
Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
---|---|---|---|---|---|---|
<< First < Prev 7 8 9 10 11 Next > Last >> | ||||||
S2055 | 7.98 | 34.76 | 1.716 | 39.63 | 1.048 | 0.0056 |
S2048.COR | 8.62 | 35.35 | 1.952 | 55.17 | 1.07 | 0.0059 |
S2048 | 8.62 | 35.35 | 1.952 | 55.17 | 1.102 | 0.0053 |
S.I. 64009 | 9.23 | 30 | 6.045 | 40 | 1.515 | 0.0093 |
S.I. 53009 | 9.07 | 30 | 5.007 | 30 | 1.178 | 0.009 |
Coordinates
XUpper | YUpper | XLower | YLower |
---|---|---|---|
0.01 | -0.1 | 0.01 | -0.1 |
0.17 | 0.42 | 0.4 | -0.54 |
0.8 | 1.05 | 1.37 | -0.95 |
1.89 | 1.7 | 2.86 | -1.32 |
3.43 | 2.36 | 4.85 | -1.62 |
5.42 | 2.99 | 7.35 | -1.86 |
7.83 | 3.59 | 10.34 | -2.04 |
10.63 | 4.14 | 13.78 | -2.19 |
13.82 | 4.59 | 17.62 | -2.29 |
17.39 | 4.94 | 21.84 | -2.36 |
21.31 | 5.22 | 26.37 | -2.39 |
25.55 | 5.42 | 31.16 | -2.39 |
30.04 | 5.56 | 36.17 | -2.35 |
34.76 | 5.62 | 41.33 | -2.29 |
39.63 | 5.62 | 46.59 | -2.21 |
44.6 | 5.55 | 51.89 | -2.09 |
49.63 | 5.41 | 57.15 | -1.96 |
54.65 | 5.19 | 62.34 | -1.79 |
59.63 | 4.88 | 67.38 | -1.6 |
64.53 | 4.5 | 72.23 | -1.38 |
69.3 | 4.06 | 76.84 | -1.13 |
73.9 | 3.58 | 81.19 | -0.87 |
78.28 | 3.07 | 85.21 | -0.62 |
82.38 | 2.57 | 88.86 | -0.39 |
86.16 | 2.08 | 92.09 | -0.21 |
89.55 | 1.61 | 94.83 | -0.08 |
92.53 | 1.15 | 97.05 | 0 |
95.08 | 0.74 | 98.67 | 0.02 |
97.15 | 0.4 | 99.67 | 0.01 |
100 | 0 | 100 | 0 |
X | Y |
---|---|
1 | 0 |
0.9715 | 0.004 |
0.9508 | 0.0074 |
0.9253 | 0.0115 |
0.8955 | 0.0161 |
0.8616 | 0.0208 |
0.8238 | 0.0257 |
0.7828 | 0.0307 |
0.739 | 0.0358 |
0.693 | 0.0406 |
0.6453 | 0.045 |
0.5963 | 0.0488 |
0.5465 | 0.0519 |
0.4963 | 0.0541 |
0.446 | 0.0555 |
0.3963 | 0.0562 |
0.3476 | 0.0562 |
0.3004 | 0.0556 |
0.2555 | 0.0542 |
0.2131 | 0.0522 |
0.1739 | 0.0494 |
0.1382 | 0.0459 |
0.1063 | 0.0414 |
0.0783 | 0.0359 |
0.0542 | 0.0299 |
0.0343 | 0.0236 |
0.0189 | 0.017 |
0.008 | 0.0105 |
0.0017 | 0.0042 |
0.0001 | -0.001 |
0.0001 | -0.001 |
0.004 | -0.0054 |
0.0137 | -0.0095 |
0.0286 | -0.0132 |
0.0485 | -0.0162 |
0.0735 | -0.0186 |
0.1034 | -0.0204 |
0.1378 | -0.0219 |
0.1762 | -0.0229 |
0.2184 | -0.0236 |
0.2637 | -0.0239 |
0.3116 | -0.0239 |
0.3617 | -0.0235 |
0.4133 | -0.0229 |
0.4659 | -0.0221 |
0.5189 | -0.0209 |
0.5715 | -0.0196 |
0.6234 | -0.0179 |
0.6738 | -0.016 |
0.7223 | -0.0138 |
0.7684 | -0.0113 |
0.8119 | -0.0087 |
0.8521 | -0.0062 |
0.8886 | -0.0039 |
0.9209 | -0.0021 |
0.9483 | -0.0008 |
0.9705 | 0 |
0.9867 | 0.0002 |
0.9967 | 0.0001 |
1 | 0 |
X | Y |
---|---|
100 | 0 |
97.15 | 0.4 |
95.08 | 0.74 |
92.53 | 1.15 |
89.55 | 1.61 |
86.16 | 2.08 |
82.38 | 2.57 |
78.28 | 3.07 |
73.9 | 3.58 |
69.3 | 4.06 |
64.53 | 4.5 |
59.63 | 4.88 |
54.65 | 5.19 |
49.63 | 5.41 |
44.6 | 5.55 |
39.63 | 5.62 |
34.76 | 5.62 |
30.04 | 5.56 |
25.55 | 5.42 |
21.31 | 5.22 |
17.39 | 4.94 |
13.82 | 4.59 |
10.63 | 4.14 |
7.83 | 3.59 |
5.42 | 2.99 |
3.43 | 2.36 |
1.89 | 1.7 |
0.8 | 1.05 |
0.17 | 0.42 |
0.01 | -0.1 |
0.01 | -0.1 |
0.4 | -0.54 |
1.37 | -0.95 |
2.86 | -1.32 |
4.85 | -1.62 |
7.35 | -1.86 |
10.34 | -2.04 |
13.78 | -2.19 |
17.62 | -2.29 |
21.84 | -2.36 |
26.37 | -2.39 |
31.16 | -2.39 |
36.17 | -2.35 |
41.33 | -2.29 |
46.59 | -2.21 |
51.89 | -2.09 |
57.15 | -1.96 |
62.34 | -1.79 |
67.38 | -1.6 |
72.23 | -1.38 |
76.84 | -1.13 |
81.19 | -0.87 |
85.21 | -0.62 |
88.86 | -0.39 |
92.09 | -0.21 |
94.83 | -0.08 |
97.05 | 0 |
98.67 | 0.02 |
99.67 | 0.01 |
100 | 0 |
V 1.1