Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|---|
| << First < Prev 30 31 32 33 34 Next > Last >> | ||||||
| MH33 | 7.27 | 29.28 | 1.124 | 43.91 | 0.779 | 0.0042 |
| MH32 | 8.71 | 30.13 | 2.368 | 44.4 | 0.742 | 0.0035 |
| MH29 | 13.6 | 40.94 | 1.626 | 26.59 | 0.97 | 0.0065 |
| MH28 | 10.05 | 40.94 | 1.319 | 48.06 | 0.822 | 0.0054 |
| MH27 | 11.98 | 44.7 | 1.499 | 39.74 | 0.991 | 0.0048 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0 | -0.05 | 0 | 0.05 |
| 0.03 | 0.17 | 0.05 | -0.15 |
| 0.09 | 0.28 | 0.15 | -0.25 |
| 0.62 | 0.84 | 0.65 | -0.57 |
| 1.61 | 1.44 | 1.76 | -1.01 |
| 3.05 | 2.03 | 3.36 | -1.41 |
| 4.93 | 2.58 | 5.44 | -1.76 |
| 7.26 | 3.09 | 7.99 | -2.05 |
| 10.01 | 3.54 | 11 | -2.28 |
| 13.17 | 3.92 | 14.43 | -2.45 |
| 16.71 | 4.22 | 18.26 | -2.56 |
| 20.6 | 4.45 | 22.44 | -2.61 |
| 24.8 | 4.6 | 26.94 | -2.61 |
| 29.28 | 4.68 | 31.71 | -2.57 |
| 33.99 | 4.68 | 36.69 | -2.49 |
| 38.89 | 4.62 | 41.84 | -2.37 |
| 43.91 | 4.5 | 47.09 | -2.22 |
| 49.02 | 4.32 | 52.39 | -2.06 |
| 54.15 | 4.09 | 57.67 | -1.88 |
| 59.25 | 3.82 | 62.88 | -1.68 |
| 69.13 | 3.5 | 67.94 | -1.49 |
| 73.8 | 2.8 | 72.81 | -1.29 |
| 78.23 | 2.42 | 77.43 | -1.1 |
| 82.36 | 2.03 | 81.73 | -0.91 |
| 86.15 | 1.63 | 85.67 | -0.72 |
| 89.56 | 1.25 | 89.21 | -0.53 |
| 92.57 | 0.88 | 92.32 | -0.34 |
| 95.13 | 0.56 | 94.97 | -0.19 |
| 97.19 | 0.3 | 97.11 | -0.07 |
| 98.73 | 0.13 | 98.69 | -0.01 |
| 99.68 | 0.03 | 99.67 | 0 |
| 100 | 0 | 100 | 0 |
| X | Y |
|---|---|
| 1 | 0 |
| 0.9968 | 0.0003 |
| 0.9873 | 0.0013 |
| 0.9719 | 0.003 |
| 0.9513 | 0.0056 |
| 0.9257 | 0.0088 |
| 0.8956 | 0.0125 |
| 0.8615 | 0.0163 |
| 0.8236 | 0.0203 |
| 0.7823 | 0.0242 |
| 0.738 | 0.028 |
| 0.6913 | 0.035 |
| 0.5925 | 0.0382 |
| 0.5415 | 0.0409 |
| 0.4902 | 0.0432 |
| 0.4391 | 0.045 |
| 0.3889 | 0.0462 |
| 0.3399 | 0.0468 |
| 0.2928 | 0.0468 |
| 0.248 | 0.046 |
| 0.206 | 0.0445 |
| 0.1671 | 0.0422 |
| 0.1317 | 0.0392 |
| 0.1001 | 0.0354 |
| 0.0726 | 0.0309 |
| 0.0493 | 0.0258 |
| 0.0305 | 0.0203 |
| 0.0161 | 0.0144 |
| 0.0062 | 0.0084 |
| 0.0009 | 0.0028 |
| 0.0003 | 0.0017 |
| 0 | -0.0005 |
| 0 | 0.0005 |
| 0.0005 | -0.0015 |
| 0.0015 | -0.0025 |
| 0.0065 | -0.0057 |
| 0.0176 | -0.0101 |
| 0.0336 | -0.0141 |
| 0.0544 | -0.0176 |
| 0.0799 | -0.0205 |
| 0.11 | -0.0228 |
| 0.1443 | -0.0245 |
| 0.1826 | -0.0256 |
| 0.2244 | -0.0261 |
| 0.2694 | -0.0261 |
| 0.3171 | -0.0257 |
| 0.3669 | -0.0249 |
| 0.4184 | -0.0237 |
| 0.4709 | -0.0222 |
| 0.5239 | -0.0206 |
| 0.5767 | -0.0188 |
| 0.6288 | -0.0168 |
| 0.6794 | -0.0149 |
| 0.7281 | -0.0129 |
| 0.7743 | -0.011 |
| 0.8173 | -0.0091 |
| 0.8567 | -0.0072 |
| 0.8921 | -0.0053 |
| 0.9232 | -0.0034 |
| 0.9497 | -0.0019 |
| 0.9711 | -0.0007 |
| 0.9869 | -0.0001 |
| 0.9967 | 0 |
| 1 | 0 |
| X | Y |
|---|---|
| 100 | 0 |
| 99.68 | 0.03 |
| 98.73 | 0.13 |
| 97.19 | 0.3 |
| 95.13 | 0.56 |
| 92.57 | 0.88 |
| 89.56 | 1.25 |
| 86.15 | 1.63 |
| 82.36 | 2.03 |
| 78.23 | 2.42 |
| 73.8 | 2.8 |
| 69.13 | 3.5 |
| 59.25 | 3.82 |
| 54.15 | 4.09 |
| 49.02 | 4.32 |
| 43.91 | 4.5 |
| 38.89 | 4.62 |
| 33.99 | 4.68 |
| 29.28 | 4.68 |
| 24.8 | 4.6 |
| 20.6 | 4.45 |
| 16.71 | 4.22 |
| 13.17 | 3.92 |
| 10.01 | 3.54 |
| 7.26 | 3.09 |
| 4.93 | 2.58 |
| 3.05 | 2.03 |
| 1.61 | 1.44 |
| 0.62 | 0.84 |
| 0.09 | 0.28 |
| 0.03 | 0.17 |
| 0 | -0.05 |
| 0 | 0.05 |
| 0.05 | -0.15 |
| 0.15 | -0.25 |
| 0.65 | -0.57 |
| 1.76 | -1.01 |
| 3.36 | -1.41 |
| 5.44 | -1.76 |
| 7.99 | -2.05 |
| 11 | -2.28 |
| 14.43 | -2.45 |
| 18.26 | -2.56 |
| 22.44 | -2.61 |
| 26.94 | -2.61 |
| 31.71 | -2.57 |
| 36.69 | -2.49 |
| 41.84 | -2.37 |
| 47.09 | -2.22 |
| 52.39 | -2.06 |
| 57.67 | -1.88 |
| 62.88 | -1.68 |
| 67.94 | -1.49 |
| 72.81 | -1.29 |
| 77.43 | -1.1 |
| 81.73 | -0.91 |
| 85.67 | -0.72 |
| 89.21 | -0.53 |
| 92.32 | -0.34 |
| 94.97 | -0.19 |
| 97.11 | -0.07 |
| 98.69 | -0.01 |
| 99.67 | 0 |
| 100 | 0 |
V 1.1