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Part-66 Module 11 Practice Questions - EASA Part-66 Module 11 - Aeroplane Aerodynamics, Structures And Systems Exam

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On a swept-wing turbine aeroplane, the speed at which airflow over the upper wing surface first reaches Mach 1.0 (M=1.0) locally while the aircraft itself is still subsonic is known as the:
Correct Answer:
Critical Mach number (Mcrit)

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