Mesh with nodes that do not coincide

How can I solve this problem ? The nodes do not coincide and are displaced from one another

 

 

Comments

  • kkanadekkanade Forum Coordinator
    edited May 19

    where did you create this mesh?

    is it workbench meshing?

    are these bodies in different parts in SpaceClaim (or design modeler)?

    Please create multibody part and use share topology. 

    please see help manual for more details. 

    Regards,

    Keyur

     

    If this helps, please mark this post as 'Is Solution' to help others.

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    How to access ANSYS help links

     

  • VICTORVERGAVICTORVERGA Member
    edited May 20

    Hi kanade,

     

    I created this geometry using the MPDL, here is the code:

     

    ! MATERIAL CONCRETO

     

    fc = 33.50 ! 33.50 N/mm2 +- 2.5

    Ec = 28640 ! 28640 N/mm2 

    nu_c = 0.19

     

    ! Define microplane model properties

     

    k0 =

    k1 =

    k2 =

    gamma = 10e-3

    alpha = 0.96

    beta = 400

    c = 4

     

    ! MATERIAL ACO

     

    fy = 500 ! 33.50 N/mm2 +- 2.5

    Es = 210000 ! 210000 N/mm2 

    nu_s = 0.3

     

    DAP = 12.7

    AP = PI*DAP**2/4

     

     

    ! MODELO

     

    /PREP7

     

    !  CONCRETO

     

    ET,1,SOLID185

     

    ! Define elastic properties of material

    TB,ELAS,1

    TBDATA,1,Ec,nu_c

     

    ! Define microplane model properties

     

    TB,MPLANE,1,,6,ORTH ! TB,MPLAN,mat,ntemp,npts,tbopt

    TBDATA,1,k0,k1,k2,gamma,alpha,beta ! TBDATA,1,C1,C2,C3,C4,C5,C6

    ! C1 = k0 Damage function constant

    ! C2 = k1 Damage function constant

    ! C3 = k2 Damage function constant

    ! C4 = gamma Critical Equivalent strain energy

    ! C5 = alpha Maximum degradation

    ! C6 = beta  Rate of degradation

    !

    !  AÇO

     

    ET,2,LINK180

     

    ! Define elastic properties of material

    MP,EX,2,Es

    MP,PRXY,2,nu_s

     

    ! Define steel nonlinear properties

    TB,BISO,2

    TBDATA,2,fy,0

     

    ! Define steel section

    SECTYPE,1,LINK

    SECDATA,AP

     

     

    ! GEOMETRY

     

    /PREP7

    A=1212.5

    B=210

    D=152

     

    L=9900

     

    RECTNG,0,A,0,B

     

    !RECORTES PARA ARMADURAS

     

    NPRESS = 5

    ESP = 190

     

    WPSTYL,DEFA

    WPROTA,,,90

     

    WPOFFS,,,56.25

    ASBW,ALL

     

    *DO,I,1,NPRESS,1

        WPOFFS,,,ESP

        ASBW,ALL

    *ENDDO

     

    WPSTYL,DEFA

    WPROTA,,,90

    WPOFFS,,,56.25+150

    ASBW,ALL

     

    *DO,I,1,NPRESS,1

        WPOFFS,,,ESP

        ASBW,ALL

    *ENDDO

     

    ! CORTES HORIZONTAIS

     

    WPSTYL,DEFA

    WPROTA,,-90

    WPOFFS,,,30 ! ARMADURA

    ASBW,ALL

     

    WPSTYL,DEFA

     

    NUMCMP,area

     

    ! FUROS

     

    ASEL,NONE

     

    CYL4,131.25,B/2,0,,D/2,360

    CYL4,131.25+190*1,B/2,0,,D/2,360

    CYL4,131.25+190*2,B/2,0,,D/2,360

    CYL4,131.25+190*3,B/2,0,,D/2,360

    CYL4,131.25+190*4,B/2,0,,D/2,360

    CYL4,131.25+190*5,B/2,0,,D/2,360

     

    ALLSELL

     

    ASBA,2,27

    ASBA,6,28

    ASBA,8,29

    ASBA,10,30

    ASBA,12,31

    ASBA,26,32

     

    ! CORTES HORIZONTAIS ADICIONAIS

     

    WPSTYL,DEFA

    WPROTA,,-90

    WPOFFS,,,90

    ASBW,ALL

    WPOFFS,,,30

    ASBW,ALL

     

    !RECORTES VERTICAIS ADICIONAIS

     

    NPRESS = 5

    ESP = 190

     

    WPSTYL,DEFA

    WPROTA,,,90

     

    WPOFFS,,,56.25

    WPOFFS,,,60

    ASBW,ALL

     

    *DO,I,1,NPRESS,1

        WPOFFS,,,ESP

        ASBW,ALL

    *ENDDO

     

    WPSTYL,DEFA

    WPROTA,,,90

     

    WPOFFS,,,56.25

    WPOFFS,,,60

    WPOFFS,,,30

    ASBW,ALL

     

    *DO,I,1,NPRESS,1

        WPOFFS,,,ESP

        ASBW,ALL

    *ENDDO

     

    WPSTYL,DEFA

     

    NUMCMP,kp

    NUMCMP,line

    NUMCMP,area

     

    ALLSEL

    VEXT,ALL,,,,,L/2

     

    ! COMPONENT PRESTRESSED REINFORCEMENT

    KSEL,S,KP,,32,39

    LSLK,S

    LSEL,R,LOC,Z,-L/2,0

    CM,AP,LINE

     

    ! COMPONENT CONCRETE

    VSEL,S,VOLU,,ALL

    CM,CONC,VOLU

     

    CMSEL,NONE

    ALLSEL

    VPLOT

     

    !

    !  ATTRIBUTES

     

    CMSEL,S,CONC

    VATT,1,,1

     

    CMSEL,S,AP

    LATT,2,,2,,,,1

     

    ALLSEL

     

    !

    !  MESH

     

    LESIZE,ALL,10

     

    CMSEL,S,CONC

    VSWEEP,ALL

     

    CMSEL,S,AP

    LMESH,ALL

    Thank you

  • VICTORVERGAVICTORVERGA Member
    edited May 20

    How can I define the share topogy through APDL ?

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