CFVR1909 - Steel checking according to British Standard 5950 1985
Lateral buckling with moments checking of a cantilever steel beam.
A steel cantilever beam is subjected to an axial compression force and moments at free end.
Determine the section class and total criterion according to BS 5950-85.
Element types used in the model: BEAM4 Needed CivilFEM Modules: |
|
| Model Statistics | |
| Number of elements | 24 |
| Number of nodes | 25 |
| Number of civil materials | 1 |
| Number of cross sections | 1 |
| Number of shell vertices | 0 |
Log file: CFVR1909.DAT
FINISH ~CFCLEAR,,1 NomFile='CFVR1909' /TITLE, %NomFile%, British Standard 5950-85: Axial compression with moments ! ------------------------------------------------------------------------------------- ! Initial data ! --------------------------------------------------------------------------------- ! CivilFEM Setup: Code & Units ~UNITS,,LENG,M ~UNITS,,TIME,S ~UNITS,,FORC,KN ~CODESEL,BS595085 /PREP7 ! Preprocessor ! -------------------------------------------------- ! Materials ~CFMP,1,LIB,STEEL,BS5950,Gr43 ! Element type ET,1,BEAM4 ! Type 1: 3D Beam ! Cross Sections ~SSECLIB,1,1,20,8 !UC 203 x 203 x 86 ! Member Properties L = 1 KLTXY = 1.0 KLTXZ = 1.0 KCXY = 1.0 KCXZ = 1.0 CteRob = 0 n = 1 m = 1 DL = 0 CFBUCKXY = 1 CFBUCKXZ = 1 CHCKAXIS = 0 ~MEMBPRO,1,BS595085,ALL,L,KLTXY,KLTXZ,KCXY,KCXZ,CteRob,n,m,DL,CFBUCKXY,CFBUCKXZ,CHCKAXIS ! Beam properties ~BMSHPRO,1,BEAM,1,1,,,4,1,0,, ! Nodes N, 1 N,25,1 FILL, 1,25 ! Elements E,1,2 EGEN,24,1,1 EPLOT /SOLU ! Solution ! -------------------------------------------------- ! Displacements D, 1,ALL ! Apply Load F,25,FX,-500 F,25,MY,30 F,25,MZ,80 ! Solve SOLVE /POST1 ! Postprocessor ! -------------------------------------------------- ! Read results ~CFSET,,1,1 ! Load first load case ! British Standard check in axial compression+bending ~CHKSTL,BUCK_BCM, ,-Z !-------------------------------------------------------------------------------------- ! DATA CHECK !-------------------------------------------------------------------------------------- ! Data comparison number NComp = 8 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) = 'CRT_AX_L' LABEL(2,1) = 'CRT_AX_0' LABEL(3,1) = 'CRT_CM_L' LABEL(4,1) = 'CRT_CM_O' LABEL(5,1) = 'CRT_TOT' LABEL(6,1) = 'PC' LABEL(7,1) = 'MB' LABEL(8,1) = 'LAMBDALT' ! Correct values VALUE(1,1)=0.172 VALUE(2,1)=0.186 VALUE(3,1)=0.79 VALUE(4,1)=0.93 VALUE( 5,1)=0.93 VALUE( 6,1)=2679 VALUE( 7,1)= 239.38 VALUE( 8,1)= 15.213 ! Obtained values ~CFSET,1 ! Load first alternative ~PLLSSTL,CRT_AX_L *GET,VALUE(1,2),ELEM,8,ETAB,CFETAB_I ~PLLSSTL,CRT_AX_O *GET,VALUE(2,2),ELEM,8,ETAB,CFETAB_I ~PLLSSTL,CRT_CM_L *GET,VALUE(3,2),ELEM,8,ETAB,CFETAB_I ~PLLSSTL,CRT_CM_O *GET,VALUE(4,2),ELEM,8,ETAB,CFETAB_I ~PLLSSTL,CRT_TOT *GET,VALUE( 5,2),ELEM,1,ETAB,CFETAB_J ~PLLSSTL,PC *GET,VALUE( 6,2),ELEM,1,ETAB,CFETAB_J ~PLLSSTL,MB *GET,VALUE( 7,2),ELEM,1,ETAB,CFETAB_J ~PLLSSTL,LAMBDALT *GET,VALUE( 8,2),ELEM,1,ETAB,CFETAB_J ! Warning and error tolerances TOLER( 1,1)= 1E-3 $ TOLER( 1,2)= 1E-3 TOLER( 2,1)= 1E-3 $ TOLER( 2,2)= 1E-3 TOLER( 3,1)= 1E-2 $ TOLER( 3,2)= 1E-2 ! Rounding error accepted TOLER( 4,1)= 1E-3 $ TOLER( 4,2)= 1E-3 TOLER( 5,1)= 1E-3 $ TOLER( 5,2)= 1E-3 TOLER( 6,1)= 1E+1 $ TOLER( 6,2)= 1E+1 ! Rounding error accepted TOLER( 7,1)= 1E-1 $ TOLER( 7,2)= 1E-1 ! Rounding error accepted TOLER( 8,1)= 1E-1 $ TOLER( 8,2)= 1E-1 ! Rounding error accepted !-------------------------------------------------------------------------------------- ! Results comparison !-------------------------------------------------------------------------------------- COMPARA.MAC |
Results
| Label | Target | CivilFEM | Ratio | Tolerance |
| CRT_AX_L | 0.172 | 0.17215 | 0.999 | 0.001 |
| CRT_AX_0 | 0.186 | 0.1868 | 0.996 | 0.001 |
| CRT_CM_L | 0.79 | 0.79665 | 0.992 | 0.01 |
| CRT_CM_O | 0.93 | 0.93051 | 1.000 | 0.001 |
| CRT_TOT | 0.93 | 0.93051 | 1.000 | 0.001 |
| PC | 2679 | 2676.7 | 1.001 | 10 |
| MB | 239.38 | 239.29 | 1.000 | 0.1 |
| LAMBDALT | 15.213 | 15.309 | 0.994 | 0.1 |
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