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

Backward Facing Step

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   May 30, 2012, 09:40
Default Backward Facing Step
  #1
New Member
 
L.M. Yang
Join Date: Oct 2011
Posts: 9
Rep Power: 14
LBMer_Young is on a distinguished road
Hi, guys
I am simulating the laminar backward facing step with a 2D incompressible CFD code. Could any of you direct me how to set the inlet and outlet boundary conditions? The velocity profile of inlet boundary have been obtained. However, how do I set the pressure of inlet boundary and pressure and velocity of outlet boundary?

With kind regards,
Laman Yang
LBMer_Young is offline   Reply With Quote

Old   May 30, 2012, 14:39
Default
  #2
Member
 
Peter Galimutti
Join Date: May 2012
Posts: 37
Rep Power: 13
p.galimutti is on a distinguished road
Since you already have a velocity profile, you do not need to set any inlet pressure. Pressure is implicit calculation based on velocity.

At the outlet 1 atm pressure can be given!

BTW, you said you are using code, so giving boundary conditions is specific to that code and check the manual on how to define b.cs
p.galimutti is offline   Reply With Quote

Old   May 30, 2012, 21:03
Default
  #3
New Member
 
L.M. Yang
Join Date: Oct 2011
Posts: 9
Rep Power: 14
LBMer_Young is on a distinguished road
Quote:
Originally Posted by p.galimutti View Post
Since you already have a velocity profile, you do not need to set any inlet pressure. Pressure is implicit calculation based on velocity.

At the outlet 1 atm pressure can be given!

BTW, you said you are using code, so giving boundary conditions is specific to that code and check the manual on how to define b.cs
Hi, Peter
Thanks for you comments. Actually, the code is developed by myself. In this code, the conventional Navier-Stokes equation is solved rather than its incompressible forms (e.g. governing equation for artificial compressibility method and pre-conditioning method). So, in the inlet boundary there are three characteristics enter and one leaves the physical domain, i.e., the pressure in b.c need to extrapolate from the interior of the physical domain. My confusion is how to calculate the pressure. Similarly, the velocities in outlet b.c need to extrapolate from the interior of the physical domain. How could I evaluate the velocities in outlet b.c.

regards
LBMer_Young is offline   Reply With Quote

Old   May 31, 2012, 08:35
Default
  #4
Senior Member
 
Andrew
Join Date: Mar 2009
Location: Washington, DC
Posts: 209
Rep Power: 18
mettler is on a distinguished road
have you thought about transforming your equations to the streamline-vorticity equations? that way your pressure term drops out, and the bc's are pretty straight forward.
mettler is offline   Reply With Quote

Old   May 31, 2012, 10:29
Default
  #5
New Member
 
L.M. Yang
Join Date: Oct 2011
Posts: 9
Rep Power: 14
LBMer_Young is on a distinguished road
Thanks for your advice. However, the flux solver in my code is developed by lattice Boltzmann method and the governing equation is the conventional Navier-Stokes equation. It is harder to transform the governing equation.
LBMer_Young 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
How to write k and epsilon before the abnormal end xiuying OpenFOAM Running, Solving & CFD 8 August 27, 2013 15:33
Backward facing step. Fluids Main CFD Forum 7 December 4, 2012 11:28
Upgraded from Karmic Koala 9.10 to Lucid Lynx10.04.3 bookie56 OpenFOAM Installation 8 August 13, 2011 04:03
IcoFoam parallel woes msrinath80 OpenFOAM Running, Solving & CFD 9 July 22, 2007 02:58
Could anybody help me see this error and give help liugx212 OpenFOAM Running, Solving & CFD 3 January 4, 2006 18:07


All times are GMT -4. The time now is 07:02.