CFVR0986 - Shell shear reinforcement check according to ACI 318 14

Shell shear reinforcement check according to ACI 318 14.

The model is made up of two square shell elements of 1.0m x 1.0m. Boundary conditions: + Node located at origin has its vertical movement restrained(perpendicular to the shells). + Node located at X=0 and Y=100 cm are completely restrained. + Node located at X=100 and Y=100 cm has its vertical movement restrained(perpendicular to the shells). Applied loads: + Pressure of 3 kg/cm² on one of the elements. + Punctual tension force of 50 kp (X=200,Y=0). + Punctual compression force of 100 kp (X=200,Y=100).
There is no bending reinforcement in the slab. The reinforcement checking code is the ACI 318 14.

Element types used in the model: SHELL43

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

ACI 318 14

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: CFVR0986.DAT

   FINISH
  ~cfclear,,1
   NomFile='CFVR0986'
  /TITLE, %NomFile%, Shell shear reinforcement check according to ACI 318 14
! ---------------------------------------------------------------------------------
! Model definition and solve
! ---------------------------------------------------------------------------------

! Setup
 ~UNITS,,MONE,EURO
 ~UNITS,,LENG,CM
 ~UNITS,,TIME,S
 ~UNITS,,FORC,KP
 ~CODESEL,EC3-05,ACI_14,EC2-08,,EC8-04
 ~CFCONFG,PLRES   ,SHELL   ,EPSW 
 ~CFCONFG,RESULT,CFSHF,1
 
  /PREP7
! Materials
  ~CFMP,5,LIB,CONCRETE,EC2,C40/50
  ~CFMP,2,LIB,REINF,EC2,S400
  ~CFMP,5,ACI_14_C,Lambda  ,,0.8  
! Element types
  ET,2,SHELL43
! Shell Vertex
  t=25     ! Thickness
  r=4      ! Cover
  th = 0   ! Reinforcement angle
 ~SHLRNF,1,t,5,2,r,0.0,0.0,0.0,0.0,0,th,45
 ~SHLSHR,1,2,5.770E-03,,,,,,,

 

! Beam & Shell property
 ~BMSHPRO,10,SHELL,1,1,1,1,43,,,,Shell property

! Nodes
  N,10,0,0
  N,20,100,0
  N,30,200,0
  N,40,0,100
  N,50,100,100
  N,60,200,100
! Elements
  MAT,5
  REAL,10
  TYPE,2
  EN,100, 10, 20, 50, 40
  EN,200, 20, 30, 60, 50
! Boundary conditions
  D,10,UZ,0.0
  D,40,ALL,
  D,50,UZ,
! Solve
  /SOLU
  SFE,100,2,PRES,,3.0
  F,30,FY,50
  F,60,FX,-100
  SOLVE

  /POST1
! ---------------------------------------------------------------------------------
! Check with CivilFEM
! ---------------------------------------------------------------------------------
 ~CFSET,,1
 ~CHKCON,SHELL,SHEAR, , , ,1, , , , , ,0  ! Phi=.75 ; fy unlimited 
 ~CFSET,1

!--------------------------------------------------------------------------------------
! DATA CHECK
!--------------------------------------------------------------------------------------
! Data comparison number
  NComp = 11
  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( 1,1) = 'VC_X'
  LABEL( 2,1) = 'VS_X'
  LABEL( 3,1) = 'VN_X'
  LABEL( 4,1) = 'VFI_X'
  LABEL( 5,1) = 'CRT_X'
  LABEL( 6,1) = 'VC_Y'
  LABEL( 7,1) = 'VS_Y'
  LABEL( 8,1) = 'VN_Y'
  LABEL( 9,1) = 'VFI_Y'
  LABEL( 10,1) = 'CRT_Y'
  LABEL( 11,1) = 'CRT_TOT'

! Correct values
  VALUE( 1,1)=180.2875
  VALUE( 2,1)=247.136
  VALUE( 3,1)=426.85
  VALUE( 4,1)=320.14
  VALUE( 5,1)=0.834973
  VALUE( 6,1)=180.00375
  VALUE( 7,1)=247.136
  VALUE( 8,1)=427.13975
  VALUE( 9,1)=320.354813
  VALUE(10,1)=0.4145
  VALUE(11,1)=0.834973


! Comparison
 ESEL,S,ELEM,,100
 ~PLSHCON,VC_X 
 *GET,VALUE(1,2),NODE,10,EPSW
~PLSHCON,VS_X 
 *GET,VALUE(2,2),NODE,10,EPSW
~PLSHCON,VN_X  
 *GET,VALUE(3,2),NODE,10,EPSW
~PLSHCON,VFI_X 
 *GET,VALUE(4,2),NODE,10,EPSW
~PLSHCON,CRT_X  
 *GET,VALUE(5,2),NODE,10,EPSW
~PLSHCON,VC_Y 
 *GET,VALUE(6,2),NODE,10,EPSW
~PLSHCON,VS_Y 
 *GET,VALUE(7,2),NODE,10,EPSW
~PLSHCON,VN_Y   
 *GET,VALUE(8,2),NODE,10,EPSW
~PLSHCON,VFI_Y 
 *GET,VALUE(9,2),NODE,10,EPSW
~PLSHCON,CRT_Y  
 *GET,VALUE(10,2),NODE,10,EPSW
 ~PLSHCON,CRT_TOT  
 *GET,VALUE(11,2),NODE,10,EPSW
 

! Warning and error tolerances
  TOLER( 1,1)= 1E0   $ TOLER( 1,2)= 1E0
  TOLER( 2,1)= 1E0   $ TOLER( 2,2)= 1E0
  TOLER( 3,1)= 1E0   $ TOLER( 3,2)= 1E0
  TOLER( 4,1)= 1E0   $ TOLER( 4,2)= 1E0
  TOLER( 5,1)= 1E-03 $ TOLER( 5,2)= 1E-03
  TOLER( 6,1)= 1E0   $ TOLER( 6,2)= 1E0
  TOLER( 7,1)= 1E0   $ TOLER( 7,2)= 1E0
  TOLER( 8,1)= 1E0   $ TOLER( 8,2)= 1E0
  TOLER( 9,1)= 1E0   $ TOLER( 9,2)= 1E0
  TOLER(10,1)= 1E-03 $ TOLER(10,2)= 1E-03
  TOLER(11,1)= 1E-03 $ TOLER(11,2)= 1E-03

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

Results

Label	Target	CivilFEM	Ratio	Tolerance
VC_X	180.29	180.06	1.001	1
VS_X	247.14	247.12	1.000	1
VN_X	426.85	427.18	0.999	1
VFI_X	320.14	320.39	0.999	1
CRT_X	0.83497	0.83433	1.001	0.001
VC_Y	180	180.63	0.997	1
VS_Y	247.14	247.12	1.000	1
VN_Y	427.14	427.75	0.999	1
VFI_Y	320.35	320.81	0.999	1
CRT_Y	0.4145	0.41386	1.002	0.001
CRT_TOT	0.83497	0.83433	1.001	0.001

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CFVR0986 - Shell shear reinforcement check according to ACI 318 14

Shell shear reinforcement check according to ACI 318 14.

Results