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The critical Mach number of an airfoil is attained when

An airfoil generates a lift of 80 N when operating in a free

Consider a supersonic stream at a Mach number M=2, undergoin

Mach number is defined as the ratio of the local flow veloci

An aircraft is flying at Mach number M = 1.5, where the ambi

An aircraft is flying at Mach number M = 1.5, where the ambi

The Mach angle for a flow at Mach 2.0 is

The critical Mach number for a flat plate of zero thickness,

Group-I contains dimensionless parameters and Group- II cont

Consider an airplane with rectangular straight wing at dihed