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

boundary layer

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   October 23, 2013, 10:10
Default boundary layer
  #1
New Member
 
Arvindh
Join Date: Oct 2013
Posts: 19
Rep Power: 13
Arvin is on a distinguished road
Hey guys, I am really stuck here. I am new to fluent and I am modelling a steady state 2d tank for natural convection problem. Size of the tank being 100 by 100 mm. I have attached a boundary layer as well as face mesh. Total no. of nodes is 1000000. Do I need to check internal continuity?. Despite many attempts, I am not able to get converged solution, not even the plumes from bottom surface. My boundary conditions are 1.Heat flux is supplied at bottom plate. 2.Other three sides are kept at ambient temperature. Working fluid is water. Please do help me out. I want to know the settings that needs to be applied in fluent. Boussinesq or Polynomial for water? Standard or PRESTO? Any other important things to be set?
Thanks. I do hope I get help as soon as possible as I am running out of time.
Arvin is offline   Reply With Quote

Old   October 24, 2013, 10:38
Default
  #2
Senior Member
 
Join Date: Mar 2009
Location: Indiana, US
Posts: 186
Rep Power: 17
delaneyluke is on a distinguished road
Could you be more specific about what's not converging.
What have you tried so far to improve convergence?
Natural convection is an unsteady phenomenon, have you tried a transient analysis?

Regards
Luke
delaneyluke is offline   Reply With Quote

Old   October 24, 2013, 10:55
Default
  #3
New Member
 
Arvindh
Join Date: Oct 2013
Posts: 19
Rep Power: 13
Arvin is on a distinguished road
No, I have not yet tried transient analysis since I am not getting convergence on steady state itself. I have a strong doubt on using Boussinesq approximation. Can you guide me on this?
Thanks.
Arvin is offline   Reply With Quote

Old   October 28, 2013, 15:11
Default
  #4
Senior Member
 
Join Date: Mar 2009
Location: Indiana, US
Posts: 186
Rep Power: 17
delaneyluke is on a distinguished road
Well the reason you dont get convergence with a steady state solver is because the phenomenon is transient. A transient phenomenon will not converge with a steady state solver.
Whats your question about the Boussinesq approx

Regards
Luke
delaneyluke is offline   Reply With Quote

Old   October 29, 2013, 05:42
Default
  #5
New Member
 
Arvindh
Join Date: Oct 2013
Posts: 19
Rep Power: 13
Arvin is on a distinguished road
Hi, thanks Luke. My question is obviously we need to specify density as a function of temperature. And we can do that either by specifying density as Boussinesq approx or by using polynomial and other piecewise functions. But for natural convection problem, generally Boussinesq approx is used. Why is that? It can be used in phenomena involving small temperature changes, so how do we know that? So, how to select the appropriate function of density?
Secondly what is the difference between pressure based solver and density based solver? For natural convection problems why can't we use density based solver?
Thanks.
Arvin is offline   Reply With Quote

Reply

Tags
boundary layer thickness, natural convection


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
Prism Layer (Boundary Layer) Thickness Peter-27 STAR-CCM+ 12 March 27, 2022 13:25
[snappyHexMesh] No layers in a small gap bobburnquist OpenFOAM Meshing & Mesh Conversion 6 August 26, 2015 10:38
Grid Independence of Boundary layer Luigi_ Main CFD Forum 0 December 14, 2011 14:42
Boundary Layer Question scottneh STAR-CCM+ 3 September 30, 2010 15:21
[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 16:42.