For NACA4313 what is the maximum camber and the position of maximum camber from the leading edge respectively is______(a) 0.04c, 0.4c(b) 0.4c, 0.03c(c) 0.13c, 0.4c(d) 0.04c, 0.03cI had been asked this question in an internship interview.Origin of the question is The Cambered Airfoil topic in chapter Incompressible Flow over Airfoils of Aerodynamics

For NACA4313 what is the maximum camber and the position of maximum ca

1.	For NACA4313 what is the maximum camber and the position of maximum camber from the leading edge respectively is______(a) 0.04c, 0.4c(b) 0.4c, 0.03c(c) 0.13c, 0.4c(d) 0.04c, 0.03cI had been asked this question in an internship interview.Origin of the question is The Cambered Airfoil topic in chapter Incompressible Flow over Airfoils of Aerodynamics
Answer» The correct choice is (a) 0.04c, 0.4c To explain I WOULD say: For NACA 4 digit airfoils the first digit GIVES the maximum camber in 100^th parts of the chord LENGTH c and the second digit gives the POSITION of maximum camber in 10^th parts of the chord length from the leading EDGE.

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