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May 11, 2022, 12:33
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Lift distribution along wing span
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#1 |
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New Member
Dheeraj Agarwal
Join Date: Apr 2021
Posts: 2
Rep Power: 0  |
Is it possible to extract lift distribution along the span of wing using SU2_CFD code.
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May 12, 2022, 02:42
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#2 |
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Senior Member
bigfoot
Join Date: Dec 2011
Location: Netherlands
Posts: 676
Rep Power: 21 |
Hi,
You can do that during postprocessing/visualization in paraview. Just save the files as a paraview multiblock file and extract the surface as a block.For more flexibility in visualization, you might want to try splitting the airfoil into a top and a bottom part. |
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