\u8981\u7d20\u304b\u3089\u6750\u6599\u30c7\u30fc\u30bf\u307e\u3067\u306e\u4fee\u6b63\u9805\u76ee<\/p>\r\n
________________________ *ELEMENT ___________________\u00a0\u00a0\u00a0<\/strong>\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 \u00a0 \u8981\u7d20\u304b\u3089\u6750\u6599\u30c7\u30fc\u30bf\u307e\u3067\u306e\u4fee\u6b63\u9805\u76ee ________________________ *ELEMENT ___________________\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 \u00a0Keyword: *SECTION_SOLID \u00a0 […]<\/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\/253"}],"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=253"}],"version-history":[{"count":1,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/posts\/253\/revisions"}],"predecessor-version":[{"id":254,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/posts\/253\/revisions\/254"}],"wp:attachment":[{"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/media?parent=253"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/categories?post=253"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.advancae.com\/blog1\/wp-json\/wp\/v2\/tags?post=253"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}
Keyword: *SECTION_SOLID \u00a0
\u00a0 Slightly modify implicit elform3 to make it compatible with explicit
\u00a0 elform3.
\u00a0
Keyword: *SECTION_SOLID \u00a0
\u00a0 Fix the deformation gradient calculation for linear solid element type 18.
\u00a0 A test case with material 123 was calculating material failure in the first cycle.
\u00a0
Keyword:\u00a0 *EOS_USER_DEFINED \u00a0
\u00a0 Fix bug associated with *EOS_USER_DEFINED in combination with ELFORM4 tetrahedrons.
\u00a0
Keyword: *SECTION_SOLID, *DATABASE_GLSTAT \u00a0
\u00a0 Fix spurious kinetic energy growth in glstat data of elform4 tets.
\u00a0
Keyword: *ELEMENT_SHELL_NURBS_PATCH, *ELEMENT_GENERALIZED_SHELL \u00a0
\u00a0 Renamed *ELEMENT_NURBS_PATCH_2D to *ELEMENT_SHELL_NURBS_PATCH
\u00a0 Activate *MAT_24 for isogeometric and generalized shells.
\u00a0
Keyword: *INTIIAL_STRESS_SOLID \u00a0
\u00a0 Fix reading of initial stresses for pentahedrons.
\u00a0
Keyword: *SECTION_TSHELL \u00a0
\u00a0 Fix problem of tshells not always eroding after reaching failure criterion.
\u00a0
Keyword: *SECTION_SHELL, *SECTION_SOLID \u00a0
\u00a0 Fix problem whereby 1-point 3D solid elements and 2D solid elements
\u00a0 could generate strain during rigid body motion when using single precision.
\u00a0
Keyword: *DAMPING_PART_STIFFNESS \u00a0
\u00a0 Fix stiffness damping to work correctly for solids.
\u00a0
Keyword: *SECTION_TSHELL, *CONTROL_PARALLEL \u00a0
\u00a0 Fix SMP parallel consistancy when PARA=1 in *CONTROL_PARALLEL for
\u00a0 thick shell forms 3 and 5, brick form 18, tet form 13.
\u00a0
Keyword: *CONTROL_ACCURACY, *SECTION_SOLID \u00a0
\u00a0 Correct pentehedral (form 15) brick element when used with invariant
\u00a0 node numbering.\u00a0 The symptom was a lack of parallel consistancy, but the
\u00a0 real problem was an incorrect calculation of the transformation matrix so
\u00a0 the behavior of ortho\/anisotropic materials was incorrect.
\u00a0
Keyword: *SECTION_SHELL \u00a0
\u00a0 Correct bug in shell formulations 23 and 24 affecting result in pure
\u00a0 bending.
\u00a0
Keyword: *SECTION_SHELL, *MAT_138, *MAT_240 \u00a0
\u00a0 Fix bug affecting 2D cohesive elements (*SECTION_SHELL, ELFORM=46\/47)
\u00a0 comprised of *MAT_COHESIVE_MIXED_MODE or
\u00a0 *MAT_COHESIVE_MIXED_MODE_ELASTOPLASTIC_RATE.
\u00a0
Keyword: *SECTION_SHELL \u00a0
\u00a0
\u00a0 Fix stress output for triangular shell formulation 17.
\u00a0
\u00a0 Fix output issues for shell element types 18, 23 and 24.
\u00a0
Keyword: *SECTION_SHELL \u00a0
\u00a0 Fix bug in output of shell element type 18 (linear DK).
\u00a0
Keyword: *SECTION_SHELL \u00a0
\u00a0 Add output of strain for 6-node triangular shell and 8-node quad shell
\u00a0 (shell formulations 23 and 24).
\u00a0 Also fix implicit formulation of these shells.
\u00a0
Keyword: *SECTION_SHELL \u00a0
\u00a0 Improve load distribution in quadratic shell formulations 23 and 24.
\u00a0
Keyword: *SECTION_SOLID \u00a0
\u00a0 Improve accuracy of solid element type 13 (tetrahedron).
\u00a0
Keyword: *SECTION_SHELL \u00a0
\u00a0 Fix for thickness update of generalized and isogeometric shells.
\u00a0
Keyword: *SECTION_SHELL \u00a0
\u00a0 Fix bug in rotation of fibers in shell formulationss 23 and 24, and
\u00a0 allow mid side nodes to take part in rigid body.
\u00a0
Keyword: *SECTION_TSHELL, *MAT_USER_DEFINED_MATERIAL_MODELS \u00a0
\u00a0 Fix thick shell forms 3 and 5 when used with user defined materials that
\u00a0 have orthotropic properties defined (IORTHO=1).\u00a0 Without the fix, the strain
\u00a0 increment, stress and deformation gradient transformations are incorrect.
\u00a0
Keyword: *SECTION_SOLID \u00a0
\u00a0 Add clean error termination when wrong solid element formulation is
\u00a0 specified for 10-noded tetrahedrons.
\u00a0
________________________ *FREQUENCY_DOMAIN ___________________\u00a0\u00a0\u00a0\u00a0 \u00a0<\/strong>
Keyword: *FREQUENCY_DOMAIN_ACOUSTIC_BEM \u00a0
\u00a0 Fix BEM acoustics when using set_segment for acoustic field nodes.
\u00a0
Keyword: *FREQUENCY_DOMAIN_RANDOM_VIBRATION \u00a0
\u00a0 Fix bug in reading mode information in random vibration.
\u00a0
Keyword: *FREQUENCY_DOMAIN_RANDOM_VIBRATION \u00a0
\u00a0 Fix bug in reading modal information and writing d3rms in random vibration analysis.
\u00a0
Keyword: *DATABASE_FREQUENCY_… \u00a0
\u00a0 Fix bug in defining output frequency curve for frequency domain databases.
\u00a0
Keyword: *FREQUENCY_DOMAIN_ACOUSIC_BEM \u00a0
\u00a0 Add a fringe plot option to all the BEM acoustic solvers.
\u00a0
\u00a0 Update BEM acoustics to remove the limitation on number of acoustic field nodes.
\u00a0
Keyword: *FREQUENCY_DOMAIN_ACOUSTIC_FEM \u00a0
\u00a0 Update frequency domain fem acoustics to introduce free pressure boundary
\u00a0 condition.
\u00a0
Keyword: *FREQUENCY_DOMAIN_ACOUSTIC_FEM \u00a0
\u00a0 Update frequency domain fem acoustics, to allow using the results of i
\u00a0 transient analysis.
\u00a0
Keyword: *FREQUENCY_DOMAIN_ACOUTIC_FEM \u00a0
\u00a0 Fix frequency domain FEM acoustics for tetrahedrons.
\u00a0
Keyword: *FREQUENCY_DOMAIN_FRF \u00a0
\u00a0 Fix a bug in FRF computation with pressure load.
\u00a0
Keyword: *FREQUENCY_DOMAIN_ACOUSTIC_BEM \u00a0
\u00a0 Fix a bug in restarting bem acoustics with SSD response.
\u00a0
Keyword: *FREQUENCY_DOMAIN_SSD \u00a0
\u00a0 Fix bug in SSD with multiple excitations.
\u00a0
\u00a0 Fix bug in SSD when using local damping option.
\u00a0
Keyword: *FREQUENCY_DOMAIN_RANDOM_VIBRATION \u00a0
\u00a0 Add xyplot output of psd_curve_print, converted from time history load,
\u00a0 for random vibration LDTYP=2.
\u00a0
Keyword: *FREQUENCY_DOMAIN_SSD \u00a0
\u00a0 Update on SSD to allow multi-axial excitation.
\u00a0
Keyword: *FREQUENCY_DOMAIN_SSD \u00a0
\u00a0 Add output of beam integration point values in Steady State Dynamics.
\u00a0
Keyword: *FREQUENCY_DOMAIN_RANDOM_VIBRATION_FATIGUE \u00a0
\u00a0
\u00a0 Add the option to define SN fatigue curves by two equations, for random fatigue.
\u00a0
\u00a0 Implemented Dirlik method to random fatigue analysis (mode acceleration
\u00a0 only).
\u00a0
Keyword: *FREQUENCY_DOMAIN_FRF \u00a0
\u00a0 Extend FRF to base velocity and base displacement excitation.
\u00a0
Keyword: *FREQUENCY_DOMAIN_ACOUSTIC_FEM \u00a0
\u00a0 Add Press_Pa_real and Press_Pa_imag output to frequency domain fem acoustics.
\u00a0
Keyword: *FREQUENCY_DOMAIN_RESPONSE_SPECTRUM \u00a0
\u00a0 Add Double Sum method to response spectrum analysis (MCOMB=3).
\u00a0
Keyword: *FREQUENCY_DOMAIN_SSD \u00a0
\u00a0 Fix a bug in writing nodout_ssd and elout_ssd files.
\u00a0
________________________ *INITIAL ___________________\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 \u00a0<\/strong>
Keyword: *INITIAL_STRESS_SOLID \u00a0
\u00a0 Add transformation of solid stresses input with *INITIAL_STRESS_SOLID
\u00a0 when *INCLUDE_TRANSFORM rotates geometry.
\u00a0
________________________ *LOAD ___________________\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 \u00a0<\/strong>
Keyword: *LOAD_BLAST_ENHANCED \u00a0
\u00a0 Fix blast wind velocity and wave index for BLAST=4.
\u00a0
Keyword: *LOAD_BLAST_ENHANCED \u00a0
\u00a0 Report the minimum computed arrival time.
\u00a0
Keyword: *LOAD_SSA \u00a0
\u00a0 Fix problem of incorrectly reading in explosive charge definitions.
\u00a0
Keyword: *LOAD_THERMAL_VARIABLE_BEAM \u00a0
\u00a0 Fix problem of *LOAD_THERMAL_VARIABLE_BEAM giving wrong temperatures for
\u00a0 tubular sections.
\u00a0
Keyword: *LOAD_BLAST_ENHANCED \u00a0
\u00a0 Fix an index problem for the blast origin when multiple
\u00a0 charges are defined.\u00a0 This problem elicited false warning messages during
\u00a0 initialization and had no ill effect on the actual blast load.
\u00a0
Keyword: *LOAD_RIGID_BODY \u00a0
\u00a0 Add warning message if *LOAD_RIGID_BODY part is a slave part in
\u00a0 *CONSTRAINED_RIGID_BODIES.
\u00a0
Keyword: *CONTROL_ADAPTIVE \u00a0
\u00a0 Fix problem when *CONTROL_ADAPTIVE and *LOAD_SEGMENT\/*LOAD_SEGMENT_SET
\u00a0 are used together for 2D analysis; problem was the effect of *LOAD_SEGMENT i
\u00a0 disappearred after adaptive step.
\u00a0
Keyword: *LOAD_BLAST_ENHANCED \u00a0
\u00a0 When BLAST=4 in *LOAD_BLAST_ENHANCED, eliminate ground encounter when
\u00a0 determining which entity is first hit by a shock wave.\u00a0 Use correct
\u00a0 time parameters and scaled distance so velocity decay is correctly
\u00a0 computed for encounter with the ground reflected wave.
\u00a0
________________________ *MAT ___________________<\/strong>\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 \u00a0
Keyword: *DEFINE_CONNECTION_PROPERTIES \u00a0
\u00a0 Fix case of AREAEQ.ne.0:
\u00a0 The true area was not correctly used in the failure function,
\u00a0 if the exponents EXSN, EXSB, EXSS were not 1.0.
\u00a0
Keyword: *MAT_ADD_EROSION \u00a0
\u00a0 Fix GISSMO damage history output to d3hsp.
\u00a0
Keyword: *MAT_156,_221,_226,_232,_233,_244,_267 \u00a0
\u00a0 Fix various material model bugs in
\u00a0 *MAT_MUSCLE (for truss elements),
\u00a0 *MAT_ORTHOTROPIC_SIMPLIED_DAMAGE,
\u00a0 *MAT_KINEMATIC_HARDENING_BARLAT89,
\u00a0 *MAT_BIOT_HYSTERETIC,
\u00a0 *MAT_CAZACU_BARLAT,
\u00a0 *MAT_UHS_STEEL,
\u00a0 *MAT_EIGHT_CHAIN_RUBBER
\u00a0
Keyword: *MAT_034 \u00a0
\u00a0 Make fabric material forms 12, 13, and 14 output global stress to the
\u00a0 d3plot file like the other fabric forms and other materials.
\u00a0
Keyword: *MAT_244 \u00a0
\u00a0 Implement *MAT_UHS_STEEL for 2D solid elements.
\u00a0
Keyword: *MAT_100 \u00a0
\u00a0 Make *MAT_SPOTWELD\/SIGY<0 consistent with *MAT_SPOTWELD\/SIGY>0.
\u00a0
Keyword: *MAT_174 \u00a0
\u00a0 Fix output of curvature to “plastic strain” position in output of
\u00a0 *MAT_RC_BEAM.
\u00a0
Keyword: *MAT_125 \u00a0
\u00a0 Fix energy calculation in *MAT_KINEMATIC_TRANSVERSELY_ANISOTROPIC.
\u00a0
Keyword: *MAT_…_THERMAL \u00a0
\u00a0 Correct calculation of heat flux vector for orthotropic materials.
\u00a0
Keyword: *MAT_036, *MAT_190 \u00a0
\u00a0 A bug fix for these materials in the case of equi-biaxial stretching.
\u00a0
Keyword: *MAT_100 \u00a0
\u00a0 Fix for damage calculation in *MAT_SPOTWELD_DAMAGE-FAILURE when SIGY<0.
\u00a0
Keyword: *MAT_THERMAL_USER_DEFINED \u00a0
\u00a0 Correct temperature in user materials in combination with 2D solids.
\u00a0
\u00a0 Correct history variable handling in thermal user materials.
\u00a0
Keyword: *MAT_233 \u00a0
\u00a0
\u00a0 Fix NUMINT option of *MAT_CAZACU_BARLAT.
\u00a0
\u00a0 Add new options related to rate effects and damage.
\u00a0
Keyword: *MAT_019 \u00a0
\u00a0 Make the strain rate the first history variable after the
\u00a0 plastic strain for all versions of *MAT_STRAIN_RATE_DEPENDENT_PLASTICITY.
\u00a0
Keyword: *MAT_181 \u00a0
\u00a0 Fix instability of *MAT_SIMPLIFIED_RUBBER\/FOAM in full deck restart.
\u00a0
Keyword: *MAT_224 \u00a0
\u00a0 Add *MAT_TABULATED_JOHNSON_COOK for type 13 tetrahedon.
\u00a0
Keyword: *MAT_ADD_EROSION \u00a0
\u00a0 Modify GISSMO parameters SHRF and BIAXF.
\u00a0
Keyword: *MAT_169 \u00a0
\u00a0 Add new option to *MAT_ARUP_ADHESIVE: If parameter BTHK<0, then do not
\u00a0 modify time step.\u00a0 This helps to avoid very small time steps, but it
\u00a0 can affect stability.
\u00a0
Keyword: *MAT_036 \u00a0
\u00a0 Correct bad output of strains and thickness reduction to d3plot for
\u00a0 *MAT_3-PARAMETER_BARLAT.
\u00a0
Keyword: *PART_COMPOSITE \u00a0
\u00a0 Enable *PART_COMPOSITE to work with material types 104, 108, 122, 133, 135,
\u00a0 137, 157, 223, 226, 229, 233, 234, 235, and 242.\u00a0 Previous, a keyword
\u00a0 error was reported.
\u00a0
Keyword: *MAT_187 \u00a0
\u00a0 Fix for large curve IDs in *MAT_SAMP-1.
\u00a0
Keyword: *MAT_123 \u00a0
\u00a0 Fix RTCL damage of *MAT_MODIFIED_PIECEWISE_LINEAR_PLASTICITY_RTCL such
\u00a0 the input parameter EPS0 is now used correctly.
\u00a0
\u00a0 Add parameter TRIAX which is a limit on the triaxiality, beyond
\u00a0 which damage will not grow.
\u00a0
Keyword: *MAT_120, *MAT_120_JC \u00a0
\u00a0 Add extra history variable 16 to *MAT_GURSON and *MAT_GURSON_JC for
\u00a0 convenience in checking against GISSMO damage model.
\u00a0
Keyword: *MAT_082 \u00a0
\u00a0 Fix bug in *MAT_PLASTICITY_WITH_DAMAGE_ORTHO for brick elements and
\u00a0 2D solids which caused elements to spuriously vanish.
\u00a0
Keyword: *MAT_024 and others \u00a0
\u00a0 Improve user-defined failure subroutine template matusr_24 including
\u00a0 passing of updated strain.
\u00a0
Keyword: *MAT_100 \u00a0
\u00a0 Fix the BETA>0 option for brick or brick assembly spot welds that use
\u00a0 DMGOPT=2, 10, 11, and 12.\u00a0 Weld failure was not occuring after damage
\u00a0 initialization.
\u00a0
Keyword: *MAT_234 \u00a0
\u00a0 Fix calculation of sound speed for *MAT_VISCOELASTIC_LOOSE_FABRIC.
\u00a0 Include element number when writing out failure message.
\u00a0
Keyword: *MAT_124 \u00a0
\u00a0 Implement an optional Young’s modulus for compression in
\u00a0 *MAT_PLASTICITY_COMPRESSION_TENSION.
\u00a0
Keyword: *SECTION_SOLID, *MAT_… \u00a0
\u00a0 Improve accuracy of type 13 (pressure-averaged) tetrahedron.
\u00a0
\u00a0 Modify several existing material models for type 13 tetrahedron,
\u00a0 including *mat_015, *mat_098, *mat_106, *mat_224.
\u00a0
Keyword: *MAT_024 \u00a0
\u00a0 Made beam *MAT_PIECEWISE_LINEAR_PLASTCITY plasticity iteration consistent i
\u00a0 with *MAT_PLASTIC_KINEMATIC (*MAT_003).
\u00a0
Keyword: *MAT_NONLOCAL \u00a0
\u00a0 Modify nonlocal failure for thick shells so that if elements are stacked,
\u00a0 averaging will not occur with elements on the top and bottom, only those on
\u00a0 the side.
\u00a0
Keyword: *MAT_… \u00a0
\u00a0 Fix incorrect experimental curve data output to curveplot file for
\u00a0 materials 76, 77, 134, 175, 176, 178 and 276.
\u00a0
Keyword: *MAT_058, *MAT_158 \u00a0
\u00a0 Enable the negative AOPT (*DEFINE_COORDINATE_NODES) option for
\u00a0 *MAT_LAMINATED_COMPOSITE_FABRIC and *MAT_RATE_SENSITIVE_COMPOSITE_FABRIC.
\u00a0
Keyword: *EOS_… \u00a0
\u00a0 Add input check for duplication of EOS ID.
\u00a0
Keyword: *MAT_CRUSHABLE_FOAM \u00a0
\u00a0 Fix instability problem of *MAT_CRUSHABLE_FOAM for plain strain analysis.
\u00a0
Keyword: *MAT_107 \u00a0
\u00a0 Fix in Zerilli-Armstrong law in *MAT_MODIFIED_JOHNSON_COOK
\u00a0
Keyword: *MAT_172 \u00a0
\u00a0 Modify *MAT_CONCRETE_EC2 so that when *INTEGRATION_SHELL or
\u00a0 *PART_COMPOSITE is used, the AOPT-related angle is recalculated for
\u00a0 each integration point.
\u00a0 The standard LS-DYNA treatment is to get the AOPT-related angle from the
\u00a0 first IP made of an orthotropic material, then use the same angle for
\u00a0 subsequent points.
\u00a0
Keyword: Various *MAT_… including *MAT_ADD_EROSION \u00a0
\u00a0 Fix for NUMINT<0 in materials 120, 123, 187, 224, and GISSMO:
\u00a0 solid elements are now deleted directly after 1st IP fails,
\u00a0 i.e., input value of NUMINT is ignored.
\u00a0
Keyword: *MAT_272 \u00a0
\u00a0 Improve *MAT_RHT, including automatic parameter generation.
\u00a0
Keyword: *MAT_072R3 \u00a0
\u00a0 Make updates to *MAT_CONCRETE_DAMAGE_REL3 per KCSE.
\u00a0
Keyword: *MAT_072R3 \u00a0
\u00a0 Implement updates from KCSE for *MAT_CONCRETE_DAMAGE_REL3.
\u00a0
Keyword: *MAT_244 \u00a0
\u00a0
\u00a0 Add option to *MAT_UHS_STEEL for automatic switching between cooling and
\u00a0 heating algorithm based on the temperature slope.
\u00a0
\u00a0 Fix scaling of heat flow due to phase transitions in *MAT_UHS_STEEL.
\u00a0
\u00a0 Add thermal scale factor to *MAT_UHS_STEEL.
\u00a0
\u00a0 Support heating and\/or reheating of *MAT_UHS_STEEL. The heat equation is
\u00a0 taken from Oddy et al (1996) Microstructural Predictions Including
\u00a0 Arbitrary Thermal Historic ReAustinatization And Carbon Segregation Effects.
Keyword: *MAT_098 \u00a0
\u00a0 Fix bug in *MAT_SIMPLIFIED_JOHNSON_COOK for implicit.
\u00a0
Keyword: *MAT_021 \u00a0
\u00a0 Modify *MAT_ORTHOTROPIC_THERMAL so that it works with angles on the
\u00a0 *SECTION_SHELL or *SECTION_TSHELL card to define material directions for
\u00a0 layers.
\u00a0
Keyword: *MAT_USER_DEFINED_MATERIAL_MODELS \u00a0
\u00a0 Fix plane strain and axisymmetric elements when used with orthotropic
\u00a0 user-defined materials.\u00a0\u00a0 This fix affects shell forms 13, 14, 15, 43,
\u00a0 44, 52, 53.\u00a0 The wrong strain and stress transformation was being done.
\u00a0
<\/p>\r\n","protected":false},"excerpt":{"rendered":"