224 | 0.0238 |
0.0107 | 0.0156 |
0.0032 | 0.0076 |
0 | 0.0006 |
0 | 0.0006 |
0.0022 | -0.0049 |
0.0102 | -0.0095 |
0.0235 | -0.0135 |
0.042 | -0.0169 |
0.0655 | -0.0196 |
0.0938 | -0.0216 |
0.1268 | -0.0228 |
0.164 | -0.0234 |
0.2051 | -0.0234 |
0.2496 | -0.0229 |
0.2971 | -0.0219 |
0.347 | -0.0206 |
0.3988 | -0.0189 |
0.4518 | -0.017 |
0.5056 | -0.0148 |
0.5595 | -0.0125 |
0.6128 | -0.0102 |
0.6651 | -0.0078 |
0.7156 | -0.0056 |
0.7638 | -0.0037 |
0.809 | -0.002 |
0.8507 | -0.0007 |
0.8882 | 0.0002 |
0.921 | 0.0007 |
0.9487 | 0.0009 |
0.9708 | 0.0008 |
0.9869 | 0.0005 |
0.9967 | 0.0002 |
1 | 0 |
X | Y |
---|---|
100 | 0 |
97.13 | 0.4 |
95.02 | 0.74 |
92.41 | 1.2 |
89.37 | 1.73 |
85.94 | 2.31 |
82.17 | 2.92 |
78.08 | 3.52 |
73.72 | 4.1 |
69.12 | 4.65 |
64.33 | 5.16 |
59.4 | 5.64 |
54.4 | 6.05 |
49.37 | 6.4 |
44.37 | 6.68 |
39.45 | 6.87 |
34.66 | 6.97 |
30.04 | 6.97 |
25.64 | 6.86 |
21.51 | 6.64 |
17.67 | 6.31 |
14.16 | 5.88 |
11 | 5.33 |
8.21 | 4.7 |
5.81 | 3.98 |
3.82 | 3.2 |
2.24 | 2.38 |
1.07 | 1.56 |
0.32 | 0.76 |
0 | 0.06 |
0 | 0.06 |
0.22 | -0.49 |
1.02 | -0.95 |
2.35 | -1.35 |
4.2 | -1.69 |
6.55 | -1.96 |
9.38 | -2.16 |
12.68 | -2.28 |
16.4 | -2.34 |
20.51 | -2.34 |
24.96 | -2.29 |
29.71 | -2.19 |
34.7 | -2.06 |
39.88 | -1.89 |
45.18 | -1.7 |
50.56 | -1.48 |
55.95 | -1.25 |
61.28 | -1.02 |
66.51 | -0.78 |
71.56 | -0.56 |
76.38 | -0.37 |
80.9 | -0.2 |
85.07 | -0.07 |
88.82 | 0.02 |
92.1 | 0.07 |
94.87 | 0.09 |
97.08 | 0.08 |
98.69 | 0.05 |
99.67 | 0.02 |
100 | 0 |
V 1.1