TALK=T;RUN(1,1)
  PHOTON USE
  p




  gr ou x 1
  MSG Velocity vectors
  vec x 1 sh
  msg
  msg Press return to plot pressure contours
  pause
  cont p1 x 1 fil;.01
  msg
  msg Type e to End
  ENDUSE
  PHOTON USE
  p




  gr ou x 1
  MSG Velocity vectors
  vec x 1 sh
  msg
  msg Press return to plot pressure contours
  pause
  cont p1 x 1 fil;.01
  msg
  msg Type e to End
  ENDUSE
  PHOTON USE
  p




  gr ou x 1
  MSG Velocity vectors
  vec x 1 sh
  msg
  msg Press return to plot pressure contours
  pause
  cont p1 x 1 fil;.01
  msg
  msg Type e to End
  ENDUSE
  PHOTON USE
  p




  gr ou x 1
  MSG Velocity vectors
  vec x 1 sh
  msg
  msg Press return to plot pressure contours
  pause
  cont p1 x 1 fil;.01
  msg
  msg Type e to End
  ENDUSE
  PHOTON USE
  p




  gr ou x 1
  MSG Velocity vectors
  vec x 1 sh
  msg
  msg Press return to plot pressure contours
  pause
  cont p1 x 1 fil;.01
  msg
  msg Type e to End
  ENDUSE
  PHOTON USE
  p




  gr ou x 1
  MSG Velocity vectors
  vec x 1 sh
  msg
  msg Press return to plot pressure contours
  pause
  cont p1 x 1 fil;.01
  msg
  msg Type e to End
  ENDUSE
  DISPLAY
  This case defines a calculation of the potential flow
  about a half cylinder in a duct in the y-z plane. The
  grid is generated by PIL commands giving a 'shear
  transformation' and is non-orthogonal; so NONORT is set T.

  The potential calculation is contrived by introducing a
  uniform high resistance throughout the flow field. This
  'Darcy' flow is mathematically equivalent to potential
  flow.

  This is done in Group 13 by setting DARCY=T, which
  creates the appropriate PATCH and COVAL settings.  An
  analytical solution exists for this case to which the
  results may be compared (see Milne-Thompson, 1962,
  'Theoretical Hydrodynamics')
  ENDDIS
  DISPLAY
    This case differs from the previous one only in respect of the
  grid used. The grid is generated using the Laplace solver, which
  derives the grid by solving for the grid corner coordinates as
  dependent variables in a set of coupled non-linear equations.
  ENDDIS
  DISPLAY
    This case is similar to 514 except that the grid file now
  represents a half elliptic cylinder of aspect ratio 2:1 with its
  long axis in the z-direction. The grid is generated by
  interpolation with constant z-coordinates and is non-orthogonal
  ENDDIS
  DISPLAY
   Same as case 516 except that a nearly-orthogonal grid is used.
  ENDDIS
  DISPLAY
  Navier Stokes equations over ellipse.
    This case considers creeping flow over the ellipse: the
  Reynolds number is 1.0. The is done by de-activating the
  Darcy formulation used for the potential-flow simulations in
  the preceding cases, and restoring solution for v1 and w1
  ENDDIS
  DISPLAY
  Navier Stokes equations over ellipse.
    The high Reynolds number flow over an ellipse using a nearly-.
  orthogonal grid generated by MAGIC is considered in this case.
  The Reynolds number is 1.25E6
  ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(FLOW OVER ELLIPSE;MAGIC GRID:       B519)
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 518
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 1
 XULAST =1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 10
 YVLAST =1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 20
 ZWLAST =2.
 ************************************************************
  Group 6. Body-Fitted Coordinates
 BFC = T ;NONORT = T
 NCRT = -1
 RSTGEO = F ;SAVGEO = F
 UUP = F ;VUP = F ;WUP = F
 NGEOM =CHAM
 NAMXYZ =CHAM
 ANGMIN =20.
 DOMAIN(   1,   1,   1,  11,   1,  21)
    * Set fixed sub-domain
 FIXDOM(   1,   0,   0,   0,   0,   0,   0)
 FIXDOM(   2,   0,   0,   0,   0,   0,   0)
 FIXDOM(   3,   0,   0,   0,   0,   0,   0)
 FIXDOM(   4,   0,   0,   0,   0,   0,   0)
 FIXDOM(   5,   0,   0,   0,   0,   0,   0)
 FIXDOM(   6,   0,   0,   0,   0,   0,   0)
 FIXDOM(   7,   0,   0,   0,   0,   0,   0)
 FIXDOM(   8,   0,   0,   0,   0,   0,   0)
 FIXDOM(   9,   0,   0,   0,   0,   0,   0)
 FIXDOM(  10,   0,   0,   0,   0,   0,   0)
 MSWP = 5
 LIJ = F ;LJK = T ;LIK = F
 SLIDS = F ;SLIDN = T
 IMON = 1 ;JMON = 6 ;KMON = 11
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(5)=V1
 NAME(7)=W1 ;NAME(148)=WCRT
 NAME(149)=VCRT ;NAME(150)=UCRT
    * 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(V1,Y,Y,Y,N,N,N)
 SOLUTN(W1,Y,Y,Y,N,N,N)
 SOLUTN(WCRT,Y,N,N,N,N,N)
 SOLUTN(VCRT,Y,N,N,N,N,N)
 SOLUTN(UCRT,Y,N,N,N,N,N)
 ************************************************************
  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(V1,Y,Y,Y,N,N,N)
 TERMS(W1,Y,Y,Y,N,N,N)
 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 =1.0E-06 ;ENUT =0.
 PRNDTL(V1)=1. ;PRNDTL(W1)=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(V1)=1.0E-10
 FIINIT(W1)=1.25 ;FIINIT(WCRT)=1.0E-10
 FIINIT(VCRT)=1.0E-10 ;FIINIT(UCRT)=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(INLET ,LOW , 1, 1, 1, 10, 1, 1, 1, 1)
 COVAL(INLET ,P1 , FIXFLU ,1.25 )
 COVAL(INLET ,V1 ,0. ,0. )
 COVAL(INLET ,W1 ,0. ,1.25 )
 
 PATCH(OUTLET ,HIGH , 1, 1, 1, 10, 20, 20, 1, 1)
 COVAL(OUTLET ,P1 ,1. ,0. )
 COVAL(OUTLET ,V1 ,0. ,0. )
 COVAL(OUTLET ,W1 ,0. ,0. )
 
 PATCH(DARCY ,PHASEM, 0, 0, 0, 0, 0, 0, 1, 1)
 COVAL(DARCY ,V1 ,0. ,0. )
 COVAL(DARCY ,W1 ,0. ,0. )
 
 PATCH(WALL ,SWALL , 1, 1, 1, 1, 5, 16, 1, 1)
 COVAL(WALL ,W1 ,1. ,0. )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 200 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-05
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(V1)=2
 LITER(W1)=2
 ENDIT(P1)=1.0E-03 ;ENDIT(V1)=1.0E-03
 ENDIT(W1)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,0.5)
 RELAX(V1,FALSDT,1.0E-02)
 RELAX(W1,FALSDT,1.0E-02)
 RELAX(WCRT,LINRLX,1.)
 RELAX(VCRT,LINRLX,1.)
 RELAX(UCRT,LINRLX,1.)
 OVRRLX =0.
 EXPERT = F ;NNORSL = F
 ************************************************************
  Group 18. Limits
 VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-1.0E+10
 VARMAX(V1)=1.0E+06 ;VARMIN(V1)=-1.0E+06
 VARMAX(W1)=1.0E+06 ;VARMIN(W1)=-1.0E+06
 VARMAX(WCRT)=1.0E+10 ;VARMIN(WCRT)=-1.0E+10
 VARMAX(VCRT)=1.0E+10 ;VARMIN(VCRT)=-1.0E+10
 VARMAX(UCRT)=1.0E+10 ;VARMIN(UCRT)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 SYMBFC = T
 PARSOL = F
 ISG62 = 1
 SPEDAT(SET,GXMONI,PLOTALL,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,N,N,Y,Y,N,N)
 OUTPUT(V1,N,N,Y,Y,N,N)
 OUTPUT(W1,N,N,Y,Y,N,N)
 OUTPUT(WCRT,Y,N,Y,N,N,N)
 OUTPUT(VCRT,Y,N,Y,N,N,N)
 OUTPUT(UCRT,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 3 ;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
 NYPRIN = -1 ;IYPRF = 1 ;IYPRL = 10000
 NZPRIN = -1 ;IZPRF = 5 ;IZPRL = 15
 XZPR = F ;YZPR = F
 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
 
 PATCH(YZ ,CONTUR, 1, 1, 1, 10, 1, 20, 1, 1)
 PLOT(YZ ,P1 ,0. ,20. )
 PLOT(YZ ,W1 ,0. ,20. )
 
 PATCH(INNER ,PROFIL, 1, 1, 1, 1, 1, 20, 1, 1)
 PLOT(INNER ,P1 ,0. ,0. )
 PLOT(INNER ,W1 ,0. ,0. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP