Week 2 - Converging diverging nozzle
1. Geometry
Figure: 2-D geometry of the convergent-divergent nozzle
2. Meshing
Figure: Meshing
Figure: Named Selection
3. Setup
Figure: Solver
Figure: Turn on the Energy equation
Figure: Viscous model
Figure: Pressure Inlet boundary condition
Figure: Temperature Inlet boundary condition
Figure: Pressure outlet boundary condition
Residual:
1. Temperature:
2. Velocity:
3. Pressure:
4. Mach Number:
Conclusion: The value of Mach number is 1 at nozzle location approximately near about throat.