ONERA M6 Wing.  Low Mach, Inviscid Flow.
M_infty=0.3, alpha=0.0 deg.
4 Block. H-grid.  b = 1.0 ft.  c=0.540057 ft.

freestream static 0.3 14.7 460.0 0.0 0.0
turbulence model inviscid 

implicit boundary on

downstream pressure freestream zone 1
downstream pressure freestream zone 4

/...Reduce grid size by factor of 4.
/sequence 2 2 2 all
/...Reduce grid size by factor of 2.
/sequence 1 1 1 all

loads
   zone 3
   print totals zones lift frequency 10
   reference area 1.0
   reference length 1.0
   reference moment center 0.0 0.0 0.0
   subset i 1 last j 1 1 k 1 last force noslip
endloads

cycles 1500
iterations per cycle 5
cfl# 2.0
converge order 5

end