Using
the Anisotropic
hybrid meshing technique, we have been able to go from CAD file to viscous
mesh (5 Million
Cells)
in under
three hours. The example shown,
the DLR-F6 wing, fuselage, pylon, nacelle case from the AIAA’s Drag
Prediction Workshop, has anisotropic, highly-clustered cells
(wall spacing 0.0006)
near
the body of the vehicle that smoothly
expand to isotropic tetrahedra in the far field.