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

Mesh Independent Test

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   July 27, 2017, 11:46
Default Mesh Independent Test
  #1
New Member
 
Max
Join Date: Jun 2017
Posts: 21
Rep Power: 8
max.kozak is on a distinguished road
Hello all, I am attempting to run simulations in Fluent for a mesh that I generated in ICEM. The geometry is a pipe inlet into a vertical cylinder, which fills up and then exits out of another pipe. I have imported the initial coarse mesh and I have run a simulation. I now would like to perform a mesh independent test and I am having a few questions.

1.) I would like to do a global comparison test for my different mesh refinements where I look at multiple velocity points throughout the volume with each refinement. How do I view velocity at certain points in the volume, and continue to do so with each refinement?

2.) I would like to compute the boundary layer thickness. Is the best way to do this to make a slice plane and plot the velocity contour, determining at what position approx. 99% of the free stream velocity is reached?

3.) When I run my simulation, the residuals are high. The velocity residuals only decrease to about 1e-2, whereas the continuity residual stay close to 1. Could this be because the solution is initialized close to the actual solution value? It still seems to me the velocity residuals should further decrease, so I'm not sure how to determine convergence

I've attached my geometry in case that would be helpful. Thanks for any feedback on the questions I'm having.
Attached Images
File Type: png Geometry and Mesh.PNG (50.8 KB, 11 views)
max.kozak is offline   Reply With Quote

Old   July 31, 2017, 06:46
Default
  #2
New Member
 
Martin
Join Date: Apr 2017
Location: Germany
Posts: 26
Rep Power: 9
2phase is on a distinguished road
Hi Max,

I hope I don't tell you something wrong, but from my point of view:

3) I guess you are wrong. if you were close, residuals should be very small. Have a closer look at what residuals are and try to understand. If you do not achieve convergence in steady flow you probably have to switch to transient.

1) as far as I know you can define these sample points in CFD-Post. Create a new location and look for the right settings (it's called sample data if you create lines or faces, I never actually tried with points)

Hope I could help.

Good luck, Martin
2phase is offline   Reply With Quote

Old   July 31, 2017, 10:32
Default
  #3
Member
 
MayTheFlowBeWithYou's Avatar
 
I have to remain anonymous, I'm sorry.
Join Date: Jun 2017
Location: The Netherlands, Delft University of Technology
Posts: 48
Rep Power: 8
MayTheFlowBeWithYou is on a distinguished road
Are you looking at scaled or unscaled residuals
MayTheFlowBeWithYou is offline   Reply With Quote

Reply

Tags
boundary layer thickness, mesh independency


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
sliding mesh problem in CFX Saima CFX 46 September 11, 2021 07:38
[ICEM] 2D hybrid mesh (unstructured mesh highly dependent on structured mesh parameters) shubham jain ANSYS Meshing & Geometry 1 April 10, 2017 05:03
[snappyHexMesh] Snappyhex mesh: poor inlet mesh Swagga5aur OpenFOAM Meshing & Mesh Conversion 1 December 3, 2016 16:59
Problem with Mesh Independent Convergence kastarkas CFX 9 November 24, 2016 03:49
3D Hybrid Mesh Errors DarrenC ANSYS Meshing & Geometry 11 August 5, 2013 06:42


All times are GMT -4. The time now is 08:56.