Turbine spiral case postprocessing -- CFD Online Discussion Forums

April 24, 2008, 04:24	Turbine spiral case postprocessing	#1
mateus Guest Posts: n/a	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

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