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Problem with cfg file for SU2 simulation over airfoil

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Old   April 17, 2021, 19:42
Default Problem with cfg file for SU2 simulation over airfoil
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Cb
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Hi,
I'm having a hard time with the configuration file. I'm trying to simulate flow over an airfoil using the RANS equations and the Spalart Allmaras Model.

I'm running into a two dimensional problem. The error I run into reads

Two dimensional problem.
344 points.
2 surface markers.
250 boundary elements in index 0 (Marker = farfield).
98 boundary elements in index 1 (Marker = airfoil).

I attached my cfg file .geo file and su2 file that I am using.
Any help would be greatly appreaciated I'm so lost as to what I configured incorrectly.
Attached Files
File Type: txt meshgeo.txt (13.2 KB, 5 views)
File Type: txt configuration.txt (13.3 KB, 7 views)
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Old   April 18, 2021, 17:50
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bigfoot
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Hi!

Which version are you using? Many of the options in your configuration file are obsolete so I could not test this with a recent version.
Can you get the most recent release and try it again?The configuration files in the testcases directory are up to date so you can start with one of those.
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