|
[Sponsors] |
Does anyone know how to fix this crash running sonicFoam? |
![]() |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
![]() |
![]() |
#1 |
New Member
Zach
Join Date: Jul 2017
Posts: 11
Rep Power: 9 ![]() |
Code:
Create time Create mesh for time = 0 PIMPLE: no residual control data found. Calculations will employ 2 corrector loops Reading thermophysical properties Selecting thermodynamics package { type hePsiThermo; mixture pureMixture; transport const; thermo hConst; equationOfState perfectGas; specie specie; energy sensibleInternalEnergy; } --> FOAM Warning : From function Foam::Field<Type>::Field(const Foam::word&, const Foam::dictionary&, Foam::label) [with Type = double; Foam::label = int] in file X:/OpenFOAM-4.x/src/OpenFOAM/fields/Fields/Field/Field.T.C at line 317 Reading "C:/Program Files/blueCFD-Core-2016/msys64/home/ofuser/Thesis/forwardStep5/0/T.boundaryField.outlet" from line 31 to line 32 expected keyword 'uniform' or 'nonuniform', assuming deprecated Field format from Foam version 2.0. Reading field U Reading/calculating face flux field phi Creating turbulence model Selecting turbulence model type laminar Creating field kinetic energy K No MRF models present No finite volume options present Starting time loop Time = 2e-009 Courant Number mean: 29918.9 max: 194473 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 PIMPLE: iteration 1 smoothSolver: Solving for Ux, Initial residual = 1, Final residual = 1.04912e-016, No Iterations 1 smoothSolver: Solving for Uy, Initial residual = 1, Final residual = 1.07775e-016, No Iterations 1 smoothSolver: Solving for Uz, Initial residual = 1, Final residual = 1.11858e-016, No Iterations 1 smoothSolver: Solving for e, Initial residual = 1, Final residual = 1.40894e-016, No Iterations 1 smoothSolver: Solving for p, Initial residual = 1, Final residual = 6.84822e-009, No Iterations 2 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 time step continuity errors : sum local = 6.85073e-009, global = 6.85022e-009, cumulative = 6.85022e-009 PIMPLE: iteration 2 smoothSolver: Solving for Ux, Initial residual = 0.906424, Final residual = 1.25287e-017, No Iterations 1 smoothSolver: Solving for Uy, Initial residual = 0.900784, Final residual = 9.54391e-015, No Iterations 1 smoothSolver: Solving for Uz, Initial residual = 0.900489, Final residual = 9.52256e-015, No Iterations 1 smoothSolver: Solving for e, Initial residual = 0.176506, Final residual = 6.6883e-007, No Iterations 2 smoothSolver: Solving for p, Initial residual = 0.000708268, Final residual = 7.50466e-010, No Iterations 1 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 time step continuity errors : sum local = 3.17324e-007, global = -3.17321e-007, cumulative = -3.10471e-007 ExecutionTime = 3.001 s ClockTime = 3 s Time = 4e-009 Courant Number mean: 0.266835 max: 0.770219 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 PIMPLE: iteration 1 smoothSolver: Solving for Ux, Initial residual = 0.00147972, Final residual = 4.73247e-016, No Iterations 1 smoothSolver: Solving for Uy, Initial residual = 0.888003, Final residual = 9.81609e-012, No Iterations 1 smoothSolver: Solving for Uz, Initial residual = 0.86904, Final residual = 9.2104e-012, No Iterations 1 smoothSolver: Solving for e, Initial residual = 0.0150156, Final residual = 1.85648e-015, No Iterations 1 smoothSolver: Solving for p, Initial residual = 0.00175115, Final residual = 1.86295e-009, No Iterations 1 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 time step continuity errors : sum local = 5.22968e-007, global = -5.14875e-007, cumulative = -8.25346e-007 PIMPLE: iteration 2 smoothSolver: Solving for Ux, Initial residual = 0.002629, Final residual = 1.68732e-013, No Iterations 1 smoothSolver: Solving for Uy, Initial residual = 0.243138, Final residual = 2.77223e-011, No Iterations 1 smoothSolver: Solving for Uz, Initial residual = 0.239665, Final residual = 2.71769e-011, No Iterations 1 smoothSolver: Solving for e, Initial residual = 0.00781811, Final residual = 3.38237e-006, No Iterations 1 smoothSolver: Solving for p, Initial residual = 7.52521e-005, Final residual = 2.49087e-010, No Iterations 1 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 time step continuity errors : sum local = 1.07087e-007, global = 1.06681e-007, cumulative = -7.18666e-007 ExecutionTime = 3.016 s ClockTime = 3 s Time = 6e-009 Courant Number mean: 0.0643885 max: 0.370297 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 PIMPLE: iteration 1 smoothSolver: Solving for Ux, Initial residual = 0.00131137, Final residual = 4.37571e-012, No Iterations 1 smoothSolver: Solving for Uy, Initial residual = 0.0714118, Final residual = 1.49425e-007, No Iterations 1 smoothSolver: Solving for Uz, Initial residual = 0.0715601, Final residual = 1.54436e-007, No Iterations 1 smoothSolver: Solving for e, Initial residual = 0.00300799, Final residual = 1.69181e-012, No Iterations 1 --> FOAM FATAL ERROR: Maximum number of iterations exceeded From function Foam::scalar Foam::species::thermo<Thermo, Type>::T(Foam::scalar, Foam::scalar, Foam::scalar, Foam::scalar (Foam::species::thermo<Thermo, Type>::*)(Foam::scalar, Foam::scalar) const, Foam::scalar (Foam::species::thermo<Thermo, Type>::*)(Foam::scalar, Foam::scalar) const, Foam::scalar (Foam::species::thermo<Thermo, Type>::*)(Foam::scalar) const) const [with Thermo = Foam::hConstThermo<Foam::perfectGas<Foam::specie> >; Type = Foam::sensibleInternalEnergy; Foam::scalar = double; Foam::species::thermo<Thermo, Type> = Foam::species::thermo<Foam::hConstThermo<Foam::perfectGas<Foam::specie> >, Foam::sensibleInternalEnergy>] in file X:/OpenFOAM-4.x/src/thermophysicalModels/specie/thermo/thermo/thermoI.H at line 66. FOAM aborting We're sorry, but the application crashed and safe stack tracing isn't available in this current implementation of blueCFD-Core patches for OpenFOAM. This application has requested the Runtime to terminate it in an unusual way. Please contact the application's support team for more information. Last edited by wyldckat; December 31, 2017 at 14:25. Reason: Added [CODE][/CODE] markers |
|
![]() |
![]() |
![]() |
![]() |
#2 |
Retired Super Moderator
Bruno Santos
Join Date: Mar 2009
Location: Lisbon, Portugal
Posts: 10,981
Blog Entries: 45
Rep Power: 129 ![]() ![]() ![]() ![]() ![]() ![]() |
Greetings Thewitness,
I'm late to give an answer to you on this, but still, from what I can figure out, the problem is that the fluid either reached a non-physical temperature or at least a temperature for which there is no available interpolation data. For example, it's common for energy polynomials to only go from 200K to 5000 or 6000K, as you can see here: https://github.com/OpenFOAM/OpenFOAM...Data/therm.dat And given that the very first time step tells you this: Code:
Time = 2e-009 Courant Number mean: 29918.9 max: 194473 If you haven't solved this issue since then, please read this thread: How to give enough info to get help - and follow the instructions given there, so that it's easier to help you with this. Best regards, Bruno
__________________
|
|
![]() |
![]() |
![]() |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
how to run the propeller Tutrial | immortality | OpenFOAM Running, Solving & CFD | 10 | February 22, 2014 10:33 |
Something weird encountered when running OpenFOAM in parallel on multiple nodes | xpqiu | OpenFOAM Running, Solving & CFD | 2 | May 2, 2013 05:59 |
Crash when using sonicFoam | Horus | OpenFOAM | 1 | June 16, 2010 13:57 |
[OpenFOAM] Both paraview and paraFoam crash on Redhat Linux WS v4 64bit | sek | ParaView | 4 | August 17, 2006 17:26 |
star is not running the simulation in windows | Arnab | Siemens | 1 | August 2, 2004 03:40 |