Streamlines terminating at and originating from airfoil surface
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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