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An adiabatic diffuser at the inlet of a jet engine increases th... | Filo

The inlet ducting to a jet engine forms a diffuser that steadily decelerates the entering air to zero velocity relative to the engine before the air enters the compressor. Consider a jet airplane flying at 1000  km / h where the local atmospheric pressure is 0.6 bar and the air temperature is 8^∘ C. Assuming ideal gas behavior and neglecting heat transfer and potential energy effects, determine the temperature, in ^∘ C, of the air entering the compressor. | Numerade

The diffuser in a jet engine is designed to decrease the kinetic energy of the air entering the engine compressor without any work or heat interactions. Calculate the velocity at the exit of a diffuser when air at 100 kPa and 30^∘ C enters it with a velocity of 350  m / s and the exit state is 200 kPa and 90^∘ C | Numerade

Different Parts of the Engine and their Function [Notes & PDF]