[prak_1989]

Hi all,

I have been trying to validate a zero pressure gradient flat plate case using SST menter's model. The link to the problem I am trying to validate is https://turbmodels.larc.nasa.gov/flatplate.html

As you can see from the link, there is a symmetry and a adiabatic wall condition. My solution is blowing in the transition region between the symmetry and no slip boundary condition(adiabatic wall condition).

I am using a finite volume scheme with the flux at the interface reconstructed using symmetric average of functional values + its gradients respectively(Basically the avg of Taylor's series at points i and i+1 with 2nd order truncation error).

The grid resolution is 69x49 and clustering is done in the region of boundary layer and leading edge. It is done similar to one which is there in this link https://turbmodels.larc.nasa.gov/flatplate_grids.html