CFVR2917 - Torsion design according to SP-52-101-03
Design a reinforced concrete beam subjected to Torsion moment according to SP-52-101-03
A fixed beam which has a rectangular reinforced concrete section is subjected to a shear force of 7.52 Mp and a torsional moment of 1.52 Mp*m.
The aim of the example is to obtain the necessary steel amount according to SP-52-101-03.
Element types used in the model: BEAM4 Needed CivilFEM Modules: |
|
| Model Statistics | |
| Number of elements | 4 |
| Number of nodes | 5 |
| Number of civil materials | 2 |
| Number of cross sections | 1 |
| Number of shell vertices | 0 |
Log file: CFVR2917.DAT
FINISH ~CFCLEAR,,1 NomFile='CFVR2917' /TITLE,%NomFile%, TORSION DESIGN ACCORDING TO SP-52-101-03 ! ------------------------------------------------------------------------------------- ! Initial data ! ------------------------------------------------------------------------------------- ! CivilFEM SETUP ~UNITS,,LENG,M ~UNITS,,TIME,S ~UNITS,,FORC,MP ~CODESEL,,SP52101 ! Preprocessor /PREP7 ! Parameters L=1 ! Length in m b=.4 ! Cross-section width in m. h=.3 ! Depth in m. T=0.95*1.6 ! Torsional moment in Mp*m Q=4.7*1.6 ! Maximum concomitant design shear force in Mp ! Material Definition ~CFMP,1,LIB,CONCRETE,SP52101,B25 ~CFMP,2,LIB,REINF,SP52101,A500 ! Element Type Definition ET,1,Beam4 ! Element Type 1: 3D Beam ! Cross-section definition ~CSECDMS,1,REC,1,0.3,0.4 ! Reinforcement definition ~RNFDEF,1,TORSION,2,1E-4,,,,1E-4, ! Beam & Shell properties ~BMSHPRO,1,BEAM,1,1,,,4,1,0,,Beam Property ! Model Construction N,1 ! Nodes input N,5,L FILL,1,5 E,1,2 ! Elements input EGEN,4,1,1,1 D,1,ALL ! Boundary conditions /SOLU F,5,FY,-Q F,5,MX,T SOLVE ! Calculation /POST1 ! Postprocessor ~CFSET,,1,1 ! Read first load step ! Torsion checking according to SP-52-101-03 ~DIMCON,SHT,TORSION !-------------------------------------------------------------------------------------- ! DATA CHECK !-------------------------------------------------------------------------------------- ! Data comparison number NComp = 4 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) = 'TS1' LABEL(2,1) = 'TSW1' LABEL(3,1) = 'ASTT' LABEL(4,1) = 'ASLT' ! Correct values VALUE(1,1)=1.1949E0 VALUE(2,1)=0.3250E0 VALUE(3,1)=6.51E-04 VALUE(4,1)=6.29E-04 ! Comparison ~PLLSCON,TS1 *GET,VALUE(1,2),ELEM,3,ETAB,CFETAB_J ~PLLSCON,TSW1 *GET,VALUE(2,2),ELEM,3,ETAB,CFETAB_J ~PLLSCON,ASTT *GET,VALUE(3,2),ELEM,3,ETAB,CFETAB_J ~PLLSCON,ASLT *GET,VALUE(4,2),ELEM,3,ETAB,CFETAB_J ! Warning and error tolerances TOLER( 1, 1)= 1E-01 $ TOLER( 1, 2)= 1E-01 TOLER( 2, 1)= 1E-02 $ TOLER( 2, 2)= 1E-02 TOLER( 3, 1)= 1E-05 $ TOLER( 3, 2)= 1E-05 TOLER( 4, 1)= 1E-05 $ TOLER( 4, 2)= 1E-05 !-------------------------------------------------------------------------------------- ! Results comparison !-------------------------------------------------------------------------------------- COMPARA.MAC |
Results
| Label | Target | CivilFEM | Ratio | Tolerance |
| TS1 | 1.1949 | 1.1943 | 1.000 | 0.1 |
| TSW1 | 0.325 | 0.32571 | 0.998 | 0.01 |
| ASTT | 0.000651 | 0.00065066 | 1.000 | 1e-005 |
| ASLT | 0.000629 | 0.00062854 | 1.001 | 1e-005 |
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