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[Airfoil] Bad results for LES in comparison to RANS |
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September 28, 2020, 15:02
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#41 |
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Senior Member
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,768
Rep Power: 71  |
If z-direction is the spanwise resolution, the cell size depends on the flow conditions. If the flow is homogeneous then the cell size dz+ can be O(20-30). But if the flow is confined in spanwise direction then you have to consider if it necessary the full boundary layer resolution and a non-homogeneous grid size.
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September 29, 2020, 08:54
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#42 |
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Senior Member
Joern Beilke
Join Date: Mar 2009
Location: Dresden
Posts: 498
Rep Power: 20 |
Is there anybody willing to share a good mesh, which has been used for such an LES calculation?
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| Tags |
| airfoil, les, rans, spalart allmaras model |
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