CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > OpenFOAM > OpenFOAM Running, Solving & CFD

Problem simulating a reactor inlet area using rhoReactingFoam

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   September 3, 2014, 10:10
Default Problem simulating a reactor inlet area using rhoReactingFoam
  #1
Member
 
Join Date: May 2014
Location: Germany
Posts: 31
Rep Power: 11
hester is on a distinguished road
Hello OpenFoamers,

I'm having difficulties with rhoReactingFoam. I try to simulate a reactor but due to problems with the inlet area I created a smaller model, which just contains the inlet area (pipes) and is discussed below. I tried to make it work for weeks but I can't find my mistake.

=== geometry and mesh ===

This is what it looks like:
https://dl.dropboxusercontent.com/s/...9jfa6/mesh.jpg
The inlet area contains an abrupt cross section enlargement from 4.57 mm to 23.5 mm.
I'm using an unstructured mesh, since I use Salome to create my mesh. Later on the geometry will get more complex so I will use an unstructured mesh anyway.
All mesh checks are okay.
http://dl.dropboxusercontent.com/s/l.../checkmesh.log
Could the mesh be a problem? The max non-orthogonality is 50. Is that too high? I don't have much experience to evaluate this value correctly.

=== initial and boundary conditions ===

These are my files in 0/:
p: https://www.dropbox.com/s/337xqn2iimxd50o/p?dl=0
I have a fixed pressure of 9.5 Pa at the outlet. During my research I found the waveTransmissive boundary condition which should work for my problem. I used fixedValue at first, but then the flow got "bounced back" from the outlet area.
U: https://www.dropbox.com/s/nmkkfzz745z8t27/U?dl=0
The inlet velocity for this test case is 10 m/s, max(Co) is 0.12. In the actual reactor I have velocities up to 70 m/s.
T: https://www.dropbox.com/s/uo4viafdps08kng/T?dl=0
Uniform temperature of 293 K in the whole domain and all boundaries.

I used no mixture, only Argon. Reactions are turned off, but combustion is still on.

=== simulation setup ===

My fvSolution and fvSchemes-file:
https://www.dropbox.com/s/7v6l7iuhl7...vSolution?dl=0
https://www.dropbox.com/s/4phkmjhy8v...fvSchemes?dl=0

=== problem ===

The temperature rises up to 300 K altough it should remain constant at 293 K.
After a while the simulation crashes with a sigFpe.
I included the log- file and the errror message.
https://www.dropbox.com/s/zhyvl7ly7dti2zp/log?dl=0
https://www.dropbox.com/s/st37blb2l2fzw9i/error?dl=0

I checked the BC and I think they're okay. Could the mesh be the problem? Or did I miss something?

Any help, comment or hint is greatly appreciated!
Thank you in advance.

hester

PS: Does anyone know how to actually show pictures in a post like it was done here: http://www.cfd-online.com/Forums/openfoam/98988-how-give-enough-info-get-help.html? I couldn't figure it out myself. And the include image doesn't seem to work with dropbox-urls...
Attached Images
File Type: jpg mesh2.jpg (95.5 KB, 10 views)

Last edited by hester; September 4, 2014 at 07:46.
hester is offline   Reply With Quote

Reply


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
Define area and depth for drag coefficient calculation for flow over of cylinders engr FLUENT 5 May 26, 2023 05:22
Reference Values- Reference Area Shivakanth FLUENT 12 June 6, 2017 00:18
Water subcooled boiling Attesz CFX 7 January 5, 2013 03:32
2D flow calculation around an airfoil Talayal FLUENT 2 December 13, 2012 15:21
Adiabatic and Rotating wall (Convection problem) ParodDav CFX 5 April 29, 2007 19:13


All times are GMT -4. The time now is 07:38.