Problem with cfg file for SU2 simulation over airfoil

Milz · April 17, 2021, 19:42

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.

bigfootedrockmidget · April 18, 2021, 17:50

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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April 18, 2021, 17:50		#2
bigfootedrockmidget Senior Member bigfoot Join Date: Dec 2011 Location: Netherlands Posts: 554 Rep Power: 17	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.