Turbomachinery Blade Passage Creation
I have a 3D stator and rotor blade design as well as a 3D solidworks model for an axial turbine setup. I have ANSYS CFX (turbogrid included), and ICEMCFD at my disposal. I was looking for tips to create the blade passage geometry without having to resort to turbogrid. So that I can take the blade passage geometry into ICEMCFD and mesh it in there.
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