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Martin Diehl
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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,icomplt, mesh_dual, iactrp, mgnewton, iusedens,igsigd0,&
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iaem, icosim, inodels, nlharm, iampini, iphasetr
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dimension :: ideva(60)
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integer(pInt) num_concom
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parameter(num_concom=245)
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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
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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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! 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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!
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!
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! 58 debug output for ELSTO usage
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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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! 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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! 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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! 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
|
||||
! 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
|
||||
! 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
|
||||
! iphasetr = 1 phase transformation material model is used
|
||||
!
|
||||
!***********************************************************************
|
||||
!$omp threadprivate(/marc_concom/)
|
||||
!!
|
||||
|
|
@ -1,424 +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, iphasetr, inonlcl, inonlct, iforminp,ispecerror
|
||||
dimension :: ideva(60)
|
||||
integer(pInt) num_concom
|
||||
parameter(num_concom=249)
|
||||
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, iphasetr, inonlcl, inonlct, iforminp,ispecerror
|
||||
!
|
||||
! 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
|
||||
! 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
|
||||
! is switched on internally due to cyclic symmetry or model
|
||||
! 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)
|
||||
!
|
||||
!***********************************************************************
|
||||
!$omp threadprivate(/marc_concom/)
|
||||
!!
|
||||
|
|
@ -1,66 +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
|
||||
real(pReal) fraction_donn,timinc_ol2
|
||||
!
|
||||
integer(pInt) num_creepsr,num_creepsi,num_creeps2r
|
||||
parameter(num_creepsr=7)
|
||||
parameter(num_creepsi=17)
|
||||
parameter(num_creeps2r=6)
|
||||
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,fraction_donn,timinc_ol2
|
||||
!
|
||||
! 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
|
||||
!
|
||||
! timinc_old Time step of the previous increment
|
||||
!
|
||||
!***********************************************************************
|
||||
!!$omp threadprivate(/marc_creeps/)
|
||||
!!$omp threadprivate(/marc_creeps2/)
|
||||
!!
|
||||
|
|
@ -1,66 +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
|
||||
real(pReal) fraction_donn,timinc_ol2
|
||||
!
|
||||
integer(pInt) num_creepsr,num_creepsi,num_creeps2r
|
||||
parameter(num_creepsr=7)
|
||||
parameter(num_creepsi=17)
|
||||
parameter(num_creeps2r=6)
|
||||
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,fraction_donn,timinc_ol2
|
||||
!
|
||||
! 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
|
||||
!
|
||||
! timinc_old Time step of the previous increment
|
||||
!
|
||||
!***********************************************************************
|
||||
!!$omp threadprivate(/marc_creeps/)
|
||||
!!$omp threadprivate(/marc_creeps2/)
|
||||
!!
|
||||
Loading…
Reference in New Issue