Streamline on surface of a wing
I just simulated external flow over a wing and I would like to see streamline on my wing or near my wing. In order to see streamline, I used Tecplot.
Since I have done laminar flow, the velocity on surface of my wing is zero (no slip cond.).
Could you guide me how I should see the my streamline on my wing or near to surface of my wing?
Thanks a lot in advance.
Try playing around with the wall shear stress vector.
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