(demo.txt) RAE 2822 Airfoil

!..The RAE 2822 airfoil is a classic validation case for CFD.  The airfoil 
!..has a chord of 1.0 ft.  Experimental data available for comparison.

!..A grid was generated using ICEM CFD.  It is contained in the file (ga.x) 
!..and is in the Plot3d format (multi-block, 3D, unformatted, whole). It 
!..consists of four zones: two about the airfoil which overlaps two zones 
!..in the farfield.  The wall spacing is 0.0001 ft.  Grid spacing at the 
!..overlapped region is about 0.1 ft.  The zones are: 

 Zone 1:   81 x 61 x 1    Bottom of airfoil + wake (TE at I31, LE at IMAX)
 Zone 2:   81 x 61 x 1    Top of airfoil + wake (LE at I1, TE at I51)
 Zone 3:  125 x 23 x 1    Outer
 Zone 4:   23 x 21 x 1    Wake


!..........................................................................
!..Set up the simulation.  Convert the Plot3d grid file to the common grid 
!..file (raetaf.cgd).

/bin/rm -rf raetaf.cgd
cfcnvt < cfcnvt.x.com

!..Apply boundary conditions.
gman < gman.com


!..........................................................................
!..Running WIND. Use input data file (raetaf.dat).

/bin/rm -rf raetaf.lis
/bin/rm -rf raetaf.tda
/bin/rm -rf raetaf.cfl

wind -runinplace -dat raetaf -mp -parallel

tail -300 raetaf.lis


!..........................................................................
!..Post-Processing

!..Mach number contours.
cfpost < cfpost.mach.com

!..Convergence of Navier-Stokes equations (nsl2.gen).
resplt < resplt.nsl2.com
cfpost < cfpost.nsl2.com

!..Convergence of Spalart-Allmaras turbulence equation (sal2.gen).
resplt < resplt.sal2.com
cfpost < cfpost.sal2.com

!..Convergence of the lift, drag (liftconv.gen).
resplt < resplt.liftconv.com
cfpost < cfpost.liftconv.com

!..Forces on airfoil (forces.lis).
/bin/rm -rf forces.lis
cfpost < cfpost.forces.com
cat forces.lis

!..Cp distributions on airfoil (cp.wind.gen).
cfpost < cfpost.cp.com

!..Examine the boundary layer (blan.gen).
cfpost < cfpost.blan.com