TALK=T;RUN(1,1)
  PHOTON USE
  * dump xxx0 means no gravity source
  * dump xxxg means  gravity source linked to calculated salt
  * dump xxxh means  gravity source linked to calculated salt
  *                  with fixv salt source at outer boundary
  * dump xxxi means  gravity source linked to calculated salt
  *                  with fixv salt source at patch whole
  p
  parphi
  3 4 1




  msg        Axi-symmetrical turbulent jet with Ys multiplied by 4
  msg        Velocity vectors:
  vec x 1 sh
  vec x 8 sh
  dump velveci; vec off;red
  msg        average salt contours:
  con salt x 1 fi;0.1
  con salt x 8 fi;0.1;dump salti; con off;red
  msg        average mixl contours:
  con mixl x 1 fi;0.1
  con mixl x 8 fi;0.1;dump mixli; con off;red
  msg        concentration contours:
  con conc x 1 fi;0.1
  con conc x 8 fi;0.1; dump conci; con off;red
  msg        average f contours:
  con avef x 1 fi;0.1
  con avef x 8 fi;0.1; dump avefi; con off;red
  msg        root-mean-square fluctuation contours:
  con mnsq x 1 fi;0.1
  con mnsq x 8 fi;0.1; dump mnsqi; con off;red
  msg        f1 contours:
  con f1 x 1 fi;0.1
  con f1 x 8 fi;0.1; dump f1i; con off;red
  msg        f5 contours:
  con f5 x 1 fi;0.1
  con f5 x 8 fi;0.1; dump f5i; con off;red
  msg        f10 contours:
  con f10 x 1 fi;0.1
  con f10 x 8 fi;0.1; dump f10i; con off;red
  msg        eddy-viscosity (enut) contours:
  con enut x 1 fi;0.1
  con enut x 8 fi;0.1 ; dump enuti; con off;red
  enduse
  DISPLAY
     The development of the wake downstream of an underwater
     vessel, the propulsion system of which creates an
     axi-symmetrical jet of velocity greater than that of the
     vessel.

     The jet does not remain axi-symmetrical as distance from
     the vessel's stern increases, because it is postulated that
     the vessel is moving through density-stratified water. This
     causes mixing in the vertical direction to differ
     significantly from that in the horizontal direction.

     MFM is used for the computation of the turbulence length
     scale and the effective viscosity. Longitudinal velocity is
     used as the sole PDA.

     In-Form is used so as to define the density distribution in
     the undisturbed water.
  ENDDIS
  infrbegin
  debug t
  stored t
  source t
  formula t
  infrend
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(Round Jet; MFM; parabolic               )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 0
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = F
 NX = 12
 XULAST =3.1416
 XFRAC(1)=0.083333 ;XFRAC(2)=0.166667
 XFRAC(3)=0.25 ;XFRAC(4)=0.333333
 XFRAC(5)=0.416667 ;XFRAC(6)=0.5
 XFRAC(7)=0.583333 ;XFRAC(8)=0.666667
 XFRAC(9)=0.75 ;XFRAC(10)=0.833333
 XFRAC(11)=0.916667 ;XFRAC(12)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 20
 YVLAST =10.
 AZYV =1. ;AZRI =0. ;AZAL =0.
   Method of pairs used for grid setting.
 YFRAC(2)=0.05
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = T
 NZ = 100
 ZWADD =200.
 ZWLAST =1.
 AZDZ = GRND2
 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(7)=W1
 NAME(16)=CONC ;NAME(134)=F1
 NAME(135)=F2 ;NAME(136)=F3
 NAME(137)=F4 ;NAME(138)=F5
 NAME(139)=F6 ;NAME(140)=F7
 NAME(141)=F8 ;NAME(142)=F9
 NAME(143)=F10 ;NAME(144)=MNSQ
 NAME(145)=AVEF ;NAME(146)=RATE
 NAME(147)=SALT ;NAME(148)=MIXL
 NAME(149)=RHO1 ;NAME(150)=ENUT
    * 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(W1,Y,Y,N,N,N,Y)
 SOLUTN(CONC,Y,Y,N,N,N,Y)
 SOLUTN(F1,Y,Y,N,N,N,Y)
 SOLUTN(F2,Y,Y,N,N,N,Y)
 SOLUTN(F3,Y,Y,N,N,N,Y)
 SOLUTN(F4,Y,Y,N,N,N,Y)
 SOLUTN(F5,Y,Y,N,N,N,Y)
 SOLUTN(F6,Y,Y,N,N,N,Y)
 SOLUTN(F7,Y,Y,N,N,N,Y)
 SOLUTN(F8,Y,Y,N,N,N,Y)
 SOLUTN(F9,Y,Y,N,N,N,Y)
 SOLUTN(F10,Y,Y,N,N,N,Y)
 SOLUTN(MNSQ,Y,N,N,N,N,Y)
 SOLUTN(AVEF,Y,N,N,N,N,Y)
 SOLUTN(RATE,Y,N,N,N,N,Y)
 SOLUTN(SALT,Y,Y,N,N,N,Y)
 SOLUTN(MIXL,Y,Y,N,N,N,Y)
 SOLUTN(RHO1,Y,N,N,N,N,Y)
 SOLUTN(ENUT,Y,N,N,N,N,Y)
 DEN1 = 149
 VIST = 150
 ************************************************************
  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)
 TERMS(CONC,N,Y,Y,Y,Y,Y)
 TERMS(F1,N,Y,Y,Y,Y,Y)
 TERMS(F2,N,Y,Y,Y,N,Y)
 TERMS(F3,N,Y,Y,Y,Y,Y)
 TERMS(F4,N,Y,Y,Y,N,Y)
 TERMS(F5,N,Y,Y,Y,Y,Y)
 TERMS(F6,N,Y,Y,Y,N,Y)
 TERMS(F7,N,Y,Y,Y,Y,Y)
 TERMS(F8,N,Y,Y,Y,N,Y)
 TERMS(F9,N,Y,Y,Y,Y,Y)
 TERMS(F10,N,Y,Y,Y,N,Y)
 TERMS(SALT,N,Y,Y,Y,N,Y)
 TERMS(MIXL,N,Y,Y,Y,Y,Y)
 DIFCUT =0. ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 NEWENT = T
 ISOLX = -1 ;ISOLY = -1 ;ISOLZ = -1
 ************************************************************
  Group 9. Properties used if PRPS is not
  stored, and where PRPS = -1.0 if it is!
 RHO1 =1025. ;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-05 ;ENUT = GRND10
 ENUTA =0. ;ENUTB =0. ;ENUTC =0.
 IENUTA = 0
 PRNDTL(U1)=1. ;PRNDTL(V1)=1.
 PRNDTL(W1)=1. ;PRNDTL(CONC)=1.
 PRNDTL(F1)=1. ;PRNDTL(F2)=1.
 PRNDTL(F3)=1. ;PRNDTL(F4)=1.
 PRNDTL(F5)=1. ;PRNDTL(F6)=1.
 PRNDTL(F7)=1. ;PRNDTL(F8)=1.
 PRNDTL(F9)=1. ;PRNDTL(F10)=1.
 PRNDTL(SALT)=1. ;PRNDTL(MIXL)=1.
 PRT(U1)=1. ;PRT(V1)=1.
 PRT(W1)=1. ;PRT(CONC)=1.
 PRT(F1)=1. ;PRT(F2)=1.
 PRT(F3)=1. ;PRT(F4)=1.
 PRT(F5)=1. ;PRT(F6)=1.
 PRT(F7)=1. ;PRT(F8)=1.
 PRT(F9)=1. ;PRT(F10)=1.
 PRT(SALT)=1. ;PRT(MIXL)=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
 FIINIT(CONC)=1.0E-10 ;FIINIT(F1)=1.0E-10
 FIINIT(F2)=1.0E-10 ;FIINIT(F3)=1.0E-10
 FIINIT(F4)=1.0E-10 ;FIINIT(F5)=1.0E-10
 FIINIT(F6)=1.0E-10 ;FIINIT(F7)=1.0E-10
 FIINIT(F8)=1.0E-10 ;FIINIT(F9)=1.0E-10
 FIINIT(F10)=1.0E-10 ;FIINIT(MNSQ)=1.0E-10
 FIINIT(AVEF)=1.0E-10 ;FIINIT(RATE)=1.0E-10
 FIINIT(SALT)=1.0E-10 ;FIINIT(MIXL)=10.
 FIINIT(RHO1)=1.0E-10 ;FIINIT(ENUT)=1.0E-10
 
 PATCH(START2 ,INIVAL, 1, 12, 11, 20, 1, 1, 1, 1)
 INIT(START2 ,F10 ,0. ,1. )
 
 PATCH(START1 ,INIVAL, 1, 1, 1, 10, 1, 1, 1, 1)
 INIT(START1 ,F1 ,0. ,1. )
 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(FREE ,NORTH , 1, 12, 20, 20, 1, 100, 1, 1)
 COVAL(FREE ,P1 , FIXFLU ,384.375031 )
 COVAL(FREE ,V1 ,0. ,0. )
 COVAL(FREE ,W1 ,0. ,5. )
 COVAL(FREE ,CONC,0. ,0. )
 COVAL(FREE ,F1 ,0. ,0. )
 COVAL(FREE ,F2 ,0. ,0. )
 COVAL(FREE ,F3 ,0. ,0. )
 COVAL(FREE ,F4 ,0. ,0. )
 COVAL(FREE ,F5 ,0. ,0. )
 COVAL(FREE ,F6 ,0. ,0. )
 COVAL(FREE ,F7 ,0. ,0. )
 COVAL(FREE ,F8 ,0. ,0. )
 COVAL(FREE ,F9 ,0. ,0. )
 COVAL(FREE ,F10 ,0. ,1. )
 COVAL(FREE ,SALT,In-Form:source - see Grp 19)
 
 PATCH(UPSTJET ,LOW , 1, 12, 1, 10, 1, 1, 1, 1)
 COVAL(UPSTJET ,P1 , FIXFLU ,1.025E+04 )
 COVAL(UPSTJET ,W1 ,0. ,10. )
 COVAL(UPSTJET ,CONC,0. ,1. )
 COVAL(UPSTJET ,F1 ,0. ,1. )
 COVAL(UPSTJET ,F2 ,0. ,0. )
 COVAL(UPSTJET ,F3 ,0. ,0. )
 COVAL(UPSTJET ,F4 ,0. ,0. )
 COVAL(UPSTJET ,F5 ,0. ,0. )
 COVAL(UPSTJET ,F6 ,0. ,0. )
 COVAL(UPSTJET ,F7 ,0. ,0. )
 COVAL(UPSTJET ,F8 ,0. ,0. )
 COVAL(UPSTJET ,F9 ,0. ,0. )
 COVAL(UPSTJET ,F10 ,0. ,0. )
 COVAL(UPSTJET ,SALT,0. , SAME )
 
 PATCH(UPSTFREE,LOW , 1, 12, 11, 20, 1, 1, 1, 1)
 COVAL(UPSTFREE,P1 , FIXFLU ,5125. )
 COVAL(UPSTFREE,W1 ,0. ,5. )
 COVAL(UPSTFREE,CONC,0. ,0. )
 COVAL(UPSTFREE,F1 ,0. ,0. )
 COVAL(UPSTFREE,F2 ,0. ,0. )
 COVAL(UPSTFREE,F3 ,0. ,0. )
 COVAL(UPSTFREE,F4 ,0. ,0. )
 COVAL(UPSTFREE,F5 ,0. ,0. )
 COVAL(UPSTFREE,F6 ,0. ,0. )
 COVAL(UPSTFREE,F7 ,0. ,0. )
 COVAL(UPSTFREE,F8 ,0. ,0. )
 COVAL(UPSTFREE,F9 ,0. ,0. )
 COVAL(UPSTFREE,F10 ,0. ,0. )
 COVAL(UPSTFREE,SALT,0. , SAME )
 
 PATCH($MNSQ ,PHASEM, 1, 12, 1, 20, 1, 100, 1, 1)
 COVAL($MNSQ ,MIXL,5.0E-06 ,1.0E+05 )
 
 PATCH(WHOLE ,PHASEM, 1, 12, 1, 20, 1, 100, 1, 1)
 COVAL(WHOLE ,U1 ,In-Form:source - see Grp 19)
 COVAL(WHOLE ,V1 ,In-Form:source - see Grp 19)
 COVAL(WHOLE ,SALT,In-Form:source - see Grp 19)
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 IPARAB = 0
 AZPH =0. ;PBAR =0.
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 1 ;ISWC1 = 1
 LITHYD = 100 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-03
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=100 ;LITER(U1)=10
 LITER(V1)=10 ;LITER(W1)=10
 LITER(CONC)=20 ;LITER(F1)=20
 LITER(F2)=20 ;LITER(F3)=20
 LITER(F4)=20 ;LITER(F5)=20
 LITER(F6)=20 ;LITER(F7)=20
 LITER(F8)=20 ;LITER(F9)=20
 LITER(F10)=20 ;LITER(SALT)=20
 LITER(MIXL)=20
 ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
 ENDIT(V1)=1.0E-03 ;ENDIT(W1)=1.0E-03
 ENDIT(CONC)=1.0E-03 ;ENDIT(F1)=1.0E-03
 ENDIT(F2)=1.0E-03 ;ENDIT(F3)=1.0E-03
 ENDIT(F4)=1.0E-03 ;ENDIT(F5)=1.0E-03
 ENDIT(F6)=1.0E-03 ;ENDIT(F7)=1.0E-03
 ENDIT(F8)=1.0E-03 ;ENDIT(F9)=1.0E-03
 ENDIT(F10)=1.0E-03 ;ENDIT(SALT)=1.0E-03
 ENDIT(MIXL)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,0.5)
 RELAX(U1,FALSDT,1.0E-02)
 RELAX(V1,FALSDT,1.)
 RELAX(W1,FALSDT,10.)
 RELAX(CONC,FALSDT,1.0E+09)
 RELAX(F1,LINRLX,0.5)
 RELAX(F2,LINRLX,0.5)
 RELAX(F3,LINRLX,0.5)
 RELAX(F4,LINRLX,0.5)
 RELAX(F5,LINRLX,0.5)
 RELAX(F6,LINRLX,0.5)
 RELAX(F7,LINRLX,0.5)
 RELAX(F8,LINRLX,0.5)
 RELAX(F9,LINRLX,0.5)
 RELAX(F10,LINRLX,0.5)
 RELAX(MNSQ,LINRLX,1.)
 RELAX(AVEF,LINRLX,1.)
 RELAX(RATE,LINRLX,1.)
 RELAX(SALT,LINRLX,0.1)
 RELAX(MIXL,FALSDT,1.0E+09)
 RELAX(RHO1,LINRLX,1.)
 RELAX(ENUT,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)=1000. ;VARMIN(V1)=-1000.
 VARMAX(W1)=1.0E+06 ;VARMIN(W1)=-1.0E+06
 VARMAX(CONC)=1.0E+10 ;VARMIN(CONC)=-1.0E+10
 VARMAX(F1)=1. ;VARMIN(F1)=0.
 VARMAX(F2)=1. ;VARMIN(F2)=0.
 VARMAX(F3)=1. ;VARMIN(F3)=0.
 VARMAX(F4)=1. ;VARMIN(F4)=0.
 VARMAX(F5)=1. ;VARMIN(F5)=0.
 VARMAX(F6)=1. ;VARMIN(F6)=0.
 VARMAX(F7)=1. ;VARMIN(F7)=0.
 VARMAX(F8)=1. ;VARMIN(F8)=0.
 VARMAX(F9)=1. ;VARMIN(F9)=0.
 VARMAX(F10)=1. ;VARMIN(F10)=0.
 VARMAX(MNSQ)=1. ;VARMIN(MNSQ)=0.
 VARMAX(AVEF)=1. ;VARMIN(AVEF)=0.
 VARMAX(RATE)=1.0E+10 ;VARMIN(RATE)=-1.0E+10
 VARMAX(SALT)=1.0E+10 ;VARMIN(SALT)=-1.0E+10
 VARMAX(MIXL)=1.0E+10 ;VARMIN(MIXL)=-1.0E+10
 VARMAX(RHO1)=1.0E+10 ;VARMIN(RHO1)=-1.0E+10
 VARMAX(ENUT)=1.0E+10 ;VARMIN(ENUT)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 PARSOL = F
 DZW1 =0.1
 ISG62 = 1
 SPEDAT(SET,PROPERTY,RHO1,C,=SALT)
 SPEDAT(SET,INITIAL,SALT,C,=1027.+0.5*(TANH(YG*COS(XG)/YVLAST)+1)*$)
 SPEDAT(SET,INITIAL,SALT,C,(1023.-1027.))
 SPEDAT(SET,SOURCE,SALT!FREE,C,=1027.+0.5*(TANH(YG*COS(XG)/YVLAST)$)
 SPEDAT(SET,SOURCE,SALT!FREE,C,+1)*(1023.-1027.)!FIXVAL)
 SPEDAT(SET,SOURCE,U1!WHOLE,C,=9.81*(RHO1-1025.)*SIN(XU))
 SPEDAT(SET,SOURCE,V1!WHOLE,C,=9.81*(RHO1-1025.)*COS(XG))
 SPEDAT(SET,SOURCE,SALT!WHOLE,C,=1027.+0.5*(TANH(YG*COS(XG)/YVLAST$)
 SPEDAT(SET,SOURCE,SALT!WHOLE,C,)+1)*(1023.-1027.)!FIXVAL)
 SPEDAT(SET,MFM,MFMMOD,C,MNSQ)
 SPEDAT(SET,MFM,NFLUIDS,I,10)
 SPEDAT(SET,MFM,NFLR,I,1)
 SPEDAT(SET,MFM,NFLF,I,10)
 SPEDAT(SET,MFM,CONMIX,R,5.)
 SPEDAT(SET,MFM,VISCON,R,10.)
 SPEDAT(SET,MFM,POPMIN,R,5.)
 SPEDAT(SET,MFM,POPMAX,R,10.)
 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,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)
 OUTPUT(CONC,Y,N,Y,Y,Y,Y)
 OUTPUT(F1,Y,N,Y,Y,Y,Y)
 OUTPUT(F2,Y,N,Y,Y,Y,Y)
 OUTPUT(F3,Y,N,Y,Y,Y,Y)
 OUTPUT(F4,Y,N,Y,Y,Y,Y)
 OUTPUT(F5,Y,N,Y,Y,Y,Y)
 OUTPUT(F6,Y,N,Y,Y,Y,Y)
 OUTPUT(F7,Y,N,Y,Y,Y,Y)
 OUTPUT(F8,Y,N,Y,Y,Y,Y)
 OUTPUT(F9,Y,N,Y,Y,Y,Y)
 OUTPUT(F10,Y,N,Y,Y,Y,Y)
 OUTPUT(MNSQ,Y,N,Y,N,N,N)
 OUTPUT(AVEF,Y,N,Y,N,N,N)
 OUTPUT(RATE,Y,N,Y,N,N,N)
 OUTPUT(SALT,Y,N,Y,Y,Y,Y)
 OUTPUT(MIXL,Y,N,Y,Y,Y,Y)
 OUTPUT(RHO1,Y,N,Y,N,N,N)
 OUTPUT(ENUT,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 1 ;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 = 4 ;IYPRF = 1 ;IYPRL = 10000
 NZPRIN = 100 ;IZPRF = 1 ;IZPRL = 10000
 IPLTF = 1 ;IPLTL = 30 ;NPLT = 1
 ISWPRF = 1 ;ISWPRL = 100000
 ITABL = 1 ;IPROF = 1
 ABSIZ =0.5 ;ORSIZ =0.2
 NTZPRF = 1 ;NCOLPF = 50
 ICHR = 2 ;NCOLCO = 45 ;NROWCO = 20
 
 PATCH(IZEQNZ ,PROFIL, 1, 1, 1, 20, 100, 100, 1, 1)
 PLOT(IZEQNZ ,W1 ,0. ,0. )
 PLOT(IZEQNZ ,CONC,0. ,0. )
 PLOT(IZEQNZ ,ENUT,0. ,0. )
 
 PATCH(MIDDLE ,PROFIL, 1, 12, 10, 10, 1, 100, 1, 1)
 PLOT(MIDDLE ,F1 ,0. ,0. )
 PLOT(MIDDLE ,F4 ,0. ,0. )
 PLOT(MIDDLE ,F7 ,0. ,0. )
 PLOT(MIDDLE ,F10 ,0. ,0. )
 
 PATCH(PROF1 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF1 ,F1 ,0. ,0. )
 
 PATCH(PROF2 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF2 ,F2 ,0. ,0. )
 
 PATCH(PROF3 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF3 ,F3 ,0. ,0. )
 
 PATCH(PROF4 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF4 ,F4 ,0. ,0. )
 
 PATCH(PROF5 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF5 ,F5 ,0. ,0. )
 
 PATCH(PROF6 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF6 ,F6 ,0. ,0. )
 
 PATCH(PROF7 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF7 ,F7 ,0. ,0. )
 
 PATCH(PROF8 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF8 ,F8 ,0. ,0. )
 
 PATCH(PROF9 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF9 ,F9 ,0. ,0. )
 
 PATCH(PROF10 ,PROFIL, 1, 1, 1, 20, 1, 100, 1, 1)
 PLOT(PROF10 ,F10 ,0. ,0. )
 
 PATCH(FINAL ,PROFIL, 1, 1, 1, 20, 100, 100, 1, 1)
 PLOT(FINAL ,W1 ,0. ,0. )
 PLOT(FINAL ,MNSQ,0. ,0. )
 PLOT(FINAL ,MIXL,0. ,0. )
 PLOT(FINAL ,ENUT,0. ,0. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
 IDISPA = 1 ;IDISPB = 0 ;IDISPC = 0
STOP