4. An NACA 2415 airfoil has a chord length of 2 meters.

a. What is the maximum thickness of this airfoil?

b. What is the maximum camber of this airfoil and where is it located?

c. What is the value of the lift slope?

a. What is the maximum thickness of this airfoil?

b. What is the maximum camber of this airfoil and where is it located?

c. What is the value of the lift slope?

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