TALK=T;RUN( 1, 1)
 
 ************************************************************
   Q1 created by VDI menu, Version 2011, Date 23/03/11
 CPVNAM=VDI;SPPNAM=Core
 ************************************************************
  Echo DISPLAY / USE settings
  DISPLAY
 
  Library case Y115:
 
  
  FLOW OVER AN AIRFOIL: FGEM and PARSOL
 
  ENDDIS
 ************************************************************
 IRUNN = 1 ;LIBREF = 115
 ************************************************************
  Group 1. Run Title
 TEXT(Flow over an airfoil: Y115              )
 ************************************************************
  Group 2. Transience
 STEADY = T
 ************************************************************
  Groups 3, 4, 5  Grid Information
    * Overall number of cells, RSET(M,NX,NY,NZ,tolerance)
 RSET(M,30,20,1)
 ************************************************************
  Group 6. Body-Fitted coordinates
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
    * Solved variables list
 SOLVE(P1,U1,V1)
    * Additional solver options
 SOLUTN(P1,Y,Y,Y,N,N,Y)
 
 ************************************************************
  Group 8. Terms & Devices
 ************************************************************
  Group 9. Properties
 PRESS0 =1.0E+05 ;TEMP0 =273.
    * Domain material index is   0 signifying:
    * Air at 20 deg C, 1 atm, treated as incompressible
 SETPRPS(1, 0)
 ENUL =1.0E-03
 ENUT =0.
 DRH1DP =1.0E-05
 DVO1DT =3.41E-03
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 ************************************************************
  Group 11.Initialise Var/Porosity Fields
   No PATCHes used for this Group
 
 
 INIADD = F
 ************************************************************
  Group 12. Convection and diffusion adjustments
   No PATCHes used for this Group
 ************************************************************
  Group 13. Boundary & Special Sources
   No PATCHes used for this Group
 
 BUOYA =0. ; BUOYB =0.
 BUOYC =-9.81
 EGWF = T
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 200
 RESFAC =1.0E-03
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=50
 ************************************************************
  Group 17. Relaxation
 RELAX(P1 ,LINRLX,1. )
 RELAX(U1 ,FALSDT,1.0E-02 )
 RELAX(V1 ,FALSDT,1.0E-02 )
 ************************************************************
  Group 18. Limits
 VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-5.0E+04
 ************************************************************
  Group 19. EARTH Calls To GROUND Station
 CSG3    ='FGEM'
 ************************************************************
  Group 20. Preliminary Printout
 ************************************************************
  Group 21. Print-out of Variables
 OUTPUT(P1  ,Y,Y,Y,N,Y,Y)
 OUTPUT(U1  ,Y,Y,Y,N,Y,Y)
 OUTPUT(V1  ,Y,Y,Y,N,Y,Y)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 2 ;IYMON = 1 ;IZMON = 1
 NPRMON = 100000
 NPRMNT = 1
 TSTSWP = -1
 ************************************************************
  Group 23.Field Print-Out & Plot Control
 NPRINT = 100000
 ISWPRF = 1 ;ISWPRL = 100000
   No PATCHes used for this Group
 ************************************************************
  Group 24. Dumps For Restarts
 
 GVIEW(P,-0.206711,0.290959,0.934138)
 GVIEW(UP,0.024861,0.956012,-0.292271)
 
> DOM,    SIZE,        9.000000E+00, 4.000000E+00, 1.000000E+00
> DOM,    MONIT,       4.500000E-01, 1.000000E-01, 5.000000E-01
> DOM,    SCALE,       1.000000E+00, 1.000000E+00, 1.000000E+00
  > GRID,   RSET_X_1,      4, 1.000000E+00
  > GRID,   RSET_X_2,      1, 1.000000E+00
  > GRID,   RSET_X_3,     13, 1.000000E+00
  > GRID,   RSET_X_4,      1, 1.000000E+00
  > GRID,   RSET_X_5,     11, 1.000000E+00
  > GRID,   RSET_Y_1,      5, 1.000000E+00
> GRID,   RSET_Y_2,      1, 1.000000E+00
  > GRID,   RSET_Y_3,      3, 1.000000E+00
  > GRID,   RSET_Y_4,      1, 1.000000E+00
  > GRID,   RSET_Y_5,     10, 1.000000E+00
  > GRID,   RSET_Z_1,      1, 1.000000E+00
 
> OBJ,    NAME,        IN
> OBJ,    POSITION,    0.000000E+00, 0.000000E+00, 0.000000E+00
> OBJ,    SIZE,        0.000000E+00, 4.000000E+00, 1.000000E+00
> OBJ,    GEOMETRY,    cube3t
> OBJ,    TYPE,        INLET
> OBJ,    PRESSURE,    0.
> OBJ,    VELOCITY,    1. ,0. ,0.
 
> OBJ,    NAME,        OUT
> OBJ,    POSITION,    9.000000E+00, 0.000000E+00, 0.000000E+00
> OBJ,    SIZE,        0.000000E+00, 4.000000E+00, 1.000000E+00
> OBJ,    GEOMETRY,    cube12t
> OBJ,    TYPE,        OUTLET
> OBJ,    PRESSURE,    0.
> OBJ,    COEFFICIENT, 1000.
 
> OBJ,    NAME,        WAL2
> OBJ,    POSITION,    0.000000E+00, 0.000000E+00, 0.000000E+00
> OBJ,    SIZE,        9.000000E+00, 0.000000E+00, 1.000000E+00
> OBJ,    GEOMETRY,    cube11
> OBJ,    TYPE,        PLATE
 
> OBJ,    NAME,        WAL1
> OBJ,    POSITION,    0.000000E+00, 4.000000E+00, 0.000000E+00
> OBJ,    SIZE,        9.000000E+00, 0.000000E+00, 1.000000E+00
> OBJ,    GEOMETRY,    cube11
> OBJ,    TYPE,        PLATE
 
> OBJ,    NAME,        AIRFOIL
> OBJ,    POSITION,    1.500000E+00, 1.200000E+00, 0.000000E+00
> OBJ,    SIZE,        4.000000E+00, 6.000000E-01, 1.000000E+00
> OBJ,    GEOMETRY,    airfoil
> OBJ,    TYPE,        BLOCKAGE
> OBJ,    MATERIAL,    198,Solid with smooth-wall friction
 
> OBJ,    NAME,        FINE
> OBJ,    POSITION,    1.200000E+00, 1.000000E+00, 0.000000E+00
> OBJ,    SIZE,        4.500000E+00, 1.000000E+00, 1.000000E+00
> OBJ,    GEOMETRY,    fine
> OBJ,    TYPE,        FINE_GRID_VOL
> OBJ,    FINEFACTS,   3, 3, 1
STOP