DAMASK_EICMD/code/DAMASK_marc.f90

447 lines
27 KiB
Fortran

#define QUOTE(x) #x
#define PASTE(x,y) x ## y
#ifndef INT
#define INT 4
#endif
#ifndef FLOAT
#define FLOAT 8
#endif
#include "prec.f90"
!--------------------------------------------------------------------------------------------------
! $Id$
!--------------------------------------------------------------------------------------------------
!> @author Philip Eisenlohr, Max-Planck-Institut für Eisenforschung GmbH
!> @author Franz Roters, Max-Planck-Institut für Eisenforschung GmbH
!> @author Luc Hantcherli, Max-Planck-Institut für Eisenforschung GmbH
!> @author W.A. Counts
!> @author Denny Tjahjanto, Max-Planck-Institut für Eisenforschung GmbH
!> @author Christoph Kords, Max-Planck-Institut für Eisenforschung GmbH
!> @brief Material subroutine for MSC.Marc
!> @details Usage:
!> @details - choose material as hypela2
!> @details - set statevariable 2 to index of homogenization
!> @details - set statevariable 3 to index of microstructure
!> @details - make sure the file "material.config" exists in the working directory
!> @details - make sure the file "numerics.config" exists in the working directory
!> @details - use nonsymmetric option for solver (e.g. direct profile or multifrontal sparse, the latter seems to be faster!)
!> @details - in case of ddm (domain decomposition) a SYMMETRIC solver has to be used, i.e uncheck "non-symmetric"
!> @details Marc subroutines used:
!> @details - hypela2
!> @details - plotv
!> @details - quit
!> @details Marc common blocks included:
!> @details - concom: lovl, inc
!> @details - creeps: timinc
!--------------------------------------------------------------------------------------------------
module DAMASK_interface
implicit none
character(len=4), parameter :: InputFileExtension = '.dat'
character(len=4), parameter :: LogFileExtension = '.log'
contains
!--------------------------------------------------------------------------------------------------
!> @brief only output of current version
!--------------------------------------------------------------------------------------------------
subroutine DAMASK_interface_init
implicit none
!$OMP CRITICAL (write2out)
write(6,'(/,a)') ' <<<+- DAMASK_marc init -+>>>'
write(6,'(a)') ' $Id$'
#include "compilation_info.f90"
!$OMP END CRITICAL (write2out)
end subroutine DAMASK_interface_init
!--------------------------------------------------------------------------------------------------
!> @brief returns the current workingDir
!--------------------------------------------------------------------------------------------------
function getSolverWorkingDirectoryName()
implicit none
character(1024) getSolverWorkingDirectoryName, inputName
character(len=*), parameter :: pathSep = achar(47)//achar(92) ! forward and backward slash
getSolverWorkingDirectoryName=''
inputName=''
inquire(5, name=inputName) ! determine inputputfile
getSolverWorkingDirectoryName=inputName(1:scan(inputName,pathSep,back=.true.))
end function getSolverWorkingDirectoryName
!--------------------------------------------------------------------------------------------------
!> @brief solver job name (no extension) as combination of geometry and load case name
!--------------------------------------------------------------------------------------------------
function getSolverJobName()
use prec, only: &
pReal, &
pInt
implicit none
character(1024) :: getSolverJobName, inputName
character(len=*), parameter :: pathSep = achar(47)//achar(92) ! forward and backward slash
integer(pInt) :: extPos
getSolverJobName=''
inputName=''
inquire(5, name=inputName) ! determine inputfile
extPos = len_trim(inputName)-4
getSolverJobName=inputName(scan(inputName,pathSep,back=.true.)+1:extPos)
end function getSolverJobName
end module DAMASK_interface
#include "IO.f90"
#include "libs.f90"
#include "numerics.f90"
#include "debug.f90"
#include "math.f90"
#include "FEsolving.f90"
#include "mesh.f90"
#include "material.f90"
#include "lattice.f90"
#include "damage_none.f90"
#include "damage_brittle.f90"
#include "damage_ductile.f90"
#include "damage_gurson.f90"
#include "thermal_isothermal.f90"
#include "thermal_adiabatic.f90"
#include "constitutive_none.f90"
#include "constitutive_j2.f90"
#include "constitutive_phenopowerlaw.f90"
#include "constitutive_titanmod.f90"
#include "constitutive_dislotwin.f90"
#include "constitutive_dislokmc.f90"
#include "constitutive_nonlocal.f90"
#include "constitutive.f90"
#include "crystallite.f90"
#include "homogenization_none.f90"
#include "homogenization_isostrain.f90"
#include "homogenization_RGC.f90"
#include "homogenization.f90"
#include "CPFEM.f90"
!--------------------------------------------------------------------------------------------------
!> @brief This is the MSC.Marc user subroutine for defining material behavior
!> @details (1) F,R,U are only available for continuum and membrane elements (not for
!> @details shells and beams).
!> @details
!> @details (2) Use the -> 'Plasticity,3' card(=update+finite+large disp+constant d)
!> @details in the parameter section of input deck (updated Lagrangian formulation).
!> @details
!> @details The following operation obtains U (stretch tensor) at t=n+1 :
!> @details
!> @details call scla(un1,0.d0,itel,itel,1)
!> @details do k=1,3
!> @details do i=1,3
!> @details do j=1,3
!> @details un1(i,j)=un1(i,j)+dsqrt(strechn1(k))*eigvn1(i,k)*eigvn1(j,k)
!> @details enddo
!> @details enddo
!> @details enddo
!--------------------------------------------------------------------------------------------------
subroutine hypela2(d,g,e,de,s,t,dt,ngens,m,nn,kcus,matus,ndi,nshear,disp, &
dispt,coord,ffn,frotn,strechn,eigvn,ffn1,frotn1, &
strechn1,eigvn1,ncrd,itel,ndeg,ndm,nnode, &
jtype,lclass,ifr,ifu)
use prec, only: &
pReal, &
pInt
use numerics, only: &
!$ DAMASK_NumThreadsInt, &
numerics_unitlength, &
usePingPong
use FEsolving, only: &
cycleCounter, &
theInc, &
calcMode, &
theTime, &
theDelta, &
lastIncConverged, &
outdatedByNewInc, &
outdatedFFN1, &
terminallyIll, &
symmetricSolver, &
lastLovl
use math, only: &
math_transpose33,&
invnrmMandel
use debug, only: &
debug_level, &
debug_LEVELBASIC, &
debug_MARC, &
debug_info, &
debug_reset
use mesh, only: &
mesh_FEasCP, &
mesh_element, &
mesh_node0, &
mesh_node, &
mesh_Ncellnodes, &
mesh_cellnode, &
mesh_build_cellnodes, &
mesh_build_ipCoordinates, &
FE_Nnodes
use CPFEM, only: &
CPFEM_general, &
CPFEM_init_done, &
CPFEM_initAll, &
CPFEM_CALCRESULTS, &
CPFEM_AGERESULTS, &
CPFEM_COLLECT, &
CPFEM_RESTOREJACOBIAN, &
CPFEM_BACKUPJACOBIAN
implicit none
!$ include "omp_lib.h" ! the openMP function library
integer(pInt), intent(in) :: & ! according to MSC.Marc 2012 Manual D
ngens, & !< size of stress-strain law
nn, & !< integration point number
ndi, & !< number of direct components
nshear, & !< number of shear components
ncrd, & !< number of coordinates
itel, & !< dimension of F and R, either 2 or 3
ndeg, & !< number of degrees of freedom
ndm, & !< not specified in MSC.Marc 2012 Manual D
nnode, & !< number of nodes per element
jtype, & !< element type
ifr, & !< set to 1 if R has been calculated
ifu !< set to 1 if stretch has been calculated
integer(pInt), dimension(2), intent(in) :: & ! according to MSC.Marc 2012 Manual D
m, & !< (1) user element number, (2) internal element number
matus, & !< (1) user material identification number, (2) internal material identification number
kcus, & !< (1) layer number, (2) internal layer number
lclass !< (1) element class, (2) 0: displacement, 1: low order Herrmann, 2: high order Herrmann
real(pReal), dimension(*), intent(in) :: & ! has dimension(1) according to MSC.Marc 2012 Manual D, but according to example hypela2.f dimension(*)
e, & !< total elastic strain
de, & !< increment of strain
dt !< increment of state variables
real(pReal), dimension(itel), intent(in) :: & ! according to MSC.Marc 2012 Manual D
strechn, & !< square of principal stretch ratios, lambda(i) at t=n
strechn1 !< square of principal stretch ratios, lambda(i) at t=n+1
real(pReal), dimension(3,3), intent(in) :: & ! has dimension(itel,*) according to MSC.Marc 2012 Manual D, but we alway assume dimension(3,3)
ffn, & !< deformation gradient at t=n
ffn1 !< deformation gradient at t=n+1
real(pReal), dimension(itel,*), intent(in) :: & ! according to MSC.Marc 2012 Manual D
frotn, & !< rotation tensor at t=n
eigvn, & !< i principal direction components for j eigenvalues at t=n
frotn1, & !< rotation tensor at t=n+1
eigvn1 !< i principal direction components for j eigenvalues at t=n+1
real(pReal), dimension(ndeg,*), intent(in) :: & ! according to MSC.Marc 2012 Manual D
disp, & !< incremental displacements
dispt !< displacements at t=n (at assembly, lovl=4) and displacements at t=n+1 (at stress recovery, lovl=6)
real(pReal), dimension(ncrd,*), intent(in) :: & ! according to MSC.Marc 2012 Manual D
coord !< coordinates
real(pReal), dimension(*), intent(inout) :: & ! according to MSC.Marc 2012 Manual D
t !< state variables (comes in at t=n, must be updated to have state variables at t=n+1)
real(pReal), dimension(ndi+nshear), intent(out) :: & ! has dimension(*) according to MSC.Marc 2012 Manual D, but we need to loop over it
s, & !< stress - should be updated by user
g !< change in stress due to temperature effects
real(pReal), dimension(ngens,ngens), intent(out) :: & ! according to MSC.Marc 2012 Manual D, but according to example hypela2.f dimension(ngens,*)
d !< stress-strain law to be formed
!--------------------------------------------------------------------------------------------------
! Marc common blocks are in fixed format so they have to be reformated to free format (f90)
! Beware of changes in newer Marc versions
#include QUOTE(PASTE(../lib/MarcInclude/concom,Marc4DAMASK)) ! concom is needed for inc, lovl
#include QUOTE(PASTE(../lib/MarcInclude/creeps,Marc4DAMASK)) ! creeps is needed for timinc (time increment)
logical :: cutBack
real(pReal), dimension(6) :: stress
real(pReal), dimension(6,6) :: ddsdde
integer(pInt) :: computationMode, i, cp_en, node, CPnodeID
!$ integer :: defaultNumThreadsInt !< default value set by Marc
if (iand(debug_level(debug_MARC),debug_LEVELBASIC) /= 0_pInt) then
write(6,'(a,/,i8,i8,i2)') ' MSC.MARC information on shape of element(2), IP:', m, nn
write(6,'(a,2(1i))'), ' Jacobian: ', ngens,ngens
write(6,'(a,1i)'), ' Direct stress: ', ndi
write(6,'(a,1i)'), ' Shear stress: ', nshear
write(6,'(a,1i)'), ' DoF: ', ndeg
write(6,'(a,1i)'), ' Coordinates: ', ncrd
write(6,'(a,1i)'), ' Nodes: ', nnode
write(6,'(a,1i)'), ' Deformation gradient: ', itel
write(6,'(/,a,/,3(3(f12.7,1x)/))',advance='no') ' Deformation gradient at t=n:', &
math_transpose33(ffn)
write(6,'(/,a,/,3(3(f12.7,1x)/))',advance='no') ' Deformation gradient at t=n+1:', &
math_transpose33(ffn1)
endif
!$ defaultNumThreadsInt = omp_get_num_threads() ! remember number of threads set by Marc
if (.not. CPFEM_init_done) call CPFEM_initAll(t(1),m(1),nn)
!$ call omp_set_num_threads(DAMASK_NumThreadsInt) ! set number of threads for parallel execution set by DAMASK_NUM_THREADS
computationMode = 0_pInt ! save initialization value, since it does not result in any calculation
if (lovl == 4 ) then ! jacobian requested by marc
if (timinc < theDelta .and. theInc == inc .and. lastLovl /= lovl) & ! first after cutback
computationMode = CPFEM_RESTOREJACOBIAN
elseif (lovl == 6) then ! stress requested by marc
cp_en = mesh_FEasCP('elem',m(1))
if (cptim > theTime .or. inc /= theInc) then ! reached "convergence"
terminallyIll = .false.
cycleCounter = -1 ! first calc step increments this to cycle = 0
if (inc == 0) then ! >> start of analysis <<
lastIncConverged = .false. ! no Jacobian backup
outdatedByNewInc = .false. ! no aging of state
calcMode = .false. ! pretend last step was collection
lastLovl = lovl ! pretend that this is NOT the first after a lovl change
!$OMP CRITICAL (write2out)
write(6,'(a,i6,1x,i2)') '<< HYPELA2 >> start of analysis..! ',m(1),nn
flush(6)
!$OMP END CRITICAL (write2out)
else if (inc - theInc > 1) then ! >> restart of broken analysis <<
lastIncConverged = .false. ! no Jacobian backup
outdatedByNewInc = .false. ! no aging of state
calcMode = .true. ! pretend last step was calculation
!$OMP CRITICAL (write2out)
write(6,'(a,i6,1x,i2)') '<< HYPELA2 >> restart of analysis..! ',m(1),nn
flush(6)
!$OMP END CRITICAL (write2out)
else ! >> just the next inc <<
lastIncConverged = .true. ! request Jacobian backup
outdatedByNewInc = .true. ! request aging of state
calcMode = .true. ! assure last step was calculation
!$OMP CRITICAL (write2out)
write(6,'(a,i6,1x,i2)') '<< HYPELA2 >> new increment..! ',m(1),nn
flush(6)
!$OMP END CRITICAL (write2out)
endif
else if ( timinc < theDelta ) then ! >> cutBack <<
lastIncConverged = .false. ! no Jacobian backup
outdatedByNewInc = .false. ! no aging of state
terminallyIll = .false.
cycleCounter = -1 ! first calc step increments this to cycle = 0
calcMode = .true. ! pretend last step was calculation
!$OMP CRITICAL (write2out)
write(6,'(a,i6,1x,i2)') '<< HYPELA2 >> cutback detected..! ',m(1),nn
flush(6)
!$OMP END CRITICAL (write2out)
endif ! convergence treatment end
if (usePingPong) then
calcMode(nn,cp_en) = .not. calcMode(nn,cp_en) ! ping pong (calc <--> collect)
if (calcMode(nn,cp_en)) then ! now --- CALC ---
computationMode = CPFEM_CALCRESULTS
if (lastLovl /= lovl) then ! first after ping pong
call debug_reset() ! resets debugging
outdatedFFN1 = .false.
cycleCounter = cycleCounter + 1_pInt
mesh_cellnode = mesh_build_cellnodes(mesh_node,mesh_Ncellnodes) ! update cell node coordinates
call mesh_build_ipCoordinates() ! update ip coordinates
endif
if (outdatedByNewInc) then
computationMode = ior(computationMode,CPFEM_AGERESULTS) ! calc and age results
outdatedByNewInc = .false. ! reset flag
endif
else ! now --- COLLECT ---
computationMode = CPFEM_COLLECT ! plain collect
if (lastLovl /= lovl .and. & .not. terminallyIll) &
call debug_info() ! first after ping pong reports (meaningful) debugging
if (lastIncConverged) then
computationMode = ior(computationMode,CPFEM_BACKUPJACOBIAN) ! collect and backup Jacobian after convergence
lastIncConverged = .false. ! reset flag
endif
do node = 1,FE_Nnodes(mesh_element(2,cp_en))
CPnodeID = mesh_element(4_pInt+node,cp_en)
mesh_node(1:3,CPnodeID) = mesh_node0(1:3,CPnodeID) + numerics_unitlength * dispt(1:3,node)
enddo
endif
else ! --- PLAIN MODE ---
computationMode = CPFEM_CALCRESULTS ! always calc
if (lastLovl /= lovl) then
if (.not. terminallyIll) &
call debug_info() ! first reports (meaningful) debugging
call debug_reset() ! and resets debugging
outdatedFFN1 = .false.
cycleCounter = cycleCounter + 1_pInt
mesh_cellnode = mesh_build_cellnodes(mesh_node,mesh_Ncellnodes) ! update cell node coordinates
call mesh_build_ipCoordinates() ! update ip coordinates
endif
if (outdatedByNewInc) then
computationMode = ior(computationMode,CPFEM_AGERESULTS)
outdatedByNewInc = .false. ! reset flag
endif
if (lastIncConverged) then
computationMode = ior(computationMode,CPFEM_BACKUPJACOBIAN) ! backup Jacobian after convergence
lastIncConverged = .false. ! reset flag
endif
endif
theTime = cptim ! record current starting time
theDelta = timinc ! record current time increment
theInc = inc ! record current increment number
endif
lastLovl = lovl ! record lovl
call CPFEM_general(computationMode,usePingPong,ffn,ffn1,t(1),timinc,m(1),nn,stress,ddsdde)
! Mandel: 11, 22, 33, SQRT(2)*12, SQRT(2)*23, SQRT(2)*13
! Marc: 11, 22, 33, 12, 23, 13
! Marc: 11, 22, 33, 12
forall(i=1:ngens) d(1:ngens,i) = invnrmMandel(i)*ddsdde(1:ngens,i)*invnrmMandel(1:ngens)
s(1:ndi+nshear) = stress(1:ndi+nshear)*invnrmMandel(1:ndi+nshear)
g = 0.0_pReal
if(symmetricSolver) d = 0.5_pReal*(d+transpose(d))
!$ call omp_set_num_threads(defaultNumThreadsInt) ! reset number of threads to stored default value
end subroutine hypela2
!--------------------------------------------------------------------------------------------------
!> @brief sets user defined output variables for Marc
!> @details select a variable contour plotting (user subroutine).
!--------------------------------------------------------------------------------------------------
subroutine plotv(v,s,sp,etot,eplas,ecreep,t,m,nn,layer,ndi,nshear,jpltcd)
use prec, only: &
pReal, &
pInt
use mesh, only: &
mesh_FEasCP
use IO, only: &
IO_error
use homogenization, only: &
materialpoint_results,&
materialpoint_sizeResults
implicit none
integer(pInt), intent(in) :: &
m, & !< element number
nn, & !< integration point number
layer, & !< layer number
ndi, & !< number of direct stress components
nshear, & !< number of shear stress components
jpltcd !< user variable index
real(pReal), dimension(*), intent(in) :: &
s, & !< stress array
sp, & !< stresses in preferred direction
etot, & !< total strain (generalized)
eplas, & !< total plastic strain
ecreep, & !< total creep strain
t !< current temperature
real(pReal), intent(out) :: &
v !< variable
if (jpltcd > materialpoint_sizeResults) call IO_error(700_pInt,jpltcd) ! complain about out of bounds error
v = materialpoint_results(jpltcd,nn,mesh_FEasCP('elem', m))
end subroutine plotv