TALK=T;RUN( 1, 1)
 
 ************************************************************
   Q1 created by VDI menu, Version 2025, Date 03/02/25
 CPVNAM=VDI; SPPNAM=Core
 ************************************************************
  Echo DISPLAY / USE settings
  DISPLAY
  This case concerns 3-dimensional, incompressible flow
  around a NACA2414 aerofoil. This is a non-symmetric aerofoil,
  with maximum camber of 2% located 40% from the leading edge,
  with a maximum thickness of 14% of the chord. The chord
  length is 1, giving a Reynolds number of 3.2 million.
 
  Calculations are made with the high-Reynolds form of the
  Spalart-Allmaras turbulence model, with wall functions.
 
  ENDDIS
 ************************************************************
 IRUNN = 1 ;LIBREF = 0
 ************************************************************
  Group 1. Run Title
 TEXT(S-A NACA2414 Aerofoil                   )
 ************************************************************
  Group 2. Transience
 STEADY = T
 ************************************************************
  Groups 3, 4, 5  Grid Information
    * Overall number of cells, RSET(M,NX,NY,NZ,tolerance)
 RSET(M,197,144,88)
 ************************************************************
  Group 6. Body-Fitted coordinates
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
    * Non-default variable names
 NAME(136)=PRPS ;NAME(137)=ENUT
 NAME(138)=YPLS ;NAME(139)=DWDY
 NAME(140)=DWDX ;NAME(141)=DVDZ
 NAME(142)=DVDX ;NAME(143)=DUDZ
 NAME(144)=MACH ;NAME(145)=DUDY
 NAME(147)=WDIS ;NAME(148)=DEN1
 NAME(149) =VOR1
    * Solved variables list
 SOLVE(P1,U1,V1,W1)
    * Stored variables list
 STORE(VOR1,DEN1,WDIS,DUDY,MACH,DUDZ,DVDX,DVDZ)
 STORE(DWDX,DWDY,YPLS,ENUT,PRPS)
    * Additional solver options
 SOLUTN(P1,Y,Y,Y,N,N,Y)
 TURMOD(SPALART-ALLMARAS)
 
 ************************************************************
  Group 8. Terms & Devices
 ************************************************************
  Group 9. Properties
 PRESS0 =1.01325E+05 ;TEMP0 =273.149994
    * Domain material index is   0 signifying:
    * Air at 20 deg C, 1 atm, treated as incompressible
 SETPRPS(1, 0)
 DVO1DT =3.41E-03
 PRT(ENTI)=0.666667
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 ************************************************************
  Group 11.Initialise Var/Porosity Fields
 FIINIT(P1)=0. ;FIINIT(PRPS)=-1.
 FIINIT(WDIS)=0.4
   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
 BUOYD =1.204321
 EGWF = T
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 6000
 RESFAC =1.0E-05
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=200
 ************************************************************
  Group 17. Relaxation
 RELAX(P1 ,LINRLX,1. )
 RELAX(U1 ,FALSDT,5.0E-03 )
 RELAX(V1 ,FALSDT,5.0E-03 )
 RELAX(W1 ,FALSDT,5.0E-03 )
 RELAX(ENTI,LINRLX,0.5 )
 ************************************************************
  Group 18. Limits
 VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-7.599375E+04
 ************************************************************
  Group 19. EARTH Calls To GROUND Station
 NAMGRD =FLAR
 ISG62 = 0
 SPEDAT(SET,OUTPUT,NOFIELD,L,T)
 SPEDAT(SET,FLAIR,STOIC,R,1.908397)
 SPEDAT(SET,GXMONI,PLOTALL,L,T)
 SPEDAT(SET,RLXFAC,REFVEL,R,55.)
 ************************************************************
  Group 20. Preliminary Printout
 DISTIL = T ;NULLPR = F
 NDST = 0
 DSTTOL =1.0E-02
 EX(P1)=79.970001 ;EX(U1)=47.110001
 EX(V1)=1.298 ;EX(W1)=1.031
 EX(PRPS)=0.9489 ;EX(ENUT)=8.414E-05
 EX(YPLS)=0.8191 ;EX(DWDY)=12.57
 EX(DWDX)=4.78 ;EX(DVDZ)=15.27
 EX(DVDX)=9.425 ;EX(DUDZ)=20.450001
 EX(MACH)=0.1369 ;EX(DUDY)=36.389999
 EX(LTLS)=9.172 ;EX(WDIS)=1.71
 EX(DEN1)=1.128 ;EX(VOR1)=50.740002
 EX(ENTI)=1.223E-04
 ************************************************************
  Group 21. Print-out of Variables
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 180 ;IYMON = 107 ;IZMON = 42
 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.,0.,1.)
 GVIEW(UP,0.,1.,0.)
 GVIEW(WINDOW,MAX)
 GVIEW(DEPTH,712.129761)
 GVIEW(VDIS,4.506764)
 GVIEW(CENTRE,3.826032,2.579438,0.759813)
 
> DOM,    SIZE,        5.000000E+00, 5.000000E+00, 4.000000E+00
> DOM,    MONIT,       3.317879E+00, 2.611747E+00, 1.010247E+00
> DOM,    SCALE,       1.000000E+00, 1.000000E+00, 1.000000E+00
> GRID,   MINCELL,     2.344229E-03 ,1.0E-03 ,1.0E-03
> GRID,   RSET_X_1,     47,-1.100000E+00,G
> GRID,   RSET_X_2,     40, 1.040000E+00,G
> GRID,   RSET_X_3,     75,-1.010000E+00,G
> GRID,   RSET_X_4,     35, 1.100000E+00,G
> GRID,   RSET_Y_1,     47,-1.100000E+00,G
> GRID,   RSET_Y_2,     50, 1.000000E+00,G
> GRID,   RSET_Y_3,     47, 1.100000E+00,G
> GRID,   RSET_Z_1,     38,-1.100000E+00,G
> GRID,   RSET_Z_2,     50, 1.100000E+00,G
> DOM,    INI_AMB,    YES
> DOM,    INI_BUOY,   YES
 
> OBJ,    NAME,        BLOC1
> OBJ,    POS-CEN,     2.500000E+00, 2.500000E+00, 5.000000E-01
> OBJ,    SIZE,        1.000080E+00, 1.412570E-01, 1.000000E+00
> OBJ,    GEOMETRY,    naca2414
> OBJ,    TYPE,        BLOCKAGE
> OBJ,    COLOR-MODE,  FROM_FIL
> OBJ,    COLOR-VAL,   30
> OBJ,    MATERIAL,    198,Solid with smooth-wall friction
 
> OBJ,    NAME,        BLOC2
> OBJ,    POSITION,    1.999960E+00, 2.429372E+00, 0.000000E+00
> OBJ,    SIZE,        2.500000E-01, 1.412570E-01, 1.000000E+00
> OBJ,    GEOMETRY,    wirexyz
> OBJ,    TYPE,        NULL
> OBJ,    COLOR-MODE,  FROM_FIL
> OBJ,    COLOR-VAL,   50
 
> OBJ,    NAME,        IN
> OBJ,    POSITION,    0.000000E+00, 0.000000E+00, 0.000000E+00
> OBJ,    SIZE,        0.000000E+00, TO_END,       TO_END
> OBJ,    DOMCLIP,     NO
> OBJ,    GEOMETRY,    cube3t
> OBJ,    VISIBLE,     NO
> OBJ,    TYPE,        INLET
> OBJ,    COLOR-MODE,  FROM_FIL
> OBJ,    COLOR-VAL,   192
> OBJ,    PRESSURE,     P_AMBIENT
> OBJ,    VELOCITY,    50. ,0. ,0.
> OBJ,    TURB_IN,     VISC_RAT
> OBJ,    VISCRAT,     3.000000E+00
 
> OBJ,    NAME,        OPEN3
> OBJ,    POSITION,    AT_END,       0.000000E+00, 0.000000E+00
> OBJ,    SIZE,        0.000000E+00, TO_END,       TO_END
> OBJ,    DOMCLIP,     NO
> OBJ,    GEOMETRY,    cube12t
> OBJ,    VISIBLE,     NO
> OBJ,    TYPE,        OUTLET
> OBJ,    COLOR-MODE,  FROM_FIL
> OBJ,    COLOR-VAL,   214
> OBJ,    PRESSURE,     P_AMBIENT
> OBJ,    COEFFICIENT, 1.
> OBJ,    TURBULENCE,  0. ,4.632E-05
 
> OBJ,    NAME,        OPEN4
> OBJ,    POSITION,    0.000000E+00, 0.000000E+00, 0.000000E+00
> OBJ,    SIZE,        TO_END,       0.000000E+00, TO_END
> OBJ,    DOMCLIP,     NO
> OBJ,    GEOMETRY,    wirexyz
> OBJ,    VISIBLE,     NO
> OBJ,    TYPE,        NULL
> OBJ,    COLOR-MODE,  FROM_FIL
> OBJ,    COLOR-VAL,   50
 
> OBJ,    NAME,        OPEN5
> OBJ,    POSITION,    0.000000E+00, AT_END,       0.000000E+00
> OBJ,    SIZE,        TO_END,       0.000000E+00, TO_END
> OBJ,    DOMCLIP,     NO
> OBJ,    GEOMETRY,    wirexyz
> OBJ,    VISIBLE,     NO
> OBJ,    TYPE,        NULL
> OBJ,    COLOR-MODE,  FROM_FIL
> OBJ,    COLOR-VAL,   50
 
> OBJ,    NAME,        OPEN6
> OBJ,    POSITION,    0.000000E+00, 0.000000E+00, AT_END
> OBJ,    SIZE,        TO_END,       TO_END,       0.000000E+00
> OBJ,    DOMCLIP,     NO
> OBJ,    GEOMETRY,    wirexyz
> OBJ,    VISIBLE,     NO
> OBJ,    TYPE,        NULL
> OBJ,    COLOR-MODE,  FROM_FIL
> OBJ,    COLOR-VAL,   50
STOP