Internal:CDT3D SU2: Difference between revisions
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Created page with "== 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..." |
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== General == | == General == | ||
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. | |||
Boundary kayer is usually given the following restrictions: | Boundary kayer is usually given the following restrictions: | ||
* Δs: Distance of first cell from the solid surface | * Δs: Distance of first cell from the solid surface | ||
Revision as of 15:42, 17 October 2018
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]