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.In aerodynamics, the critical mach number (mcr or m*) of an aircraft is the lowest mach number at which the airflow over some point of the aircraft reaches the speed of sound, but does not exceed it.
In aerodynamics, the critical mach number (mcr or m*) of an aircraft is the lowest mach number at which the airflow over some point of the aircraft reaches the speed of sound, but does not exceed it.
In aerodynamics, the critical mach number (mcr or m*) of an aircraft is the lowest mach number at which the airflow over some point of the aircraft reaches the speed of sound, but does not exceed it. In aerodynamics, the critical mach number (mcr or m*) of an aircraft is the lowest mach number at which the airflow over some point of the aircraft reaches the speed of sound, but does not exceed it.