Simulate the simple Brayton cycle using Engineering Equation solver.

Assignment Problem Statement: A gas turbine system operates on a simple Brayton cycle. The compressor's efficiency is 0.95 while the efficiency of the turbine is 0.9. Inlet air to the compressor is at 27 degrees of Celcius and 100 kPa. The mass flow rate of fuel in the combustor varies according to the equation. The calorific value (energy value) of the fuel is 2000 J/kg. Plot the variation of ideal cycle thermal efficiency and the actual thermal cycle efficiency with pressure ratio. Pressure ratio varies from 1.5 to 20.5