Solving the 1D supersonic nozzle flow equations using the Macormack Method both conservative and non-conservative form

Objective: INTRODUCTION: Solving the 1D supersonic nozzle flow equations using the Macormack Method: The flow through the nozzle is subsonic at inflow and supersonic flow at outflow. The flow is considered to vary only in x direction ie one direction and not in others, that is why it is considered as 1D flow in solving the problem.…