2007
shortened stress_recovery = ... added (crucial) deMandeling for return values of CPFEM_general 2005 matched to 2007 version
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! written by F. Roters, P. Eisenlohr, L. Hantcherli, W.A. Counts
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! MPI fuer Eisenforschung, Duesseldorf
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!
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! last modified: 08.11.2007
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! last modified: 18.02.2005
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!********************************************************************
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! Usage:
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! - choose material as hypela2
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@ -153,6 +153,10 @@
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!
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dimension e(*),de(*),t(*),dt(*),g(*),d(ngens,*),s(*), n(2),coord(ncrd,*),disp(ndeg,*),matus(2),dispt(ndeg,*),ffn(itel,*),&
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frotn(itel,*),strechn(itel),eigvn(itel,*),ffn1(itel,*),frotn1(itel,*),strechn1(itel),eigvn1(itel,*),kcus(2)
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logical stress_recovery
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stress_recovery = (lovl == 6)
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!
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! subroutine cpfem_general(mpie_ffn, mpie_ffn1, temperature, mpie_inc, mpie_subinc, mpie_cn,
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! mpie_stress_recovery, mpie_tinc, mpie_en, mpie_in, mpie_s, mpie_d, mpie_ngens)
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@ -174,6 +178,10 @@
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! mpie_ngens size of stress strain law
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!********************************************************************
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call CPFEM_general(ffn, ffn1, t(1), inc, incsub, ncycle, stress_recovery, timinc, n(1), nn, s, d, ngens)
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! Mandel: 11, 22, 33, SQRT(2)*12, SQRT(2)*23, SQRT(2)*13
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! Marc: 11, 22, 33, 12, 23, 13
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forall(i=1:ngens) d(1:ngens,i) = invnrmMandel(i)*d(1:ngens,i)*invnrmMandel(1:ngens)
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s(1:ngens) = s(1:ngens)*invnrmMandel(1:ngens)
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return
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END SUBROUTINE
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@ -27,8 +27,8 @@
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! - creeps: timinc
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!********************************************************************
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!
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include "prec.f90"
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include "debug.f90"
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include "prec.f90"
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include "debug.f90"
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include "math.f90"
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include "IO.f90"
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include "mesh.f90"
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@ -121,8 +121,10 @@
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!3 continue
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!
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use prec, only: pReal,pInt
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use prec, only: pReal,pInt
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use CPFEM, only: CPFEM_general
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use math, only: invnrmMandel
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implicit real(pReal) (a-h,o-z)
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!
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! Marc common blocks are in fixed format so they have to be pasted in here
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@ -154,36 +156,45 @@
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icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
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!
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dimension e(*),de(*),t(*),dt(*),g(*),d(ngens,*),s(*), n(2),coord(ncrd,*),disp(ndeg,*),matus(2),dispt(ndeg,*),ffn(itel,*),&
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frotn(itel,*),strechn(itel),eigvn(itel,*),ffn1(itel,*),frotn1(itel,*),strechn1(itel),eigvn1(itel,*),kcus(2)
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logical stress_recovery
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if(lovl==6) then
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stress_recovery = .true.
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else
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stress_recovery = .false.
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endif
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frotn(itel,*),strechn(itel),eigvn(itel,*),ffn1(itel,*),frotn1(itel,*),strechn1(itel),eigvn1(itel,*),kcus(2)
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logical stress_recovery
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stress_recovery = (lovl == 6)
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!
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! subroutine cpfem_general(mpie_ffn, mpie_ffn1, temperature, mpie_inc, mpie_subinc, mpie_cn,
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! subroutine cpfem_general(mpie_ffn, mpie_ffn1, temperature, mpie_inc, mpie_subinc, mpie_cn,
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! mpie_stress_recovery, mpie_tinc, mpie_en, mpie_in, mpie_s, mpie_d, mpie_ngens)
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!********************************************************************
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! This routine calculates the material behaviour
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!********************************************************************
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! mpie_ffn deformation gradient for t=t0
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! mpie_ffn1 deformation gradient for t=t1
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! temperature temperature
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! mpie_inc increment number
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! mpie_subinc subincrement number
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! mpie_ffn1 deformation gradient for t=t1
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! temperature temperature
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! mpie_inc increment number
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! mpie_subinc subincrement number
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! mpie_cn number of cycle
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! mpie_stress_recovery indicates wether we are in stiffness assemly(lovl==4) or stress recovery(lovl==6)
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! mpie_stress_recovery indicates wether we are in stiffness assemly(lovl==4) or stress recovery(lovl==6)
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! mpie_tinc time increment
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! mpie_en element number
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! mpie_in intergration point number
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! mpie_s stress vector in Marc notation, i.e. 11 22 33 12, 23, 13
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! mpie_d jacoby in Marc notation
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! mpie_in intergration point number
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! mpie_s stress vector in Marc notation, i.e. 11 22 33 12, 23, 13
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! mpie_d jacoby in Marc notation
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! mpie_ngens size of stress strain law
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!********************************************************************
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call CPFEM_general(ffn, ffn1, t(1), inc, incsub, ncycle, stress_recovery, timinc, n(1), nn, s, d, ngens)
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! Mandel: 11, 22, 33, SQRT(2)*12, SQRT(2)*23, SQRT(2)*13
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! Marc: 11, 22, 33, 12, 23, 13
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forall(i=1:ngens) d(1:ngens,i) = invnrmMandel(i)*d(1:ngens,i)*invnrmMandel(1:ngens)
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s(1:ngens) = s(1:ngens)*invnrmMandel(1:ngens)
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return
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END SUBROUTINE
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