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)
0.04c, 0.03c
D)
0.13c, 0.4c

Correct Answer :   0.04c, 0.4c


Explanation : 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.