How do you display the wing tip vortices?
I am using ANSYS 12 workbench. fluent to run simulation.
Set up: Homogeneous wing, symmetrical aerofoil, Angle of attack = 10degrees. inviscid.
I heard about isosufaces, q-criterion, lambda2? i cannot find any tutorials relating to this problem. I hope someone can help me.
if you would like details of the full set up and mesh, please ask.
You could look at the rotation of the flow: Nabla_x_V
The vector product of Nabla with Velocity
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