Winfoil Airfoils - Total Number: 277
| Name | T/C % | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|
| << First < Prev 40 41 42 43 44 Next > Last >> | |||||
| NASA/LANGLEY SC(2)-0714 | 13.97 | 2.246 | 81 | 1.52 | 0.0144 |
| P-51D ROOT (BL17.5) | 16.45 | 1.266 | 68.267 | 1.482 | 0.0063 |
| P-51D TIP (BL215) | 11.37 | 1.313 | 46.26 | 0.958 | 0.0054 |
| P-51H ROOT | 15.49 | 1.333 | 47.5 | 1.223 | 0.0031 |
| P-51H TIP | 11.99 | 1.332 | 47.5 | 0.895 | 0.0062 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0 | 0 | 0 | 0 |
| 0.2 | 1.08 | 0.2 | -1.08 |
| 0.5 | 1.67 | 0.5 | -1.65 |
| 1 | 2.25 | 1 | -2.23 |
| 2 | 2.97 | 2 | -2.95 |
| 3 | 3.46 | 3 | -3.43 |
| 4 | 3.83 | 4 | -3.81 |
| 5 | 4.14 | 5 | -4.11 |
| 6 | 4.4 | 6 | -4.38 |
| 7 | 4.63 | 7 | -4.61 |
| 8 | 4.84 | 8 | -4.81 |
| 9 | 5.02 | 9 | -5 |
| 10 | 5.19 | 10 | -5.17 |
| 11 | 5.35 | 11 | -5.33 |
| 12 | 5.49 | 12 | -5.47 |
| 13 | 5.62 | 13 | -5.61 |
| 14 | 5.74 | 14 | -5.74 |
| 15 | 5.85 | 15 | -5.85 |
| 16 | 5.96 | 16 | -5.96 |
| 17 | 6.06 | 17 | -6.06 |
| 18 | 6.15 | 18 | -6.16 |
| 19 | 6.24 | 19 | -6.25 |
| 20 | 6.32 | 20 | -6.33 |
| 21 | 6.4 | 21 | -6.41 |
| 22 | 6.47 | 22 | -6.48 |
| 23 | 6.53 | 23 | -6.55 |
| 24 | 6.59 | 24 | -6.61 |
| 25 | 6.65 | 25 | -6.67 |
| 26 | 6.7 | 26 | -6.72 |
| 27 | 6.75 | 27 | -6.77 |
| 28 | 6.79 | 28 | -6.81 |
| 29 | 6.83 | 29 | -6.85 |
| 30 | 6.86 | 30 | -6.88 |
| 31 | 6.89 | 31 | -6.91 |
| 32 | 6.92 | 32 | -6.93 |
| 33 | 6.94 | 33 | -6.95 |
| 34 | 6.96 | 34 | -6.96 |
| 35 | 6.98 | 35 | -6.97 |
| 36 | 6.99 | 36 | -6.97 |
| 37 | 7 | 37 | -6.97 |
| 38 | 7 | 38 | -6.96 |
| 39 | 7 | 39 | -6.95 |
| 40 | 7 | 40 | -6.93 |
| 41 | 6.99 | 41 | -6.91 |
| 42 | 6.98 | 42 | -6.89 |
| 43 | 6.97 | 43 | -6.86 |
| 44 | 6.96 | 44 | -6.82 |
| 45 | 6.94 | 45 | -6.78 |
| 46 | 6.92 | 46 | -6.73 |
| 47 | 6.89 | 47 | -6.67 |
| 48 | 6.86 | 48 | -6.61 |
| 49 | 6.83 | 49 | -6.54 |
| 50 | 6.8 | 50 | -6.46 |
| 51 | 6.76 | 51 | -6.37 |
| 52 | 6.72 | 52 | -6.27 |
| 53 | 6.68 | 53 | -6.16 |
| 54 | 6.63 | 54 | -6.04 |
| 55 | 6.58 | 55 | -5.91 |
| 56 | 6.52 | 56 | -5.77 |
| 57 | 6.46 | 57 | -5.62 |
| 58 | 6.4 | 58 | -5.46 |
| 59 | 6.34 | 59 | -5.29 |
| 60 | 6.27 | 60 | -5.11 |
| 61 | 6.2 | 61 | -4.93 |
| 62 | 6.13 | 62 | -4.74 |
| 63 | 6.05 | 63 | -4.54 |
| 64 | 5.96 | 64 | -4.34 |
| 65 | 5.87 | 65 | -4.13 |
| 66 | 5.78 | 66 | -3.92 |
| 67 | 5.68 | 67 | -3.71 |
| 68 | 5.58 | 68 | -3.49 |
| 69 | 5.47 | 69 | -3.27 |
| 70 | 5.36 | 70 | -3.05 |
| 71 | 5.24 | 71 | -2.83 |
| 72 | 5.12 | 72 | -2.61 |
| 73 | 4.99 | 73 | -2.39 |
| 74 | 4.86 | 74 | -2.17 |
| 75 | 4.72 | 75 | -1.95 |
| 76 | 4.57 | 76 | -1.73 |
| 77 | 4.42 | 77 | -1.52 |
| 78 | 4.26 | 78 | -1.32 |
| 79 | 4.09 | 79 | -1.13 |
| 80 | 3.92 | 80 | -0.95 |
| 81 | 3.74 | 81 | -0.79 |
| 82 | 3.56 | 82 | -0.64 |
| 83 | 3.37 | 83 | -0.5 |
| 84 | 3.17 | 84 | -0.38 |
| 85 | 2.97 | 85 | -0.28 |
| 86 | 2.76 | 86 | -0.2 |
| 87 | 2.55 | 87 | -0.14 |
| 88 | 2.33 | 88 | -0.1 |
| 89 | 2.1 | 89 | -0.08 |
| 90 | 1.86 | 90 | -0.08 |
| 91 | 1.62 | 91 | -0.11 |
| 92 | 1.37 | 92 | -0.16 |
| 93 | 1.11 | 93 | -0.24 |
| 94 | 0.84 | 94 | -0.35 |
| 95 | 0.57 | 95 | -0.49 |
| 96 | 0.29 | 96 | -0.66 |
| 97 | 0 | 97 | -0.86 |
| 98 | -0.3 | 98 | -1.09 |
| 99 | -0.62 | 99 | -1.36 |
| 100 | -0.95 | 100 | -1.65 |
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