Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|---|
| << First < Prev 10 11 12 13 14 Next > Last >> | ||||||
| DF101 | 11 | 29.13 | 2.055 | 43.51 | 1.216 | 0.006 |
| DF102 | 11 | 29.13 | 2.365 | 43.52 | 1.338 | 0.0054 |
| DF103 | 11.16 | 32.12 | 2.181 | 44.98 | 1.166 | 0.0069 |
| ENG.COR | 12.42 | 26.739 | 0 | 0 | 1.013 | 0.0084 |
| EPPLER 1200 | 16.93 | 36.11 | 3.48 | 40.77 | 1.818 | 0.0072 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0.11 | 0.45 | 0.11 | 0.45 |
| 0.65 | 1.23 | 0.48 | -0.77 |
| 1.64 | 2.11 | 1.51 | -1.35 |
| 3.08 | 3.05 | 2.99 | -1.89 |
| 4.98 | 3.97 | 4.88 | -2.4 |
| 7.31 | 4.83 | 7.19 | -2.85 |
| 10.06 | 5.58 | 9.94 | -3.22 |
| 13.21 | 6.21 | 13.13 | -3.48 |
| 16.72 | 6.72 | 16.76 | -3.61 |
| 20.56 | 7.11 | 20.78 | -3.63 |
| 24.71 | 7.4 | 25.16 | -3.55 |
| 29.13 | 7.58 | 29.83 | -3.4 |
| 33.77 | 7.65 | 34.76 | -3.21 |
| 38.58 | 7.61 | 39.88 | -2.99 |
| 43.51 | 7.44 | 45.16 | -2.75 |
| 48.52 | 7.15 | 50.53 | -2.5 |
| 53.55 | 6.76 | 55.93 | -2.23 |
| 58.57 | 6.28 | 61.3 | -1.95 |
| 63.53 | 5.73 | 66.54 | -1.69 |
| 68.38 | 5.13 | 71.62 | -1.44 |
| 73.07 | 4.48 | 76.45 | -1.22 |
| 77.56 | 3.81 | 80.99 | -1 |
| 81.78 | 3.12 | 85.17 | -0.79 |
| 85.7 | 2.45 | 88.92 | -0.59 |
| 89.25 | 1.82 | 92.2 | -0.39 |
| 92.38 | 1.26 | 94.94 | -0.23 |
| 95.03 | 0.79 | 97.13 | -0.11 |
| 97.16 | 0.44 | 98.72 | -0.05 |
| 99.68 | 0.05 | 99.68 | -0.02 |
| 100 | 0 | 100 | 0 |
| X | Y |
|---|---|
| 1 | 0 |
| 0.9968 | 0.0005 |
| 0.9716 | 0.0044 |
| 0.9503 | 0.0079 |
| 0.9238 | 0.0126 |
| 0.8925 | 0.0182 |
| 0.857 | 0.0245 |
| 0.8178 | 0.0312 |
| 0.7756 | 0.0381 |
| 0.7307 | 0.0448 |
| 0.6838 | 0.0513 |
| 0.6353 | 0.0573 |
| 0.5857 | 0.0628 |
| 0.5355 | 0.0676 |
| 0.4852 | 0.0715 |
| 0.4351 | 0.0744 |
| 0.3858 | 0.0761 |
| 0.3377 | 0.0765 |
| 0.2913 | 0.0758 |
| 0.2471 | 0.074 |
| 0.2056 | 0.0711 |
| 0.1672 | 0.0672 |
| 0.1321 | 0.0621 |
| 0.1006 | 0.0558 |
| 0.0731 | 0.0483 |
| 0.0498 | 0.0397 |
| 0.0308 | 0.0305 |
| 0.0164 | 0.0211 |
| 0.0065 | 0.0123 |
| 0.0011 | 0.0045 |
| 0.0011 | 0.0045 |
| 0.0048 | -0.0077 |
| 0.0151 | -0.0135 |
| 0.0299 | -0.0189 |
| 0.0488 | -0.024 |
| 0.0719 | -0.0285 |
| 0.0994 | -0.0322 |
| 0.1313 | -0.0348 |
| 0.1676 | -0.0361 |
| 0.2078 | -0.0363 |
| 0.2516 | -0.0355 |
| 0.2983 | -0.034 |
| 0.3476 | -0.0321 |
| 0.3988 | -0.0299 |
| 0.4516 | -0.0275 |
| 0.5053 | -0.025 |
| 0.5593 | -0.0223 |
| 0.613 | -0.0195 |
| 0.6654 | -0.0169 |
| 0.7162 | -0.0144 |
| 0.7645 | -0.0122 |
| 0.8099 | -0.01 |
| 0.8517 | -0.0079 |
| 0.8892 | -0.0059 |
| 0.922 | -0.0039 |
| 0.9494 | -0.0023 |
| 0.9713 | -0.0011 |
| 0.9872 | -0.0005 |
| 0.9968 | -0.0002 |
| 1 | 0 |
| X | Y |
|---|---|
| 100 | 0 |
| 99.68 | 0.05 |
| 97.16 | 0.44 |
| 95.03 | 0.79 |
| 92.38 | 1.26 |
| 89.25 | 1.82 |
| 85.7 | 2.45 |
| 81.78 | 3.12 |
| 77.56 | 3.81 |
| 73.07 | 4.48 |
| 68.38 | 5.13 |
| 63.53 | 5.73 |
| 58.57 | 6.28 |
| 53.55 | 6.76 |
| 48.52 | 7.15 |
| 43.51 | 7.44 |
| 38.58 | 7.61 |
| 33.77 | 7.65 |
| 29.13 | 7.58 |
| 24.71 | 7.4 |
| 20.56 | 7.11 |
| 16.72 | 6.72 |
| 13.21 | 6.21 |
| 10.06 | 5.58 |
| 7.31 | 4.83 |
| 4.98 | 3.97 |
| 3.08 | 3.05 |
| 1.64 | 2.11 |
| 0.65 | 1.23 |
| 0.11 | 0.45 |
| 0.11 | 0.45 |
| 0.48 | -0.77 |
| 1.51 | -1.35 |
| 2.99 | -1.89 |
| 4.88 | -2.4 |
| 7.19 | -2.85 |
| 9.94 | -3.22 |
| 13.13 | -3.48 |
| 16.76 | -3.61 |
| 20.78 | -3.63 |
| 25.16 | -3.55 |
| 29.83 | -3.4 |
| 34.76 | -3.21 |
| 39.88 | -2.99 |
| 45.16 | -2.75 |
| 50.53 | -2.5 |
| 55.93 | -2.23 |
| 61.3 | -1.95 |
| 66.54 | -1.69 |
| 71.62 | -1.44 |
| 76.45 | -1.22 |
| 80.99 | -1 |
| 85.17 | -0.79 |
| 88.92 | -0.59 |
| 92.2 | -0.39 |
| 94.94 | -0.23 |
| 97.13 | -0.11 |
| 98.72 | -0.05 |
| 99.68 | -0.02 |
| 100 | 0 |
V 1.1