I want to make a air flow simulation through Roots kompressor, but I face a problem which i cant solve. I choose the rotating regions and boundary contitions and everythinfg seems ok. But while I want to solve the simulation there is an error:
|Mesh generation started||20:35:30 , Dec 01|
|Warning! Unable to resolve the local rotating region||20:35:43 , Dec 01|
|Mesh generation terminated||20:35:44 , Dec 01|
The geometry of a Roots kompressor causes that the rotating regions of the lobes overlap. Is it possilbe to solve such a simulation?