Internal:CDT3D SU2: Difference between revisions
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m Ctsolakis moved page Interal:CDT3D SU2 to Internal:CDT3D SU2 without leaving a redirect: wrong namespace |
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== General == | == General == | ||
=== BL discussion with Beckett === | |||
For the target method RANS+LES boundary layer is needed to resolve the turbulance. | 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. | Specifically for the Delta wing see thje link bellow for more details of the simulation. | ||
Revision as of 18:02, 30 October 2018
General
BL discussion with Beckett
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. During the fine-tunning of the mesh it it expected to require changes mostly in the boundary layer, since, this is where the turbulance near the boundary ( which we are trying to resolve) lives.
Boundary layer 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]