Sub and supersonic nozzle flow equation

Objective: Results obtined: I ran this case for 30,60,90,120 grid points with cfl number 0.5,0.6,0.9 and 1.2 increasing the cfl number for same grid size gave faster results the results have been attached to the google drive although i like to mention few of the numerical values that i got from the case is nearly matched to the john…