Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|---|
| << First < Prev 41 42 43 44 45 Next > Last >> | ||||||
| PRD 2A | 12.95 | 30 | 3.852 | 40 | 1.744 | 0.0085 |
| PRD 2B | 12.25 | 30 | 4.725 | 40 | 1.371 | 0.0023 |
| PRD 2C | 8.66 | 30 | 3.399 | 30 | 1.091 | 0 |
| RAE 2822 | 12.09 | 37.85 | 1.263 | 75.71 | 0.903 | 0.0066 |
| RAE 5214 | 9.64 | 30.87 | 1.433 | 69.13 | 1.2 | 0.0042 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0 | 4.15 | 0 | 4.15 |
| 0.6 | 5.73 | 0.6 | 3.27 |
| 2.5 | 7.24 | 2.5 | 2.25 |
| 5 | 8.63 | 5 | 1.51 |
| 7.5 | 9.64 | 7.5 | 1 |
| 10 | 10.5 | 10 | 0.7 |
| 20 | 12.62 | 20 | 0.5 |
| 30 | 13.17 | 30 | 0.2 |
| 40 | 12.65 | 40 | 0 |
| 50 | 11.57 | 50 | 0 |
| 60 | 9.82 | 60 | 0 |
| 70 | 8 | 70 | 0 |
| 80 | 5.77 | 80 | 0 |
| 90 | 3.11 | 90 | 0 |
| 100 | 0 | 100 | 0 |
| X | Y |
|---|---|
| 1 | 0 |
| 0.9 | 0.0311 |
| 0.8 | 0.0577 |
| 0.7 | 0.08 |
| 0.6 | 0.0982 |
| 0.5 | 0.1157 |
| 0.4 | 0.1265 |
| 0.3 | 0.1317 |
| 0.2 | 0.1262 |
| 0.1 | 0.105 |
| 0.075 | 0.0964 |
| 0.05 | 0.0863 |
| 0.025 | 0.0724 |
| 0.006 | 0.0573 |
| 0 | 0.0415 |
| 0 | 0.0415 |
| 0.006 | 0.0327 |
| 0.025 | 0.0225 |
| 0.05 | 0.0151 |
| 0.075 | 0.01 |
| 0.1 | 0.007 |
| 0.2 | 0.005 |
| 0.3 | 0.002 |
| 0.4 | 0 |
| 0.5 | 0 |
| 0.6 | 0 |
| 0.7 | 0 |
| 0.8 | 0 |
| 0.9 | 0 |
| 1 | 0 |
| X | Y |
|---|---|
| 100 | 0 |
| 90 | 3.11 |
| 80 | 5.77 |
| 70 | 8 |
| 60 | 9.82 |
| 50 | 11.57 |
| 40 | 12.65 |
| 30 | 13.17 |
| 20 | 12.62 |
| 10 | 10.5 |
| 7.5 | 9.64 |
| 5 | 8.63 |
| 2.5 | 7.24 |
| 0.6 | 5.73 |
| 0 | 4.15 |
| 0 | 4.15 |
| 0.6 | 3.27 |
| 2.5 | 2.25 |
| 5 | 1.51 |
| 7.5 | 1 |
| 10 | 0.7 |
| 20 | 0.5 |
| 30 | 0.2 |
| 40 | 0 |
| 50 | 0 |
| 60 | 0 |
| 70 | 0 |
| 80 | 0 |
| 90 | 0 |
| 100 | 0 |
V 1.1