A gas turbine power cycle is to be modeled using the cold-air standard ideal Brayton cycle. The air entering the compressor is at 0.1 MPa and 15 C and the pressure ratio across the compressor is 10. The maximum temperature in the cycle is 1100 C. a. Find the pressure and temperature at the end of each process in the cycle. b. Determine the compressor and turbine work and the cycle efficiency.