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CFVR0919 - Shell reinforcement design according to NBR6118

Shell reinforcement design according to the Brazilian code NBR6118 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
NBR 6118

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: CFVR0919.DAT


   FINISH
  ~CFCLEAR,,1
   NomFile='CFVR0919'
  /TITLE, %NomFile%, Shell reinforcement design according to NBR6118
! ---------------------------------------------------------------------------------
! Model definition and analysis
! ---------------------------------------------------------------------------------

! Setup
 ~UNITS,SI
 ~CODESEL,EC3-92,NBR6118,,,EC8-94
 ~CFCONFG,PLRES   ,SHELL   ,EPSW 
 ~CFCONFG,RESULT,CFSHF,1

/PREP7
! Materials
 ~CFMP,5,LIB,CONCRETE,NBR6118,C40
 ~CFMP,2,LIB,REINF,NBR6118,CA50
! 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,NBR_C,FCD
 ~CFGET,FYD,MATERIAL,2,NBR_S,FYD
 ~CFGET,GAMMAC,MATERIAL,5,NBR_C,GAMC
 ~CFGET,GAMMAS,MATERIAL,2,NBR_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_I2.2173e+0062.2173e+0061.000 1
TX_J2.2173e+0062.2173e+0061.000 1
TX_K2.6818e+0052.6818e+0051.000 0.1
TX_L2.6818e+0052.6818e+0051.000 0.1
TY_I2.4855e+0052.4855e+0051.000 0.1
TY_J-2.9496e+005-2.9496e+0051.000 0.1
TY_K-2.9496e+005-2.9496e+0051.000 0.1
TY_L2.4855e+0052.4855e+0051.000 0.1
TXY_I5.2253e+0055.2253e+0051.000 0.1
TXY_J5.2253e+0055.2253e+0051.000 0.1
TXY_K5.2253e+0055.2253e+0051.000 0.1
TXY_L5.2253e+0055.2253e+0051.000 0.1
MX_I-1.1011e+005-1.1011e+0051.000 0.1
MX_J -10548 -105481.000 0.01
MX_K-1.053e+005-1.053e+0051.000 0.1
MX_L 56153 561531.000 0.01
MY_I -32934 -329341.000 0.1
MY_J -8027.7 -8027.71.000 0.001
MY_K -2474.6 -2474.61.000 0.001
MY_L 22143 221431.000 0.01
MXY_I 12319 123191.000 0.01
MXY_J 33847 338471.000 0.01
MXY_K 43427 434271.000 0.01
MXY_L 21899 218991.000 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 23299 232991.000 0.01
MDxi_K 0 00.000 1e-014
MDxi_L 78052 780521.000 0.01
MDyi_I 0 00.000 1e-014
MDyi_J 25820 258201.000 0.01
MDyi_K 15436 154361.000 0.01
MDyi_L 44042 440421.000 0.01
MDxs_I-1.2243e+005-1.2243e+0051.000 0.1
MDxs_J -44396 -443961.000 0.01
MDxs_K-1.4872e+005-1.4872e+0051.000 0.1
MDxs_L 0 00.000 1e-014
MDys_I -45254 -452541.000 0.01
MDys_J -41875 -418751.000 0.01
MDys_K -45902 -459021.000 0.01
MDys_L 0 00.000 1e-014
ASxi_I 0.0025761 0.00257611.000 1e-005
ASxi_J0.000638920.000638921.000 1e-005
ASxi_K 0.0038461 0.00384611.000 1e-005
ASxi_L 0.0027019 0.00270191.000 1e-005
ASyi_I 0 00.000 1e-005
ASyi_J0.000714190.000714191.000 1e-005
ASyi_K0.000412610.000412611.000 1e-005
ASyi_L 0.0013078 0.00130781.000 1e-005
ASxs_I 0.004403 0.0044031.000 1e-005
ASxs_J 0.0013203 0.00132031.000 1e-005
ASxs_K 0.005411 0.0054111.000 1e-005
ASxs_L0.000432680.000432681.000 1e-005
ASys_I 0.001351 0.0013511.000 1e-005
ASys_J 0.0012318 0.00123181.000 1e-005
ASys_K 0.0013743 0.00137431.000 1e-005
ASys_L 0 00.000 1e-005

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