tutorials/heatTransfer/chtMultiRegionFoam/reverseBurner: Changed to perfectGas
Only perfectGas and real-gas equations of state are consistent with standard Janaf thermo data based on Cp. Using other equations of state is possible but the Janaf Cp data would have to be modified for consistency.
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@ -17,7 +17,7 @@ FoamFile
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dimensions [ 1 -1 -2 0 0 0 0 ];
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internalField uniform 0;
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internalField uniform 1e6;
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boundaryField
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{
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@ -17,7 +17,7 @@ FoamFile
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dimensions [ 1 -1 -2 0 0 0 0 ];
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internalField uniform 0;
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internalField uniform 1e6;
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boundaryField
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{
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@ -17,7 +17,7 @@ FoamFile
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dimensions [ 1 -1 -2 0 0 0 0 ];
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internalField uniform 0;
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internalField uniform 1e6;
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boundaryField
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{
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@ -29,7 +29,7 @@ options
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sources
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{
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e
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h
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{
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explicit 5e7; // kg/m/s^3
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implicit 0;
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@ -22,9 +22,7 @@ O2
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molWeight 31.9988;
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}
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equationOfState
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{
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pRef 1e6;
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}
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{}
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thermodynamics
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{
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Tlow 200;
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@ -47,9 +45,7 @@ H2O
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molWeight 18.0153;
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}
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equationOfState
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{
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pRef 1e6;
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}
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{}
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thermodynamics
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{
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Tlow 200;
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@ -72,9 +68,7 @@ CH4
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molWeight 16.0428;
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}
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equationOfState
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{
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pRef 1e6;
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}
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{}
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thermodynamics
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{
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Tlow 200;
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@ -97,9 +91,7 @@ CO2
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molWeight 44.01;
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}
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equationOfState
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{
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pRef 1e6;
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}
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{}
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thermodynamics
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{
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Tlow 200;
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@ -122,9 +114,7 @@ N2
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molWeight 28.0134;
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}
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equationOfState
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{
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pRef 1e6;
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}
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{}
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thermodynamics
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{
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Tlow 200;
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@ -21,9 +21,9 @@ thermoType
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mixture multiComponentMixture;
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transport sutherland;
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thermo janaf;
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equationOfState incompressiblePerfectGas;
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equationOfState perfectGas;
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specie specie;
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energy sensibleInternalEnergy;
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energy sensibleEnthalpy;
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}
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inertSpecie N2;
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@ -30,7 +30,7 @@ divSchemes
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default none;
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div(phi,U) Gauss linearUpwind grad(U);
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div(phi,e) Gauss linearUpwind limitedGrad;
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div(phi,h) Gauss linearUpwind limitedGrad;
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div(phi,Yi_h) Gauss limitedLinear 1;
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div(phi,k) Gauss linearUpwind limitedGrad;
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div(phi,epsilon) Gauss linearUpwind limitedGrad;
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@ -36,7 +36,7 @@ solvers
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relTol 0;
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}
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"(U|e|k|epsilon|Yi)"
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"(U|h|k|epsilon|Yi)"
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{
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solver PBiCGStab;
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preconditioner DILU;
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@ -44,7 +44,7 @@ solvers
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relTol 0.1;
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}
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"(U|e|k|epsilon|Yi)Final"
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"(U|h|k|epsilon|Yi)Final"
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{
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$U;
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tolerance 1e-7;
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