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August 8, 2012, 12:02 |
rhoSImplecFoam still having issues!
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#1 |
Senior Member
Mihai Pruna
Join Date: Apr 2010
Location: Boston
Posts: 195
Rep Power: 16 |
Please help!
Code:
/*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2.1.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ Build : 2.1.1-221db2718bbb Exec : rhoSimplecFoam Date : Aug 08 2012 Time : 10:49:13 Host : "cadnexus-cae" PID : 29421 Case : /home/cadnexus/OpenFOAM/cadnexus-2.1.1/run/sduct_div/sduct_100_inlet_vel_baseline nProcs : 1 sigFpe : Enabling floating point exception trapping (FOAM_SIGFPE). fileModificationChecking : Monitoring run-time modified files using timeStampMaster allowSystemOperations : Disallowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create mesh for time = 0 SIMPLE: convergence criteria field p tolerance 1e-05 field U tolerance 1e-05 field omega tolerance 1e-05 Reading thermophysical properties Selecting thermodynamics package hPsiThermo<pureMixture<sutherlandTransport<specieThermo<hConstThermo<perfectGas>>>>> Reading field U Reading/calculating face flux field phi Creating turbulence model Selecting RAS turbulence model kOmegaSST kOmegaSSTCoeffs { alphaK1 0.85034; alphaK2 1; alphaOmega1 0.5; alphaOmega2 0.85616; Prt 1; gamma1 0.5532; gamma2 0.4403; beta1 0.075; beta2 0.0828; betaStar 0.09; a1 0.31; c1 10; } Starting time loop Reading surface description: zNormal --> FOAM Warning : From function Foam::List<Foam::tetIndices> Foam::polyMeshTetDecomposition::faceTetIndices(const polyMesh&, label, label) in file meshes/polyMesh/polyMeshTetDecomposition/polyMeshTetDecomposition.C at line 565 No base point for face 160047, 4(62180 36360 67554 53019), produces a valid tet decomposition. --> FOAM Warning : From function Foam::List<Foam::tetIndices> Foam::polyMeshTetDecomposition::faceTetIndices(const polyMesh&, label, label) in file meshes/polyMesh/polyMeshTetDecomposition/polyMeshTetDecomposition.C at line 565 No base point for face 160047, 4(62180 36360 67554 53019), produces a valid tet decomposition. --> FOAM Warning : From function Foam::List<Foam::tetIndices> Foam::polyMeshTetDecomposition::faceTetIndices(const polyMesh&, label, label) in file meshes/polyMesh/polyMeshTetDecomposition/polyMeshTetDecomposition.C at line 565 No base point for face 169137, 4(32651 49488 69117 53693), produces a valid tet decomposition. --> FOAM Warning : From function Foam::List<Foam::tetIndices> Foam::polyMeshTetDecomposition::faceTetIndices(const polyMesh&, label, label) in file meshes/polyMesh/polyMeshTetDecomposition/polyMeshTetDecomposition.C at line 565 No base point for face 169137, 4(32651 49488 69117 53693), produces a valid tet decomposition. --> FOAM Warning : From function Foam::List<Foam::tetIndices> Foam::polyMeshTetDecomposition::faceTetIndices(const polyMesh&, label, label) in file meshes/polyMesh/polyMeshTetDecomposition/polyMeshTetDecomposition.C at line 565 No base point for face 174804, 4(24053 54113 70087 54114), produces a valid tet decomposition. --> FOAM Warning : From function Foam::List<Foam::tetIndices> Foam::polyMeshTetDecomposition::faceTetIndices(const polyMesh&, label, label) in file meshes/polyMesh/polyMeshTetDecomposition/polyMeshTetDecomposition.C at line 565 No base point for face 174804, 4(24053 54113 70087 54114), produces a valid tet decomposition. --> FOAM Warning : From function Foam::List<Foam::tetIndices> Foam::polyMeshTetDecomposition::faceTetIndices(const polyMesh&, label, label) in file meshes/polyMesh/polyMeshTetDecomposition/polyMeshTetDecomposition.C at line 565 No base point for face 179330, 4(24272 54485 70817 54484), produces a valid tet decomposition. --> FOAM Warning : From function Foam::List<Foam::tetIndices> Foam::polyMeshTetDecomposition::faceTetIndices(const polyMesh&, label, label) in file meshes/polyMesh/polyMeshTetDecomposition/polyMeshTetDecomposition.C at line 565 No base point for face 179330, 4(24272 54485 70817 54484), produces a valid tet decomposition. Time = 1 GAMG: Solving for Ux, Initial residual = 1, Final residual = 0.0181092, No Iterations 2 GAMG: Solving for Uy, Initial residual = 1, Final residual = 0.0169639, No Iterations 2 GAMG: Solving for Uz, Initial residual = 1, Final residual = 0.026404, No Iterations 2 GAMG: Solving for p, Initial residual = 1, Final residual = 0.096998, No Iterations 19 time step continuity errors : sum local = 474.441, global = -56.4332, cumulative = -56.4332 rho max/min : 1.28594 0.5 GAMG: Solving for h, Initial residual = 1, Final residual = 0.0497605, No Iterations 2 GAMG: Solving for omega, Initial residual = 0.123066, Final residual = 0.00214602, No Iterations 2 GAMG: Solving for k, Initial residual = 1, Final residual = 0.0881728, No Iterations 1 ExecutionTime = 177.11 s ClockTime = 180 s Time = 2 GAMG: Solving for Ux, Initial residual = 0.511533, Final residual = 0.0391677, No Iterations 1 GAMG: Solving for Uy, Initial residual = 0.541348, Final residual = 0.0441529, No Iterations 1 GAMG: Solving for Uz, Initial residual = 0.588956, Final residual = 0.0252274, No Iterations 2 GAMG: Solving for p, Initial residual = 0.0901925, Final residual = 0.00839962, No Iterations 6 time step continuity errors : sum local = 323.523, global = -51.6731, cumulative = -108.106 rho max/min : 1.28886 0.5 GAMG: Solving for h, Initial residual = 0.958599, Final residual = 0.0217326, No Iterations 2 #0 Foam::error::printStack(Foam::Ostream&) in "/opt/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" #1 Foam::sigFpe::sigHandler(int) in "/opt/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" #2 in "/lib/x86_64-linux-gnu/libc.so.6" #3 Foam::hPsiThermo<Foam::pureMixture<Foam::sutherlandTransport<Foam::specieThermo<Foam::hConstThermo<Foam::perfectGas> > > > >::calculate() in "/opt/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libbasicThermophysicalModels.so" #4 Foam::hPsiThermo<Foam::pureMixture<Foam::sutherlandTransport<Foam::specieThermo<Foam::hConstThermo<Foam::perfectGas> > > > >::correct() in "/opt/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libbasicThermophysicalModels.so" #5 in "/opt/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/bin/rhoSimplecFoam" #6 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6" #7 in "/opt/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/bin/rhoSimplecFoam" Floating point exception (core dumped) cadnexus@cadnexus-cae:~/OpenFOAM/cadnexus-2.1.1/run/sduct_div/sduct_100_inlet_vel_baseline$ |
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August 8, 2012, 12:04 |
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#2 |
Senior Member
Mihai Pruna
Join Date: Apr 2010
Location: Boston
Posts: 195
Rep Power: 16 |
checkmesh results:
Code:
Exec : checkMesh Date : Aug 08 2012 Time : 11:02:04 Host : "cadnexus-cae" PID : 29636 Case : /home/cadnexus/OpenFOAM/cadnexus-2.1.1/run/sduct_div/sduct_100_inlet_vel_baseline nProcs : 1 sigFpe : Enabling floating point exception trapping (FOAM_SIGFPE). fileModificationChecking : Monitoring run-time modified files using timeStampMaster allowSystemOperations : Disallowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time fileName::stripInvalid() called for invalid fileName constant(copy).tar.gz For debug level (= 2) > 1 this is considered fatal Aborted (core dumped) cadnexus@cadnexus-cae:~/OpenFOAM/cadnexus-2.1.1/run/sduct_div/sduct_100_inlet_vel_baseline$ checkMesh /*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2.1.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ Build : 2.1.1-221db2718bbb Exec : checkMesh Date : Aug 08 2012 Time : 11:03:06 Host : "cadnexus-cae" PID : 29643 Case : /home/cadnexus/OpenFOAM/cadnexus-2.1.1/run/sduct_div/sduct_100_inlet_vel_baseline nProcs : 1 sigFpe : Enabling floating point exception trapping (FOAM_SIGFPE). fileModificationChecking : Monitoring run-time modified files using timeStampMaster allowSystemOperations : Disallowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create polyMesh for time = 0 Time = 0 Mesh stats points: 6376565 faces: 16789124 internal faces: 15762710 cells: 5249544 boundary patches: 12 point zones: 0 face zones: 0 cell zones: 0 Overall number of cells of each type: hexahedra: 4568654 prisms: 143215 wedges: 0 pyramids: 0 tet wedges: 1 tetrahedra: 0 polyhedra: 537674 Checking topology... Boundary definition OK. Cell to face addressing OK. Point usage OK. Upper triangular ordering OK. Face vertices OK. Number of regions: 1 (OK). Checking patch topology for multiply connected surfaces ... Patch Faces Points Surface topology topYmax 0 0 ok (empty) bottomYmin 0 0 ok (empty) inletXmin 0 0 ok (empty) outletXmax 0 0 ok (empty) rightZmax 0 0 ok (empty) leftZmin 36672 41286 ok (non-closed singly connected) SDuctOutlet 29668 30254 ok (non-closed singly connected) vol1face2 605591 690845 ok (non-closed singly connected) vol1face3 0 0 ok (empty) vol1face4 0 0 ok (empty) vol1face5 313384 317020 ok (non-closed singly connected) SDuctInlet 41099 41814 ok (non-closed singly connected) Checking geometry... Overall domain bounding box (-0.100006 -0.0814332 0) (2.05019 0.911797 0.353048) Mesh (non-empty, non-wedge) directions (1 1 1) Mesh (non-empty) directions (1 1 1) Boundary openness (-2.48235e-15 2.82511e-16 -1.21331e-14) OK. Max cell openness = 3.4866e-16 OK. Max aspect ratio = 8.79826 OK. Minumum face area = 3.80834e-08. Maximum face area = 0.0025653. Face area magnitudes OK. Min volume = 7.99893e-12. Max volume = 0.000127949. Total volume = 0.257158. Cell volumes OK. Mesh non-orthogonality Max: 57.0097 average: 9.26743 Non-orthogonality check OK. Face pyramids OK. Max skewness = 3.91413 OK. Coupled point location match (average 0) OK. Mesh OK. End |
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August 8, 2012, 12:06 |
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#3 |
Senior Member
Mihai Pruna
Join Date: Apr 2010
Location: Boston
Posts: 195
Rep Power: 16 |
Image of a solved case (using simpleFoam)
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August 10, 2012, 16:09 |
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#5 |
Senior Member
Mihai Pruna
Join Date: Apr 2010
Location: Boston
Posts: 195
Rep Power: 16 |
as of now, yes, no matter what I do I am experiencing crashes rather soon in the solution.
Thank you. |
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August 10, 2012, 16:26 |
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#7 |
Super Moderator
Tobias Holzmann
Join Date: Oct 2010
Location: Bad Wörishofen
Posts: 2,711
Blog Entries: 6
Rep Power: 52 |
Your uploaded files are working.
I dont know what you are wanna do exaclty couse your files are in caos And I think you are not using OF in a terminal arent you? Couse all headers are away. Well i can solve that block with rhoSimplecFoam and I am not sure if you declare BC in k and omega like that: Code:
inletXmin { type freestream; freestreamValue uniform 12.500000; value uniform 12.500000; } But I have never used the freeStream BC. I am confused, where is your problem? Well maybe there is a problem of your BC for p and U time step continuity errors : sum local = 474.441, global = -56.4332, cumulative = -56.4332 |
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August 11, 2012, 19:04 |
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#8 |
Senior Member
Mihai Pruna
Join Date: Apr 2010
Location: Boston
Posts: 195
Rep Power: 16 |
Tobi, that patch is not considered because of the internal flow condition which meshes inside the duct and thus eliminates the patches outside that domain.
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August 12, 2012, 05:06 |
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#9 | |
Super Moderator
Tobias Holzmann
Join Date: Oct 2010
Location: Bad Wörishofen
Posts: 2,711
Blog Entries: 6
Rep Power: 52 |
Quote:
But your case is working, so whats the problem? I just wanted to help you but I think you dont need my help at all. Hope you get it work and have a nice sunday. Tobi |
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August 12, 2012, 10:41 |
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#10 |
Senior Member
Mihai Pruna
Join Date: Apr 2010
Location: Boston
Posts: 195
Rep Power: 16 |
hi Tobi, I included the streamlines I got using the incompressible solver simpleFoam in order to showcase the geometry and desired flow. Unfortunately, to perform a realistic and accurate simulation at the inlet speeds I used - 100m/s, a compressible flow solver is required. and that's where it crashes.
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August 12, 2012, 11:30 |
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#11 |
Super Moderator
Tobias Holzmann
Join Date: Oct 2010
Location: Bad Wörishofen
Posts: 2,711
Blog Entries: 6
Rep Power: 52 |
hi,
okay you used a simpleFoam solver to test if its working. Hmmm ... but your continuity crashes too. Look at your values. Maybe you can have a look at the first time step and see where your problem zones are. Can you uplaod your case, if yes, I c an have a look at it. Tobi |
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