Turbine spiral case postprocessing
 

Hi,

I'm simulating a turbine spiral case,stay and guide vanes. There was no problem with simulation but I have an issue with postprocessing.

To evaluate the design I need to determine the flow rate through individual guide vane passage. Is there any way to do this in Fluent. I guess I need to make isosurfaces at constant radial dimension that would be bound to individual blade passage and then calculate the flow rate...

Any ideas?

Mateus