TALK=f;RUN(1,1)
  DISPLAY
  Problem: Vertical prismatic (0.3x03x2.5 m) bar & gravity force 
           -Rho*g.
           At the upper end - a uniform normal stress equal to 
           total weight of the bar Rho*g*LZ.
   1. Comparison - a analytical solution:
      U = -P*Rho*g*x*z/E,
      V = -P*Rho*g*z*y/E,
      W = Rho*g/E/2*[ (z^2 - LZ^2) + P*(x^2+y^2)]
      
   2. Similar to s301, But fluid-layers are used     

  ENDDIS

 
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
TEXT(3D Prismatic bar & gravity force)
  Declarations and settings
REAL(Rho,GF,FZ,LX,LY,LZ,POISSON,YOUNG)
Rho = 1.e4
GF=9.8 
FZ= Rho*GF
LX=0.15
LZ=2.5
LY=0.15 
YOUNG   = 1/0.5E-11   ! Young's modulus
POISSON=0.3           ! Poisson's ratio
INTEGER(NXBODY,NYBODY,NZBODY)

 ************************************************************
  Group 2. Time dependence
 STEADY  =    T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES  =    T
 NXBODY = 5
 NREGX=3                             ! 3 regions
 IREGX=1;GRDPWR(X,1,0.01*LX,1.0)     ! single inner fluid cell
 IREGX=2;GRDPWR(X,NXBODY,LX,1)  
 IREGX=3;GRDPWR(X,1,0.01*LX,1.0)     ! single outer fluid cell 

 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NYBODY = 5
 NREGY=3                             ! 3 regions
 IREGY=1;GRDPWR(Y,1,0.01*LY,1.0)     ! single inner fluid cell
 IREGY=2;GRDPWR(Y,NYBODY,LY,1)  
 IREGY=3;GRDPWR(Y,1,0.01*LY,1.0)     ! single outer fluid cell 
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 NZBODY = 5
 NREGZ=3                             ! 3 regions
 IREGZ=1;GRDPWR(Z,1,0.01*LZ,1.0)     ! single inner fluid cell
 IREGZ=2;GRDPWR(Z,NZBODY,LZ,1)  
 IREGZ=3;GRDPWR(Z,1,0.01*LZ,1.0)     ! single outer fluid cell 
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS  =    T
 SOLVE(P1,V1,U1,W1)
 SOLUTN(P1  ,Y,Y,Y,N,N,N)
 SOLUTN(U1  ,Y,Y,Y,N,N,Y)
 SOLUTN(V1  ,Y,Y,Y,N,N,Y)
 SOLUTN(W1  ,Y,Y,Y,N,N,Y)
 
 STORE(PRPS)
 STORE(DRH1,VISL) 

      STORE(STRZ)  
 STORE(EPSY,EPSX,EPSZ)
 STORE(U1T,V1T,W1T,U1/T,V1/T,W1/T)

 ************************************************************
  GROUP 8. ITERATION NUMBERS ETC
RESFAC=1.e-7
RESREF(V1)=0.0 
RESREF(U1)=0.0  ! to prevent premature exit
LITER(V1) = 50 ! from solver
LITER(U1) = 50 
LITER(P1) = 50 
RESREF(W1)=0.0 
LITER(W1) = 50 

 ************************************************************
  GROUP 9. PROPERTIES
  
 CSG10='Q1'                  ! materials with various POISSON ratios
  MATFLG=T;NMAT=1         
  160    7800.0    0.3       473.0   43.0      1.0e-5   0.5e-11 
 
 ************************************************************
  GROUP 11. INITIAL VALUES
fiinit(p1)=0.0
fiinit(u1)=0.0
fiinit(v1)=0.0
fiinit(w1)=0.0
 
 FIINIT(PRPS)=0
 PATCH(BODY,INIVAL,2,NX-1,2,NY-1,2,NZ-1,1,1)
 INIT(BODY,PRPS,FIXVAL,160)

 ************************************************************
  GROUP 13. BOUNDARY & SPECIAL SOURCES
 
PATCH(FORC01,HIGH,2,NX-1,2,NY-1,NZ-1,NZ-1,1,1)            ! Upper - sprain
COVAL(FORC01,W1,FIXFLU,FZ*LZ)

PATCH(FORCGRA,VOLUME,2,NX-1,2,NY-1,1,NZ-1,1,1)             ! Volume - gravity force
COVAL(FORCGRA,W1,FIXFLU,-FZ)

PATCH(ONEP,CELL,2,NX-1,2,NY-1,NZ-1,NZ-1,1,1)                           ! Fixed moving
real(C00)
C00 = FZ/YOUNG*POISSON/2
char(Frm00)
Frm00 = :C00:*(XG^2 + YG^2)
(source of W1 at ONEP is COVAL(1,:FRM00:))

PATCH(AXESXX,EAST,1,1,2,NY-1,2,NZ-1,1,1)            ! X = 0 plate
COVAL(AXESXX,U1,FIXVAL,0.0)

PATCH(AXESYY,NORTH,2,NX-1,1,1,2,NZ-1,1,1)            ! Y = 0 plate
COVAL(AXESYY,V1,FIXVAL,0.0)



 ************************************************************
  GROUP 15. TERMINATE SWEEPS
 LSWEEP  =      700
 ISG21=LSWEEP
 ************************************************************
  GROUP 17. RELAXATION
     #CONPROM
 RELAX(P1  ,LINRLX, 1.000000E+00)
     spedat(rlxfac,rlxu1d,r,0.5)  
     spedat(rlxfac,rlxv1d,r,0.5)  
     spedat(rlxfac,rlxw1d,r,0.5)  
 ************************************************************
  GROUP 19. DATA TRANSMITTED TO GROUND
 STRA    =    T
 PARSOL  =    F
 ISG52   =    3   !   probe & res

 ************************************************************
  GROUP 23.FIELD PRINT-OUT & PLOT CONTROL
TSTSWP = - 1   ! graphic-mode
    NYPRIN = 1
    NXPRIN = 1
NZPRIN = 1
IXMON = NX-2
IYMON = NY-2
IZMON = NZ-2
output(prps,n,n,n,n,n,n) 
output(drh1,n,n,n,n,n,n) 
output(visl,n,n,n,n,n,n) 
output(epsZ,n,n,n,n,n,n) 

      #conprom 

  inform7begin
real(CX,CZ,CZ05)
CX = FZ/YOUNG*POISSON
CZ = FZ/YOUNG
CZ05 = CZ/2
char(Frm1,Frm2,FRM3)
Frm1 = :CZ05:*((ZW-0.01*:LZ:)^2 - :LZ:^2)+
Frm2 = :CX:/2*((XG-0.01*:LX:)^2+(YG-0.01*:LY:)^2)
Frm3=*(ZG-0.01*:LZ:)
   **** CALCULATE analytical solution ***
(STORED VAR W1T IS :Frm1::Frm2: with imat>100)

(STORED VAR U1T IS -:CX:*(XU-0.01*:LX:):frm3: with imat>100)
(STORED VAR V1T IS -:CX:*(YV-0.01*:LY:):frm3: with imat>100)

(STORED VAR U1/T IS U1/(U1T+1.e-20) with imat>100)
(STORED VAR V1/T IS V1/(V1T+1.e-20) with imat>100)
(STORED VAR W1/T IS W1/(W1T+1.e-20) with imat>100)

  inform7end

       restrt(all) 

STOP