February 11, 2020, 21:48
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Streamlines terminating at and originating from airfoil surface
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#1
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New Member
Anonymous
Join Date: Feb 2020
Posts: 1
Rep Power: 0
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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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