A gas turbine with air flowing in at 1200 kpa 1200 k has an, Civil Engineering

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A gas turbine with air flowing in at 1200 kpa 1200 k has an

1. A gas turbine with air flowing in at 1200 kPa, 1200 K has an exit pressure of 200 kPa and an isentropic efficiency of 87%. Find the exit temperature.

2. A gas turbine with air flowing in at 1200 kPa, 1200 K has an exit pressure of 200 kPa. Find the lowest possible exit temperature. Which efficiency does that correspond to?

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Civil Engineering: A gas turbine with air flowing in at 1200 kpa 1200 k has an

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Civil Engineering: A gas turbine with air flowing in at 1200 kpa 1200 k has an

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