Question: 1 0 . 4 1 . ) Consider an ideal air - standard cycle for a gas - turbine, jet propulsion unit, such as that

10.41.) Consider an ideal air-standard cycle for a gas-turbine, jet propulsion unit, such as that shown in fig. 10.11. The pressure and temperature entering the compressor are 90kPa, 290K. The pressure ratio across the compressor is 14:1, and the turbine inlet temperature is 1500K.

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