Simulation of a 1D Super-sonic nozzle flow simulation using Macormack Method

Objective: Main Script: clear all close all clc %Inputs % Length of the domain L = 3 ; %Number of grid points n=31 ; %Number of points in x axis x=linspace(0,L,n); % Grid spacing dx = x(2)-x(1) % Area,a a = 1+2.2*(x-1.5).^2 ; gamma=1.4 ; % Exact node at the throat throat = ((n-1)/2)+1 ; % courant number c = 0.5 ; % No. of time steps…