Which of these techniques is employed to delay the critical Mach number?

A)
Swept wing
B)
Increase camber
C)
Increasing the thickness of airfoil
D)
Decrease drag – divergence Mach number

Correct Answer :   Swept wing


Explanation : There are two ways employed to increase the critical Mach number thereby increasing drag – divergence Mach number. First is to reduce the thickness of the airfoil, and second is to add sweep to the wing.