|
[Sponsors] |
[snappyHexMesh] min y+ that can be gain with snappyHexMesh around airfoil |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
April 9, 2013, 02:54 |
min y+ that can be gain with snappyHexMesh around airfoil
|
#1 |
Senior Member
saeideh mohamadi
Join Date: Aug 2012
Posts: 229
Rep Power: 15 |
Hi,
i have a one element and a three element airfoil, and i wand use low Re turbulence models so i need yPlus < 50 for my mesh. i use snappyHexMesh. my problem is to create a boundary layer with snappyHexMesh. How to control the number and thickness of the layers? with what numbers in add layerControls we can reach to y+ < 50 ? |
|
April 23, 2013, 11:57 |
|
#2 |
Senior Member
HECKMANN Frédéric
Join Date: Jul 2010
Posts: 249
Rep Power: 17 |
First you have to "guess" the thickness of your first cell: http://www.cfd-online.com/Tools/yplus.php
You cannot calculate exactly what is the thickness needed because y+ depends of your solution. The link I gave you can however give you a good estimation. I don't use snappyHexMesh but I can tell you that your first cell height must be of a close value from the estimation given by the link and the growth rate must be lower than 1.2. Hope somebody can help you with Snappy |
|
April 23, 2013, 19:00 |
|
#3 | |
New Member
Phillip
Join Date: Mar 2012
Location: Germany
Posts: 27
Rep Power: 14 |
Quote:
when you use a so-called "low-Re" turbulence model the yPlus values are usually much lower in this assumption (y+ ~ 1) or (y+ < 5, with attention). In snappyHexMesh you can control the number and thickness of the layers with: Code:
addLayersControls { relativeSizes true; // when set to false --> change thickness to absolute values layers { myWall { nSurfaceLayers 5; } } expansionRatio 1.0; finalLayerThickness 1.0; minThickness 0.1; nGrow 0; featureAngle 30; slipFeatureAngle 30; nRelaxIter 5; nSmoothSurfaceNormals 1; nSmoothNormals 3; nSmoothThickness 10; maxFaceThicknessRatio 0.5; maxThicknessToMedialRatio 0.3; minMedianAxisAngle 80; nBufferCellsNoExtrude 0; nLayerIter 50; } For a good mesh you have to change the upper parameters, because this is only a example of usage... hope i can help you? For more details post your case and entitle your problem with some code-examples and pictures... |
||
April 24, 2013, 05:58 |
|
#4 |
Member
Andreas Wendy
Join Date: Aug 2012
Posts: 73
Rep Power: 14 |
hi,
like Frédéric said you can guess use the tool to calculate the thickness of the first wall layer. the final layer thickness in snappy hexmesh is the layer thickness wich is tha last layer (not the one at the wall) so you have to calculate final oundary layer depending on the expension ratio, number of layers and desired first layer thickness. yfinal = y*ratio^(n-1) (I think). be sure to set relativeSize to false! if you want to resolve your y+ should be smaller than 1 but at least below 5! best wishes Andreas |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
y+ and u+ values with low-Re RANS turbulence models: utility + testcase | florian_krause | OpenFOAM | 114 | August 23, 2023 06:37 |
Near wall treatment in k-omega SST | Arnoldinho | OpenFOAM Running, Solving & CFD | 38 | March 8, 2017 14:48 |
High drag for airfoil compared to XFOIL and wind tunnel data | Ry10 | SU2 | 15 | October 30, 2016 18:27 |
Problem of simulating of small droplet with radius of 2mm | liguifan | OpenFOAM Running, Solving & CFD | 5 | June 3, 2014 03:53 |
On the damBreak4phaseFine cases | paean | OpenFOAM Running, Solving & CFD | 0 | November 14, 2008 22:14 |