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TALK=T;RUN(1,1)
DISPLAY
A long, hollow, thick-walled cylinder, immersed in an outer fluid,
contains a second fluid having a different pressure.

Since conditions vary with radius alone, nx and nz are set = 1 .

Two constraints on its length are considered, namely:
1. the cylinder length may extend freely; and
2. the cylinder length may not extend at all.

To enable the computed stresses and strains to be compared with
theoretical (text-book) values, the latter have been computed.

So as to make comparison easy, variables named P1/T etc have also
been computed. They represent the calculated values divided by
text-book ones. They should all be, and indeed are, close to 1.0;
but zero is printed when the text-book value is zero

Parameters which may be changed by editing this file include:
(a) Material properties:  Young's modulus and Poisson's ratio
(b) Geometric quantities: inner and outer radius, and length.
(d) The grid fineness (via NYCYL)
(e) The grid-fineness distribution (via POWER)

The text-book solution may be found in section 14.4 of Benham,
Crawford and Armstrong, Mechanics of Engineering Materials; and
also in Love's Mathematical Theory of Elasticity p144 .

ENDDIS
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************

TEXT(Pressurised long cylinder; 1Dy          )

************************************************************
************************************************************

IRUNN = 1 ;LIBREF = 0
************************************************************
Group 2. Time dependence
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = F
NX = 1
XULAST =0.2
XFRAC(1)=1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 33
YVLAST =0.808
YFRAC(1)=0.247525 ;YFRAC(2)=0.248297
YFRAC(3)=0.250616 ;YFRAC(4)=0.254479
YFRAC(5)=0.259888 ;YFRAC(6)=0.266842
YFRAC(7)=0.275342 ;YFRAC(8)=0.285388
YFRAC(9)=0.296978 ;YFRAC(10)=0.310114
YFRAC(11)=0.324796 ;YFRAC(12)=0.341023
YFRAC(13)=0.358795 ;YFRAC(14)=0.378113
YFRAC(15)=0.398976 ;YFRAC(16)=0.421384
YFRAC(17)=0.445338 ;YFRAC(18)=0.470838
YFRAC(19)=0.497883 ;YFRAC(20)=0.526473
YFRAC(21)=0.556609 ;YFRAC(22)=0.58829
YFRAC(23)=0.621516 ;YFRAC(24)=0.656288
YFRAC(25)=0.692606 ;YFRAC(26)=0.730468
YFRAC(27)=0.769877 ;YFRAC(28)=0.81083
YFRAC(29)=0.853329 ;YFRAC(30)=0.897374
YFRAC(31)=0.942964 ;YFRAC(32)=0.990099
YFRAC(33)=1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 1
ZWLAST =1.
ZFRAC(1)=1.
************************************************************
Group 6. Body-Fitted Coordinates
************************************************************
Group 7. Variables: STOREd,SOLVEd,NAMEd
ONEPHS = T
NAME(1)=P1 ;NAME(5)=V1
NAME(127)=EZ/T ;NAME(128)=EY/T
NAME(129)=EX/T ;NAME(130)=V1/T
NAME(131)=P1TH ;NAME(132)=V1TH
NAME(133)=EZTH ;NAME(134)=EPSZ
NAME(135)=SZTH ;NAME(136)=STRZ
NAME(137)=EYTH ;NAME(138)=EPSY
NAME(139)=SYTH ;NAME(140)=STRY
NAME(141)=EXTH ;NAME(142)=EPSX
NAME(143)=SXTH ;NAME(144)=STRX
NAME(145)=DRH1 ;NAME(146)=DVO1
NAME(147)=ENUL ;NAME(148)=DEN1
NAME(149)=PRPS ;NAME(150)=DISY
* 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,N,N,N,N,Y)
SOLUTN(V1,Y,Y,N,N,N,Y)
SOLUTN(EZ/T,Y,N,N,N,N,N)
SOLUTN(EY/T,Y,N,N,N,N,N)
SOLUTN(EX/T,Y,N,N,N,N,N)
SOLUTN(V1/T,Y,N,N,N,N,N)
SOLUTN(P1TH,Y,N,N,N,N,N)
SOLUTN(V1TH,Y,N,N,N,N,N)
SOLUTN(EZTH,Y,N,N,N,N,Y)
SOLUTN(EPSZ,Y,N,N,N,N,Y)
SOLUTN(SZTH,Y,N,N,N,N,Y)
SOLUTN(STRZ,Y,N,N,N,N,Y)
SOLUTN(EYTH,Y,N,N,N,N,Y)
SOLUTN(EPSY,Y,N,N,N,N,Y)
SOLUTN(SYTH,Y,N,N,N,N,Y)
SOLUTN(STRY,Y,N,N,N,N,Y)
SOLUTN(EXTH,Y,N,N,N,N,Y)
SOLUTN(EPSX,Y,N,N,N,N,Y)
SOLUTN(SXTH,Y,N,N,N,N,Y)
SOLUTN(STRX,Y,N,N,N,N,Y)
SOLUTN(DRH1,Y,N,N,N,N,Y)
SOLUTN(DVO1,Y,N,N,N,N,Y)
SOLUTN(ENUL,Y,N,N,N,N,Y)
SOLUTN(DEN1,Y,N,N,N,N,Y)
SOLUTN(PRPS,Y,N,N,N,N,Y)
SOLUTN(DISY,Y,Y,N,N,N,Y)
DEN1 = 148
VISL = 147
PRPS = 149
************************************************************
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(V1,Y,Y,Y,Y,Y,Y)
TERMS(DISY,N,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 =0. ;TMP1 =0.
EL1 =0.
TSURR =0. ;TEMP0 =0.
PRESS0 =0.
DVO1DT =3.41E-03 ;DRH1DP =0.
EMISS =0. ;SCATT =0.
ENUL =0. ;ENUT =0.
PRNDTL(V1)=1. ;PRNDTL(DISY)=1.
PRT(V1)=1. ;PRT(DISY)=1.
CP1 =1005. ;CP2 =1.
*  List of user-defined materials to be read by EARTH
MATFLG=T;IMAT=1
*  Name
*Ind. Dens.  Viscos.  Spec.heat  Conduct.  Expans.  Compr.
*
160 7800.0 0.3 473.0 43.0 1.0E-5 0.5E-11
************************************************************
Group 10.Inter-Phase Transfer Processes
************************************************************
Group 11.Initial field variables (PHIs)
FIINIT(P1)=1.0E-10 ;FIINIT(V1)=1.0E-10
FIINIT(EZ/T)=1.0E-10 ;FIINIT(EY/T)=1.0E-10
FIINIT(EX/T)=1.0E-10 ;FIINIT(V1/T)=1.0E-10
FIINIT(P1TH)=1.0E-10 ;FIINIT(V1TH)=1.0E-10
FIINIT(EZTH)=1.001E-10 ;FIINIT(EPSZ)=1.001E-10
FIINIT(SZTH)=1.001E-10 ;FIINIT(STRZ)=1.001E-10
FIINIT(EYTH)=1.001E-10 ;FIINIT(EPSY)=1.001E-10
FIINIT(SYTH)=1.001E-10 ;FIINIT(STRY)=1.001E-10
FIINIT(EXTH)=1.001E-10 ;FIINIT(EPSX)=1.001E-10
FIINIT(SXTH)=1.001E-10 ;FIINIT(STRX)=1.001E-10
FIINIT(DRH1)=1.001E-10 ;FIINIT(DVO1)=1.001E-10
FIINIT(ENUL)=1.001E-10 ;FIINIT(DEN1)=1.001E-10
FIINIT(PRPS)=0. ;FIINIT(DISY)=1.0E-10

PATCH(INNER ,INIVAL, 1, 1, 1, 1, 1, 1, 1, 1)
INIT(INNER ,P1 ,In-Form:initial value - G19)

PATCH(OUTER ,INIVAL, 1, 1, 33, 33, 1, 1, 1, 1)
INIT(OUTER ,P1 ,In-Form:initial value - G19)

PATCH(OB3 ,INIVAL, 1, 1, 2, 32, 1, 1, 1, 1)
INIT(OB3 ,PRPS,0. ,160. )
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(IN ,VOLUME, 1, 1, 1, 1, 1, 1, 1, 1)
COVAL(IN ,P1 ,In-Form:source - see Grp 19)

PATCH(OUT ,VOLUME, 1, 1, 33, 33, 1, 1, 1, 1)
COVAL(OUT ,P1 ,In-Form:source - see Grp 19)
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-04
************************************************************
Group 16. Terminate Iterations
LITER(V1)=10 ;LITER(DISY)=20
ENDIT(V1)=1.0E-03 ;ENDIT(DISY)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(V1,FALSDT,1.)
RELAX(EZ/T,LINRLX,1.)
RELAX(EY/T,LINRLX,1.)
RELAX(EX/T,LINRLX,1.)
RELAX(V1/T,LINRLX,1.)
RELAX(P1TH,LINRLX,1.)
RELAX(V1TH,LINRLX,1.)
RELAX(EZTH,LINRLX,1.)
RELAX(EPSZ,LINRLX,1.)
RELAX(SZTH,LINRLX,1.)
RELAX(STRZ,LINRLX,1.)
RELAX(EYTH,LINRLX,1.)
RELAX(EPSY,LINRLX,1.)
RELAX(SYTH,LINRLX,1.)
RELAX(STRY,LINRLX,1.)
RELAX(EXTH,LINRLX,1.)
RELAX(EPSX,LINRLX,1.)
RELAX(SXTH,LINRLX,1.)
RELAX(STRX,LINRLX,1.)
RELAX(DRH1,LINRLX,1.)
RELAX(DVO1,LINRLX,1.)
RELAX(ENUL,LINRLX,1.)
RELAX(DEN1,LINRLX,1.)
RELAX(PRPS,LINRLX,1.)
RELAX(DISY,FALSDT,1.0E+09)
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(EZ/T)=1.0E+10 ;VARMIN(EZ/T)=-1.0E+10
VARMAX(EY/T)=1.0E+10 ;VARMIN(EY/T)=-1.0E+10
VARMAX(EX/T)=1.0E+10 ;VARMIN(EX/T)=-1.0E+10
VARMAX(V1/T)=1.0E+10 ;VARMIN(V1/T)=-1.0E+10
VARMAX(P1TH)=1.0E+10 ;VARMIN(P1TH)=-1.0E+10
VARMAX(V1TH)=1.0E+10 ;VARMIN(V1TH)=-1.0E+10
VARMAX(EZTH)=1.0E+10 ;VARMIN(EZTH)=-1.0E+10
VARMAX(EPSZ)=1.0E+10 ;VARMIN(EPSZ)=-1.0E+10
VARMAX(SZTH)=1.0E+10 ;VARMIN(SZTH)=-1.0E+10
VARMAX(STRZ)=1.0E+10 ;VARMIN(STRZ)=-1.0E+10
VARMAX(EYTH)=1.0E+10 ;VARMIN(EYTH)=-1.0E+10
VARMAX(EPSY)=1.0E+10 ;VARMIN(EPSY)=-1.0E+10
VARMAX(SYTH)=1.0E+10 ;VARMIN(SYTH)=-1.0E+10
VARMAX(STRY)=1.0E+10 ;VARMIN(STRY)=-1.0E+10
VARMAX(EXTH)=1.0E+10 ;VARMIN(EXTH)=-1.0E+10
VARMAX(EPSX)=1.0E+10 ;VARMIN(EPSX)=-1.0E+10
VARMAX(SXTH)=1.0E+10 ;VARMIN(SXTH)=-1.0E+10
VARMAX(STRX)=1.0E+10 ;VARMIN(STRX)=-1.0E+10
VARMAX(DRH1)=1.0E+10 ;VARMIN(DRH1)=-1.0E+10
VARMAX(DVO1)=1.0E+10 ;VARMIN(DVO1)=-1.0E+10
VARMAX(ENUL)=1.0E+10 ;VARMIN(ENUL)=-1.0E+10
VARMAX(DEN1)=1.0E+10 ;VARMIN(DEN1)=-1.0E+10
VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
VARMAX(DISY)=1.0E+10 ;VARMIN(DISY)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
STRA = T
PARSOL = F
CONWIZ = T
ISG21 = 200
ISG52 = 3
ISG59 = 1
ISG62 = 1
CSG10   ='Q1'
SPEDAT(SET,DOMAIN,PHASE_1_MAT,I,0)
SPEDAT(SET,DOMAIN,PROPS_FILE_1,C,Q1)
SPEDAT(SET,BOUNDARY,XCONST,R,1.0E+20)
SPEDAT(SET,BOUNDARY,ZCONST,R,0.)
SPEDAT(SET,STORED,SYTH,C,=6.666667E+05*(1.0-0.64/RG^2)-0.*(1.0-0.\$)
SPEDAT(SET,STORED,SYTH,C,04/RG^2)!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,SXTH,C,=6.666667E+05*(1.0+0.64/RG^2)-0.*(1.0+0.\$)
SPEDAT(SET,STORED,SXTH,C,04/RG^2)!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,SZTH,C,=0.0!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,EZTH,C,=-5.0E-12!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,V1TH,C,=0.*RV+0./RV!ZSLFIN)
SPEDAT(SET,STORED,EXTH,C,=(SXTH-0.3*(SYTH+SZTH))/2.0E+11!ZSLFIN)
SPEDAT(SET,STORED,EYTH,C,=(SYTH-0.3*(SXTH+SZTH))/2.0E+11!ZSLFIN)
SPEDAT(SET,STORED,P1TH,C,=(EXTH+EYTH+EZTH)!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,V1/T,C,=DISY/V1TH!ZSLFIN)
SPEDAT(SET,STORED,EX/T,C,=EPSX/EXTH!ZSLFIN)
SPEDAT(SET,STORED,EY/T,C,=EPSY/EYTH!ZSLFIN)
SPEDAT(SET,STORED,EZ/T,C,=EPSZ/EZTH!ZSLFIN)
SPEDAT(SET,INITIAL,P1!INNER,C,=1.0E+07)
SPEDAT(SET,INITIAL,P1!OUTER,C,=1.E6)
SPEDAT(SET,SOURCE,R1!IN,C,=COVAL(2.0E+10&1.0E+07))
SPEDAT(SET,SOURCE,R1!OUT,C,=COVAL(2.0E+10&1.E6))
SPEDAT(SET,OBJNAM,!INNER,C,INNER)
SPEDAT(SET,OBJTYP,!INNER,C,USER_DEFINED)
SPEDAT(SET,OBJNAM,!OUTER,C,OUTER)
SPEDAT(SET,OBJTYP,!OUTER,C,USER_DEFINED)
SPEDAT(SET,OBJNAM,!IN,C,INNER)
SPEDAT(SET,OBJTYP,!IN,C,USER_DEFINED)
SPEDAT(SET,OBJNAM,!OUT,C,OUTER)
SPEDAT(SET,OBJTYP,!OUT,C,USER_DEFINED)
SPEDAT(SET,OBJNAM,!OB3,C,CYLINDER)
SPEDAT(SET,OBJTYP,!OB3,C,BLOCKAGE)
SPEDAT(SET,CYLINDER,MATERIAL,R,160.)
SPEDAT(SET,FACETDAT,NUMOBJ,I,3)
SPEDAT(SET,MATERIAL,0,L,T)
SPEDAT(SET,MATERIAL,160,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,N,N,N)
OUTPUT(V1,Y,N,Y,Y,Y,Y)
OUTPUT(EZ/T,Y,N,Y,N,N,N)
OUTPUT(EY/T,Y,N,Y,N,N,N)
OUTPUT(EX/T,Y,N,Y,N,N,N)
OUTPUT(V1/T,Y,N,Y,N,N,N)
OUTPUT(P1TH,Y,N,Y,N,N,N)
OUTPUT(V1TH,Y,N,Y,N,N,N)
OUTPUT(EZTH,Y,N,Y,N,N,N)
OUTPUT(EPSZ,Y,N,Y,N,N,N)
OUTPUT(SZTH,Y,N,Y,N,N,N)
OUTPUT(STRZ,Y,N,Y,N,N,N)
OUTPUT(EYTH,Y,N,Y,N,N,N)
OUTPUT(EPSY,Y,N,Y,N,N,N)
OUTPUT(SYTH,Y,N,Y,N,N,N)
OUTPUT(STRY,Y,N,Y,N,N,N)
OUTPUT(EXTH,Y,N,Y,N,N,N)
OUTPUT(EPSX,Y,N,Y,N,N,N)
OUTPUT(SXTH,Y,N,Y,N,N,N)
OUTPUT(STRX,Y,N,Y,N,N,N)
OUTPUT(DRH1,N,N,N,N,N,N)
OUTPUT(DVO1,N,N,N,N,N,N)
OUTPUT(ENUL,N,N,N,N,N,N)
OUTPUT(DEN1,N,N,N,N,N,N)
OUTPUT(PRPS,N,N,N,N,N,N)
OUTPUT(DISY,Y,N,Y,Y,Y,Y)
************************************************************
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
NYPRIN = 1 ;IYPRF = 1 ;IYPRL = 33
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
No PATCHes yet used for this Group
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP
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