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 30oC enters it with a velocity of 350 m/s and the exit state is 200 kPa and 90oC

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FIGURE P5-28 eStockbvie/Punchstack RF