Internal:CDT3D SU2

General

For the target method RANS+LES boundary layer is needed to resolve the turbulance. Specifically for the Delta wing see thje link bellow for more details of the simulation.

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]