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|
Comparing Airfoils
NACA 63-015A AIRFOIL
NACA M10 AIRFOIL
|
NACA 63-015A AIRFOIL |
NACA M10 AIRFOIL |
|---|
| Thickness (%) |
14.991 |
6.189 |
| Camber (%) |
0.051 |
1.909 |
| Trailing Edge Angle (%) |
17.196 |
10.372 |
| Lower Surface Flatness |
20.890 |
97.656 |
| Leading Edge Radius (%) |
1.945 |
2.361 |
Maximum Lift (CL) |
0.995 |
0.810 |
Maximum Lift Angle-of-Attack (deg) |
15.000 |
12.500 |
Maximum Lift-to-drag (L/D) |
36.354 |
30.065 |
Lift at Maximum Lift-to-drag |
0.769 |
0.483 |
Angle-of-Attack for Maximum Lift-to-drag (L/D) |
7.000 |
3.000 |
|
