Internal:CDT3D SU2: Difference between revisions
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* European Knowledge base for CFD simulations [http://www.kbwiki.ercoftac.org/w/index.php/Main_Page] | * European Knowledge base for CFD simulations [http://www.kbwiki.ercoftac.org/w/index.php/Main_Page] | ||
* Project page in the site above for the Delta wing case [http://www.kbwiki.ercoftac.org/w/index.php/CFD_Simulations_AC1-09] | * Project page in the site above for the Delta wing case [http://www.kbwiki.ercoftac.org/w/index.php/CFD_Simulations_AC1-09] | ||
= Delta Wing Project = | |||
Revision as of 10:31, 11 February 2019
General
- Oct 30 2018 presentation [1]
- Pointwise and SU2 [2]
- Paper : Construction of Prism and Hex Layers from Anisotropic Tetrahedra [3] see also [4]
Interesting points from SU2 developers
- linear scalability is expected if there are at least 5000 grid points per core. [5]
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 [6]
- Project page in the site above for the Delta wing case [7]