These meshes were created with ANSA v21.1.0

All mesh dimensions (including the ones with the wind tunnel) are in inches
for the full scale aircraft of length 2469 inches.

Unstructured meshes with quad dominant surface mesh, hexa layers and hexa-dominant farfield.

Available mesh formats:

UGRID
CFD++
OpenFOAM
TAU (HDF5)
StarCCM+
CGNS (Mixed HDF5)
Fluent
SU2


101 - Case1a
y+ = 1 wall resolution for the three flap angles
and with wake refinement up to 7 deg AoA
  Level C resolution: mesh size = 217-220 million cells, 172 million nodes

102 - Case1a
Wall function y+ = 100 resolution for the three flap angles
and with wake refinement up to 7 deg AoA
  Level C resolution: mesh size = 102-103 million cells, 68 million nodes

103 - Case2a
y+ = 1 wall resolution for the nominal flap angle
and with wake refinement up to 20 deg AoA
  Level A resolution: mesh size =  91 million cells,  68 million nodes
  Level B resolution: mesh size = 173 million cells, 138 million nodes
  Level C resolution: mesh size = 276 million cells, 218 million nodes
  Level D resolution: mesh size = 389 million cells, 323 million nodes
  Level E resolution: mesh size = 723 million cells, 629 million nodes

104 - Case2a
Wall function y+ = 100 resolution for the nominal flap angle
and with wake refinement up to 20 deg AoA
  Level C resolution: mesh size = 153 million cells, 110 million nodes

105T - Case2b - Currently available in CFD++, UGRID and OpenFOAM only
y+ = 1 wall resolution for the nominal flap angle
with the model inside the wind tunnel
at 7 different AoA positions
  Level C resolution: mesh size = 278 million cells, 226 million nodes
  * Note: check the BCs and reset at tunnel inlet and outlet if appropriate

106T - Case2b - Currently available in CFD++, UGRID and OpenFOAM only
Wall function y+ = 100 resolution for the nominal flap angle
with the model inside the wind tunnel
at 7 different AoA positions
  Level C resolution: mesh size = 168 million cells, 125 million nodes
  * Note: check the BCs and reset at tunnel inlet and outlet if appropriate


Contact person: Vangelis Skaperdas (vangelis@beta-cae.com)

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Disclaimer: The grids available for download may or may not be appropriate for
your solver, and may or may not be of sufficient density and quality to yield
accurate results. You must judge for yourself.