ANALYSISG IN OPTIMIZED EXHAUST NOZZLE DESIGN FOR A SUPERSONIC MACH-2 AERO ENGINE

Last time I did the simulation for a simple conical nozzle as in my project. And I got similar results with the calculation. But the panel refused my project because there is a shock wave inside the nozzle. This time I did the calculation for Vitoshinsky nozzle formulation. So this time I need the optimized simulation for the Vitoshinsky nozzle. I am not good at cfd ansys. I want your help to design the nozzle by using Solid work for my calculated dimensions and do the optimization by using cfd ansys. If you can it is better to show the behaviour of the gas inside the nozzle and 5 meters after the exit. Please find the attachments below, my calculated dimension for Vitoshinsky nozzle and Initial data for calculation. My submission date is on the 25th of May, so i would like to receive the work before 20th May.