{"id":5505,"date":"2019-04-01T14:12:56","date_gmt":"2019-04-01T05:12:56","guid":{"rendered":"http:\/\/advancae.com\/blog1\/?p=5505"},"modified":"2019-04-01T14:12:56","modified_gmt":"2019-04-01T05:12:56","slug":"lsdyna-r10-2-%e3%83%aa%e3%83%aa%e3%83%bc%e3%82%b9%e3%83%8e%e3%83%bc%e3%83%88","status":"publish","type":"post","link":"https:\/\/www.advancae.com\/blog1\/2019\/04\/01\/lsdyna-r10-2-%e3%83%aa%e3%83%aa%e3%83%bc%e3%82%b9%e3%83%8e%e3%83%bc%e3%83%88\/","title":{"rendered":"lsdyna R10.2 \u30ea\u30ea\u30fc\u30b9\u30ce\u30fc\u30c8"},"content":{"rendered":"<pre>MPP\u7248\u3001Hybrid\u7248\u3001\u30ea\u30ea\u30fc\u30b9\u30ce\u30fc\u30c8\u7b49\u4e00\u901a\u308a\u51fa\u63c3\u3063\u305f\u306e\u3067\u3001\u5f0a\u793eHP\u306b\u30a2\u30c3\u30d7\u3057\u307e\u3057\u305f\u3002<br \/>\u73fe\u72b6\u3001Windows\u7528MPP\u7248\u304c\u51fa\u3066\u3044\u307e\u305b\u3093\u3001\u3068\u3044\u3046\u304b\u51fa\u308b\u96f0\u56f2\u6c17\u306f\u5e0c\u8584\u3002<br \/>AVX2\u3068AVX512\u7248\u306b\u3064\u3044\u3066\u3082\u3001Windows\u4e0a\u3067\u306f\u5dee\u304c\u306a\u3044\u306e\u304b\uff1f\u3001\u3069\u308c\u3067\u3082\u4f7f\u3048\u308b\u5171\u901a\u30e2\u30b8\u30e5\u30fc\u30eb\u306e\u307f\u3067\u3059\u3002<br \/><br \/>\u4ee5\u4e0bR10.2\u30ea\u30ea\u30fc\u30b9\u30ce\u30fc\u30c8\u3067\u3059\u3002<br \/><br \/>---------------------------------------------------------------------------------<br \/>This file constitutes revision 0 of the release notes for LS-DYNA version R10.2.0.<br \/>---------------------------------------------------------------------------------<br \/><br \/>I. LICENSE<br \/><br \/>The string \"REVISION 10\" must appear in the LS-DYNA license file in order to run <br \/>version R10.2.0.  Please contact your LS-DYNA distributor (keys@lstc.com if<br \/>you're a direct customer of LSTC) if you need to have your license updated.<br \/><br \/><br \/>----------------------------------------------------------------------------<br \/><br \/>II. DOCUMENTATION<br \/><br \/>Documentation of R10.2.0 is provided in the R10.0 User's Manuals which may<br \/>be downloaded from www.lstc.com\/download\/manuals. <br \/>For features mentioned in these release notes but which appear to be missing <br \/>from the R10.0 User's Manuals, please refer to the DRAFT User's Manuals at <br \/>www.lstc.com\/download\/manuals.   Please note though that not all the features <br \/>in the DRAFT User's Manuals are available in version R10.2.0.<br \/><br \/>----------------------------------------------------------------------------<br \/><br \/>III. NOTES<br \/><br \/>The remainder of this file describes what's been added or fixed in version R10.2.0 <br \/>since the release of version R10.1.0. The changes are primarily just bug fixes. <br \/><br \/>The items are arranged by category.  Understand that in many cases,<br \/>a particular item could fall under more than one category, but in the<br \/>interest of brevity, each item is listed only once, under a single category.<br \/><br \/>Excluding the \"Miscellaneous\" category, the categories are arranged alphabetically.<br \/><br \/>The categories are:<br \/><br \/>________________________ *AIRBAG ___________________                          <br \/>________________________ ALE ___________________                              <br \/>________________________ *BOUNDARY ___________________                        <br \/>________________________ CESE (Compressible Fluid Solver)  ________________   <br \/>________________________ CONTACT ___________________                          <br \/>________________________ *CONSTRAINED ___________________                     <br \/>________________________ *CONTROL ___________________                         <br \/>________________________ Discrete Element Method ___________________          <br \/>________________________ EFG (Element Free Galerkin) _____________            <br \/>________________________ *ELEMENT ___________________                         <br \/>________________________ Forming Analysis __________                          <br \/>________________________ *FREQUENCY_DOMAIN ___________________                <br \/>________________________ ICFD (Incompressible Fluid Solver)  ______________   <br \/>________________________ Implicit (Mechanical) Solver _______                 <br \/>________________________ *INITIAL ___________________                         <br \/>________________________ Isogeometric Elements ___________________            <br \/>________________________ *LOAD ___________________                            <br \/>________________________ *MAT and *EOS ______________                         <br \/>________________________ MPP ___________________                              <br \/>________________________ Output ___________________                           <br \/>________________________ Restarts ___________________                         <br \/>________________________ *SENSOR ___________________                          <br \/>________________________ SPG (Smooth Particle Galerkin)  __________________   <br \/>________________________ SPH (Smooth Particle Hydrodynamics) ______________   <br \/>________________________ Thermal Solver ____________                          <br \/>________________________ Miscellaneous ___________________                    <br \/><br \/>==============================================================================<br \/><br \/><br \/>________________________ *AIRBAG ___________________                          <br \/><br \/>Exclude *AIRBAG_LOAD_CURVE and *AIRBAG_LINEAR_FLUID airbags from the<br \/>instability stablilization added to *AIRBAG_INTERACTION in<br \/>r117308\/R9 and 117309\/R10.<br \/><br \/>*AIRBAG_PARTICLE:<br \/>-  Improve p2f and p2p algorithms. In general CPM is speeded up by 3x.<br \/>-  OpenMP enabled.<br \/>-  Support autoliv mat_34 VOPT=-1\/-2 option.<br \/>-  Impulse decay scale factor can be controlled by each bag.<br \/>-  If the internal parts are solids, the volume from those parts is removed from bag volume.<br \/>-  External drag CD_ext can be applied as time dependent curve.<br \/>-  New option allows energy exchange between gas and surrounding structure parts.<br \/>    To turn on the feature, provide Cp of target parts.<br \/>    The initial temperature of the parts is same as the resident air (not ambient temperature).<br \/>    The time history of part temperature is reported to abstat_cpm under part_temp<br \/>-  If chamber definition is used, the code will error terminate when inflator nodes<br \/>    are not not associated with any chamber ID.<br \/>-  Support SENSOR_SWITCH_SHELL_TO_VENT for SMP.<br \/><br \/>Control Volume (Uniform Pressure) *AIRBAG types:<br \/>-  Fix bug in *AIRBAG_HYBRID_JETTING with vent coefficient defined with a load curve.<br \/>-  *AIRBAG_INTERACTION with LCID will error terminate if used with *AIRBAG_LOAD_CURVE<br \/>    or *AIRBAG_LINEAR_FLUID.<br \/><br \/><br \/>________________________ ALE ___________________                              <br \/><br \/>*DATABASE_BINARY_FSILNK, *LOAD_SEGMENT_FSILNK:<br \/>Fix a bug in the routine reading the binary file that created empty files with<br \/>random numbers appended to their names.<br \/><br \/>*ALE_REFERENCE_SYSTEM_GROUP:<br \/>If PRTRYPE=9 (the ALE mesh can expand and move with a structure), correct<br \/>truncation errors in the moving mesh logic<br \/><br \/>*INITIAL_VOLUME_FRACTION_GEOMETRY:<br \/>If VX or VY or VZ or VR &gt; 0 (initialize the velocities for an ALE group),<br \/>fix an issue related to the order in which the velocities of the ALE groups<br \/>are initialized.<br \/><br \/>*CONTROL_ALE:<br \/>If DCT&gt;-1, add warning messag (KEY+1199) to advise the user to set DCT=-1<br \/><br \/><br \/>________________________ *BOUNDARY ___________________                        <br \/><br \/>Fix old bug in *INTERFACE_LINKING that would cause<br \/>incorrect behavior for displacements scaled via a *DEFINE_FUNCTION<br \/>if (and only if) the function was defined in terms of 3<br \/>variables (spatial displacement dependence only).<br \/><br \/>Fix SMP *INTERFACE_LINKING which was broken in r109945.<br \/><br \/>Corrected the local rigid body rotation in implicit prescribed by<br \/>*BOUNDARY_PRESCRIBED_MOTION_RIGID_LOCAL which could be wrong when<br \/>combined with translational motion.<br \/><br \/>Fix processing of prescribed motion constraints for explict computation with superelements<br \/>(*ELEMENT_DIRECT_MATRIX_INPUT).<br \/><br \/>Add a more robust solution for using birth and death times for<br \/>prescribed motion constraints when using explicit LaGrange Multiplier<br \/>Formulation for joints and rigid bodies.<br \/><br \/>Fix seg fault when using *INTERFACE_LINKING_NODE_SET.<br \/><br \/>Fix *BOUNDARY_PRESCRIBED_ORIENTATION_RIGID_DIRCOS which does not orientate the<br \/>rigid body when angles are close to PI when using double precision.<br \/><br \/>*BOUNDARY_SPC_SYMMETRY_PLANE:<br \/>-  Fix segmentation fault.<br \/>-  Fix adaptive nodes which were not constrained.<br \/>-  Allow for more than 2 symmetry planes to be defined.<br \/><br \/><br \/>________________________ CESE (Compressible Fluid Solver)  ________________   <br \/><br \/>Expanded a scratch memory array in the CESE 3D FSI-ibm solver in<br \/>order to avoid issues in very rare cases.<br \/><br \/>For the *CESE_DATABASE cards, corrected these issues:<br \/>   a) Any used segments that are not in the CESE mesh are reported.<br \/>   b) Element sets look up is now guaranteed to work.<br \/>   c) Drag calculation output that is attempted for the incorrect FSI method,<br \/>      is now reported.  Here are the illegal cases:<br \/>      i) *CESE_DATABASE_FSIDRAG is only available with the CESE immersed<br \/>         boundary FSI solvers.<br \/>      ii) *CESE_DATABASE_SSETDRAG is not available with the CESE immersed<br \/>          boundary FSI solvers.  In other words, it only works with the<br \/>          non-FSI solvers and moving mesh FSI solvers.<br \/>   d) Failure to find an internal node number in *CESE_DATABASE commands is now<br \/>      reported.<br \/>   e) Output was not being performed for the initial conditions.  Instead, it<br \/>      is now done after the first time step.<br \/><br \/><br \/>________________________ CONTACT ___________________                          <br \/><br \/>Fix possible hanging of SMP single precision when interforce file<br \/>output (*DATABASE_BINARY_INTFOR) is requested.<br \/><br \/>Undo r108248, which was not a good idea.<br \/>\"Interface Pressure\" in the intfor file is now returned<br \/>to always being positive.<br \/><br \/>Fix initialization error related to *CONTACT_AUTOMATIC_GENERAL_INTERIOR<br \/>that resulted in every subsequent *CONTACT_AUTOMATIC_GENERAL also being<br \/>treated as INTERIOR.<br \/><br \/>Fix for spotwelds improperly deleted due to<br \/>rigid body conflict when an IPBACK contact interface<br \/>is in effect.  MPP only.<br \/><br \/>Fix to recompute rotational node<br \/>mass increment for BEAM_OFFSET contact after full<br \/>deck restart.<br \/><br \/>Corrected the collection of resultant forces in implicit for tied contact using<br \/>the OFFSET option.  Other tied contact options such as CONSTRAINED_OFFSET<br \/>were correct.<br \/><br \/>Made correction to bndout output, including that from prescribed motion,<br \/>for Implicit Mechanics.<br \/><br \/>Account for inertia relief modes in MPP for the computation of<br \/>resulting forces from constraints for Implicit Mechanics.<br \/><br \/>Ignore spotwelds with inactive parts during implicit dynamic relaxation computations.<br \/><br \/>Implement consistency, i.e. ncpu&lt;0, when using *CONTACT_SURFACE_TO_SURFACE_THERMAL_FRICTION<br \/>where static and dynamic coefficients of friction are function of temperature.<br \/><br \/>Fix incorrect rigidwall forces &amp; stonewall energy which will result in incorrect<br \/>rigidwall frictional behavior when using *RIGIDWALL_PLANAR_ORTHO.<br \/><br \/>Fix *CONTACT_AUTOMATIC_GENERAL for spotweld beams when using SSID=0, i.e. all<br \/>parts included in the contact, and CPARM8=2.<br \/><br \/>Implement unloading curve, UNLCID, for options FCM=2\/3 in *CONTACT_RIGID_(OPTION).<br \/><br \/>Fix zero frictional energy output to glstat and sleout when using<br \/>*CONTACT_AUTOMATIC_SURFACE_TO_SURFACE_ORTHO_FRICTION.<br \/><br \/>Fix input error for duplicate part if multiple *RIGIDWALL_GEOMETRIC_..._DISPLAY<br \/>are used with some with specified part id, PID, while some are not.<br \/><br \/>Enabled entity contact (*CONTACT_ENTITY) to work with thick shell elements.<br \/>It previously  error terminated in the input phase.<br \/><br \/>Fixed *CONTACT_2D_AUTOMATIC_TIED when used with selective mass scaling, which is<br \/>made active by setting  IMSL=1 and DT2MS&lt;0 on *CONTROL_CONTACT.  The problem occcured<br \/>when selective mass scaleing was applied to the nodes that are tied.  Prior to the change,<br \/>kinematic constraints were failing.<br \/><br \/>Enabled *CONTACT_2D_AUTOMATIC to work with element erosion when using cohesive<br \/>element forms 29 and -29.<br \/><br \/>Enabled *CONTACT_2D_AUTOMATIC to work with element erosion when using material types 81 or 82.<br \/><br \/>Fixed MPP *CONTACT_2D_AUTOMATIC when beams were in contact, or when solids were used with<br \/>nonzero values of SLDSOS or SLDSOM.  Both cases could lead to using invalid memory space<br \/>and a segmentation fault.<br \/><br \/>Added support for death time in *CONTACT_2D_TIED.  When the death time is reached, the ties are released.<br \/>To prevent penetration of the released nodes, add another contact definition such as<br \/>*CONTACT_2D_AUTOMATIC_SURFACE_TO_SURFACE with a birth time equal to the death time of the tied contact.<br \/><br \/>Enabled multiple instances of *CONTACT_2D_AUTOMATIC_TIED to work correctly.<br \/>Runs were error terminating.<br \/><br \/>Fixed an MPP segment based (SOFT=2) contact error that could occur if the contact<br \/>uses SBOXID to eliminate slave segments.  This could cause a segmentation fault during<br \/>initialization.<br \/><br \/>Fixed MPP implicit segment based contact which was failing to properly reset the segment<br \/>and node data leading to possible \"floating invalid\" error or possible convergence failure.<br \/><br \/>Fixed an error in MPP segment based eroding contact that could cause force spikes<br \/>and inappropriate contact detection after solid elements erode.<br \/><br \/>Improve spotweld beams in MORTAR contact, by making sure the end is not<br \/>subject to contact when already tied or merged to another element,<br \/>thus avoiding large spurious penetrations and bad convergence in implicit.<br \/><br \/>Fixed interface force file (*DATABASE_BINARY_INTFOR) for SMP version<br \/>if the file size is larger than 7M byte.<br \/><br \/><br \/>________________________ *CONSTRAINED ___________________                     <br \/><br \/>Correct the MPP communication during the testing of co-linear nodes in<br \/>*CONSTRAINED_INTERPOLATION.  Promote linear algebra processing for explicit use<br \/>of *CONSTRAINED_INTERPOLATION to always use double precision even<br \/>in the single precision executables in order to remove round-off error accumulation.<br \/><br \/>Add additional error checking on coincident nodes for REVOLUTE and SCREW joints.<br \/><br \/>Implement handling of failure of *CONSTRAINE_TIE_BREAK for implicit.<br \/>This required saving of the failure flag to use when constraint matrix<br \/>structure has to be the same as the last analyze phase.<br \/><br \/>Fix kinetic energy dependence on cpu count when using *CONSTRAINED_JOINT_(OPTION)<br \/>with LMF=1 in *CONTROL_RIGID for MPP.<br \/><br \/>Several updates for *CONSTRAINED_INTERPOLATION_SPOTWELD (new card 5):<br \/>- Allow definition of separate stiffnesses STIFF, STIFF2, and STIFF3<br \/>   for tension, shear, and bending.<br \/>- Optional exponential damage law via LCDEXP.<br \/>- Alternative shear kinematics treatment, variable SROPT.<br \/>- Output of history variables with NEIPB=7 on *DATABASE_EXTENT_BINARY.<br \/><br \/>Fixed bug in reading *CONSTRAINED_NODAL_RIGID_BODY and *PART_INERTIA.<br \/><br \/>*CONSTRAINED_COORDINATE:<br \/>Fix a machine dependent error when the defined coordinates are far away from the actual part.<br \/><br \/><br \/>________________________ *CONTROL ___________________                         <br \/><br \/>*CONTROL_REFINE_SOLID, *CONTROL_REFINE_SHELL:<br \/>- If NLVL&gt;1 (refine more than one level) and CRITRM&gt;0 (a coarsening criterion exists),<br \/>  fix a condition that prevents the coarsening of a given element if one of its<br \/>  child elements is itself still refined.<br \/>- If CRITRM&gt;0 (a coarsening criterion exists), deactivate contact segments of<br \/>  child elements that become inactive after coarsening.<br \/><br \/>*CONTROL_REFINE_SOLID, *CONTROL_REFINE_ALE:<br \/>If NLVL&gt;1 (refine more than one level), fix the logic merging elements refined at<br \/>different levels that only share sides.<br \/><br \/>*CONTROL_ADAPTIVE:<br \/>If IADPOPT=8 (r-adaptive remeshing) and ELFORM=12 (plane stress elements),<br \/>map the shell thicknesses from old to new mesh.<br \/><br \/>Improve the cleanup of temporary files during adaptive (*CONTROL_ADAPTIVE) steps.<br \/><br \/>Fix excessive memory growth during adaptive problems, and reduce<br \/>memory requirements overall.<br \/><br \/>Expand the meaning of *CONTROL_ADAPTIVE's variable CNLA:<br \/>Avoid simplified boundary description in 2D r-adaptive remeshing (ADPOPT=8)<br \/>by setting CNLA less than zero, recommended value is CNLA = -110.<br \/><br \/>Fix tolerance in selective mass scaling (*CONTROL_TIMESTEP) to avoid<br \/>non-convergence in single precision.<br \/><br \/>Fixed bug in reading multiple entries for *CONTROL_REQUIRE_REVISION.<br \/><br \/>Fixed bug in reading *CONTROL_REQUIRE_REVISION if free format is used.<br \/><br \/>*CONTROL_ADAPTIVE:<br \/>-  Fix bug in models featuring shell adaptivity but which also had beam elements<br \/>    (such as used in drawbeads).  The bug caused an error termination.<br \/>-  Allow a parameter file name in *INCLUDE.<br \/><br \/><br \/>________________________ Discrete Element Method ___________________          <br \/><br \/>Fix bug when both *DEFINE_DE_MASSFLOW_PLANE and *DATABASE_BINARY_DEMFOR are defined.<br \/><br \/>Fix output bug if multiple *PARTICLE_BLAST are defined ---MPP only.<br \/><br \/><br \/>________________________ EFG (Element Free Galerkin) _____________            <br \/><br \/>Fixed bug in reading mutiple *SECTION_SHELL_EFG.<br \/><br \/>3D adaptivity EFG now supports output associated with variables<br \/>STRFLG and INTOUT in *DATABASE_EXTENT_BINARY.<br \/><br \/>EFG shell (ELFORM=41) parts are distributed to all CPUs by default in MPP.<br \/><br \/>Fixed incorrect stresses in EFG plane strain formulation 43 for both implicit and explicit<br \/>analyses and EFG axisymmetric solid formulation 44 for explicit analysis only.<br \/><br \/><br \/>________________________ *ELEMENT ___________________                         <br \/><br \/>Fix a MPP bug for type 9 *ELEMENT_SEATBELT_PRETENSIONER that could be triggered<br \/>by having more than one type 9 pretensioner.<br \/><br \/>Fixed mass and kinetic energy output in d3hsp and matsum files for type 8 (axisymmetric) beams.<br \/><br \/>Enabled thick shell form 7 to output data for 4 points per layer to the ELOUTDET file.<br \/><br \/>Added support of the NINTSLD variable on *DATABASE_EXTENT_BINARY for solid pentehedral<br \/>element forms 15 and 115.  Also, when NINTSLD=1, form 15 now averages the data from the<br \/>two points for output rather than printing the data of the first point.<br \/><br \/>Fixed bulk viscosity of thick shell forms 1, 2, and 6.  Unstable behavior was likely.<br \/><br \/>Fixed the behavior of CDL and TDL on *SECTION_DISCRETE when one of the nodes is<br \/>constrained by an SPC.  Also, corrected the DEFORC output when CDL and TDL limits are reached.<br \/><br \/>Fixed thick shell forms 5 and 7 when used with total Lagrangian material models such<br \/>as *MAT_002.  The thick shells use a corotational coordinate system which rotates when<br \/>the element rotates.  However, the calculation of the deformation gradient, F for the<br \/>strain measure also includes this rotation, so we were accounting for the rotation twice.<br \/>To fix this, the thick shells now calculate F using the symmetric rate of deformation, D,<br \/>rather than the velocity gradient, L.  With this change, large rotation of elements is<br \/>possible and the strain and stress remain accurate.<br \/><br \/>*SECTION_SOLID, ELFORM=19,20,21,22:<br \/>Suppress unnecessary writing of warning messages concerning element type<br \/>switching for cohesive pentas.<br \/>This change does not affect the analysis!<br \/><br \/>Triangular shell element type 4 that combines thermal expansion and<br \/>thick thermal shells, see *MAT_ADD_THERMAL_EXPANSION and TSHELL on<br \/>*CONTROL_SHELL, now correctly treat temperature gradient through<br \/>the thickness to create bending moments. This is already available<br \/>for shell element types 2 and 16 since R10.0.0.<br \/><br \/>Fix *ELEMENT_BEAM_PID when offsets from *INCLUDE_TRANSFORM are used<br \/>for PID1 and PID2.<br \/><br \/>Fix seg fault in Cosserat element, solid formulation 1 or 16 with hourglass<br \/>type 10, when hourglass energy is not asked for, and fix hourglass energy<br \/>output for when it is asked for.<br \/><br \/>Fix spurious read error for *SECTION_BEAM_AISC.<br \/><br \/>Fix error in reading Card 5 of *SECTION_SHELL for user-defined shell elements.<br \/><br \/><br \/>________________________ Forming Analysis __________                          <br \/><br \/>*DEFINE_CURVE_TRIM:<br \/>-  Fix bug for trimming with a vector (option _2D), which was not recognized.<br \/>-  Fix bug in missing strain tensors after trimming.<br \/>-  Fix bug for \"Normal Termination\" not written into mes0000.<br \/>-  Fix bug for trimming of tshell with a defined vector, which was not recognized.<br \/>-  Fix bug for trimming of sandwiched parts with a defined vector, which was not recognized.<br \/>-  Fix bug for some lost history information during trimming of shells.<br \/>-  Fix bug in 3D trimming, where specifying a vector which is not needed causes<br \/>    an error termination.<br \/>-  Fix bug in trimming of multi-layer sandwiched sheets, where it would generate<br \/>    unnecessary shells at the top and bottom of every solid.<br \/>-  Fix stress output issue.<br \/><br \/>*CONTROL_FORMING_OUTPUT:<br \/>-  Fix bug when the smallest distance in the curve referenced by *CONTROL_FORMING_OUTPUT<br \/>    is equal to the total travel distance of the tool, LS-DYNA outputs d3plot<br \/>    files every time step.<br \/>-  Fix bug where only the 2nd NOUT (forming) is recognized and 1st NOUT (closing) is missed.<br \/><br \/>*ELEMENT_BLANKING:<br \/>Fix bug of not filling the corner with elements properly.<br \/><br \/>*CONTROL_FORMING_REMOVE_ADAPTIVE_CONSTRAINTS:<br \/>Fix bug for trianglar elements whose adaptive constraints were not removed.<br \/><br \/>*CONTROL_IMPLICIT_FORMING:<br \/>-  Type=2: fix bug for implicit calcuation convergence issue; the problem was<br \/>    caused by truncation error causing solution to oscillate leading to non-convergence.<br \/>-  Type=1: fix truncation error which caused solution to diverge.<br \/>-  Type=1: fix energy explosion and division by zero error, and fix truncation<br \/>    error when blank and binder are far apart.<br \/><br \/>Fix bug where *PART_MOVE with IFSET=1 does not move parts if set is defined using<br \/>*SET_PART_ADD, and\/or *SET_PART_LIST_COLLECT.<br \/><br \/>*DEFINE_FORMING_CLAMP:<br \/>-  Output an error message: \"Vector: xx was not defined\" in case a vector is<br \/>    prescribed to a fixed rigid tool by mistake.<br \/>-  Check constraints for the rigid clamper and free the constraints from the moving clampers.<br \/><br \/>*DEFINE_MULTI_DRAWBEADS_IGES:<br \/>Fix duplicate node set problem, which caused the simulation to crash.<br \/><br \/><br \/>________________________ *FREQUENCY_DOMAIN ___________________                <br \/><br \/>*FREQUENCY_DOMAIN_RANDOM_VIBRATION:<br \/>Fixed a bug in computing RMS (Root Mean Square) values of Von Mises stress for<br \/>solid elements.<br \/><br \/>*FREQUENCY_DOMAIN_RESPONSE_SPECTRUM:<br \/>Fixed nodal displacement output to d3spcm. Only the nodal displacement (u) itself<br \/>(not updated nodal coordinates, which is u+x0) is written to d3spcm.<br \/><br \/>*FREQUENCY_DOMAIN_SSD:<br \/>Fixed dumping nodout_ssd for the load cases of base velocity (vad=2) and base<br \/>acceleration (vad=3), when local damping is used (dmpflg=1).<br \/><br \/><br \/>________________________ ICFD (Incompressible Fluid Solver)  ______________   <br \/><br \/>Fixed HCSFLCID and TCSFLCID issue in *ICFD_MAT. Those two optional load curve IDs were ignored in MPP.<br \/><br \/>Fixed erroneous stabilization of temperature field. Results should now be close again to R9 and R11 versions.<br \/><br \/>Brought in R11 fix for multiphase cases (eg air+water problem) which should now be more accurate and stable.<br \/><br \/>Changed the format of ICFD_BOUNDARY_FSWAVE keyword to reflect the subsequent changes in R11 and Dev.<br \/><br \/><br \/>________________________ Implicit (Mechanical) Solver _______                 <br \/><br \/>Corrected Multistep linear (NSOLVR=-1) for the case of just one step.<br \/><br \/>Properly size an array used during the computation of participation factors associated<br \/>with eigenmodes for the very small model case.<br \/><br \/>Assure that Implicit Mechanics is turned off for thermal only solutions.<br \/><br \/>Enhanced the MMD ordering for Implicit Mechanics ISOLVR=2 option.<br \/><br \/>Corrected an inefficiency in Implicit Mechanics when there are numerous<br \/>AutoSPC constraints in MPP.  A linear search through the AutoSPC<br \/>constraints was replaced with a binary search.<br \/><br \/>Fix divide by zero in power iteration for buckling problems with<br \/>inertia relief.<br \/><br \/>Fix to properly handle an exactly singular constraint matrix for<br \/>*CONSTRAINED_INTERPOLATION running in fast\/vector mode.<br \/><br \/>Extend logic for implicit constraint handling to tied contact with<br \/>CONSTRAINED_OFFSET to skip any SPC constraints on the rotational dofs<br \/>of the slave nodes.  We already have such logic to skip the SPC<br \/>constraints on the translational dofs for the slave nodes for all<br \/>tied contact.<br \/><br \/>Restrict a block of code executed during *PART_MODES initialization<br \/>to only run on Processor 0 in MPP.<br \/><br \/>Enhance the logic for dumping matrices in the presence of rotational<br \/>dynamics.<br \/><br \/>Correct the issue where use of *LOAD_BODY is applied to a model with<br \/>rigid bodies.  If the vector of nodes having the load applied belong to<br \/>a rigid body then the vector of elemental stiffness matrices is null.<br \/>Added logic to skip the call to the implicit matrix assembly<br \/>subroutine for that case.<br \/><br \/>Solution control was unexpectedly returning to implicit after a \"sw1\"<br \/>sense switch.  This termination is now cleanly handled.<br \/><br \/>Correct the dumping of matrices from implicit when MTXDMP &gt; 1.<br \/><br \/>Added an error test for improper DRTERM when using implicit for dynamic<br \/>relaxation.  Enhanced implicit key point logic during dynamic relaxation<br \/>phase.<br \/><br \/>Enable Implicit to collect resultant forces for SPC constraints in<br \/>local coordinates.<br \/><br \/>Fixed implicit element stiffness of shell element when used with laminated shell<br \/>theory, and when also using anisotropic material models 22, 34, 40, 54, 55, or 58.<br \/>It was likely that the shear stiffness was too small.<br \/><br \/>Fixed implicit treatment of beam spot weld elements (*SECTION_BEAM ELFORM=9) when<br \/>used with NF&gt;0 on *MAT_SPOTWELD.  The averaging of the stress was causing the model<br \/>to converge to the wrong solution with beam forces too low.<br \/><br \/>Fix stiffness matrix for Belytschko-Tsay shell to yield proper rigid body modes<br \/>in an eigenvalue analysis.<br \/><br \/>Fix bug that made rigid bodies deform in implicit-explicit switching problems.<br \/><br \/><br \/>________________________ *INITIAL ___________________                         <br \/><br \/>Fix seg fault or incorrect stresses when initializing stresses using *INITIAL_STRESS_SOLID<br \/>for *MAT_107\/*MAT_MODIFIED_JOHNSON_COOK.<br \/><br \/>Fixed *INITIAL_STRESS_SHELL and *INITIAL_STRESS_TSHELL when used with *INTEGRATION_SHELL.<br \/>The integration rule was getting lost leading to unecessary interpolation of data.<br \/><br \/>Fix beam ID in message file when *INITIAL_AXIAL_FORCE_BEAM preload is completed.<br \/><br \/><br \/>________________________ Isogeometric Elements ___________________            <br \/><br \/>*ELEMENT_SHELL_NURBS_PATCH:<br \/>Fixed bug in reduced integration rule INT=2 that appeared if continuity within<br \/>a quadratic patch may have been reduced to C0 locally due to duplicated<br \/>knot-vector-values.<br \/><br \/><br \/>________________________ *LOAD ___________________                            <br \/><br \/>Fix output to nodfor when using *LOAD_SSA.<br \/><br \/>Fix ineffective *LOAD_THERMAL_CONSTANT when used on *MAT_106_THERMAL\/<br \/>*MAT_ELASTIC_VISCOPLASTIC_THERMAL.<br \/><br \/>Fixed *LOAD_THERMAL_VARIABLE_ELEMENT_TSHELL and *LOAD_THERMAL_LOAD_CURVE when used with thick shells.<br \/><br \/>Fixed bug for *LOAD_SEGMENT_FILE when jobid is used.<br \/><br \/><br \/>________________________ *MAT and *EOS ______________                         <br \/><br \/>Fixed bug in *MAT_203\/*MAT_HYSTERETIC_REINFORCEMENT affecting beam elements with<br \/>EPDAM1, EPDAM2 non-zero, and DRESID equal to zero. When the beam reached its<br \/>erosion limit, error termination could occur or there could be unexpected<br \/>failure of the whole model.<br \/><br \/>Fixed bug in *MAT_211\/*MAT_SPR_JLR.<br \/>Load curve IDs 8 or 9 digits long were not read correctly from *MAT card in<br \/>single precision executables.<br \/><br \/>Bug fix to resolve a divergence issue when using *MAT_242\/*MAT_KINEMATIC_HARDENING_BARLAT2000.<br \/><br \/>Fix ineffective load curves LCSRA LCSRB LCSRC LCSRAB LCSRBC LCSCA in card<br \/>7 of *MAT_MODIFIED_HONEYCOMB\/MAT_126.<br \/><br \/>Fix ineffective FAIL&lt;0 flag for *MAT_MODIFIED_PIECEWISE_LINEAR_PLASTICITY\/*MAT_123,<br \/>i.e. using user-defined failure subroutine, matusr_24 in dyn21.F, to determine<br \/>failure.<br \/><br \/>Fix output to elout for solids using *MAT_PAPER\/*MAT_274 and CMPFLG&gt;0 in<br \/>*DATABASE_EXTENT_BINARY.<br \/><br \/>Fix seg fault when using *MAT_ADD_EROSION for *PART_COMPOSITE when the<br \/>first layer of the *PART_COMPOSITE is not using *MAT_ADD_EROSION.<br \/><br \/>Fix incorrect direction of thermal expansion when using *MAT_NONLINEAR_ORTHOTROPIC\/<br \/>*MAT_040 with *MAT_ADD_THERMAL_EXPANSION.<br \/><br \/>Fix contact penetration after element erosion when using *MAT_110\/<br \/>*MAT_JOHNSON_HOLMQUIST_CERAMICS with eroding contact.<br \/><br \/>Fix incorrect stress\/strain output to d3plot when using *MAT_TEMPERATURE_DEPENDENT_ORTHOTROPIC\/<br \/>*MAT_023 and running 2D analysis and MAXINT&gt;3 in *DATABASE_EXTENT_BINARY.<br \/><br \/>Fix incorrect stress initialization when using *MAT_005\/*MAT_SOIL_AND_FOAM with<br \/>LCID (pressure vs. volumetric strain), combined with *LOAD_DENSITY_DEPTH.<br \/><br \/>Fix strain rate effects on *MAT_157\/*MAT_ANISOTROPIC_ELASTIC_PLASTIC for implicit<br \/>static analysis.<br \/><br \/>Fixed *MAT_128\/*MAT_HEART_TISSUE for thick shell forms 3, 5, and 7.  Initializaion of<br \/>the F tensor was missing causing termination in the first cycle.<br \/><br \/>Fixed use of *MAT_FABRIC form -14 with Rayleigh damping.  Runs were failing in the first cycle.<br \/><br \/>Improved the behavior of hourglass form 6 with used with *MAT_089.  The material<br \/>parameter used to scale the hourglass stiffness was wrong leading to bad results.<br \/><br \/>Fixed *MAT_126 when used with type 3, 5, or 7 thick shells.  The angle initialization was<br \/>incorrect leading to bad stress values.<br \/><br \/>*MAT_LAMINATED_COMPOSITE_FABRIC (*MAT_058):<br \/>Fixed bug when using *MAT_058 with load curves defined for EA, EB, GAB<br \/>together with thick shell elements type=1 and 2.<br \/>Prior to this fix, the analysis with this combination may have gone unstable.<br \/><br \/>*MAT_LAMINATED_FRACTURE_DAIMLER_CAMANHO (*MAT_262):<br \/>Add flag \"DSF\" to *MAT_262 (Card 3, Column 7) that controls the failure of an<br \/>integration point based on in-plane shear failure.<br \/>This feature was added to reinstate the behavior of this material model prior<br \/>to a fix made in r117876.<br \/>Note: The behavior prior to r117876 was not really correct due to the theory of<br \/>      the model, but customers adjusted their model with this setting. Using<br \/>      the new DSF flag allows to enforce the same behavior as before.<br \/><br \/>*MAT_LAMINATED_FRACTURE_DAIMLER_PINHO\/_CAMANHO (*MAT_261\/*MAT_262):<br \/>Fix bug in *MAT_261\/262 (shells) that may have appeared if this material was<br \/>used in *PART_COMPOSITE with a different material model located at first<br \/>integration point (layer).<br \/>Prior to this fix, the deletion of the layered element was not triggered<br \/>correctly.<br \/><br \/>*MAT_LAMINATED_FRACTURE_DAIMLER_PINHO\/_CAMANHO (*MAT_261\/*MAT_262):<br \/>Fix bug when using table (2D) for defining strain rate dependent fracture<br \/>toughness values with respect to characteristic element length.<br \/>Prior to this fix, a wrong value for the fracture toughness could have been<br \/>used.<br \/><br \/>*MAT_ENHANCED_COMPOSITE_DAMAGE (*MAT_054):<br \/>In case EPSR and EPSF are defined,<br \/>correct computation of transverse shear strains for solids and tshells.<br \/><br \/>*MAT_LAMINATED_FRACTURE_DAIMLER_CAMANHO (*MAT_262):<br \/>Added a criterion to avoid possible snapback behavior in *MAT_262 by only<br \/>allowing certain \"softening\" modulus with respect to the elastic stiffness.<br \/>This might have lead to problems when using rate-dependent strength limits<br \/>together with fracture toughnesses values that are not properly set.<br \/><br \/>Bug fixes for *MAT_264 that resolve issues with AWG Test Case 16<br \/>(https:\/\/awg.lstc.com\/tiki-index.php?page=AWG+ERIF+Test+Example+16).<br \/><br \/>Fix NaN problem with shells using *MAT_024_LOG_INTERPOLATION<br \/>with VP=1 and dynamic relaxation.<br \/><br \/>Improve algorithm for the LOG_INTERPOLATION option of *MAT_024<br \/>when used with VP=1 for shell elements.<br \/>CPU time is reduced and results better match the alternative<br \/>approach for log interpolation (negative first value in table).<br \/><br \/>Fix for combination of *MAT_ADD_EROSION and thick shell type 2.<br \/>Strain-based criteria (e.g. MXEPS) did not work correctly before.<br \/><br \/>Fix for combination of *MAT_ADD_EROSION and *PART_COMPOSITE<br \/>by clearly detecting if erosion\/damage is used for a layer.<br \/><br \/>Add failure function terms (normal, bending, shear) as arguments<br \/>of functions in *DEFINE_CONNECTION_PROPERTIES with PRUL.ge.2.<br \/><br \/>Fix for GISSMO to be used in adaptive remeshing. Evaluation of damage<br \/>coupling flag could go wrong due to averaging of history variables in rezone step.<br \/><br \/>*MAT_SPOTWELD_DAIMLERCHRYSLER:<br \/>Add new option DGTYP=5 to *DEFINE_CONNECTION_PROPERTIES.<br \/><br \/>Fix for failure treatment in *MAT_224_GYS:<br \/>Update of failure function F could have been wrong, because the plastic<br \/>strain increment was not always zero for elastic integration points.<br \/><br \/>Fix bug in *MAT_ADD_EROSION, DIEM option, that would otherwise result in<br \/>spurious damage when more than damage model is used (IDAM less than -1)<br \/><br \/>Fix *MAT_ADD_EROSION, DIEM option, in combination with *INTEGRATION_SHELL<br \/>that would otherwise not work.<br \/><br \/>Support logarithmic strain rates in tables for *MAT_ADD_EROSION, DIEM option,<br \/>activated by having the first strain rate negative.<br \/><br \/>Fix incorrect internal energy calculations in *MAT_ADD_THERMAL_EXPANSION.<br \/><br \/>Change the stress update in *MAT_PML_ELASTIC_FLUID to make it stable.<br \/><br \/>A first-order low-pass filter is implemented to smooth the effective strain rate used for<br \/>MXEPS&lt;0 in *MAT_ADD_EROSION. All high frequency response above the cutoff frequency is filtered out.<br \/>The variable for invoking this filter is DTEFLT.<br \/><br \/>*MAT226_NLP:<br \/>-  Fix truncation error problems which caused the simulation to crash.<br \/>-  Add a lower limit for strain ratio after smoothing, which will be the the<br \/>    strain ratio of the first point on the FLD curve input.<br \/><br \/>*MAT_036_NLP:<br \/>Bug fix for non-linear strain path forming limit; reset beta value to zero.<br \/><br \/><br \/>________________________ MPP ___________________                              <br \/><br \/>Fix problem with \"%proc\" option in the region based<br \/>decomposition in the pfile, which was always putting the<br \/>indicated region onto a range of processors starting<br \/>at processor 0, even if that would result in poor<br \/>load balance.<br \/><br \/>Improve MPP decomposition processor assignment<br \/>for regions assigned to a subset of the processors.<br \/><br \/>Fix for possible incorrect synchronization of<br \/>shared nodal coordinates after initial penetration<br \/>checking in MPP contact.<br \/><br \/>Fix missing initialization that broke d3plot<br \/>files when MPP predecomposition was used with<br \/>models having *DEFINE_CURVE_FUNCTIONS that used<br \/>the PIDCTL function.<br \/><br \/>Fix for MULTISCALE_SPOTWELD in double precision<br \/><br \/>Support Intel MPI 2018 on Linux Cent OS 6.5 and later.<br \/><br \/>AVX2 MPP binaries should now get identical results from AMD and Intel chip.<br \/><br \/>A listing of part sets defined in the keyword input is output by LS_DYNA to an<br \/>ASCII file called group_file.  To display the parts in any part set, read the<br \/>keyword input into LS-PrePost and then go to \"Model&gt;Groups\".  group_file is<br \/>automatically loaded and a list of part sets appears.  You can highlight any of those<br \/>part sets and click \"Select\" to display the parts in those selected part set(s).<br \/><br \/>Output user defined *PART_SET to group_file with title.<br \/><br \/>Collect and print massless nodes from all processors to mes0000 and d3hsp files.<br \/><br \/>Report time history of compute node memory, max\/min memory to binary glstat for performance analysis.<br \/><br \/>MPP option VSPEED will test and report network latency for performance debugging.<br \/><br \/>*PART_AVERAGED, which pertains to truss elements, is enhanced for the better MPP<br \/>scalability without special MPP decomposition.<br \/><br \/>A new option \"together\" for MPP decompostion is implemented to keep a region together<br \/>on one processor, as a super block as \"lumped\". It is also kept for the decomposition<br \/>with other parts to reduce the MPP communication.<br \/><br \/><br \/>________________________ Output ___________________                           <br \/><br \/>Corrected internal energy output for *DAMPING_FREQUENCY_RANGE_DEFORM.<br \/>The bug affected solid elements only, and related only to the<br \/>output values of internal energy.  The solution itself was not affected,<br \/>but users may have been concerned that the energy did not seem to balance.<br \/><br \/>Corrected internal energy and external work outputs for staged construction<br \/>(*CONTROL_STAGED_CONSTRUCTION, *DEFINE_STAGED_CONSTRUCTION_PART).<br \/>The bug affected only the output values of internal energy and external<br \/>work. The solution itself was not affected by the bug, but users may have<br \/>been concerned that the energy did not seem to balance.<br \/><br \/>Corrected internal energy output for pore fluid (*CONTROL_PORE_FLUID)<br \/>with multi-integration-point solid elements such as ELFORM=2.<br \/>The bug affected only the output values of internal energy.<br \/>The solution itself was not affected, but users may have been concerned<br \/>that the energy did not seem to balance.<br \/><br \/>Fix bug, the effect of which is not obvious, but could possibly<br \/>have led to incorrect output of beam data in elout.<br \/><br \/>Fix a MPP bug for nodal stress\/strain output to eloutdet (see variable NODOUT<br \/>in *DATABASE_EXTENT_BINARY), which could occur when multiple parts share the same<br \/>node where stress\/strain output is requested.<br \/><br \/>Fix a bug for 2d seatbelts whereby incorrect ID of 2d seatbelt retractor was<br \/>output to binary sbtout data.<br \/><br \/>Improved the reporting of hourglass energy to the glstat and matsum files.<br \/>Hourglass energy of eroded bricks was added to the eroded hourglass energy without<br \/>removing it from the regular hourglass energy.<br \/>Also, thick shells were not reporting eroded hourglass energy.  Fixing these issues<br \/>does not affect the solution, but improves the energy balance reported to glstat.<br \/><br \/>Fixed a memory error that occurred when there were spot weld assemblies that failed and the<br \/>input file did not include the keyword *DATABASE_SWFORC.<br \/><br \/>Fixed bug for d3plot output if both high order and ALE elements<br \/>are present in a model.<br \/><br \/>Echo *DATABASE_EXTENT_BINARY_COMP flags in d3hsp.<br \/><br \/>Fixed bug for d3plot if DCOMP=5 or 6 in *DATABASE_EXTENT_BINARY and<br \/>PSETID in *DATABASE_BINARY_D3PLOT is used.<br \/><br \/>Fixed bug for *DATABASE_HISTORY_NODE_ID in free format if the heading is more<br \/>than 10 characters.<br \/><br \/>Fixed part id output for discrete element in d3hsp.<br \/><br \/><br \/>________________________ Restarts ___________________                         <br \/><br \/>Fix MPP full deck restart issue that caused hanging<br \/>if the new input file contained encrypted input.<br \/><br \/>Corrected old memory pointers to work correctly in implicit on restart.<br \/>Also correct dump and restart length for implicit common<br \/>blocks to enable new nonlinear solution features.<br \/><br \/>Fix seg fault when using *DELETE_CONTACT for restart when running with SMP.<br \/><br \/>Fix error termination for full deck restart including *DEFINE_ELEMENT_DEATH.<br \/><br \/>Fixed corruption of d3part caused by a simple restart.<br \/><br \/>Fixed bug for corrupted d3part on small restart.<br \/><br \/>Fix bug in full-deck restart of tied contact so that contact forces are continuous across the restart.<br \/><br \/>*loa<br \/>Fix bug in accessing ground motion ID (*DEFINE_GROUND_MOTION) from<br \/>*LOAD_SEISMIC_SSI.<br \/><br \/><br \/>________________________ *SENSOR ___________________                          <br \/><br \/>Fix problem that the presence of *DATABASE_BNDOUT could cause *SENSORs<br \/>in the model to misbehave, with unexpected results.<br \/><br \/>Fix a bug for the ELESET option of *SENSOR_CONTROL.<br \/><br \/>Fix a bug for *SENSOR_DEFINE_FORCE, TYPE=JOINT, triggered by having a joint ID &gt; 9999999.<br \/><br \/>Fix a bug for *SENSOR_DEFINE_..._SET that could occur if the *SENSOR command appears<br \/>before the corresponding *SET command in the input file.<br \/><br \/><br \/>________________________ SPG (Smooth Particle Galerkin)  __________________   <br \/><br \/>Fixed problem of zero stress being output to d3plot for SPG with isotropic materials<br \/>when CMPFLG=1 in *DATABASE_EXTENT_BINARY.<br \/><br \/><br \/>________________________ SPH (Smooth Particle Hydrodynamics) ______________   <br \/><br \/>SPH performance improvement for OpenMP and HYBRID.<br \/><br \/>Support full deck restart for SPH.<br \/><br \/>Improve performance of *DEFINE_ADAPTIVE_SOLID_TO_SPH.<br \/><br \/>Support up to 6 SPH particles in each direction of each solid element in<br \/>*DEFINE_ADAPTIVE_SOLID_TO_SPH.<br \/><br \/>Identify element type as SPH when echoing part information in d3hsp:<br \/>     element type ..................... =    4<br \/>          eq.0: 4, 6, 8, 10-node solid element<br \/>          eq.1: 2-node beam or truss or 2D shell element<br \/>          eq.2: 3, 4-node membrane\/shell or 2D continuum element<br \/>          eq.3: 8-node thick shell element<br \/>          eq.4: SPH element<br \/><br \/><br \/>________________________ Thermal Solver ____________                          <br \/><br \/>Correct logic on acceptable thermal solver options for SMP.<br \/><br \/>Fixed bug where dynain file was missing some thermal history variables when using<br \/>*INTERFACE_SPRINGBACK_LSDYNA_THICKNESS with NTTHSV&gt;0.<br \/><br \/>Improved reporting of the thermal time step.<br \/><br \/><br \/>________________________ Miscellaneous ___________________                    <br \/><br \/>Fix functions PIDCTL and DELAY in *DEFINE_CURVE_FUNCTION when used in a full restart.<br \/><br \/>Fix a bug for MIRROR option of *DEFINE_TRANSFORMATION that was triggered when used<br \/>together with other transformation options.<br \/><br \/>Fix wrong pointer used for section id\/properties when generating part for visualization<br \/>of rigid wall during adaptivity. This caused error message, KEY+137, during adaptivity.<br \/><br \/>*DEFINE_FUNCTION:<br \/>Corrected output of function definition to d3hsp for double<br \/>precision executables.<br \/><br \/>Fixed segmentation fault when using *DEFINE_BOX_ADAPTIVE<br \/>in a large model.<br \/><br \/>Fixed bug affecting node sets created by *SET_NODE_ADD.<br \/><br \/>Fixed bug where use of *SET_PART_COLLECT caused parts in PSETID of<br \/>of *DATABASE_BINARY_D3PLOT not to be excluded from d3plot.<br \/>This was related to the duplicated ID in *SET_PART_COLLECT.<br \/>Now, an error message will be issued.<br \/><br \/>Fixed bug in newformat option for *NODE_SCALAR.<br \/><br \/>For newformat=i10 option, \"%\" sign is only added to the modified keyword.<br \/><br \/>Fixed command line option: plabel=(yes,no).<br \/>This command (plabel=no) will disable the checking for alpha IDs<br \/>file to speed up the input phase or disable any bug in the checking of labels.<br \/><br \/>Fixed legend output in nodout file if long format is used.<br \/><br \/>Fixed bug in reading long format if \"*KEYWORD long=yes\" is used in include file.<br \/><br \/>Fixed bug for *DATABASE_HISTORY_NODE_LOCAL_ID when long=s is used.<br \/><br \/>Fixed bug for reading long format input in the following keywords:<br \/>  *ALE_FSI_TO_LOAD_NODE<br \/>  *AIRBAG_HYBRID_ID<br \/>  *BOUNDARY_PRESCRIBED_FINAL_GEOMETRY<br \/>  *CONSTRAINED_GENERALIZED_WELD_FILLET<br \/>  *CONSTRAINED_TIED_NODES_FAILURE<br \/>  *CONTACT_AUTOMATIC_GENERAL_INTERIOR_MPP<br \/>  *CONTACT_ERODING_SINGLE_SURFACE_MPP<br \/>  *CONTROL_ADAPTIVE (3D)<br \/>  *DEFINE_HEX_SPOTWELD_ASSEMBLY<br \/>  *DEFINE_SPH_TO_SPH_COUPLING<br \/>  *DEFINE_TABLE_MATRIX<br \/>  *ELEMENT_BEAM_PIPE<br \/>  *ELEMENT_BEARING<br \/>  *FREQUENCY_DOMAIN_FRF<br \/>  *INCLUDE_STAMPED_PART<br \/>  *INITIAL_VOLUME_FRACTION<br \/>  *INTERFACE_SPRINGBACK_LSDYNA<br \/>  *NODE_MERGE<br \/>  *PARAMETER<br \/>  *PARAMETER_EXPRESSION<br \/>  *PERTURBATION_NODE<br \/>  *SPH_COUPLING<br \/>  *MAT_ADD_EROSION<br \/>  *MAT_EMMI<br \/>  *EOS_PHASE_CHANGE<br \/>*SET_NODE_LIST_GENERATE:<br \/>Fix bug which resulted in a corrupt node list.<br \/><br \/><br \/>====================== END of Release Notes for version R10.2.0 =============================<\/pre>","protected":false},"excerpt":{"rendered":"<p>MPP\u7248\u3001Hybrid\u7248\u3001\u30ea\u30ea\u30fc\u30b9\u30ce\u30fc\u30c8\u7b49\u4e00\u901a\u308a\u51fa\u63c3\u3063\u305f\u306e\u3067\u3001\u5f0a\u793eHP\u306b\u30a2\u30c3\u30d7\u3057\u307e\u3057\u305f\u3002\u73fe\u72b6\u3001Windows\u7528MPP\u7248\u304c\u51fa\u3066\u3044\u307e\u305b\u3093\u3001\u3068\u3044\u3046\u304b\u51fa\u308b\u96f0\u56f2\u6c17\u306f\u5e0c\u8584\u3002AVX2\u3068AVX512\u7248\u306b\u3064\u3044\u3066\u3082\u3001Windows\u4e0a\u3067\u306f\u5dee\u304c [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":[],"categories":[5],"tags":[],"_links":{"self":[{"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/posts\/5505"}],"collection":[{"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/comments?post=5505"}],"version-history":[{"count":1,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/posts\/5505\/revisions"}],"predecessor-version":[{"id":5506,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/posts\/5505\/revisions\/5506"}],"wp:attachment":[{"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/media?parent=5505"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/categories?post=5505"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/tags?post=5505"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}