[JohnEFM]

Hello,


I am trying to set up a 2D simulation of a swirl burner using a thin slab from the original geometry. To set up my simulation, I would like to add a swirl component for an inlet boundary condition, specifically for the air inlet boundary. Some specifications of my simulation are: it's time-based, and it uses a transient solver, a spray model for the injector, a SAGE combustion model, a LES dynamic structure turbulence model, and a source model for ignition. Does anyone know a way to add a swirl component for an inlet boundary condition?


Thank you