Hi, I am trying to run compressible flow simulations over different NACA airfoils.
I have been able to run the tutorial “Compressible flow over airfoil” for the speed range I need, which is 223 m/s (M 0.65), but when I try to run the simulations for the geometries I have with meshes created using SimScale the data achieved is completely wrong due to you can see the outlines of the different cell refinements of the mesh in the post processor (I attach two screenshots, one of the pressure field and one of the mesh, but as happens in the pressure field happen the same for the temperature a speed field).
Therefore as it is a problem with the meshes (I tried different ones with same results) can someone explain me how to create the mesh used in the tutorial?
The project I am working on it is call “final project compressible” and it is in my dashboard (atalavera_diez). I have create different simulations and I also check if the meshes works for incompressible flow conditions (their work). The pictures are taken from the simulation “NACA0012 0 -> NACA0012 0 c”. Also the link for the project is https://www.simscale.com/workbench/?pid=5352451548804250842#tab_1-0