Question

During a flight test it is noticed that, the air speed of a turbojet engine is 250m/s. Ambient air temperature is -14℃

Answer 1

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ANSWER: The nozzle is supplied from an air reservoir in which the pressure is 500 kPa; the temperature is 400 K. The nozzle throat area is 5 cm2.

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Answer 2

The nozzle is supplied from an air reservoir in which the pressure is 500 kPa; the temperature is 400 K. The nozzle throat area is 5 cm².

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