CFVR0989 - In-Plane Shear Calculation – ACI 349 06 WALLS - seismic/non-seismic
Check of reinforcement for in-plane shear and membrane forces
To investigate the design of reinforcement for in-plane shear and membrane forces for ACI 349 06, a simple 5 ft x 25 ft x 1 ft slab model was used.
The 5-element model consists of Shell43 elements. Vertical and lateral loads were applied at nodes 3 and 8.
The wall is restrained at nodes 1 and 2 at the base of the model. Node 1 is restrained in the x, y, and z directions for translation as well as rotation in the x and z directions.
Node 2 is restrained in the y and z directions for translation as well as rotation in the x and z directions.
Element types used in the model: SHELL43 Needed CivilFEM Modules: |
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| Model Statistics | |
| Number of elements | 5 |
| Number of nodes | 12 |
| Number of civil materials | 2 |
| Number of cross sections | 0 |
| Number of shell vertices | 1 |
Log file: CFVR0989.dat
FINISH ~CFCLEAR,,1 NomFile='CFVR0989' /TITLE, %NomFile%,In-Plane Shear Calculation, ACI 349 06 Wall ~CODESEL,,ACI34906 ~UNITS,,LENG,IN ~UNITS,,FORC,LBF ~UNITS,,PRES,,0 ,uuP ! ~CFCONFG,RESULT,CFSHF,1 !------------------------------------------------------------------------------- ! Model definition !------------------------------------------------------------------------------- THK = 1*12.0 ! shell thickness COVER = 0.8 ! cover WDTH = 5*12.0 ! wall width L = 25*12.0 ! wall heigth /PREP7 ET,1,SHELL43 ~CFMP,1,LIB,CONCRETE,ACI,fc_6000 ~CFMP,1,USER ~CFMP,1,ACI_C ,fc_t ,,6000 ,7,0,0 ~CFMP,2,LIB,REINF,ACI,fy_60000 ~SHLRNF,1,THK,1,2,COVER ! Bending Reinforcement ! ~SHLSHR, IVTX, MATOP,ASSOP, PHIOP, NXOP, NYOP, SXOP, SYOP, ASSOPX, ASSOPY ~SHLSHR, 1, 2, , , , , , , ! Shear Reinforcement ! ~SHLIPSH,IVTX, MATIP, ASSIPX, ASSIPY ~SHLIPSH, 1, 2, 0.0987,0.08334 ! In-plane Reinforcement ~BMSHPRO,1,SHELL,1,1,1,1,43,,,,Shell 1 ! VERIFICAMOS CON NUEVOS CHEQUEOS LAS MEJORAS REALIZADAS CON LA ACI 349-13 !------------------------------------------------------------------------------- ~MEMBPRO,1,ACI349,ALL,,1.5 ~BMSHPRO,1,SHELL,1,1,1,1, 43,1,, ,Shell 1 K,1 K,2, ,,L K,3,WDTH,,L K,4,WDTH,, A,1,2,3,4 TYPE,1 REAL,1 MAT,1 AESIZE,ALL,5*12.0, MSHAPE,0,2D MSHKEY,1 AMESH,ALL LOCAL,11,0,-10,0,0,-90,,-90,1,1, EMODIF,ALL,ESYS,11, ! Y Element horizontal, x Element vertical CSYS,0 /VIEW,1,,-1 /SOLU ! Node 1 is restrained in x,y,z directions for translation ! as well as rotation in the x and z directions D,1, , , , , ,UX,UY,UZ,ROTX,ROTZ, ! Node 2 is restrained in y,z directions for translation ! as well as rotation in the x and z directions D,8, , , , , ,UY,UZ,ROTX,ROTZ, , ALLSEL F,2,FX,140000 F,2,FY,80000 F,2,FZ,-40000 F,7,FX,140000 F,7,FY,80000 F,7,FZ,-40000 ALLSEL SOLVE /POST1 ~CFSET,,1 ESEL,S,,,1 ~DIMCON,SHELL, IPSHEAR,,,, 1, , 1 , 1 ! VAL1=1-> Walls non-seismic loads, VAL3=1->Fi=0.85 VAL4=2->Y=direccion vertical ~DIMCON,SHELL, IPSHEAR,,,, 2, , 1 , 1 ! VAL1=1-> Walls seismic loads , VAL3=1->Fi=0.85 VAL4=2->Y=direccion vertical !-------------------------------------------------------------------------------------- ! DATA CHECK !-------------------------------------------------------------------------------------- ! Data comparison number NComp = 16 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 ! Correct values ~CFGET,Txy_Shell, ELEMENT, 1, FORCE,TXY, I ! In-plane shear ! Walls non-seismic design VALUE( 1,1) = 1487.23 ! VC_Y, VALUE( 2,1) = 753.892 ! VC_X, VALUE( 3,1) = 0.098645 ! AIPSS_Y, VALUE( 4,1) = 0.113923 ! AIPSS_X, VALUE( 5,1) = ABS(Txy_Shell/5577.096) ! CRT_2_X, VALUE( 6,1) = ABS(Txy_Shell/5577.096) ! CRT_2_Y, VALUE( 7,1) = 0.0025*12/0.098645 ! CRT_3_Y, VALUE( 8,1) = 0.5646 ! CRT_3_X, ! Walls seismic design VALUE( 9,1) = 1487.23*3.0/2.0 ! VC_Y, VALUE(10,1) = 753.892 ! VC_X, VALUE(11,1) = 0.083154 ! AIPSS_Y, VALUE(12,1) = 0.113923 ! AIPSS_X, VALUE(13,1) = ABS(Txy_Shell/5577.096) ! CRT_2_X, VALUE(14,1) = ABS(Txy_Shell/5577.096) ! CRT_2_Y, VALUE(15,1) = 0.360778 ! CRT_3_Y, VALUE(16,1) = 0.4959 ! CRT_3_X, ! CivilFEM values ~CFSET,1 ! Walls non-seismic design ~CFGET,VALUE( 1,2), ELEMENT, 1 ,RESULT , VC_Y, I ~CFGET,VALUE( 2,2), ELEMENT, 1 ,RESULT , VC_X, I ~CFGET,VALUE( 3,2), ELEMENT, 1 ,RESULT , AIPSS_Y, I ~CFGET,VALUE( 4,2), ELEMENT, 1 ,RESULT , AIPSS_X, I ~CFGET,VALUE( 5,2), ELEMENT, 1 ,RESULT , CRT_2_X, I ~CFGET,VALUE( 6,2), ELEMENT, 1 ,RESULT , CRT_2_Y, I ~CFGET,VALUE( 7,2), ELEMENT, 1 ,RESULT , CRT_3_Y, I ~CFGET,VALUE( 8,2), ELEMENT, 1 ,RESULT , CRT_3_X, I ~CFSET,2 ! Walls seismic design ~CFGET,VALUE( 9,2), ELEMENT, 1 ,RESULT , VC_Y, I ~CFGET,VALUE(10,2), ELEMENT, 1 ,RESULT , VC_X, I ~CFGET,VALUE(11,2), ELEMENT, 1 ,RESULT , AIPSS_Y, I ~CFGET,VALUE(12,2), ELEMENT, 1 ,RESULT , AIPSS_X, I ~CFGET,VALUE(13,2), ELEMENT, 1 ,RESULT , CRT_2_X, I ~CFGET,VALUE(14,2), ELEMENT, 1 ,RESULT , CRT_2_Y, I ~CFGET,VALUE(15,2), ELEMENT, 1 ,RESULT , CRT_3_Y, I ~CFGET,VALUE(16,2), ELEMENT, 1 ,RESULT , CRT_3_X, I ! Labels LABEL( 1,1) = 'NS_VCY' ! ACI 349-01 Ch.14 (11.10.5) LABEL( 2,1) = 'NS_VCX' ! ACI 349-01 Ch.14 (11.3.2.3) LABEL( 3,1) = 'NSAIPSSY' ! ACI 349-01 Ch.14 (11.10.9.1) eq.11-33 LABEL( 4,1) = 'NSAIPSSX' LABEL( 5,1) = 'NSCRT_2X' ! ACI 349-01 Ch.14 (11.10.3) LABEL( 6,1) = 'NSCRT_2Y' LABEL( 7,1) = 'NSCRT_3Y' ! ACI 349-01 Ch.14 (11.10.9.2) LABEL( 8,1) = 'NSCRT_3X' LABEL( 9,1) = 'S_VC_Y' LABEL(10,1) = 'S_VC_X' ! ACI 349-01 Ch.14 (11.3.2.3) LABEL(11,1) = 'S_AIPSSY' ! ACI 349-01 Ch.21 (21.6.5.2) eq.11-33 LABEL(12,1) = 'S_AIPSSX' LABEL(13,1) = 'S_CRT_2X' ! ACI 349-01 Ch.21 (21.6.5.6) LABEL(14,1) = 'S_CRT_2Y' LABEL(15,1) = 'S_CRT_3Y' ! ACI 349-01 Ch.21 (21.6.2.1) LABEL(16,1) = 'S_CRT_3X' ! Warning and error tolerances TOLER( 1,1)= 1E-2 $ TOLER( 1,2)= 1E-2 TOLER( 2,1)= 1E-2 $ TOLER( 2,2)= 1E-2 TOLER( 3,1)= 1E-1 $ TOLER( 3,2)= 1E-2 TOLER( 4,1)= 1E-1 $ TOLER( 4,2)= 1E-2 TOLER( 5,1)= 1E-2 $ TOLER( 5,2)= 1E-2 TOLER( 6,1)= 1E-2 $ TOLER( 6,2)= 1E-2 TOLER( 7,1)= 1E-2 $ TOLER( 7,2)= 1E-2 TOLER( 8,1)= 1E-2 $ TOLER( 8,2)= 1E-2 TOLER( 9,1)= 1E-2 $ TOLER( 9,2)= 1E-2 TOLER(10,1)= 1E-2 $ TOLER(10,2)= 1E-2 TOLER(11,1)= 1E-2 $ TOLER(11,2)= 1E-2 TOLER(12,1)= 1E-2 $ TOLER(12,2)= 1E-2 TOLER(13,1)= 1E-1 $ TOLER(13,2)= 1E-2 TOLER(14,1)= 1E-1 $ TOLER(14,2)= 1E-2 TOLER(15,1)= 1E-2 $ TOLER(15,2)= 1E-2 TOLER(16,1)= 1E-2 $ TOLER(16,2)= 1E-2 !------------------------------------------------------------------------------- ! Results comparison !------------------------------------------------------------------------------- COMPARA.MAC |
Results
| Label | Target | CivilFEM | Ratio | Tolerance |
| NS_VCY | 1487.2 | 1487.2 | 1.000 | 0.01 |
| NS_VCX | 753.89 | 753.89 | 1.000 | 0.01 |
| NSAIPSSY | 0.098645 | 0.098646 | 1.000 | 0.01 |
| NSAIPSSX | 0.11392 | 0.11392 | 1.000 | 0.01 |
| NSCRT_2X | 0.83676 | 0.83676 | 1.000 | 0.01 |
| NSCRT_2Y | 0.83676 | 0.83676 | 1.000 | 0.01 |
| NSCRT_3Y | 0.30412 | 0.30412 | 1.000 | 0.01 |
| NSCRT_3X | 0.5646 | 0.56461 | 1.000 | 0.01 |
| S_VC_Y | 2230.8 | 2230.8 | 1.000 | 0.01 |
| S_VC_X | 753.89 | 753.89 | 1.000 | 0.01 |
| S_AIPSSY | 0.083154 | 0.083154 | 1.000 | 0.01 |
| S_AIPSSX | 0.11392 | 0.11392 | 1.000 | 0.01 |
| S_CRT_2X | 0.83676 | 0.83676 | 1.000 | 0.01 |
| S_CRT_2Y | 0.83676 | 0.83676 | 1.000 | 0.01 |
| S_CRT_3Y | 0.36078 | 0.36078 | 1.000 | 0.01 |
| S_CRT_3X | 0.4959 | 0.49662 | 0.999 | 0.01 |
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