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Engineering 21 Online
OpenStudy (anonymous):

[Thermodynamics] Air enters a gas turbine at 1600K and exits at 100kPa and 830K. The turbine efficiency is estimated to be 85%. What is the turbine inlet pressure? I have the solution and the final answer, but everything's unclear. I was hoping someone would have a better solution, or is willing to discuss the solution I have with me.

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