CFVR8851 - AASHTO12: Tension Checking L section.
Tension checking according to AASHTO12 for a cantilever beam which has a L cross section.
A cantilever steel beam is subjected to an axial tensile force of 135 kips.
The beam has a length of 21 in. The cross section is a L 4x4x1/2 with 0.87 in2 of holes area.
The beam is made of A36 steel which has a fy of 36 kips/in2.
The aim of the example is to obtain the tension criterion according to AASHTO12.
Element types used in the model: BEAM3 Needed CivilFEM Modules: |
|
| Model Statistics | |
| Number of elements | 20 |
| Number of nodes | 21 |
| Number of civil materials | 1 |
| Number of cross sections | 1 |
| Number of shell vertices | 0 |
Log file: CFVR8851.DAT
FINISH ~CFCLEAR,,1 NomFile='CFVR8851' /TITLE, %NomFile%, AASHTO12: Tension Checking L section !-------------------------------------------------------------------------------------- ! Model definition !-------------------------------------------------------------------------------------- ! CivilFEM Setup: Code & Units ~UNITS,,LENG,IN ~UNITS,,TIME,S ~UNITS,,FORC,KIPS! in, sec, Kips ~CODESEL,AASHTO12 FINISH /PREP7 ! Preprocessor ! -------------------------------------------------- ! Materials ~CFMP,1,LIB,STEEL,ASTM,A36 ! Element Types ET,1,BEAM3 ! Type 1: 2D Beam ! Cross Section ~SSECLIB,1,1,57,67 !L 4x4x1/2 ~SECMDF,1,AASH12PR,AHOLES ,,0.87,0,0,0 ! Member property ~MEMBPRO,1,NLMOD,ALL,0 ! Beam & Shell Property ~BMSHPRO,1,BEAM,1,1,,,3,1,0,,Beam 1 ! Nodes N,1 N,21,,21 FILL,1,21,19, , ,1,1,1, ! Elements REAL,1 E,1,2 EGEN,20,1,1,1 /SOLU ! Solution ! -------------------------------------------------- ! Constrains D,1,ALL ! Apply Load F,21,FY,135 ! Solve SOLVE /POST1 ! Postprocessor ! -------------------------------------------------- ! Read results ~CFSET,,1,1 ! First load case ! Checking ~CHKSTL,TENSION !-------------------------------------------------------------------------------------- ! DATA CHECK !-------------------------------------------------------------------------------------- ! Data comparison number NComp = 4 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(1,1) = 'FiPNG' LABEL(2,1) = 'FiPNE' LABEL(3,1) = 'FiPn' LABEL(4,1) = 'CRT_TOT' ! Correct values VALUE(1,1)=128.25 VALUE(2,1)=133.632 VALUE(3,1)=128.25 VALUE(4,1)=1.053 ! Comparison ~CFGET,VALUE(1,2),ELEMENT,1,RESULT,FIPNG,I ~CFGET,VALUE(2,2),ELEMENT,1,RESULT,FIPNE,I ~CFGET,VALUE(3,2),ELEMENT,1,RESULT,FIPN,I ~CFGET,VALUE(4,2),ELEMENT,1,RESULT,CRT_TOT,I ! Warning and error tolerances TOLER(1,1)= 0.001*VALUE(1,1) $ TOLER(1,2)= 0.001*VALUE(1,1) TOLER(2,1)= 0.001*VALUE(2,1) $ TOLER(2,2)= 0.001*VALUE(2,1) TOLER(3,1)= 0.001*VALUE(3,1) $ TOLER(3,2)= 0.001*VALUE(3,1) TOLER(4,1)= 0.001*VALUE(4,1) $ TOLER(4,2)= 0.001*VALUE(4,1) !-------------------------------------------------------------------------------------- ! Results comparison !-------------------------------------------------------------------------------------- COMPARA.MAC |
Results
| Label | Target | CivilFEM | Ratio | Tolerance |
| FiPNG | 128.25 | 128.25 | 1.000 | 0.1283 |
| FiPNE | 133.63 | 133.63 | 1.000 | 0.1336 |
| FiPn | 128.25 | 128.25 | 1.000 | 0.1283 |
| CRT_TOT | 1.053 | 1.0526 | 1.000 | 0.001053 |
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