CFVR5230 - Prestressed rectangular solid model.
Prestress loads on rectangular solid model.
The model is a prestressed rectangular solid segment of 5 m length.
The beam is made of C35/45 concrete and the tendon is made of Y1860C steel.
The section is rectangular.
The aim of the example is to verify the prestress loads on rotated nodal coordinate systems.
Element types used in the model: SOLID45 Needed CivilFEM Modules: |
|

| Model Statistics | |
| Number of elements | 320 |
| Number of nodes | 525 |
| Number of civil materials | 2 |
| Number of cross sections | 0 |
| Number of shell vertices | 0 |
Log file: CFVR5230.DAT
FINISH ~CFCLEAR,,1 ~CFACTIV,PRSC,Y ~CFACTIV,NLBR,Y NomFile='CFVR5230' /TITLE, CFVR5230 - Prestressed rectangular solid model. ! ------------------------------------------------------------------------------------- ! Initial data ! ------------------------------------------------------------------------------------- ~UNITS,SI ! Parameters a=1 ! Section Width b=1 ! Section Height L=5 ! Length of the model ESIZ=0.25 ! Element size N_Ax=8.00E6 ! Axial force /PREP7 ! Elements ET,1,45 ! SOLID 45 ! Real contants R,1,0 ! Real constant for solid element (unused) ! Materials ~CFMP,1,LIB,CONCRETE,EC2,C35/45 ! EC2 C35/40 ~CFMP,2,LIB,PREST,EN10138,Y1860C ! EHE Y1860C ~CFMP,2,Prest,A ,,0 ~CFMP,2,Prest,K ,,0 ~CFMP,2,Prest,MU,,0 ~CFMP,1,USER ~CFMP,1,Concr ,ExLn ,,3.3282e+010 ! GEOMETRY AND MESHING BLOCK,-a/2,a/2,-b/2,b/2,0,5 MSHAPE,0,3D MSHKEY,1 ESIZE,ESIZ,0, VMESH,ALL /VIEW, 1, -0.54, 0.33, 0.78 EPLOT /IMAGE, SAVE, %NomFile%,BMP CSYS,0 ! Tendon geometry K,100,0.0,0.0,0.0 K,101,0.0,0.0,L LSEL,NONE L,100,101 LESIZE,13,ESIZ,, NSEL,ALL ESEL,ALL LOCAL,11, , , , ,30,45,10 NROTAT,all,all CSYS,0 /SOLU ~GENTEN,1,N_Ax,100,0.1,2,1,0 ~TENLD,1 ! Loads free prestressing tendon into the model /SOLU ! Boundary conditions NSEL,S,LOC,Z,0 D,ALL,ALL ALLSEL SOLVE /POST1 ~CFSET,,1 Node1=Node(0,0,5) !-------------------------------------------------------------------------------------- ! DATA CHECK !-------------------------------------------------------------------------------------- ! Data comparison number NComp = 5 NComp_ch = 0 ! Marix 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) = 'FX' LABEL( 2) = 'FY' LABEL( 3) = 'FZ' LABEL( 4) = 'SY' LABEL( 5) = 'USUM' ! Correct data, obtained data !-------------------------------------------------------------------------------------- VALUE( 1,1) = 982302.43 $ *GET,value( 1,2),NODE,Node1,F,FX VALUE( 2,1) = -5656854.25 $ *GET,value( 2,2),NODE,Node1,F,FY VALUE( 3,1) = -5570913.92 $ *GET,value( 3,2),NODE,Node1,F,FZ VALUE( 4,1) = -53957572.2 $ *GET,value( 4,2),NODE,Node1,S,Y VALUE( 5,1) = 2.61835E-03 $ *GET,value( 5,2),NODE,Node1,U,SUM ! Warning and error tolerances *DO,II,1,4 TOLER(II,1) = 1E2 TOLER(II,2) = 1E2 *ENDDO TOLER(5,1) = 1E-5 $ TOLER(5,2) = 1E-5 !-------------------------------------------------------------------------------------- ! Result comparison !-------------------------------------------------------------------------------------- COMPARA.MAC |
Results
| Label | Target | CivilFEM | Ratio | Tolerance |
| FX | 9.823e+005 | 9.823e+005 | 1.000 | 100 |
| FY | -5.6569e+006 | -5.6569e+006 | 1.000 | 100 |
| FZ | -5.5709e+006 | -5.5709e+006 | 1.000 | 100 |
| SY | -5.3958e+007 | -5.3958e+007 | 1.000 | 100 |
| USUM | 0.0026184 | 0.0026184 | 1.000 | 1e-005 |
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