Flow in the supersonic nozzle (Mach, density based)
Mach number visualization for the flow in the nozzle (k-e standard wall function, density based model, non-equilibrium flow) Chamber pressure 42.5bar, Standard atmosphere
Mach number visualization for the flow in the nozzle (k-e standard wall function, density based model, non-equilibrium flow) Chamber pressure 42.5bar, Standard atmosphere