You’ve developed a cold air standard Brayton cycle with input from combustion of 5.0×10^6 Btu/h with a mass flow rate of 6 lb(mass)/s. Air enters the turbine at 2800°R and exit at 520°R the cycle has a compression pressure ratio of 12. If the specific heat is evaluated at 500°R and the turbine and compressor both have isentropic and chopping efficiencies of 95%. what is the net power developed by the cycle in hp.
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