I'm working on a project of which involves the analysis of a fixed area ideal turbojet. I'm calculating all the parameters at each station. I'm having a problem with stations 3, 4, 5 (end of compressor, end of burner, end of turbine). What happens to the mach number, pressure, and temperature (not total pressure and temperature) at each of these stations. I've calculated the parameters for all other stations but I can't find information on what happens to P and T.