Carbon dioxide flows steadily through a converging-diverging nozzle at a mass flow rate of 3.0 kg/s. The carbon dioxide enters the duct at a pressure of 1400 kPa and 200°C with a low velocity, and it expands in the nozzle to an exit static pressure of 200 kPa. The duct is designed so that the flow can be approximated as isentropic. Determine the density, velocity, flow area, and Mach number at 5 axial stations and at the throat.