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Air enters the compressor of an air-standard Brayton cycle at 100kPa, 300K, with a volumetric flow rate of 5m^3/s. The turbine inlet temperature is...

Air enters the compressor of an air-standard Brayton cycle at 100kPa, 300K, with avolumetric flow rate of 5m^3/s. The turbine inlet temperature is 1400K. The compressorand Turbine both have isentropic efficiencies of 88%. For pressure ratios of6,7,8,9,10,11 and 12, tabulate and then graph the following on the same graph using thecold-air standard assumption and briefly discuss the effect of pressure ratio on thefollowing parameters:a) Thermal efficiency versus pressure ratiob) Back work ratio versus pressure ratioc) Net power developed in kW versus pressure ratioShow all calculations for a pressure ratio of 6 – the rest of your calculations can be done by hand, in excel or another program if you like

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