
Winfoil Airfoils - Total Number: 277
Coordinates
XUpper | YUpper | XLower | YLower |
---|---|---|---|
0 | 0 | 0 | 0 |
0.83 | 2.33 | 0.61 | -2.09 |
1.32 | 2.98 | 0.62 | -2.1 |
2.56 | 4.25 | 0.88 | -2.47 |
5.04 | 6.03 | 1.38 | -3.07 |
7.52 | 7.39 | 2.64 | -4.16 |
10.01 | 8.5 | 5.15 | -5.48 |
14.98 | 10.23 | 7.66 | -6.37 |
19.97 | 11.49 | 10.16 | -7.03 |
24.95 | 12.3 | 15.17 | -8.01 |
29.94 | 12.72 | 20.17 | -8.69 |
39.94 | 12.53 | 25.17 | -9.1 |
49.94 | 11.3 | 30.16 | -9.26 |
59.95 | 9.34 | 40.15 | -9.05 |
69.96 | 6.95 | 50.13 | -8.34 |
79.98 | 4.45 | 60.11 | -7.28 |
89.99 | 2.07 | 70.09 | -5.91 |
95 | 0.98 | 80.06 | -4.28 |
100 | 0 | 90.03 | -2.35 |
X | Y |
---|---|
1 | 0 |
0.95 | 0.0098 |
0.8999 | 0.0207 |
0.7998 | 0.0445 |
0.6996 | 0.0695 |
0.5995 | 0.0934 |
0.4994 | 0.113 |
0.3994 | 0.1253 |
0.2994 | 0.1272 |
0.2495 | 0.123 |
0.1997 | 0.1149 |
0.1498 | 0.1023 |
0.1001 | 0.085 |
0.0752 | 0.0739 |
0.0504 | 0.0603 |
0.0256 | 0.0425 |
0.0132 | 0.0298 |
0.0083 | 0.0233 |
0 | 0 |
0 | 0 |
0.0061 | -0.0209 |
0.0062 | -0.021 |
0.0088 | -0.0247 |
0.0138 | -0.0307 |
0.0264 | -0.0416 |
0.0515 | -0.0548 |
0.0766 | -0.0637 |
0.1016 | -0.0703 |
0.1517 | -0.0801 |
0.2017 | -0.0869 |
0.2517 | -0.091 |
0.3016 | -0.0926 |
0.4015 | -0.0905 |
0.5013 | -0.0834 |
0.6011 | -0.0728 |
0.7009 | -0.0591 |
0.8006 | -0.0428 |
0.9003 | -0.0235 |
X | Y |
---|---|
100 | 0 |
95 | 0.98 |
89.99 | 2.07 |
79.98 | 4.45 |
69.96 | 6.95 |
59.95 | 9.34 |
49.94 | 11.3 |
39.94 | 12.53 |
29.94 | 12.72 |
24.95 | 12.3 |
19.97 | 11.49 |
14.98 | 10.23 |
10.01 | 8.5 |
7.52 | 7.39 |
5.04 | 6.03 |
2.56 | 4.25 |
1.32 | 2.98 |
0.83 | 2.33 |
0 | 0 |
0 | 0 |
0.61 | -2.09 |
0.62 | -2.1 |
0.88 | -2.47 |
1.38 | -3.07 |
2.64 | -4.16 |
5.15 | -5.48 |
7.66 | -6.37 |
10.16 | -7.03 |
15.17 | -8.01 |
20.17 | -8.69 |
25.17 | -9.1 |
30.16 | -9.26 |
40.15 | -9.05 |
50.13 | -8.34 |
60.11 | -7.28 |
70.09 | -5.91 |
80.06 | -4.28 |
90.03 | -2.35 |
V 1.1