|September 16, 2013, 08:16||
Join Date: May 2013
Location: South Africa
Posts: 32Rep Power: 4
I am new to Fluent and need to generate airfoil polars for a 2D airfoil.What is the best procedure to do this?
My procedure so far has been to make a c-grid mesh and to run it in fluent, applying the velocity (thus far) at 0 degrees AoA. I could recalculate the velocity for each point but it seems like a long process and I'm guessing there is an easier way to just change the oncoming angle of the flow?
|2d flow, airfoil, airfoil analysis, fluent, polar|
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