Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|---|
| << First < Prev 50 51 52 53 54 Next > Last >> | ||||||
| SD2030 | 8.56 | 35.49 | 2.24 | 45.28 | 1.169 | 0.0056 |
| SD2083 | 8.97 | 35.17 | 2.871 | 39.91 | 1.14 | 0.0055 |
| SD5060 | 9.45 | 24.93 | 2.343 | 43.51 | 1.217 | 0.006 |
| SD6060 | 10.36 | 33.86 | 1.945 | 38.57 | 1.087 | 0.0058 |
| SD6080 | 9.18 | 30.86 | 3.587 | 39.99 | 1.306 | 0.0051 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0 | 0.02 | 0 | 0.02 |
| 0.28 | 0.66 | 0.25 | -0.5 |
| 1 | 1.37 | 1.07 | -0.94 |
| 2.15 | 2.1 | 2.42 | -1.31 |
| 3.75 | 2.8 | 4.3 | -1.6 |
| 5.8 | 3.48 | 6.69 | -1.83 |
| 8.27 | 4.1 | 9.58 | -2 |
| 11.16 | 4.66 | 12.94 | -2.11 |
| 14.43 | 5.16 | 16.73 | -2.18 |
| 18.07 | 5.58 | 20.9 | -2.21 |
| 22.03 | 5.92 | 25.4 | -2.21 |
| 26.29 | 6.18 | 30.19 | -2.17 |
| 30.79 | 6.36 | 35.21 | -2.11 |
| 35.49 | 6.46 | 40.4 | -2.02 |
| 40.34 | 6.48 | 45.69 | -1.91 |
| 45.28 | 6.42 | 51.04 | -1.78 |
| 50.27 | 6.27 | 56.37 | -1.63 |
| 55.26 | 6.04 | 61.62 | -1.47 |
| 60.19 | 5.72 | 66.74 | -1.29 |
| 65.02 | 5.33 | 71.67 | -1.08 |
| 69.71 | 4.86 | 76.37 | -0.85 |
| 74.22 | 4.32 | 80.8 | -0.62 |
| 78.51 | 3.74 | 84.91 | -0.4 |
| 82.54 | 3.15 | 88.63 | -0.21 |
| 86.25 | 2.56 | 91.93 | -0.07 |
| 89.59 | 1.99 | 94.73 | 0.02 |
| 92.54 | 1.44 | 96.99 | 0.06 |
| 95.06 | 0.93 | 98.64 | 0.05 |
| 97.13 | 0.51 | 99.66 | 0.02 |
| 100 | 0 | 100 | 0 |
| X | Y |
|---|---|
| 1 | 0 |
| 0.9713 | 0.0051 |
| 0.9506 | 0.0093 |
| 0.9254 | 0.0144 |
| 0.8959 | 0.0199 |
| 0.8625 | 0.0256 |
| 0.8254 | 0.0315 |
| 0.7851 | 0.0374 |
| 0.7422 | 0.0432 |
| 0.6971 | 0.0486 |
| 0.6502 | 0.0533 |
| 0.6019 | 0.0572 |
| 0.5526 | 0.0604 |
| 0.5027 | 0.0627 |
| 0.4528 | 0.0642 |
| 0.4034 | 0.0648 |
| 0.3549 | 0.0646 |
| 0.3079 | 0.0636 |
| 0.2629 | 0.0618 |
| 0.2203 | 0.0592 |
| 0.1807 | 0.0558 |
| 0.1443 | 0.0516 |
| 0.1116 | 0.0466 |
| 0.0827 | 0.041 |
| 0.058 | 0.0348 |
| 0.0375 | 0.028 |
| 0.0215 | 0.021 |
| 0.01 | 0.0137 |
| 0.0028 | 0.0066 |
| 0 | 0.0002 |
| 0 | 0.0002 |
| 0.0025 | -0.005 |
| 0.0107 | -0.0094 |
| 0.0242 | -0.0131 |
| 0.043 | -0.016 |
| 0.0669 | -0.0183 |
| 0.0958 | -0.02 |
| 0.1294 | -0.0211 |
| 0.1673 | -0.0218 |
| 0.209 | -0.0221 |
| 0.254 | -0.0221 |
| 0.3019 | -0.0217 |
| 0.3521 | -0.0211 |
| 0.404 | -0.0202 |
| 0.4569 | -0.0191 |
| 0.5104 | -0.0178 |
| 0.5637 | -0.0163 |
| 0.6162 | -0.0147 |
| 0.6674 | -0.0129 |
| 0.7167 | -0.0108 |
| 0.7637 | -0.0085 |
| 0.808 | -0.0062 |
| 0.8491 | -0.004 |
| 0.8863 | -0.0021 |
| 0.9193 | -0.0007 |
| 0.9473 | 0.0002 |
| 0.9699 | 0.0006 |
| 0.9864 | 0.0005 |
| 0.9966 | 0.0002 |
| 1 | 0 |
| X | Y |
|---|---|
| 100 | 0 |
| 97.13 | 0.51 |
| 95.06 | 0.93 |
| 92.54 | 1.44 |
| 89.59 | 1.99 |
| 86.25 | 2.56 |
| 82.54 | 3.15 |
| 78.51 | 3.74 |
| 74.22 | 4.32 |
| 69.71 | 4.86 |
| 65.02 | 5.33 |
| 60.19 | 5.72 |
| 55.26 | 6.04 |
| 50.27 | 6.27 |
| 45.28 | 6.42 |
| 40.34 | 6.48 |
| 35.49 | 6.46 |
| 30.79 | 6.36 |
| 26.29 | 6.18 |
| 22.03 | 5.92 |
| 18.07 | 5.58 |
| 14.43 | 5.16 |
| 11.16 | 4.66 |
| 8.27 | 4.1 |
| 5.8 | 3.48 |
| 3.75 | 2.8 |
| 2.15 | 2.1 |
| 1 | 1.37 |
| 0.28 | 0.66 |
| 0 | 0.02 |
| 0 | 0.02 |
| 0.25 | -0.5 |
| 1.07 | -0.94 |
| 2.42 | -1.31 |
| 4.3 | -1.6 |
| 6.69 | -1.83 |
| 9.58 | -2 |
| 12.94 | -2.11 |
| 16.73 | -2.18 |
| 20.9 | -2.21 |
| 25.4 | -2.21 |
| 30.19 | -2.17 |
| 35.21 | -2.11 |
| 40.4 | -2.02 |
| 45.69 | -1.91 |
| 51.04 | -1.78 |
| 56.37 | -1.63 |
| 61.62 | -1.47 |
| 66.74 | -1.29 |
| 71.67 | -1.08 |
| 76.37 | -0.85 |
| 80.8 | -0.62 |
| 84.91 | -0.4 |
| 88.63 | -0.21 |
| 91.93 | -0.07 |
| 94.73 | 0.02 |
| 96.99 | 0.06 |
| 98.64 | 0.05 |
| 99.66 | 0.02 |
| 100 | 0 |
V 1.1