[cbowen11]

Hi,

I'm using a mixing plane to model a stator-rotor fluid interaction. I followed other examples and feel confident that I have the correct boundary conditions. My flow solution even looks reasonable, however, after a few hundred iterations none of the properties are circumferentially averaged at the mixing plane interface. From what i understand the properties have to be averaged at every iteration and passes to the stator exit or rotor inlet before each domain can be iterated again. Has anyone seen this behavior before?