474 lines
29 KiB
Groff
474 lines
29 KiB
Groff
! 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 &
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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,icomplt, mesh_dual, iactrp, mgnewton, iusedens,igsigd0,&
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iaem, icosim, inodels, nlharm, iampini, iphasetr, inonlcl, inonlct, iforminp,ispecerror,&
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icsprg, imol, imolt, idatafit,iharmpar, inclcase, imultifreq,init_elas, ifatig, iftgmat,&
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nchybrid, ibuckle, iexpande, matfor, ishormem, imsdifths
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dimension :: ideva(60)
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integer num_concom
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parameter(num_concom=266)
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common/marc_concom/&
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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,icomplt, mesh_dual, iactrp, mgnewton, iusedens,igsigd0,&
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iaem, icosim, inodels, nlharm, iampini, iphasetr, inonlcl, inonlct, iforminp,ispecerror,&
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icsprg, imol, imolt, idatafit,iharmpar, inclcase, imultifreq,init_elas, ifatig, iftgmat,&
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nchybrid, ibuckle, iexpande, matfor, ishormem, imsdifths
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!
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! comments of variables:
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!
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! iacous Control flag for acoustic analysis. Input data.
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! iacous=1 modal acoustic analysis.
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! iacous=2 harmonic acoustic-structural analysis.
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! iasmbl Control flag to indicate that operator matrix should be
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! recalculated.
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! iautth Control flag for AUTO THERM option.
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! ibear Control flag for bearing analysis. Input data.
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! icompl Control variable to indicate that a complex analysis is
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! being performed. Either a Harmonic analysis with damping,
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! or a harmonic electro-magnetic analysis. Input data.
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! iconj Flag for EBE conjugate gradient solver (=solver 1, retired)
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! Also used for VKI iterative solver.
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! icreep Control flag for creep analysis. Input data.
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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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! print local adaptivity info
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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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! 55 print information related to viscoelasticity calculations
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! 56 print out detailed information for element coloring for multithreading
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! 57 print out extra overheads due to multi-threading.
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! These overhead includes (i) time and (ii) memory.
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! The memory report will be summed over all the children.
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! 58 debug output for ELSTO usage
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! 59 print out contact body forces and nodes in contact
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!
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! idyn Control flag for dynamics. Input data.
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! 1 = eigenvalue extraction and / or modal superposition
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! 2 = Newmark Beta and Single Step Houbolt (ssh with idynme=1)
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! 3 = Houbolt
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! 4 = Central difference
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! 5 = Newer central difference
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! idynt Copy of idyn at begining of increment
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! ielas Control flag for ELASTIC analysis. Input data.
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! Set by user or automatically turned on by Fourier option.
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! Implies that each load case is treated separately.
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! In Adaptive meshing analysis , forces re-analysis until
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! convergence obtained.
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! Also seriously misused to indicate no convergence.
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! = 1 elastic option with fourier analysis
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! = 2 elastic option without fourier analysis
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! =-1 no convergence in recycles or max # increments reached
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! Set to 1 if ELASTIC or SUBSTRUC parameter cards are used,
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! or if fourier option is used.
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! Then set to 2 if not fourier analysis.
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! ielcma Control flag for electromagnetic analysis. Input data.
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! ielcma = 1 Harmonic formulation
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! ielcma = 2 Transient formulation
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! ielect Control flag for electrostatic option. Input data.
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! iform Control flag indicating that contact will be performed.
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! ifour Control flag for Fourier analysis.
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! 0 = Odd and even terms.
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! 1 = symmetric (cosine) terms
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! 2 = antisymmetric (sine) terms.
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! iharm Control flag to indicate that a harmonic analysis will
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! be performed. May change between passes.
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! ihcps Control flag for coupled thermal - stress analysis.
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! iheat Control flag for heat transfer analysis. Input data.
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! iheatt Permanent control flag for heat transfer analysis.
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! Note in coupled analysis iheatt will remain as one,
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! but iheat will be zero in stress pass.
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! ihresp Control flag to indicate to perform a harmonic subincrement.
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! ijoule Control flag for Joule heating.
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! ilem Control flag to determin which vector is to be transformed.
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! Control flag to see where one is:
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! ilem = 1 - elem.f
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! ilem = 2 - initst.f
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! ilem = 3 - pressr.f
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! ilem = 3 - fstif.f
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! ilem = 4 - jflux.f
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! ilem = 4 - strass.f
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! ilem = 5 - mass.f
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! ilem = 5 - osolty.f
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! ilnmom Control flag for soil - pore pressure calculation. Input data.
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! ilnmom = 0 - perform only pore pressure calculation.
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! = 1 - couples pore pressure - displacement analysis
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! iloren Control flag for DeLorenzi J-Integral evaluation. Input data.
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! inc Increment number.
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! incext Control flag indicating that currently working on a
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! subincrement.
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! Could be due to harmonics , damping component (bearing),
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! stiffness component (bearing), auto therm creep or
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! old viscoplaticity
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! incsub Sub-increment number.
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! inonlcl control flag for nonlocal pass
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! inonlct permanent control flag for nonlocal pass
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! ipass Control flag for which part of coupled analysis.
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! ipass = -1 - reset to base values
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! ipass = 0 - do nothing
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! ipass = 1 - stress part
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! ipass = 2 - heat transfer part
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! 3 - fluid pass
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! 4 - joule heating pass
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! 5 - pore pressure pass
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! 6 - electrostatic pass
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! 7 - magnetostatic pass
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! 8 - electromagnetic pass
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! 9 - diffusion pass
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! ipass = 10 - nonlocal part
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! iplres Flag indicating that either second matrix is stored.
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! dynamic analysis - mass matrix
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! heat transfer - specific heat matrix
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! buckle - initial stress stiffness
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! ipois Control flag indicating Poisson type analysis
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! ipois = 1 for heat transfer
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! = 1 for heat transfer part of coupled
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! = 1 for bearing
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! = 1 for electrostatic
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! = 1 for magnetostatic
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! = 1 for nonlocal part
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! ipoist Permanent copy of ipois. In coupled analysis , ipois = 0
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! in stress portion, yet ipoist will still =1.
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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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! ismall control flag to indicate small displacement analysis. input data.
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! ismall = 0 - large disp included.
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! ismall = 1 - small displacement.
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! the flag is changing between passes.
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! ismalt permanent copy of ismall . in heat transfer portion of
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! coupled analysis ismall =0 , but ismalt remains the same.
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! isoil control flag indicating that soil / pore pressure
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! calculation . input data.
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! ispect control flag for response spectrum calculation. input data.
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! ispnow control flag to indicate to perform a spectrum response
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! calculation now.
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! istore store stresses flag.
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! istore = 0 in elem.f and if first pass of creep
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! convergence checking in ogetst.f
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! or harmonic analysis or thruc.f if not
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! converged.
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! iswep control flag for eigenvalue analysis.
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! iswep=1 - go do extraction process
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! ithcrp control flag for auto therm creep option. input data.
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! itherm control flag for either temperature dependent material
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! properties and/or thermal loads.
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! iupblg control flag for follower force option. input data.
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! iupdat control flag for update lagrange option for current element.
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! jacflg control flag for lanczos iteration method. input data.
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! jel control flag indicating that total load applied in
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! increment, ignore previous solution.
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! jel = 1 in increment 0
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! = 1 if elastic or fourier
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! = 1 in subincrements with elastic and adaptive
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! jparks control flag for j integral by parks method. input data.
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! largst control flag for finite strain plasticity. input data.
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! lfond control variable that indicates if doing elastic
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! foundation or film calculation. influences whether
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! this is volumetric or surface integration.
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! loadup control flag that indicates that nonlinearity occurred
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! during previous increment.
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! loaduq control flag that indicates that nonlinearity occurred.
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! lodcor control flag for switching on the residual load correction.
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! notice in input stage lodcor=0 means no loadcor,
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! after omarc lodcor=1 means no loadcor
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! lovl control flag for determining which "overlay" is to
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! be called from ellib.
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! lovl = 1 omarc
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! = 2 oaread
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! = 3 opress
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! = 4 oasemb
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! = 5 osolty
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! = 6 ogetst
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! = 7 oscinc
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! = 8 odynam
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! = 9 opmesh
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! = 10 omesh2
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! = 11 osetz
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! = 12 oass
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! = 13 oincdt
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! = 14 oasmas
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! = 15 ofluas
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! = 16 ofluso
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! = 17 oshtra
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! = 18 ocass
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! = 19 osoltc
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! = 20 orezon
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! = 21 otest
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! = 22 oeigen
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! lsub control variable to determine which part of element
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! assembly function is being done.
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! lsub = 1 - no longer used
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! = 2 - beta*
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! = 3 - cons*
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! = 4 - ldef*
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! = 5 - posw*
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! = 6 - theta*
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! = 7 - tmarx*
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! = 8 - geom*
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! magnet control flag for magnetostatic analysis. input data.
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! ncycle cycle number. accumulated in osolty.f
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! note first time through oasemb.f , ncycle = 0.
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! newtnt control flag for permanent copy of newton.
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! newton iteration type. input data.
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! newton : = 1 full newton raphson
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! 2 modified newton raphson
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! 3 newton raphson with strain correct.
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! 4 direct substitution
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! 5 direct substitution followed by n.r.
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! 6 direct substitution with line search
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! 7 full newton raphson with secant initial stress
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! 8 secant method
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! 9 full newton raphson with line search
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! noshr control flag for calculation interlaminar shears for
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! elements 22,45, and 75. input data.
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!ees
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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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! iharmt = 1 global flag if a coupled analysis contains an harmonic pass
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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 based on finite difference for the force computation
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! = 2 - Maxwell stress tensor
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! = 3 - Virtual work method based on local derivative for the force computation
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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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! ioffsz0 = 1 if composite are used with reference position.ne.0
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! icomplt = 1 global flag if a coupled analysis contains an complex pass
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! mesh_dual = 1 two independent meshes are used in magnetodynamic/thermal/structural
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! one for magnetodynamic and the other for the remaining passes
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! iactrp = 1 in an analysis with global remeshing, include inactive
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! rigid bodies on post file
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! mgnewton = 1 Use full Newton Raphson iteration for magnetostatic pass
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!
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! iusedens > 0 if mass density is used in the analysis (dynamics, mass dependent loading)
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! igsigd0 = 1 set varselem(igsigd) to zero in next oasemb
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! iaem = 1 if marc is called from aem (0 - off - default)
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! icosim = 1 if marc is used in co-simulation analysis with ADAMS using the CosimEngine
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! = 2 if marc is used in co-simulation analysis with ADAMS using the ACSI interface
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! = 3 if marc is used in co-simulation analysis with scFLOW using the CosimEngine
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! = 4 if marc is used in co-simulation analysis with scFLOW and ADAMS using the CosimEngine
|
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! inodels = 1 nodal integration elements 239/240/241 present
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! nlharm = 0 harmonic subincrements are linear
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|
! = 1 harmonic subincrements are nonlinear
|
|
! iampini = 0 amplitude of previous harmonic subinc is initial estimate (default)
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|
! = 1 zero amplitude is initial estimate
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|
! iphasetr = 1 phase transformation material model is used
|
|
! iforminp flag indicating that contact is switched on via the CONTACT
|
|
! option in the input file (as opposed to the case that contact
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|
! is switched on internally due to cyclic symmetry or model
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|
! section creation)
|
|
! ispecerror = a+10*b (only for spectrum response analysis with missing mass option)
|
|
! a=0 or a=1 (modal shape with non-zero shift)
|
|
! b=0 or b=1 (recover with new assembly of stiffness matrix)
|
|
! icsprg = set to 1 if spring elements present in model
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|
! imol Control flag for molecualr diffusion pass
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|
! imolt Permanent control flag for molecualr diffusion pass
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|
! Note in coupled analysis imolt will remain as one,
|
|
! but imol will be zero in stress pass or thermal pass.
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|
! idatafit = run Marc to fit parameters
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|
! iharmpar = 1 if harmonic parameter option is used
|
|
! inclcase load case increment use for cyclic plasticity data fitting
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|
! imultifreq flag to indicate how many harmonic magnetodynamic passes are computed in coupled
|
|
! magnetodynamic/thermal(/structural) analyses.
|
|
! 0 or 1 one pass 2 two passes 3 or more is not supported
|
|
! init_elas use elastic stress-strain law as the material tangent for
|
|
! the first cycle of an increment
|
|
! ifatig packed integer telling which fatigue mode is active
|
|
! 1 = elastomer
|
|
! 10 = stress-life
|
|
! 100 = strain-life
|
|
! = 2 strain-life fatigue
|
|
! iftgmat = 0 no fatigue material properties in the dat file
|
|
! = 1 fatigue material properties in the dat file
|
|
! nchybrid cycle count used for hybrid contact; meant to force an extra iteration
|
|
! if the overlap for a node in hybrid contact is too large
|
|
! ibuckle buckle parameter option is active
|
|
! iexpande set to 1 if expanded elements (248, 249, 250 or 251) are
|
|
! present, 0 otherwise
|
|
! matfor flag for material forces computation
|
|
! 0: Eshleby stress and material force vector not requested
|
|
! 1: output Eshelby stress tensor, but no material force vector
|
|
! 2: output material force vector, but no Eshelby stress tensor
|
|
! 3: output Eshelby stress tensor and material force vector
|
|
! ishormem set to 1 if shell or membrane elements are present, 0 otherwise
|
|
! imsdifths flag for diffusion(pressure)/thermal/structural analysis
|
|
!
|
|
!***********************************************************************
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|
!$omp threadprivate(/marc_concom/)
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|
!!
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