A jet-propelled airliner flies at an altitude of (15,000 mathrm{~m}) and a velocity of (265 mathrm{~m} /

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A jet-propelled airliner flies at an altitude of \(15,000 \mathrm{~m}\) and a velocity of \(265 \mathrm{~m} / \mathrm{s}\). What is the stagnation pressure and stagnation temperature of the air entering the engine? If the airliner is stationary on the ground, the engines are running with the same Mach number flow into the engines, and the air flow to each engine is \(40 \mathrm{~kg} / \mathrm{s}\), what is the airflow to each engine at the above flight conditions?

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