About boundary conditions in k-omega-SST model
I'm running simpleFoam in OpenFOAM using k-omega-SST model on calculating flow around airfoil. But the solution blow up after several hundreds of iterations. Would any help me with that?
Here are the flow conditions: U=139.4m/s p=72319.7 Pa Re=10e6 airfoil cord=1 m computational domain length 40 m Timestep=10e-6; should it be smaller or larger? y+=1; Here are the Boundary Conditions: P boundary condition: internalField uniform 72319.7; AIRFOIL1 { type zeroGradient; } INLET { type fixedValue; value uniform 72319.7; } OUTLET { type zeroGradient; } UPPERWALL { type zeroGradient; } LOWERWALL { type zeroGradient; } U boundary condition: internalField uniform (139.4 0 0); AIRFOIL1 { type fixedValue; value uniform (0 0 0); } INLET { type fixedValue; value (139.4 0 0); } OUTLET { type zeroGradient; } UPPERWALL { type zeroGradient; } LOWERWALL { type zeroGradient; } k boundary condition internalField uniform 2.8982; { AIRFOIL1 { type kqRWallFunction; value uniform 0; } frontPlate { type symmetryPlane; } top { type symmetryPlane; } INLET { type fixedValue; value uniform 2.8982; } OUTLET { type zeroGradient; } UPPERWALL { type kqRWallFunction; value uniform 0; } LOWERWALL { type kqRWallFunction; value uniform 0; } omega boundary condition internalField uniform 697; boundaryField { AIRFOIL1 { type omegaWallFunction; value uniform 0; } INLET { type fixedValue; value uniform 697; } OUTLET { type zeroGradient; } UPPERWALL { type zeroGradient; } LOWERWALL { type zeroGradient; } |
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