TALK=T;RUN(1,1)
DISPLAY
The bending of a beam is calculated in accordance with the
ordinary-differential-equations method, known as the
Engineer's theory, for three cases:
1. uniform bending moment,
2. uniform load, and
3. point load.
ENDDIS
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Group 1. Run Title and Number
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TEXT(bent beam; engineer's theory;s105 )
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IRUNN = 1 ;LIBREF = 3
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Group 2. Time dependence
STEADY = T
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Group 3. X-Direction Grid Spacing
CARTES = T
NX = 21
XULAST =1.212
XFRAC(1)=0.049505 ;XFRAC(2)=0.09901
XFRAC(3)=0.148515 ;XFRAC(4)=0.19802
XFRAC(5)=0.247525 ;XFRAC(6)=0.29703
XFRAC(7)=0.346535 ;XFRAC(8)=0.39604
XFRAC(9)=0.445545 ;XFRAC(10)=0.49505
XFRAC(11)=0.544554 ;XFRAC(12)=0.594059
XFRAC(13)=0.643564 ;XFRAC(14)=0.693069
XFRAC(15)=0.742574 ;XFRAC(16)=0.792079
XFRAC(17)=0.841584 ;XFRAC(18)=0.891089
XFRAC(19)=0.940594 ;XFRAC(20)=0.990099
XFRAC(21)=1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 3
YVLAST =5.1E-03
YFRAC(1)=9.803922E-03 ;YFRAC(2)=0.990196
YFRAC(3)=1.
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Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 1
ZWLAST =5.0E-03
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(1)=P1 ;NAME(3)=U1
NAME(5)=V1 ;NAME(141)=DRH1
NAME(142)=DVO1 ;NAME(143)=VISL
NAME(144)=V1/T ;NAME(145)=V1TH
NAME(146)=EPSZ ;NAME(147)=EPSX
NAME(148)=EPSY ;NAME(149)=STRY
NAME(150)=PRPS
* 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(DRH1,Y,N,N,N,N,Y)
SOLUTN(DVO1,Y,N,N,N,N,Y)
SOLUTN(VISL,Y,N,N,N,N,Y)
SOLUTN(V1/T,Y,N,N,N,N,Y)
SOLUTN(V1TH,Y,N,N,N,N,Y)
SOLUTN(EPSZ,Y,N,N,N,N,Y)
SOLUTN(EPSX,Y,N,N,N,N,Y)
SOLUTN(EPSY,Y,N,N,N,N,Y)
SOLUTN(STRY,Y,N,N,N,N,Y)
SOLUTN(PRPS,Y,N,N,N,N,Y)
VISL = 143
PRPS = 150
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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(P1,Y,Y,Y,N,Y,Y)
TERMS(U1,Y,Y,Y,Y,Y,Y)
TERMS(V1,Y,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 =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-05 ;ENUT =0.
PRNDTL(U1)=1. ;PRNDTL(V1)=1.
PRT(U1)=1. ;PRT(V1)=1.
CP1 =1. ;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.
*
161 7800.0 0.0 473.0 43.0 1.0E-5 0.5E-11
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Group 10.Inter-Phase Transfer Processes
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Group 11.Initial field variables (PHIs)
FIINIT(P1)=0. ;FIINIT(U1)=0.
FIINIT(V1)=0. ;FIINIT(DRH1)=1.0E-10
FIINIT(DVO1)=1.0E-10 ;FIINIT(VISL)=1.0E-10
FIINIT(V1/T)=0. ;FIINIT(V1TH)=0.
FIINIT(EPSZ)=1.0E-10 ;FIINIT(EPSX)=1.0E-10
FIINIT(EPSY)=1.0E-10 ;FIINIT(STRY)=1.0E-10
FIINIT(PRPS)=0.
PATCH(BODY ,INIVAL, 1, 20, 2, 2, 1, 1, 1, 1)
INIT(BODY ,PRPS, FIXVAL ,161. )
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(AXESUU ,WWALL , 1, 1, 2, 2, 1, 1, 1, 1)
COVAL(AXESUU ,U1 ,1. ,0. )
PATCH(AXESVV ,WWALL , 1, 1, 1, 2, 1, 1, 1, 1)
COVAL(AXESVV ,V1 ,1. ,0. )
PATCH(BEAMEND ,EAST , 20, 20, 1, 2, 1, 1, 1, 1)
COVAL(BEAMEND ,V1 ,In-Form:source - see Grp 19)
PATCH(BEAM ,VOLUME, 1, 20, 1, 2, 1, 1, 1, 1)
COVAL(BEAM ,V1 ,In-Form:source - see Grp 19)
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 = 100 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =1.0E-08
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Group 16. Terminate Iterations
LITER(P1)=4 ;LITER(U1)=10
LITER(V1)=100
ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
ENDIT(V1)=0.
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Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(U1,FALSDT,1.)
RELAX(V1,FALSDT,1.)
RELAX(DRH1,LINRLX,1.)
RELAX(DVO1,LINRLX,1.)
RELAX(VISL,LINRLX,1.)
RELAX(V1/T,LINRLX,1.)
RELAX(V1TH,LINRLX,1.)
RELAX(EPSZ,LINRLX,1.)
RELAX(EPSX,LINRLX,1.)
RELAX(EPSY,LINRLX,1.)
RELAX(STRY,LINRLX,1.)
RELAX(PRPS,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)=1.0E+06 ;VARMIN(V1)=-1.0E+06
VARMAX(DRH1)=1.0E+10 ;VARMIN(DRH1)=-1.0E+10
VARMAX(DVO1)=1.0E+10 ;VARMIN(DVO1)=-1.0E+10
VARMAX(VISL)=1.0E+10 ;VARMIN(VISL)=-1.0E+10
VARMAX(V1/T)=1.0E+10 ;VARMIN(V1/T)=-1.0E+10
VARMAX(V1TH)=1.0E+10 ;VARMIN(V1TH)=-1.0E+10
VARMAX(EPSZ)=1.0E+10 ;VARMIN(EPSZ)=-1.0E+10
VARMAX(EPSX)=1.0E+10 ;VARMIN(EPSX)=-1.0E+10
VARMAX(EPSY)=1.0E+10 ;VARMIN(EPSY)=-1.0E+10
VARMAX(STRY)=1.0E+10 ;VARMIN(STRY)=-1.0E+10
VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
STRA = T
PARSOL = F
ISG21 = 100
ISG50 = 1
ISG52 = 1
ISG62 = 1
CSG10 ='Q1'
SPEDAT(SET,BOUNDARY,ZCONST,R,1.0E+20)
SPEDAT(SET,SOURCE,V1!BEAM,C,=COVAL(2.0E-10&1.44E+07))
SPEDAT(SET,SOURCE,V1!BEAMEND,C,=COVAL(2.0E-10&-1.728E+07))
SPEDAT(SET,STORED,V1TH,C,=-7.200001E-05*(XG)^2!SWPS!ZSLFIN)
SPEDAT(SET,STORED,V1/T,C,=V1/V1TH!ZSLFIN)
SPEDAT(SET,LONGNAME,P1,C,pressure_or_dilatation)
SPEDAT(SET,LONGNAME,PTH,C,dilatation_theoretical)
SPEDAT(SET,LONGNAME,ENUL,C,viscosity_or__LAME's_G*1.E11)
SPEDAT(SET,LONGNAME,VISL,C,viscosity_or__LAME's_G*1.E11)
SPEDAT(SET,LONGNAME,DRH1,C,compressibility_or_LAME's_L+G*1.E11)
SPEDAT(SET,LONGNAME,DVO1,C,th.exp.co_r_or_H*1.E11)
SPEDAT(SET,LONGNAME,U1,C,x-direction_velocity_or_displacement)
SPEDAT(SET,LONGNAME,EPSX,C,x-direction_strain)
SPEDAT(SET,LONGNAME,EXTH,C,x-direction_strain_theoretical)
SPEDAT(SET,LONGNAME,STRX,C,x-direction_stress)
SPEDAT(SET,LONGNAME,SXTH,C,x-direction_stress_theoretical)
SPEDAT(SET,LONGNAME,V1,C,y-direction_velocity_or_displacement)
SPEDAT(SET,LONGNAME,EPSY,C,y-direction_strain)
SPEDAT(SET,LONGNAME,EYTH,C,y-direction_strain_theoretical)
SPEDAT(SET,LONGNAME,STRY,C,y-direction_stress)
SPEDAT(SET,LONGNAME,SYTH,C,y-direction_stress_theoretical)
SPEDAT(SET,LONGNAME,W1,C,z-direction_velocity_or_displacement)
SPEDAT(SET,LONGNAME,EPSZ,C,z-direction_strain)
SPEDAT(SET,LONGNAME,STRZ,C,z-direction_stress)
SPEDAT(SET,LONGNAME,EZTH,C,z-direction_strain_theoretical)
SPEDAT(SET,LONGNAME,SZTH,C,z-direction_stress_theoretical)
SPEDAT(SET,LONGNAME,EPST,C,linearthermalexpansion)
SPEDAT(SET,GXMONI,PLOTALL,L,T)
SPEDAT(SET,MATERIAL,0,L,T)
SPEDAT(SET,MATERIAL,161,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(P1,Y,N,Y,Y,Y,Y)
OUTPUT(U1,Y,N,Y,Y,Y,Y)
OUTPUT(V1,Y,N,Y,Y,Y,Y)
OUTPUT(DRH1,N,N,N,N,N,N)
OUTPUT(DVO1,Y,N,Y,N,N,N)
OUTPUT(VISL,N,N,N,N,N,N)
OUTPUT(V1/T,Y,N,Y,N,N,N)
OUTPUT(V1TH,Y,N,Y,N,N,N)
OUTPUT(EPSZ,Y,N,Y,N,N,N)
OUTPUT(EPSX,Y,N,Y,N,N,N)
OUTPUT(EPSY,Y,N,Y,N,N,N)
OUTPUT(STRY,Y,N,Y,N,N,N)
OUTPUT(PRPS,Y,N,Y,N,N,N)
************************************************************
Group 22. Monitor Print-Out
IXMON = 19 ;IYMON = 1 ;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
NXPRIN = -1 ;IXPRF = 1 ;IXPRL = 10000
NYPRIN = 1 ;IYPRF = 1 ;IYPRL = 10000
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(VPROF ,PROFIL, 1, 21, 1, 1, 1, 1, 1, 1)
PLOT(VPROF ,V1 ,0. ,0. )
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Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP