Inlet pressure, $P_1 = 150000 \text{ Pa}$
Inlet temperature, $T_1 = 320 \text{ K}$
Mass flow rate, $\dot{m} = 8 \text{ kg/s}$
Compressor pressure ratio, $r_p = P_2/P_1 = 10$
Turbine inlet temperature, $T_3 = 1400 \text{ K}$
Specific heat ratio, $k = 1.4$
For air,
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