CFVR1908 - Steel checking according to British Standard 5950 1985
Lateral torsional buckling check of a steel beam.
A supported steel beam with an angle built-up shape section is subjected to a uniform load of 500 KN/m.
Determine the total criterion according to BS 5950-85.
Element types used in the model: BEAM3 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: CFVR1908.DAT
FINISH ~CFCLEAR,,1 NomFile='CFVR1908' /TITLE, %NomFile%, British Standard 5950-85: Lateral torsional buckling ! ------------------------------------------------------------------------------------- ! 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,BEAM3 ! Type 1: 3D Beam ! Cross Sections ~SSECDMS,1,L,1,0.2,1.8e-002,0.15,1.8e-002,0 ! 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,,,3,1,0 ! Nodes N, 1 N,25,1 FILL, 1,25 ! Elements E,1,2 EGEN,24,1,1 EPLOT /SOLU ! Solution ! -------------------------------------------------- ! Displacements NSEL,S,,,1 NSEL,A,,,25 D,ALL,,,,,,UX,UY ALLSEL ! Apply Load SFBEAM,ALL,1,PRES,500 ! Solve SOLVE /POST1 ! Postprocessor ! -------------------------------------------------- ! Read results ~CFSET,,1,1 ! Load first load case ! British Standard check in lateral buckling ~CHKSTL,BUCK_LAT, ,-Z !-------------------------------------------------------------------------------------- ! DATA CHECK !-------------------------------------------------------------------------------------- ! Data comparison number NComp = 3 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) = 'LAMBDA' LABEL(2,1) = 'MB' LABEL(3,1) = 'CRT_TOT' ! Correct values VALUE(1,1)=22.69 VALUE(2,1)=22.11 VALUE(3,1)=2.3354 ! Obtained values ~CFSET,1 ! Load first alternative ~PLLSSTL,LAMBDA *GET,VALUE(1,2),ELEM,8,ETAB,CFETAB_I ~PLLSSTL,MB *GET,VALUE(2,2),ELEM,8,ETAB,CFETAB_I ~PLLSSTL,CRT_TOT *GET,VALUE(3,2),ELEM,8,ETAB,CFETAB_I ! Warning and error tolerances TOLER( 1,1)= 1E-2 $ TOLER( 1,2)= 1E-2 ! Rounding error accepted TOLER( 2,1)= 1E-2 $ TOLER( 2,2)= 1E-2 ! Rounding error accepted TOLER( 3,1)= 1E-3 $ TOLER( 3,2)= 1E-3 !-------------------------------------------------------------------------------------- ! Results comparison !-------------------------------------------------------------------------------------- COMPARA.MAC |
Results
| Label | Target | CivilFEM | Ratio | Tolerance |
| LAMBDA | 22.69 | 22.699 | 1.000 | 0.01 |
| MB | 22.11 | 22.116 | 1.000 | 0.01 |
| CRT_TOT | 2.3354 | 2.3354 | 1.000 | 0.001 |
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