325 - ATPL - In case of supersonic flow retarded by a normal shock wave a high efficiency (low loss in total pressure) can be obtained if the Mach number in front of the shock is
Question 325 - Principles of Flight - ATPL - Airline Transport Pilot license
Lower than 1.
High (supersonic).
Exactly 1.
Small but still supersonic.
Training tests and timed exam simulations ATPL - Airline Transport Pilot license
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