Velocity magnitude distribution not showing properly

Hey guys, whenever I plot the velocity distribution on this wing’s surface, all points are equal to zero. I do know that the velocity magnitude is null in the very first layer of the boundary layer, but I would like to get the velocity of the first layer adjacent to the boundary layer, so that I can see the effects of the wing on the fluid. If anyone knows how to solve this, it would help me a lot.

Velocity distribution


Please refer to this thread with a similar discussion.


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Ok, thank you, Ricardo.