Issue Description
Dear all,
my research group and me found a problem when using the JST scheme.
The problem consists in a difference in the skin friction coefficient along the airfoil between 2D and 3D meshes (the 3D one is obtained by extruding the 2D mesh using only 1 cell in the span wise direction).
This difference arises when the JST scheme is used, and it leads to a ~25% of difference in the drag coefficient.
In order to better explain what is happening, here is a summary table of the results for the CRM airfoil:

It is possible to notice that this difference does not emerge if the ROE scheme is used.
For the 3D case, the boundary conditions at the side faces of the domain are MARKER_SYM, so that we think that this issue could be connected to the #1125 .
To Reproduce
In order to reproduce the issue, a zip file is attached. It contains the configuration files for the 3D and 2D cases using JST and ROE, and the two grids of the CRM airfoil. It is possible to reproduce this issue also using a different airfoil.
ROEvsJST.zip
Desktop:
- OS: Linux (Ubuntu)
- C++ compiler and version: -
- MPI implementation and version: -
- SU2 Version: v7.1.1 and previous.
Thanks for your help.
Ettore Saetta
Theoretical and Applied Aerodynamics Research Group (TAARG)
University of Naples Federico II
Issue Description
Dear all,
my research group and me found a problem when using the JST scheme.
The problem consists in a difference in the skin friction coefficient along the airfoil between 2D and 3D meshes (the 3D one is obtained by extruding the 2D mesh using only 1 cell in the span wise direction).
This difference arises when the JST scheme is used, and it leads to a ~25% of difference in the drag coefficient.
In order to better explain what is happening, here is a summary table of the results for the CRM airfoil:

It is possible to notice that this difference does not emerge if the ROE scheme is used.
For the 3D case, the boundary conditions at the side faces of the domain are
MARKER_SYM, so that we think that this issue could be connected to the #1125 .To Reproduce
In order to reproduce the issue, a zip file is attached. It contains the configuration files for the 3D and 2D cases using JST and ROE, and the two grids of the CRM airfoil. It is possible to reproduce this issue also using a different airfoil.
ROEvsJST.zip
Desktop:
Thanks for your help.
Ettore Saetta
Theoretical and Applied Aerodynamics Research Group (TAARG)
University of Naples Federico II