ONERA M6 Wing. Transonic Turbulent Flow.
M_infty=0.84, alpha=3.06 deg.  Rec=11.72E+06.
4 Block. H-grid.  b = 1.0 ft.  c=0.540057 ft.

freestream static 0.8395 45.82899 460.0 3.06 0.0

turbulence model spalart allmaras
wall function on 

implicit boundary on
dq limiter on

downstream pressure freestream zone 1
downstream pressure freestream zone 4

loads
   print totals zones lift frequency 20
   reference area 1.0
   reference length 1.0
   reference moment center 0.0 0.0 0.0
   zone 2
   subset i 1 last j 1 1 k 1 last force noslip
   zone 3
   subset i 1 last j 1 1 k 1 last force noslip
endloads

cycles 1000
iterations per cycle 5 print frequency 5
cfl 2.5
converge order 9 

end