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September 16, 2013, 09:16
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Airfoil polars
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#1 |
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Member
Jason
Join Date: May 2013
Location: South Africa
Posts: 32
Rep Power: 13  |
Hi,
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? |
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| Tags |
| 2d flow, airfoil, airfoil analysis, fluent, polar |
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