Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|---|
| 1 2 3 4 5 Next > Last >> | ||||||
| WB14035 | 13.92 | 30 | 3.58 | 45 | 1.58 | 0.0099 |
| WB13535 | 13.54 | 25 | 3.747 | 50 | 0.84 | 0.0241 |
| USA 50 AIRFOIL | 7.01 | 30 | 1.953 | 40 | 0.986 | 0.005 |
| TSAGI 8% AIRFOIL | 7.94 | 30 | 1.343 | 30 | 0.923 | 0.0045 |
| TSAGI 12% AIRFOIL | 11.88 | 30 | 2.003 | 30 | 1.217 | 0.0058 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0 | 0 | 0 | 0 |
| 1.25 | 1.875 | 1.25 | -1.35 |
| 2.5 | 3 | 2.5 | -1.8 |
| 5 | 4.63 | 5 | -2.65 |
| 7.5 | 5.9 | 7.5 | -3.275 |
| 10 | 6.95 | 10 | -3.675 |
| 12.5 | 7.7 | 12.5 | -3.95 |
| 15 | 8.325 | 15 | -4.05 |
| 17.5 | 8.83 | 17.5 | -4.075 |
| 20 | 9.225 | 20 | -4.05 |
| 22.5 | 9.55 | 22.5 | -4.025 |
| 25 | 9.775 | 25 | -3.95 |
| 27.5 | 10.05 | 27.5 | -3.8 |
| 30 | 10.225 | 30 | -3.7 |
| 35 | 10.45 | 35 | -3.475 |
| 40 | 10.45 | 40 | -3.225 |
| 45 | 10.365 | 45 | -2.975 |
| 50 | 10.125 | 50 | -2.75 |
| 55 | 9.725 | 55 | -2.475 |
| 60 | 9.1 | 60 | -2.275 |
| 65 | 8.3 | 65 | -2.05 |
| 70 | 7.1 | 70 | -1.8 |
| 75 | 6.275 | 75 | -1.575 |
| 80 | 5.15 | 80 | -1.3 |
| 85 | 4 | 85 | -1.025 |
| 90 | 2.775 | 90 | -0.8 |
| 95 | 1.475 | 95 | -0.5 |
| 100 | 0.25 | 100 | -0.25 |
| X | Y |
|---|---|
| 1 | 0.0025 |
| 0.95 | 0.01475 |
| 0.9 | 0.02775 |
| 0.85 | 0.04 |
| 0.8 | 0.0515 |
| 0.75 | 0.06275 |
| 0.7 | 0.071 |
| 0.65 | 0.083 |
| 0.6 | 0.091 |
| 0.55 | 0.09725 |
| 0.5 | 0.10125 |
| 0.45 | 0.10365 |
| 0.4 | 0.1045 |
| 0.35 | 0.1045 |
| 0.3 | 0.10225 |
| 0.275 | 0.1005 |
| 0.25 | 0.09775 |
| 0.225 | 0.0955 |
| 0.2 | 0.09225 |
| 0.175 | 0.0883 |
| 0.15 | 0.08325 |
| 0.125 | 0.077 |
| 0.1 | 0.0695 |
| 0.075 | 0.059 |
| 0.05 | 0.0463 |
| 0.025 | 0.03 |
| 0.0125 | 0.01875 |
| 0 | 0 |
| 0 | 0 |
| 0.0125 | -0.0135 |
| 0.025 | -0.018 |
| 0.05 | -0.0265 |
| 0.075 | -0.03275 |
| 0.1 | -0.03675 |
| 0.125 | -0.0395 |
| 0.15 | -0.0405 |
| 0.175 | -0.04075 |
| 0.2 | -0.0405 |
| 0.225 | -0.04025 |
| 0.25 | -0.0395 |
| 0.275 | -0.038 |
| 0.3 | -0.037 |
| 0.35 | -0.03475 |
| 0.4 | -0.03225 |
| 0.45 | -0.02975 |
| 0.5 | -0.0275 |
| 0.55 | -0.02475 |
| 0.6 | -0.02275 |
| 0.65 | -0.0205 |
| 0.7 | -0.018 |
| 0.75 | -0.01575 |
| 0.8 | -0.013 |
| 0.85 | -0.01025 |
| 0.9 | -0.008 |
| 0.95 | -0.005 |
| 1 | -0.0025 |
| X | Y |
|---|---|
| 100 | 0.25 |
| 95 | 1.475 |
| 90 | 2.775 |
| 85 | 4 |
| 80 | 5.15 |
| 75 | 6.275 |
| 70 | 7.1 |
| 65 | 8.3 |
| 60 | 9.1 |
| 55 | 9.725 |
| 50 | 10.125 |
| 45 | 10.365 |
| 40 | 10.45 |
| 35 | 10.45 |
| 30 | 10.225 |
| 27.5 | 10.05 |
| 25 | 9.775 |
| 22.5 | 9.55 |
| 20 | 9.225 |
| 17.5 | 8.83 |
| 15 | 8.325 |
| 12.5 | 7.7 |
| 10 | 6.95 |
| 7.5 | 5.9 |
| 5 | 4.63 |
| 2.5 | 3 |
| 1.25 | 1.875 |
| 0 | 0 |
| 0 | 0 |
| 1.25 | -1.35 |
| 2.5 | -1.8 |
| 5 | -2.65 |
| 7.5 | -3.275 |
| 10 | -3.675 |
| 12.5 | -3.95 |
| 15 | -4.05 |
| 17.5 | -4.075 |
| 20 | -4.05 |
| 22.5 | -4.025 |
| 25 | -3.95 |
| 27.5 | -3.8 |
| 30 | -3.7 |
| 35 | -3.475 |
| 40 | -3.225 |
| 45 | -2.975 |
| 50 | -2.75 |
| 55 | -2.475 |
| 60 | -2.275 |
| 65 | -2.05 |
| 70 | -1.8 |
| 75 | -1.575 |
| 80 | -1.3 |
| 85 | -1.025 |
| 90 | -0.8 |
| 95 | -0.5 |
| 100 | -0.25 |
V 1.1