NACA Airfoil |
Sectional Zero-Lift Angle-of-Attack,
|
0006 |
0.0 |
0009 |
0.0 |
0012 |
0.0 |
1408 |
-0.8 |
1412 |
-1.1 |
2412 |
-2.0 |
2418 |
-2.8 |
2424 |
-1.8 |
4412 |
-3.8 |
4418 |
-3.8 |
4424 |
-3.8 |
23012 |
-1.4 |
23018 |
-1.2 |
23024 |
-0.8 |
63-006 |
0.0 |
63-009 |
0.0 |
63,1-012 |
0.0 |
63,2-015 |
0.0 |
63,3-018 |
0.0 |
63,1-212 |
-2.0 |
63,1-412 |
-2.8 |
64-006 |
0.0 |
64-009 |
0.0 |
64-206 |
-1.0 |
64-209 |
-1.5 |
64-210 |
-1.6 |
64,1-012 |
0.0 |
64,1-212 |
-1.3 |
64,1-412 |
-2.6 |
65-006 |
0.0 |
65-009 |
0.0 |
65-206 |
-1.6 |
65-209 |
-1.2 |
65-210 |
-1.6 |
65,1-212 |
-1.0 |
65,1-412 |
-3.0 |
65,2-015 |
0.0 |
65,3-018 |
0.0 |
63A010 |
0.0 |
63A210 |
-1.5 |
64A010 |
0.0 |
64A210 |
-1.5 |
64A410 |
-3.0 |
64,1-A212 |
-2.0 |
64,2-A215 |
-2.0 |