|
[Sponsors] |
August 4, 2018, 08:09 |
integral thickness for boundary-layer
|
#1 |
Senior Member
Syavash Asgari
Join Date: Apr 2010
Posts: 473
Rep Power: 18 |
Dear Foamers,
I have developed a utility code to calculate the integral thicknesses of a boundary-layer. It has been developed to work on a hex-mesh but it may work on a non-hex mesh either. The utility is particularly useful in LES/DNS post-processing of the results. https://github.com/syavash20/TurbLab...egralThickness Regards, Syavash |
|
March 8, 2022, 21:23 |
|
#2 |
Senior Member
Dongyue Li
Join Date: Jun 2012
Location: Beijing, China
Posts: 840
Rep Power: 17 |
Syavash,
In line 151 and 152, do we need to consider U? like: U[celli].component(0)/U*(1.0-U[celli].component(0)/U)
__________________
My OpenFOAM algorithm website: http://dyfluid.com By far the largest Chinese CFD-based forum: http://www.cfd-china.com/category/6/openfoam We provide lots of clusters to Chinese customers, and we are considering to do business overseas: http://dyfluid.com/DMCmodel.html |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[snappyHexMesh] Error defining boundary layer around cube snappyHexMesh | crizpi21 | OpenFOAM Meshing & Mesh Conversion | 5 | October 16, 2021 10:56 |
[snappyHexMesh] Help with Snappy: no layers growing | GianF | OpenFOAM Meshing & Mesh Conversion | 2 | September 23, 2020 08:26 |
[snappyHexMesh] snappyHexMesh Boundary Layer at Corner | panpanzhong | OpenFOAM Meshing & Mesh Conversion | 5 | July 3, 2018 05:53 |
Questions about Boundary Layer Thickness and Turbulence Models | famerfamer | STAR-CCM+ | 3 | July 12, 2012 09:47 |
errors | Fahad | Main CFD Forum | 0 | March 23, 2004 13:20 |