Problems in Boundary Layer Generation for Aerodynamic Analysis

Hi, I am trying to mesh my design for the CFD simulation of a Formula 1 front wing. But even though I am using the parametric hex dominant mode, I seem to encounter a problem where my boundary layers are not being generated. I tried using multiple methods and even decreased the number of boundary layers. But when I conduct a mesh inspection for the boundary layer, I see that the layers have completely collapsed the mesh has not generated properly.

This is how the layers look like for the entire mid-span of the wing. Ideally there should have been 5 layers from the airfoils, but it seems to be that the layers have been deleted. I am attaching screenshots of my mesh generation settings for better information.

I have tried to clean my geometry and whenever I run an interference check, I don’t seem to have any issues with the geometry itself, so it is a clean geometry. For the bounding box, I am using a 5x chord length upstream, 15x downstream, and 5x chord length in Y and Z direction. I have tried following each and every tutorial step by step according to the multiple posts in the fourm but for some reason I can’t seem to create a better mesh than this with the accurately generated boundary layers.

If someone could create a proper mesh with the boundary layers and send me screenshot helping me out with the parameters that I need to address or tweak, it will be very helpful for my project. I genuinely want to understand why is my generation going wrong even though I am following the same steps as everyone.