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Streamlines terminating at and originating from airfoil surface

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Old   February 11, 2020, 22:48
Smile Streamlines terminating at and originating from airfoil surface
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Hello!

I am trying to run a RANS simulation on NACA0012 airfoil using INC_RANS available with SU2 7.0.1. Tecplot 360 is the software that I am using to view the results.

Weirdly, for Angle of Attack=20, the streamlines r observed to terminate at the lower surface of the airfoil and re-emerge from the upper surface, for some sections of the airfoil.

I wish to know what might be the cause of this discrepancy and how could it be overcome.

Thank you!
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naca0012, rans, streamlines, su2, tecplot 360

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