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

   cl
   msg 2D U1 CORIOLIS/DIFFUSION TEST:RINNER=0
   msg Velocity (U1) profile
   msg Green line --- PHOENICS solution
   msg crosses ---   analytical solution
   da 1 u1 x 5;da 1 uana x 5
   col9 1;blb4 2
   scale x 1 2;redraw

   msg press  to end
   pause
   end
   END_USE
  DISPLAY

  The case considered is the same as case 826, except that RINNER=0
  with the inner cylinder represented through porosities. Therefore,
  the case considered is 1d radial laminar flow of a swirling fluid
  between two porous coaxial cylinders of radius RADI and RADO, the
  outer one of which is rotating with an angular velocity of OMEGO
  and the inner one with angular velocity OMEGI. This case provides,
  for NX > 1 and RINNER=0, a test of the U1 equation for: radial
  convection and diffusion; cyclic boundary conditions; wall
  friction; and coriolis forces. The analyical solution for the
  tangential velocity is: U=A/R+B*R**(1.+REYM) where the Reynolds
  number REYM=VIN*RADI/ENUL and the constants A and B are given by:
  B=(OMEGI*RADI**2-OMEGO*RADO**2)/(RADI**(2.+REYM)-RADO**(2.+REYM)
  and A=OMEGI*RADI**2-B*RADI**(2.+REYM).

  ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(2D U1 Coriolis/Diffusion Test:Rinner=0  )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 14
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = F
 NX = 10
 XULAST =1.
 XFRAC(1)=0.1 ;XFRAC(2)=0.2
 XFRAC(3)=0.3 ;XFRAC(4)=0.4
 XFRAC(5)=0.5 ;XFRAC(6)=0.6
 XFRAC(7)=0.7 ;XFRAC(8)=0.8
 XFRAC(9)=0.9 ;XFRAC(10)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 22
 YVLAST =2.
 YFRAC(1)=0.25 ;YFRAC(2)=0.5
 YFRAC(3)=0.561411 ;YFRAC(4)=0.599763
 YFRAC(5)=0.632506 ;YFRAC(6)=0.662066
 YFRAC(7)=0.689465 ;YFRAC(8)=0.715256
 YFRAC(9)=0.739783 ;YFRAC(10)=0.763276
 YFRAC(11)=0.785903 ;YFRAC(12)=0.807786
 YFRAC(13)=0.829021 ;YFRAC(14)=0.849684
 YFRAC(15)=0.869836 ;YFRAC(16)=0.889528
 YFRAC(17)=0.908802 ;YFRAC(18)=0.927694
 YFRAC(19)=0.946235 ;YFRAC(20)=0.964451
 YFRAC(21)=0.982366 ;YFRAC(22)=1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 1
 ZWLAST =1.
 ZFRAC(1)=1.
 ************************************************************
  Group 6. Body-Fitted Coordinates
    * X-cyclic boundaries switched
 XCYIZ( 1, T )
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(3)=U1
 NAME(5)=V1 ;NAME(148)=PRPS
 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(PRPS,Y,N,N,N,N,N)
 SOLUTN(UANA,Y,N,N,N,N,Y)
 PRPS = 148
 ************************************************************
  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 =1. ;TMP1 =0.
 EL1 =0.
 TSURR =0. ;TEMP0 =0.
 PRESS0 =0.
 DVO1DT =0. ;DRH1DP =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =1. ;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(PRPS)=-1.
 FIINIT(UANA)=1.0E-10
 
 PATCH(BLK1 ,INIVAL, 1, 10, 1, 2, 1, 1, 1, 1)
 INIT(BLK1 ,PRPS,0. ,199. )
 
 PATCH(IN1 ,INIVAL, 1, 10, 1, 1, 1, 1, 1, 1)
 INIT(IN1 ,UANA,0. ,125.663712 )
 
 PATCH(IN2 ,INIVAL, 1, 10, 2, 2, 1, 1, 1, 1)
 INIT(IN2 ,UANA,0. ,41.887905 )
 
 PATCH(IN3 ,INIVAL, 1, 10, 3, 3, 1, 1, 1, 1)
 INIT(IN3 ,UANA,0. ,29.598257 )
 
 PATCH(IN4 ,INIVAL, 1, 10, 4, 4, 1, 1, 1, 1)
 INIT(IN4 ,UANA,0. ,27.055302 )
 
 PATCH(IN5 ,INIVAL, 1, 10, 5, 5, 1, 1, 1, 1)
 INIT(IN5 ,UANA,0. ,25.494383 )
 
 PATCH(IN6 ,INIVAL, 1, 10, 6, 6, 1, 1, 1, 1)
 INIT(IN6 ,UANA,0. ,24.267443 )
 
 PATCH(IN7 ,INIVAL, 1, 10, 7, 7, 1, 1, 1, 1)
 INIT(IN7 ,UANA,0. ,23.24472 )
 
 PATCH(IN8 ,INIVAL, 1, 10, 8, 8, 1, 1, 1, 1)
 INIT(IN8 ,UANA,0. ,22.364599 )
 
 PATCH(IN9 ,INIVAL, 1, 10, 9, 9, 1, 1, 1, 1)
 INIT(IN9 ,UANA,0. ,21.591373 )
 
 PATCH(IN10 ,INIVAL, 1, 10, 10, 10, 1, 1, 1, 1)
 INIT(IN10 ,UANA,0. ,20.902229 )
 
 PATCH(IN11 ,INIVAL, 1, 10, 11, 11, 1, 1, 1, 1)
 INIT(IN11 ,UANA,0. ,20.282188 )
 
 PATCH(IN12 ,INIVAL, 1, 10, 12, 12, 1, 1, 1, 1)
 INIT(IN12 ,UANA,0. ,19.722651 )
 
 PATCH(IN13 ,INIVAL, 1, 10, 13, 13, 1, 1, 1, 1)
 INIT(IN13 ,UANA,0. ,19.223127 )
 
 PATCH(IN14 ,INIVAL, 1, 10, 14, 14, 1, 1, 1, 1)
 INIT(IN14 ,UANA,0. ,18.79812 )
 
 PATCH(IN15 ,INIVAL, 1, 10, 15, 15, 1, 1, 1, 1)
 INIT(IN15 ,UANA,0. ,18.494398 )
 
 PATCH(IN16 ,INIVAL, 1, 10, 16, 16, 1, 1, 1, 1)
 INIT(IN16 ,UANA,0. ,18.429964 )
 
 PATCH(IN17 ,INIVAL, 1, 10, 17, 17, 1, 1, 1, 1)
 INIT(IN17 ,UANA,0. ,18.877596 )
 
 PATCH(IN18 ,INIVAL, 1, 10, 18, 18, 1, 1, 1, 1)
 INIT(IN18 ,UANA,0. ,20.437458 )
 
 PATCH(IN19 ,INIVAL, 1, 10, 19, 19, 1, 1, 1, 1)
 INIT(IN19 ,UANA,0. ,24.383095 )
 
 PATCH(IN20 ,INIVAL, 1, 10, 20, 20, 1, 1, 1, 1)
 INIT(IN20 ,UANA,0. ,33.336716 )
 
 PATCH(IN21 ,INIVAL, 1, 10, 21, 21, 1, 1, 1, 1)
 INIT(IN21 ,UANA,0. ,52.555031 )
 
 PATCH(IN22 ,INIVAL, 1, 10, 22, 22, 1, 1, 1, 1)
 INIT(IN22 ,UANA,0. ,92.323524 )
 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(INLET ,SOUTH , 1, 10, 3, 3, 1, 1, 1, 1)
 COVAL(INLET ,P1 , FIXFLU ,40. )
 COVAL(INLET ,U1 ,0. ,31.415928 )
 COVAL(INLET ,V1 ,0. ,40. )
 
 PATCH(OUTLET ,NORTH , 1, 10, 22, 22, 1, 1, 1, 1)
 COVAL(OUTLET ,P1 ,1. ,0. )
 
 PATCH(INNER ,SWALL , 1, 10, 3, 3, 1, 1, 1, 1)
 COVAL(INNER ,U1 ,1. ,31.415928 )
 
 PATCH(OUTER ,NWALL , 1, 10, 22, 22, 1, 1, 1, 1)
 COVAL(OUTER ,U1 ,1. ,125.663712 )
 XCYCLE = T
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 40 ;ISWC1 = 1
 LITHYD = 2 ;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,1.)
 RELAX(V1,FALSDT,1.)
 RELAX(PRPS,LINRLX,1.)
 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(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
 VARMAX(UANA)=1.0E+10 ;VARMIN(UANA)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 PARSOL = F
 ISG62 = 1
 SPEDAT(SET,MATERIAL,199,L,T)
 ************************************************************
  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(PRPS,Y,N,Y,N,N,N)
 OUTPUT(UANA,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 10 ;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 = 2
 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