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CFVR0918 - Shell reinforcement design according to GB50010

Shell reinforcement design according to the Chinese code GB50010 using the Wood-Armer method.

The model is made up of two square shell elements of 1.0m x 1.0m. The nodes of one side are completely restrained and one of the nodes between both element has its vertical movement restrained (perpendicular to the shells).
The applied loads are fixed displacements at the free side of the model.

The reinforcement design method is the Wood-Armer method. The values obtained by CivilFEM are compared to the analytical values obtained in the log file.

Element types used in the model: SHELL63

Needed CivilFEM Modules:
Geotechnical Module
Bridges and Civil Non Linearities Module
Advanced Prestressed Concrete Module

The example can be launched on an educational license.
KEYWORDS
Shell
Shell Vertex
Reinforced Concrete
GB 50010

Model Statistics
Number of elements 2
Number of nodes 6
Number of civil materials 2
Number of cross sections 0
Number of shell vertices 1

Log file: CFVR0918.DAT


   FINISH
  ~CFCLEAR,,1
   NomFile='CFVR0918'
  /TITLE, %NomFile%, Shell reinforcement design according to GB50010
! ---------------------------------------------------------------------------------
! Model definition and analysis
! ---------------------------------------------------------------------------------

! Setup
 ~UNITS,SI
 ~CODESEL,EC3-92,GB50010,,,EC8-94
 ~CFCONFG,PLRES   ,SHELL   ,EPSW 
 ~CFCONFG,RESULT,CFSHF,1

/PREP7
! Materials
 ~CFMP,5,LIB,CONCRETE,GB50010,C40
 ~CFMP,2,LIB,REINF,GB50010,HRB400
! Elements type
  ET,2,SHELL63
! Shell Vertex
  t=0.12     ! Thickness
  r=0.03     ! Cover
  th = 0     ! Reinforcement angle
 ~SHLRNF,1,t,5,2,r,0.0,0.0,0.0,0.0,0,th,45
! Beam & Shell property
 ~BMSHPRO,10,SHELL,1,1,1,1,63,,,,Shell property

! Nodes
  N,10,0.0,0.0
  N,20,1.0,0.0
  N,30,2.0,0.0
  N,40,0.0,1.0
  N,50,1.0,1.0
  N,60,2.0,1.0
! Elements
  MAT,5
  REAL,10
  TYPE,2
  EN,100, 10, 20, 50, 40
  EN,200, 20, 30, 60, 50
! Boundary conditions
  D,10,ALL,0.0
  D,40,ALL,0.0
  D,50,UZ,0.0
! Analysis
  /SOLU
  D,30,UZ,-0.025
  D,60,UX, 0.001
  D,60,UY, 0.001
  SOLVE

/POST1
! ---------------------------------------------------------------------------------
! Forces and moments calculation in element 100
! ---------------------------------------------------------------------------------
  *DIM,S  ,,6,3,4 ! Stesses (direction,layer,node)
  *DIM,ESF,,8,4   ! Forces and moments (Component,node) (Tx,Ty,Txy,Mx,My,Mxy,Nx,Ny)

  ESEL,S,ELEM,,100
! Stresses
  SHELL,TOP
  *VGET,S(1,1,1),NODE,10,S,X,,,4
  *VGET,S(1,1,2),NODE,20,S,X,,,4
  *VGET,S(1,1,3),NODE,50,S,X,,,4
  *VGET,S(1,1,4),NODE,40,S,X,,,4
  SHELL,MID
  *VGET,S(1,2,1),NODE,10,S,X,,,4
  *VGET,S(1,2,2),NODE,20,S,X,,,4
  *VGET,S(1,2,3),NODE,50,S,X,,,4
  *VGET,S(1,2,4),NODE,40,S,X,,,4
  SHELL,BOT
  *VGET,S(1,3,1),NODE,10,S,X,,,4
  *VGET,S(1,3,2),NODE,20,S,X,,,4
  *VGET,S(1,3,3),NODE,50,S,X,,,4
  *VGET,S(1,3,4),NODE,40,S,X,,,4
! Forces and moments
  *DO,I,1,4
    ESF(1,I)=t*(S(1,1,I)+4*S(1,2,I)+S(1,3,I))/6
    ESF(2,I)=t*(S(2,1,I)+4*S(2,2,I)+S(2,3,I))/6
    ESF(3,I)=t*(S(4,1,I)+4*S(4,2,I)+S(4,3,I))/6
    ESF(4,I)=-t**2*(S(1,1,I)-S(1,3,I))/12
    ESF(5,I)=-t**2*(S(2,1,I)-S(2,3,I))/12
    ESF(6,I)=-t**2*(S(4,1,I)-S(4,3,I))/12
    ESF(7,I)=t*(S(6,1,I)+4*S(6,2,I)+S(6,3,I))/6
    ESF(8,I)=t*(S(5,1,I)+4*S(5,2,I)+S(5,3,I))/6
  *ENDDO
! Design moments
  *DIM,Mxi,,4
  *DIM,Myi,,4
  *DIM,Mxs,,4
  *DIM,Mys,,4
  ! Lower reinforcement moments
    *DO,I,1,4
      Mxi(I)=ESF(4,I)-2*ESF(6,I)*TAN(th)+ESF(5,I)*(TAN(th))**2
      Mxi(I)=Mxi(I)+ABS((ESF(6,I)-ESF(5,I)*TAN(th))/COS(th))
      Myi(I)=ESF(5,I)/(COS(th))**2+ABS((ESF(6,I)-ESF(5,I)*TAN(th))/COS(th))
      *IF,Mxi(I),LT,0,THEN
         Mxi(I)=0
         Myi(I)=(ESF(6,I)-ESF(5,I)*TAN(th))**2
         Myi(I)=ABS(Myi(I)/(ESF(4,I)-2*ESF(6,I)*TAN(th)+ESF(5,I)*(TAN(th))**2))
         Myi(I)=(ESF(5,I)+Myi(I))/(COS(th))**2
         Myi(I)=(Myi(I)>0)
      *ENDIF
      *IF,Myi(I),LT,0,THEN
         Mxi(I)=ESF(5,I)*(TAN(th))**2+ABS((ESF(6,I)-ESF(5,I)*TAN(th))**2/ESF(5,I))
         Mxi(I)=Mxi(I)+2*ESF(6,I)*TAN(th)+Mxi(I)
         Mxi(I)=(Mxi(I)>0)
         Myi(I)=0
      *ENDIF
    *ENDDO
  ! Upper reinforcement moments
    *DO,I,1,4
      Mxs(I)=ESF(4,I)-2*ESF(6,I)*TAN(th)+ESF(5,I)*(TAN(th))**2
      Mxs(I)=Mxs(I)-ABS((ESF(6,I)-ESF(5,I)*TAN(th))/COS(th))
      Mys(I)=ESF(5,I)/(COS(th))**2-ABS((ESF(6,I)-ESF(5,I)*TAN(th))/COS(th))
      *IF,Mxs(I),GT,0,THEN
         Mxs(I)=0
         Mys(I)=(ESF(6,I)-ESF(5,I)*TAN(th))**2
         Mys(I)=ABS(Mys(I)/(ESF(4,I)-2*ESF(6,I)*TAN(th)+ESF(5,I)*(TAN(th))**2))
         Mys(I)=(ESF(5,I)-Mys(I))/(COS(th))**2
         Mys(I)=(Mys(I)<0)
      *ENDIF
      *IF,Mys(I),GT,0,THEN
         Mxs(I)=ESF(5,I)*(TAN(th))**2-ABS((ESF(6,I)-ESF(5,I)*TAN(th))**2/ESF(5,I))
         Mxs(I)=Mxs(I)+2*ESF(6,I)*TAN(th)+Mxs(I)
         Mxs(I)=(Mxs(I)<0)
         Mys(I)=0
      *ENDIF
    *ENDDO
! Designed reinforcement
  *DIM,Axi,,4
  *DIM,Ayi,,4
  *DIM,Axs,,4
  *DIM,Ays,,4
 ~CFGET,FCD,MATERIAL,5,GBMAT_C,FC
 ~CFGET,FYD,MATERIAL,2,GBMAT_S,FY
 ~CFGET,GAMMAC,MATERIAL,5,GBMAT_C,GAMC
 ~CFGET,GAMMAS,MATERIAL,2,GBMAT_S,GAMS
 ~CFGET,EX,MATERIAL,2,DATGEN,EX

I=1
  ~SBPAR,Mxi(I),1.0,t,'ASBxi','ASTxi',r,r,FCD,FYD,EX
  ~SBPAR,Myi(I),1.0,t,'ASByi','ASTyi',r,r,FCD,FYD,EX
  ~SBPAR,Mxs(I),1.0,t,'ASBxs','ASTxs',r,r,FCD,FYD,EX
  ~SBPAR,Mys(I),1.0,t,'ASBys','ASTys',r,r,FCD,FYD,EX
   Axi(I)= (ASBxi > ASBxs)
   Ayi(I)= (ASByi > ASBys)
   Axs(I)= (ASTxs > ASTxi)
   Ays(I)= (ASTys > ASTyi)

I=2
  ~SBPAR,Mxi(I),1.0,t,'ASBxi','ASTxi',r,r,FCD,FYD,EX
  ~SBPAR,Myi(I),1.0,t,'ASByi','ASTyi',r,r,FCD,FYD,EX
  ~SBPAR,Mxs(I),1.0,t,'ASBxs','ASTxs',r,r,FCD,FYD,EX
  ~SBPAR,Mys(I),1.0,t,'ASBys','ASTys',r,r,FCD,FYD,EX
   Axi(I)= (ASBxi > ASBxs)
   Ayi(I)= (ASByi > ASBys)
   Axs(I)= (ASTxs > ASTxi)
   Ays(I)= (ASTys > ASTyi)

I=3
  ~SBPAR,Mxi(I),1.0,t,'ASBxi','ASTxi',r,r,FCD,FYD,EX
  ~SBPAR,Myi(I),1.0,t,'ASByi','ASTyi',r,r,FCD,FYD,EX
  ~SBPAR,Mxs(I),1.0,t,'ASBxs','ASTxs',r,r,FCD,FYD,EX
  ~SBPAR,Mys(I),1.0,t,'ASBys','ASTys',r,r,FCD,FYD,EX
   Axi(I)= (ASBxi > ASBxs)
   Ayi(I)= (ASByi > ASBys)
   Axs(I)= (ASTxs > ASTxi)
   Ays(I)= (ASTys > ASTyi)

I=4
  ~SBPAR,Mxi(I),1.0,t,'ASBxi','ASTxi',r,r,FCD,FYD,EX
  ~SBPAR,Myi(I),1.0,t,'ASByi','ASTyi',r,r,FCD,FYD,EX
  ~SBPAR,Mxs(I),1.0,t,'ASBxs','ASTxs',r,r,FCD,FYD,EX
  ~SBPAR,Mys(I),1.0,t,'ASBys','ASTys',r,r,FCD,FYD,EX
   Axi(I)= (ASBxi > ASBxs)
   Ayi(I)= (ASByi > ASBys)
   Axs(I)= (ASTxs > ASTxi)
   Ays(I)= (ASTys > ASTyi)

  ESEL,ALL

! ---------------------------------------------------------------------------------
! Design with CivilFEM
! ---------------------------------------------------------------------------------
 ~CFSET,,1,1
 ~DIMCON,SHELL,WOOD

  ESEL,S,ELEM,,100
! Forces and moments with civilFEM
  *DIM,ESF_CF,,8,4   ! Forces and moments (component,node) (Tx,Ty,Txy,Mx,My,Mxy,Nx,Ny)
~PLSHFOR,TX
  *GET,ESF_CF(1,1),NODE,10,EPSW
  *GET,ESF_CF(1,2),NODE,20,EPSW
  *GET,ESF_CF(1,3),NODE,50,EPSW
  *GET,ESF_CF(1,4),NODE,40,EPSW
~PLSHFOR,TY
  *GET,ESF_CF(2,1),NODE,10,EPSW
  *GET,ESF_CF(2,2),NODE,20,EPSW
  *GET,ESF_CF(2,3),NODE,50,EPSW
  *GET,ESF_CF(2,4),NODE,40,EPSW
~PLSHFOR,TXY
  *GET,ESF_CF(3,1),NODE,10,EPSW
  *GET,ESF_CF(3,2),NODE,20,EPSW
  *GET,ESF_CF(3,3),NODE,50,EPSW
  *GET,ESF_CF(3,4),NODE,40,EPSW
~PLSHFOR,MX
  *GET,ESF_CF(4,1),NODE,10,EPSW
  *GET,ESF_CF(4,2),NODE,20,EPSW
  *GET,ESF_CF(4,3),NODE,50,EPSW
  *GET,ESF_CF(4,4),NODE,40,EPSW
~PLSHFOR,MY
  *GET,ESF_CF(5,1),NODE,10,EPSW
  *GET,ESF_CF(5,2),NODE,20,EPSW
  *GET,ESF_CF(5,3),NODE,50,EPSW
  *GET,ESF_CF(5,4),NODE,40,EPSW
~PLSHFOR,MXY
  *GET,ESF_CF(6,1),NODE,10,EPSW
  *GET,ESF_CF(6,2),NODE,20,EPSW
  *GET,ESF_CF(6,3),NODE,50,EPSW
  *GET,ESF_CF(6,4),NODE,40,EPSW
~PLSHFOR,NX
  *GET,ESF_CF(7,1),NODE,10,EPSW
  *GET,ESF_CF(7,2),NODE,20,EPSW
  *GET,ESF_CF(7,3),NODE,50,EPSW
  *GET,ESF_CF(7,4),NODE,40,EPSW
~PLSHFOR,NY
  *GET,ESF_CF(8,1),NODE,10,EPSW
  *GET,ESF_CF(8,2),NODE,20,EPSW
  *GET,ESF_CF(8,3),NODE,50,EPSW
  *GET,ESF_CF(8,4),NODE,40,EPSW

! Design moments obtained with CivilFEM
  *DIM,Mxi_CF,,4
  *DIM,Myi_CF,,4
  *DIM,Mxs_CF,,4
  *DIM,Mys_CF,,4
~PLSHCON,MXB
  *GET,Mxi_CF(1),NODE,10,EPSW
  *GET,Mxi_CF(2),NODE,20,EPSW
  *GET,Mxi_CF(3),NODE,50,EPSW
  *GET,Mxi_CF(4),NODE,40,EPSW
~PLSHCON,MYB
  *GET,Myi_CF(1),NODE,10,EPSW
  *GET,Myi_CF(2),NODE,20,EPSW
  *GET,Myi_CF(3),NODE,50,EPSW
  *GET,Myi_CF(4),NODE,40,EPSW
~PLSHCON,MXT
  *GET,Mxs_CF(1),NODE,10,EPSW
  *GET,Mxs_CF(2),NODE,20,EPSW
  *GET,Mxs_CF(3),NODE,50,EPSW
  *GET,Mxs_CF(4),NODE,40,EPSW
~PLSHCON,MYT
  *GET,Mys_CF(1),NODE,10,EPSW
  *GET,Mys_CF(2),NODE,20,EPSW
  *GET,Mys_CF(3),NODE,50,EPSW
  *GET,Mys_CF(4),NODE,40,EPSW

! Design reinforcement obtained with CivilFEM
  *DIM,Axi_CF,,4
  *DIM,Ayi_CF,,4
  *DIM,Axs_CF,,4
  *DIM,Ays_CF,,4
~PLSHCON,ASBX
  *GET,Axi_CF(1),NODE,10,EPSW
  *GET,Axi_CF(2),NODE,20,EPSW
  *GET,Axi_CF(3),NODE,50,EPSW
  *GET,Axi_CF(4),NODE,40,EPSW
~PLSHCON,ASBY
  *GET,Ayi_CF(1),NODE,10,EPSW
  *GET,Ayi_CF(2),NODE,20,EPSW
  *GET,Ayi_CF(3),NODE,50,EPSW
  *GET,Ayi_CF(4),NODE,40,EPSW
~PLSHCON,ASTX
  *GET,Axs_CF(1),NODE,10,EPSW
  *GET,Axs_CF(2),NODE,20,EPSW
  *GET,Axs_CF(3),NODE,50,EPSW
  *GET,Axs_CF(4),NODE,40,EPSW
~PLSHCON,ASTY
  *GET,Ays_CF(1),NODE,10,EPSW
  *GET,Ays_CF(2),NODE,20,EPSW
  *GET,Ays_CF(3),NODE,50,EPSW
  *GET,Ays_CF(4),NODE,40,EPSW

!--------------------------------------------------------------------------------------
! DATA CHECK
!--------------------------------------------------------------------------------------
! Data comparison number
  NComp = 64
  NComp_ch = 0

! Matrix dim.
  *DIM,LABEL,CHAR,Ncomp,1
  *DIM,LABEL_CH,CHAR,Ncomp_ch,1
  *DIM,VALUE,,Ncomp,3
  *DIM,VALUE_CH,CHAR,Ncomp_ch,3
  *DIM,TOLER,,Ncomp,2

! Labels
!--------------------------------------------------------------------------------------
  LABEL( 1) ='TX_I'
  LABEL( 2) ='TX_J'
  LABEL( 3) ='TX_K'
  LABEL( 4) ='TX_L'
  LABEL( 5) ='TY_I'
  LABEL( 6) ='TY_J'
  LABEL( 7) ='TY_K'
  LABEL( 8) ='TY_L'
  LABEL( 9) ='TXY_I'
  LABEL(10) ='TXY_J'
  LABEL(11) ='TXY_K'
  LABEL(12) ='TXY_L'
  LABEL(13) ='MX_I'
  LABEL(14) ='MX_J'
  LABEL(15) ='MX_K'
  LABEL(16) ='MX_L'
  LABEL(17) ='MY_I'
  LABEL(18) ='MY_J'
  LABEL(19) ='MY_K'
  LABEL(20) ='MY_L'
  LABEL(21) ='MXY_I'
  LABEL(22) ='MXY_J'
  LABEL(23) ='MXY_K'
  LABEL(24) ='MXY_L'
  LABEL(25) ='NX_I'
  LABEL(26) ='NX_J'
  LABEL(27) ='NX_K'
  LABEL(28) ='NX_L'
  LABEL(29) ='NY_I'
  LABEL(30) ='NY_J'
  LABEL(31) ='NY_K'
  LABEL(32) ='NY_L'
  LABEL(33) ='MDxi_I'
  LABEL(34) ='MDxi_J'
  LABEL(35) ='MDxi_K'
  LABEL(36) ='MDxi_L'
  LABEL(37) ='MDyi_I'
  LABEL(38) ='MDyi_J'
  LABEL(39) ='MDyi_K'
  LABEL(40) ='MDyi_L'
  LABEL(41) ='MDxs_I'
  LABEL(42) ='MDxs_J'
  LABEL(43) ='MDxs_K'
  LABEL(44) ='MDxs_L'
  LABEL(45) ='MDys_I'
  LABEL(46) ='MDys_J'
  LABEL(47) ='MDys_K'
  LABEL(48) ='MDys_L'
  LABEL(49) ='ASxi_I'
  LABEL(50) ='ASxi_J'
  LABEL(51) ='ASxi_K'
  LABEL(52) ='ASxi_L'
  LABEL(53) ='ASyi_I'
  LABEL(54) ='ASyi_J'
  LABEL(55) ='ASyi_K'
  LABEL(56) ='ASyi_L'
  LABEL(57) ='ASxs_I'
  LABEL(58) ='ASxs_J'
  LABEL(59) ='ASxs_K'
  LABEL(60) ='ASxs_L'
  LABEL(61) ='ASys_I'
  LABEL(62) ='ASys_J'
  LABEL(63) ='ASys_K'
  LABEL(64) ='ASys_L'

! Correct values
!--------------------------------------------------------------------------------------
  ! Forces and moments
    *DO,I,1,8
      *DO,J,1,4
        VALUE(4*(I-1)+J,1)= ESF(I,J)
      *ENDDO
    *ENDDO
  ! Design moments
    *DO,I,1,4
      VALUE(32+I,1)=Mxi(I) ! Mxi(I)
    *ENDDO
    *DO,I,1,4
      VALUE(36+I,1)=Myi(I) ! Myi(I)
    *ENDDO
    *DO,I,1,4
      VALUE(40+I,1)=Mxs(I) ! Mxs(I)
    *ENDDO
    *DO,I,1,4
      VALUE(44+I,1)=Mys(I) ! Mys(I)
    *ENDDO
  ! Reinforcements
    *DO,I,1,4
      VALUE(48+I,1)=Axi(I)
    *ENDDO
    *DO,I,1,4
      VALUE(52+I,1)=Ayi(I)
    *ENDDO
    *DO,I,1,4
      VALUE(56+I,1)=Axs(I)
    *ENDDO
    *DO,I,1,4
      VALUE(60+I,1)=Ays(I)
    *ENDDO

! Obtained values
!--------------------------------------------------------------------------------------
  ! Forces and moments
    *DO,I,1,8
      *DO,J,1,4
        VALUE(4*(I-1)+J,2)= ESF_CF(I,J)
      *ENDDO
    *ENDDO
  ! Design moments
    *DO,I,1,4
      VALUE(32+I,2)=Mxi_CF(I)
    *ENDDO
    *DO,I,1,4
      VALUE(36+I,2)=Myi_CF(I)
    *ENDDO
    *DO,I,1,4
      VALUE(40+I,2)=Mxs_CF(I)
    *ENDDO
    *DO,I,1,4
      VALUE(44+I,2)=Mys_CF(I)
    *ENDDO
  ! Reinforcements
    *DO,I,1,4
      VALUE(48+I,2)=Axi_CF(I)
    *ENDDO
    *DO,I,1,4
      VALUE(52+I,2)=Ayi_CF(I)
    *ENDDO
    *DO,I,1,4
      VALUE(56+I,2)=Axs_CF(I)
    *ENDDO
    *DO,I,1,4
      VALUE(60+I,2)=Ays_CF(I)
    *ENDDO

! Warning and error tolerances
  TOLER( 1, 1)= 1E-01   $   TOLER( 1, 2)= 1E-00
  TOLER( 2, 1)= 1E-01   $   TOLER( 2, 2)= 1E-00
  TOLER( 3, 1)= 1E-02   $   TOLER( 3, 2)= 1E-01
  TOLER( 4, 1)= 1E-02   $   TOLER( 4, 2)= 1E-01
  TOLER( 5, 1)= 1E-02   $   TOLER( 5, 2)= 1E-01
  TOLER( 6, 1)= 1E-02   $   TOLER( 6, 2)= 1E-01
  TOLER( 7, 1)= 1E-02   $   TOLER( 7, 2)= 1E-01
  TOLER( 8, 1)= 1E-02   $   TOLER( 8, 2)= 1E-01
  TOLER( 9, 1)= 1E-02   $   TOLER( 9, 2)= 1E-01
  TOLER(10, 1)= 1E-02   $   TOLER(10, 2)= 1E-01
  TOLER(11, 1)= 1E-02   $   TOLER(11, 2)= 1E-01
  TOLER(12, 1)= 1E-02   $   TOLER(12, 2)= 1E-01
  TOLER(13, 1)= 1E-02   $   TOLER(13, 2)= 1E-01
  TOLER(14, 1)= 1E-03   $   TOLER(14, 2)= 1E-02
  TOLER(15, 1)= 1E-02   $   TOLER(15, 2)= 1E-01
  TOLER(16, 1)= 1E-03   $   TOLER(16, 2)= 1E-02
  TOLER(17, 1)= 1E-02   $   TOLER(17, 2)= 1E-01
  TOLER(18, 1)= 1E-04   $   TOLER(18, 2)= 1E-03
  TOLER(19, 1)= 1E-04   $   TOLER(19, 2)= 1E-03
  TOLER(20, 1)= 1E-03   $   TOLER(20, 2)= 1E-02
  TOLER(21, 1)= 1E-03   $   TOLER(21, 2)= 1E-02
  TOLER(22, 1)= 1E-03   $   TOLER(22, 2)= 1E-02
  TOLER(23, 1)= 1E-03   $   TOLER(23, 2)= 1E-02
  TOLER(24, 1)= 1E-03   $   TOLER(24, 2)= 1E-02
  TOLER(25, 1)= 1E-15   $   TOLER(25, 2)= 1E-14
  TOLER(26, 1)= 1E-15   $   TOLER(26, 2)= 1E-14
  TOLER(27, 1)= 1E-15   $   TOLER(27, 2)= 1E-14
  TOLER(28, 1)= 1E-15   $   TOLER(28, 2)= 1E-14
  TOLER(29, 1)= 1E-15   $   TOLER(29, 2)= 1E-14
  TOLER(30, 1)= 1E-15   $   TOLER(30, 2)= 1E-14
  TOLER(31, 1)= 1E-15   $   TOLER(31, 2)= 1E-14
  TOLER(32, 1)= 1E-15   $   TOLER(32, 2)= 1E-14
  TOLER(33, 1)= 1E-15   $   TOLER(33, 2)= 1E-14
  TOLER(34, 1)= 1E-03   $   TOLER(34, 2)= 1E-02
  TOLER(35, 1)= 1E-15   $   TOLER(35, 2)= 1E-14
  TOLER(36, 1)= 1E-03   $   TOLER(36, 2)= 1E-02
  TOLER(37, 1)= 1E-15   $   TOLER(37, 2)= 1E-14
  TOLER(38, 1)= 1E-03   $   TOLER(38, 2)= 1E-02
  TOLER(39, 1)= 1E-03   $   TOLER(39, 2)= 1E-02
  TOLER(40, 1)= 1E-03   $   TOLER(40, 2)= 1E-02
  TOLER(41, 1)= 1E-02   $   TOLER(41, 2)= 1E-01
  TOLER(42, 1)= 1E-03   $   TOLER(42, 2)= 1E-02
  TOLER(43, 1)= 1E-02   $   TOLER(43, 2)= 1E-01
  TOLER(44, 1)= 1E-15   $   TOLER(44, 2)= 1E-14
  TOLER(45, 1)= 1E-03   $   TOLER(45, 2)= 1E-02
  TOLER(46, 1)= 1E-03   $   TOLER(46, 2)= 1E-02
  TOLER(47, 1)= 1E-03   $   TOLER(47, 2)= 1E-02
  TOLER(48, 1)= 1E-15   $   TOLER(48, 2)= 1E-14
  TOLER(49, 1)= 1E-06   $   TOLER(49, 2)= 1E-05
  TOLER(50, 1)= 1E-06   $   TOLER(50, 2)= 1E-05
  TOLER(51, 1)= 1E-06   $   TOLER(51, 2)= 1E-05
  TOLER(52, 1)= 1E-06   $   TOLER(52, 2)= 1E-05
  TOLER(53, 1)= 1E-06   $   TOLER(53, 2)= 1E-05
  TOLER(54, 1)= 1E-06   $   TOLER(54, 2)= 1E-05
  TOLER(55, 1)= 1E-06   $   TOLER(55, 2)= 1E-05
  TOLER(56, 1)= 1E-06   $   TOLER(56, 2)= 1E-05
  TOLER(57, 1)= 1E-06   $   TOLER(57, 2)= 1E-05
  TOLER(58, 1)= 1E-06   $   TOLER(58, 2)= 1E-05
  TOLER(59, 1)= 1E-06   $   TOLER(59, 2)= 1E-05
  TOLER(60, 1)= 1E-06   $   TOLER(60, 2)= 1E-05
  TOLER(61, 1)= 1E-06   $   TOLER(61, 2)= 1E-05
  TOLER(62, 1)= 1E-06   $   TOLER(62, 2)= 1E-05
  TOLER(63, 1)= 1E-06   $   TOLER(63, 2)= 1E-05
  TOLER(64, 1)= 1E-06   $   TOLER(64, 2)= 1E-05

!--------------------------------------------------------------------------------------
! Results comparison
!--------------------------------------------------------------------------------------
  COMPARA.MAC

Results

LabelTargetCivilFEMRatioTolerance
TX_I2.4011e+0062.4011e+0061.000 1
TX_J2.4011e+0062.4011e+0061.000 1
TX_K2.9041e+0052.9041e+0051.000 0.1
TX_L2.9041e+0052.9041e+0051.000 0.1
TY_I2.6915e+0052.6915e+0051.000 0.1
TY_J-3.194e+005-3.194e+0051.000 0.1
TY_K-3.194e+005-3.194e+0051.000 0.1
TY_L2.6915e+0052.6915e+0051.000 0.1
TXY_I5.6584e+0055.6584e+0051.000 0.1
TXY_J5.6584e+0055.6584e+0051.000 0.1
TXY_K5.6584e+0055.6584e+0051.000 0.1
TXY_L5.6584e+0055.6584e+0051.000 0.1
MX_I-1.1924e+005-1.1924e+0051.000 0.1
MX_J -11423 -114231.000 0.01
MX_K-1.1402e+005-1.1402e+0051.000 0.1
MX_L 60806 608061.000 0.01
MY_I -35664 -356641.000 0.1
MY_J -8693 -86931.000 0.001
MY_K -2679.6 -2679.61.000 0.001
MY_L 23978 239781.000 0.01
MXY_I 13340 133401.000 0.01
MXY_J 36653 366531.000 0.01
MXY_K 47026 470261.000 0.01
MXY_L 23714 237141.000 0.01
NX_I 0 00.000 1e-014
NX_J 0 00.000 1e-014
NX_K 0 00.000 1e-014
NX_L 0 00.000 1e-014
NY_I 0 00.000 1e-014
NY_J 0 00.000 1e-014
NY_K 0 00.000 1e-014
NY_L 0 00.000 1e-014
MDxi_I 0 00.000 1e-014
MDxi_J 25230 252301.000 0.01
MDxi_K 0 00.000 1e-014
MDxi_L 84520 845201.000 0.01
MDyi_I 0 00.000 1e-014
MDyi_J 27960 279601.000 0.01
MDyi_K 16715 167151.000 0.01
MDyi_L 47692 476921.000 0.01
MDxs_I-1.3258e+005-1.3258e+0051.000 0.1
MDxs_J -48075 -480751.000 0.01
MDxs_K-1.6105e+005-1.6105e+0051.000 0.1
MDxs_L 0 00.000 1e-014
MDys_I -49004 -490041.000 0.01
MDys_J -45346 -453461.000 0.01
MDys_K -49706 -497061.000 0.01
MDys_L 0 00.000 1e-014
ASxi_I 0.004276 0.0042761.000 1e-005
ASxi_J0.000872420.000872421.000 1e-005
ASxi_K 0.005759 0.0057591.000 1e-005
ASxi_L 0.003678 0.0036781.000 1e-005
ASyi_I 0 00.000 1e-005
ASyi_J0.000981590.000981591.000 1e-005
ASyi_K0.000553640.000553641.000 1e-005
ASyi_L 0.0019312 0.00193121.000 1e-005
ASxs_I 0.0059029 0.00590291.000 1e-005
ASxs_J 0.0019539 0.00195391.000 1e-005
ASxs_K 0.0072211 0.00722111.000 1e-005
ASxs_L 0.0017731 0.00177311.000 1e-005
ASys_I 0.0020099 0.00200991.000 1e-005
ASys_J 0.0017973 0.00179731.000 1e-005
ASys_K 0.0020532 0.00205321.000 1e-005
ASys_L 0 00.000 1e-005

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