TALK=T;RUN(1,1)
DISPLAY
The problem considered is the submerged free turbulent plane
jet in stagnant surroundings. The jet issues from a slot H
at a Reynolds number of 14,000. The calculation exploits
symmetry, and is carried out with the elliptic solver for a
domain which is 30H long by 7.5H wide.
Calculations are performed with the standard k-e & the Chen-Kim,
RNG and Realisable k-e variants. Simulations are also made with
the 1988 & 2008 Wilcox k-w models, the Menter k-w model and the
k-w SST variant. The experimental data indicate a velocity half-
width spreading rate of 0.11 in the self-similar region of
the jet. The present calculations predict the following
half-width spreading rates:
data KE CK RNG RKE KW KWR KWM SST
dy/dz 0.11 0.099 0.076 0.119 0.099 0.115 0.106 0.106 0.102
The Realisable, RNG & standard k-e models produce fairly good
agreement with the data, and likewise with the Wilcox 2008,
Menter and k-w-SST models. However, the Chen-Kim k-e model
significantly underestimates the jet spreading, and the Wilcox
1988 k-w model with the default model constants produces an
excessive spreading rate. The value reported above for the
Wilcox 1988 model was obtained with a 30% reduction in the
value of C2w in the w-equation. It should be mentioned that the
results reported here have not been subjected to a grid-sensitivi$
ty
test. The half-width spreading rate is calculated approximately
using In-Form commands and then written to the text-output file
named inforout.
ENDDIS
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************
TEXT(Realisable KE_2D Elliptic Plane Jet )
************************************************************
************************************************************
IRUNN = 1 ;LIBREF = 14
************************************************************
Group 2. Time dependence
STEADY = T
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = T
NX = 1
XULAST =1.
XFRAC(1)=1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 60
YVLAST =0.1875
YFRAC(1)=6.666667E-03 ;YFRAC(2)=0.013333
YFRAC(3)=0.02 ;YFRAC(4)=0.026667
YFRAC(5)=0.033333 ;YFRAC(6)=0.04
YFRAC(7)=0.046667 ;YFRAC(8)=0.053333
YFRAC(9)=0.06 ;YFRAC(10)=0.066667
YFRAC(11)=0.07278 ;YFRAC(12)=0.079138
YFRAC(13)=0.085751 ;YFRAC(14)=0.092628
YFRAC(15)=0.09978 ;YFRAC(16)=0.107218
YFRAC(17)=0.114953 ;YFRAC(18)=0.122998
YFRAC(19)=0.131365 ;YFRAC(20)=0.140066
YFRAC(21)=0.149116 ;YFRAC(22)=0.158527
YFRAC(23)=0.168315 ;YFRAC(24)=0.178495
YFRAC(25)=0.189081 ;YFRAC(26)=0.200092
YFRAC(27)=0.211542 ;YFRAC(28)=0.223451
YFRAC(29)=0.235835 ;YFRAC(30)=0.248716
YFRAC(31)=0.262111 ;YFRAC(32)=0.276042
YFRAC(33)=0.290531 ;YFRAC(34)=0.305599
YFRAC(35)=0.32127 ;YFRAC(36)=0.337568
YFRAC(37)=0.354517 ;YFRAC(38)=0.372145
YFRAC(39)=0.390477 ;YFRAC(40)=0.409543
YFRAC(41)=0.429372 ;YFRAC(42)=0.449994
YFRAC(43)=0.47144 ;YFRAC(44)=0.493745
YFRAC(45)=0.516941 ;YFRAC(46)=0.541066
YFRAC(47)=0.566155 ;YFRAC(48)=0.592248
YFRAC(49)=0.619385 ;YFRAC(50)=0.647607
YFRAC(51)=0.676958 ;YFRAC(52)=0.707484
YFRAC(53)=0.73923 ;YFRAC(54)=0.772246
YFRAC(55)=0.806583 ;YFRAC(56)=0.842293
YFRAC(57)=0.879431 ;YFRAC(58)=0.918055
YFRAC(59)=0.958224 ;YFRAC(60)=1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 120
ZWLAST =0.75
ZFRAC(1)=4.347098E-03 ;ZFRAC(2)=8.737667E-03
ZFRAC(3)=0.013172 ;ZFRAC(4)=0.017651
ZFRAC(5)=0.022175 ;ZFRAC(6)=0.026743
ZFRAC(7)=0.031358 ;ZFRAC(8)=0.036019
ZFRAC(9)=0.040726 ;ZFRAC(10)=0.04548
ZFRAC(11)=0.050282 ;ZFRAC(12)=0.055132
ZFRAC(13)=0.06003 ;ZFRAC(14)=0.064978
ZFRAC(15)=0.069975 ;ZFRAC(16)=0.075022
ZFRAC(17)=0.080119 ;ZFRAC(18)=0.085267
ZFRAC(19)=0.090467 ;ZFRAC(20)=0.095719
ZFRAC(21)=0.101023 ;ZFRAC(22)=0.10638
ZFRAC(23)=0.111791 ;ZFRAC(24)=0.117256
ZFRAC(25)=0.122776 ;ZFRAC(26)=0.128351
ZFRAC(27)=0.133981 ;ZFRAC(28)=0.139668
ZFRAC(29)=0.145412 ;ZFRAC(30)=0.151213
ZFRAC(31)=0.157073 ;ZFRAC(32)=0.16299
ZFRAC(33)=0.168967 ;ZFRAC(34)=0.175004
ZFRAC(35)=0.181101 ;ZFRAC(36)=0.187259
ZFRAC(37)=0.193479 ;ZFRAC(38)=0.199761
ZFRAC(39)=0.206106 ;ZFRAC(40)=0.212514
ZFRAC(41)=0.218986 ;ZFRAC(42)=0.225523
ZFRAC(43)=0.232125 ;ZFRAC(44)=0.238794
ZFRAC(45)=0.245529 ;ZFRAC(46)=0.252331
ZFRAC(47)=0.259201 ;ZFRAC(48)=0.266141
ZFRAC(49)=0.273149 ;ZFRAC(50)=0.280228
ZFRAC(51)=0.287377 ;ZFRAC(52)=0.294598
ZFRAC(53)=0.301891 ;ZFRAC(54)=0.309257
ZFRAC(55)=0.316697 ;ZFRAC(56)=0.324211
ZFRAC(57)=0.3318 ;ZFRAC(58)=0.339465
ZFRAC(59)=0.347207 ;ZFRAC(60)=0.355026
ZFRAC(61)=0.362923 ;ZFRAC(62)=0.3709
ZFRAC(63)=0.378956 ;ZFRAC(64)=0.387092
ZFRAC(65)=0.39531 ;ZFRAC(66)=0.403611
ZFRAC(67)=0.411994 ;ZFRAC(68)=0.420461
ZFRAC(69)=0.429012 ;ZFRAC(70)=0.43765
ZFRAC(71)=0.446373 ;ZFRAC(72)=0.455184
ZFRAC(73)=0.464083 ;ZFRAC(74)=0.473071
ZFRAC(75)=0.482149 ;ZFRAC(76)=0.491317
ZFRAC(77)=0.500578 ;ZFRAC(78)=0.50993
ZFRAC(79)=0.519377 ;ZFRAC(80)=0.528918
ZFRAC(81)=0.538554 ;ZFRAC(82)=0.548287
ZFRAC(83)=0.558117 ;ZFRAC(84)=0.568045
ZFRAC(85)=0.578072 ;ZFRAC(86)=0.5882
ZFRAC(87)=0.598429 ;ZFRAC(88)=0.608761
ZFRAC(89)=0.619195 ;ZFRAC(90)=0.629734
ZFRAC(91)=0.640379 ;ZFRAC(92)=0.65113
ZFRAC(93)=0.661988 ;ZFRAC(94)=0.672955
ZFRAC(95)=0.684032 ;ZFRAC(96)=0.695219
ZFRAC(97)=0.706518 ;ZFRAC(98)=0.717931
ZFRAC(99)=0.729457 ;ZFRAC(100)=0.741099
ZFRAC(101)=0.752857 ;ZFRAC(102)=0.764732
ZFRAC(103)=0.776727 ;ZFRAC(104)=0.788841
ZFRAC(105)=0.801077 ;ZFRAC(106)=0.813435
ZFRAC(107)=0.825916 ;ZFRAC(108)=0.838522
ZFRAC(109)=0.851255 ;ZFRAC(110)=0.864114
ZFRAC(111)=0.877102 ;ZFRAC(112)=0.890221
ZFRAC(113)=0.90347 ;ZFRAC(114)=0.916852
ZFRAC(115)=0.930367 ;ZFRAC(116)=0.944018
ZFRAC(117)=0.957805 ;ZFRAC(118)=0.97173
ZFRAC(119)=0.985795 ;ZFRAC(120)=1.
************************************************************
Group 6. Body-Fitted Coordinates
************************************************************
Group 7. Variables: STOREd,SOLVEd,NAMEd
ONEPHS = T
NAME(1)=P1 ;NAME(5)=V1
NAME(7)=W1 ;NAME(12)=KE
NAME(13)=EP ;NAME(137)=YH3D
NAME(138)=ZGM ;NAME(139)=YH
NAME(140)=YGP ;NAME(141)=WH
NAME(142)=LEN1 ;NAME(143)=C1E
NAME(144)=DWDZ ;NAME(145)=DWDY
NAME(146)=DVDZ ;NAME(147)=DVDY
NAME(148)=EPKE ;NAME(149)=CMU
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,Y,N,N,Y)
SOLUTN(V1,Y,Y,N,N,N,N)
SOLUTN(W1,Y,Y,N,N,N,N)
SOLUTN(KE,Y,Y,N,N,N,N)
SOLUTN(EP,Y,Y,N,N,N,N)
SOLUTN(YH3D,Y,N,N,N,N,N)
SOLUTN(ZGM,Y,N,N,N,N,N)
SOLUTN(YH,Y,N,N,N,N,N)
SOLUTN(YGP,Y,N,N,N,N,N)
SOLUTN(WH,Y,N,N,N,N,N)
SOLUTN(LEN1,Y,N,N,N,N,Y)
SOLUTN(C1E,Y,N,N,N,N,Y)
SOLUTN(DWDZ,Y,N,N,N,N,N)
SOLUTN(DWDY,Y,N,N,N,N,N)
SOLUTN(DVDZ,Y,N,N,N,N,N)
SOLUTN(DVDY,Y,N,N,N,N,N)
SOLUTN(EPKE,Y,N,N,N,N,N)
SOLUTN(CMU,Y,N,N,N,N,N)
SOLUTN(ENUT,Y,N,N,N,N,Y)
VIST = 150
LEN1 = 142
************************************************************
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,Y,Y,Y)
TERMS(W1,Y,Y,Y,Y,Y,Y)
TERMS(KE,N,Y,Y,Y,Y,N)
TERMS(EP,N,Y,Y,Y,Y,N)
DIFCUT =0.5 ;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 =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 =3.571429E-05 ;ENUT = GRND5
ENUTA =0. ;ENUTB =0. ;ENUTC =0.
IENUTA = 14
PRNDTL(V1)=1. ;PRNDTL(W1)=1.
PRNDTL(KE)=1. ;PRNDTL(EP)=1.
PRT(V1)=1. ;PRT(W1)=1.
PRT(KE)=1. ;PRT(EP)=1.2
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)=1.0E-02 ;FIINIT(KE)=0.25
FIINIT(EP)=16.429998 ;FIINIT(YH3D)=1.0E-10
FIINIT(ZGM)=1.0E-10 ;FIINIT(YH)=1.0E-10
FIINIT(YGP)=1.0E-10 ;FIINIT(WH)=1.0E-10
FIINIT(LEN1)=1.0E-10 ;FIINIT(C1E)=1.0E-10
FIINIT(DWDZ)=1.0E-10 ;FIINIT(DWDY)=1.0E-10
FIINIT(DVDZ)=1.0E-10 ;FIINIT(DVDY)=1.0E-10
FIINIT(EPKE)=1.0E-10 ;FIINIT(CMU)=0.09
FIINIT(ENUT)=1.0E-10
PATCH(INIT ,INIVAL, 1, 1, 1, 10, 1, 120, 1, 1)
INIT(INIT ,W1 ,0. ,10. )
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(KESOURCE,PHASEM, 0, 0, 0, 0, 0, 0, 1, 1)
COVAL(KESOURCE,KE , GRND4 , GRND4 )
PATCH(REKESO ,PHASEM, 0, 0, 0, 0, 0, 0, 1, 1)
COVAL(REKESO ,EP , GRND4 , GRND4 )
PATCH(IN1 ,LOW , 1, 1, 1, 10, 1, 1, 1, 1)
COVAL(IN1 ,P1 , FIXFLU ,10. )
COVAL(IN1 ,V1 ,0. ,0. )
COVAL(IN1 ,W1 ,0. ,10. )
COVAL(IN1 ,KE ,0. ,0.25 )
COVAL(IN1 ,EP ,0. ,16.429998 )
PATCH(IN2 ,LOW , 1, 1, 11, 60, 1, 1, 1, 1)
COVAL(IN2 ,P1 , FIXFLU ,1.0E-02 )
COVAL(IN2 ,V1 ,0. ,0. )
COVAL(IN2 ,W1 ,0. ,1.0E-02 )
COVAL(IN2 ,KE ,0. ,2.5E-07 )
COVAL(IN2 ,EP ,0. ,1.575E-10 )
PATCH(FREEB ,NORTH , 1, 1, 60, 60, 1, 120, 1, 1)
COVAL(FREEB ,P1 ,1.0E+04 ,0. )
COVAL(FREEB ,W1 ,0. ,1.0E-02 )
COVAL(FREEB ,KE ,0. ,2.5E-07 )
COVAL(FREEB ,EP ,0. ,1.575E-10 )
PATCH(OUT ,HIGH , 1, 1, 1, 60, 120, 120, 1, 1)
COVAL(OUT ,P1 ,1.0E+04 ,0. )
COVAL(OUT ,V1 ,0. ,0. )
COVAL(OUT ,W1 ,0. ,0. )
COVAL(OUT ,KE ,0. ,0. )
COVAL(OUT ,EP ,0. ,0. )
PATCH(HWIDTH ,CELL , 1, 1, 1, 60, 1, 119, 1, 1)
PATCH(HWIDTH1 ,CELL , 1, 1, 2, 59, 90, 90, 1, 1)
PATCH(HWIDTH2 ,CELL , 1, 1, 2, 59, 119, 119, 1, 1)
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 1000 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =1.0E-04
************************************************************
Group 16. Terminate Iterations
LITER(P1)=20 ;LITER(V1)=10
LITER(W1)=10 ;LITER(KE)=20
LITER(EP)=20
ENDIT(P1)=1.0E-03 ;ENDIT(V1)=1.0E-03
ENDIT(W1)=1.0E-03 ;ENDIT(KE)=1.0E-03
ENDIT(EP)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(V1,FALSDT,5.0E-03)
RELAX(W1,FALSDT,5.0E-03)
RELAX(KE,FALSDT,5.0E-03)
RELAX(EP,FALSDT,5.0E-03)
RELAX(YH3D,LINRLX,1.)
RELAX(ZGM,LINRLX,1.)
RELAX(YH,LINRLX,1.)
RELAX(YGP,LINRLX,1.)
RELAX(WH,LINRLX,1.)
RELAX(LEN1,LINRLX,1.)
RELAX(C1E,LINRLX,1.)
RELAX(DWDZ,LINRLX,1.)
RELAX(DWDY,LINRLX,1.)
RELAX(DVDZ,LINRLX,1.)
RELAX(DVDY,LINRLX,1.)
RELAX(EPKE,LINRLX,1.)
RELAX(CMU,LINRLX,1.)
RELAX(ENUT,LINRLX,0.2)
KELIN = 3
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(KE)=1.0E+10 ;VARMIN(KE)=1.0E-10
VARMAX(EP)=1.0E+10 ;VARMIN(EP)=1.0E-10
VARMAX(YH3D)=1.0E+10 ;VARMIN(YH3D)=-1.0E+10
VARMAX(ZGM)=1.0E+10 ;VARMIN(ZGM)=-1.0E+10
VARMAX(YH)=1.0E+10 ;VARMIN(YH)=-1.0E+10
VARMAX(YGP)=1.0E+10 ;VARMIN(YGP)=-1.0E+10
VARMAX(WH)=1.0E+10 ;VARMIN(WH)=-1.0E+10
VARMAX(LEN1)=1.0E+10 ;VARMIN(LEN1)=-1.0E+10
VARMAX(C1E)=1.0E+10 ;VARMIN(C1E)=-1.0E+10
VARMAX(DWDZ)=1.0E+10 ;VARMIN(DWDZ)=-1.0E+10
VARMAX(DWDY)=1.0E+10 ;VARMIN(DWDY)=-1.0E+10
VARMAX(DVDZ)=1.0E+10 ;VARMIN(DVDZ)=-1.0E+10
VARMAX(DVDY)=1.0E+10 ;VARMIN(DVDY)=-1.0E+10
VARMAX(EPKE)=1.0E+10 ;VARMIN(EPKE)=-1.0E+10
VARMAX(CMU)=1.0E+10 ;VARMIN(CMU)=-1.0E+10
VARMAX(ENUT)=0.1 ;VARMIN(ENUT)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
GENK = T
PARSOL = F
IENUTA = 14
ISG62 = 1
SPEDAT(SET,KECONST,C2E,R,1.9)
SPEDAT(SET,STORED,WH,C,=0.5*W1[&1&]!ZSLFIN)
SPEDAT(SET,STORED,YGP,C,=YG!ZSLFIN)
SPEDAT(SET,STORED,YH,C,=0.0!ZSLFIN)
SPEDAT(SET,STORED,YH!HWIDTH,C,=YGP!IF(W1.GE.WH.AND.W1[&+1&].LE.WH$)
SPEDAT(SET,STORED,YH!HWIDTH,C,)!ZSLFIN)
SPEDAT(SET,MAKE,YH1,C,=1.E-10)
SPEDAT(SET,STORED,YH1!HWIDTH1,C,=MAX(YH&1.1E-10)!ZSLFIN)
SPEDAT(SET,PRINT,YH1,C,=YH1)
SPEDAT(SET,MAKE,YH2,C,=1.E-10)
SPEDAT(SET,STORED,YH2!HWIDTH2,C,=MAX(YH&1.1E-10)!ZSLFIN)
SPEDAT(SET,PRINT,YH2,C,=YH2)
SPEDAT(SET,MAKE,DYHDZ,C,=1.E-10)
SPEDAT(SET,STORED,ZGM,C,=ZG!ZSLFIN)
SPEDAT(SET,STORED,DYHDZ,C,=(YH2-YH1)/(ZGM[&1&NZ-1]-ZGM[&1&90])!ZS$)
SPEDAT(SET,STORED,DYHDZ,C,LFIN)
SPEDAT(SET,PRINT,DYHDZ,C,=DYHDZ)
SPEDAT(SET,MAKE,YH0D,C,=0)
SPEDAT(SET,STORED,YH0D!HWIDTH,C,=YGP!IF(W1.GE.WH.AND.W1[&+1&].LE.$)
SPEDAT(SET,STORED,YH0D!HWIDTH,C,WH)!ZSLFIN)
SPEDAT(SET,STORED,YH3D,C,=YH0D!ZSLFIN)
SPEDAT(SET,GXMONI,PLOTALL,L,T)
************************************************************
Group 20. Preliminary Printout
DISTIL = T ;NULLPR = F
NDST = 0
DSTTOL =1.0E-02
EX(P1)=0.08042 ;EX(V1)=0.1931
EX(W1)=2.548 ;EX(KE)=1.038
EX(EP)=59.27 ;EX(YH3D)=0.02861
EX(ZGM)=0.3021 ;EX(YH)=4.69E-04
EX(YGP)=0.06195 ;EX(WH)=4.051
EX(LEN1)=0.0481 ;EX(C1E)=0.6296
EX(DWDZ)=5.43 ;EX(DWDY)=88.300003
EX(DVDZ)=1.44 ;EX(DVDY)=5.612
EX(EPKE)=27.01 ;EX(CMU)=0.06639
EX(ENUT)=3.312E-03
************************************************************
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(V1,Y,N,Y,Y,Y,Y)
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(YH3D,Y,N,Y,N,N,N)
OUTPUT(ZGM,Y,N,Y,N,N,N)
OUTPUT(YH,Y,N,Y,N,N,N)
OUTPUT(YGP,Y,N,Y,N,N,N)
OUTPUT(WH,Y,N,Y,N,N,N)
OUTPUT(LEN1,Y,N,Y,N,N,N)
OUTPUT(C1E,Y,N,Y,N,Y,Y)
OUTPUT(DWDZ,Y,N,Y,N,N,N)
OUTPUT(DWDY,Y,N,Y,N,N,N)
OUTPUT(DVDZ,Y,N,Y,N,N,N)
OUTPUT(DVDY,Y,N,Y,N,N,N)
OUTPUT(EPKE,Y,N,Y,N,N,N)
OUTPUT(CMU,Y,N,Y,N,Y,Y)
OUTPUT(ENUT,Y,N,Y,N,N,N)
************************************************************
Group 22. Monitor Print-Out
IXMON = 1 ;IYMON = 12 ;IZMON = 119
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 = 1 ;IZPRL = 10000
XZPR = F ;YZPR = F
IPLTF = 1 ;IPLTL = -1 ;NPLT = 10
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(IY1 ,PROFIL, 1, 1, 1, 1, 1, 119, 1, 1)
PLOT(IY1 ,W1 ,0. ,0. )
PLOT(IY1 ,KE ,0. ,0. )
PLOT(IY1 ,YH3D,0. ,0. )
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP