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#1 |
New Member
Mingi Park
Join Date: Jan 2016
Posts: 1
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$ sonicFoam
/*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2.3.x | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ /* Windows port by CFD support (www.cfdsupport.com) [based on Symscape] *\ \*---------------------------------------------------------------------------*/ Build : 2.3.x-819030ed51bd Exec : C:\OpenFOAM\cygwin64\opt\OpenFOAM\OpenFOAM-2.3.x\platforms\cygwin64mingw-w64DPOpt\bin\sonicFoam.exe Date : Jan 19 2016 Time : 07:54:39 Host : "MSDN-SPECIAL" PID : 6776 Case : C:/OpenFOAM/cygwin64/home/Administrator/OpenFOAM_cases/case-compressible-sonic nProcs : 1 fileModificationChecking : Monitoring run-time modified files using timeStampMaster allowSystemOperations : Disallowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create mesh for time = 0 Reading thermophysical properties Selecting thermodynamics package { type hePsiThermo; mixture pureMixture; transport const; thermo hConst; equationOfState perfectGas; specie specie; energy sensibleInternalEnergy; } Reading field U Reading/calculating face flux field phi Creating turbulence model Selecting turbulence model type laminar Creating field kinetic energy K No finite volume options present PIMPLE: no residual control data found. Calculations will employ 2 corrector loops Starting time loop Time = 0.001 Courant Number mean: 0 max: 0 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 = 1.65843e-017, No Iterations 1 smoothSolver: Solving for Uy, Initial residual = 1, Final residual = 1.36774e-017, No Iterations 1 smoothSolver: Solving for Uz, Initial residual = 1, Final residual = 1.70257e-017, No Iterations 1 smoothSolver: Solving for e, Initial residual = 0.000411005, Final residual = 2.93986e-006, No Iterations 1 smoothSolver: Solving for p, Initial residual = 1, Final residual = 0.00273701, No Iterations 1000 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 time step continuity errors : sum local = 0.069875, global = 0.069875, cumulative = 0.069875 PIMPLE: iteration 2 smoothSolver: Solving for Ux, Initial residual = 0.993202, Final residual = 7.8103e-006, No Iterations 36 smoothSolver: Solving for Uy, Initial residual = 0.965719, Final residual = 8.64959e-006, No Iterations 40 smoothSolver: Solving for Uz, Initial residual = 0.993176, Final residual = 9.24674e-006, No Iterations 37 smoothSolver: Solving for e, Initial residual = 1, Final residual = nan, No Iterations 1000 smoothSolver: Solving for p, Initial residual = nan, Final residual = nan, No Iterations 1000 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 time step continuity errors : sum local = nan, global = nan, cumulative = nan ExecutionTime = 97.533 s ClockTime = 98 s Time = 0.002 Courant Number mean: nan max: nan diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 PIMPLE: iteration 1 smoothSolver: Solving for Ux, Initial residual = nan, Final residual = nan, No Iterations 1000 smoothSolver: Solving for Uy, Initial residual = nan, Final residual = nan, No Iterations 1000 smoothSolver: Solving for Uz, Initial residual = nan, Final residual = nan, No Iterations 1000 smoothSolver: Solving for e, Initial residual = nan, Final residual = nan, No Iterations 1000 smoothSolver: Solving for p, Initial residual = nan, Final residual = nan, No Iterations 1000 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 time step continuity errors : sum local = nan, global = nan, cumulative = nan PIMPLE: iteration 2 smoothSolver: Solving for Ux, Initial residual = nan, Final residual = nan, No Iterations 1000 smoothSolver: Solving for Uy, Initial residual = nan, Final residual = nan, No Iterations 1000 smoothSolver: Solving for Uz, Initial residual = nan, Final residual = nan, No Iterations 1000 --> FOAM FATAL IO ERROR: wrong token type - expected Scalar, found on line 0 the word 'nan' file: C:/OpenFOAM/cygwin64/home/Administrator/OpenFOAM_cases/case-compressible-sonic/system/data.solverPerformance.U at line 0. From function operator>>(Istream&, Scalar&) in file lnInclude/Scalar.C at line 93. FOAM exiting i'm running a simulation of a rocket nozzle using openFoam since the Fluent license expired. I'm very new to openFoam, so i have almost no idea why this error happens. The simulation was based on sonicFoam laminar tutorial. Here's the case file: https://www.dropbox.com/s/lzgbwv7yce...sonic.zip?dl=0 |
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#2 |
New Member
Teja
Join Date: Jul 2016
Posts: 6
Rep Power: 10 ![]() |
Hi,
Is your problem solved? I got a similar error in my code. If your problem is solved, could you please help me. Thank you |
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