Edge association in ICEM CFD for compressor flow passage- Need help!
 

Hello all,

I'm modelling a flow between two adjacent compressor blades, and I need some help with splitting blocks and edge association in ICEM CFD for the flow domain, as I'm relatively new to ICEM CFD. Since the flow is in 3D and somewhat "twisted", I'm not really able to understand which edge needs to be associated to which curve of the domain, and I know the splitting of blocks directly affects this association too. Could you please guide me as to how the edge association needs to be done and also how further steps can be applied, such as inflation, O-Grids and so on? I've attached the .blk file and I'd be really grateful if anyone would like to demonstrate the process in the file itself and send it back to me. Thanks a lot!

Please help people !