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Thanks you very much, i have succeed to launch a calcul.
But the results are not really acceptable.
I think i really don't understand the syntax of the boundary conditions. If i am right, the group is the nomber in the last column of the mesh file in the points definitions but when i launch the simulation, the hole domain is affected.
In fact, i need to impose a field of temperature on the edges of the airfoil, this is why i try to understand how to impose a temperature at one node of the mesh.