DLR-F6 + Wing Body + FX2B Fairing
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1. Volume grid suitable for cell centered solvers using wall functions, produced using NASA's TetrUSS / Vgrid software.

2. Grid parameters.

   Type of Grid                      = Coarse
   No. of surface points             = 29832
   No. of surface triangles          = 59660
   No. of field points               = 544326
   No. of tetrahedral cells          = 3142285
   No. of layers of boundary cells   = 8
   Height of first boundary cell     = 0.03868 mm ( Y+ = 50)

3. Grid developed by

Dr. Chittur (Venkat) Venkatasubban
Principal Engineer, Advanced Design
Raytheon Aircraft Company
9709 E. Central, MS B-12/916
Wichita, Kansas - 67209, USA

Tel: (316) 676 1286
e-mail: chittur_venkatasubban@rac.ray.com


