Samanthacook5626
03.05.2021 •
Engineering
In an open type of gas turbine, which is operating at steady state, air enters the compressor with a mass flow rate of 4 kg/s at 0.95 bar at 22oC and exits at 5.6 bar. The air then passes through a heat exchanger before entering the turbine at 827oC, 5.6 bar. Air exits the turbine at 0.95 bar. The compressor and turbine operate adiabatically and have isentropic efficiencies of 85% each. Using the ideal gas model for air, determine (i) the net power developed; and (ii) the rates of exergy destruction for the compressor and turbine.
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Ответ:
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