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

Low Reynolds Modeling Lam Bremhorst

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   April 13, 2010, 16:23
Default Low Reynolds Modeling Lam Bremhorst
  #1
Member
 
Moritz Wied
Join Date: Mar 2010
Location: suttgart, germany
Posts: 35
Rep Power: 16
Mo-ITB is on a distinguished road
Hi everybody,

i am new in openFoam and at the moment also trying to make a low-Reynolds-Model work.
I use the LamBremhorstKE with the pisoFoam solver. I think that k and epsilon explode, and i get this error message:








/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
Build : 1.6-f802ff2d6c5a
Exec : pisoFoam
Date : Apr 12 2010
Time : 17:38:30
Host : itb15
PID : 13551
Case : /CFD/Moritz/ahmed_low_re_2
nProcs : 1
SigFpe : Enabling floating point exception trapping (FOAM_SIGFPE).

// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Create time

Create mesh for time = 0

Reading field p

Reading field U

Reading/calculating face flux field phi

Selecting incompressible transport model Newtonian
Selecting turbulence model type RASModel
Selecting RAS turbulence model LamBremhorstKE
--> FOAM Warning :
From function GeometricField<Type, PatchField, GeoMesh>::readIfPresent()
in file /CFD/Daniel/src-openfoam/install/OpenFOAM-1.6/src/OpenFOAM/lnInclude/GeometricField.C at line 107
read option IOobject::MUST_READ suggests that a read constructor for field epsilon would be more appropriate.
^[[5;5~LamBremhorstKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 1.3;
}


Starting time loop

Time = 1e-07

Courant Number mean: 0 max: 0
DILUPBiCG: Solving for Ux, Initial residual = 1, Final residual = 1.31903e-16, No Iterations 1
DILUPBiCG: Solving for Uy, Initial residual = 0, Final residual = 0, No Iterations 0
DILUPBiCG: Solving for Uz, Initial residual = 0, Final residual = 0, No Iterations 0
DICPCG: Solving for p, Initial residual = 1, Final residual = 0.0978004, No Iterations 297
time step continuity errors : sum local = 5.58285e-08, global = -1.88251e-10, cumulative = -1.88251e-10
DICPCG: Solving for p, Initial residual = 0.0402446, Final residual = 9.95978e-07, No Iterations 367
time step continuity errors : sum local = 8.99511e-11, global = 1.63882e-14, cumulative = -1.88235e-10
#0 Foam::error:rintStack(Foam::Ostream&) in "/usr/local/OPENFOAM/OpenFOAM-1.6/lib/linux64GccDPOpt/libOpenFOAM.so"
#1 Foam::sigFpe::sigFpeHandler(int) in "/usr/local/OPENFOAM/OpenFOAM-1.6/lib/linux64GccDPOpt/libOpenFOAM.so"
#2 ?? in "/lib64/libc.so.6"
#3 Foam::divide(Foam::Field<double>&, Foam::UList<double> const&, Foam::UList<double> const&) in "/usr/local/OPENFOAM/OpenFOAM-1.6/lib/linux64GccDPOpt/libOpenFOAM.so"
#4 void Foam::divide<Foam::fvPatchField, Foam::volMesh>(Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&) in "/usr/local/OPENFOAM/OpenFOAM-1.6/lib/linux64GccDPOpt/libincompressibleRASModels.so"
#5 Foam::tmp<Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> > Foam:perator/<Foam::fvPatchField, Foam::volMesh>(Foam::tmp<Foam::GeometricField<doub le, Foam::fvPatchField, Foam::volMesh> > const&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&) in "/usr/local/OPENFOAM/OpenFOAM-1.6/lib/linux64GccDPOpt/libincompressibleRASModels.so"
#6 Foam::incompressible::RASModels::LamBremhorstKE::c orrect() in "/usr/local/OPENFOAM/OpenFOAM-1.6/lib/linux64GccDPOpt/libincompressibleRASModels.so"
#7 main in "/usr/local/OPENFOAM/OpenFOAM-1.6/applications/bin/linux64GccDPOpt/pisoFoam"
#8 __libc_start_main in "/lib64/libc.so.6"
#9 __gxx_personality_v0 in "/usr/local/OPENFOAM/OpenFOAM-1.6/applications/bin/linux64GccDPOpt/pisoFoam"
Gleitkomma-Ausnahme







I also ran the model with a coarser mesh, there it started calculating but k and epsilon went to -e12 to e12 and it finally crashed.
by the way, is it allowed that those values become negative?


Does anybody know if the LamBremhorst-Model is working in the actual version?

If yes, could you give me a hint, which initial conditions you use?
As boundary cond. i use

epsilon zeroGradient
k fixed value 0.000000001
nut calculated

all surfaces are defined as patch.

it would be great if somebody could explain experiences maybe already made.

all the best,
Moritz
Mo-ITB is offline   Reply With Quote

Old   April 14, 2010, 03:21
Default
  #2
Super Moderator
 
niklas's Avatar
 
Niklas Nordin
Join Date: Mar 2009
Location: Stockholm, Sweden
Posts: 693
Rep Power: 29
niklas will become famous soon enoughniklas will become famous soon enough
#4 void Foam::divide<Foam::fvPatchField, Foam::volMesh>(Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&) in "/usr/local/OPENFOAM/OpenFOAM-1.6/lib/linux64GccDPOpt/libincompressibleRASModels.so"

divison by zero, i.e initial and/or BC values of epsilon set to 0.

foam solver go booboo and complain, make unhappy noises and cry on the inside
niklas is offline   Reply With Quote

Old   April 15, 2010, 06:52
Default
  #3
Member
 
Moritz Wied
Join Date: Mar 2010
Location: suttgart, germany
Posts: 35
Rep Power: 16
Mo-ITB is on a distinguished road
thanks for your response, Niklas. I guess the problem is not that i have zeros, but that the epsilon is going up till the value gets too large. i can see in postprocessing, that first epsilon rises and k follows the next time step, so i guess something is wrong with the epsilon...
if somebody is able to use the model, could you post your settings (layer width, nu, U, bc an initials)? That would be a great help, i just dont find my mistake.

cheers,
moritz
Mo-ITB is offline   Reply With Quote

Old   November 17, 2017, 12:07
Default
  #4
New Member
 
Felipe Murad
Join Date: Mar 2017
Posts: 11
Rep Power: 9
FMurad is on a distinguished road
Sorry to pick this thread up after 7 years (hehe). I was facing the same problem you mentioned when I used this model (my epsilon's values were growing too high).
Then I tried to use other model's results (LienCubic in my case) as a initial condition for k and epsilon and I've got better (but not perfect) results.

Also, this document,
http://www.diva-portal.org/smash/get...FULLTEXT01.pdf

compares some openfoam's low(and high) reynolds models. Moreover they got excelent results for the lambremhorst model. However, they use epsilon=0 as
a boundary condition at the wall even though the lambremhorst model specify
d epsilon/ dy =0


Hope this somewhat helps you or anyone.
FMurad 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
Turbulence model for low Reynolds number flow? Nokadu Main CFD Forum 3 May 26, 2013 12:42
low reynolds number models in Fluent doug Main CFD Forum 6 August 4, 2012 15:39
Low Reynolds number airfoil. Pablo Cornejo FLUENT 14 October 19, 2005 10:41
Multicomponent fluid Andrea CFX 2 October 11, 2004 06:12
Low Reynolds number K-Omega modeling Athar Zaidi Main CFD Forum 0 October 31, 1999 14:59


All times are GMT -4. The time now is 23:13.