Question: The NACA 4412 airfoil has a mean camber line given by Using thin airfoil theory, calculate (a) ?L = 0 (b) c1 when ? =

The NACA 4412 airfoil has a mean camber line given by Using thin airfoil theory, calculate

(a) ?L = 0

(b) c1 when ? = 3?

[0.25 [0.8 +- (-)] 10.11 [0.2+0.8-()] C X for 0 0.4 C

[0.25 [0.8 +- (-)] 10.11 [0.2+0.8-()] C X for 0 0.4 C X for 0.4-1 C

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