Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|---|
| << First < Prev 28 29 30 31 32 Next > Last >> | ||||||
| MH61 | 10.25 | 32.15 | 1.365 | 41.57 | 0.842 | 0.0042 |
| MH60 | 10.07 | 27.66 | 1.939 | 32.14 | 1.089 | 0.0034 |
| MH54 | 8 | 35.47 | 0.595 | 40.1 | 0.776 | 0.0044 |
| MH53 | 9.43 | 38.33 | 0.416 | 14.96 | 0.558 | 0.0056 |
| MH52 | 9.01 | 35.04 | 0.076 | 0.19 | 0.675 | 0.0061 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0.03 | 0.18 | 0.03 | 0.18 |
| 0.51 | 0.83 | 0.13 | -0.35 |
| 1.46 | 1.56 | 0.86 | -0.86 |
| 2.84 | 2.32 | 2.1 | -1.39 |
| 4.66 | 3.08 | 3.83 | -1.91 |
| 6.89 | 3.8 | 6.02 | -2.39 |
| 9.52 | 4.48 | 8.65 | -2.82 |
| 12.52 | 5.09 | 11.71 | -3.17 |
| 15.87 | 5.61 | 15.16 | -3.45 |
| 19.53 | 6.03 | 18.98 | -3.63 |
| 23.49 | 6.34 | 23.15 | -3.73 |
| 27.71 | 6.52 | 27.62 | -3.74 |
| 32.15 | 6.58 | 32.36 | -3.68 |
| 36.79 | 6.51 | 37.32 | -3.55 |
| 41.57 | 6.33 | 42.45 | -3.36 |
| 46.45 | 6.03 | 47.69 | -3.14 |
| 51.39 | 5.61 | 52.99 | -2.89 |
| 56.35 | 5.08 | 58.27 | -2.62 |
| 61.3 | 4.46 | 63.48 | -2.35 |
| 66.2 | 3.76 | 68.55 | -2.07 |
| 71.02 | 3.03 | 73.42 | -1.8 |
| 75.71 | 2.31 | 78.02 | -1.54 |
| 80.19 | 1.65 | 82.31 | -1.29 |
| 84.39 | 1.07 | 86.24 | -1.06 |
| 88.25 | 0.61 | 89.74 | -0.84 |
| 91.67 | 0.27 | 92.78 | -0.65 |
| 94.58 | 0.06 | 95.32 | -0.47 |
| 96.92 | -0.05 | 97.32 | -0.31 |
| 98.63 | -0.06 | 98.78 | -0.16 |
| 99.66 | -0.02 | 99.68 | -0.04 |
| 100 | 0 | 100 | 0 |
| X | Y |
|---|---|
| 1 | 0 |
| 0.9966 | -0.0002 |
| 0.9863 | -0.0006 |
| 0.9692 | -0.0005 |
| 0.9458 | 0.0006 |
| 0.9167 | 0.0027 |
| 0.8825 | 0.0061 |
| 0.8439 | 0.0107 |
| 0.8019 | 0.0165 |
| 0.7571 | 0.0231 |
| 0.7102 | 0.0303 |
| 0.662 | 0.0376 |
| 0.613 | 0.0446 |
| 0.5635 | 0.0508 |
| 0.5139 | 0.0561 |
| 0.4645 | 0.0603 |
| 0.4157 | 0.0633 |
| 0.3679 | 0.0651 |
| 0.3215 | 0.0658 |
| 0.2771 | 0.0652 |
| 0.2349 | 0.0634 |
| 0.1953 | 0.0603 |
| 0.1587 | 0.0561 |
| 0.1252 | 0.0509 |
| 0.0952 | 0.0448 |
| 0.0689 | 0.038 |
| 0.0466 | 0.0308 |
| 0.0284 | 0.0232 |
| 0.0146 | 0.0156 |
| 0.0051 | 0.0083 |
| 0.0003 | 0.0018 |
| 0.0003 | 0.0018 |
| 0.0013 | -0.0035 |
| 0.0086 | -0.0086 |
| 0.021 | -0.0139 |
| 0.0383 | -0.0191 |
| 0.0602 | -0.0239 |
| 0.0865 | -0.0282 |
| 0.1171 | -0.0317 |
| 0.1516 | -0.0345 |
| 0.1898 | -0.0363 |
| 0.2315 | -0.0373 |
| 0.2762 | -0.0374 |
| 0.3236 | -0.0368 |
| 0.3732 | -0.0355 |
| 0.4245 | -0.0336 |
| 0.4769 | -0.0314 |
| 0.5299 | -0.0289 |
| 0.5827 | -0.0262 |
| 0.6348 | -0.0235 |
| 0.6855 | -0.0207 |
| 0.7342 | -0.018 |
| 0.7802 | -0.0154 |
| 0.8231 | -0.0129 |
| 0.8624 | -0.0106 |
| 0.8974 | -0.0084 |
| 0.9278 | -0.0065 |
| 0.9532 | -0.0047 |
| 0.9732 | -0.0031 |
| 0.9878 | -0.0016 |
| 0.9968 | -0.0004 |
| 1 | 0 |
| X | Y |
|---|---|
| 100 | 0 |
| 99.66 | -0.02 |
| 98.63 | -0.06 |
| 96.92 | -0.05 |
| 94.58 | 0.06 |
| 91.67 | 0.27 |
| 88.25 | 0.61 |
| 84.39 | 1.07 |
| 80.19 | 1.65 |
| 75.71 | 2.31 |
| 71.02 | 3.03 |
| 66.2 | 3.76 |
| 61.3 | 4.46 |
| 56.35 | 5.08 |
| 51.39 | 5.61 |
| 46.45 | 6.03 |
| 41.57 | 6.33 |
| 36.79 | 6.51 |
| 32.15 | 6.58 |
| 27.71 | 6.52 |
| 23.49 | 6.34 |
| 19.53 | 6.03 |
| 15.87 | 5.61 |
| 12.52 | 5.09 |
| 9.52 | 4.48 |
| 6.89 | 3.8 |
| 4.66 | 3.08 |
| 2.84 | 2.32 |
| 1.46 | 1.56 |
| 0.51 | 0.83 |
| 0.03 | 0.18 |
| 0.03 | 0.18 |
| 0.13 | -0.35 |
| 0.86 | -0.86 |
| 2.1 | -1.39 |
| 3.83 | -1.91 |
| 6.02 | -2.39 |
| 8.65 | -2.82 |
| 11.71 | -3.17 |
| 15.16 | -3.45 |
| 18.98 | -3.63 |
| 23.15 | -3.73 |
| 27.62 | -3.74 |
| 32.36 | -3.68 |
| 37.32 | -3.55 |
| 42.45 | -3.36 |
| 47.69 | -3.14 |
| 52.99 | -2.89 |
| 58.27 | -2.62 |
| 63.48 | -2.35 |
| 68.55 | -2.07 |
| 73.42 | -1.8 |
| 78.02 | -1.54 |
| 82.31 | -1.29 |
| 86.24 | -1.06 |
| 89.74 | -0.84 |
| 92.78 | -0.65 |
| 95.32 | -0.47 |
| 97.32 | -0.31 |
| 98.78 | -0.16 |
| 99.68 | -0.04 |
| 100 | 0 |
V 1.1