Internal:CDT3D SU2: Difference between revisions
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== Interesting points from SU2 developers == | == Interesting points from SU2 developers == | ||
* linear scalaibility is expecting is there are at least 5000 | * linear scalaibility is expecting is there are at least 5000 grid points per core. [https://youtu.be/oEhlwbye90w?t=1186] | ||
=== BL discussion with Beckett === | === BL discussion with Beckett === | ||
Revision as of 08:26, 21 November 2018
General
Oct 30 2018 presentation [1]
Interesting points from SU2 developers
- linear scalaibility is expecting is there are at least 5000 grid points per core. [2]
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 [3]
- Project page in the site above for the Delta wing case [4]