|
[Sponsors] |
July 18, 2005, 09:54 |
residual in the pressure correction
|
#1 |
Guest
Posts: n/a
|
Hi all! I am facing a problem of convergence in the pressure correction equation.The code that I am writing is about compressible viscous unsteady turbulent flow.The residual of the pressure correction is of the order of 0.001 and it never becomes less.I think the thing that I am not doing correct is the implementation of the boundary conditions.Can you please describe me with detail what they should be? (Ap*P'=SUM(Ai*Pi)+Su). The cell next to the wall has: Ai=0.0 and on the inlet and outlet is again: Aw=0.0 and Ae=0.0.
I hope there is someone out there that can help me. Thank you in advance! |
|
July 21, 2005, 22:25 |
Re: residual in the pressure correction
|
#2 |
Guest
Posts: n/a
|
First contour the L1-norm of pressure coreection to see where are the locations of the maxima, then the next step. All those Ai equal to 0 at both the inlet and outlet imply both pressure values fixed. That is wrong, I guess.
|
|
July 28, 2005, 05:43 |
Re: residual in the pressure correction
|
#3 |
Guest
Posts: n/a
|
Sorry for being late, but I was on holidays these days. Yes, I specify pressure at both inlet and outlet. Because the velocity is not that high (around 20-30 m/sec), I specify static pressure there. My question was if I should add some more boundary conditions next to the walls and at inlet-outlet. Thank you!
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Darcy-Forchheimer law for specifying Porous Zones | Ger_US | OpenFOAM Running, Solving & CFD | 37 | April 10, 2022 04:38 |
Compressible Nozzle Flow | sebastian | OpenFOAM Running, Solving & CFD | 14 | September 21, 2016 11:47 |
ForcesCoeffs | ronaldo | OpenFOAM | 4 | September 14, 2009 08:11 |
Convergence moving mesh | lr103476 | OpenFOAM Running, Solving & CFD | 30 | November 19, 2007 15:09 |
Modeling in micron scale using icoFoam | m9819348 | OpenFOAM Running, Solving & CFD | 7 | October 27, 2007 01:36 |