Select a design exit Mach # (M>1), and set up a converging-diverging nozzle CFD simulation to recreate the following flows: 1. Sub-sonic choked flow condition 2. Super-sonic design condition 3. Increase the back pressure from part 2 enough to have a Normal Shock in the diverging section of the nozzle 4. Increase the back pressure from part 2 enough to have an Oblique Shock outside of the nozzle 5. Decrease the back pressure from part 2, to have expansion waves outside the nozzle 6. Compare all the above CFD results to the theoretical 1D calculations done in class 7. Summarize all findings in an Engineering report All cases should be run with the same inlet pressure.