|
[Sponsors] |
[rhoCentralFoam] simulating compressible inviscid flow |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
September 5, 2014, 11:24 |
[rhoCentralFoam] simulating compressible inviscid flow
|
#1 |
New Member
Yuval
Join Date: Jul 2014
Location: Munich, Germany
Posts: 3
Rep Power: 12 |
Hi,
I'm trying to simulate a compressible inviscid flow through a de-laval nozzle into vacuum. Later I will want to add viscosity to the simulation but for now I want to get inviscid results. For that purpose I tried setting the thermophysicalProperties dictionary with a janaf model to have Cp changed with temperature and since janaf model has to to go with sutherland's model for transport, and since I want an invscid flow, I set As=Ts=0 to have zero viscosity. Here is my file: Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2.3.0 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; location "constant"; object thermophysicalProperties; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // thermoType { type hePsiThermo; mixture pureMixture; transport sutherland; /*const;*/ thermo janaf; /*hConst;*/ equationOfState perfectGas; specie specie; energy sensibleInternalEnergy; } mixture //H2O { specie { nMoles 1; molWeight 18.0153; } thermodynamics //from http://www2.galcit.caltech.edu/EDL/public/thermo/nasadat { Tlow 200; Thigh 6000; Tcommon 1000; highCpCoeffs (2.67703787 2.97318329E-03 -7.73769690E-07 9.44336689E-11 -4.26900959E-15 -2.98858938E+04 6.88255571); lowCpCoeffs (4.19864056 -2.03643410E-03 6.52040211E-06 -5.48797062E-09 1.77197817E-12 -3.02937267E+04 -8.49032208E-01); //Cp 2609; // for T=1500K from http://www.engineeringtoolbox.com/water-vapor-d_979.html //Hf 0; //3.34e5; } transport //from http://labspace.open.ac.uk/file.php/6999/t236_1_b2_unit03.pdf pg. 14 (constants applicable for temprature range 0-523 K { As 0; //1.383e-06; Ts 0; //405.5; //mu 0; //Pr 1; } } // ************************************************************************* // But the simulation crashes after sometime with the following error: Code:
Mean and max Courant Numbers = 714.712961755555 7526243.04395094 deltaT = 1.29974885066034e-150 --> FOAM Warning : From function Time::operator++() in file db/Time/Time.C at line 1055 Increased the timePrecision from 1883 to 1884 to distinguish between timeNames at time 0.0409300097404806 Time = 0.040930009740480610691548690738272853195667266845703125 [1] #0 Foam::error::printStack(Foam::Ostream&)[0] #0 Foam::error::printStack(Foam::Ostream&) in "/opt/openfoam230/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" [0] #1 Foam::sigFpe::sigHandler(int) in "/opt/openfoam230/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" [0] #2 in "/opt/openfoam230/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" [1] #1 Foam::sigFpe::sigHandler(int) in "/lib/x86_64-linux-gnu/libc.so.6" [0] #3 Foam::multiply(Foam::Field<double>&, Foam::UList<double> const&, Foam::UList<double> const&) in "/opt/openfoam230/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" [1] #2 in "/opt/openfoam230/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" [0] #4 in "/lib/x86_64-linux-gnu/libc.so.6" [1] #3 Foam::multiply(Foam::Field<double>&, Foam::UList<double> const&, Foam::UList<double> const&)void Foam::multiply<Foam::fvsPatchField, Foam::surfaceMesh>(Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh>&, Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh> const&, Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh> const&) in "/opt/openfoam230/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" [1] #4 in "/opt/openfoam230/platforms/linux64GccDPOpt/bin/rhoCentralFoam" [0] #5 void Foam::multiply<Foam::fvsPatchField, Foam::surfaceMesh>(Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh>&, Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh> const&, Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh> const&)[0] at rhoCentralFoam.C:0 [0] #6 in "/opt/openfoam230/platforms/linux64GccDPOpt/bin/rhoCentralFoam" [1] #5 [0] in "/opt/openfoam230/platforms/linux64GccDPOpt/bin/rhoCentralFoam" [0] #7 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6" [0] #8 [1] at rhoCentralFoam.C:0 [1] #6 [0] in "/opt/openfoam230/platforms/linux64GccDPOpt/bin/rhoCentralFoam" [LRT:20892] *** Process received signal *** [LRT:20892] Signal: Floating point exception (8) [LRT:20892] Signal code: (-6) [LRT:20892] Failing at address: 0x3e80000519c [LRT:20892] [ 0] /lib/x86_64-linux-gnu/libc.so.6(+0x36150) [0x7f637fa55150] [LRT:20892] [ 1] /lib/x86_64-linux-gnu/libc.so.6(gsignal+0x35) [0x7f637fa550d5] [LRT:20892] [ 2] /lib/x86_64-linux-gnu/libc.so.6(+0x36150) [0x7f637fa55150] [LRT:20892] [ 3] /opt/openfoam230/platforms/linux64GccDPOpt/lib/libOpenFOAM.so(_ZN4Foam8multiplyERNS_5FieldIdEERKNS_5UListIdEES6_+0xe6) [0x7f6380ce92a6] [LRT:20892] [ 4] rhoCentralFoam(_ZN4Foam8multiplyINS_13fvsPatchFieldENS_11surfaceMeshEEEvRNS_14GeometricFieldIdT_T0_EERKS6_S9_+0x3e) [0x44b4ae] [LRT:20892] [ 5] rhoCentralFoam() [0x432b8f] [LRT:20892] [ 6] rhoCentralFoam() [0x42406c] [LRT:20892] [ 7] /lib/x86_64-linux-gnu/libc.so.6(__libc_start_main+0xed) [0x7f637fa4076d] [LRT:20892] [ 8] rhoCentralFoam() [0x42ba3d] [LRT:20892] *** End of error message *** [1] in "/opt/openfoam230/platforms/linux64GccDPOpt/bin/rhoCentralFoam" [1] #7 __libc_start_main-------------------------------------------------------------------------- mpirun noticed that process rank 0 with PID 20892 on node LRT exited on signal 8 (Floating point exception). -------------------------------------------------------------------------- Killing PID 20885 Getting LinuxMem: [Errno 2] No such file or directory: '/proc/20885/status' I'm a bit confused. My turbulenceProperties is obviously also set to laminar. Could someone please help me? Thanks a lot in advance! Yuval. P.S. If more information is needed pls let me know... |
|
January 27, 2016, 16:46 |
|
#2 | |
New Member
Mr.liu
Join Date: Sep 2012
Posts: 27
Rep Power: 14 |
Quote:
|
||
January 27, 2016, 22:33 |
|
#3 |
Member
Peter
Join Date: Feb 2015
Location: New York
Posts: 73
Rep Power: 11 |
Hi,
There is a pretty simple answer to this, and as with most issues in OpenFOAM, just having a quick look at the source code will usually resolve things. So, if you want inviscid, you need to have mu set less than or equal to 0. From createFields.H in the rhoCentralFoam solver directory: Code:
bool inviscid(true); if (max(mu.internalField()) > 0.0) { inviscid = false; } Peter |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
compressible flow | maria teresa | FLUENT | 1 | September 7, 2007 17:58 |
Convergence for inviscid flow over sylinder | Rjakk | Main CFD Forum | 2 | March 21, 2007 11:53 |
compressible flow computation | amv | Main CFD Forum | 5 | June 27, 2003 08:27 |
Boundary Layer created by Euler Solvers | Jim | Main CFD Forum | 31 | November 18, 2001 00:18 |
compressible channel flow.. | R.D.Prabhu | Main CFD Forum | 0 | July 17, 1998 18:23 |