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any question any answer in Abaqus Ansys and finite element modeling
Sun, 2012-10-28 09:39 - eng.femiran
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bean frp
hi
i am ali reza
i cannot speeck english good but a need a help.my project is frp tup fill with concreat i want to modeling in ansys but i can not modelig failur tsai i need help.this is may work
/PREP7
ET,1,SOLID65
ET,2,SOLID46
R,1,,,,,,,
R,2
RMODIF,2,1,9,0,0,0
RMODIF,2,7,0
RMODIF,2,13,2,-88,.32,2,3,.35,
RMODIF,2,19,2,-88,.27,2,3,.48,
RMODIF,2,25,2,-88,.26,2,3,.51,
RMODIF,2,31,2,-88,.19,2,3,.51,
RMODIF,2,37,2,-88,.46,
CYLIND,50,0,0,100,0,90,
CYLIND,50,0,0,100,270,360,
CYLIND,51.675,50,0,100,0,90,
CYLIND,51.675,50,0,100,270,360,
CYLIND,50,0,100,650,0,90,
CYLIND,50,0,100,650,270,360,
CYLIND,51.675,50,100,650,0,90,
CYLIND,51.675,50,100,650,270,360,
VGLUE,ALL
VSEL,S,VOLU,,12,15
VATT,2,2,2,0
VSEL,S,VOLU,,1
VSEL,A,VOLU,,9,11
VATT,1,1,1,0
ALLSEL,ALL
FLST,5,9,4,ORDE,9
FITEM,5,1
FITEM,5,-2
FITEM,5,5
FITEM,5,-6
FITEM,5,47
FITEM,5,-48
FITEM,5,88
FITEM,5,91
FITEM,5,93
CM,_Y,LINE
LSEL, , , ,P51X
CM,_Y1,LINE
CMSEL,,_Y
LESIZE,ALL,25,,,,1,,,1,
VSEL,s,VOLU,,1
VSEL,A,VOLU,,9,15
VSWEEP,ALL
FINISH
/SOL
NSEL,S,LOC,Z,
DSYM,SYMM,Z, ,
NSEL,S,LOC,X,
DSYM,SYMM,X,
ALLSEL,ALL
ALLSEL,ALL
NSEL,S,LOC,Z,650
FLST,2,3,1,ORDE,3
FITEM,2,975
FITEM,2,981
FITEM,2,-982
FINISH
/PREP7
MPTEMP,,,,,,,,
MPTEMP,1,0
MPDATA,EX,1,,30413
MPDATA,PRXY,1,,0.2
TB,PLAS1,1,1,2,1
TBTEMP,0
TBPT,,0.0012,37
TBPT,,0.054,160
TB,CONC,1,1,9,
TBTEMP,0
TBDATA,,0.8,0.99,4.25,-1,,
TBDATA,,,,0.6,,,
MPTEMP,,,,,,,,
MPTEMP,1,0
MPDATA,EX,2,,38000
MPDATA,EY,2,,38000
MPDATA,EZ,2,,7800
MPDATA,NUXY,2,,0.28
MPDATA,NUYZ,2,,0.28
MPDATA,NUXZ,2,,0.28
MPDATA,GXY,2,,3500
MPDATA,GYZ,2,,3500
MPDATA,GXZ,2,,3500
NSEL,S,LOC,Z,650
FINISH
/SOL
FINISH
NSEL,S,LOC,Z,650
/SOLU
FLST,2,3,1,ORDE,2
FITEM,2,589
FITEM,2,-591
FLST,2,3,1,ORDE,2
FITEM,2,589
FITEM,2,-591
/GO
D,P51X, , , , , ,UX,UY, , , ,
ALLSEL,ALL
NSEL,S,LOC,Z,100
FLST,2,3,1,ORDE,3
FITEM,2,522
FITEM,2,524
FITEM,2,-525
/GO
F,P51X,FY,-5000
ALLSEL,ALL
FINISH
/POST1
FC,2,S,XTEN,795
FC,2,S,YTEN,39
FC,2,S,ZTEN,795
FC,2,S,XCMP,-533
FC,2,S,YCMP,-122
FC,2,S,ZCMP,-533
FC,2,S,XY,89
FC,2,S,YZ,89
FC,2,S,XZ,89
FC,2,S,XYCP,-1
FC,2,S,YZCP,-1
FC,2,S,XZCP,-1
FC,2,EPEL,XTEN,
FC,2,EPEL,YTEN,
FC,2,EPEL,ZTEN,
FC,2,EPEL,XCMP,
FC,2,EPEL,YCMP,
FC,2,EPEL,ZCMP,
FC,2,EPEL,XY,
FC,2,EPEL,YZ,
FC,2,EPEL,XZ,
FINISH
/SOL
NSUBST,50,100,1
OUTRES,ERASE
OUTRES,ALL,1
AUTOTS,1
LNSRCH,1
NEQIT,1000
SOLVE
FINISH
/POST1
SET,LIST,999
SET,,, ,,, ,86
FINISH
/POST26
FILE,'file','rst','.'
/UI,COLL,1
NUMVAR,200
SOLU,191,NCMIT
STORE,MERGE
FILLDATA,191,,,,1,1
REALVAR,191,191
NSOL,2,560,U,Y, UY_2
STORE,MERGE
FINISH
frp
Dear Alireza,
I read this codes but ansys didn't.are you sure this codes are correct?
but i guess what is your problem.
It can be related to frp material,or concrete material.give correct amounts and run again.
other thing is mesh,if your mesh sizes is large,try smaller.
be contact with us.
best regards.
www.femiran.com
frp
hi,
i am modeling concrete beam with frp
but what ( real constant and material models) should i use for frp....
thanks
FRP modeling in ABAQUS
Hello,
It depends on your analyses and FRP type.there are so many FRP types with different propertis,For example the CFRP should been modelled as an isotropic linear elastic material. the unidirectional CFRP composite actually shows an orthotropic behaviour, but it was shown in many reffrences that only the axial modulus is of importance in an application of this type. The elastic modulus and strength should taken to be E(CFRP)=165 GPa and f(CFRP)=2 GPa respectively.The Poisson ratio of the CFRP composite was assumed to be 0.3
if you has more questions I'll be glad to help you.
www.femiran.com
FRP Hashin Damage
I forgot to remind that if you want to model damage parameters for FRP, you should use Hashin Damage in ABAQUS..
good luck
www.femiran.com
frp question
hi,
i am trying to use solid185 for frp and inter205 for the cohesive .....these elements do not have real constant.....so how can i enter thiere thickness and failure criteria ?
i tryed this code but i am not sure that the program read it
for soli185
ET,7,185
keyopt,7,3,1
sectype,7,shell
secdata,1.2,,0
mp,Ex,5,165E6 !orthotropic material
mp,Ey,5,9.65E6
mp,Ez,5,9.65E6
mp,GxY,5,5.3E6
mp,GyZ,5,3.4E6
mp,GXZ,5,5.3E6
mp,PRXY,5,0.3
mp,PRYZ,5,0.45
mp,PRXZ,5,0.3
type,7
mat,5
FC,7,S,XTEN,2000
FC,7,S,YTEN,
FC,7,S,ZTEN,
FC,7,S,XCMP,-2000
FC,7,S,YCMP,
FC,7,S,ZCMP,
FC,7,S,XY,
FC,7,S,YZ,
FC,7,S,XZ,
FC,7,S,XYCP,
FC,7,S,YZCP,
FC,7,S,XZCP,
FC,7,EPEL,XTEN,
FC,7,EPEL,YTEN,
FC,7,EPEL,ZTEN,
FC,7,EPEL,XCMP,
FC,7,EPEL,YCMP,
FC,7,EPEL,ZCMP,
FC,7,EPEL,XY,
FC,7,EPEL,YZ,
FC,7,EPEL,XZ,
and for inter205
ET,6,INTER205
MPTEMP,,,,,,,,
MPTEMP,1,0
MPDATA,EX,4,,2500
MPDATA,PRXY,4,,0.4
TB,czm,4,,,expo
TBDATA,1,1.5,0.00318,0.00753
are these data enough?
and if i want to use solid46 and combin39 .....what datashould i enter?
thank you
can you tell me how to
can you tell me how to simulate the orthotropic material with elastic-plastic behavior in abaqus cae?
hi brother iam trying to
hi brother iam trying to model rc slab with opening and strengthening that opening with CFRP sheets so i tried to select the engineering constants form the elastic window and selected the hashin damage and give it damage evloution but the CFRP still dont take more than 5 KN load till failure !!! it must take about 25 KN before failure occur please help me what should i do and to make the cfrp sheet more stronger ??by the way the parameters i used for engineering constants is
80000 231000 80000 0.05 0.05 0.45 3700 79655 79655
and for the jashin damage is
4100 50 4100 50 100 100
and for damage evolution is
1 1000 1 1000
my cfrp E is 231000 Mpa and tensile strength is 4100 Mpa
so the upper parameters i calaculate them from excel sheet belong to my friend
and my cfrp sheet is unidirectional
please help . . . .