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162 - ATPL Question Bank in English - A stationary bow shock ahead of a blunt nose in the free stream requires supersonic upstream flow. It can first exist at a free-stream Mach number:

Question 162 - Principles of Flight - ATPL - Airline Transport Pilot Licence

A Mach number just below M = 1
Mach 1
A Mach number just above M = 1
The critical Mach number

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