TALK=T;RUN(1,1)
   PHOTON USE
   AUTOPLOT
   file
   phi 5

   cl
   msg U1 FLOW IN AN ANNULUS: OMEGI = 0.
   msg Velocity (U1) profile
   msg Green line --- PHOENICS solution
   msg crosses ---   analytical solution
   da 1 u1 x 3;da 1 uana x 3
   col9 1;blb4 2

   msg press  to end
   pause
   end
   END_USE
   DISPLAY

   The case considered is the same as case 823, except that the
   simulation is performed two-dimensionally with convection
   present. Therefore, the case considered is the 1d tangential
   laminar flow of an incompressible fluid between two coaxial
   cylinders of radius RADI and RADO, the outer one of which is
   rotating with an angular velocity of OMEGO. This case provides
   a test, for NX>1, of the U1 radial diffusion terms and the wall
   boundary treatment with RINNER=0. The analyical solution for the
   tangential velocity is U1=OMEGO*GRADO**2*(GRADI**2-GR**2)/[GR*
   (GRADI**2-GRADO**2)] where GR is the radius.

   ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(2D U1 Flow In An Annulus;Omegi=0.0      )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 14
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = F
 NX = 5
 XULAST =0.087266
 XFRAC(1)=0.2 ;XFRAC(2)=0.4
 XFRAC(3)=0.6 ;XFRAC(4)=0.8
 XFRAC(5)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 10
 YVLAST =0.05
 RINNER =0.05 ;SNALFA =0.
 YFRAC(1)=0.1 ;YFRAC(2)=0.2
 YFRAC(3)=0.3 ;YFRAC(4)=0.4
 YFRAC(5)=0.5 ;YFRAC(6)=0.6
 YFRAC(7)=0.7 ;YFRAC(8)=0.8
 YFRAC(9)=0.9 ;YFRAC(10)=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)=UANA
    * 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(UANA,Y,N,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)
 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 =1000. ;TMP1 =0.
 EL1 =0.
 TSURR =0. ;TEMP0 =0.
 PRESS0 =0.
 DVO1DT =0. ;DRH1DP =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =1.0E-06 ;ENUT =0.
 PRNDTL(U1)=1. ;PRNDTL(V1)=1.
 PRT(U1)=1. ;PRT(V1)=1.
 CP1 =1. ;CP2 =1.
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 ************************************************************
  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=1.0E-10 ;FIINIT(U1)=31.415928
 FIINIT(V1)=1.0E-10 ;FIINIT(UANA)=1.0E-10
 
 PATCH(IN1 ,INIVAL, 1, 5, 1, 1, 1, 1, 1, 1)
 INIT(IN1 ,UANA,0. ,0.204453 )
 
 PATCH(IN2 ,INIVAL, 1, 5, 2, 2, 1, 1, 1, 1)
 INIT(IN2 ,UANA,0. ,0.587341 )
 
 PATCH(IN3 ,INIVAL, 1, 5, 3, 3, 1, 1, 1, 1)
 INIT(IN3 ,UANA,0. ,0.942478 )
 
 PATCH(IN4 ,INIVAL, 1, 5, 4, 4, 1, 1, 1, 1)
 INIT(IN4 ,UANA,0. ,1.27603 )
 
 PATCH(IN5 ,INIVAL, 1, 5, 5, 5, 1, 1, 1, 1)
 INIT(IN5 ,UANA,0. ,1.592463 )
 
 PATCH(IN6 ,INIVAL, 1, 5, 6, 6, 1, 1, 1, 1)
 INIT(IN6 ,UANA,0. ,1.89509 )
 
 PATCH(IN7 ,INIVAL, 1, 5, 7, 7, 1, 1, 1, 1)
 INIT(IN7 ,UANA,0. ,2.186421 )
 
 PATCH(IN8 ,INIVAL, 1, 5, 8, 8, 1, 1, 1, 1)
 INIT(IN8 ,UANA,0. ,2.468394 )
 
 PATCH(IN9 ,INIVAL, 1, 5, 9, 9, 1, 1, 1, 1)
 INIT(IN9 ,UANA,0. ,2.742526 )
 
 PATCH(IN10 ,INIVAL, 1, 5, 10, 10, 1, 1, 1, 1)
 INIT(IN10 ,UANA,0. ,3.010021 )
 INIADD = F
 FSWEEP = 1
 IURINI = -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(INLET1 ,WEST , 1, 1, 1, 1, 1, 1, 1, 1)
 COVAL(INLET1 ,P1 , FIXFLU ,204.452972 )
 COVAL(INLET1 ,U1 ,0. ,0.204453 )
 
 PATCH(INLET2 ,WEST , 1, 1, 2, 2, 1, 1, 1, 1)
 COVAL(INLET2 ,P1 , FIXFLU ,587.341187 )
 COVAL(INLET2 ,U1 ,0. ,0.587341 )
 
 PATCH(INLET3 ,WEST , 1, 1, 3, 3, 1, 1, 1, 1)
 COVAL(INLET3 ,P1 , FIXFLU ,942.477661 )
 COVAL(INLET3 ,U1 ,0. ,0.942478 )
 
 PATCH(INLET4 ,WEST , 1, 1, 4, 4, 1, 1, 1, 1)
 COVAL(INLET4 ,P1 , FIXFLU ,1276.029541 )
 COVAL(INLET4 ,U1 ,0. ,1.27603 )
 
 PATCH(INLET5 ,WEST , 1, 1, 5, 5, 1, 1, 1, 1)
 COVAL(INLET5 ,P1 , FIXFLU ,1592.462769 )
 COVAL(INLET5 ,U1 ,0. ,1.592463 )
 
 PATCH(INLET6 ,WEST , 1, 1, 6, 6, 1, 1, 1, 1)
 COVAL(INLET6 ,P1 , FIXFLU ,1895.089844 )
 COVAL(INLET6 ,U1 ,0. ,1.89509 )
 
 PATCH(INLET7 ,WEST , 1, 1, 7, 7, 1, 1, 1, 1)
 COVAL(INLET7 ,P1 , FIXFLU ,2186.421143 )
 COVAL(INLET7 ,U1 ,0. ,2.186421 )
 
 PATCH(INLET8 ,WEST , 1, 1, 8, 8, 1, 1, 1, 1)
 COVAL(INLET8 ,P1 , FIXFLU ,2468.394287 )
 COVAL(INLET8 ,U1 ,0. ,2.468394 )
 
 PATCH(INLET9 ,WEST , 1, 1, 9, 9, 1, 1, 1, 1)
 COVAL(INLET9 ,P1 , FIXFLU ,2742.525635 )
 COVAL(INLET9 ,U1 ,0. ,2.742526 )
 
 PATCH(INLET10 ,WEST , 1, 1, 10, 10, 1, 1, 1, 1)
 COVAL(INLET10 ,P1 , FIXFLU ,3010.02124 )
 COVAL(INLET10 ,U1 ,0. ,3.010021 )
 
 PATCH(OUTER ,NWALL , 1, 5, 10, 10, 1, 1, 1, 1)
 COVAL(OUTER ,U1 ,1. ,3.141593 )
 
 PATCH(INNER ,SWALL , 1, 5, 1, 1, 1, 1, 1, 1)
 COVAL(INNER ,U1 ,1. ,0. )
 
 PATCH(OUT ,EAST , 5, 5, 1, 10, 1, 1, 1, 1)
 COVAL(OUT ,P1 ,10. ,0. )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 40 ;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
 ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
 ENDIT(V1)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(U1,FALSDT,100.)
 RELAX(V1,FALSDT,100.)
 RELAX(UANA,LINRLX,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(UANA)=1.0E+10 ;VARMIN(UANA)=-1.0E+10
 ************************************************************
  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(UANA,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 3 ;IZMON = 1
 NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = 12345
 UWATCH = T ;USTEER = T
 HIGHLO = F
 ************************************************************
  Group 23.Field Print-Out & Plot Control
 NPRINT = 40 ;NUMCLS = 5
 NXPRIN = -1 ;IXPRF = 1 ;IXPRL = 10000
 NYPRIN = 1 ;IYPRF = 1 ;IYPRL = 10000
 IPLTF = 1 ;IPLTL = 40 ;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