CFVR8694 - AISC15: Chapter D Design of Members for Tension.
Compression check according to AISC/ASD15 - RECTANGULAR HSS TENSION MEMBER.
A HSS-shape column is subjected to a tension force.
The aim of the example is to obtain the tensile criterion according to AISC15 (LRFD/ASD). REFERENCE: Volume 1: Design Examples Version 15.1 EXAMPLE D.4 RECTANGULAR HSS TENSION MEMBER
Element types used in the model: BEAM188 Needed CivilFEM Modules: |
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| Model Statistics | |
| Number of elements | 1 |
| Number of nodes | 2 |
| Number of civil materials | 1 |
| Number of cross sections | 1 |
| Number of shell vertices | 0 |
Log file: CFVR8694.DAT
FINISH ~CFCLEAR,,1 NomFile='CFVR8694' /TITLE, %NomFile%, AISC15: Tension Check !-------------------------------------------------------------------------------------- ! Model definition !-------------------------------------------------------------------------------------- ! CivilFEM Setup: Code & Units ~UNITS,,LENG,IN ~UNITS,,TIME,S ~UNITS,,FORC,KIPS! in, sec, Kips ~CODESEL,AISC15 ! Parameters P = 224 ! Axial force kips Fyy = 50 ! ksi Fuu = 62 ! ksi /PREP7 ! Preprocessor ! -------------------------------------------------- ! Materials ~CFMP,1,LIB,STEEL,ASTM,A36 ! ASTM A500 Grade C ~CFMP,1,NAME,,,ASTM A500 Grade C ~CFMP,1,USER ~CFMP,1,AISC15 ,Fy,,Fyy ,1,0,0 ~CFMP,1,AISC15 ,Fu,,Fuu ,1,0,0 ! Element Types ET,1,188 ! Type 1: 3D Beam ! Cross Section ~SSECLIB,1,1,61,246 ! HSS 6x4X3/8 ~SECMDF,1,MECHPROP,A ,,6.18,2,0,0 ~SECMDF,1,UPDATE aholes = 0.39 ! gap in fit-up between the HSS and the gusset plate ~SECMDF,1,AISC15PR,AHOLES ,,aholes,0,0,0 ! area of holes ! Shear leg factor is not included (always 1), so when Shear leg factor < 1, ! net area must be modified to obtain the correcect effective net section ~CFGET, AN, SECTION, 1, MECHPROP, A,, 3 ~SECMDF,1,MECHPROP,A ,,AN*0.90,3,0,0 ~SECMDF,1,UPDATE ! Beam & Shell Property ~BMSHPRO,1,BEAM,1,1,,,188,1,0,,Beam 1 ! Nodes N,1 N,2,,2 ! Elements SECNUM,1 REAL,1 E,1,2 /SOLU ! Solution ! -------------------------------------------------- ! Constrains D,1,ALL ! Apply Load F,2,FY,P ! Solve SOLVE /POST1 ! Postprocessor ! -------------------------------------------------- ! Read results ~CFSET,,1 ! First load case ! Checking ~CHKSTL,TENSION,Z,LRFD ~CHKSTL,TENSION,Z,ASD !-------------------------------------------------------------------------------------- ! DATA CHECK !-------------------------------------------------------------------------------------- ! Data comparison number NComp = 6 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) = 'CLS_COMP' LABEL(5,1) = 'CRT_LRFD' LABEL(6,1) = 'CRT_ASD' ! Correct values VALUE(1,1)=278 ! Tensile Yielding strength in gross section VALUE(2,1)=242 ! available tensile rupture strength VALUE(3,1)=242 ! available tensile strength VALUE(4,1)=1.00 ! VALUE(5,1)=0.925 ! LRFD CRITERION VALUE(6,1)=1.382 ! ASD CRITERION ! Comparison ~CFSET,1 ! LRFD ~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,CLS_COMP,I ~CFGET,VALUE(5,2),ELEMENT,1,RESULT,CRT_TOT,I ~CFSET,2 ! ASD ~CFGET,VALUE(6,2),ELEMENT,1,RESULT,CRT_TOT,I ! Warning and error tolerances *DO,JJ,1,6 TOLER(JJ,1)= 0.04*VALUE(JJ,1) $ TOLER(JJ,2)= 0.04*VALUE(JJ,1) *ENDDO !-------------------------------------------------------------------------------------- ! Results comparison !-------------------------------------------------------------------------------------- COMPARA.MAC |
Results
| Label | Target | CivilFEM | Ratio | Tolerance |
| FIPNG | 278 | 278.1 | 1.000 | 11.12 |
| FIPNE | 242 | 242.31 | 0.999 | 9.68 |
| FIPN | 242 | 242.31 | 0.999 | 9.68 |
| CLS_COMP | 1 | 1 | 1.000 | 0.04 |
| CRT_LRFD | 0.925 | 0.92443 | 1.001 | 0.037 |
| CRT_ASD | 1.382 | 1.3866 | 0.997 | 0.05528 |
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