Turbine spiral case postprocessing
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...
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