SIMULATION OF A 1-D SUPERSONIC NOZZLE

Objective: AIM : To solve the 1D supersonic nozzle flow equations using the Macormack Method. THEORY : Non-Conservtive form Equations : Continuity `(delrho\')/(delt\')=-rho(delV\')/(delx\')-rho\'V\'(del(ln A\'))/(delx\')-V\'(delrho\')/(delx\')` Momentum : `(delV\')/(delt\")=-V\'(delV\')/(delx\')-1/gamma((delT\')/(delx\')+(T\')/(rho\')(delrho\')/(delx\'))`…