Camber of an airfoil is
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100%
maximum distance between the mean camber line and the chord line and is measured perpendicular to this chord line
0%
a line of the locus of points that is halfway between the upper and lower surfaces which is measured perpendicular to this line itself
0%
thickness between the upper and lower surfaces of the airfoil
0%
straight line connecting the leading and the trailing edges of the airfoil
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