Cyclic AMI for turbomachinery blade passage
 

Hi,
The domain is divided into 3 cellzones (Inlet, Passage, and Outlet). The passage part is supposed to rotate with prescribed angular velocity using cyclicAMI interface condition with inlet and outlet. I have done this for full passage comprising of all the blades.
Now, I am trying to simulate this for single passage(say a sector of the whole). The cyclicAMI is not working with symmetric boundary condition for passage.
Does OpenFOAM have this capability?
The problem I am facing is after a few iteration passage part moves away from inlet and outlet. Is there a way to implement cyclicAMI condition for this?