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LoginWhat 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
Aerodynamics Incompressible Flow over Airfoils in Aerodynamics 3 years ago
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.
Posted on 02 Dec 2021, this text provides information on Aerodynamics related to Incompressible Flow over Airfoils in Aerodynamics. Please note that while accuracy is prioritized, the data presented might not be entirely correct or up-to-date. This information is offered for general knowledge and informational purposes only, and should not be considered as a substitute for professional advice.
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