Winfoil Airfoils - Total Number: 277
        | Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min | 
|---|---|---|---|---|---|---|
| << First < Prev 51 52 53 54 55 Next > Last >> | ||||||
| SD7003 | 8.5 | 24.36 | 1.584 | 33.41 | 1.124 | 0.0064 | 
| SD7032 | 9.96 | 26.6 | 3.79 | 40.22 | 1.453 | 0.0066 | 
| SD7037 | 9.19 | 26.13 | 2.905 | 44.75 | 1.301 | 0.0062 | 
| SD7043 | 9.13 | 26.64 | 3.664 | 45.28 | 1.461 | 0.0058 | 
| SD7062 | 13.97 | 25.5 | 4.167 | 38.78 | 1.77 | 0.0077 | 
Coordinates
        
        | XUpper | YUpper | XLower | YLower | 
|---|---|---|---|
| 0.03 | -0.19 | 0.03 | -0.19 | 
| 0.13 | 0.44 | 0.46 | -0.74 | 
| 0.7 | 1.17 | 1.41 | -1.29 | 
| 1.7 | 1.93 | 2.84 | -1.76 | 
| 3.13 | 2.68 | 4.76 | -2.14 | 
| 4.98 | 3.37 | 7.18 | -2.44 | 
| 7.24 | 3.99 | 10.07 | -2.66 | 
| 9.92 | 4.53 | 13.41 | -2.81 | 
| 12.99 | 4.96 | 17.15 | -2.89 | 
| 16.44 | 5.29 | 21.27 | -2.9 | 
| 20.24 | 5.52 | 25.72 | -2.85 | 
| 24.36 | 5.64 | 30.46 | -2.75 | 
| 28.76 | 5.66 | 35.43 | -2.61 | 
| 33.41 | 5.58 | 40.57 | -2.43 | 
| 38.25 | 5.42 | 45.84 | -2.22 | 
| 43.25 | 5.17 | 51.16 | -1.98 | 
| 48.35 | 4.86 | 56.48 | -1.72 | 
| 53.5 | 4.49 | 61.75 | -1.45 | 
| 58.64 | 4.09 | 66.9 | -1.17 | 
| 63.72 | 3.65 | 71.88 | -0.89 | 
| 68.67 | 3.2 | 76.64 | -0.63 | 
| 73.45 | 2.74 | 81.12 | -0.4 | 
| 77.99 | 2.3 | 85.24 | -0.22 | 
| 82.22 | 1.88 | 88.96 | -0.08 | 
| 86.11 | 1.49 | 92.21 | 0.01 | 
| 89.6 | 1.14 | 94.95 | 0.05 | 
| 92.64 | 0.82 | 97.13 | 0.06 | 
| 95.19 | 0.55 | 98.72 | 0.04 | 
| 97.24 | 0.31 | 99.68 | 0.01 | 
| 100 | 0 | 100 | 0 | 
| X | Y | 
|---|---|
| 1 | 0 | 
| 0.9724 | 0.0031 | 
| 0.9519 | 0.0055 | 
| 0.9264 | 0.0082 | 
| 0.896 | 0.0114 | 
| 0.8611 | 0.0149 | 
| 0.8222 | 0.0188 | 
| 0.7799 | 0.023 | 
| 0.7345 | 0.0274 | 
| 0.6867 | 0.032 | 
| 0.6372 | 0.0365 | 
| 0.5864 | 0.0409 | 
| 0.535 | 0.0449 | 
| 0.4835 | 0.0486 | 
| 0.4325 | 0.0517 | 
| 0.3825 | 0.0542 | 
| 0.3341 | 0.0558 | 
| 0.2876 | 0.0566 | 
| 0.2436 | 0.0564 | 
| 0.2024 | 0.0552 | 
| 0.1644 | 0.0529 | 
| 0.1299 | 0.0496 | 
| 0.0992 | 0.0453 | 
| 0.0724 | 0.0399 | 
| 0.0498 | 0.0337 | 
| 0.0313 | 0.0268 | 
| 0.017 | 0.0193 | 
| 0.007 | 0.0117 | 
| 0.0013 | 0.0044 | 
| 0.0003 | -0.0019 | 
| 0.0003 | -0.0019 | 
| 0.0046 | -0.0074 | 
| 0.0141 | -0.0129 | 
| 0.0284 | -0.0176 | 
| 0.0476 | -0.0214 | 
| 0.0718 | -0.0244 | 
| 0.1007 | -0.0266 | 
| 0.1341 | -0.0281 | 
| 0.1715 | -0.0289 | 
| 0.2127 | -0.029 | 
| 0.2572 | -0.0285 | 
| 0.3046 | -0.0275 | 
| 0.3543 | -0.0261 | 
| 0.4057 | -0.0243 | 
| 0.4584 | -0.0222 | 
| 0.5116 | -0.0198 | 
| 0.5648 | -0.0172 | 
| 0.6175 | -0.0145 | 
| 0.669 | -0.0117 | 
| 0.7188 | -0.0089 | 
| 0.7664 | -0.0063 | 
| 0.8112 | -0.004 | 
| 0.8524 | -0.0022 | 
| 0.8896 | -0.0008 | 
| 0.9221 | 0.0001 | 
| 0.9495 | 0.0005 | 
| 0.9713 | 0.0006 | 
| 0.9872 | 0.0004 | 
| 0.9968 | 0.0001 | 
| 1 | 0 | 
| X | Y | 
|---|---|
| 100 | 0 | 
| 97.24 | 0.31 | 
| 95.19 | 0.55 | 
| 92.64 | 0.82 | 
| 89.6 | 1.14 | 
| 86.11 | 1.49 | 
| 82.22 | 1.88 | 
| 77.99 | 2.3 | 
| 73.45 | 2.74 | 
| 68.67 | 3.2 | 
| 63.72 | 3.65 | 
| 58.64 | 4.09 | 
| 53.5 | 4.49 | 
| 48.35 | 4.86 | 
| 43.25 | 5.17 | 
| 38.25 | 5.42 | 
| 33.41 | 5.58 | 
| 28.76 | 5.66 | 
| 24.36 | 5.64 | 
| 20.24 | 5.52 | 
| 16.44 | 5.29 | 
| 12.99 | 4.96 | 
| 9.92 | 4.53 | 
| 7.24 | 3.99 | 
| 4.98 | 3.37 | 
| 3.13 | 2.68 | 
| 1.7 | 1.93 | 
| 0.7 | 1.17 | 
| 0.13 | 0.44 | 
| 0.03 | -0.19 | 
| 0.03 | -0.19 | 
| 0.46 | -0.74 | 
| 1.41 | -1.29 | 
| 2.84 | -1.76 | 
| 4.76 | -2.14 | 
| 7.18 | -2.44 | 
| 10.07 | -2.66 | 
| 13.41 | -2.81 | 
| 17.15 | -2.89 | 
| 21.27 | -2.9 | 
| 25.72 | -2.85 | 
| 30.46 | -2.75 | 
| 35.43 | -2.61 | 
| 40.57 | -2.43 | 
| 45.84 | -2.22 | 
| 51.16 | -1.98 | 
| 56.48 | -1.72 | 
| 61.75 | -1.45 | 
| 66.9 | -1.17 | 
| 71.88 | -0.89 | 
| 76.64 | -0.63 | 
| 81.12 | -0.4 | 
| 85.24 | -0.22 | 
| 88.96 | -0.08 | 
| 92.21 | 0.01 | 
| 94.95 | 0.05 | 
| 97.13 | 0.06 | 
| 98.72 | 0.04 | 
| 99.68 | 0.01 | 
| 100 | 0 | 
V 1.1