HiLiftPW-2 grids for group 014 (KTH/BCAM)

NB:

We use a goal-oriented (targeted toward cd and cl) adaptive mesh
refinement method and solver. Therefore we have used the same
configuration (Config 4 (including Slat Tracks and Flap Track
Fairings)) for both the grid convergence in case1 and the full results
in case2b, i.e. the adaptive mesh refinement method generates a
sequence of successively finer meshes and corresponding solutions,
where we use the finest mesh for case2b.

_Contact information_

Name: Johan Jansson
Email: jjan@kth.se

_Grid information_

We have used the grid "aoa12_mesh.tec" for aoa=12 and the grid
"aoa22.4_mesh.tec" for aoa=20, 21, 22.4. These are the finest grids
generated in the adaptive mesh refinement iterative sequence.

aoa12_mesh.tec, unstructured tetrahedral mesh
Number of vertices: 4274122
Format: Tecplot, generated by VisIt 2.5.2

aoa22.4_mesh.tec, unstructured tetrahedral mesh
Number of vertices: 3006757
Format: Tecplot, generated by VisIt 2.5.2