Winfoil Airfoils - Total Number: 277
| Name | T/C % | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|
| << First < Prev 38 39 40 41 42 Next > Last >> | |||||
| EPPLER 62 (5.62%) | 5.66 | 5.307 | 49.334 | 1.302 | 0.0058 |
| EPPLER 61 | 6.15 | 6.517 | 50 | 1.149 | 0.0005 |
| EPPLER 397 | 13.5 | 5.331 | 52.1 | 1.47 | 0.0017 |
| EPPLER 387 | 9.07 | 3.797 | 40.08 | 1.199 | 0.0064 |
| EPPLER 378 | 4.08 | 8.109 | 35.92 | 1.686 | 0.0014 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0.024 | 0.14 | 0.024 | 0.14 |
| 0.421 | 0.72 | 0.115 | -0.24 |
| 1.238 | 1.4 | 0.762 | -0.44 |
| 2.476 | 2.14 | 1.974 | -0.53 |
| 4.133 | 2.91 | 3.744 | -0.5 |
| 6.202 | 3.66 | 6.068 | -0.35 |
| 8.672 | 4.4 | 8.936 | -0.09 |
| 11.523 | 5.09 | 12.328 | 0.23 |
| 14.736 | 5.73 | 16.216 | 0.63 |
| 18.28 | 6.3 | 20.561 | 1.06 |
| 22.126 | 6.8 | 25.315 | 1.5 |
| 26.238 | 7.22 | 30.425 | 1.92 |
| 30.578 | 7.54 | 35.828 | 2.31 |
| 35.102 | 7.77 | 41.449 | 2.62 |
| 39.768 | 7.9 | 47.195 | 2.85 |
| 44.527 | 7.93 | 52.982 | 2.99 |
| 49.334 | 7.86 | 58.733 | 3.05 |
| 54.145 | 7.66 | 64.371 | 3.03 |
| 58.925 | 7.36 | 69.823 | 2.92 |
| 63.636 | 6.95 | 75.016 | 2.75 |
| 68.242 | 6.46 | 79.879 | 2.5 |
| 72.697 | 5.9 | 84.347 | 2.19 |
| 76.951 | 5.3 | 88.357 | 1.84 |
| 80.955 | 4.66 | 91.854 | 1.46 |
| 84.665 | 4.01 | 94.785 | 1.05 |
| 88.036 | 3.36 | 97.092 | 0.65 |
| 91.03 | 2.71 | 98.725 | 0.3 |
| 93.61 | 2.08 | 99.685 | 0.07 |
| 100 | 0 | 100 | 0 |
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