When is the critical Mach number of an airfoil attained ?
The critical Mach number of an airfoil is attained when
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the Mach number some where on the airfoil is unity.
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the freestream Mach number is sonic .
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the free stream Mach number is supersonic.
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the Mach number everywhere on the airfoil is supersonic.
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At some point on the airfoil surface the flow has Mach number 1 while having subsonic free stream flow condition.That subsonic free stream Mach number is called the critical Mach number.