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What is the thickness of NACA 0002 airfoil?

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in Aerodynamics by (773k points)
What is the thickness of NACA 0002 airfoil?

(a) 3%

(b) 1%

(c) 0%

(d) 2%

I had been asked this question in exam.

My question is based upon The Symmetric Airfoil topic in chapter Incompressible Flow over Airfoils of Aerodynamics

1 Answer

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Best answer
The correct choice is (d) 2%

Easiest explanation: The thickness of the NACA 0002 airfoil is 2 percent. There is no camber in the NACA 0002 airfoil because of the mean camber line and chord line intersect in the same line, so the position maximum camber in the NACA 0002 airfoil is zero.

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