Lift distribution along wing span
Is it possible to extract lift distribution along the span of wing using SU2_CFD code.
|
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. |
All times are GMT -4. The time now is 12:30. |