more cleaning of old commercial FEM solver files

This commit is contained in:
Martin Diehl 2018-07-06 13:18:55 +02:00
parent 2a33dcdd04
commit ce32372f1c
18 changed files with 3 additions and 2705 deletions

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@ -424,20 +424,11 @@ SpectralRuntime:
- release
###################################################################################################
AbaqusExp:
stage: createDocumentation
script:
- module load $IntelCompiler $MPICH_Intel $PETSc_MPICH_Intel $Doxygen
- $DAMASKROOT/PRIVATE/documenting/runDoxygen.sh $DAMASKROOT abaqus_exp
except:
- master
- release
AbaqusStd:
stage: createDocumentation
script:
- module load $IntelCompiler $MPICH_Intel $PETSc_MPICH_Intel $Doxygen
- $DAMASKROOT/PRIVATE/documenting/runDoxygen.sh $DAMASKROOT abaqus_std
- $DAMASKROOT/PRIVATE/documenting/runDoxygen.sh $DAMASKROOT abaqus
except:
- master
- release

@ -1 +1 @@
Subproject commit 6c43b54ecd4a3a5b3ec8771514ef2c7c839a31e7
Subproject commit 1581e8e53910725bac354f5e6f5af1a6914a0a59

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@ -1,205 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: concom.cmn
!
! MSC.Marc include file
!
integer(pInt) &
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen , idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush, istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout, igena_meth,&
magf_meth, non_assumed, iredoboudry
integer(pInt) num_concom
parameter(num_concom=232)
common/marc_concom/&
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva(60), idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen, idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush , istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout,igena_meth,&
magf_meth, non_assumed, iredoboudry
!
! comments of variables:
!
! ideva(60) - debug print out flag
! 1 print element stiffness matrices, mass matrix
! 2 output matrices used in tying
! 3 force the solution of a nonpositive definite matrix
! 4 print info of connections to each node
! 5 info of gap convergence, internal heat generated, contact
! touching and separation
! 6 nodal value array during rezoning
! 7 tying info in CONRAD GAP option, fluid element numbers in
! CHANNEL option
! 8 output incremental displacements in local coord. system
! 9 latent heat output
! 10 stress-strain in local coord. system
! 11 additional info on interlaminar stress
! 12 output right hand side and solution vector
! 13 info of CPU resources used and memory available on NT
! 14 info of mesh adaption process, 2D outline information
! info of penetration checking for remeshing
! save .fem files after afmesh3d meshing
! 15 surface energy balance flag
! 16 print info regarding pyrolysis
! 17 print info of "streamline topology"
! 18 print mesh data changes after remeshing
! 19 print material flow stress data read in from *.mat file
! if unit flag is on, print out flow stress after conversion
! 20 print information on table input
! 21 print out information regarding kinematic boundary conditions
! 22 print out information regarding dist loads, point loads, film
! and foundations
! 23 print out information about automatic domain decomposition
! 24 print out iteration information in SuperForm status report file
! 25 print out information for ablation
! 26 print out information for films - Table input
! 27 print out the tying forces
! 28 print out for CASI solver, convection,
! 29 DDM single file debug printout
! 30 print out cavity debug info
! 31 print out welding related info
! 32 prints categorized DDM memory usage
! 33 print out the cutting info regarding machining feature
! 34 print out the list of quantities which can be defined via a table
! and for each quantity the supported independent variables
! 35 print out detailed coupling region info
! 36 print out solver debug info level 1 (Least Detailed)
! 37 print out solver debug info level 1 (Medium Detailed)
! 38 print out solver debug info level 1 (Very Detailed)
! 39 print detailed memory allocation info
! 40 print out marc-adams debug info
! 41 output rezone mapping post file for debugging
! 42 output post file after calling oprofos() for debugging
! 43 debug printout for vcct
! 44 debug printout for progressive failure
! 45 print out automatically generated midside node coordinates (arecrd)
! 46 print out message about routine and location, where the ibort is raised (ibort_inc)
! 47 print out summary message of element variables on a
! group-basis after all the automatic changes have been
! made (em_ellibp)
! 48 Automatically generate check results based on max and min vals.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the generate_check_results script from /marc/tools
! 49 Automatically generate check results based on the real calculated values
! at the sppecified check result locations.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the update_check_results script from /marc/tools
! 50 generate a file containing the resistance or capacity matrix;
! this file can be used to compare results with a reference file
! 51 print out detailed information for segment-to-segment contact
! 52 print out detailed relative displacement information
! for uniaxial sliding contact
! 53 print out detailed sliding direction information for
! uniaxial sliding contact
! 54 print out detailed information for edges attached to a curve
!
!
! irpflo global flag for rigid plastic flow analysis
! = 1 eularian formulation
! = 2 regular formulation; rigid material present in the analysis
!
! jactch = 1 or 2 if elements are activated or deactivated
! = 3 if elements are adaptively remeshed or rezoned
! = 0 normally / reset to 0 when assembly is done
! ifricsh = 0 call to fricsh in otest not needed
! = 1 call to fricsh (nodal friction) in otest needed
! iremkin = 0 remove deactivated kinematic boundary conditions
! immediately - only in new input format (this is default)
! = 1 remove deactivated kinematic boundary conditions
! gradually - only in new input format
! iremfor = 0 remove force boundary conditions immediately -
! only in new input format (this is default)
! = 1 remove force boundary conditions gradually -
! only in new input format (this is default)
! ishearp set to 1 if shear panel elements are present in the model
!
! jspf = 0 not in spf loadcase
! > 0 in spf loadcase (jspf=1 during first increment)
! machining = 1 if the metal cutting feature is used, for memory allocation purpose
! = 0 (default) if no metal cutting feature required
!
! jlshell = 1 if there is a shell element in the mesh
! icompsol = 1 if there is a composite solid element in the mesh
! iupblgfo = 1 if follower force for point loads
! jcondir = 1 if contact priority option is used
! nstcrp = 0 (default) steady state creep flag (undocumented feature.
! if not 0, turns off special ncycle = 0 code in radial.f)
! nactive = number of active passes, if =1 then it's not a coupled analysis
! ipassref = reference ipass, if not in a multiphysics pass ipass=ipassref
! icheckmpc = value of mpc-check parameter option
! noline = set to 1 in osolty if no line seacrh should be done in ogetst
! icuring = set to 1 if the curing is included for the heat transfer analysis.
! ishrink = set to 1 if shrinkage strain is included for mechancial analysis.
! ioffsflg = 1 for small displacement beam/shell offsets
! = 2 for large displacement beam/shell offsets
! isetoff = 0 - do not apply beam/shell offsets
! = 1 - apply beam/shell offsets
! ioffsetm = min. value of offset flag
! inc_incdat = flag to record increment number of a new loadcase in incdat.f
! iautspc = flag for AutoSPC option
! ibrake = brake squeal in this increment
! icbush = set to 1 if cbush elements present in model
! istream_input = set to 1 for streaming input calling Marc as library
! iprsinp = set to 1 if pressure input, introduced so other variables
! such as h could be a function of pressure
! ivlsinp = set to 1 if velocity input, introduced so other variables
! such as h could be a function of velocity
! ipin_m = # of beam element with PIN flag
! jgnstr_glb = global control over pre or fast integrated composite shells
! imarc_return = Marc return flag for streaming input control
! iqvcimp = if non-zero, then the number of QVECT boundary conditions
! nqvceid = number of QVECT boundary conditions, where emisivity/absorbtion id entered
! istpnx = 1 if to stop at end of increment
! imicro1 = 1 if micro1 interface is used
! iaxisymm = set to 1 if axisymmetric analysis
! jbreakglue = set to 1 if breaking glued option is used
! iglstif = 1 if ddm and global stiffness matrix formed (sgi solver 6 or solver9)
! jfastasm = 1 do fast assembly using SuperForm code
! iwear = set to 1 if wear model, set to 2 if wear model and coordinates updated
! iwearcf = set to 1 to store nodal coefficient of friction for wear calculation
! imixmeth = set=1 then use nonlinear mixture material - allocate memory
! ielcmadyn = flag for magnetodynamics
! 0 - electromagnetics using newmark beta
! 1 - transient magnetics using backward euler
! idinout = flag to control if inside out elements should be deactivated
! igena_meth = 0 - generalized alpha parameters depend on whether or not contact
! is flagged (dynamic,7)
! 10 - generalized alpha parameters are optimized for a contact
! analysis (dynamic,8)
! 11 - generalized alpha parameters are optimized for an analysis
! without contact (dynamic,8)
! magf_meth = - Method to compute force in magnetostatic - structural
! = 1 - Virtual work method
! = 2 - Maxwell stress tensor
! non_assumed = 1 no assumed strain formulation (forced)
! iredoboudry set to 1 if contact boundary needs to be recalculated
!
!***********************************************************************

View File

@ -1,206 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: concom.cmn
!
! MSC.Marc include file
!
integer(pInt) &
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen , idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush, istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout, igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0
integer(pInt) num_concom
parameter(num_concom=233)
common/marc_concom/&
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva(60), idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen, idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush , istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout,igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0
!
! comments of variables:
!
! ideva(60) - debug print out flag
! 1 print element stiffness matrices, mass matrix
! 2 output matrices used in tying
! 3 force the solution of a nonpositive definite matrix
! 4 print info of connections to each node
! 5 info of gap convergence, internal heat generated, contact
! touching and separation
! 6 nodal value array during rezoning
! 7 tying info in CONRAD GAP option, fluid element numbers in
! CHANNEL option
! 8 output incremental displacements in local coord. system
! 9 latent heat output
! 10 stress-strain in local coord. system
! 11 additional info on interlaminar stress
! 12 output right hand side and solution vector
! 13 info of CPU resources used and memory available on NT
! 14 info of mesh adaption process, 2D outline information
! info of penetration checking for remeshing
! save .fem files after afmesh3d meshing
! 15 surface energy balance flag
! 16 print info regarding pyrolysis
! 17 print info of "streamline topology"
! 18 print mesh data changes after remeshing
! 19 print material flow stress data read in from *.mat file
! if unit flag is on, print out flow stress after conversion
! 20 print information on table input
! 21 print out information regarding kinematic boundary conditions
! 22 print out information regarding dist loads, point loads, film
! and foundations
! 23 print out information about automatic domain decomposition
! 24 print out iteration information in SuperForm status report file
! 25 print out information for ablation
! 26 print out information for films - Table input
! 27 print out the tying forces
! 28 print out for CASI solver, convection,
! 29 DDM single file debug printout
! 30 print out cavity debug info
! 31 print out welding related info
! 32 prints categorized DDM memory usage
! 33 print out the cutting info regarding machining feature
! 34 print out the list of quantities which can be defined via a table
! and for each quantity the supported independent variables
! 35 print out detailed coupling region info
! 36 print out solver debug info level 1 (Least Detailed)
! 37 print out solver debug info level 1 (Medium Detailed)
! 38 print out solver debug info level 1 (Very Detailed)
! 39 print detailed memory allocation info
! 40 print out marc-adams debug info
! 41 output rezone mapping post file for debugging
! 42 output post file after calling oprofos() for debugging
! 43 debug printout for vcct
! 44 debug printout for progressive failure
! 45 print out automatically generated midside node coordinates (arecrd)
! 46 print out message about routine and location, where the ibort is raised (ibort_inc)
! 47 print out summary message of element variables on a
! group-basis after all the automatic changes have been
! made (em_ellibp)
! 48 Automatically generate check results based on max and min vals.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the generate_check_results script from /marc/tools
! 49 Automatically generate check results based on the real calculated values
! at the sppecified check result locations.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the update_check_results script from /marc/tools
! 50 generate a file containing the resistance or capacity matrix;
! this file can be used to compare results with a reference file
! 51 print out detailed information for segment-to-segment contact
! 52 print out detailed relative displacement information
! for uniaxial sliding contact
! 53 print out detailed sliding direction information for
! uniaxial sliding contact
! 54 print out detailed information for edges attached to a curve
!
!
! irpflo global flag for rigid plastic flow analysis
! = 1 eularian formulation
! = 2 regular formulation; rigid material present in the analysis
!
! jactch = 1 or 2 if elements are activated or deactivated
! = 3 if elements are adaptively remeshed or rezoned
! = 0 normally / reset to 0 when assembly is done
! ifricsh = 0 call to fricsh in otest not needed
! = 1 call to fricsh (nodal friction) in otest needed
! iremkin = 0 remove deactivated kinematic boundary conditions
! immediately - only in new input format (this is default)
! = 1 remove deactivated kinematic boundary conditions
! gradually - only in new input format
! iremfor = 0 remove force boundary conditions immediately -
! only in new input format (this is default)
! = 1 remove force boundary conditions gradually -
! only in new input format (this is default)
! ishearp set to 1 if shear panel elements are present in the model
!
! jspf = 0 not in spf loadcase
! > 0 in spf loadcase (jspf=1 during first increment)
! machining = 1 if the metal cutting feature is used, for memory allocation purpose
! = 0 (default) if no metal cutting feature required
!
! jlshell = 1 if there is a shell element in the mesh
! icompsol = 1 if there is a composite solid element in the mesh
! iupblgfo = 1 if follower force for point loads
! jcondir = 1 if contact priority option is used
! nstcrp = 0 (default) steady state creep flag (undocumented feature.
! if not 0, turns off special ncycle = 0 code in radial.f)
! nactive = number of active passes, if =1 then it's not a coupled analysis
! ipassref = reference ipass, if not in a multiphysics pass ipass=ipassref
! icheckmpc = value of mpc-check parameter option
! noline = set to 1 in osolty if no line seacrh should be done in ogetst
! icuring = set to 1 if the curing is included for the heat transfer analysis.
! ishrink = set to 1 if shrinkage strain is included for mechancial analysis.
! ioffsflg = 1 for small displacement beam/shell offsets
! = 2 for large displacement beam/shell offsets
! isetoff = 0 - do not apply beam/shell offsets
! = 1 - apply beam/shell offsets
! ioffsetm = min. value of offset flag
! inc_incdat = flag to record increment number of a new loadcase in incdat.f
! iautspc = flag for AutoSPC option
! ibrake = brake squeal in this increment
! icbush = set to 1 if cbush elements present in model
! istream_input = set to 1 for streaming input calling Marc as library
! iprsinp = set to 1 if pressure input, introduced so other variables
! such as h could be a function of pressure
! ivlsinp = set to 1 if velocity input, introduced so other variables
! such as h could be a function of velocity
! ipin_m = # of beam element with PIN flag
! jgnstr_glb = global control over pre or fast integrated composite shells
! imarc_return = Marc return flag for streaming input control
! iqvcimp = if non-zero, then the number of QVECT boundary conditions
! nqvceid = number of QVECT boundary conditions, where emisivity/absorbtion id entered
! istpnx = 1 if to stop at end of increment
! imicro1 = 1 if micro1 interface is used
! iaxisymm = set to 1 if axisymmetric analysis
! jbreakglue = set to 1 if breaking glued option is used
! iglstif = 1 if ddm and global stiffness matrix formed (sgi solver 6 or solver9)
! jfastasm = 1 do fast assembly using SuperForm code
! iwear = set to 1 if wear model, set to 2 if wear model and coordinates updated
! iwearcf = set to 1 to store nodal coefficient of friction for wear calculation
! imixmeth = set=1 then use nonlinear mixture material - allocate memory
! ielcmadyn = flag for magnetodynamics
! 0 - electromagnetics using newmark beta
! 1 - transient magnetics using backward euler
! idinout = flag to control if inside out elements should be deactivated
! igena_meth = 0 - generalized alpha parameters depend on whether or not contact
! is flagged (dynamic,7)
! 10 - generalized alpha parameters are optimized for a contact
! analysis (dynamic,8)
! 11 - generalized alpha parameters are optimized for an analysis
! without contact (dynamic,8)
! magf_meth = - Method to compute force in magnetostatic - structural
! = 1 - Virtual work method
! = 2 - Maxwell stress tensor
! non_assumed = 1 no assumed strain formulation (forced)
! iredoboudry set to 1 if contact boundary needs to be recalculated
! ioffsz0 = 1 if composite are used with reference position.ne.0
!
!***********************************************************************

View File

@ -1,217 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: concom.cmn
!
! MSC.Marc include file
!
integer(pInt) &
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen , idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush, istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout, igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton
dimension :: ideva(60)
integer(pInt) num_concom
parameter(num_concom=237)
common/marc_concom/&
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen, idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush , istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout,igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton
!
! comments of variables:
!
! ideva(60) - debug print out flag
! 1 print element stiffness matrices, mass matrix
! 2 output matrices used in tying
! 3 force the solution of a nonpositive definite matrix
! 4 print info of connections to each node
! 5 info of gap convergence, internal heat generated, contact
! touching and separation
! 6 nodal value array during rezoning
! 7 tying info in CONRAD GAP option, fluid element numbers in
! CHANNEL option
! 8 output incremental displacements in local coord. system
! 9 latent heat output
! 10 stress-strain in local coord. system
! 11 additional info on interlaminar stress
! 12 output right hand side and solution vector
! 13 info of CPU resources used and memory available on NT
! 14 info of mesh adaption process, 2D outline information
! info of penetration checking for remeshing
! save .fem files after afmesh3d meshing
! 15 surface energy balance flag
! 16 print info regarding pyrolysis
! 17 print info of "streamline topology"
! 18 print mesh data changes after remeshing
! 19 print material flow stress data read in from *.mat file
! if unit flag is on, print out flow stress after conversion
! 20 print information on table input
! 21 print out information regarding kinematic boundary conditions
! 22 print out information regarding dist loads, point loads, film
! and foundations
! 23 print out information about automatic domain decomposition
! 24 print out iteration information in SuperForm status report file
! 25 print out information for ablation
! 26 print out information for films - Table input
! 27 print out the tying forces
! 28 print out for CASI solver, convection,
! 29 DDM single file debug printout
! 30 print out cavity debug info
! 31 print out welding related info
! 32 prints categorized DDM memory usage
! 33 print out the cutting info regarding machining feature
! 34 print out the list of quantities which can be defined via a table
! and for each quantity the supported independent variables
! 35 print out detailed coupling region info
! 36 print out solver debug info level 1 (Least Detailed)
! 37 print out solver debug info level 1 (Medium Detailed)
! 38 print out solver debug info level 1 (Very Detailed)
! 39 print detailed memory allocation info
! 40 print out marc-adams debug info
! 41 output rezone mapping post file for debugging
! 42 output post file after calling oprofos() for debugging
! 43 debug printout for vcct
! 44 debug printout for progressive failure
! 45 print out automatically generated midside node coordinates (arecrd)
! 46 print out message about routine and location, where the ibort is raised (ibort_inc)
! 47 print out summary message of element variables on a
! group-basis after all the automatic changes have been
! made (em_ellibp)
! 48 Automatically generate check results based on max and min vals.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the generate_check_results script from /marc/tools
! 49 Automatically generate check results based on the real calculated values
! at the sppecified check result locations.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the update_check_results script from /marc/tools
! 50 generate a file containing the resistance or capacity matrix;
! this file can be used to compare results with a reference file
! 51 print out detailed information for segment-to-segment contact
! 52 print out detailed relative displacement information
! for uniaxial sliding contact
! 53 print out detailed sliding direction information for
! uniaxial sliding contact
! 54 print out detailed information for edges attached to a curve
! 55 print information related to viscoelasticity calculations
! 56 print out detailed information for element coloring for multithreading
!
!
! irpflo global flag for rigid plastic flow analysis
! = 1 eularian formulation
! = 2 regular formulation; rigid material present in the analysis
!
! jactch = 1 or 2 if elements are activated or deactivated
! = 3 if elements are adaptively remeshed or rezoned
! = 0 normally / reset to 0 when assembly is done
! ifricsh = 0 call to fricsh in otest not needed
! = 1 call to fricsh (nodal friction) in otest needed
! iremkin = 0 remove deactivated kinematic boundary conditions
! immediately - only in new input format (this is default)
! = 1 remove deactivated kinematic boundary conditions
! gradually - only in new input format
! iremfor = 0 remove force boundary conditions immediately -
! only in new input format (this is default)
! = 1 remove force boundary conditions gradually -
! only in new input format (this is default)
! ishearp set to 1 if shear panel elements are present in the model
!
! jspf = 0 not in spf loadcase
! > 0 in spf loadcase (jspf=1 during first increment)
! machining = 1 if the metal cutting feature is used, for memory allocation purpose
! = 0 (default) if no metal cutting feature required
!
! jlshell = 1 if there is a shell element in the mesh
! icompsol = 1 if there is a composite solid element in the mesh
! iupblgfo = 1 if follower force for point loads
! jcondir = 1 if contact priority option is used
! nstcrp = 0 (default) steady state creep flag (undocumented feature.
! if not 0, turns off special ncycle = 0 code in radial.f)
! nactive = number of active passes, if =1 then it's not a coupled analysis
! ipassref = reference ipass, if not in a multiphysics pass ipass=ipassref
! icheckmpc = value of mpc-check parameter option
! noline = set to 1 in osolty if no line seacrh should be done in ogetst
! icuring = set to 1 if the curing is included for the heat transfer analysis.
! ishrink = set to 1 if shrinkage strain is included for mechancial analysis.
! ioffsflg = 1 for small displacement beam/shell offsets
! = 2 for large displacement beam/shell offsets
! isetoff = 0 - do not apply beam/shell offsets
! = 1 - apply beam/shell offsets
! ioffsetm = min. value of offset flag
! iharmt = 1 global flag if a coupled analysis contains an harmonic pass
! inc_incdat = flag to record increment number of a new loadcase in incdat.f
! iautspc = flag for AutoSPC option
! ibrake = brake squeal in this increment
! icbush = set to 1 if cbush elements present in model
! istream_input = set to 1 for streaming input calling Marc as library
! iprsinp = set to 1 if pressure input, introduced so other variables
! such as h could be a function of pressure
! ivlsinp = set to 1 if velocity input, introduced so other variables
! such as h could be a function of velocity
! ipin_m = # of beam element with PIN flag
! jgnstr_glb = global control over pre or fast integrated composite shells
! imarc_return = Marc return flag for streaming input control
! iqvcimp = if non-zero, then the number of QVECT boundary conditions
! nqvceid = number of QVECT boundary conditions, where emisivity/absorbtion id entered
! istpnx = 1 if to stop at end of increment
! imicro1 = 1 if micro1 interface is used
! iaxisymm = set to 1 if axisymmetric analysis
! jbreakglue = set to 1 if breaking glued option is used
! iglstif = 1 if ddm and global stiffness matrix formed (sgi solver 6 or solver9)
! jfastasm = 1 do fast assembly using SuperForm code
! iwear = set to 1 if wear model, set to 2 if wear model and coordinates updated
! iwearcf = set to 1 to store nodal coefficient of friction for wear calculation
! imixmeth = set=1 then use nonlinear mixture material - allocate memory
! ielcmadyn = flag for magnetodynamics
! 0 - electromagnetics using newmark beta
! 1 - transient magnetics using backward euler
! idinout = flag to control if inside out elements should be deactivated
! igena_meth = 0 - generalized alpha parameters depend on whether or not contact
! is flagged (dynamic,7)
! 10 - generalized alpha parameters are optimized for a contact
! analysis (dynamic,8)
! 11 - generalized alpha parameters are optimized for an analysis
! without contact (dynamic,8)
! magf_meth = - Method to compute force in magnetostatic - structural
! = 1 - Virtual work method based on finite difference for the force computation
! = 2 - Maxwell stress tensor
! = 3 - Virtual work method based on local derivative for the force computation
! non_assumed = 1 no assumed strain formulation (forced)
! iredoboudry set to 1 if contact boundary needs to be recalculated
! ioffsz0 = 1 if composite are used with reference position.ne.0
! icomplt = 1 global flag if a coupled analysis contains an complex pass
! mesh_dual = 1 two independent meshes are used in magnetodynamic/thermal/structural
! one for magnetodynamic and the other for the remaining passes
! iactrp = 1 in an analysis with global remeshing, include inactive
! rigid bodies on post file
! mgnewton = 1 Use full Newton Raphson iteration for magnetostatic pass
!
!***********************************************************************

View File

@ -1,224 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: concom.cmn
!
! MSC.Marc include file
!
integer(pInt) &
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen , idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush, istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout, igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton, iusedens
dimension :: ideva(60)
integer(pInt) num_concom
parameter(num_concom=238)
common/marc_concom/&
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen, idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush , istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout,igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton, iusedens
!
! comments of variables:
!
! ideva(60) - debug print out flag
! 1 print element stiffness matrices, mass matrix
! 2 output matrices used in tying
! 3 force the solution of a nonpositive definite matrix
! 4 print info of connections to each node
! 5 info of gap convergence, internal heat generated, contact
! touching and separation
! 6 nodal value array during rezoning
! 7 tying info in CONRAD GAP option, fluid element numbers in
! CHANNEL option
! 8 output incremental displacements in local coord. system
! 9 latent heat output
! 10 stress-strain in local coord. system
! 11 additional info on interlaminar stress
! 12 output right hand side and solution vector
! 13 info of CPU resources used and memory available on NT
! 14 info of mesh adaption process, 2D outline information
! info of penetration checking for remeshing
! save .fem files after afmesh3d meshing
! 15 surface energy balance flag
! 16 print info regarding pyrolysis
! 17 print info of "streamline topology"
! 18 print mesh data changes after remeshing
! 19 print material flow stress data read in from *.mat file
! if unit flag is on, print out flow stress after conversion
! 20 print information on table input
! 21 print out information regarding kinematic boundary conditions
! 22 print out information regarding dist loads, point loads, film
! and foundations
! 23 print out information about automatic domain decomposition
! 24 print out iteration information in SuperForm status report file
! 25 print out information for ablation
! 26 print out information for films - Table input
! 27 print out the tying forces
! 28 print out for CASI solver, convection,
! 29 DDM single file debug printout
! 30 print out cavity debug info
! 31 print out welding related info
! 32 prints categorized DDM memory usage
! 33 print out the cutting info regarding machining feature
! 34 print out the list of quantities which can be defined via a table
! and for each quantity the supported independent variables
! 35 print out detailed coupling region info
! 36 print out solver debug info level 1 (Least Detailed)
! 37 print out solver debug info level 1 (Medium Detailed)
! 38 print out solver debug info level 1 (Very Detailed)
! 39 print detailed memory allocation info
! 40 print out marc-adams debug info
! 41 output rezone mapping post file for debugging
! 42 output post file after calling oprofos() for debugging
! 43 debug printout for vcct
! 44 debug printout for progressive failure
! 45 print out automatically generated midside node coordinates (arecrd)
! 46 print out message about routine and location, where the ibort is raised (ibort_inc)
! 47 print out summary message of element variables on a
! group-basis after all the automatic changes have been
! made (em_ellibp)
! 48 Automatically generate check results based on max and min vals.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the generate_check_results script from /marc/tools
! 49 Automatically generate check results based on the real calculated values
! at the sppecified check result locations.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the update_check_results script from /marc/tools
! 50 generate a file containing the resistance or capacity matrix;
! this file can be used to compare results with a reference file
! 51 print out detailed information for segment-to-segment contact
! 52 print out detailed relative displacement information
! for uniaxial sliding contact
! 53 print out detailed sliding direction information for
! uniaxial sliding contact
! 54 print out detailed information for edges attached to a curve
! 55 print information related to viscoelasticity calculations
! 56 print out detailed information for element coloring for multithreading
! 57 print out extra overheads due to multi-threading.
! These overhead includes (i) time and (ii) memory.
! The memory report will be summed over all the children.
!
!
! irpflo global flag for rigid plastic flow analysis
! = 1 eularian formulation
! = 2 regular formulation; rigid material present in the analysis
!
! jactch = 1 or 2 if elements are activated or deactivated
! = 3 if elements are adaptively remeshed or rezoned
! = 0 normally / reset to 0 when assembly is done
! ifricsh = 0 call to fricsh in otest not needed
! = 1 call to fricsh (nodal friction) in otest needed
! iremkin = 0 remove deactivated kinematic boundary conditions
! immediately - only in new input format (this is default)
! = 1 remove deactivated kinematic boundary conditions
! gradually - only in new input format
! iremfor = 0 remove force boundary conditions immediately -
! only in new input format (this is default)
! = 1 remove force boundary conditions gradually -
! only in new input format (this is default)
! ishearp set to 1 if shear panel elements are present in the model
!
! jspf = 0 not in spf loadcase
! > 0 in spf loadcase (jspf=1 during first increment)
! machining = 1 if the metal cutting feature is used, for memory allocation purpose
! = 0 (default) if no metal cutting feature required
!
! jlshell = 1 if there is a shell element in the mesh
! icompsol = 1 if there is a composite solid element in the mesh
! iupblgfo = 1 if follower force for point loads
! jcondir = 1 if contact priority option is used
! nstcrp = 0 (default) steady state creep flag (undocumented feature.
! if not 0, turns off special ncycle = 0 code in radial.f)
! nactive = number of active passes, if =1 then it's not a coupled analysis
! ipassref = reference ipass, if not in a multiphysics pass ipass=ipassref
! icheckmpc = value of mpc-check parameter option
! noline = set to 1 in osolty if no line seacrh should be done in ogetst
! icuring = set to 1 if the curing is included for the heat transfer analysis.
! ishrink = set to 1 if shrinkage strain is included for mechancial analysis.
! ioffsflg = 1 for small displacement beam/shell offsets
! = 2 for large displacement beam/shell offsets
! isetoff = 0 - do not apply beam/shell offsets
! = 1 - apply beam/shell offsets
! ioffsetm = min. value of offset flag
! iharmt = 1 global flag if a coupled analysis contains an harmonic pass
! inc_incdat = flag to record increment number of a new loadcase in incdat.f
! iautspc = flag for AutoSPC option
! ibrake = brake squeal in this increment
! icbush = set to 1 if cbush elements present in model
! istream_input = set to 1 for streaming input calling Marc as library
! iprsinp = set to 1 if pressure input, introduced so other variables
! such as h could be a function of pressure
! ivlsinp = set to 1 if velocity input, introduced so other variables
! such as h could be a function of velocity
! ipin_m = # of beam element with PIN flag
! jgnstr_glb = global control over pre or fast integrated composite shells
! imarc_return = Marc return flag for streaming input control
! iqvcimp = if non-zero, then the number of QVECT boundary conditions
! nqvceid = number of QVECT boundary conditions, where emisivity/absorbtion id entered
! istpnx = 1 if to stop at end of increment
! imicro1 = 1 if micro1 interface is used
! iaxisymm = set to 1 if axisymmetric analysis
! jbreakglue = set to 1 if breaking glued option is used
! iglstif = 1 if ddm and global stiffness matrix formed (sgi solver 6 or solver9)
! jfastasm = 1 do fast assembly using SuperForm code
! iwear = set to 1 if wear model, set to 2 if wear model and coordinates updated
! iwearcf = set to 1 to store nodal coefficient of friction for wear calculation
! imixmeth = set=1 then use nonlinear mixture material - allocate memory
! ielcmadyn = flag for magnetodynamics
! 0 - electromagnetics using newmark beta
! 1 - transient magnetics using backward euler
! idinout = flag to control if inside out elements should be deactivated
! igena_meth = 0 - generalized alpha parameters depend on whether or not contact
! is flagged (dynamic,7)
! 10 - generalized alpha parameters are optimized for a contact
! analysis (dynamic,8)
! 11 - generalized alpha parameters are optimized for an analysis
! without contact (dynamic,8)
! magf_meth = - Method to compute force in magnetostatic - structural
! = 1 - Virtual work method based on finite difference for the force computation
! = 2 - Maxwell stress tensor
! = 3 - Virtual work method based on local derivative for the force computation
! non_assumed = 1 no assumed strain formulation (forced)
! iredoboudry set to 1 if contact boundary needs to be recalculated
! ioffsz0 = 1 if composite are used with reference position.ne.0
! icomplt = 1 global flag if a coupled analysis contains an complex pass
! mesh_dual = 1 two independent meshes are used in magnetodynamic/thermal/structural
! one for magnetodynamic and the other for the remaining passes
! iactrp = 1 in an analysis with global remeshing, include inactive
! rigid bodies on post file
! mgnewton = 1 Use full Newton Raphson iteration for magnetostatic pass
!
! iusedens > 0 if mass density is used in the analysis (dynamics, mass dependent loading)
!
!***********************************************************************
!$omp threadprivate(/marc_concom/)
!!

View File

@ -1,411 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: concom.cmn
!
! MSC.Marc include file
!
integer(pInt) &
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen , idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush, istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout, igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton, iusedens,igsigd0,&
iaem
dimension :: ideva(60)
integer(pInt) num_concom
parameter(num_concom=240)
common/marc_concom/&
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen, idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush , istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout,igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton, iusedens,igsigd0,&
iaem
!
! comments of variables:
!
! iacous Control flag for acoustic analysis. Input data.
! iacous=1 modal acoustic analysis.
! iacous=2 harmonic acoustic-structural analysis.
! iasmbl Control flag to indicate that operator matrix should be
! recalculated.
! iautth Control flag for AUTO THERM option.
! ibear Control flag for bearing analysis. Input data.
! icompl Control variable to indicate that a complex analysis is
! being performed. Either a Harmonic analysis with damping,
! or a harmonic electro-magnetic analysis. Input data.
! iconj Flag for EBE conjugate gradient solver (=solver 1, retired)
! Also used for VKI iterative solver.
! icreep Control flag for creep analysis. Input data.
! ideva(60) - debug print out flag
! 1 print element stiffness matrices, mass matrix
! 2 output matrices used in tying
! 3 force the solution of a nonpositive definite matrix
! 4 print info of connections to each node
! 5 info of gap convergence, internal heat generated, contact
! touching and separation
! 6 nodal value array during rezoning
! 7 tying info in CONRAD GAP option, fluid element numbers in
! CHANNEL option
! 8 output incremental displacements in local coord. system
! 9 latent heat output
! 10 stress-strain in local coord. system
! 11 additional info on interlaminar stress
! 12 output right hand side and solution vector
! 13 info of CPU resources used and memory available on NT
! 14 info of mesh adaption process, 2D outline information
! info of penetration checking for remeshing
! save .fem files after afmesh3d meshing
! 15 surface energy balance flag
! 16 print info regarding pyrolysis
! 17 print info of "streamline topology"
! 18 print mesh data changes after remeshing
! 19 print material flow stress data read in from *.mat file
! if unit flag is on, print out flow stress after conversion
! 20 print information on table input
! 21 print out information regarding kinematic boundary conditions
! 22 print out information regarding dist loads, point loads, film
! and foundations
! 23 print out information about automatic domain decomposition
! 24 print out iteration information in SuperForm status report file
! 25 print out information for ablation
! 26 print out information for films - Table input
! 27 print out the tying forces
! 28 print out for CASI solver, convection,
! 29 DDM single file debug printout
! 30 print out cavity debug info
! 31 print out welding related info
! 32 prints categorized DDM memory usage
! 33 print out the cutting info regarding machining feature
! 34 print out the list of quantities which can be defined via a table
! and for each quantity the supported independent variables
! 35 print out detailed coupling region info
! 36 print out solver debug info level 1 (Least Detailed)
! 37 print out solver debug info level 1 (Medium Detailed)
! 38 print out solver debug info level 1 (Very Detailed)
! 39 print detailed memory allocation info
! 40 print out marc-adams debug info
! 41 output rezone mapping post file for debugging
! 42 output post file after calling oprofos() for debugging
! 43 debug printout for vcct
! 44 debug printout for progressive failure
! 45 print out automatically generated midside node coordinates (arecrd)
! 46 print out message about routine and location, where the ibort is raised (ibort_inc)
! 47 print out summary message of element variables on a
! group-basis after all the automatic changes have been
! made (em_ellibp)
! 48 Automatically generate check results based on max and min vals.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the generate_check_results script from /marc/tools
! 49 Automatically generate check results based on the real calculated values
! at the sppecified check result locations.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the update_check_results script from /marc/tools
! 50 generate a file containing the resistance or capacity matrix;
! this file can be used to compare results with a reference file
! 51 print out detailed information for segment-to-segment contact
! 52 print out detailed relative displacement information
! for uniaxial sliding contact
! 53 print out detailed sliding direction information for
! uniaxial sliding contact
! 54 print out detailed information for edges attached to a curve
! 55 print information related to viscoelasticity calculations
! 56 print out detailed information for element coloring for multithreading
! 57 print out extra overheads due to multi-threading.
! These overhead includes (i) time and (ii) memory.
! The memory report will be summed over all the children.
!
!
! 58 debug output for ELSTO usage
!
! idyn Control flag for dynamics. Input data.
! 1 = eigenvalue extraction and / or modal superposition
! 2 = Newmark Beta and Single Step Houbolt (ssh with idynme=1)
! 3 = Houbolt
! 4 = Central difference
! 5 = Newer central difference
! idynt Copy of idyn at begining of increment
! ielas Control flag for ELASTIC analysis. Input data.
! Set by user or automatically turned on by Fourier option.
! Implies that each load case is treated separately.
! In Adaptive meshing analysis , forces re-analysis until
! convergence obtained.
! Also seriously misused to indicate no convergence.
! = 1 elastic option with fourier analysis
! = 2 elastic option without fourier analysis
! =-1 no convergence in recycles or max # increments reached
! Set to 1 if ELASTIC or SUBSTRUC parameter cards are used,
! or if fourier option is used.
! Then set to 2 if not fourier analysis.
! ielcma Control flag for electromagnetic analysis. Input data.
! ielcma = 1 Harmonic formulation
! ielcma = 2 Transient formulation
! ielect Control flag for electrostatic option. Input data.
! iform Control flag indicating that contact will be performed.
! ifour Control flag for Fourier analysis.
! 0 = Odd and even terms.
! 1 = symmetric (cosine) terms
! 2 = antisymmetric (sine) terms.
! iharm Control flag to indicate that a harmonic analysis will
! be performed. May change between passes.
! ihcps Control flag for coupled thermal - stress analysis.
! iheat Control flag for heat transfer analysis. Input data.
! iheatt Permanent control flag for heat transfer analysis.
! Note in coupled analysis iheatt will remain as one,
! but iheat will be zero in stress pass.
! ihresp Control flag to indicate to perform a harmonic subincrement.
! ijoule Control flag for Joule heating.
! ilem Control flag to determin which vector is to be transformed.
! Control flag to see where one is:
! ilem = 1 - elem.f
! ilem = 2 - initst.f
! ilem = 3 - pressr.f
! ilem = 3 - fstif.f
! ilem = 4 - jflux.f
! ilem = 4 - strass.f
! ilem = 5 - mass.f
! ilem = 5 - osolty.f
! ilnmom Control flag for soil - pore pressure calculation. Input data.
! ilnmom = 0 - perform only pore pressure calculation.
! = 1 - couples pore pressure - displacement analysis
! iloren Control flag for DeLorenzi J-Integral evaluation. Input data.
! inc Increment number.
! incext Control flag indicating that currently working on a
! subincrement.
! Could be due to harmonics , damping component (bearing),
! stiffness component (bearing), auto therm creep or
! old viscoplaticity
! incsub Sub-increment number.
! ipass Control flag for which part of coupled analysis.
! ipass = -1 - reset to base values
! ipass = 0 - do nothing
! ipass = 1 - stress part
! ipass = 2 - heat transfer part
! iplres Flag indicating that either second matrix is stored.
! dynamic analysis - mass matrix
! heat transfer - specific heat matrix
! buckle - initial stress stiffness
! ipois Control flag indicating Poisson type analysis
! ipois = 1 for heat transfer
! = 1 for heat transfer part of coupled
! = 1 for bearing
! = 1 for electrostatic
! = 1 for magnetostatic
! ipoist Permanent copy of ipois. In coupled analysis , ipois = 0
! in stress portion, yet ipoist will still =1.
! irpflo global flag for rigid plastic flow analysis
! = 1 eularian formulation
! = 2 regular formulation; rigid material present in the analysis
! ismall control flag to indicate small displacement analysis. input data.
! ismall = 0 - large disp included.
! ismall = 1 - small displacement.
! the flag is changing between passes.
! ismalt permanent copy of ismall . in heat transfer portion of
! coupled analysis ismall =0 , but ismalt remains the same.
! isoil control flag indicating that soil / pore pressure
! calculation . input data.
! ispect control flag for response spectrum calculation. input data.
! ispnow control flag to indicate to perform a spectrum response
! calculation now.
! istore store stresses flag.
! istore = 0 in elem.f and if first pass of creep
! convergence checking in ogetst.f
! or harmonic analysis or thruc.f if not
! converged.
! iswep control flag for eigenvalue analysis.
! iswep=1 - go do extraction process
! ithcrp control flag for auto therm creep option. input data.
! itherm control flag for either temperature dependent material
! properties and/or thermal loads.
! iupblg control flag for follower force option. input data.
! iupdat control flag for update lagrange option for current element.
! jacflg control flag for lanczos iteration method. input data.
! jel control flag indicating that total load applied in
! increment, ignore previous solution.
! jel = 1 in increment 0
! = 1 if elastic or fourier
! = 1 in subincrements with elastic and adaptive
! jparks control flag for j integral by parks method. input data.
! largst control flag for finite strain plasticity. input data.
! lfond control variable that indicates if doing elastic
! foundation or film calculation. influences whether
! this is volumetric or surface integration.
! loadup control flag that indicates that nonlinearity occurred
! during previous increment.
! loaduq control flag that indicates that nonlinearity occurred.
! lodcor control flag for switching on the residual load correction.
! notice in input stage lodcor=0 means no loadcor,
! after omarc lodcor=1 means no loadcor
! lovl control flag for determining which "overlay" is to
! be called from ellib.
! lovl = 1 omarc
! = 2 oaread
! = 3 opress
! = 4 oasemb
! = 5 osolty
! = 6 ogetst
! = 7 oscinc
! = 8 odynam
! = 9 opmesh
! = 10 omesh2
! = 11 osetz
! = 12 oass
! = 13 oincdt
! = 14 oasmas
! = 15 ofluas
! = 16 ofluso
! = 17 oshtra
! = 18 ocass
! = 19 osoltc
! = 20 orezon
! = 21 otest
! = 22 oeigen
! lsub control variable to determine which part of element
! assembly function is being done.
! lsub = 1 - no longer used
! = 2 - beta*
! = 3 - cons*
! = 4 - ldef*
! = 5 - posw*
! = 6 - theta*
! = 7 - tmarx*
! = 8 - geom*
! magnet control flag for magnetostatic analysis. input data.
! ncycle cycle number. accumulated in osolty.f
! note first time through oasemb.f , ncycle = 0.
! newtnt control flag for permanent copy of newton.
! newton iteration type. input data.
! newton : = 1 full newton raphson
! 2 modified newton raphson
! 3 newton raphson with strain correct.
! 4 direct substitution
! 5 direct substitution followed by n.r.
! 6 direct substitution with line search
! 7 full newton raphson with secant initial stress
! 8 secant method
! 9 full newton raphson with line search
! noshr control flag for calculation interlaminar shears for
! elements 22,45, and 75. input data.
!ees
!
! jactch = 1 or 2 if elements are activated or deactivated
! = 3 if elements are adaptively remeshed or rezoned
! = 0 normally / reset to 0 when assembly is done
! ifricsh = 0 call to fricsh in otest not needed
! = 1 call to fricsh (nodal friction) in otest needed
! iremkin = 0 remove deactivated kinematic boundary conditions
! immediately - only in new input format (this is default)
! = 1 remove deactivated kinematic boundary conditions
! gradually - only in new input format
! iremfor = 0 remove force boundary conditions immediately -
! only in new input format (this is default)
! = 1 remove force boundary conditions gradually -
! only in new input format (this is default)
! ishearp set to 1 if shear panel elements are present in the model
!
! jspf = 0 not in spf loadcase
! > 0 in spf loadcase (jspf=1 during first increment)
! machining = 1 if the metal cutting feature is used, for memory allocation purpose
! = 0 (default) if no metal cutting feature required
!
! jlshell = 1 if there is a shell element in the mesh
! icompsol = 1 if there is a composite solid element in the mesh
! iupblgfo = 1 if follower force for point loads
! jcondir = 1 if contact priority option is used
! nstcrp = 0 (default) steady state creep flag (undocumented feature.
! if not 0, turns off special ncycle = 0 code in radial.f)
! nactive = number of active passes, if =1 then it's not a coupled analysis
! ipassref = reference ipass, if not in a multiphysics pass ipass=ipassref
! icheckmpc = value of mpc-check parameter option
! noline = set to 1 in osolty if no line seacrh should be done in ogetst
! icuring = set to 1 if the curing is included for the heat transfer analysis.
! ishrink = set to 1 if shrinkage strain is included for mechancial analysis.
! ioffsflg = 1 for small displacement beam/shell offsets
! = 2 for large displacement beam/shell offsets
! isetoff = 0 - do not apply beam/shell offsets
! = 1 - apply beam/shell offsets
! ioffsetm = min. value of offset flag
! iharmt = 1 global flag if a coupled analysis contains an harmonic pass
! inc_incdat = flag to record increment number of a new loadcase in incdat.f
! iautspc = flag for AutoSPC option
! ibrake = brake squeal in this increment
! icbush = set to 1 if cbush elements present in model
! istream_input = set to 1 for streaming input calling Marc as library
! iprsinp = set to 1 if pressure input, introduced so other variables
! such as h could be a function of pressure
! ivlsinp = set to 1 if velocity input, introduced so other variables
! such as h could be a function of velocity
! ipin_m = # of beam element with PIN flag
! jgnstr_glb = global control over pre or fast integrated composite shells
! imarc_return = Marc return flag for streaming input control
! iqvcimp = if non-zero, then the number of QVECT boundary conditions
! nqvceid = number of QVECT boundary conditions, where emisivity/absorbtion id entered
! istpnx = 1 if to stop at end of increment
! imicro1 = 1 if micro1 interface is used
! iaxisymm = set to 1 if axisymmetric analysis
! jbreakglue = set to 1 if breaking glued option is used
! iglstif = 1 if ddm and global stiffness matrix formed (sgi solver 6 or solver9)
! jfastasm = 1 do fast assembly using SuperForm code
! iwear = set to 1 if wear model, set to 2 if wear model and coordinates updated
! iwearcf = set to 1 to store nodal coefficient of friction for wear calculation
! imixmeth = set=1 then use nonlinear mixture material - allocate memory
! ielcmadyn = flag for magnetodynamics
! 0 - electromagnetics using newmark beta
! 1 - transient magnetics using backward euler
! idinout = flag to control if inside out elements should be deactivated
! igena_meth = 0 - generalized alpha parameters depend on whether or not contact
! is flagged (dynamic,7)
! 10 - generalized alpha parameters are optimized for a contact
! analysis (dynamic,8)
! 11 - generalized alpha parameters are optimized for an analysis
! without contact (dynamic,8)
! magf_meth = - Method to compute force in magnetostatic - structural
! = 1 - Virtual work method based on finite difference for the force computation
! = 2 - Maxwell stress tensor
! = 3 - Virtual work method based on local derivative for the force computation
! non_assumed = 1 no assumed strain formulation (forced)
! iredoboudry set to 1 if contact boundary needs to be recalculated
! ioffsz0 = 1 if composite are used with reference position.ne.0
! icomplt = 1 global flag if a coupled analysis contains an complex pass
! mesh_dual = 1 two independent meshes are used in magnetodynamic/thermal/structural
! one for magnetodynamic and the other for the remaining passes
! iactrp = 1 in an analysis with global remeshing, include inactive
! rigid bodies on post file
! mgnewton = 1 Use full Newton Raphson iteration for magnetostatic pass
!
! iusedens > 0 if mass density is used in the analysis (dynamics, mass dependent loading)
! igsigd0 = 1 set varselem(igsigd) to zero in next oasemb
! iaem = 1 if marc is called from aem (0 - off - default)
!
!
!***********************************************************************
!$omp threadprivate(/marc_concom/)
!!

View File

@ -1,412 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: concom.cmn
!
! MSC.Marc include file
!
integer(pInt) &
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen , idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush, istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout, igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton, iusedens,igsigd0,&
iaem, icosim
dimension :: ideva(60)
integer(pInt) num_concom
parameter(num_concom=241)
common/marc_concom/&
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen, idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush , istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout,igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton, iusedens,igsigd0,&
iaem, icosim
!
! comments of variables:
!
! iacous Control flag for acoustic analysis. Input data.
! iacous=1 modal acoustic analysis.
! iacous=2 harmonic acoustic-structural analysis.
! iasmbl Control flag to indicate that operator matrix should be
! recalculated.
! iautth Control flag for AUTO THERM option.
! ibear Control flag for bearing analysis. Input data.
! icompl Control variable to indicate that a complex analysis is
! being performed. Either a Harmonic analysis with damping,
! or a harmonic electro-magnetic analysis. Input data.
! iconj Flag for EBE conjugate gradient solver (=solver 1, retired)
! Also used for VKI iterative solver.
! icreep Control flag for creep analysis. Input data.
! ideva(60) - debug print out flag
! 1 print element stiffness matrices, mass matrix
! 2 output matrices used in tying
! 3 force the solution of a nonpositive definite matrix
! 4 print info of connections to each node
! 5 info of gap convergence, internal heat generated, contact
! touching and separation
! 6 nodal value array during rezoning
! 7 tying info in CONRAD GAP option, fluid element numbers in
! CHANNEL option
! 8 output incremental displacements in local coord. system
! 9 latent heat output
! 10 stress-strain in local coord. system
! 11 additional info on interlaminar stress
! 12 output right hand side and solution vector
! 13 info of CPU resources used and memory available on NT
! 14 info of mesh adaption process, 2D outline information
! info of penetration checking for remeshing
! save .fem files after afmesh3d meshing
! 15 surface energy balance flag
! 16 print info regarding pyrolysis
! 17 print info of "streamline topology"
! 18 print mesh data changes after remeshing
! 19 print material flow stress data read in from *.mat file
! if unit flag is on, print out flow stress after conversion
! 20 print information on table input
! 21 print out information regarding kinematic boundary conditions
! 22 print out information regarding dist loads, point loads, film
! and foundations
! 23 print out information about automatic domain decomposition
! 24 print out iteration information in SuperForm status report file
! 25 print out information for ablation
! 26 print out information for films - Table input
! 27 print out the tying forces
! 28 print out for CASI solver, convection,
! 29 DDM single file debug printout
! 30 print out cavity debug info
! 31 print out welding related info
! 32 prints categorized DDM memory usage
! 33 print out the cutting info regarding machining feature
! 34 print out the list of quantities which can be defined via a table
! and for each quantity the supported independent variables
! 35 print out detailed coupling region info
! 36 print out solver debug info level 1 (Least Detailed)
! 37 print out solver debug info level 1 (Medium Detailed)
! 38 print out solver debug info level 1 (Very Detailed)
! 39 print detailed memory allocation info
! 40 print out marc-adams debug info
! 41 output rezone mapping post file for debugging
! 42 output post file after calling oprofos() for debugging
! 43 debug printout for vcct
! 44 debug printout for progressive failure
! 45 print out automatically generated midside node coordinates (arecrd)
! 46 print out message about routine and location, where the ibort is raised (ibort_inc)
! 47 print out summary message of element variables on a
! group-basis after all the automatic changes have been
! made (em_ellibp)
! 48 Automatically generate check results based on max and min vals.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the generate_check_results script from /marc/tools
! 49 Automatically generate check results based on the real calculated values
! at the sppecified check result locations.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the update_check_results script from /marc/tools
! 50 generate a file containing the resistance or capacity matrix;
! this file can be used to compare results with a reference file
! 51 print out detailed information for segment-to-segment contact
! 52 print out detailed relative displacement information
! for uniaxial sliding contact
! 53 print out detailed sliding direction information for
! uniaxial sliding contact
! 54 print out detailed information for edges attached to a curve
! 55 print information related to viscoelasticity calculations
! 56 print out detailed information for element coloring for multithreading
! 57 print out extra overheads due to multi-threading.
! These overhead includes (i) time and (ii) memory.
! The memory report will be summed over all the children.
!
!
! 58 debug output for ELSTO usage
!
! idyn Control flag for dynamics. Input data.
! 1 = eigenvalue extraction and / or modal superposition
! 2 = Newmark Beta and Single Step Houbolt (ssh with idynme=1)
! 3 = Houbolt
! 4 = Central difference
! 5 = Newer central difference
! idynt Copy of idyn at begining of increment
! ielas Control flag for ELASTIC analysis. Input data.
! Set by user or automatically turned on by Fourier option.
! Implies that each load case is treated separately.
! In Adaptive meshing analysis , forces re-analysis until
! convergence obtained.
! Also seriously misused to indicate no convergence.
! = 1 elastic option with fourier analysis
! = 2 elastic option without fourier analysis
! =-1 no convergence in recycles or max # increments reached
! Set to 1 if ELASTIC or SUBSTRUC parameter cards are used,
! or if fourier option is used.
! Then set to 2 if not fourier analysis.
! ielcma Control flag for electromagnetic analysis. Input data.
! ielcma = 1 Harmonic formulation
! ielcma = 2 Transient formulation
! ielect Control flag for electrostatic option. Input data.
! iform Control flag indicating that contact will be performed.
! ifour Control flag for Fourier analysis.
! 0 = Odd and even terms.
! 1 = symmetric (cosine) terms
! 2 = antisymmetric (sine) terms.
! iharm Control flag to indicate that a harmonic analysis will
! be performed. May change between passes.
! ihcps Control flag for coupled thermal - stress analysis.
! iheat Control flag for heat transfer analysis. Input data.
! iheatt Permanent control flag for heat transfer analysis.
! Note in coupled analysis iheatt will remain as one,
! but iheat will be zero in stress pass.
! ihresp Control flag to indicate to perform a harmonic subincrement.
! ijoule Control flag for Joule heating.
! ilem Control flag to determin which vector is to be transformed.
! Control flag to see where one is:
! ilem = 1 - elem.f
! ilem = 2 - initst.f
! ilem = 3 - pressr.f
! ilem = 3 - fstif.f
! ilem = 4 - jflux.f
! ilem = 4 - strass.f
! ilem = 5 - mass.f
! ilem = 5 - osolty.f
! ilnmom Control flag for soil - pore pressure calculation. Input data.
! ilnmom = 0 - perform only pore pressure calculation.
! = 1 - couples pore pressure - displacement analysis
! iloren Control flag for DeLorenzi J-Integral evaluation. Input data.
! inc Increment number.
! incext Control flag indicating that currently working on a
! subincrement.
! Could be due to harmonics , damping component (bearing),
! stiffness component (bearing), auto therm creep or
! old viscoplaticity
! incsub Sub-increment number.
! ipass Control flag for which part of coupled analysis.
! ipass = -1 - reset to base values
! ipass = 0 - do nothing
! ipass = 1 - stress part
! ipass = 2 - heat transfer part
! iplres Flag indicating that either second matrix is stored.
! dynamic analysis - mass matrix
! heat transfer - specific heat matrix
! buckle - initial stress stiffness
! ipois Control flag indicating Poisson type analysis
! ipois = 1 for heat transfer
! = 1 for heat transfer part of coupled
! = 1 for bearing
! = 1 for electrostatic
! = 1 for magnetostatic
! ipoist Permanent copy of ipois. In coupled analysis , ipois = 0
! in stress portion, yet ipoist will still =1.
! irpflo global flag for rigid plastic flow analysis
! = 1 eularian formulation
! = 2 regular formulation; rigid material present in the analysis
! ismall control flag to indicate small displacement analysis. input data.
! ismall = 0 - large disp included.
! ismall = 1 - small displacement.
! the flag is changing between passes.
! ismalt permanent copy of ismall . in heat transfer portion of
! coupled analysis ismall =0 , but ismalt remains the same.
! isoil control flag indicating that soil / pore pressure
! calculation . input data.
! ispect control flag for response spectrum calculation. input data.
! ispnow control flag to indicate to perform a spectrum response
! calculation now.
! istore store stresses flag.
! istore = 0 in elem.f and if first pass of creep
! convergence checking in ogetst.f
! or harmonic analysis or thruc.f if not
! converged.
! iswep control flag for eigenvalue analysis.
! iswep=1 - go do extraction process
! ithcrp control flag for auto therm creep option. input data.
! itherm control flag for either temperature dependent material
! properties and/or thermal loads.
! iupblg control flag for follower force option. input data.
! iupdat control flag for update lagrange option for current element.
! jacflg control flag for lanczos iteration method. input data.
! jel control flag indicating that total load applied in
! increment, ignore previous solution.
! jel = 1 in increment 0
! = 1 if elastic or fourier
! = 1 in subincrements with elastic and adaptive
! jparks control flag for j integral by parks method. input data.
! largst control flag for finite strain plasticity. input data.
! lfond control variable that indicates if doing elastic
! foundation or film calculation. influences whether
! this is volumetric or surface integration.
! loadup control flag that indicates that nonlinearity occurred
! during previous increment.
! loaduq control flag that indicates that nonlinearity occurred.
! lodcor control flag for switching on the residual load correction.
! notice in input stage lodcor=0 means no loadcor,
! after omarc lodcor=1 means no loadcor
! lovl control flag for determining which "overlay" is to
! be called from ellib.
! lovl = 1 omarc
! = 2 oaread
! = 3 opress
! = 4 oasemb
! = 5 osolty
! = 6 ogetst
! = 7 oscinc
! = 8 odynam
! = 9 opmesh
! = 10 omesh2
! = 11 osetz
! = 12 oass
! = 13 oincdt
! = 14 oasmas
! = 15 ofluas
! = 16 ofluso
! = 17 oshtra
! = 18 ocass
! = 19 osoltc
! = 20 orezon
! = 21 otest
! = 22 oeigen
! lsub control variable to determine which part of element
! assembly function is being done.
! lsub = 1 - no longer used
! = 2 - beta*
! = 3 - cons*
! = 4 - ldef*
! = 5 - posw*
! = 6 - theta*
! = 7 - tmarx*
! = 8 - geom*
! magnet control flag for magnetostatic analysis. input data.
! ncycle cycle number. accumulated in osolty.f
! note first time through oasemb.f , ncycle = 0.
! newtnt control flag for permanent copy of newton.
! newton iteration type. input data.
! newton : = 1 full newton raphson
! 2 modified newton raphson
! 3 newton raphson with strain correct.
! 4 direct substitution
! 5 direct substitution followed by n.r.
! 6 direct substitution with line search
! 7 full newton raphson with secant initial stress
! 8 secant method
! 9 full newton raphson with line search
! noshr control flag for calculation interlaminar shears for
! elements 22,45, and 75. input data.
!ees
!
! jactch = 1 or 2 if elements are activated or deactivated
! = 3 if elements are adaptively remeshed or rezoned
! = 0 normally / reset to 0 when assembly is done
! ifricsh = 0 call to fricsh in otest not needed
! = 1 call to fricsh (nodal friction) in otest needed
! iremkin = 0 remove deactivated kinematic boundary conditions
! immediately - only in new input format (this is default)
! = 1 remove deactivated kinematic boundary conditions
! gradually - only in new input format
! iremfor = 0 remove force boundary conditions immediately -
! only in new input format (this is default)
! = 1 remove force boundary conditions gradually -
! only in new input format (this is default)
! ishearp set to 1 if shear panel elements are present in the model
!
! jspf = 0 not in spf loadcase
! > 0 in spf loadcase (jspf=1 during first increment)
! machining = 1 if the metal cutting feature is used, for memory allocation purpose
! = 0 (default) if no metal cutting feature required
!
! jlshell = 1 if there is a shell element in the mesh
! icompsol = 1 if there is a composite solid element in the mesh
! iupblgfo = 1 if follower force for point loads
! jcondir = 1 if contact priority option is used
! nstcrp = 0 (default) steady state creep flag (undocumented feature.
! if not 0, turns off special ncycle = 0 code in radial.f)
! nactive = number of active passes, if =1 then it's not a coupled analysis
! ipassref = reference ipass, if not in a multiphysics pass ipass=ipassref
! icheckmpc = value of mpc-check parameter option
! noline = set to 1 in osolty if no line seacrh should be done in ogetst
! icuring = set to 1 if the curing is included for the heat transfer analysis.
! ishrink = set to 1 if shrinkage strain is included for mechancial analysis.
! ioffsflg = 1 for small displacement beam/shell offsets
! = 2 for large displacement beam/shell offsets
! isetoff = 0 - do not apply beam/shell offsets
! = 1 - apply beam/shell offsets
! ioffsetm = min. value of offset flag
! iharmt = 1 global flag if a coupled analysis contains an harmonic pass
! inc_incdat = flag to record increment number of a new loadcase in incdat.f
! iautspc = flag for AutoSPC option
! ibrake = brake squeal in this increment
! icbush = set to 1 if cbush elements present in model
! istream_input = set to 1 for streaming input calling Marc as library
! iprsinp = set to 1 if pressure input, introduced so other variables
! such as h could be a function of pressure
! ivlsinp = set to 1 if velocity input, introduced so other variables
! such as h could be a function of velocity
! ipin_m = # of beam element with PIN flag
! jgnstr_glb = global control over pre or fast integrated composite shells
! imarc_return = Marc return flag for streaming input control
! iqvcimp = if non-zero, then the number of QVECT boundary conditions
! nqvceid = number of QVECT boundary conditions, where emisivity/absorbtion id entered
! istpnx = 1 if to stop at end of increment
! imicro1 = 1 if micro1 interface is used
! iaxisymm = set to 1 if axisymmetric analysis
! jbreakglue = set to 1 if breaking glued option is used
! iglstif = 1 if ddm and global stiffness matrix formed (sgi solver 6 or solver9)
! jfastasm = 1 do fast assembly using SuperForm code
! iwear = set to 1 if wear model, set to 2 if wear model and coordinates updated
! iwearcf = set to 1 to store nodal coefficient of friction for wear calculation
! imixmeth = set=1 then use nonlinear mixture material - allocate memory
! ielcmadyn = flag for magnetodynamics
! 0 - electromagnetics using newmark beta
! 1 - transient magnetics using backward euler
! idinout = flag to control if inside out elements should be deactivated
! igena_meth = 0 - generalized alpha parameters depend on whether or not contact
! is flagged (dynamic,7)
! 10 - generalized alpha parameters are optimized for a contact
! analysis (dynamic,8)
! 11 - generalized alpha parameters are optimized for an analysis
! without contact (dynamic,8)
! magf_meth = - Method to compute force in magnetostatic - structural
! = 1 - Virtual work method based on finite difference for the force computation
! = 2 - Maxwell stress tensor
! = 3 - Virtual work method based on local derivative for the force computation
! non_assumed = 1 no assumed strain formulation (forced)
! iredoboudry set to 1 if contact boundary needs to be recalculated
! ioffsz0 = 1 if composite are used with reference position.ne.0
! icomplt = 1 global flag if a coupled analysis contains an complex pass
! mesh_dual = 1 two independent meshes are used in magnetodynamic/thermal/structural
! one for magnetodynamic and the other for the remaining passes
! iactrp = 1 in an analysis with global remeshing, include inactive
! rigid bodies on post file
! mgnewton = 1 Use full Newton Raphson iteration for magnetostatic pass
!
! iusedens > 0 if mass density is used in the analysis (dynamics, mass dependent loading)
! igsigd0 = 1 set varselem(igsigd) to zero in next oasemb
! iaem = 1 if marc is called from aem (0 - off - default)
! icosim = 1 if marc is used in co-simulation software (ADAMS-MARC)
!
!
!***********************************************************************
!$omp threadprivate(/marc_concom/)
!!

View File

@ -1,416 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: concom.cmn
!
! MSC.Marc include file
!
integer(pInt) &
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen , idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush, istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout, igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton, iusedens,igsigd0,&
iaem, icosim, inodels, nlharm, iampini
dimension :: ideva(60)
integer(pInt) num_concom
parameter(num_concom=244)
common/marc_concom/&
iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
ncycnt, marmen, idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush , istream_input,&
iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout,igena_meth,&
magf_meth, non_assumed, iredoboudry, ioffsz0,icomplt, mesh_dual, iactrp, mgnewton, iusedens,igsigd0,&
iaem, icosim, inodels, nlharm, iampini
!
! comments of variables:
!
! iacous Control flag for acoustic analysis. Input data.
! iacous=1 modal acoustic analysis.
! iacous=2 harmonic acoustic-structural analysis.
! iasmbl Control flag to indicate that operator matrix should be
! recalculated.
! iautth Control flag for AUTO THERM option.
! ibear Control flag for bearing analysis. Input data.
! icompl Control variable to indicate that a complex analysis is
! being performed. Either a Harmonic analysis with damping,
! or a harmonic electro-magnetic analysis. Input data.
! iconj Flag for EBE conjugate gradient solver (=solver 1, retired)
! Also used for VKI iterative solver.
! icreep Control flag for creep analysis. Input data.
! ideva(60) - debug print out flag
! 1 print element stiffness matrices, mass matrix
! 2 output matrices used in tying
! 3 force the solution of a nonpositive definite matrix
! 4 print info of connections to each node
! 5 info of gap convergence, internal heat generated, contact
! touching and separation
! 6 nodal value array during rezoning
! 7 tying info in CONRAD GAP option, fluid element numbers in
! CHANNEL option
! 8 output incremental displacements in local coord. system
! 9 latent heat output
! 10 stress-strain in local coord. system
! 11 additional info on interlaminar stress
! 12 output right hand side and solution vector
! 13 info of CPU resources used and memory available on NT
! 14 info of mesh adaption process, 2D outline information
! info of penetration checking for remeshing
! save .fem files after afmesh3d meshing
! 15 surface energy balance flag
! 16 print info regarding pyrolysis
! 17 print info of "streamline topology"
! 18 print mesh data changes after remeshing
! 19 print material flow stress data read in from *.mat file
! if unit flag is on, print out flow stress after conversion
! 20 print information on table input
! 21 print out information regarding kinematic boundary conditions
! 22 print out information regarding dist loads, point loads, film
! and foundations
! 23 print out information about automatic domain decomposition
! 24 print out iteration information in SuperForm status report file
! 25 print out information for ablation
! 26 print out information for films - Table input
! 27 print out the tying forces
! 28 print out for CASI solver, convection,
! 29 DDM single file debug printout
! 30 print out cavity debug info
! 31 print out welding related info
! 32 prints categorized DDM memory usage
! 33 print out the cutting info regarding machining feature
! 34 print out the list of quantities which can be defined via a table
! and for each quantity the supported independent variables
! 35 print out detailed coupling region info
! 36 print out solver debug info level 1 (Least Detailed)
! 37 print out solver debug info level 1 (Medium Detailed)
! 38 print out solver debug info level 1 (Very Detailed)
! 39 print detailed memory allocation info
! 40 print out marc-adams debug info
! 41 output rezone mapping post file for debugging
! 42 output post file after calling oprofos() for debugging
! 43 debug printout for vcct
! 44 debug printout for progressive failure
! 45 print out automatically generated midside node coordinates (arecrd)
! 46 print out message about routine and location, where the ibort is raised (ibort_inc)
! 47 print out summary message of element variables on a
! group-basis after all the automatic changes have been
! made (em_ellibp)
! 48 Automatically generate check results based on max and min vals.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the generate_check_results script from /marc/tools
! 49 Automatically generate check results based on the real calculated values
! at the sppecified check result locations.
! These vals are stored in the checkr file, which is inserted
! into the *dat file by the update_check_results script from /marc/tools
! 50 generate a file containing the resistance or capacity matrix;
! this file can be used to compare results with a reference file
! 51 print out detailed information for segment-to-segment contact
! 52 print out detailed relative displacement information
! for uniaxial sliding contact
! 53 print out detailed sliding direction information for
! uniaxial sliding contact
! 54 print out detailed information for edges attached to a curve
! 55 print information related to viscoelasticity calculations
! 56 print out detailed information for element coloring for multithreading
! 57 print out extra overheads due to multi-threading.
! These overhead includes (i) time and (ii) memory.
! The memory report will be summed over all the children.
!
!
! 58 debug output for ELSTO usage
!
! idyn Control flag for dynamics. Input data.
! 1 = eigenvalue extraction and / or modal superposition
! 2 = Newmark Beta and Single Step Houbolt (ssh with idynme=1)
! 3 = Houbolt
! 4 = Central difference
! 5 = Newer central difference
! idynt Copy of idyn at begining of increment
! ielas Control flag for ELASTIC analysis. Input data.
! Set by user or automatically turned on by Fourier option.
! Implies that each load case is treated separately.
! In Adaptive meshing analysis , forces re-analysis until
! convergence obtained.
! Also seriously misused to indicate no convergence.
! = 1 elastic option with fourier analysis
! = 2 elastic option without fourier analysis
! =-1 no convergence in recycles or max # increments reached
! Set to 1 if ELASTIC or SUBSTRUC parameter cards are used,
! or if fourier option is used.
! Then set to 2 if not fourier analysis.
! ielcma Control flag for electromagnetic analysis. Input data.
! ielcma = 1 Harmonic formulation
! ielcma = 2 Transient formulation
! ielect Control flag for electrostatic option. Input data.
! iform Control flag indicating that contact will be performed.
! ifour Control flag for Fourier analysis.
! 0 = Odd and even terms.
! 1 = symmetric (cosine) terms
! 2 = antisymmetric (sine) terms.
! iharm Control flag to indicate that a harmonic analysis will
! be performed. May change between passes.
! ihcps Control flag for coupled thermal - stress analysis.
! iheat Control flag for heat transfer analysis. Input data.
! iheatt Permanent control flag for heat transfer analysis.
! Note in coupled analysis iheatt will remain as one,
! but iheat will be zero in stress pass.
! ihresp Control flag to indicate to perform a harmonic subincrement.
! ijoule Control flag for Joule heating.
! ilem Control flag to determin which vector is to be transformed.
! Control flag to see where one is:
! ilem = 1 - elem.f
! ilem = 2 - initst.f
! ilem = 3 - pressr.f
! ilem = 3 - fstif.f
! ilem = 4 - jflux.f
! ilem = 4 - strass.f
! ilem = 5 - mass.f
! ilem = 5 - osolty.f
! ilnmom Control flag for soil - pore pressure calculation. Input data.
! ilnmom = 0 - perform only pore pressure calculation.
! = 1 - couples pore pressure - displacement analysis
! iloren Control flag for DeLorenzi J-Integral evaluation. Input data.
! inc Increment number.
! incext Control flag indicating that currently working on a
! subincrement.
! Could be due to harmonics , damping component (bearing),
! stiffness component (bearing), auto therm creep or
! old viscoplaticity
! incsub Sub-increment number.
! ipass Control flag for which part of coupled analysis.
! ipass = -1 - reset to base values
! ipass = 0 - do nothing
! ipass = 1 - stress part
! ipass = 2 - heat transfer part
! iplres Flag indicating that either second matrix is stored.
! dynamic analysis - mass matrix
! heat transfer - specific heat matrix
! buckle - initial stress stiffness
! ipois Control flag indicating Poisson type analysis
! ipois = 1 for heat transfer
! = 1 for heat transfer part of coupled
! = 1 for bearing
! = 1 for electrostatic
! = 1 for magnetostatic
! ipoist Permanent copy of ipois. In coupled analysis , ipois = 0
! in stress portion, yet ipoist will still =1.
! irpflo global flag for rigid plastic flow analysis
! = 1 eularian formulation
! = 2 regular formulation; rigid material present in the analysis
! ismall control flag to indicate small displacement analysis. input data.
! ismall = 0 - large disp included.
! ismall = 1 - small displacement.
! the flag is changing between passes.
! ismalt permanent copy of ismall . in heat transfer portion of
! coupled analysis ismall =0 , but ismalt remains the same.
! isoil control flag indicating that soil / pore pressure
! calculation . input data.
! ispect control flag for response spectrum calculation. input data.
! ispnow control flag to indicate to perform a spectrum response
! calculation now.
! istore store stresses flag.
! istore = 0 in elem.f and if first pass of creep
! convergence checking in ogetst.f
! or harmonic analysis or thruc.f if not
! converged.
! iswep control flag for eigenvalue analysis.
! iswep=1 - go do extraction process
! ithcrp control flag for auto therm creep option. input data.
! itherm control flag for either temperature dependent material
! properties and/or thermal loads.
! iupblg control flag for follower force option. input data.
! iupdat control flag for update lagrange option for current element.
! jacflg control flag for lanczos iteration method. input data.
! jel control flag indicating that total load applied in
! increment, ignore previous solution.
! jel = 1 in increment 0
! = 1 if elastic or fourier
! = 1 in subincrements with elastic and adaptive
! jparks control flag for j integral by parks method. input data.
! largst control flag for finite strain plasticity. input data.
! lfond control variable that indicates if doing elastic
! foundation or film calculation. influences whether
! this is volumetric or surface integration.
! loadup control flag that indicates that nonlinearity occurred
! during previous increment.
! loaduq control flag that indicates that nonlinearity occurred.
! lodcor control flag for switching on the residual load correction.
! notice in input stage lodcor=0 means no loadcor,
! after omarc lodcor=1 means no loadcor
! lovl control flag for determining which "overlay" is to
! be called from ellib.
! lovl = 1 omarc
! = 2 oaread
! = 3 opress
! = 4 oasemb
! = 5 osolty
! = 6 ogetst
! = 7 oscinc
! = 8 odynam
! = 9 opmesh
! = 10 omesh2
! = 11 osetz
! = 12 oass
! = 13 oincdt
! = 14 oasmas
! = 15 ofluas
! = 16 ofluso
! = 17 oshtra
! = 18 ocass
! = 19 osoltc
! = 20 orezon
! = 21 otest
! = 22 oeigen
! lsub control variable to determine which part of element
! assembly function is being done.
! lsub = 1 - no longer used
! = 2 - beta*
! = 3 - cons*
! = 4 - ldef*
! = 5 - posw*
! = 6 - theta*
! = 7 - tmarx*
! = 8 - geom*
! magnet control flag for magnetostatic analysis. input data.
! ncycle cycle number. accumulated in osolty.f
! note first time through oasemb.f , ncycle = 0.
! newtnt control flag for permanent copy of newton.
! newton iteration type. input data.
! newton : = 1 full newton raphson
! 2 modified newton raphson
! 3 newton raphson with strain correct.
! 4 direct substitution
! 5 direct substitution followed by n.r.
! 6 direct substitution with line search
! 7 full newton raphson with secant initial stress
! 8 secant method
! 9 full newton raphson with line search
! noshr control flag for calculation interlaminar shears for
! elements 22,45, and 75. input data.
!ees
!
! jactch = 1 or 2 if elements are activated or deactivated
! = 3 if elements are adaptively remeshed or rezoned
! = 0 normally / reset to 0 when assembly is done
! ifricsh = 0 call to fricsh in otest not needed
! = 1 call to fricsh (nodal friction) in otest needed
! iremkin = 0 remove deactivated kinematic boundary conditions
! immediately - only in new input format (this is default)
! = 1 remove deactivated kinematic boundary conditions
! gradually - only in new input format
! iremfor = 0 remove force boundary conditions immediately -
! only in new input format (this is default)
! = 1 remove force boundary conditions gradually -
! only in new input format (this is default)
! ishearp set to 1 if shear panel elements are present in the model
!
! jspf = 0 not in spf loadcase
! > 0 in spf loadcase (jspf=1 during first increment)
! machining = 1 if the metal cutting feature is used, for memory allocation purpose
! = 0 (default) if no metal cutting feature required
!
! jlshell = 1 if there is a shell element in the mesh
! icompsol = 1 if there is a composite solid element in the mesh
! iupblgfo = 1 if follower force for point loads
! jcondir = 1 if contact priority option is used
! nstcrp = 0 (default) steady state creep flag (undocumented feature.
! if not 0, turns off special ncycle = 0 code in radial.f)
! nactive = number of active passes, if =1 then it's not a coupled analysis
! ipassref = reference ipass, if not in a multiphysics pass ipass=ipassref
! icheckmpc = value of mpc-check parameter option
! noline = set to 1 in osolty if no line seacrh should be done in ogetst
! icuring = set to 1 if the curing is included for the heat transfer analysis.
! ishrink = set to 1 if shrinkage strain is included for mechancial analysis.
! ioffsflg = 1 for small displacement beam/shell offsets
! = 2 for large displacement beam/shell offsets
! isetoff = 0 - do not apply beam/shell offsets
! = 1 - apply beam/shell offsets
! ioffsetm = min. value of offset flag
! iharmt = 1 global flag if a coupled analysis contains an harmonic pass
! inc_incdat = flag to record increment number of a new loadcase in incdat.f
! iautspc = flag for AutoSPC option
! ibrake = brake squeal in this increment
! icbush = set to 1 if cbush elements present in model
! istream_input = set to 1 for streaming input calling Marc as library
! iprsinp = set to 1 if pressure input, introduced so other variables
! such as h could be a function of pressure
! ivlsinp = set to 1 if velocity input, introduced so other variables
! such as h could be a function of velocity
! ipin_m = # of beam element with PIN flag
! jgnstr_glb = global control over pre or fast integrated composite shells
! imarc_return = Marc return flag for streaming input control
! iqvcimp = if non-zero, then the number of QVECT boundary conditions
! nqvceid = number of QVECT boundary conditions, where emisivity/absorbtion id entered
! istpnx = 1 if to stop at end of increment
! imicro1 = 1 if micro1 interface is used
! iaxisymm = set to 1 if axisymmetric analysis
! jbreakglue = set to 1 if breaking glued option is used
! iglstif = 1 if ddm and global stiffness matrix formed (sgi solver 6 or solver9)
! jfastasm = 1 do fast assembly using SuperForm code
! iwear = set to 1 if wear model, set to 2 if wear model and coordinates updated
! iwearcf = set to 1 to store nodal coefficient of friction for wear calculation
! imixmeth = set=1 then use nonlinear mixture material - allocate memory
! ielcmadyn = flag for magnetodynamics
! 0 - electromagnetics using newmark beta
! 1 - transient magnetics using backward euler
! idinout = flag to control if inside out elements should be deactivated
! igena_meth = 0 - generalized alpha parameters depend on whether or not contact
! is flagged (dynamic,7)
! 10 - generalized alpha parameters are optimized for a contact
! analysis (dynamic,8)
! 11 - generalized alpha parameters are optimized for an analysis
! without contact (dynamic,8)
! magf_meth = - Method to compute force in magnetostatic - structural
! = 1 - Virtual work method based on finite difference for the force computation
! = 2 - Maxwell stress tensor
! = 3 - Virtual work method based on local derivative for the force computation
! non_assumed = 1 no assumed strain formulation (forced)
! iredoboudry set to 1 if contact boundary needs to be recalculated
! ioffsz0 = 1 if composite are used with reference position.ne.0
! icomplt = 1 global flag if a coupled analysis contains an complex pass
! mesh_dual = 1 two independent meshes are used in magnetodynamic/thermal/structural
! one for magnetodynamic and the other for the remaining passes
! iactrp = 1 in an analysis with global remeshing, include inactive
! rigid bodies on post file
! mgnewton = 1 Use full Newton Raphson iteration for magnetostatic pass
!
! iusedens > 0 if mass density is used in the analysis (dynamics, mass dependent loading)
! igsigd0 = 1 set varselem(igsigd) to zero in next oasemb
! iaem = 1 if marc is called from aem (0 - off - default)
! icosim = 1 if marc is used in co-simulation software (ADAMS-MARC)
! inodels = 1 nodal integration elements 239/240/241 present
! nlharm = 0 harmonic subincrements are linear
! = 1 harmonic subincrements are nonlinear
! iampini = 0 amplitude of previous harmonic subinc is initial estimate (default)
! = 1 zero amplitude is initial estimate
!
!***********************************************************************
!$omp threadprivate(/marc_concom/)
!!

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@ -1,28 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: creeps.cmn
!
! MSC.Marc include file
!
real(pReal) cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b,creept
integer(pInt) icptim,icfte,icfst,icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,&
icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
real(pReal) time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
integer(pInt) num_creepsr,num_creepsi,num_creeps2r
parameter(num_creepsr=40)
parameter(num_creepsi=18)
parameter(num_creeps2r=4)
common/marc_creeps/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
common/marc_creeps2/time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
! time_beg_lcase time at the beginning of the current load case
! time_beg_inc time at the beginning of the current increment
! fractol fraction of loadcase or increment time when we
! consider it to be finished
! time_beg_pst time corresponding to first increment to be
! read in from thermal post file for auto step
!
!***********************************************************************

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@ -1,28 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: creeps.cmn
!
! MSC.Marc include file
!
real(pReal) cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b,creept
integer(pInt) icptim,icfte,icfst,icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,&
icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
real(pReal) time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
integer(pInt) num_creepsr,num_creepsi,num_creeps2r
parameter(num_creepsr=40)
parameter(num_creepsi=18)
parameter(num_creeps2r=4)
common/marc_creeps/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
common/marc_creeps2/time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
! time_beg_lcase time at the beginning of the current load case
! time_beg_inc time at the beginning of the current increment
! fractol fraction of loadcase or increment time when we
! consider it to be finished
! time_beg_pst time corresponding to first increment to be
! read in from thermal post file for auto step
!
!***********************************************************************

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@ -1,28 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: creeps.cmn
!
! MSC.Marc include file
!
real(pReal) cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b,creept
integer(pInt) icptim,icfte,icfst,icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,&
icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
real(pReal) time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
integer(pInt) num_creepsr,num_creepsi,num_creeps2r
parameter(num_creepsr=40)
parameter(num_creepsi=18)
parameter(num_creeps2r=4)
common/marc_creeps/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
common/marc_creeps2/time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
! time_beg_lcase time at the beginning of the current load case
! time_beg_inc time at the beginning of the current increment
! fractol fraction of loadcase or increment time when we
! consider it to be finished
! time_beg_pst time corresponding to first increment to be
! read in from thermal post file for auto step
!
!***********************************************************************

View File

@ -1,31 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: creeps.cmn
!
! MSC.Marc include file
!
real(pReal) cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b
integer(pInt) icptim,icfte,icfst,icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,&
icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
real(pReal) time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
integer(pInt) num_creepsr,num_creepsi,num_creeps2r
parameter(num_creepsr=7)
parameter(num_creepsi=18)
parameter(num_creeps2r=4)
common/marc_creeps/cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b,icptim,icfte,icfst,&
icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
common/marc_creeps2/time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
! time_beg_lcase time at the beginning of the current load case
! time_beg_inc time at the beginning of the current increment
! fractol fraction of loadcase or increment time when we
! consider it to be finished
! time_beg_pst time corresponding to first increment to be
! read in from thermal post file for auto step
!
!***********************************************************************
!$omp threadprivate(/marc_creeps/)
!$omp threadprivate(/marc_creeps2/)
!!

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@ -1,63 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: creeps.cmn
!
! MSC.Marc include file
!
real(pReal) cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b
integer(pInt) icfte,icfst,icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,&
icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
real(pReal) time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
integer(pInt) num_creepsr,num_creepsi,num_creeps2r
parameter(num_creepsr=7)
parameter(num_creepsi=17)
parameter(num_creeps2r=4)
common/marc_creeps/cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b,icfte,icfst,&
icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
common/marc_creeps2/time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
! cptim Total time at begining of increment.
! timinc Incremental time for this step.
! icfte Local copy number of slopes of creep strain rate function
! versus temperature. Is -1 if exponent law used.
! icfst Local copy number of slopes of creep strain rate function
! versus equivalent stress. Is -1 if exponent law used.
! icfeq Local copy number of slopes of creep strain rate function
! versus equivalent strain. Is -1 if exponent law used.
! icftm Local copy number of slopes of creep strain rate function
! versus time. Is -1 if exponent law used.
! icetem Element number that needs to be checked for creep convergence
! or, if negative, the number of elements that need to
! be checked. In the latter case the elements to check
! are stored in ielcp.
! mcreep Maximum nuber of iterations for explicit creep.
! jcreep Counter of number of iterations for explicit creep
! procedure. jcreep must be .le. mcreep
! icpa Pointer to constant in creep strain rate expression.
! icftmp Pointer to temperature dependent creep strain rate data.
! icfstr Pointer to equivalent stress dependent creep strain rate data.
! icfqcp Pointer to equivalent creep strain dependent creep strain
! rate data.
! icfcpm Pointer to equivalent creep strain rate dependent
! creep strain rate data.
! icrppr Permanent copy of icreep
! icrcha Control flag for creep convergence checking , if set to
! 1 then testing on absolute change in stress and creep
! strain, not relative testing. Input data.
! icpb Pointer to storage of material id cross reference numbers.
! iicpmt
! iicpa Pointer to constant in creep strain rate expression
!
! time_beg_lcase time at the beginning of the current load case
! time_beg_inc time at the beginning of the current increment
! fractol fraction of loadcase or increment time when we
! consider it to be finished
! time_beg_pst time corresponding to first increment to be
! read in from thermal post file for auto step
!
!***********************************************************************
!!$omp threadprivate(/marc_creeps/)
!!$omp threadprivate(/marc_creeps2/)
!!

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@ -1,63 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: creeps.cmn
!
! MSC.Marc include file
!
real(pReal) cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b
integer(pInt) icfte,icfst,icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,&
icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
real(pReal) time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
integer(pInt) num_creepsr,num_creepsi,num_creeps2r
parameter(num_creepsr=7)
parameter(num_creepsi=17)
parameter(num_creeps2r=4)
common/marc_creeps/cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b,icfte,icfst,&
icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
common/marc_creeps2/time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
! cptim Total time at begining of increment.
! timinc Incremental time for this step.
! icfte Local copy number of slopes of creep strain rate function
! versus temperature. Is -1 if exponent law used.
! icfst Local copy number of slopes of creep strain rate function
! versus equivalent stress. Is -1 if exponent law used.
! icfeq Local copy number of slopes of creep strain rate function
! versus equivalent strain. Is -1 if exponent law used.
! icftm Local copy number of slopes of creep strain rate function
! versus time. Is -1 if exponent law used.
! icetem Element number that needs to be checked for creep convergence
! or, if negative, the number of elements that need to
! be checked. In the latter case the elements to check
! are stored in ielcp.
! mcreep Maximum nuber of iterations for explicit creep.
! jcreep Counter of number of iterations for explicit creep
! procedure. jcreep must be .le. mcreep
! icpa Pointer to constant in creep strain rate expression.
! icftmp Pointer to temperature dependent creep strain rate data.
! icfstr Pointer to equivalent stress dependent creep strain rate data.
! icfqcp Pointer to equivalent creep strain dependent creep strain
! rate data.
! icfcpm Pointer to equivalent creep strain rate dependent
! creep strain rate data.
! icrppr Permanent copy of icreep
! icrcha Control flag for creep convergence checking , if set to
! 1 then testing on absolute change in stress and creep
! strain, not relative testing. Input data.
! icpb Pointer to storage of material id cross reference numbers.
! iicpmt
! iicpa Pointer to constant in creep strain rate expression
!
! time_beg_lcase time at the beginning of the current load case
! time_beg_inc time at the beginning of the current increment
! fractol fraction of loadcase or increment time when we
! consider it to be finished
! time_beg_pst time corresponding to first increment to be
! read in from thermal post file for auto step
!
!***********************************************************************
!!$omp threadprivate(/marc_creeps/)
!!$omp threadprivate(/marc_creeps2/)
!!

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@ -1,63 +0,0 @@
! common block definition file taken from respective MSC.Marc release and reformated to free format
!***********************************************************************
!
! File: creeps.cmn
!
! MSC.Marc include file
!
real(pReal) cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b
integer(pInt) icfte,icfst,icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,&
icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
real(pReal) time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
integer(pInt) num_creepsr,num_creepsi,num_creeps2r
parameter(num_creepsr=7)
parameter(num_creepsi=17)
parameter(num_creeps2r=4)
common/marc_creeps/cptim,timinc,timinc_p,timinc_s,timincm,timinc_a,timinc_b,icfte,icfst,&
icfeq,icftm,icetem,mcreep,jcreep,icpa,icftmp,icfstr,icfqcp,icfcpm,icrppr,icrcha,icpb,iicpmt,iicpa
common/marc_creeps2/time_beg_lcase,time_beg_inc,fractol,time_beg_pst
!
! cptim Total time at begining of increment.
! timinc Incremental time for this step.
! icfte Local copy number of slopes of creep strain rate function
! versus temperature. Is -1 if exponent law used.
! icfst Local copy number of slopes of creep strain rate function
! versus equivalent stress. Is -1 if exponent law used.
! icfeq Local copy number of slopes of creep strain rate function
! versus equivalent strain. Is -1 if exponent law used.
! icftm Local copy number of slopes of creep strain rate function
! versus time. Is -1 if exponent law used.
! icetem Element number that needs to be checked for creep convergence
! or, if negative, the number of elements that need to
! be checked. In the latter case the elements to check
! are stored in ielcp.
! mcreep Maximum nuber of iterations for explicit creep.
! jcreep Counter of number of iterations for explicit creep
! procedure. jcreep must be .le. mcreep
! icpa Pointer to constant in creep strain rate expression.
! icftmp Pointer to temperature dependent creep strain rate data.
! icfstr Pointer to equivalent stress dependent creep strain rate data.
! icfqcp Pointer to equivalent creep strain dependent creep strain
! rate data.
! icfcpm Pointer to equivalent creep strain rate dependent
! creep strain rate data.
! icrppr Permanent copy of icreep
! icrcha Control flag for creep convergence checking , if set to
! 1 then testing on absolute change in stress and creep
! strain, not relative testing. Input data.
! icpb Pointer to storage of material id cross reference numbers.
! iicpmt
! iicpa Pointer to constant in creep strain rate expression
!
! time_beg_lcase time at the beginning of the current load case
! time_beg_inc time at the beginning of the current increment
! fractol fraction of loadcase or increment time when we
! consider it to be finished
! time_beg_pst time corresponding to first increment to be
! read in from thermal post file for auto step
!
!***********************************************************************
!!$omp threadprivate(/marc_creeps/)
!!$omp threadprivate(/marc_creeps2/)
!!

View File

@ -25,4 +25,4 @@ class Abaqus(Solver):
detectedVersion = process.stdout.readlines()[1].split()[1]
if self.version != detectedVersion:
raise Exception('found Abaqus version %s, but requested %s'%(detectedVersion,self.version))
return '%s -job %s -user %s/src/DAMASK_abaqus_std interactive'%(cmd,model,env.rootDir())
return '%s -job %s -user %s/src/DAMASK_abaqus interactive'%(cmd,model,env.rootDir())

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@ -1,298 +0,0 @@
!--------------------------------------------------------------------------------------------------
!> @author Philip Eisenlohr, Max-Planck-Institut für Eisenforschung GmbH
!> @author Franz Roters, Max-Planck-Institut für Eisenforschung GmbH
!> @author Koen Janssens, Paul Scherrer Institut
!> @author Arun Prakash, Fraunhofer IWM
!> @brief interfaces DAMASK with Abaqus/Explicit
!> @details put the included file abaqus_v6.env in either your home or model directory,
!> it is a minimum Abaqus environment file containing all changes necessary to use the
!> DAMASK subroutine (see Abaqus documentation for more information on the use of abaqus_v6.env)
!--------------------------------------------------------------------------------------------------
#ifndef INT
#define INT 4
#endif
#ifndef FLOAT
#define FLOAT 8
#endif
#define Abaqus
#include "prec.f90"
module DAMASK_interface
implicit none
character(len=4), dimension(2), parameter :: INPUTFILEEXTENSION = ['.pes','.inp']
character(len=4), parameter :: LOGFILEEXTENSION = '.log'
contains
!--------------------------------------------------------------------------------------------------
!> @brief just reporting
!--------------------------------------------------------------------------------------------------
subroutine DAMASK_interface_init
integer, dimension(8) :: &
dateAndTime ! type default integer
call date_and_time(values = dateAndTime)
write(6,'(/,a)') ' <<<+- DAMASK_abaqus_exp -+>>>'
write(6,'(/,a)') ' Roters et al., Computational Materials Science, 2018'
write(6,'(/,a)') ' Version: '//DAMASKVERSION
write(6,'(a,2(i2.2,a),i4.4)') ' Date: ',dateAndTime(3),'/',&
dateAndTime(2),'/',&
dateAndTime(1)
write(6,'(a,2(i2.2,a),i2.2)') ' Time: ',dateAndTime(5),':',&
dateAndTime(6),':',&
dateAndTime(7)
write(6,'(/,a)') ' <<<+- DAMASK_interface init -+>>>'
#include "compilation_info.f90"
end subroutine DAMASK_interface_init
!--------------------------------------------------------------------------------------------------
!> @brief using Abaqus/Explicit function to get working directory name
!--------------------------------------------------------------------------------------------------
character(1024) function getSolverWorkingDirectoryName()
implicit none
integer :: lenOutDir
getSolverWorkingDirectoryName=''
call vgetOutDir(getSolverWorkingDirectoryName, lenOutDir)
getSolverWorkingDirectoryName=trim(getSolverWorkingDirectoryName)//'/'
end function getSolverWorkingDirectoryName
!--------------------------------------------------------------------------------------------------
!> @brief using Abaqus/Explicit function to get solver job name
!--------------------------------------------------------------------------------------------------
character(1024) function getSolverJobName()
implicit none
integer :: lenJobName
getSolverJobName=''
call vGetJobName(getSolverJobName, lenJobName)
end function getSolverJobName
end module DAMASK_interface
#include "commercialFEM_fileList.f90"
subroutine vumat(nBlock, nDir, nshr, nStateV, nFieldV, nProps, lAnneal, &
stepTime, totalTime, dt, cmName, coordMp, charLength, &
props, density, strainInc, relSpinInc, &
tempOld, stretchOld, defgradOld, fieldOld, &
stressOld, stateOld, enerInternOld, enerInelasOld, &
tempNew, stretchNew, defgradNew, fieldNew, &
stressNew, stateNew, enerInternNew, enerInelasNew)
use prec, only: &
pReal, &
pInt
!$ use numerics, only: &
!$ DAMASK_NumThreadsInt
use FEsolving, only: &
symmetricSolver, &
terminallyIll
use math, only: &
invnrmMandel
use debug, only: &
debug_info, &
debug_reset, &
debug_levelBasic, &
debug_level, &
debug_abaqus
use mesh, only: &
mesh_unitlength, &
mesh_FEasCP, &
mesh_ipCoordinates
use CPFEM, only: &
CPFEM_general, &
CPFEM_init_done, &
CPFEM_initAll, &
CPFEM_CALCRESULTS, &
CPFEM_AGERESULTS, &
cycleCounter, &
theTime, &
outdatedByNewInc, &
outdatedFFN1
use homogenization, only: &
materialpoint_sizeResults, &
materialpoint_results
implicit none
integer(pInt), intent(in) :: &
nDir, & !< number of direct components in a symmetric tensor
nshr, & !< number of indirect components in a symmetric tensor
nStateV, & !< number of user-defined state variables that are associated with this material type
nFieldV, & !< number of user-defined external field variables
nprops, & !< user-specified number of user-defined material properties
lAnneal !< indicating whether the routine is being called during an annealing process
integer(pInt), dimension(*), intent(in) :: &
nBlock !< 1: No of Materialpoints in this call, 2: No of Materialpoint (IP)
!< 3: No of layer, 4: No of secPoint, 5+: element numbers
character(len=80), intent(in) :: &
cmname !< uses-specified material name, left justified
real(pReal), dimension(nprops), intent(in) :: &
props !< user-supplied material properties
real(pReal), intent(in) :: &
stepTime, & !< value of time since the step began
totalTime, & !< value of total time
dt !< time increment size
real(pReal), dimension(nblock(1)), intent(in) :: &
density, & !< current density at material points in the midstep configuration
charLength, & !< characteristic element length
enerInternOld, & !< internal energy per unit mass at each material point at the beginning of the increment
enerInelasOld, & !< dissipated inelastic energy per unit mass at each material point at the beginning of the increment
tempOld, & !< temperature at each material point at the beginning of the increment
tempNew !< temperature at each material point at the end of the increment (Temperature calculated in ABAQUS boundary conditions)
real(pReal), dimension(nblock(1),*), intent(in) :: &
coordMp !< material point coordinates
real(pReal), dimension(nblock(1),ndir+nshr), intent(in) :: &
strainInc, & !< strain increment tensor at each material point
stretchOld, & !< stretch tensor U at each material point
stretchNew, & !< stretch tensor U at each material point
stressOld !< stress tensor at each material point
real(pReal), dimension(nblock(1),nshr), intent(in) :: &
relSpinInc !< incremental relative rotation vector
real(pReal), dimension(nblock(1),nstatev), intent(in) :: &
stateOld !< state variables at each material point at the beginning of the increment
real(pReal), dimension(nblock(1),nfieldv), intent(in) :: &
fieldOld, & !< user-defined field variables
fieldNew !< user-defined field variables
real(pReal), dimension(nblock(1),ndir+2*nshr), intent(in) :: &
defgradOld, &
defgradNew
real(pReal), dimension(nblock(1)), intent(out) :: &
enerInternNew, & !< internal energy per unit mass at each material point at the end of the increment
enerInelasNew !< dissipated inelastic energy per unit mass at each material point at the end of the increment
real(pReal), dimension(nblock(1),ndir+nshr), intent(out) :: &
stressNew !< stress tensor at each material point at the end of the increment
real(pReal), dimension(nblock(1),nstatev), intent(out) :: &
stateNew !< state variables at each material point at the end of the increment
real(pReal), dimension(3) :: coordinates
real(pReal), dimension(3,3) :: defgrd0,defgrd1
real(pReal), dimension(6) :: stress
real(pReal), dimension(6,6) :: ddsdde
real(pReal) :: temp, timeInc, stresspower
integer(pInt) :: computationMode, n, i, cp_en
#ifdef _OPENMP
integer :: defaultNumThreadsInt !< default value set by Abaqus
include "omp_lib.h"
defaultNumThreadsInt = omp_get_num_threads() ! remember number of threads set by Marc
call omp_set_num_threads(DAMASK_NumThreadsInt) ! set number of threads for parallel execution set by DAMASK_NUM_THREADS
#endif
computationMode = CPFEM_CALCRESULTS ! always calculate
do n = 1,nblock(1) ! loop over vector of IPs
temp = tempOld(n) ! temp is intent(in)
if ( .not. CPFEM_init_done ) then
call CPFEM_initAll(nBlock(4_pInt+n),nBlock(2))
outdatedByNewInc = .false.
if (iand(debug_level(debug_abaqus),debug_levelBasic) /= 0) then
write(6,'(i8,1x,i2,1x,a)') nBlock(4_pInt+n),nBlock(2),'first call special case..!'; flush(6)
endif
else if (theTime < totalTime) then ! reached convergence
outdatedByNewInc = .true.
if (iand(debug_level(debug_abaqus),debug_levelBasic) /= 0) then
write (6,'(i8,1x,i2,1x,a)') nBlock(4_pInt+n),nBlock(2),'lastIncConverged + outdated'; flush(6)
endif
endif
outdatedFFN1 = .false.
terminallyIll = .false.
cycleCounter = 1_pInt
if ( outdatedByNewInc ) then
outdatedByNewInc = .false.
call debug_info() ! first after new inc reports debugging
call debug_reset() ! resets debugging
computationMode = ior(computationMode, CPFEM_AGERESULTS) ! age results
endif
theTime = totalTime ! record current starting time
if (iand(debug_level(debug_abaqus),debug_levelBasic) /= 0) then
write(6,'(a,i8,i2,a)') '(',nBlock(4_pInt+n),nBlock(2),')'; flush(6)
write(6,'(a,l1)') 'Aging Results: ', iand(computationMode, CPFEM_AGERESULTS) /= 0_pInt
endif
defgrd0 = 0.0_pReal
defgrd1 = 0.0_pReal
timeInc = dt
! ABAQUS explicit: deformation gradient as vector 11, 22, 33, 12, 23, 31, 21, 32, 13
! ABAQUS explicit: deformation gradient as vector 11, 22, 33, 12, 21
forall (i=1:ndir)
defgrd0(i,i) = defgradOld(n,i)
defgrd1(i,i) = defgradNew(n,i)
end forall
if (nshr == 1) then
defgrd0(1,2) = defgradOld(n,4)
defgrd1(1,2) = defgradNew(n,4)
defgrd0(2,1) = defgradOld(n,5)
defgrd1(2,1) = defgradNew(n,5)
else
defgrd0(1,2) = defgradOld(n,4)
defgrd1(1,2) = defgradNew(n,4)
defgrd0(1,3) = defgradOld(n,9)
defgrd1(1,3) = defgradNew(n,9)
defgrd0(2,1) = defgradOld(n,7)
defgrd1(2,1) = defgradNew(n,7)
defgrd0(2,3) = defgradOld(n,5)
defgrd1(2,3) = defgradNew(n,5)
defgrd0(3,1) = defgradOld(n,6)
defgrd1(3,1) = defgradNew(n,6)
defgrd0(3,2) = defgradOld(n,8)
defgrd1(3,2) = defgradNew(n,8)
endif
cp_en = mesh_FEasCP('elem',nBlock(4_pInt+n))
mesh_ipCoordinates(1:3,nblock(2),cp_en) = mesh_unitlength * coordMp(n,1:3)
call CPFEM_general(computationMode,.false.,defgrd0,defgrd1,temp,timeInc,cp_en,nBlock(2),stress,ddsdde)
! Mandel: 11, 22, 33, SQRT(2)*12, SQRT(2)*23, SQRT(2)*13
! straight: 11, 22, 33, 12, 23, 13
! ABAQUS implicit: 11, 22, 33, 12, 13, 23
! ABAQUS explicit: 11, 22, 33, 12, 23, 13
! ABAQUS explicit: 11, 22, 33, 12
stressNew(n,1:ndir+nshr) = stress(1:ndir+nshr)*invnrmMandel(1:ndir+nshr)
stateNew(n,1:min(nstatev,materialpoint_sizeResults)) = &
materialpoint_results(1:min(nstatev,materialpoint_sizeResults),&
nBlock(2),mesh_FEasCP('elem', nBlock(4_pInt+n)))
stresspower = 0.5_pReal*sum((stressOld(n,1:ndir)+stressNew(n,1:ndir))*straininc(n,1:ndir))+&
sum((stressOld(n,ndir+1:ndir+nshr)+stressNew(n,ndir+1:ndir+nshr))*straininc(n,ndir+1:ndir+nshr))
enerInternNew(n) = enerInternOld(n) + stresspower / density(n) ! Internal energy per unit mass
enerInelasNew(n) = enerInternNew(n) ! Dissipated inelastic energy per unit mass(Temporary output)
enddo
!$ call omp_set_num_threads(defaultNumThreadsInt) ! reset number of threads to stored default value
end subroutine vumat
!--------------------------------------------------------------------------------------------------
!> @brief calls the exit function of Abaqus/Explicit
!--------------------------------------------------------------------------------------------------
subroutine quit(mpie_error)
use prec, only: &
pInt
implicit none
integer(pInt) :: mpie_error
flush(6)
call xplb_exit
end subroutine quit