OpenFOAM-4.x/tutorials/compressible/sonicFoam/ras/nacaAirfoil/Running_Notes
2014-12-10 22:40:10 +00:00

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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 corrected 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