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