TALK=T;RUN(1,1)
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  Group 1. Run Title and Number
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 TEXT(Flow over an airfoil: Y115              )
 
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 IRUNN = 1 ;LIBREF = 0
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  Group 2. Time dependence
 STEADY = T
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  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 30
 XULAST =9.
 XFRAC(1)=0.033333 ;XFRAC(2)=0.066667
 XFRAC(3)=0.1 ;XFRAC(4)=0.133333
 XFRAC(5)=0.166667 ;XFRAC(6)=0.200855
 XFRAC(7)=0.235043 ;XFRAC(8)=0.269231
 XFRAC(9)=0.303419 ;XFRAC(10)=0.337607
 XFRAC(11)=0.371795 ;XFRAC(12)=0.405983
 XFRAC(13)=0.440171 ;XFRAC(14)=0.474359
 XFRAC(15)=0.508547 ;XFRAC(16)=0.542735
 XFRAC(17)=0.576923 ;XFRAC(18)=0.611111
 XFRAC(19)=0.633333 ;XFRAC(20)=0.666667
 XFRAC(21)=0.7 ;XFRAC(22)=0.733333
 XFRAC(23)=0.766667 ;XFRAC(24)=0.8
 XFRAC(25)=0.833333 ;XFRAC(26)=0.866667
 XFRAC(27)=0.9 ;XFRAC(28)=0.933333
 XFRAC(29)=0.966667 ;XFRAC(30)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 20
 YVLAST =4.
 YFRAC(1)=0.05 ;YFRAC(2)=0.1
 YFRAC(3)=0.15 ;YFRAC(4)=0.2
 YFRAC(5)=0.25 ;YFRAC(6)=0.3
 YFRAC(7)=0.35 ;YFRAC(8)=0.4
 YFRAC(9)=0.45 ;YFRAC(10)=0.5
 YFRAC(11)=0.55 ;YFRAC(12)=0.6
 YFRAC(13)=0.65 ;YFRAC(14)=0.7
 YFRAC(15)=0.75 ;YFRAC(16)=0.8
 YFRAC(17)=0.85 ;YFRAC(18)=0.9
 YFRAC(19)=0.95 ;YFRAC(20)=1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 1
 ZWLAST =1.
 ZFRAC(1)=1.
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  Group 6. Body-Fitted Coordinates
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  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(3)=U1
 NAME(5)=V1 ;NAME(150)=PRPS
    * Y in SOLUTN argument list denotes:
    * 1-stored 2-solved 3-whole-field
    * 4-point-by-point 5-explicit 6-harmonic averaging 
 SOLUTN(P1,Y,Y,Y,N,N,Y)
 SOLUTN(U1,Y,Y,N,N,N,Y)
 SOLUTN(V1,Y,Y,N,N,N,Y)
 SOLUTN(PRPS,Y,N,N,N,N,N)
 PRPS = 150
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  Group 8. Terms & Devices
    * Y in TERMS argument list denotes:
    * 1-built-in source 2-convection 3-diffusion 4-transient
    * 5-first phase variable 6-interphase transport         
 TERMS(P1,Y,Y,Y,N,Y,Y)
 TERMS(U1,Y,Y,Y,Y,Y,Y)
 TERMS(V1,Y,Y,Y,Y,Y,Y)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 ISOLX = -1 ;ISOLY = -1 ;ISOLZ = -1
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  Group 9. Properties used if PRPS is not
  stored, and where PRPS = -1.0 if it is!
 RHO1 =1.189 ;TMP1 =0. ;EL1 =0.
 TSURR =0. ;TEMP0 =273. ;PRESS0 =1.0E+05
 DVO1DT =3.41E-03 ;DRH1DP =1.0E-05
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =1.0E-03 ;ENUT =0.
 PRNDTL(U1)=1. ;PRNDTL(V1)=1.
 PRT(U1)=1. ;PRT(V1)=1.
 CP1 =1005. ;CP2 =1.
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  Group 10.Inter-Phase Transfer Processes
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  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=1.0E-10 ;FIINIT(U1)=1.0E-10
 FIINIT(V1)=1.0E-10 ;FIINIT(PRPS)=-1.
 
 PATCH(^OB6 ,INIVAL, 6, 0, 0, 0, 0, 0, 1, 1)
 INIT(^OB6 ,PRPS,0. ,198. )
 INIADD = F
 FSWEEP = 1
 NAMFI =CHAM
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  Group 12. Patchwise adjustment of terms
  Patches for this group are printed with those
  for Group 13.
  Their names begin either with GP12 or &
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  Group 13. Boundary & Special Sources
 
 PATCH(^OB1 ,CELL , 1, 0, 0, 0, 0, 0, 1, 1)
 
 PATCH(^OB2 ,WEST , 2, 0, 0, 0, 0, 0, 1, 1)
 COVAL(^OB2 ,P1 , FIXFLU ,1.189 )
 COVAL(^OB2 ,U1 ,0. ,1. )
 COVAL(^OB2 ,V1 ,0. ,0. )
 
 PATCH(^OB3 ,EAST , 3, 0, 0, 0, 0, 0, 1, 1)
 COVAL(^OB3 ,P1 ,1000. ,0. )
 COVAL(^OB3 ,U1 ,0. ,0. )
 COVAL(^OB3 ,V1 ,0. ,0. )
 
 PATCH(^OB4 ,CELL , 4, 8, 0, 0, 0, 0, 1, 1)
 COVAL(^OB4 ,U1 ,1. ,0. )
 
 PATCH(^OB5 ,CELL , 5, 7, 0, 0, 0, 0, 1, 1)
 COVAL(^OB5 ,U1 ,1. ,0. )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 BUOYA =0. ; BUOYB =0. ; BUOYC =-9.81
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  Group 14. Downstream Pressure For PARAB
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  Group 15. Terminate Sweeps
 LSWEEP = 200 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-03
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  Group 16. Terminate Iterations
 LITER(P1)=50 ;LITER(U1)=10
 LITER(V1)=10
 ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
 ENDIT(V1)=1.0E-03
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  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(U1,FALSDT,1.0E-02)
 RELAX(V1,FALSDT,1.0E-02)
 RELAX(PRPS,LINRLX,1.)
 OVRRLX =0.
 EXPERT = F ;NNORSL = F
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  Group 18. Limits
 VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-5.0E+04
 VARMAX(U1)=1.0E+06 ;VARMIN(U1)=-1.0E+06
 VARMAX(V1)=1.0E+06 ;VARMIN(V1)=-1.0E+06
 VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
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  Group 19. Data transmitted to GROUND
 ISG62 = 0
 CSG3    ='FGEM'
 SPEDAT(SET,DOMAIN,PHASE_1_MAT,I,0)
 SPEDAT(SET,GXMONI,PLOTALL,L,T)
 SPEDAT(SET,OBJNAM,^OB1,C,FINE)
 SPEDAT(SET,OBJTYP,^OB1,C,FINE_GRID_VOL)
 SPEDAT(SET,^OB1,FINEX,I,3)
 SPEDAT(SET,^OB1,FINEY,I,3)
 SPEDAT(SET,^OB1,FINEZ,I,1)
 SPEDAT(SET,OBJNAM,^OB2,C,IN)
 SPEDAT(SET,OBJTYP,^OB2,C,INLET)
 SPEDAT(SET,OBJNAM,^OB3,C,OUT)
 SPEDAT(SET,OBJTYP,^OB3,C,OUTLET)
 SPEDAT(SET,ARATIO,^OB3,R,1.)
 SPEDAT(SET,OBJNAM,^OB4,C,WAL2)
 SPEDAT(SET,OBJTYP,^OB4,C,PLATE)
 SPEDAT(SET,OBJNAM,^OB5,C,WAL1)
 SPEDAT(SET,OBJTYP,^OB5,C,PLATE)
 SPEDAT(SET,OBJNAM,^OB6,C,AIRFOIL)
 SPEDAT(SET,OBJTYP,^OB6,C,BLOCKAGE)
 SPEDAT(SET,AIRFOIL,MATERIAL,R,198.)
 SPEDAT(SET,FACETDAT,NUMOBJ,I,6)
 SPEDAT(SET,MATERIAL,198,L,T)
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  Group 20. Preliminary Printout
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  Group 21. Print-out of Variables
 INIFLD = F ;SUBWGR = F
    * Y in OUTPUT argument list denotes:
    * 1-field 2-correction-eq. monitor 3-selective dumping      
    * 4-whole-field residual 5-spot-value table 6-residual table
 OUTPUT(P1,Y,Y,Y,N,Y,Y)
 OUTPUT(U1,Y,Y,Y,N,Y,Y)
 OUTPUT(V1,Y,Y,Y,N,Y,Y)
 OUTPUT(PRPS,Y,N,Y,N,N,N)
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  Group 22. Monitor Print-Out
 IXMON = 2 ;IYMON = 1 ;IZMON = 1
 NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = -1
 UWATCH = T ;USTEER = T
 HIGHLO = F
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  Group 23.Field Print-Out & Plot Control
 NPRINT = 100000 ;NUMCLS = 5
 NXPRIN = -1 ;IXPRF = 1 ;IXPRL = 10000
 NYPRIN = -1 ;IYPRF = 1 ;IYPRL = 10000
 IPLTF = 1 ;IPLTL = -1 ;NPLT = -1
 ISWPRF = 1 ;ISWPRL = 100000
 ITABL = 3 ;IPROF = 1
 ABSIZ =0.5 ;ORSIZ =0.4
 NTZPRF = 1 ;NCOLPF = 50
 ICHR = 2 ;NCOLCO = 45 ;NROWCO = 20
   No PATCHes yet used for this Group
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  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP