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

Objective: Non-Conservative Function: function [rho,v,T,a,x,mach,q,mass_flow,rho_throat,Temp_throat, mach_throat, Pr_throat, m_throat,k] = non_conservative(L,n,nt) x = linspace (0,L,n); dx = x(2)-x(1); gamma = 1.4; %% Initial profiles rho = 1-0.3146*x; %rho =density T = 1- 0.2314*x; %T = temperature v = (0.1 +1.09*x).*T.^0.5; %v…