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TALK=T;RUN(1,1)
DISPLAY
This run illustrates the flow arising when a cold round
laminar jet impinges directly on to a flat surface
(referred to as the floor). The jet enters the domain
through the low boundary at iz=1, and it is spread over
several cells in order to represent the round shape of the
jet, as indicated in the diagram on the right:

|--------------------->x         |---|---|---|---------->x
|   \                            |---|---|---|
|    \                           |---|---|
|     \                          |---| \
|      \                         |      \
|       \                        |       cells through
| jet    \                       |       which jet enters
z|         \                      |       domain.
V|          \                    y|
|           \------              V
|______________________floor
ENDDIS
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************

TEXT(Impinging Jet In  Rectangular Grid      )

************************************************************
************************************************************

IRUNN = 1 ;LIBREF = 14
************************************************************
Group 2. Time dependence
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = T
NX = 12
XULAST =1.
XFRAC(1)=0.05 ;XFRAC(2)=0.075
XFRAC(3)=0.1 ;XFRAC(4)=0.125
XFRAC(5)=0.1575 ;XFRAC(6)=0.19975
XFRAC(7)=0.254675 ;XFRAC(8)=0.326077
XFRAC(9)=0.418901 ;XFRAC(10)=0.539571
XFRAC(11)=0.696442 ;XFRAC(12)=1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 12
YVLAST =1.
YFRAC(1)=0.05 ;YFRAC(2)=0.075
YFRAC(3)=0.1 ;YFRAC(4)=0.125
YFRAC(5)=0.1575 ;YFRAC(6)=0.19975
YFRAC(7)=0.254675 ;YFRAC(8)=0.326077
YFRAC(9)=0.418901 ;YFRAC(10)=0.539571
YFRAC(11)=0.696442 ;YFRAC(12)=1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 10
ZWLAST =1.
ZFRAC(1)=0.1 ;ZFRAC(5)=0.5
ZFRAC(9)=0.9
************************************************************
Group 6. Body-Fitted Coordinates
************************************************************
Group 7. Variables: STOREd,SOLVEd,NAMEd
ONEPHS = T
NAME(1)=P1 ;NAME(3)=U1
NAME(5)=V1 ;NAME(7)=W1
* 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,N)
SOLUTN(U1,Y,Y,N,N,N,Y)
SOLUTN(V1,Y,Y,N,N,N,Y)
SOLUTN(W1,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(W1,Y,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. ;TMP1 =0.
EL1 =0.
TSURR =0. ;TEMP0 =0.
PRESS0 =0.
DVO1DT =0. ;DRH1DP =0.
EMISS =0. ;SCATT =0.
ENUL =1.0E-02 ;ENUT =0.
PRNDTL(U1)=1. ;PRNDTL(V1)=1.
PRNDTL(W1)=1.
PRT(U1)=1. ;PRT(V1)=1.
PRT(W1)=1.
CP1 =1. ;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(W1)=1.0E-10
No PATCHes yet used for this Group
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(JET1 ,LOW , 1, 1, 1, 3, 1, 1, 1, 1)
COVAL(JET1 ,P1 , FIXFLU ,10. )
COVAL(JET1 ,U1 ,0. ,0. )
COVAL(JET1 ,V1 ,0. ,0. )
COVAL(JET1 ,W1 ,0. ,10. )

PATCH(JET2 ,LOW , 2, 2, 1, 2, 1, 1, 1, 1)
COVAL(JET2 ,P1 , FIXFLU ,10. )
COVAL(JET2 ,U1 ,0. ,0. )
COVAL(JET2 ,V1 ,0. ,0. )
COVAL(JET2 ,W1 ,0. ,10. )

PATCH(JET3 ,LOW , 3, 3, 1, 1, 1, 1, 1, 1)
COVAL(JET3 ,P1 , FIXFLU ,10. )
COVAL(JET3 ,U1 ,0. ,0. )
COVAL(JET3 ,V1 ,0. ,0. )
COVAL(JET3 ,W1 ,0. ,10. )

PATCH(FREE1 ,EAST , 12, 12, 1, 12, 1, 10, 1, 1)
COVAL(FREE1 ,P1 ,1000. ,0. )
COVAL(FREE1 ,U1 ,0. ,0. )
COVAL(FREE1 ,V1 ,0. ,0. )
COVAL(FREE1 ,W1 ,0. ,0. )

PATCH(FREE2 ,NORTH , 1, 12, 12, 12, 1, 10, 1, 1)
COVAL(FREE2 ,P1 ,1000. ,0. )
COVAL(FREE2 ,U1 ,0. ,0. )
COVAL(FREE2 ,V1 ,0. ,0. )
COVAL(FREE2 ,W1 ,0. ,0. )

PATCH(FREE3 ,LOW , 4, 12, 1, 12, 1, 1, 1, 1)
COVAL(FREE3 ,P1 ,1000. ,0. )
COVAL(FREE3 ,U1 ,0. ,0. )
COVAL(FREE3 ,V1 ,0. ,0. )
COVAL(FREE3 ,W1 ,0. ,0. )

PATCH(FREE4 ,LOW , 1, 4, 4, 12, 1, 1, 1, 1)
COVAL(FREE4 ,P1 ,1000. ,0. )
COVAL(FREE4 ,U1 ,0. ,0. )
COVAL(FREE4 ,V1 ,0. ,0. )
COVAL(FREE4 ,W1 ,0. ,0. )

PATCH(FREE5 ,LOW , 3, 3, 2, 3, 1, 1, 1, 1)
COVAL(FREE5 ,P1 ,1000. ,0. )
COVAL(FREE5 ,U1 ,0. ,0. )
COVAL(FREE5 ,V1 ,0. ,0. )
COVAL(FREE5 ,W1 ,0. ,0. )

PATCH(FREE6 ,LOW , 2, 2, 3, 3, 1, 1, 1, 1)
COVAL(FREE6 ,P1 ,1000. ,0. )
COVAL(FREE6 ,U1 ,0. ,0. )
COVAL(FREE6 ,V1 ,0. ,0. )
COVAL(FREE6 ,W1 ,0. ,0. )

PATCH(FLOOR ,HWALL , 1, 12, 1, 12, 10, 10, 1, 1)
COVAL(FLOOR ,U1 ,1. ,0. )
COVAL(FLOOR ,V1 ,1. ,0. )
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 60 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =1.0E-04
************************************************************
Group 16. Terminate Iterations
LITER(P1)=20 ;LITER(U1)=10
LITER(V1)=10 ;LITER(W1)=10
ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
ENDIT(V1)=1.0E-03 ;ENDIT(W1)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(U1,FALSDT,1.)
RELAX(V1,FALSDT,1.)
RELAX(W1,FALSDT,1.)
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(W1)=1.0E+06 ;VARMIN(W1)=-1.0E+06
************************************************************
Group 19. Data transmitted to GROUND
PARSOL = F
ISG62 = 1
************************************************************
Group 20. Preliminary Printout
************************************************************
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(W1,Y,N,Y,Y,Y,Y)
************************************************************
Group 22. Monitor Print-Out
IXMON = 6 ;IYMON = 6 ;IZMON = 10
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 = 8
NYPRIN = -1 ;IYPRF = 1 ;IYPRL = 8
NZPRIN = 4 ;IZPRF = 1 ;IZPRL = 10000
XZPR = F ;YZPR = F
IPLTF = 1 ;IPLTL = -1 ;NPLT = 2
ISWPRF = 1 ;ISWPRL = 100000
ITABL = 3 ;IPROF = 1
ABSIZ =0.5 ;ORSIZ =0.4
NTZPRF = 1 ;NCOLPF = 50
ICHR = 3 ;NCOLCO = 45 ;NROWCO = 20

PATCH(IXEQ10 ,CONTUR, 1, 8, 1, 8, 10, 10, 1, 1)
PLOT(IXEQ10 ,P1 ,0. ,20. )
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP
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