See Graphic
NACA Airfoil |
Sectional Maximum Lift Coefficient,
|
0006 |
0.92 |
0009 |
1.32 |
0012 |
1.50 |
1408 |
1.35 |
1412 |
1.58 |
2412 |
1.68 |
2418 |
1.47 |
2424 |
1.29 |
4412 |
1.67 |
4418 |
1.53 |
4424 |
1.38 |
23012 |
1.79 |
23018 |
1.60 |
23024 |
1.40 |
63-006 |
0.87 |
63-009 |
1.15 |
63,1-012 |
1.45 |
63,2-015 |
1.47 |
63,3-018 |
1.54 |
63,1-212 |
1.63 |
63,1-412 |
1.77 |
64-006 |
0.80 |
64-009 |
1.17 |
64-206 |
1.03 |
64-209 |
1.40 |
64-210 |
1.45 |
64,1-012 |
1.45 |
64,1-212 |
1.55 |
64,1-412 |
1.67 |
65-006 |
0.92 |
65-009 |
1.08 |
65-206 |
1.03 |
65-209 |
1.30 |
65-210 |
1.40 |
65,1-212 |
1.47 |
65,1-412 |
1.66 |
65,2-015 |
1.42 |
65,3-018 |
1.37 |
63A010 |
1.20 |
63A210 |
1.43 |
64A010 |
1.28 |
64A210 |
1.44 |
64A410 |
1.61 |
64,1-A212 |
1.54 |
64,2-A215 |
1.50 |