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