|
[Sponsors] |
December 20, 2019, 21:57 |
cournat number for flow past cylinder(3D)
|
#1 |
New Member
sarva
Join Date: Feb 2017
Posts: 4
Rep Power: 9 |
Hi all,
I am studying the flow past 3D fixed cylinder in range of Reynolds number from 1000-100000. The physics is segregated flow-implicit unsteady - RANS - k omega SST. I have chosen the time step as 0.001s. The results are good and comparable, but simulation time is high. So i want to know, Is there any rule to calculate the time step for this problem like courant number, CFL? 1.How can i chose the time step for this problem? 2.If courant number is the criteria, What is the courant number for the flow past cylinder problem? 3. If I change the turbulence model, cournat number will change? Thanks in advance. |
|
December 23, 2019, 00:50 |
|
#2 | |
Senior Member
|
Quote:
Courant number is "u∆t/∆x". Back calculate your time step "∆t" taking Courant number as 1. 1 is ideal. u is free-steam velocity and ∆x is first layer height. Your Courant number may give recommended time step value less than 1ms as you have used. Then the only option is to do trial and error to find out optimum time step for your case. Courant number doesn't change with turbulence model. Just refer the formula given above. Hope this helps. |
||
December 25, 2019, 23:02 |
|
#3 |
New Member
sarva
Join Date: Feb 2017
Posts: 4
Rep Power: 9 |
Thanks Ashok..
|
|
Tags |
cournat number, cylinder flow |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
SimpleFoam & Theater | jipai | OpenFOAM Running, Solving & CFD | 3 | June 18, 2019 11:11 |
GenerateVolumeMesh Error - Surface Wrapper Self Interacting (?) | AndreP | STAR-CCM+ | 10 | August 2, 2018 08:48 |
decomposePar pointfield | flying | OpenFOAM Running, Solving & CFD | 28 | December 30, 2013 16:05 |
DecomposePar unequal number of shared faces | maka | OpenFOAM Pre-Processing | 6 | August 12, 2010 10:01 |
[blockMesh] BlockMeshmergePatchPairs | hjasak | OpenFOAM Meshing & Mesh Conversion | 11 | August 15, 2008 08:36 |