CFD Online Logo CFD Online URL
Home > Forums > Software User Forums > SU2

Streamlines terminating at and originating from airfoil surface

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Search this Thread Display Modes
Old   February 11, 2020, 21:48
Smile Streamlines terminating at and originating from airfoil surface
New Member
Join Date: Feb 2020
Posts: 1
Rep Power: 0
Space_Ninja is on a distinguished road

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!
Space_Ninja is offline   Reply With Quote


naca0012, rans, streamlines, su2, tecplot 360

Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On

All times are GMT -4. The time now is 16:14.