Consider an ideal simple gas turbine cycle. For a net power output of 10,000 horse power, an inlet air temperature of T1=500 R, an inlet turbine temperature of T3=2000 R, and a compression ratio of 10, calculate: (assume constant specific heat of Cp=0.24 Btu/lbm.R and k=1.4) a) The compressor exit temperature (T2) and the turbine exit temperature (T4), b) The air mass flow rate, and c) The cycle efficiency.