more cleaning of old commercial FEM solver files
This commit is contained in:
Martin Diehl
parent
2a33dcdd04
commit
ce32372f1c
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@ -424,20 +424,11 @@ SpectralRuntime:
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- release
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- release
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###################################################################################################
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###################################################################################################
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AbaqusExp:
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stage: createDocumentation
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script:
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- module load $IntelCompiler $MPICH_Intel $PETSc_MPICH_Intel $Doxygen
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- $DAMASKROOT/PRIVATE/documenting/runDoxygen.sh $DAMASKROOT abaqus_exp
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except:
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- master
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- release
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AbaqusStd:
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AbaqusStd:
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stage: createDocumentation
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stage: createDocumentation
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script:
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script:
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- module load $IntelCompiler $MPICH_Intel $PETSc_MPICH_Intel $Doxygen
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- module load $IntelCompiler $MPICH_Intel $PETSc_MPICH_Intel $Doxygen
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- $DAMASKROOT/PRIVATE/documenting/runDoxygen.sh $DAMASKROOT abaqus_std
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- $DAMASKROOT/PRIVATE/documenting/runDoxygen.sh $DAMASKROOT abaqus
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except:
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except:
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- master
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- master
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- release
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- release
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2
PRIVATE
2
PRIVATE
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@ -1 +1 @@
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Subproject commit 6c43b54ecd4a3a5b3ec8771514ef2c7c839a31e7
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Subproject commit 1581e8e53910725bac354f5e6f5af1a6914a0a59
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@ -1,205 +0,0 @@
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! common block definition file taken from respective MSC.Marc release and reformated to free format
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!***********************************************************************
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!
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! File: concom.cmn
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!
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! MSC.Marc include file
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!
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integer(pInt) &
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iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
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ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
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ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
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ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
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itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
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lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
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icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
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isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
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ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
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ncycnt, marmen , idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
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ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
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imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
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kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
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iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
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ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush, istream_input,&
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iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
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iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout, igena_meth,&
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magf_meth, non_assumed, iredoboudry
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integer(pInt) num_concom
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parameter(num_concom=232)
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common/marc_concom/&
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iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva(60), idyn, idynt,&
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ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
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ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
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ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
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itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
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lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
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icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
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isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
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ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
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ncycnt, marmen, idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
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ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
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imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
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kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
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iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
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ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush , istream_input,&
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iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
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iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout,igena_meth,&
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magf_meth, non_assumed, iredoboudry
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!
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! comments of variables:
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!
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! ideva(60) - debug print out flag
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! 1 print element stiffness matrices, mass matrix
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! 2 output matrices used in tying
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! 3 force the solution of a nonpositive definite matrix
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! 4 print info of connections to each node
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! 5 info of gap convergence, internal heat generated, contact
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! touching and separation
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! 6 nodal value array during rezoning
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! 7 tying info in CONRAD GAP option, fluid element numbers in
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! CHANNEL option
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! 8 output incremental displacements in local coord. system
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! 9 latent heat output
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! 10 stress-strain in local coord. system
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! 11 additional info on interlaminar stress
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! 12 output right hand side and solution vector
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! 13 info of CPU resources used and memory available on NT
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! 14 info of mesh adaption process, 2D outline information
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! info of penetration checking for remeshing
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! save .fem files after afmesh3d meshing
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! 15 surface energy balance flag
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! 16 print info regarding pyrolysis
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! 17 print info of "streamline topology"
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! 18 print mesh data changes after remeshing
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! 19 print material flow stress data read in from *.mat file
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! if unit flag is on, print out flow stress after conversion
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! 20 print information on table input
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! 21 print out information regarding kinematic boundary conditions
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! 22 print out information regarding dist loads, point loads, film
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! and foundations
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! 23 print out information about automatic domain decomposition
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! 24 print out iteration information in SuperForm status report file
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! 25 print out information for ablation
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! 26 print out information for films - Table input
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! 27 print out the tying forces
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! 28 print out for CASI solver, convection,
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! 29 DDM single file debug printout
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! 30 print out cavity debug info
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! 31 print out welding related info
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! 32 prints categorized DDM memory usage
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! 33 print out the cutting info regarding machining feature
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! 34 print out the list of quantities which can be defined via a table
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! and for each quantity the supported independent variables
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! 35 print out detailed coupling region info
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! 36 print out solver debug info level 1 (Least Detailed)
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! 37 print out solver debug info level 1 (Medium Detailed)
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! 38 print out solver debug info level 1 (Very Detailed)
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! 39 print detailed memory allocation info
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! 40 print out marc-adams debug info
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! 41 output rezone mapping post file for debugging
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! 42 output post file after calling oprofos() for debugging
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! 43 debug printout for vcct
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! 44 debug printout for progressive failure
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! 45 print out automatically generated midside node coordinates (arecrd)
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! 46 print out message about routine and location, where the ibort is raised (ibort_inc)
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! 47 print out summary message of element variables on a
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! group-basis after all the automatic changes have been
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! made (em_ellibp)
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! 48 Automatically generate check results based on max and min vals.
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! These vals are stored in the checkr file, which is inserted
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! into the *dat file by the generate_check_results script from /marc/tools
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! 49 Automatically generate check results based on the real calculated values
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! at the sppecified check result locations.
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! These vals are stored in the checkr file, which is inserted
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! into the *dat file by the update_check_results script from /marc/tools
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! 50 generate a file containing the resistance or capacity matrix;
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! this file can be used to compare results with a reference file
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! 51 print out detailed information for segment-to-segment contact
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! 52 print out detailed relative displacement information
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! for uniaxial sliding contact
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! 53 print out detailed sliding direction information for
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! uniaxial sliding contact
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! 54 print out detailed information for edges attached to a curve
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!
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!
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! irpflo global flag for rigid plastic flow analysis
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! = 1 eularian formulation
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! = 2 regular formulation; rigid material present in the analysis
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!
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! jactch = 1 or 2 if elements are activated or deactivated
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! = 3 if elements are adaptively remeshed or rezoned
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! = 0 normally / reset to 0 when assembly is done
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! ifricsh = 0 call to fricsh in otest not needed
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! = 1 call to fricsh (nodal friction) in otest needed
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! iremkin = 0 remove deactivated kinematic boundary conditions
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! immediately - only in new input format (this is default)
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! = 1 remove deactivated kinematic boundary conditions
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! gradually - only in new input format
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! iremfor = 0 remove force boundary conditions immediately -
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! only in new input format (this is default)
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! = 1 remove force boundary conditions gradually -
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! only in new input format (this is default)
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! ishearp set to 1 if shear panel elements are present in the model
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!
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! jspf = 0 not in spf loadcase
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! > 0 in spf loadcase (jspf=1 during first increment)
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! machining = 1 if the metal cutting feature is used, for memory allocation purpose
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! = 0 (default) if no metal cutting feature required
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!
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! jlshell = 1 if there is a shell element in the mesh
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! icompsol = 1 if there is a composite solid element in the mesh
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! iupblgfo = 1 if follower force for point loads
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! jcondir = 1 if contact priority option is used
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! nstcrp = 0 (default) steady state creep flag (undocumented feature.
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! if not 0, turns off special ncycle = 0 code in radial.f)
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! nactive = number of active passes, if =1 then it's not a coupled analysis
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! ipassref = reference ipass, if not in a multiphysics pass ipass=ipassref
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! icheckmpc = value of mpc-check parameter option
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! noline = set to 1 in osolty if no line seacrh should be done in ogetst
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! icuring = set to 1 if the curing is included for the heat transfer analysis.
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! ishrink = set to 1 if shrinkage strain is included for mechancial analysis.
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! ioffsflg = 1 for small displacement beam/shell offsets
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! = 2 for large displacement beam/shell offsets
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! isetoff = 0 - do not apply beam/shell offsets
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! = 1 - apply beam/shell offsets
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! ioffsetm = min. value of offset flag
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! inc_incdat = flag to record increment number of a new loadcase in incdat.f
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! iautspc = flag for AutoSPC option
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! ibrake = brake squeal in this increment
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! icbush = set to 1 if cbush elements present in model
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! istream_input = set to 1 for streaming input calling Marc as library
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! iprsinp = set to 1 if pressure input, introduced so other variables
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! such as h could be a function of pressure
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! ivlsinp = set to 1 if velocity input, introduced so other variables
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! such as h could be a function of velocity
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! ipin_m = # of beam element with PIN flag
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! jgnstr_glb = global control over pre or fast integrated composite shells
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! imarc_return = Marc return flag for streaming input control
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! iqvcimp = if non-zero, then the number of QVECT boundary conditions
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! nqvceid = number of QVECT boundary conditions, where emisivity/absorbtion id entered
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! istpnx = 1 if to stop at end of increment
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! imicro1 = 1 if micro1 interface is used
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! iaxisymm = set to 1 if axisymmetric analysis
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! jbreakglue = set to 1 if breaking glued option is used
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! iglstif = 1 if ddm and global stiffness matrix formed (sgi solver 6 or solver9)
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! jfastasm = 1 do fast assembly using SuperForm code
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! iwear = set to 1 if wear model, set to 2 if wear model and coordinates updated
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! iwearcf = set to 1 to store nodal coefficient of friction for wear calculation
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! imixmeth = set=1 then use nonlinear mixture material - allocate memory
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! ielcmadyn = flag for magnetodynamics
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! 0 - electromagnetics using newmark beta
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! 1 - transient magnetics using backward euler
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! idinout = flag to control if inside out elements should be deactivated
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! igena_meth = 0 - generalized alpha parameters depend on whether or not contact
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! is flagged (dynamic,7)
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! 10 - generalized alpha parameters are optimized for a contact
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! analysis (dynamic,8)
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! 11 - generalized alpha parameters are optimized for an analysis
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! without contact (dynamic,8)
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! magf_meth = - Method to compute force in magnetostatic - structural
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! = 1 - Virtual work method
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! = 2 - Maxwell stress tensor
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! non_assumed = 1 no assumed strain formulation (forced)
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! iredoboudry set to 1 if contact boundary needs to be recalculated
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!
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!***********************************************************************
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@ -1,206 +0,0 @@
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! common block definition file taken from respective MSC.Marc release and reformated to free format
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!***********************************************************************
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!
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! File: concom.cmn
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!
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! MSC.Marc include file
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!
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integer(pInt) &
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iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva, idyn, idynt,&
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ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
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ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
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ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
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itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
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lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
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icrpim, iradrt, ipshft, itshr, iangin, iupmdr, iconjf, jincfl, jpermg, jhour,&
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isolvr, jritz, jtable, jshell, jdoubl, jform, jcentr, imini, kautth, iautof,&
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ibukty, iassum, icnstd, icnstt, kmakmas, imethvp, iradrte, iradrtp, iupdate, iupdatp,&
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ncycnt, marmen , idynme, ihavca, ispf, kmini, imixex, largtt, kdoela, iautofg,&
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ipshftp, idntrc, ipore, jtablm, jtablc, isnecma, itrnspo, imsdif, jtrnspo, mcnear,&
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imech, imecht, ielcmat, ielectt, magnett, imsdift, noplas, jtabls, jactch, jtablth,&
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kgmsto , jpzo, ifricsh, iremkin, iremfor, ishearp, jspf, machining, jlshell, icompsol,&
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iupblgfo, jcondir, nstcrp, nactive, ipassref, nstspnt, ibeart, icheckmpc, noline, icuring,&
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ishrink, ioffsflg, isetoff, ioffsetm,iharmt, inc_incdat, iautspc, ibrake, icbush, istream_input,&
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iprsinp, ivlsinp, ifirst_time,ipin_m, jgnstr_glb, imarc_return,iqvcinp, nqvceid, istpnx, imicro1,&
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iaxisymm, jbreakglue,iglstif, jfastasm,iwear, iwearcf, imixmeth, ielcmadyn, idinout, igena_meth,&
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magf_meth, non_assumed, iredoboudry, ioffsz0
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integer(pInt) num_concom
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parameter(num_concom=233)
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common/marc_concom/&
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iacous, iasmbl, iautth, ibear, icompl, iconj, icreep, ideva(60), idyn, idynt,&
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||||||
ielas, ielcma, ielect, iform, ifour, iharm, ihcps, iheat, iheatt, ihresp,&
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ijoule, ilem, ilnmom, iloren, inc, incext, incsub, ipass, iplres, ipois,&
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ipoist, irpflo, ismall, ismalt, isoil, ispect, ispnow, istore, iswep, ithcrp,&
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itherm, iupblg, iupdat, jacflg, jel, jparks, largst, lfond, loadup, loaduq,&
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lodcor, lovl, lsub, magnet, ncycle, newtnt, newton, noshr, linear, ivscpl,&
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|
||||||
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
|
|
||||||
!
|
|
||||||
!***********************************************************************
|
|
||||||
|
|
@ -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
|
|
||||||
!
|
|
||||||
!***********************************************************************
|
|
||||||
|
|
@ -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/)
|
|
||||||
!!
|
|
||||||
|
|
@ -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/)
|
|
||||||
!!
|
|
||||||
|
|
@ -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/)
|
|
||||||
!!
|
|
||||||
|
|
@ -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/)
|
|
||||||
!!
|
|
||||||
|
|
@ -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
|
|
||||||
!
|
|
||||||
!***********************************************************************
|
|
||||||
|
|
@ -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
|
|
||||||
!
|
|
||||||
!***********************************************************************
|
|
||||||
|
|
@ -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
|
|
||||||
!
|
|
||||||
!***********************************************************************
|
|
||||||
|
|
@ -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/)
|
|
||||||
!!
|
|
||||||
|
|
@ -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/)
|
|
||||||
!!
|
|
||||||
|
|
@ -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/)
|
|
||||||
!!
|
|
||||||
|
|
@ -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/)
|
|
||||||
!!
|
|
||||||
|
|
@ -25,4 +25,4 @@ class Abaqus(Solver):
|
||||||
detectedVersion = process.stdout.readlines()[1].split()[1]
|
detectedVersion = process.stdout.readlines()[1].split()[1]
|
||||||
if self.version != detectedVersion:
|
if self.version != detectedVersion:
|
||||||
raise Exception('found Abaqus version %s, but requested %s'%(detectedVersion,self.version))
|
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())
|
||||||
|
|
|
||||||
|
|
@ -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
|
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||||||
! 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
|
|
||||||
Loading…
Reference in New Issue