Ressure ratio 81 air mass flow 60 kgs all components are

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An air-standard Brayton cycle is utilized as a jet propulsion engine. The aircraft flies at an altitude of 5000 m at a constant speed of 260 m/s. The cycle operates with the following conditions: diffuse inlet: 60 kPa, 250 K; turbine inlet, 1300 K; pressure ratio, 8:1; air mass flow, 60 kg/s; all components are ideal. Find the compressor power, the temperatures and pressures throughout the cycle, and the exit-jet velocity.

Reference no: EM13619458

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