SIMULATION OF 1-D SUPERSONIC NOZZLE FLOW USING MAC-CORMACK METHOD

Objective: PROBLEM SETUP DESCRIPTION 1. Steady isentropic flow through a Convergent Divergent Nozzle is Assumed. 2. Source flow into the inlet of the nozzle is at constant temperature and pressure. 3. Isentropic supersonic expansion of the flow occurs as denoted by the Mach Number Values as shown is the above schematic.…