TALK=T;RUN(1,1)
  DISPLAY
   This example illustrates a use of In-Form for the introduction
   of input boundary conditions for TEM1 variable.

   As a problem is considered injection into a plane flow.

                                                           !
                                     !                     !
               \!/                  \!/   Wall            \!/
              /////////////////////////////////////////////////////
  Non-uniform -----------------------------------------------------
  specified   ->                                                ->
  mass-flux   -->                                               -->
  and         --->                                              --->
  velocity    - - - - - - - - - - -Symmetry plane - - - - - - - - -
               ^ y
               |-------> x-direction


  The inlet flow has a parabolic structure. Inflowing gas has
  TEMINL temperature. It is supposed that the specific heat of
  the inflowing material is the same as that in domain. In this
  case it is enough to specify the inlet temperature value only
  in a boundary condition. EARTH automatically multiplies the
  inflow temperature TEMINL by the specific heat which prevails
  in the cells into which the mass is flowing.

  The injection size on a wall is increased proportionally
  to its length. Injecting gas has TEMINJ temperature. It is
  supposed that injecting gas has the CPINJ specific heat
  distinguished from that inside the domain. In this case
  in the boundary condition it should multiply the injecting
  temperature value on the injecting specific heat and to use

  The Q1 contains PHOTON USE commands
  ENDDIS
  PHOTON USE
  p
  phi
  1 8 1

  msg picture is enlarged 8 times in y direction
  gr ou z 1
  msg contours of TEM1
  con tem1 z 1 fi;0.001;upause 2
  msg velocity vectors
  vec z 1
  enduse
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(Injection In Channel By In-Form.        )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 0
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 20
 XULAST =0.2
 XFRAC(1)=0.05 ;XFRAC(2)=0.1
 XFRAC(3)=0.15 ;XFRAC(4)=0.2
 XFRAC(5)=0.25 ;XFRAC(6)=0.3
 XFRAC(7)=0.35 ;XFRAC(8)=0.4
 XFRAC(9)=0.45 ;XFRAC(10)=0.5
 XFRAC(11)=0.55 ;XFRAC(12)=0.6
 XFRAC(13)=0.65 ;XFRAC(14)=0.7
 XFRAC(15)=0.75 ;XFRAC(16)=0.8
 XFRAC(17)=0.85 ;XFRAC(18)=0.9
 XFRAC(19)=0.95 ;XFRAC(20)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 20
 YVLAST =1.0E-02
 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.
 ************************************************************
  Group 6. Body-Fitted Coordinates
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(3)=U1
 NAME(5)=V1 ;NAME(150)=TEM1
    * 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,N,N,N,Y)
 SOLUTN(U1,Y,Y,N,N,N,Y)
 SOLUTN(V1,Y,Y,N,N,N,Y)
 SOLUTN(TEM1,Y,Y,N,N,N,Y)
 ************************************************************
  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)
 TERMS(TEM1,N,Y,Y,Y,Y,Y)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 ISOLX = -1 ;ISOLY = -1 ;ISOLZ = -1
 ************************************************************
  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 =0.
 PRESS0 =0.
 DVO1DT =3.41E-03 ;DRH1DP =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =1.544E-05 ;ENUT =0.
 PRNDTL(U1)=1. ;PRNDTL(V1)=1.
 PRNDTL(TEM1)=-0.0258
 PRT(U1)=1. ;PRT(V1)=1.
 PRT(TEM1)=1.
 CP1 =1005. ;CP2 =1.
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 ************************************************************
  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=1.0E-10 ;FIINIT(U1)=1.0E-10
 FIINIT(V1)=1.0E-10 ;FIINIT(TEM1)=1.0E-10
   No PATCHes yet used for this Group
 INIADD = F
 FSWEEP = 1
 NAMFI =CHAM
 ************************************************************
  Group 12. Patchwise adjustment of terms
  Patches for this group are printed with those
  for Group 13.
  Their names begin either with GP12 or &
 ************************************************************
  Group 13. Boundary & Special Sources
 
 PATCH(INL ,WEST , 1, 1, 1, 20, 1, 1, 1, 1)
 COVAL(INL ,P1 ,In-Form:source - see Grp 19)
 COVAL(INL ,U1 ,In-Form:source - see Grp 19)
 COVAL(INL ,V1 ,In-Form:source - see Grp 19)
 COVAL(INL ,TEM1,In-Form:source - see Grp 19)
 
 PATCH(NOCPINJ ,NORTH , 1, 20, 20, 20, 1, 1, 1, 1)
 COVAL(NOCPINJ ,P1 ,In-Form:source - see Grp 19)
 COVAL(NOCPINJ ,V1 ,In-Form:source - see Grp 19)
 COVAL(NOCPINJ ,TEM1,In-Form:source - see Grp 19)
 
 PATCH(NW ,NORTH , 1, 20, 20, 20, 1, 1, 1, 1)
 COVAL(NW ,U1 ,In-Form:source - see Grp 19)
 
 PATCH(OUT ,EAST , 20, 20, 1, 20, 1, 1, 1, 1)
 COVAL(OUT ,P1 ,In-Form:source - see Grp 19)
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 50 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =0.1
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(U1)=10
 LITER(V1)=10 ;LITER(TEM1)=20
 ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
 ENDIT(V1)=1.0E-03 ;ENDIT(TEM1)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(U1,FALSDT,0.1)
 RELAX(V1,FALSDT,0.1)
 RELAX(TEM1,FALSDT,1.0E+09)
 OVRRLX =0.
 EXPERT = F ;NNORSL = F
 ************************************************************
  Group 18. Limits
 VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-1.0E+10
 VARMAX(U1)=1.0E+06 ;VARMIN(U1)=-1.0E+06
 VARMAX(V1)=1.0E+06 ;VARMIN(V1)=-1.0E+06
 VARMAX(TEM1)=1.0E+10 ;VARMIN(TEM1)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 PARSOL = F
 CONWIZ = T
 ISG50 = 1
 ISG52 = 2
 ISG62 = 1
 SPEDAT(SET,DOMAIN,PHASE_1_MAT,I,0)
 SPEDAT(SET,SOURCE,R1!INL,C,=RHO1*0.5*(1.-(YG/YVLAST)^2))
 SPEDAT(SET,SOURCE,U1!INL,C,=0.5*(1.-(YG/YVLAST)^2)!ONLYMS)
 SPEDAT(SET,SOURCE,V1!INL,C,=0.0!ONLYMS)
 SPEDAT(SET,SOURCE,TEM1!INL,C,=0.!ONLYMS)
 SPEDAT(SET,SOURCE,R1!NOCPINJ,C,=RHO1*0.1*XG/XULAST)
 SPEDAT(SET,SOURCE,V1!NOCPINJ,C,=-0.1*XG/XULAST!ONLYMS)
 SPEDAT(SET,SOURCE,TEM1!NOCPINJ,C,=1.*5000.!ONLYMS)
 SPEDAT(SET,SOURCE,U1!NW,C,=0.0!LAMWALL)
 SPEDAT(SET,SOURCE,R1!OUT,C,=1000.*(0.-P1)!LINE)
 ************************************************************
  Group 20. Preliminary Printout
 DISTIL = T ;NULLPR = F
 NDST = 0
 DSTTOL =1.0E-02
 EX(P1)=1.626 ;EX(U1)=0.6584
 EX(V1)=0.0325 ;EX(TEM1)=2.689
 ************************************************************
  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,N,Y,Y,Y,Y)
 OUTPUT(U1,Y,N,Y,Y,Y,Y)
 OUTPUT(V1,Y,N,Y,Y,Y,Y)
 OUTPUT(TEM1,Y,N,Y,Y,Y,Y)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 10 ;IYMON = 19 ;IZMON = 1
 NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = -1
 UWATCH = T ;USTEER = T
 HIGHLO = F
 ************************************************************
  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
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP