The defining assumption for finding the skin- friction drag on an airfoil is____
(a) Airfoil is new low-speed airfoil
(b) Skin- friction acts due to shear force
(c) Airfoil has a zero angle of attack
(d) Airfoil is considered a flat plate at zero angle of attack
The question was asked by my school principal while I was bunking the class.
I would like to ask this question from Laminar Flow topic in portion Incompressible Flow over Airfoils of Aerodynamics