Question: Rework Problem 9.37 except that the compressor exit temperature is a) 600°C b) 800°C. Air enters the gas turbine cycle of Fig. 9.44 at 25°C
a) 600°C
b) 800°C.
Air enters the gas turbine cycle of Fig. 9.44 at 25°C and 100 kPa with a flow rate of 1.2 kg/s. It is compressed so that the temperature at state 2 is 400°C. The temperature entering the turbine is 1400ºC. Assuming constant specific heats for the air and ideal conditions in all components, calculate:
i) The thermal efficiency
ii) The heat added in the combustor
iii) The net power produced by the cycle
iv) The back-work ratio
Figure 9.44
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in Combustor Heat exchanger 1 IC) 800C Compresson Turbine net ) 100 kPa 25C Heat exchanger
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