Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|---|
| << First < Prev 46 47 48 49 50 Next > Last >> | ||||||
| S2048.COR | 8.62 | 35.35 | 1.952 | 55.17 | 1.07 | 0.0059 |
| S2055 | 7.98 | 34.76 | 1.716 | 39.63 | 1.048 | 0.0056 |
| S2091 | 10.1 | 26.04 | 4.104 | 39.45 | 1.477 | 0.006 |
| S3010 | 10.32 | 24.97 | 2.769 | 38.44 | 1.345 | 0.0064 |
| S3014 | 9.45 | 29.35 | 2.571 | 38.63 | 1.189 | 0.0054 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0 | -0.03 | 0 | -0.03 |
| 0.25 | 0.55 | 0.31 | -0.51 |
| 0.95 | 1.22 | 1.2 | -0.94 |
| 2.11 | 1.91 | 2.6 | -1.34 |
| 3.72 | 2.59 | 4.52 | -1.67 |
| 5.77 | 3.26 | 6.94 | -1.93 |
| 8.23 | 3.89 | 9.85 | -2.15 |
| 11.09 | 4.46 | 13.21 | -2.33 |
| 14.32 | 4.94 | 16.97 | -2.46 |
| 17.93 | 5.32 | 21.1 | -2.55 |
| 21.88 | 5.62 | 25.53 | -2.6 |
| 26.13 | 5.85 | 30.23 | -2.6 |
| 30.64 | 6 | 35.13 | -2.55 |
| 35.35 | 6.09 | 40.19 | -2.43 |
| 40.21 | 6.09 | 45.36 | -2.26 |
| 45.17 | 6.03 | 50.6 | -2.03 |
| 50.18 | 5.88 | 55.85 | -1.74 |
| 55.17 | 5.65 | 61.08 | -1.4 |
| 60.12 | 5.33 | 66.26 | -1.05 |
| 64.97 | 4.93 | 71.3 | -0.72 |
| 69.69 | 4.47 | 76.14 | -0.44 |
| 74.24 | 3.95 | 80.7 | -0.21 |
| 78.57 | 3.42 | 84.91 | -0.04 |
| 82.62 | 2.88 | 88.71 | 0.07 |
| 86.34 | 2.35 | 92.04 | 0.12 |
| 89.68 | 1.83 | 94.83 | 0.13 |
| 92.62 | 1.32 | 97.06 | 0.1 |
| 95.13 | 0.86 | 98.68 | 0.06 |
| 97.17 | 0.47 | 99.67 | 0.02 |
| 100 | 0 | 100 | 0 |
| X | Y |
|---|---|
| 1 | 0 |
| 0.9717 | 0.0047 |
| 0.9513 | 0.0086 |
| 0.9262 | 0.0132 |
| 0.8968 | 0.0183 |
| 0.8634 | 0.0235 |
| 0.8262 | 0.0288 |
| 0.7857 | 0.0342 |
| 0.7424 | 0.0395 |
| 0.6969 | 0.0447 |
| 0.6497 | 0.0493 |
| 0.6012 | 0.0533 |
| 0.5517 | 0.0565 |
| 0.5018 | 0.0588 |
| 0.4517 | 0.0603 |
| 0.4021 | 0.0609 |
| 0.3535 | 0.0609 |
| 0.3064 | 0.06 |
| 0.2613 | 0.0585 |
| 0.2188 | 0.0562 |
| 0.1793 | 0.0532 |
| 0.1432 | 0.0494 |
| 0.1109 | 0.0446 |
| 0.0823 | 0.0389 |
| 0.0577 | 0.0326 |
| 0.0372 | 0.0259 |
| 0.0211 | 0.0191 |
| 0.0095 | 0.0122 |
| 0.0025 | 0.0055 |
| 0 | -0.0003 |
| 0 | -0.0003 |
| 0.0031 | -0.0051 |
| 0.012 | -0.0094 |
| 0.026 | -0.0134 |
| 0.0452 | -0.0167 |
| 0.0694 | -0.0193 |
| 0.0985 | -0.0215 |
| 0.1321 | -0.0233 |
| 0.1697 | -0.0246 |
| 0.211 | -0.0255 |
| 0.2553 | -0.026 |
| 0.3023 | -0.026 |
| 0.3513 | -0.0255 |
| 0.4019 | -0.0243 |
| 0.4536 | -0.0226 |
| 0.506 | -0.0203 |
| 0.5585 | -0.0174 |
| 0.6108 | -0.014 |
| 0.6626 | -0.0105 |
| 0.713 | -0.0072 |
| 0.7614 | -0.0044 |
| 0.807 | -0.0021 |
| 0.8491 | -0.0004 |
| 0.8871 | 0.0007 |
| 0.9204 | 0.0012 |
| 0.9483 | 0.0013 |
| 0.9706 | 0.001 |
| 0.9868 | 0.0006 |
| 0.9967 | 0.0002 |
| 1 | 0 |
| X | Y |
|---|---|
| 100 | 0 |
| 97.17 | 0.47 |
| 95.13 | 0.86 |
| 92.62 | 1.32 |
| 89.68 | 1.83 |
| 86.34 | 2.35 |
| 82.62 | 2.88 |
| 78.57 | 3.42 |
| 74.24 | 3.95 |
| 69.69 | 4.47 |
| 64.97 | 4.93 |
| 60.12 | 5.33 |
| 55.17 | 5.65 |
| 50.18 | 5.88 |
| 45.17 | 6.03 |
| 40.21 | 6.09 |
| 35.35 | 6.09 |
| 30.64 | 6 |
| 26.13 | 5.85 |
| 21.88 | 5.62 |
| 17.93 | 5.32 |
| 14.32 | 4.94 |
| 11.09 | 4.46 |
| 8.23 | 3.89 |
| 5.77 | 3.26 |
| 3.72 | 2.59 |
| 2.11 | 1.91 |
| 0.95 | 1.22 |
| 0.25 | 0.55 |
| 0 | -0.03 |
| 0 | -0.03 |
| 0.31 | -0.51 |
| 1.2 | -0.94 |
| 2.6 | -1.34 |
| 4.52 | -1.67 |
| 6.94 | -1.93 |
| 9.85 | -2.15 |
| 13.21 | -2.33 |
| 16.97 | -2.46 |
| 21.1 | -2.55 |
| 25.53 | -2.6 |
| 30.23 | -2.6 |
| 35.13 | -2.55 |
| 40.19 | -2.43 |
| 45.36 | -2.26 |
| 50.6 | -2.03 |
| 55.85 | -1.74 |
| 61.08 | -1.4 |
| 66.26 | -1.05 |
| 71.3 | -0.72 |
| 76.14 | -0.44 |
| 80.7 | -0.21 |
| 84.91 | -0.04 |
| 88.71 | 0.07 |
| 92.04 | 0.12 |
| 94.83 | 0.13 |
| 97.06 | 0.1 |
| 98.68 | 0.06 |
| 99.67 | 0.02 |
| 100 | 0 |
V 1.1