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August 23, 2013, 05:07
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#21 | |
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Member
Martin Novák
Join Date: Dec 2012
Location: Prague
Posts: 70
Rep Power: 13  |
Quote:
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August 23, 2013, 05:25
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#22 | |
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New Member
Basta
Join Date: Jul 2013
Posts: 28
Rep Power: 12 |
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August 23, 2013, 05:40
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#23 | |
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Member
Martin Novák
Join Date: Dec 2012
Location: Prague
Posts: 70
Rep Power: 13 |
Quote:
Prepare the test case properly and post it here. After that I may take a look on it. BR Martin |
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August 23, 2013, 06:45
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#24 | |
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New Member
Basta
Join Date: Jul 2013
Posts: 28
Rep Power: 12 |
Quote:
Which case do you mean because at the begining i posted my valve studying case problem . After that i posted just a simple case to generalize my problem which is just a cylinder see post #18. So i thought that you told me about the simple case which is just a cyliner and i had the same problem at the interface between the inlet and the wall with elements with very high pressure. |
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August 23, 2013, 12:24
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#25 | |
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Member
Martin Novák
Join Date: Dec 2012
Location: Prague
Posts: 70
Rep Power: 13 |
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August 26, 2013, 09:22
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#26 |
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New Member
Basta
Join Date: Jul 2013
Posts: 28
Rep Power: 12 |
Dear Martin,
Excuse me , I attached a wrong case. Here are the write one. Best regards, Mina |
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August 28, 2013, 09:08
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#27 |
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New Member
Basta
Join Date: Jul 2013
Posts: 28
Rep Power: 12 |
Hello all,
Did anybody have a solution for my problem? Best regards, Mina |
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August 28, 2013, 11:46
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#28 |
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Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 26 |
Hi Mina
I changed divScheme by adding bounded to the terms with phi and it seems run without problem. Code:
divSchemes
{
default none;
div(phi,U) bounded Gauss GammaV 0.5; //was 0.5 1.0
div(phi,k) bounded Gauss limitedLinear 1;
div(phi,epsilon) bounded Gauss limitedLinear 1;
//div((nuEff*dev(grad(U).T()))) Gauss linear;
div((nuEff*dev(T(grad(U))))) Gauss linear;
//div((nuEff*dev(grad(U).T()))) Gauss linear faceMDLimited Gauss linear 0.85;
//div(phi,U) Gauss linearUpwindV faceMDLimited linear 0.68; //was 0.5 1.0
//div(phi,k) Gauss linearUpwind faceMDLimited Gauss linear 0.2;
//div(phi,epsilon) Gauss linearUpwind faceMDLimited Gauss linear 0.91;
//div((nuEff*dev(grad(U).T()))) Gauss linearUpwind faceMDLimited Gauss linear 0.85;
}
__________________
Injustice Anywhere is a Threat for Justice Everywhere.Martin Luther King. To Be or Not To Be,Thats the Question! The Only Stupid Question Is the One that Goes Unasked. |
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August 29, 2013, 04:29
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#29 | |
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New Member
Basta
Join Date: Jul 2013
Posts: 28
Rep Power: 12 |
Quote:
Dear Ehsan, I got this error after modifying divScheme: Code:
--> FOAM FATAL IO ERROR:
Unknown convection scheme bounded
Valid convection schemes are :
1
(
Gauss
)
file: /home/fayez/Bureau/ehsan_test/system/fvSchemes::divSchemes::div(phi,U) at line 30.
From function convectionScheme<Type>::New(const fvMesh&, const surfaceScalarField&, Istream&)
in file /home/opencfd/OpenFOAM/OpenFOAM-2.1.1/src/finiteVolume/lnInclude/convectionScheme.C at line 97.
FOAM exiting
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August 29, 2013, 05:06
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#30 |
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Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 26 |
it works fine for me!
Code:
Time = 293 smoothSolver: Solving for Ux, Initial residual = 0.00302422, Final residual = 1.63714e-05, No Iterations 3 smoothSolver: Solving for Uy, Initial residual = 0.00286406, Final residual = 1.40895e-05, No Iterations 3 smoothSolver: Solving for Uz, Initial residual = 0.00163624, Final residual = 9.37947e-06, No Iterations 3 GAMG: Solving for p, Initial residual = 0.00816459, Final residual = 4.26288e-05, No Iterations 2 time step continuity errors : sum local = 4.67106, global = -1.04718, cumulative = -1602.9 smoothSolver: Solving for epsilon, Initial residual = 0.000209883, Final residual = 1.19376e-06, No Iterations 2 bounding epsilon, min: -138.041 max: 2.9235e+08 average: 9.09496e+06 smoothSolver: Solving for k, Initial residual = 0.000215752, Final residual = 8.36107e-07, No Iterations 3 ExecutionTime = 1.22 s ClockTime = 1 s Time = 294 smoothSolver: Solving for Ux, Initial residual = 0.00299998, Final residual = 1.35978e-05, No Iterations 3 smoothSolver: Solving for Uy, Initial residual = 0.00283594, Final residual = 1.3551e-05, No Iterations 3 smoothSolver: Solving for Uz, Initial residual = 0.00161325, Final residual = 8.1245e-06, No Iterations 3 GAMG: Solving for p, Initial residual = 0.00804053, Final residual = 1.87376e-05, No Iterations 2 time step continuity errors : sum local = 2.05042, global = -1.73826, cumulative = -1604.64 smoothSolver: Solving for epsilon, Initial residual = 0.000211165, Final residual = 1.19876e-06, No Iterations 2 smoothSolver: Solving for k, Initial residual = 0.000214596, Final residual = 8.11414e-07, No Iterations 3 ExecutionTime = 1.22 s ClockTime = 1 s Time = 295 smoothSolver: Solving for Ux, Initial residual = 0.00269395, Final residual = 1.35094e-05, No Iterations 3 smoothSolver: Solving for Uy, Initial residual = 0.00268798, Final residual = 1.34244e-05, No Iterations 3 smoothSolver: Solving for Uz, Initial residual = 0.00138372, Final residual = 8.11865e-06, No Iterations 3 GAMG: Solving for p, Initial residual = 0.00734547, Final residual = 2.72228e-05, No Iterations 2 time step continuity errors : sum local = 2.98289, global = -1.95487, cumulative = -1606.59 smoothSolver: Solving for epsilon, Initial residual = 0.000209892, Final residual = 1.16917e-06, No Iterations 2 smoothSolver: Solving for k, Initial residual = 0.000211634, Final residual = 8.11507e-07, No Iterations 3 ExecutionTime = 1.23 s ClockTime = 1 s Time = 296 smoothSolver: Solving for Ux, Initial residual = 0.00260183, Final residual = 1.34072e-05, No Iterations 3 smoothSolver: Solving for Uy, Initial residual = 0.00259837, Final residual = 1.34191e-05, No Iterations 3 smoothSolver: Solving for Uz, Initial residual = 0.00141887, Final residual = 8.04426e-06, No Iterations 3 GAMG: Solving for p, Initial residual = 0.00717931, Final residual = 2.6446e-05, No Iterations 2 time step continuity errors : sum local = 2.89427, global = -1.88796, cumulative = -1608.48 smoothSolver: Solving for epsilon, Initial residual = 0.000205624, Final residual = 1.19057e-06, No Iterations 2 smoothSolver: Solving for k, Initial residual = 0.000209961, Final residual = 7.95193e-07, No Iterations 3 ExecutionTime = 1.23 s ClockTime = 1 s Time = 297 smoothSolver: Solving for Ux, Initial residual = 0.00246914, Final residual = 1.34119e-05, No Iterations 3 smoothSolver: Solving for Uy, Initial residual = 0.00247703, Final residual = 1.31678e-05, No Iterations 3 smoothSolver: Solving for Uz, Initial residual = 0.00133655, Final residual = 8.0358e-06, No Iterations 3 GAMG: Solving for p, Initial residual = 0.00733201, Final residual = 2.25581e-05, No Iterations 2 time step continuity errors : sum local = 2.47292, global = -1.16714, cumulative = -1609.65 smoothSolver: Solving for epsilon, Initial residual = 0.000209202, Final residual = 1.17054e-06, No Iterations 2 bounding epsilon, min: -15.779 max: 2.92343e+08 average: 9.09302e+06 smoothSolver: Solving for k, Initial residual = 0.000209555, Final residual = 8.24086e-07, No Iterations 3 ExecutionTime = 1.24 s ClockTime = 1 s Time = 298 smoothSolver: Solving for Ux, Initial residual = 0.00262038, Final residual = 1.38132e-05, No Iterations 3 smoothSolver: Solving for Uy, Initial residual = 0.00253905, Final residual = 1.35259e-05, No Iterations 3 smoothSolver: Solving for Uz, Initial residual = 0.00141747, Final residual = 8.14806e-06, No Iterations 3 GAMG: Solving for p, Initial residual = 0.00717604, Final residual = 2.40071e-05, No Iterations 2 time step continuity errors : sum local = 2.62906, global = -0.296388, cumulative = -1609.95 smoothSolver: Solving for epsilon, Initial residual = 0.00020553, Final residual = 1.17951e-06, No Iterations 2 smoothSolver: Solving for k, Initial residual = 0.000212137, Final residual = 7.99386e-07, No Iterations 3 ExecutionTime = 1.24 s ClockTime = 1 s Time = 299 smoothSolver: Solving for Ux, Initial residual = 0.00262036, Final residual = 1.34373e-05, No Iterations 3 smoothSolver: Solving for Uy, Initial residual = 0.00243577, Final residual = 1.31502e-05, No Iterations 3 smoothSolver: Solving for Uz, Initial residual = 0.0013605, Final residual = 8.10666e-06, No Iterations 3 GAMG: Solving for p, Initial residual = 0.00723721, Final residual = 1.94311e-05, No Iterations 2 time step continuity errors : sum local = 2.13106, global = 0.691298, cumulative = -1609.26 smoothSolver: Solving for epsilon, Initial residual = 0.000209559, Final residual = 1.17209e-06, No Iterations 2 bounding epsilon, min: -24.6726 max: 2.92349e+08 average: 9.09526e+06 smoothSolver: Solving for k, Initial residual = 0.000210269, Final residual = 8.30651e-07, No Iterations 3 ExecutionTime = 1.24 s ClockTime = 1 s Time = 300 smoothSolver: Solving for Ux, Initial residual = 0.00257644, Final residual = 1.3703e-05, No Iterations 3 smoothSolver: Solving for Uy, Initial residual = 0.0025284, Final residual = 1.34594e-05, No Iterations 3 smoothSolver: Solving for Uz, Initial residual = 0.00143646, Final residual = 8.13869e-06, No Iterations 3 GAMG: Solving for p, Initial residual = 0.00720673, Final residual = 2.29444e-05, No Iterations 2 time step continuity errors : sum local = 2.51267, global = 1.1237, cumulative = -1608.13 smoothSolver: Solving for epsilon, Initial residual = 0.000206882, Final residual = 1.18584e-06, No Iterations 2 smoothSolver: Solving for k, Initial residual = 0.000211105, Final residual = 7.97838e-07, No Iterations 3 ExecutionTime = 1.25 s ClockTime = 1 s End
__________________
Injustice Anywhere is a Threat for Justice Everywhere.Martin Luther King. To Be or Not To Be,Thats the Question! The Only Stupid Question Is the One that Goes Unasked. |
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August 29, 2013, 05:16
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#31 | |
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New Member
Basta
Join Date: Jul 2013
Posts: 28
Rep Power: 12 |
I tried also with your folders (0 , constant, system) but I got the same error
 don't know why Quote:
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August 29, 2013, 05:37
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#32 |
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Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 26 |
you use 2.1.1 vesion? download 2.2.0 or 2.2.1 version so that can run.
__________________
Injustice Anywhere is a Threat for Justice Everywhere.Martin Luther King. To Be or Not To Be,Thats the Question! The Only Stupid Question Is the One that Goes Unasked. |
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August 29, 2013, 19:19
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#33 | |
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New Member
Basta
Join Date: Jul 2013
Posts: 28
Rep Power: 12 |
Quote:
I used OpenFoam 2.2 and finally, I didn't have this error. But after launching Paraview, I realised that my problem didn't been solved. Here are the attachement that i got with elements at the interface between the inlet and wall with high pressure ! |
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August 30, 2013, 04:46
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#34 |
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Senior Member
Ehsan
Join Date: Oct 2012
Location: Iran
Posts: 2,208
Rep Power: 26 |
why youe mesh is so coarse? use a finer mesh and see if changes.
__________________
Injustice Anywhere is a Threat for Justice Everywhere.Martin Luther King. To Be or Not To Be,Thats the Question! The Only Stupid Question Is the One that Goes Unasked. |
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