CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > FLUENT

continuity-convergence problems during mesh independence study

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   January 13, 2021, 06:31
Unhappy continuity-convergence problems during mesh independence study
  #1
New Member
 
Join Date: Dec 2020
Posts: 1
Rep Power: 0
cola93 is on a distinguished road
Dear all,

I'm quite new to Fluent and this is my first thread. I hope someone can help me.


I’m facing continuity-convergence problems in my steady k-w SST simulation with refined meshes.


I'm trying to simulate a flow with one inlet and ten outlets (one main outlet and 9 smaller outlets, see picture Initial_Meshing). The flow rate at the inlet and the main outlet is known and I want to examine the distribution between the 9 smaller outlets.


My initial simulation, with a coarse mesh (750.000 nodes, 1.750.000 elements) converged for first and second order discretization (see picture CoarseMesh_SecondOrder_ResidualPlot). For a mesh independence study I used the same settings with refined meshes (1.050.000 nodes, 2.770.000 elements and 1.500.000 nodes, 4.560.000 elements) . With the refined meshes, the simulation only converged with first order discretization but not with second order (see picture RefinedMesh_SecondOrder_ResidualPlot). I monitored the flow at the outlets. The monitors showed a constant, almost oscillating, change in the outflow (see picture RefinedMesh_SecondOrder_MassFlowMonitor). This was not the case in the initial simulation with the coarse mesh.



I'm unsing the following settings with a tet-Mesh. For the flow I've calculated reynolds numbers of about 4000 at the inlet, about 3000 at the main outlet and about 1000 at the small outlets.



Model: k-w-SST, with Low Re correction

Boundary Conditions
Inlet: Mass-Flow-Inlet
Main Outlet: Mass- Flow- Outlet
Small Outlets: Pressure Outlet with 0 gauge pressure
Methods:
Scheme: Coupled
Gradient: Green-Gaus Node Based
Pressure: PRESTO!
Momentum: Second Order Upwind
Turbulent Kinetic Energy: Second Order Upwind
Specific Dissipation Rate: Second Order Upwind
with pseudo transient setting

Controls:
Pressure: 0,2
Momentum: 0,3
Density: 1
Body Forces: 1
Turbulent Kinetic Energy: 0,75
Specific Dissipation Rate: 0,75
Turbulent Viscosity: 1


So far I've tried to:
- lower the relaxation factors
- use differnt discretization methods
- use differnt initializations


I really hope someone can help me.



Best regards,
Peter









Last edited by cola93; March 31, 2021 at 09:32.
cola93 is offline   Reply With Quote

Reply

Tags
convergence problems, mesh independence study, sst k-omega


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Mesh independence study for transient simulation snejball91 CFX 9 November 17, 2022 02:12
pimpleDyMFoam computation randomly stops babapeti OpenFOAM Running, Solving & CFD 5 January 24, 2018 06:28
Moving mesh Niklas Wikstrom (Wikstrom) OpenFOAM Running, Solving & CFD 122 June 15, 2014 07:20
[blockMesh] mesh causing problems with convergence Tetragramm OpenFOAM Meshing & Mesh Conversion 0 September 22, 2012 17:00
Could anybody help me see this error and give help liugx212 OpenFOAM Running, Solving & CFD 3 January 4, 2006 19:07


All times are GMT -4. The time now is 06:53.