Hello,
I am trying to run a steady converging-diverging nozzle simulation that has a specified subsonic flow at the inlet, with known values of temperature, pressure, and Mach number. I am noticing, however, that there is no function that defines a subsonic inlet BC, only supersonic:
InFlowBC_Supersonic:new{flowState, x0=0.0, y0=0.0, z0=0.0, r=0.0}
Can this function also be used for subsonic flow? If not, what is the recommended approach to define it?
Thank you
Hello,
I am trying to run a steady converging-diverging nozzle simulation that has a specified subsonic flow at the inlet, with known values of temperature, pressure, and Mach number. I am noticing, however, that there is no function that defines a subsonic inlet BC, only supersonic:
InFlowBC_Supersonic:new{flowState, x0=0.0, y0=0.0, z0=0.0, r=0.0}Can this function also be used for subsonic flow? If not, what is the recommended approach to define it?
Thank you