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

settlingFoam crash when velocity increase

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   February 8, 2014, 06:42
Default settlingFoam crash when velocity increase
  #1
New Member
 
Zhengbing
Join Date: Apr 2013
Posts: 20
Rep Power: 13
jimbean is on a distinguished road
Dear Foamers,

I have built a case with settlingFoam in open channel and succeeded to implement settlingFoam with upstream velocity U=0.01m/s. But when I increase velocity to 0.1m/s and then decrease deltaT to 1/10 of original value with other parameters unchanged, settlingFoam crash only in a few steps.

I have checked the mesh and other parameters, they all seem ok. And the successful run with velocity U=0.01m/s also verify the correctness of the model.

So where is the problem?

Please help check it
https://www.dropbox.com/s/avyqgvppc5...ingFoamTry.rar

Thank you so much!

The error are:
[4] --> FOAM FATAL IO ERROR:
[4] wrong token type - expected Scalar, found on line 6 the word 'nan'
[4]
[4] file: /work/jchb_work/tryCase3/processor4/system/data.solverPerformance.p_rgh at line 6.
[4]
[4] From function operator>>(Istream&, Scalar&)
[4] in file lnInclude/Scalar.C at line 91.
[4]
FOAM parallel run exiting


and

the last few outputs before crash
Courant Number mean: 157.258 max: 2.78008e+09
Time = 0.0035

diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
DILUPBiCG: Solving for Ux, Initial residual = 0.961496, Final residual = 21.6592, No Iterations 1001
DILUPBiCG: Solving for Uy, Initial residual = 0.479107, Final residual = 66.819, No Iterations 1001
DILUPBiCG: Solving for Uz, Initial residual = 0.989586, Final residual = 1181.08, No Iterations 1001
DILUPBiCG: Solving for Alpha, Initial residual = 7.05917e-29, Final residual = 7.05917e-29, No Iterations 0
Solid phase fraction = 7.59423e-09 Min(Alpha) = 0 Max(Alpha) = 0.0001
DICPCG: Solving for p_rgh, Initial residual = 1, Final residual = 0.00937167, No Iterations 285
diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = 1.56205e+10, global = 3.54897e+09, cumulative = 1.88911e+10
DICPCG: Solving for p_rgh, Initial residual = 1, Final residual = 1161.01, No Iterations 1001
diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = -1.76542e+77, global = 1.14126e+79, cumulative = 1.14126e+79
DILUPBiCG: Solving for epsilon, Initial residual = 1.04384e-16, Final residual = 1.04384e-16, No Iterations 0
DILUPBiCG: Solving for k, Initial residual = 3.74426e-10, Final residual = 3.74426e-10, No Iterations 0
ExecutionTime = 31.49 s ClockTime = 31 s

Courant Number mean: 9.93646e+06 max: 2.91565e+14
Time = 0.004

diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
DILUPBiCG: Solving for Ux, Initial residual = 0.385816, Final residual = 3.31484e-08, No Iterations 152
DILUPBiCG: Solving for Uy, Initial residual = 0.586937, Final residual = 7.98723e-08, No Iterations 48
DILUPBiCG: Solving for Uz, Initial residual = 0.426142, Final residual = 9.93456e-08, No Iterations 30
DILUPBiCG: Solving for Alpha, Initial residual = 0.00565905, Final residual = 6.1556e-08, No Iterations 15
Solid phase fraction = 7.75057e-09 Min(Alpha) = -3.91074e-07 Max(Alpha) = 0.0001
DICPCG: Solving for p_rgh, Initial residual = 1, Final residual = 3324.1, No Iterations 1001
diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = 5.58815e+73, global = 5.56881e+73, cumulative = 1.14127e+79
DICPCG: Solving for p_rgh, Initial residual = 1, Final residual = nan, No Iterations 1001
diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = nan, global = nan, cumulative = nan
DILUPBiCG: Solving for epsilon, Initial residual = nan, Final residual = nan, No Iterations 1001
DILUPBiCG: Solving for k, Initial residual = nan, Final residual = nan, No Iterations 1001
ExecutionTime = 47.43 s ClockTime = 47 s

Courant Number mean: nan max: nan
Time = 0.0045

diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
DILUPBiCG: Solving for Ux, Initial residual = nan, Final residual = nan, No Iterations 1001
DILUPBiCG: Solving for Uy, Initial residual = nan, Final residual = nan, No Iterations 1001
DILUPBiCG: Solving for Uz, Initial residual = nan, Final residual = nan, No Iterations 1001
DILUPBiCG: Solving for Alpha, Initial residual = nan, Final residual = nan, No Iterations 1001
Solid phase fraction = nan Min(Alpha) = nan Max(Alpha) = nan
DICPCG: Solving for p_rgh, Initial residual = nan, Final residual = nan, No Iterations 1001
diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = nan, global = nan, cumulative = nan
DICPCG: Solving for p_rgh, Initial residual = nan, Final residual = nan, No Iterations 1001
jimbean is offline   Reply With Quote

Old   March 26, 2014, 03:59
Default
  #2
Member
 
Jeremy Dudley
Join Date: Jul 2010
Posts: 45
Rep Power: 15
bendel_boy is on a distinguished road
I'e tried using the 'adaptive timestep. control, which times the timestep down to c. 1E-27 to control the Courant number. I've tried changing the outlet boundary. No success.

Your grid has some small cells around the middle - is this trying to represent settling around a heat exchanger bundle?

I think you may have to try and change the integration method from explicit to implicit. I haven't tried that.
bendel_boy 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
UDF error - parabolic velocity profile - 3D turbine Zaqie Fluent UDF and Scheme Programming 9 June 25, 2016 19:08
LES and TKE calculations MST Main CFD Forum 3 May 30, 2016 06:26
Radial velocity and tangential velocity on centrifugal fan, johnnyp FLUENT 2 May 24, 2013 07:10
reactingFoam , FOAM Warning : Increase time precision and then crash camille131 OpenFOAM Running, Solving & CFD 7 March 26, 2013 13:50
Terrible Mistake In Fluid Dynamics History Abhi Main CFD Forum 12 July 8, 2002 09:11


All times are GMT -4. The time now is 06:29.