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August 22, 2013, 11:22 |
RAMjet diffuser flow
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#1 |
New Member
Devayan Bir
Join Date: Jul 2013
Posts: 15
Rep Power: 12 |
Hi,
New to CFD trying to simulate flow in a ramjet diffuser with Openfoam my geometry Attachment 24734 Attachment 24735 Attachment 24736 Attachment 24737 Using rhoCentralFoam solver it keeps saying maxIter ireached limit specieThermo Using sonicFoam now simulation is running but rho=0 (isnt sonicFoam compressible solver) also used setFields to set non uniform boundary conditions defaultFieldValues ( volScalarFieldValue p 85592 volScalarFieldValue epsilon 35008 volScalarFieldValue k 74 volVectorFieldValue U (703.2 0 0) volScalarFieldValue T 279.06 ); regions ( cylinderAnnulusToCell { p1 ( 0.525985 0 0 ) ; p2 ( 1.54485 0 0 ); outerRadius 0.140 ; innerRadius 0.105 ; fieldValues ( volScalarFieldValue p 409540 volScalarFieldValue epsilon 35008 volScalarFieldValue k 74 volVectorFieldValue U (250 0 0) volScalarFieldValue T 494 Plz advice |
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August 22, 2013, 12:00 |
body
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#2 |
New Member
Devayan Bir
Join Date: Jul 2013
Posts: 15
Rep Power: 12 |
body.jpg
body geometry used setFields to create a normal shock in th region of the cowl where it becomes straight as non uniform conditions to subsonic.Boundary Top is the semi cylindrical shell covering the region from inlet to cowl. |
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August 23, 2013, 00:49 |
sonicFoam error
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#3 |
New Member
Devayan Bir
Join Date: Jul 2013
Posts: 15
Rep Power: 12 |
getting an error using sonicFoam solver
Time = 0.0237024 Courant Number mean: 0.0151219 max: 14.2721 diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0 DILUPBiCG: Solving for Ux, Initial residual = 0.000870388, Final residual = 1.50063e-06, No Iterations 1 DILUPBiCG: Solving for Uy, Initial residual = 0.00374136, Final residual = 1.09437e-09, No Iterations 2 DILUPBiCG: Solving for Uz, Initial residual = 0.00147596, Final residual = 1.95045e-06, No Iterations 1 DILUPBiCG: Solving for e, Initial residual = 0.000371632, Final residual = 3.91739e-06, No Iterations 1 --> FOAM FATAL ERROR: Maximum number of iterations exceeded From function specieThermo<Thermo>::T(scalar f, scalar T0, scalar (specieThermo<Thermo>::*F)(const scalar) const, scalar (specieThermo<Thermo>::*dFdT)(const scalar) const) const in file /home/bir/OpenFOAM/OpenFOAM-2.1.1/src/thermophysicalModels/specie/lnInclude/specieThermoI.H at line 69. FOAM aborting #0 Foam::error:rintStack(Foam::Ostream&) in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" #1 Foam::error::abort() in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" #2 Foam::specieThermo<Foam::eConstThermo<Foam:erfec tGas> >::T(double, double, double (Foam::specieThermo<Foam::eConstThermo<Foam:erfe ctGas> >::*)(double) const, double (Foam::specieThermo<Foam::eConstThermo<Foam:erfe ctGas> >::*)(double) const, double (Foam::specieThermo<Foam::eConstThermo<Foam:erfe ctGas> >::*)(double) const) const in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libbasicThermophysicalModels.so" #3 Foam::ePsiThermo<Foam:ureMixture<Foam::constTran sport<Foam::specieThermo<Foam::eConstThermo<Foam:: perfectGas> > > > >::calculate() in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libbasicThermophysicalModels.so" #4 Foam::ePsiThermo<Foam:ureMixture<Foam::constTran sport<Foam::specieThermo<Foam::eConstThermo<Foam:: perfectGas> > > > >::correct() in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libbasicThermophysicalModels.so" #5 in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/bin/sonicFoam" #6 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6" #7 in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/bin/sonicFoam" Aborted (core dumped) plz advice |
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November 19, 2013, 11:33 |
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#4 |
New Member
Rahul Soni
Join Date: Feb 2013
Location: IIT Kanpur
Posts: 13
Rep Power: 13 |
Hi Devayan,
Is your problem solved. --> FOAM FATAL ERROR: Maximum number of iterations exceeded From function specieThermo<Thermo>::T(scalar f, scalar T0, scalar (specieThermo<Thermo>::*F)(const scalar) const, scalar (specieThermo<Thermo>::*dFdT)(const scalar) const) const in file /home/bir/OpenFOAM/OpenFOAM-2.1.1/src/thermophysicalModels/specie/lnInclude/specieThermoI.H at line 69. FOAM aborting #0 Foam::error:rintStack(Foam::Ostream&) in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" #1 Foam::error::abort() in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libOpenFOAM.so" #2 Foam::specieThermo<Foam::eConstThermo<Foam:erfec tGas> >::T(double, double, double (Foam::specieThermo<Foam::eConstThermo<Foam:erfe ctGas> >::*)(double) const, double (Foam::specieThermo<Foam::eConstThermo<Foam:erfe ctGas> >::*)(double) const, double (Foam::specieThermo<Foam::eConstThermo<Foam:erfe ctGas> >::*)(double) const) const in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libbasicThermophysicalModels.so" #3 Foam::ePsiThermo<Foam:ureMixture<Foam::constTran sport<Foam::specieThermo<Foam::eConstThermo<Foam:: perfectGas> > > > >::calculate() in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libbasicThermophysicalModels.so" #4 Foam::ePsiThermo<Foam:ureMixture<Foam::constTran sport<Foam::specieThermo<Foam::eConstThermo<Foam:: perfectGas> > > > >::correct() in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/lib/libbasicThermophysicalModels.so" #5 in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/bin/sonicFoam" #6 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6" #7 in "/home/bir/OpenFOAM/OpenFOAM-2.1.1/platforms/linux64GccDPOpt/bin/sonicFoam" Aborted (core dumped) |
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November 22, 2013, 01:45 |
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#5 |
New Member
Devayan Bir
Join Date: Jul 2013
Posts: 15
Rep Power: 12 |
ya was able to sove it
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November 22, 2013, 02:46 |
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#6 |
New Member
Rahul Soni
Join Date: Feb 2013
Location: IIT Kanpur
Posts: 13
Rep Power: 13 |
Hi Devayan,
Many thankx for you reply, can you offer me some suggestion how to eliminate this issue. Looking forward to your reply. Regards, Rahul |
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November 24, 2013, 02:37 |
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#7 |
New Member
Devayan Bir
Join Date: Jul 2013
Posts: 15
Rep Power: 12 |
I am a newbie at CFD. This issue I solved by using different boundary condition which is very problem specific. Please elaborate your issue maybe the problem lies there.
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