[nicodsi78]

Hello,

First, thank you to all the contributors of SU2 and this forum!

I would like to have your feedback concerning my study : I need to impose a non-uniform field of temperature on an airfoil (this is in a 2D computation).

In my mind, the best option would be to have the possibility to define this boundary condition in specifying a file (for example) in which the temperature is written for each point of the airfoil boundary.
If I’m not mistaken, this feature does not exist natively in SU2.

Thus, I have discretized my airfoil shape into n small segments Ln that I have defined as markers in the mesh file.

In the configuration file I get this :

% Navier-Stokes (no-slip), isothermal wall marker(s) (NONE = no marker)
% Format: ( marker name, constant wall temperature (K), ... )
MARKER_ISOTHERMAL= ( L1, T1,....... Ln, Tn )

%
% Farfield boundary marker(s) (NONE = no marker)
MARKER_FAR= ( farfield )

% Marker(s) of the surface to be plotted or designed
MARKER_PLOTTING= ( L1,......Ln)
%
% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
MARKER_MONITORING= ( L1,.......Ln)

For the moment this is not working, the computation stops with the following error message :
"85331, 0.0017285331, 0.0017285331, 0.0017285331, 0.001728533:24068 terminated with signal 11 at PC=3d5867e50e SP=7fff6dfd05d8. Backtrace: segmentation fault"

Do you think the way I’m managing this boundary condition is correct?

Thank you in advance,
Regards,