Simulation of a Quasi 1-D Subsonic Supersonic Nozzle Flow using MacCormack s technique

Objective: Objective 1. To write matlab code to solve 1D subsonic-supersonic nozzle flow equation in consevation and non consevation form of governing equation. 2. To find minimum number of iteration of required for convergence 3. Compare the normalized mass flow rate between the conservative forms and non- …