Modifications of cpfem_marc2005r3 according the ones in cpfem_marc2007r1
This commit is contained in:
Luc Hantcherli
parent
1267ce78b6
commit
6d721dc16c
|
|
@ -1,15 +1,15 @@
|
||||||
!********************************************************************
|
!********************************************************************
|
||||||
! Material subroutine for MSC.Marc Version 0.1
|
! Material subroutine for MSC.Marc Version 0.1
|
||||||
!
|
!
|
||||||
! written by F. Roters, P. Eisenlohr, L. Hantcherli, W.A. Counts
|
! written by F. Roters, P. Eisenlohr, L. Hantcherli, W.A. Counts
|
||||||
! MPI fuer Eisenforschung, Duesseldorf
|
! MPI fuer Eisenforschung, Duesseldorf
|
||||||
!
|
!
|
||||||
! last modified: 08.11.2007
|
! last modified: 08.11.2007
|
||||||
!********************************************************************
|
!********************************************************************
|
||||||
! Usage:
|
! Usage:
|
||||||
! - choose material as hypela2
|
! - choose material as hypela2
|
||||||
! - set statevariable 2 to index of material
|
! - set statevariable 2 to index of material
|
||||||
! - set statevariable 3 to index of texture
|
! - set statevariable 3 to index of texture
|
||||||
! - choose output of user variables if desired
|
! - choose output of user variables if desired
|
||||||
! - make sure the file "mattex.mpie" exists in the working
|
! - make sure the file "mattex.mpie" exists in the working
|
||||||
! directory
|
! directory
|
||||||
|
|
@ -27,108 +27,119 @@
|
||||||
! - creeps: timinc
|
! - creeps: timinc
|
||||||
!********************************************************************
|
!********************************************************************
|
||||||
!
|
!
|
||||||
include "prec.f90"
|
include "prec.f90"
|
||||||
include "debug.f90"
|
include "FEsolving.f90"
|
||||||
|
include "debug.f90"
|
||||||
include "math.f90"
|
include "math.f90"
|
||||||
include "IO.f90"
|
include "IO.f90"
|
||||||
include "mesh.f90"
|
include "mesh.f90"
|
||||||
include "crystal.f90"
|
include "crystal.f90"
|
||||||
include "constitutive.f90"
|
include "constitutive.f90"
|
||||||
include "CPFEM.f90"
|
include "CPFEM.f90"
|
||||||
|
!
|
||||||
SUBROUTINE hypela2(d,g,e,de,s,t,dt,ngens,n,nn,kcus,matus,ndi,&
|
|
||||||
nshear,disp,dispt,coord,ffn,frotn,strechn,eigvn,ffn1,&
|
SUBROUTINE hypela2(d,g,e,de,s,t,dt,ngens,n,nn,kcus,matus,ndi,&
|
||||||
frotn1,strechn1,eigvn1,ncrd,itel,ndeg,ndm,&
|
nshear,disp,dispt,coord,ffn,frotn,strechn,eigvn,ffn1,&
|
||||||
|
frotn1,strechn1,eigvn1,ncrd,itel,ndeg,ndm,&
|
||||||
nnode,jtype,lclass,ifr,ifu)
|
nnode,jtype,lclass,ifr,ifu)
|
||||||
!********************************************************************
|
!********************************************************************
|
||||||
! This is the Marc material routine
|
! This is the Marc material routine
|
||||||
!********************************************************************
|
!********************************************************************
|
||||||
!
|
!
|
||||||
! ************* user subroutine for defining material behavior **************
|
! ************* user subroutine for defining material behavior **************
|
||||||
!
|
|
||||||
!
|
|
||||||
! CAUTION : Due to calculation of the Deformation gradients, Stretch Tensors and
|
|
||||||
! Rotation tensors at previous and current states, the analysis can be
|
|
||||||
! computationally expensive. Please use the user subroutine -> hypela
|
|
||||||
! if these kinematic quantities are not needed in the constitutive model
|
|
||||||
!
|
|
||||||
!
|
|
||||||
! IMPORTANT NOTES :
|
|
||||||
!
|
|
||||||
! (1) F,R,U are only available for continuum and membrane elements (not for
|
|
||||||
! shells and beams).
|
|
||||||
!
|
|
||||||
! (2) For total Lagrangian formulation use the -> 'Elasticity,1' card(=
|
|
||||||
! total Lagrange with large disp) in the parameter section of input deck.
|
|
||||||
! For updated Lagrangian formulation use the -> 'Plasticity,3' card(=
|
|
||||||
! update+finite+large disp+constant d) in the parameter section of
|
|
||||||
! input deck.
|
|
||||||
!
|
|
||||||
!
|
|
||||||
! d stress strain law to be formed
|
|
||||||
! g change in stress due to temperature effects
|
|
||||||
! e total elastic strain
|
|
||||||
! de increment of strain
|
|
||||||
! s stress - should be updated by user
|
|
||||||
! t state variables (comes in at t=n, must be updated
|
|
||||||
! to have state variables at t=n+1)
|
|
||||||
! dt increment of state variables
|
|
||||||
! ngens size of stress - strain law
|
|
||||||
! n element number
|
|
||||||
! nn integration point number
|
|
||||||
! kcus(1) layer number
|
|
||||||
! kcus(2) internal layer number
|
|
||||||
! matus(1) user material identification number
|
|
||||||
! matus(2) internal material identification number
|
|
||||||
! ndi number of direct components
|
|
||||||
! nshear number of shear components
|
|
||||||
! disp incremental displacements
|
|
||||||
! dispt displacements at t=n (at assembly, lovl=4) and
|
|
||||||
! displacements at t=n+1 (at stress recovery, lovl=6)
|
|
||||||
! coord coordinates
|
|
||||||
! ncrd number of coordinates
|
|
||||||
! ndeg number of degrees of freedom
|
|
||||||
! itel dimension of F and R, either 2 or 3
|
|
||||||
! nnode number of nodes per element
|
|
||||||
! jtype element type
|
|
||||||
! lclass element class
|
|
||||||
! ifr set to 1 if R has been calculated
|
|
||||||
! ifu set to 1 if strech has been calculated
|
|
||||||
!
|
|
||||||
! at t=n :
|
|
||||||
!
|
|
||||||
! ffn deformation gradient
|
|
||||||
! frotn rotation tensor
|
|
||||||
! strechn square of principal stretch ratios, lambda(i)
|
|
||||||
! eigvn(i,j) i principal direction components for j eigenvalues
|
|
||||||
!
|
|
||||||
! at t=n+1 :
|
|
||||||
!
|
|
||||||
! ffn1 deformation gradient
|
|
||||||
! frotn1 rotation tensor
|
|
||||||
! strechn1 square of principal stretch ratios, lambda(i)
|
|
||||||
! eigvn1(i,j) i principal direction components for j eigenvalues
|
|
||||||
!
|
|
||||||
! The following operation obtains U (stretch tensor) at t=n+1 :
|
|
||||||
!
|
|
||||||
! call scla(un1,0.d0,itel,itel,1)
|
|
||||||
! do 3 k=1,3
|
|
||||||
! do 2 i=1,3
|
|
||||||
! do 1 j=1,3
|
|
||||||
! un1(i,j)=un1(i,j)+dsqrt(strechn1(k))*eigvn1(i,k)*eigvn1(j,k)
|
|
||||||
!1 continue
|
|
||||||
!2 continue
|
|
||||||
!3 continue
|
|
||||||
!
|
|
||||||
!
|
!
|
||||||
use prec, only: pReal,pInt
|
!
|
||||||
|
! CAUTION : Due to calculation of the Deformation gradients, Stretch Tensors and
|
||||||
|
! Rotation tensors at previous and current states, the analysis can be
|
||||||
|
! computationally expensive. Please use the user subroutine -> hypela
|
||||||
|
! if these kinematic quantities are not needed in the constitutive model
|
||||||
|
!
|
||||||
|
!
|
||||||
|
! IMPORTANT NOTES :
|
||||||
|
!
|
||||||
|
! (1) F,R,U are only available for continuum and membrane elements (not for
|
||||||
|
! shells and beams).
|
||||||
|
!
|
||||||
|
! (2) For total Lagrangian formulation use the -> 'Elasticity,1' card(=
|
||||||
|
! total Lagrange with large disp) in the parameter section of input deck.
|
||||||
|
! For updated Lagrangian formulation use the -> 'Plasticity,3' card(=
|
||||||
|
! update+finite+large disp+constant d) in the parameter section of
|
||||||
|
! input deck.
|
||||||
|
!
|
||||||
|
!
|
||||||
|
! d stress strain law to be formed
|
||||||
|
! g change in stress due to temperature effects
|
||||||
|
! e total elastic strain
|
||||||
|
! de increment of strain
|
||||||
|
! s stress - should be updated by user
|
||||||
|
! t state variables (comes in at t=n, must be updated
|
||||||
|
! to have state variables at t=n+1)
|
||||||
|
! dt increment of state variables
|
||||||
|
! ngens size of stress - strain law
|
||||||
|
! n element number
|
||||||
|
! nn integration point number
|
||||||
|
! kcus(1) layer number
|
||||||
|
! kcus(2) internal layer number
|
||||||
|
! matus(1) user material identification number
|
||||||
|
! matus(2) internal material identification number
|
||||||
|
! ndi number of direct components
|
||||||
|
! nshear number of shear components
|
||||||
|
! disp incremental displacements
|
||||||
|
! dispt displacements at t=n (at assembly, lovl=4) and
|
||||||
|
! displacements at t=n+1 (at stress recovery, lovl=6)
|
||||||
|
! coord coordinates
|
||||||
|
! ncrd number of coordinates
|
||||||
|
! ndeg number of degrees of freedom
|
||||||
|
! itel dimension of F and R, either 2 or 3
|
||||||
|
! nnode number of nodes per element
|
||||||
|
! jtype element type
|
||||||
|
! lclass element class
|
||||||
|
! ifr set to 1 if R has been calculated
|
||||||
|
! ifu set to 1 if strech has been calculated
|
||||||
|
!
|
||||||
|
! at t=n :
|
||||||
|
!
|
||||||
|
! ffn deformation gradient
|
||||||
|
! frotn rotation tensor
|
||||||
|
! strechn square of principal stretch ratios, lambda(i)
|
||||||
|
! eigvn(i,j) i principal direction components for j eigenvalues
|
||||||
|
!
|
||||||
|
! at t=n+1 :
|
||||||
|
!
|
||||||
|
! ffn1 deformation gradient
|
||||||
|
! frotn1 rotation tensor
|
||||||
|
! strechn1 square of principal stretch ratios, lambda(i)
|
||||||
|
! eigvn1(i,j) i principal direction components for j eigenvalues
|
||||||
|
!
|
||||||
|
! The following operation obtains U (stretch tensor) at t=n+1 :
|
||||||
|
!
|
||||||
|
! call scla(un1,0.d0,itel,itel,1)
|
||||||
|
! do 3 k=1,3
|
||||||
|
! do 2 i=1,3
|
||||||
|
! do 1 j=1,3
|
||||||
|
! un1(i,j)=un1(i,j)+dsqrt(strechn1(k))*eigvn1(i,k)*eigvn1(j,k)
|
||||||
|
!1 continue
|
||||||
|
!2 continue
|
||||||
|
!3 continue
|
||||||
|
!
|
||||||
|
|
||||||
|
use prec, only: pReal,pInt, ijaco
|
||||||
|
use FEsolving
|
||||||
use CPFEM, only: CPFEM_general
|
use CPFEM, only: CPFEM_general
|
||||||
|
use math, only: invnrmMandel
|
||||||
|
|
||||||
implicit real(pReal) (a-h,o-z)
|
implicit real(pReal) (a-h,o-z)
|
||||||
!
|
|
||||||
|
integer(pInt) computationMode
|
||||||
|
|
||||||
|
dimension e(*),de(*),t(*),dt(*),g(*),d(ngens,*),s(*), n(2),coord(ncrd,*),disp(ndeg,*),matus(2),dispt(ndeg,*),ffn(itel,*),&
|
||||||
|
frotn(itel,*),strechn(itel),eigvn(itel,*),ffn1(itel,*),frotn1(itel,*),strechn1(itel),eigvn1(itel,*),kcus(2)
|
||||||
|
|
||||||
|
|
||||||
! Marc common blocks are in fixed format so they have to be pasted in here
|
! Marc common blocks are in fixed format so they have to be pasted in here
|
||||||
! Beware of changes in newer Marc versions -- these are from 2005r3
|
! Beware of changes in newer Marc versions -- these are from 2005r3
|
||||||
! concom is needed for inc, subinc, ncycle, lovl
|
! concom is needed for inc, subinc, ncycle, lovl
|
||||||
! include 'concom'
|
! include 'concom'
|
||||||
common/concom/ &
|
common/concom/ &
|
||||||
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva(50), idyn, idynt,&
|
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva(50), idyn, idynt,&
|
||||||
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
|
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
|
||||||
|
|
@ -144,37 +155,44 @@
|
||||||
imech, imecht, ielcmat, ielectt,magnett, imsdift,noplas, jtabls, jactch, jtablth,&
|
imech, imecht, ielcmat, ielectt,magnett, imsdift,noplas, jtabls, jactch, jtablth,&
|
||||||
kgmsto ,jpzo, ifricsh, iremkin,iremfor, ishearp,jspf, machining, jlshell,icompsol,&
|
kgmsto ,jpzo, ifricsh, iremkin,iremfor, ishearp,jspf, machining, jlshell,icompsol,&
|
||||||
iupblgfo,jcondir,nstcrp, nactive,ipassref, nstspnt,ibeart,icheckmpc, noline, icuring,&
|
iupblgfo,jcondir,nstcrp, nactive,ipassref, nstspnt,ibeart,icheckmpc, noline, icuring,&
|
||||||
ishrink,ioffsflg,isetoff, iharmt, inc_incdat, iautspc,ibrake
|
ishrink,ioffsflg,isetoff, iharmt, inc_incdat, iautspc,ibrake
|
||||||
! creeps is needed for timinc (time increment)
|
|
||||||
! include 'creeps'
|
! creeps is needed for timinc (time increment)
|
||||||
common/creeps/ &
|
! include 'creeps'
|
||||||
cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b,creept(33),icptim,icfte,icfst,&
|
common/marc_creeps/ &
|
||||||
icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
|
cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b,creept(33),icptim,icfte,icfst,&
|
||||||
!
|
icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
|
||||||
dimension e(*),de(*),t(*),dt(*),g(*),d(ngens,*),s(*), n(2),coord(ncrd,*),disp(ndeg,*),matus(2),dispt(ndeg,*),ffn(itel,*),&
|
|
||||||
frotn(itel,*),strechn(itel),eigvn(itel,*),ffn1(itel,*),frotn1(itel,*),strechn1(itel),eigvn1(itel,*),kcus(2)
|
|
||||||
!
|
if (inc == 0) then
|
||||||
! subroutine cpfem_general(mpie_ffn, mpie_ffn1, temperature, mpie_inc, mpie_subinc, mpie_cn,
|
cycleCounter = 0
|
||||||
! mpie_stress_recovery, mpie_tinc, mpie_en, mpie_in, mpie_s, mpie_d, mpie_ngens)
|
else
|
||||||
!********************************************************************
|
if (theInc /= inc .or. theCycle /= ncycle .or. theLovl /= lovl) cycleCounter = cycleCounter+1
|
||||||
! This routine calculates the material behaviour
|
endif
|
||||||
!********************************************************************
|
|
||||||
! mpie_ffn deformation gradient for t=t0
|
if (theInc /= inc) outdatedByNewInc = .true.
|
||||||
! mpie_ffn1 deformation gradient for t=t1
|
|
||||||
! temperature temperature
|
if (mod(cycleCounter,2) /= 0) computationMode = 4 ! recycle
|
||||||
! mpie_inc increment number
|
if (mod(cycleCounter,4) == 2) computationMode = 3 ! collect
|
||||||
! mpie_subinc subincrement number
|
if (mod(cycleCounter,4) == 0) computationMode = 2 ! compute
|
||||||
! mpie_cn number of cycle
|
if (computationMode == 2 .and. outdatedByNewInc) then
|
||||||
! mpie_stress_recovery indicates wether we are in stiffness assemly(lovl==4) or stress recovery(lovl==6)
|
outdatedByNewInc = .false.
|
||||||
! mpie_tinc time increment
|
computationMode = 1 ! compute and age former results
|
||||||
! mpie_en element number
|
endif
|
||||||
! mpie_in intergration point number
|
|
||||||
! mpie_s stress vector in Marc notation, i.e. 11 22 33 12, 23, 13
|
theInc = inc
|
||||||
! mpie_d jacoby in Marc notation
|
theCycle = ncycle
|
||||||
! mpie_ngens size of stress strain law
|
theLovl = lovl
|
||||||
!********************************************************************
|
|
||||||
call CPFEM_general(ffn, ffn1, t(1), inc, incsub, ncycle, stress_recovery, timinc, n(1), nn, s, d, ngens)
|
call CPFEM_general(computationMode,ffn,ffn1,t(1),timinc,n(1),nn,s,mod(theCycle,2_pInt*ijaco)==0,d,ngens)
|
||||||
return
|
|
||||||
|
|
||||||
|
! Mandel: 11, 22, 33, SQRT(2)*12, SQRT(2)*23, SQRT(2)*13
|
||||||
|
! Marc: 11, 22, 33, 12, 23, 13
|
||||||
|
forall(i=1:ngens) d(1:ngens,i) = invnrmMandel(i)*d(1:ngens,i)*invnrmMandel(1:ngens)
|
||||||
|
s(1:ngens) = s(1:ngens)*invnrmMandel(1:ngens)
|
||||||
|
|
||||||
|
return
|
||||||
|
|
||||||
END SUBROUTINE
|
END SUBROUTINE
|
||||||
!
|
!
|
||||||
|
|
@ -199,21 +217,21 @@
|
||||||
! ndi (3) number of direct stress components
|
! ndi (3) number of direct stress components
|
||||||
! nshear (3) number of shear stress components
|
! nshear (3) number of shear stress components
|
||||||
!
|
!
|
||||||
!********************************************************************
|
!********************************************************************
|
||||||
use prec, only: pReal,pInt
|
use prec, only: pReal,pInt
|
||||||
use CPFEM, only: CPFEM_results, CPFEM_Nresults
|
use CPFEM, only: CPFEM_results, CPFEM_Nresults
|
||||||
use constitutive, only: constitutive_maxNresults
|
use constitutive, only: constitutive_maxNresults
|
||||||
use mesh, only: mesh_FEasCP
|
use mesh, only: mesh_FEasCP
|
||||||
implicit none
|
implicit none
|
||||||
!
|
!
|
||||||
real(pReal) s(*),etot(*),eplas(*),ecreep(*),sp(*)
|
real(pReal) s(*),etot(*),eplas(*),ecreep(*),sp(*)
|
||||||
real(pReal) v, t(*)
|
real(pReal) v, t(*)
|
||||||
integer(pInt) m, nn, layer, ndi, nshear, jpltcd
|
integer(pInt) m, nn, layer, ndi, nshear, jpltcd
|
||||||
!
|
!
|
||||||
! assign result variable
|
! assign result variable
|
||||||
v=CPFEM_results(mod(jpltcd-1_pInt, CPFEM_Nresults+constitutive_maxNresults)+1_pInt,&
|
v=CPFEM_results(mod(jpltcd-1_pInt, CPFEM_Nresults+constitutive_maxNresults)+1_pInt,&
|
||||||
(jpltcd-1_pInt)/(CPFEM_Nresults+constitutive_maxNresults)+1_pInt,&
|
(jpltcd-1_pInt)/(CPFEM_Nresults+constitutive_maxNresults)+1_pInt,&
|
||||||
nn, mesh_FEasCP('elem', m))
|
nn, mesh_FEasCP('elem', m))
|
||||||
return
|
return
|
||||||
END SUBROUTINE
|
END SUBROUTINE
|
||||||
!
|
!
|
||||||
|
|
|
||||||
Loading…
Reference in New Issue