For NACA4313 what is the maximum camber and the position of maximum camber from the leading edge respectively is______

For NACA4313 what is the maximum camber and the position of maximum camber from the leading edge respectively is______ Correct Answer 0.04c, 0.4c

For NACA 4 digit airfoils the first digit gives the maximum camber in 100th parts of the chord length c and the second digit gives the position of maximum camber in 10th parts of the chord length from the leading edge.
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