What is the purpose of supercritical airfoil?
(a) Reduce critical Mach number
(b) Increase drag divergence Mach number
(c) Reduce drag divergence Mach number
(d) Increase lift of the airfoil at supersonic speed
I got this question in unit test.
Origin of the question is The Supercritical Airfoil topic in section Subsonic Compressible Flow over Airfoils : Linear Theory, Linearized Supersonic Flow of Aerodynamics