Right option is (b) False
To elaborate: The shape of the airfoil in (x, y) space is given by y = f(x) and in (ξ, η) space is given by η = q(ξ). Since \(\frac {df}{dx} = \frac {dq}{dξ}\) hence the shape of the airfoil in both the spaces irrespective of the transformation remains same.