CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > General Forums > Main CFD Forum

Boundary conditions for windtunnel

Register Blogs Community New Posts Updated Threads Search

Like Tree1Likes
  • 1 Post By Totalsim

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   December 10, 2015, 18:55
Default Boundary conditions for windtunnel
  #1
New Member
 
Join Date: Jun 2015
Location: Great Britain
Posts: 16
Rep Power: 11
cfdblender is on a distinguished road
Hello,

I've got a rectangular domain setup to simulate a 3/4 open-section windtunnel. What would be the correct boundary conditions for the walls that represent the open areas of the tunnel?

I already tried pressure outlet conditions for the 'open' walls and the simulation failed miserably - reversed flow all over the place! I'm now using slip walls and suppressed the prism layer on them, but I'm not sure this is really correct.

The inlet wall is set to velocity inlet condition. The outlet set to pressure outlet condition.
cfdblender is offline   Reply With Quote

Old   December 11, 2015, 06:17
Default
  #2
Member
 
Totalsim's Avatar
 
Jon
Join Date: Mar 2013
Posts: 47
Rep Power: 13
Totalsim is on a distinguished road
The only real option with wind tunnel correlation work is to model the whole thing. You will need to include the room the jet sits in and ideally and upstream geometry you can get hold of.

If you replace the edge of the jet with a free slip wall or symmetry plane you will not get reasonable correlation.

When we do tunnel correlation work the models can get huge. It's necessary to get things to correlate.

Good luck.
cfdblender likes this.
__________________
TotalSim CFD Engineer
www.totalsimulation.co.uk
Totalsim is offline   Reply With Quote

Old   December 11, 2015, 07:17
Default
  #3
New Member
 
Join Date: Jun 2015
Location: Great Britain
Posts: 16
Rep Power: 11
cfdblender is on a distinguished road
Quote:
Originally Posted by Totalsim View Post
The only real option with wind tunnel correlation work is to model the whole thing. You will need to include the room the jet sits in and ideally and upstream geometry you can get hold of.

If you replace the edge of the jet with a free slip wall or symmetry plane you will not get reasonable correlation.

When we do tunnel correlation work the models can get huge. It's necessary to get things to correlate.

Good luck.
Thanks Totalsim. I see your point. I don't have complete information on the geometry around windtunnel - I'll have to use my best guess or use a simplified geometry.
cfdblender is offline   Reply With Quote

Reply

Tags
boundary conditions, wall boundary condition, windtunnel


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 08:38
Radiation in semi-transparent media with surface-to-surface model? mpeppels CFX 11 August 22, 2019 08:30
GETVAR Error in Multiband Monte Carlo Radiation Simulation with Directional Source silvan CFX 3 June 16, 2014 10:49
Question about heat transfer coefficient setting for CFX Anna Tian CFX 1 June 16, 2013 07:28
[Commercial meshers] Trimmed cell and embedded refinement mesh conversion issues michele OpenFOAM Meshing & Mesh Conversion 2 July 15, 2005 05:15


All times are GMT -4. The time now is 00:27.