Internal:CDT3D SU2
General
For the target method RANS+LES boundary layer is needed to resolve the turbulance. Boundary kayer is usually given the following restrictions:
- Δs: Distance of first cell from the solid surface
- Thickness of the boundary layer
- Stretching factor / number of layers
More Links
- Open source tool for creating meshes https://www.salome-platform.org/
- European Knowledge base for CFD simulations [1]
- Project page in the site above for the Delta wing case [2]