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222 - ATPL Question Bank in English - For the same upstream conditions and Mach number in a calorically perfect gas, compared with an oblique compression shock inclined at less than 90° to the flow, a normal shock has:

Question 222 - Principles of Flight - ATPL - Airline Transport Pilot Licence

Higher total pressure.
Higher total temperature.
Higher loss in total pressure.
Lower static temperature.

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