Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 0016 | 15.91 | 27.3202 | 0 | 0 | 1.332 | 0.0106 |
View
|
| P-51H ROOT | 15.49 | 44.98 | 1.333 | 47.5 | 1.223 | 0.0031 |
View
|
| KC-135 BL52.44 | 15.45 | 35 | 1.015 | 25 | 1.382 | 0.0079 |
View
|
| BOEING 737 ROOT AIRFOI | 15.33 | 19.61 | 0.233 | 4.95 | 1.372 | 0.011 |
View
|
| NACA 0015 | 15.01 | 28.73 | 0 | 0 | 1.287 | 0.0064 |
View
|
V 1.0