KE_PIPE FLOW OF A BINGHAM FLUID: T305


TALK=T;RUN(1,1)
  DISPLAY
  The problem concerns the steady fully-developed turbulent flow
  of a Bingham-plastic non-Newtonian fluid. This type of fluid
  remains rigid when the shearing stress is less than the yield
  stress tauy and flows somewhat like a Newtonian fluid when the
  shearing stress exceeds tauy. The turbulence is simulated by the
  high-Reynolds number k-e model plus wall functions, although the
  user might like to try the low-Reynolds-number k-e model because
  the laminar viscosity varies rapidly in the near-wall layer due
  to the rapid increase in the rate of strain as the wall is
  approached.
  ENDDIS
   AUTOPLOT USE
   file
   phi 5

   da 1 w1
   col9 1
   msg Velocity (W1) profile
   msg Press RETURN to continue
   pause

   clear;da 1 ke
   col9 1
   msg KE profile
   msg Press e to END
   ENDUSE
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  Group 1. Run Title and Number
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 TEXT(KE_PIPE FLOW OF A BINGHAM FLUID: T305   )
 
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 IRUNN = 1 ;LIBREF = 14
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  Group 2. Time dependence
 STEADY = T
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  Group 3. X-Direction Grid Spacing
 CARTES = F
 NX = 1
 XULAST =1.
 XFRAC(1)=1.
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  Group 4. Y-Direction Grid Spacing
 NY = 20
 YVLAST =0.1
 YFRAC(1)=0.083234 ;YFRAC(2)=0.144918
 YFRAC(3)=0.200445 ;YFRAC(4)=0.252317
 YFRAC(5)=0.30163 ;YFRAC(6)=0.348996
 YFRAC(7)=0.3948 ;YFRAC(8)=0.43931
 YFRAC(9)=0.482718 ;YFRAC(10)=0.525169
 YFRAC(11)=0.566778 ;YFRAC(12)=0.607637
 YFRAC(13)=0.647819 ;YFRAC(14)=0.687387
 YFRAC(15)=0.726394 ;YFRAC(16)=0.764883
 YFRAC(17)=0.802894 ;YFRAC(18)=0.84046
 YFRAC(19)=0.877611 ;YFRAC(20)=1.
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  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 1
 ZWLAST =0.1
 ZFRAC(1)=1.
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  Group 6. Body-Fitted Coordinates
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  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(7)=W1 ;NAME(12)=KE
 NAME(13)=EP ;NAME(146)=LEN1
 NAME(147)=ENUT ;NAME(148)=GENK
 NAME(149)=BTAU ;NAME(150)=VISL
    * Y in SOLUTN argument list denotes:
    * 1-stored 2-solved 3-whole-field
    * 4-point-by-point 5-explicit 6-harmonic averaging 
 SOLUTN(W1,Y,Y,N,N,N,Y)
 SOLUTN(KE,Y,Y,N,N,N,N)
 SOLUTN(EP,Y,Y,N,N,N,N)
 SOLUTN(LEN1,Y,N,N,N,N,Y)
 SOLUTN(ENUT,Y,N,N,N,N,Y)
 SOLUTN(GENK,Y,N,N,N,N,Y)
 SOLUTN(BTAU,Y,N,N,N,N,Y)
 SOLUTN(VISL,Y,N,N,N,N,Y)
 VISL = 150
 VIST = 147
 LEN1 = 146
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  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(W1,N,N,Y,Y,Y,Y)
 TERMS(KE,Y,N,Y,Y,Y,N)
 TERMS(EP,Y,N,Y,Y,Y,N)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 NEWENL = T
 NEWENT = T
 USOURC = T
 ISOLX = -1 ;ISOLY = -1 ;ISOLZ = -1
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  Group 9. Properties used if PRPS is not
  stored, and where PRPS = -1.0 if it is!
 RHO1 =1. ;TMP1 =0. ;EL1 = GRND4
 TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
 DVO1DT =0. ;DRH1DP =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 EL1A =0. ;EL1B =0. ;EL1C =0.
 ENUL = GRND5 ;ENUT = GRND3
 ENULA =6.666667E-06 ;ENULB =1.666667E-04 ;ENULC =0. ;ENULD =0.
 ENULE =0. ;ENULF =0. ;ENULG =0.
 IENULA = 0 ;IENULB = 0
 ENUTA =0. ;ENUTB =0. ;ENUTC =0.
 IENUTA = 0
 PRNDTL(W1)=1. ;PRNDTL(KE)=1.
 PRNDTL(EP)=1.
 PRT(W1)=1. ;PRT(KE)=1.
 PRT(EP)=1.314
 CP1 =1. ;CP2 =1.
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  Group 10.Inter-Phase Transfer Processes
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  Group 11.Initial field variables (PHIs)
 FIINIT(W1)=1. ;FIINIT(KE)=1.0E-10
 FIINIT(EP)=1.0E-10 ;FIINIT(LEN1)=1.0E-10
 FIINIT(ENUT)=1.0E-10 ;FIINIT(GENK)=1.0E-10
 FIINIT(BTAU)=1.0E-10 ;FIINIT(VISL)=1.0E-10
   No PATCHes yet used for this Group
 INIADD = F
 FSWEEP = 1
 NAMFI =CHAM
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  Group 12. Patchwise adjustment of terms
  Patches for this group are printed with those
  for Group 13.
  Their names begin either with GP12 or &
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  Group 13. Boundary & Special Sources
 
 PATCH(KESOURCE,PHASEM, 0, 0, 0, 0, 0, 0, 1, 1)
 COVAL(KESOURCE,KE , GRND4 , GRND4 )
 COVAL(KESOURCE,EP , GRND4 , GRND4 )
 
 PATCH(WALLN ,NWALL , 1, 1, 20, 20, 1, 1, 1, 1)
 COVAL(WALLN ,W1 , GRND2 ,0. )
 COVAL(WALLN ,KE , GRND2 , GRND2 )
 COVAL(WALLN ,EP , GRND2 , GRND2 )
 
 PATCH(FDFW1DP ,VOLUME, 1, 1, 1, 20, 1, 1, 1, 1)
 COVAL(FDFW1DP ,W1 ,5.0E-03 , GRND1 )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
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  Group 14. Downstream Pressure For PARAB
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  Group 15. Terminate Sweeps
 LSWEEP = 10 ;ISWC1 = 1
 LITHYD = 50 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-05
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  Group 16. Terminate Iterations
 LITER(W1)=10 ;LITER(KE)=20
 LITER(EP)=20
 ENDIT(W1)=1.0E-03 ;ENDIT(KE)=1.0E-03
 ENDIT(EP)=1.0E-03
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  Group 17. Relaxation
 RELAX(W1,FALSDT,0.1)
 RELAX(KE,FALSDT,0.1)
 RELAX(EP,FALSDT,0.1)
 RELAX(LEN1,LINRLX,1.)
 RELAX(ENUT,LINRLX,1.)
 RELAX(GENK,LINRLX,1.)
 RELAX(BTAU,LINRLX,1.)
 RELAX(VISL,LINRLX,1.)
 KELIN = 0
 OVRRLX =0.
 EXPERT = F ;NNORSL = F
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  Group 18. Limits
 VARMAX(W1)=1.0E+06 ;VARMIN(W1)=-1.0E+06
 VARMAX(KE)=1.0E+10 ;VARMIN(KE)=1.0E-10
 VARMAX(EP)=1.0E+10 ;VARMIN(EP)=1.0E-10
 VARMAX(LEN1)=1.0E+10 ;VARMIN(LEN1)=-1.0E+10
 VARMAX(ENUT)=1.0E+10 ;VARMIN(ENUT)=-1.0E+10
 VARMAX(GENK)=1.0E+10 ;VARMIN(GENK)=-1.0E+10
 VARMAX(BTAU)=1.0E+10 ;VARMIN(BTAU)=-1.0E+10
 VARMAX(VISL)=1.0E+10 ;VARMIN(VISL)=-1.0E+10
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  Group 19. Data transmitted to GROUND
 DWDY = T
 GENK = T
 FDFSOL = T
 PARSOL = F
 ISG62 = 1
 SPEDAT(SET,GXMONI,PLOTALL,L,T)
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  Group 20. Preliminary Printout
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  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(W1,Y,N,Y,Y,Y,Y)
 OUTPUT(KE,Y,N,Y,Y,Y,Y)
 OUTPUT(EP,Y,N,Y,Y,Y,Y)
 OUTPUT(LEN1,Y,N,Y,N,N,N)
 OUTPUT(ENUT,Y,N,Y,N,N,N)
 OUTPUT(GENK,Y,N,Y,N,N,N)
 OUTPUT(BTAU,Y,N,Y,N,N,N)
 OUTPUT(VISL,Y,N,N,Y,Y,Y)
 WALPRN = T
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  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 20 ;IZMON = 1
 NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = -1
 UWATCH = T ;USTEER = T
 HIGHLO = F
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  Group 23.Field Print-Out & Plot Control
 NPRINT = 100000 ;NUMCLS = 5
 NYPRIN = 1 ;IYPRF = 1 ;IYPRL = 10000
 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 = 2 ;NCOLCO = 45 ;NROWCO = 20
   No PATCHes yet used for this Group
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  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP