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foam-extend4.1-coherent-io/tutorials/compressible/sonicFoam/ras/nacaAirfoil/Running_Notes

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2010-10-01 09:29:30 +00:00
nacaAirfoil
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* large domain with airfoil section near centre
* extremely non-orthogonal, highly skew mesh refined around the airfoil
* running at Mach 1.78
* limited 0.5 on all laplacianSchemes because the mesh is so poor
* run to t = 0.02 with nextWrite; change to stopAt endTime to continue running
* deltaT can be increased later in the run to 2e-07