discontinuous region over Vorticity contour
3 Attachment(s)
Hi, all
I've studyed 3d Wing recently but I can't deal with some region where quantities show discontinuity especially Vorticity magnitude. The reason I think is fine grid spacing without reasonable stretching ratio or asepct ratio. But I want mesh refinement near wingtip, and can't change blocking strategy. here are details of simulation. grid generation : Icem CFD multiblock hexa solver : fluent Re=1.2e6 k-omega SST node based, 2nd order, steady, AoA=8deg Thanks in advance. |
All times are GMT -4. The time now is 20:22. |