3.2.30 Translating Nastran bulk data files to Abaqus input files

Products: Abaqus/Standard  Abaqus/Explicit  

Overview

The translator from Nastran to Abaqus converts certain entities in a Nastran input file into their equivalent in Abaqus.

Using the translator

The Nastran data must be in a file with the extension .bdf, .dat, .nas, .nastran, .blk, or .bulk. The Nastran data entries that are translated are listed in the tables below. Other valid Nastran data are skipped over and noted in the log file.

The translator is designed to translate a complete Nastran input file. If only bulk data are present, the first two lines in the file should be the terminators for the executive control and case control sections, namely:

CEND 
BEGIN BULK
For normal termination, end the Nastran input data with the line
ENDDATA
Nastran solution sequences are translated to the Abaqus procedures listed in Table 3.2.30–1. The translator attempts to create a history section based on the contents of the case control data in the Nastran file.

Summary of Nastran entities translated

Table 3.2.30–1 Executive control data.

Nastran StatementAbaqus Equivalent
SOL 
1 (STATICS1)*STATIC
24 (STATICS)
101(SESTATIC)
106 (NLSTATIC)
3 (MODES)*FREQUENCY
25 (OLDMODES)
103 (SEMODES)
5 (BUCKLING)*BUCKLE
105 (SEBUCKL)
26 (DFREQ)*STEADY STATE DYNAMICS, DIRECT
108 (SEDFREQ)
27 (DTRAN)*DYNAMIC
109 (SEDTRAN)
107(SEDCEIG)*COMPLEX FREQUENCY
110 (SEMCEIG)
30 (DFREQ)*FREQUENCY and *STEADY STATE DYNAMICS
111 (SEMFREQ)
31 (MTRAN)*FREQUENCY and *MODAL DYNAMIC
112 (SEMTRAN)

Table 3.2.30–2 Case control data.

Nastran CommandComment
SPCSelects SPC sets alone or in combinations
LOADSelects individual loads and load combinations
METHODSelects EIGRL, EIGR, or EIGB from bulk data for eigenfrequency extraction and eigenvalue buckling prediction procedures
SUBCASEDelimiter for steps or load cases; optional if there is only one step
TITLEEchoed as comment at top of input file and for each step
SUBTITLEEchoed as comment for the step to which it applies
LABELUsed as text following the *STEP option
DLOADSelects dynamic loads from bulk data
LOADSET
FREQUENCYSelects forcing frequencies from bulk data
MPCSelects MPCADD and MPC from bulk data if referenced in the first SUBCASE
SUPORT1Selects SUPORT1 from bulk data
TSTEPSelects TSTEP from bulk data
K2GGSelects DMIG from bulk data using the matrix name from the first SUBCASE
K2PP
M2GG
M2PP
B2GG
B2PP
K42GG
TEMPERATURESelects nodal temperatures from bulk data
SETSelects nodal quantities for output
DISPLACEMENT
VELOCITY
ACCELERATION
SPCFORCES
PRESSURE

Table 3.2.30–3 Bulk data.

Nastran Data EntryComment
PARAMIgnored except for:
1. WTMASS, which can be used to modify density, mass, and rotary inertia values if the wtmass_fixup command line parameter is used
2. INREL, which if equal to –1 or –2 will create inertia relief loads
3. G, which is translated to *GLOBAL DAMPING, STRUCTURAL, FIELD=MECHANICAL
4. GFL, which is translated to *GLOBAL DAMPING, STRUCTURAL, FIELD=ACOUSTIC
CDAMP1DASHPOT1/DASHPOT2 and *DASHPOT
CDAMP2
PDAMP
PDAMPT
CELAS1SPRING1/SPRING2 and *SPRING
(CELAS2 at SPOINTs are translated to *MATRIX INPUT, stiffness, and/or structural damping terms.)
CELAS2
PELAS
PELAST
CMASS2*MATRIX INPUT mass terms
CBUSHCONN3D2 and *CONNECTOR SECTION
PBUSH
PBUSHT
CWELD*FASTENER and *FASTENER PROPERTY
PWELD
CONM1MASS and/or ROTARY INERTIA and/or UEL
CONM2MASS and/or ROTARY INERTIA
CHEXAC3D8I/C3D20R/C3D6/C3D15/C3D4/C3D10 and *SOLID SECTION
CPENTA
CTETRA
PSOLID
PLSOLID
CQUAD4S4/S3R/S8R/STRI65, and *SHELL SECTION, *SHELL GENERAL SECTION, or *MEMBRANE SECTION.
CTRIA3
CQUAD8
CTRIA6
CQUADR
CTRIAR
PSHELL
PCOMP
PCOMPG
CSHEAR*USER ELEMENT, LINEAR and *MATRIX, TYPE=STIFFNESS and TYPE=MASS
PSHEAR
CBARB31 and *BEAM SECTION or *BEAM GENERAL SECTION
CBEAM
PBAR
PBARL
PBEAM
PBEAML
CRODT3D2 and *SOLID SECTION
CONROD
PROD
CGAPGAPUNI and *GAP
PGAP
RBAR*COUPLING or *MPC, type BEAM
MAT1*ELASTIC, TYPE=ISO; *EXPANSION, TYPE=ISO; *DENSITY; and *DAMPING (G is used only for *BEAM GENERAL SECTION)
MAT2When used alone in a PSHELL, MAT2 is translated to *ELASTIC, TYPE=LAMINA or *ELASTIC, TYPE=ANISOTROPIC. When used in combination with other materials, the coefficients relating midsurface strains and curvatures to section forces and moments are computed and entered following the *SHELL GENERAL SECTION option.
MAT8*ELASTIC, TYPE=LAMINA; *EXPANSION, TYPE=ORTHO; *DENSITY; and *DAMPING
MAT9*ELASTIC, TYPE=ANISOTROPIC unless the data are found to be orthotropic, in which case the data are analyzed to create *ELASTIC, TYPE=ENGINEERING CONSTANTS. Also *DENSITY; *EXPANSION, TYPE=ANISO or ORTHO; and *DAMPING.
MAT10*ACOUSTIC MEDIUM and *DENSITY
ACMODL*TIE between a *SURFACE, TYPE=ELEMENT defining the exterior surfaces of all acoustic solid elements and a *SURFACE, TYPE=NODE defined by the SET1 referenced by the SSID.
NSM*NONSTRUCTURAL MASS
NSM1
NSML
NSML1
NSMADD
GRID*NODE and *SYSTEM
CORD1R*SYSTEM for nodes; *TRANSFORM if referred to on GRID; *ORIENTATION for some elements
CORD1C
CORD1S
CORD2R
CORD2C
CORD2S
RBE2*COUPLING and *KINEMATIC; or *KINEMATIC COUPLING
(If the RBE2 has only two nodes and neither node has rotational stiffness, the RBE2 is translated to *MPC, type LINK)
RBE3*COUPLING and *DISTRIBUTING; or DCOUP3D and *DISTRIBUTING COUPLING
SPCADDUsed to combine SPC/SPC1/SPCD data into a new set
SPC*BOUNDARY
SPC1
SPCD
LOADUsed to combine FORCE, MOMENT, etc. data into a new set
FORCE*CLOAD
FORCE1
FORCE2
MOMENT
MOMENT1
MOMENT2
PLOAD*DLOAD
PLOAD1
PLOAD2
PLOAD4
RFORCE
DLOADDynamic loads as functions of time or frequency
DAREA
LSEQ
RLOAD1
RLOAD2
TLOAD1
TABLED1
TABLED2
TABLED4
DELAY
DPHASE
TEMP*INITIAL CONDITIONS, TYPE=TEMPERATURE and *TEMPERATURE
TEMPD
TSTEPTime step size for dynamic and modal dynamic procedures
EIGB*BUCKLE
EIGR*FREQUENCY
EIGRL
EIGC*COMPLEX FREQUENCY
TABDMP1*MODAL DAMPING
FREQForcing frequencies for steady-state dynamic procedures
FREQ1
FREQ2
FREQ3
FREQ4
FREQ5
MPCADD*EQUATION
MPC
SUPORT*INERTIA RELIEF and *BOUNDARY
SUPORT1
DMIG*MATRIX INPUT and *MATRIX ASSEMBLE
GENEL *USER ELEMENT, LINEAR and *MATRIX, TYPE=STIFFNESS
PLOTEL T3D2 (Ignored unless the command line option plotel=ON.)

Command summary

abaqus fromnastran
job=job-name
 
[input=input-file]
[wtmass_fixup={OFF |  ON}]
[loadcases={OFF |  ON}]
[pbar_zero_reset=[small-real-number]]
[distribution={OFF |  preservePID | ON}]
[beam_offset_coupling={OFF |  ON}]
[cbar=2-node-beam-element]
[cquad4=4-node-shell-element]
[chexa=8-node-brick-element]
[ctetra=10-node-tetrahedron-element]
[plotel={OFF | ON}]
[cdh_weld={OFF | RIGID | COMPLIANT}]

Command line options

job

This option is used to specify the name of the Abaqus input file to be output by the translator. It is also the default name of the file containing the Nastran data. Diagnostics created by the translator will be written to a file named job-name.log.

input

This option is used to specify the name of the file containing the Nastran data if it is different from job-name.

wtmass_fixup

If wtmass_fixup=ON, the value on the Nastran data line PARAM, WTMASS, value is used as a multiplier for all density, mass, and rotary inertia values created in the Abaqus input file.

This option can be defined in the Abaqus environment file as follows:

fromnastran_wtmass_fixup={OFF | ON}

loadcases

By default, each SUBCASE is translated to a *STEP option in Abaqus. If loadcases=ON, this behavior is altered for linear static analyses: each SUBCASE is translated to a *LOAD CASE option, and all such *LOAD CASE options are grouped in a single *STEP option.

This option can be defined in the Abaqus environment file as follows:

fromnastran_loadcases={OFF | ON}

pbar_zero_reset

Nastran allows beams to have zero values for cross-sectional area or moments of inertia; Abaqus does not. Set this option equal to a small real number to reset any zero values for A, , , or J to the specified small real number. If this option is omitted or present without a value, the default value of 1.0 × 10–20 is used in place of the zeros. To retain the zeros in the translated Abaqus input file, set pbar_zero_reset=0.

This option can be defined in the Abaqus environment file as follows:

fromnastran_pbar_zero_reset=small-real-number

distribution

This option determines how shell and membrane sections in Nastran data are translated to Abaqus. If distribution=OFF, a separate section is created for each combination of orientation, material offset, and/or thickness. If distribution=preservePID or ON, element orientations and offsets are written using the *DISTRIBUTION option. If distribution=preservePID, an Abaqus section is created corresponding to each PSHELL or PCOMP property ID. If distribution=ON, a single Abaqus section is created for all homogeneous elements referencing the same material.

This option can be defined in the Abaqus environment file as follows:

fromnastran_distribution={OFF | preservePID | ON}

surface_based_coupling

Certain Nastran rigid elements have more than one equivalent in Abaqus. If surface_based_coupling=ON, RBE2 and RBE3 elements translate to *COUPLING with the appropriate parameters. Otherwise, RBE2 elements translate to *KINEMATIC COUPLING and RBE3 elements translate to *DISTRIBUTING COUPLING. This translation behavior also applies to “implied” RBE2-type rigid elements used for offsets on CBAR, CBEAM, and CONM2 elements.

For input files created with surface_based_coupling=ON, the translated elements can be visualized and manipulated in Abaqus/CAE. However, large numbers of these elements may cause slower performance.

This option can be defined in the Abaqus environment file as follows:

fromnastran_surface_based_coupling={OFF | ON}

beam_offset_coupling

If beam_offset_coupling=ON, beam element offsets are translated by creating new nodes at the offset locations, changing the beam connectivity to the new nodes, and rigidly coupling the new and original nodes.

If beam_offset_coupling=OFF, beam element offsets are translated to the *CENTROID and *SHEAR CENTER options, which are suboptions of the *BEAM GENERAL SECTION option.

The setting for this parameter is ignored if the beam element references a PBARL or PBEAML property or if the beam offset has a significant component in the direction of the beam axis. In these situations the beam offsets are always translated as if beam_offset_coupling=ON.

This option can be defined in the Abaqus environment file as follows:

fromnastran_beam_offset_coupling={OFF | ON}

beam_orientation_vector

If beam_orientation_vector=OFF, beam cross-section orientations are translated by creating new nodes at the tips of vectors defining the first principal direction of the cross-section and changing the beam connectivity to the new nodes.

If beam_orientation_vector=ON, beam cross-sections are translated by defining vectors on the *BEAM SECTION and *BEAM GENERAL SECTION options.

This option can be defined in the Abaqus environment file as follows:

fromnastran_beam_orientation_vector={OFF | ON}

cbar

This option is used to define the 2-node beam that is created from CBAR and CBEAM elements. The default is B31.

This option can be defined in the Abaqus environment file as follows:

fromnastran_cbar=2-node-beam-element

cquad4

This option is used to define the 4-node shell that is created from CQUAD4 elements. The default is S4R. If a reduced-integration element is chosen, the enhanced hourglass formulation is applied automatically.

This option can be defined in the Abaqus environment file as follows:

fromnastran_cquad4=4-node-shell-element

chexa

This option is used to define the 8-node brick that is created from CHEXA elements. The default is C3D8I. If a reduced-integration element is chosen, the enhanced hourglass formulation is applied automatically.

This option can be defined in the Abaqus environment file as follows:

fromnastran_chexa=8-node-brick-element

ctetra

This option is used to define the 10-node tetrahedron that is created from CTETRA elements. The default is C3D10.

This option can be defined in the Abaqus environment file as follows:

fromnastran_ctetra=10-node-tetrahedron-element

plotel

By default, PLOTEL elements are not translated. If plotel=ON, PLOTEL elements are translated to T3D2 truss elements in an element set named PLOTEL_TRUSSES. The cross-sectional area of the trusses is 1.0 × 10–20, and the material has a Young's modulus, E, equal to 1.0.

cdh_weld

By default, CHEXA elements with RBE3 elements at all eight corner nodes are translated to the type of 8-node element specified in the chexa parameter. If cdh_weld=RIGID, CHEXA elements with RBE3 elements at all eight corner nodes are translated to rigid fasteners in Abaqus. If cdh_weld=COMPLIANT, CHEXA elements with RBE3 elements at all eight corner nodes are translated to compliant fasteners in Abaqus.

Your query was poorly formed. Please make corrections.


3.2.30 Translating Nastran bulk data files to Abaqus input files

Products: Abaqus/Standard  Abaqus/Explicit  

Your query was poorly formed. Please make corrections.

Overview

The translator from Nastran to Abaqus converts certain entities in a Nastran input file into their equivalent in Abaqus.

Your query was poorly formed. Please make corrections.
Your query was poorly formed. Please make corrections.

Using the translator

The Nastran data must be in a file with the extension .bdf, .dat, .nas, .nastran, .blk, or .bulk. The Nastran data entries that are translated are listed in the tables below. Other valid Nastran data are skipped over and noted in the log file.

The translator is designed to translate a complete Nastran input file. If only bulk data are present, the first two lines in the file should be the terminators for the executive control and case control sections, namely:

CEND 
BEGIN BULK
For normal termination, end the Nastran input data with the line
ENDDATA
Nastran solution sequences are translated to the Abaqus procedures listed in Table 3.2.30–1. The translator attempts to create a history section based on the contents of the case control data in the Nastran file.

Your query was poorly formed. Please make corrections.
Your query was poorly formed. Please make corrections.

Summary of Nastran entities translated

Table 3.2.30–1 Executive control data.

Nastran StatementAbaqus Equivalent
SOL 
1 (STATICS1)*STATIC
24 (STATICS)
101(SESTATIC)
106 (NLSTATIC)
3 (MODES)*FREQUENCY
25 (OLDMODES)
103 (SEMODES)
5 (BUCKLING)*BUCKLE
105 (SEBUCKL)
26 (DFREQ)*STEADY STATE DYNAMICS, DIRECT
108 (SEDFREQ)
27 (DTRAN)*DYNAMIC
109 (SEDTRAN)
107(SEDCEIG)*COMPLEX FREQUENCY
110 (SEMCEIG)
30 (DFREQ)*FREQUENCY and *STEADY STATE DYNAMICS
111 (SEMFREQ)
31 (MTRAN)*FREQUENCY and *MODAL DYNAMIC
112 (SEMTRAN)

Table 3.2.30–2 Case control data.

Nastran CommandComment
SPCSelects SPC sets alone or in combinations
LOADSelects individual loads and load combinations
METHODSelects EIGRL, EIGR, or EIGB from bulk data for eigenfrequency extraction and eigenvalue buckling prediction procedures
SUBCASEDelimiter for steps or load cases; optional if there is only one step
TITLEEchoed as comment at top of input file and for each step
SUBTITLEEchoed as comment for the step to which it applies
LABELUsed as text following the *STEP option
DLOADSelects dynamic loads from bulk data
LOADSET
FREQUENCYSelects forcing frequencies from bulk data
MPCSelects MPCADD and MPC from bulk data if referenced in the first SUBCASE
SUPORT1Selects SUPORT1 from bulk data
TSTEPSelects TSTEP from bulk data
K2GGSelects DMIG from bulk data using the matrix name from the first SUBCASE
K2PP
M2GG
M2PP
B2GG
B2PP
K42GG
TEMPERATURESelects nodal temperatures from bulk data
SETSelects nodal quantities for output
DISPLACEMENT
VELOCITY
ACCELERATION
SPCFORCES
PRESSURE

Table 3.2.30–3 Bulk data.

Nastran Data EntryComment
PARAMIgnored except for:
1. WTMASS, which can be used to modify density, mass, and rotary inertia values if the wtmass_fixup command line parameter is used
2. INREL, which if equal to –1 or –2 will create inertia relief loads
3. G, which is translated to *GLOBAL DAMPING, STRUCTURAL, FIELD=MECHANICAL
4. GFL, which is translated to *GLOBAL DAMPING, STRUCTURAL, FIELD=ACOUSTIC
CDAMP1DASHPOT1/DASHPOT2 and *DASHPOT
CDAMP2
PDAMP
PDAMPT
CELAS1SPRING1/SPRING2 and *SPRING
(CELAS2 at SPOINTs are translated to *MATRIX INPUT, stiffness, and/or structural damping terms.)
CELAS2
PELAS
PELAST
CMASS2*MATRIX INPUT mass terms
CBUSHCONN3D2 and *CONNECTOR SECTION
PBUSH
PBUSHT
CWELD*FASTENER and *FASTENER PROPERTY
PWELD
CONM1MASS and/or ROTARY INERTIA and/or UEL
CONM2MASS and/or ROTARY INERTIA
CHEXAC3D8I/C3D20R/C3D6/C3D15/C3D4/C3D10 and *SOLID SECTION
CPENTA
CTETRA
PSOLID
PLSOLID
CQUAD4S4/S3R/S8R/STRI65, and *SHELL SECTION, *SHELL GENERAL SECTION, or *MEMBRANE SECTION.
CTRIA3
CQUAD8
CTRIA6
CQUADR
CTRIAR
PSHELL
PCOMP
PCOMPG
CSHEAR*USER ELEMENT, LINEAR and *MATRIX, TYPE=STIFFNESS and TYPE=MASS
PSHEAR
CBARB31 and *BEAM SECTION or *BEAM GENERAL SECTION
CBEAM
PBAR
PBARL
PBEAM
PBEAML
CRODT3D2 and *SOLID SECTION
CONROD
PROD
CGAPGAPUNI and *GAP
PGAP
RBAR*COUPLING or *MPC, type BEAM
MAT1*ELASTIC, TYPE=ISO; *EXPANSION, TYPE=ISO; *DENSITY; and *DAMPING (G is used only for *BEAM GENERAL SECTION)
MAT2When used alone in a PSHELL, MAT2 is translated to *ELASTIC, TYPE=LAMINA or *ELASTIC, TYPE=ANISOTROPIC. When used in combination with other materials, the coefficients relating midsurface strains and curvatures to section forces and moments are computed and entered following the *SHELL GENERAL SECTION option.
MAT8*ELASTIC, TYPE=LAMINA; *EXPANSION, TYPE=ORTHO; *DENSITY; and *DAMPING
MAT9*ELASTIC, TYPE=ANISOTROPIC unless the data are found to be orthotropic, in which case the data are analyzed to create *ELASTIC, TYPE=ENGINEERING CONSTANTS. Also *DENSITY; *EXPANSION, TYPE=ANISO or ORTHO; and *DAMPING.
MAT10*ACOUSTIC MEDIUM and *DENSITY
ACMODL*TIE between a *SURFACE, TYPE=ELEMENT defining the exterior surfaces of all acoustic solid elements and a *SURFACE, TYPE=NODE defined by the SET1 referenced by the SSID.
NSM*NONSTRUCTURAL MASS
NSM1
NSML
NSML1
NSMADD
GRID*NODE and *SYSTEM
CORD1R*SYSTEM for nodes; *TRANSFORM if referred to on GRID; *ORIENTATION for some elements
CORD1C
CORD1S
CORD2R
CORD2C
CORD2S
RBE2*COUPLING and *KINEMATIC; or *KINEMATIC COUPLING
(If the RBE2 has only two nodes and neither node has rotational stiffness, the RBE2 is translated to *MPC, type LINK)
RBE3*COUPLING and *DISTRIBUTING; or DCOUP3D and *DISTRIBUTING COUPLING
SPCADDUsed to combine SPC/SPC1/SPCD data into a new set
SPC*BOUNDARY
SPC1
SPCD
LOADUsed to combine FORCE, MOMENT, etc. data into a new set
FORCE*CLOAD
FORCE1
FORCE2
MOMENT
MOMENT1
MOMENT2
PLOAD*DLOAD
PLOAD1
PLOAD2
PLOAD4
RFORCE
DLOADDynamic loads as functions of time or frequency
DAREA
LSEQ
RLOAD1
RLOAD2
TLOAD1
TABLED1
TABLED2
TABLED4
DELAY
DPHASE
TEMP*INITIAL CONDITIONS, TYPE=TEMPERATURE and *TEMPERATURE
TEMPD
TSTEPTime step size for dynamic and modal dynamic procedures
EIGB*BUCKLE
EIGR*FREQUENCY
EIGRL
EIGC*COMPLEX FREQUENCY
TABDMP1*MODAL DAMPING
FREQForcing frequencies for steady-state dynamic procedures
FREQ1
FREQ2
FREQ3
FREQ4
FREQ5
MPCADD*EQUATION
MPC
SUPORT*INERTIA RELIEF and *BOUNDARY
SUPORT1
DMIG*MATRIX INPUT and *MATRIX ASSEMBLE
GENEL *USER ELEMENT, LINEAR and *MATRIX, TYPE=STIFFNESS
PLOTEL T3D2 (Ignored unless the command line option plotel=ON.)

Your query was poorly formed. Please make corrections.
Your query was poorly formed. Please make corrections.

Command summary

abaqus fromnastran
job=job-name
 
[input=input-file]
[wtmass_fixup={OFF |  ON}]
[loadcases={OFF |  ON}]
[pbar_zero_reset=[small-real-number]]
[distribution={OFF |  preservePID | ON}]
[beam_offset_coupling={OFF |  ON}]
[cbar=2-node-beam-element]
[cquad4=4-node-shell-element]
[chexa=8-node-brick-element]
[ctetra=10-node-tetrahedron-element]
[plotel={OFF | ON}]
[cdh_weld={OFF | RIGID | COMPLIANT}]

Your query was poorly formed. Please make corrections.
Your query was poorly formed. Please make corrections.

Command line options

job

This option is used to specify the name of the Abaqus input file to be output by the translator. It is also the default name of the file containing the Nastran data. Diagnostics created by the translator will be written to a file named job-name.log.

input

This option is used to specify the name of the file containing the Nastran data if it is different from job-name.

wtmass_fixup

If wtmass_fixup=ON, the value on the Nastran data line PARAM, WTMASS, value is used as a multiplier for all density, mass, and rotary inertia values created in the Abaqus input file.

This option can be defined in the Abaqus environment file as follows:

fromnastran_wtmass_fixup={OFF | ON}

loadcases

By default, each SUBCASE is translated to a *STEP option in Abaqus. If loadcases=ON, this behavior is altered for linear static analyses: each SUBCASE is translated to a *LOAD CASE option, and all such *LOAD CASE options are grouped in a single *STEP option.

This option can be defined in the Abaqus environment file as follows:

fromnastran_loadcases={OFF | ON}

pbar_zero_reset

Nastran allows beams to have zero values for cross-sectional area or moments of inertia; Abaqus does not. Set this option equal to a small real number to reset any zero values for A, , , or J to the specified small real number. If this option is omitted or present without a value, the default value of 1.0 × 10–20 is used in place of the zeros. To retain the zeros in the translated Abaqus input file, set pbar_zero_reset=0.

This option can be defined in the Abaqus environment file as follows:

fromnastran_pbar_zero_reset=small-real-number

distribution

This option determines how shell and membrane sections in Nastran data are translated to Abaqus. If distribution=OFF, a separate section is created for each combination of orientation, material offset, and/or thickness. If distribution=preservePID or ON, element orientations and offsets are written using the *DISTRIBUTION option. If distribution=preservePID, an Abaqus section is created corresponding to each PSHELL or PCOMP property ID. If distribution=ON, a single Abaqus section is created for all homogeneous elements referencing the same material.

This option can be defined in the Abaqus environment file as follows:

fromnastran_distribution={OFF | preservePID | ON}

surface_based_coupling

Certain Nastran rigid elements have more than one equivalent in Abaqus. If surface_based_coupling=ON, RBE2 and RBE3 elements translate to *COUPLING with the appropriate parameters. Otherwise, RBE2 elements translate to *KINEMATIC COUPLING and RBE3 elements translate to *DISTRIBUTING COUPLING. This translation behavior also applies to “implied” RBE2-type rigid elements used for offsets on CBAR, CBEAM, and CONM2 elements.

For input files created with surface_based_coupling=ON, the translated elements can be visualized and manipulated in Abaqus/CAE. However, large numbers of these elements may cause slower performance.

This option can be defined in the Abaqus environment file as follows:

fromnastran_surface_based_coupling={OFF | ON}

beam_offset_coupling

If beam_offset_coupling=ON, beam element offsets are translated by creating new nodes at the offset locations, changing the beam connectivity to the new nodes, and rigidly coupling the new and original nodes.

If beam_offset_coupling=OFF, beam element offsets are translated to the *CENTROID and *SHEAR CENTER options, which are suboptions of the *BEAM GENERAL SECTION option.

The setting for this parameter is ignored if the beam element references a PBARL or PBEAML property or if the beam offset has a significant component in the direction of the beam axis. In these situations the beam offsets are always translated as if beam_offset_coupling=ON.

This option can be defined in the Abaqus environment file as follows:

fromnastran_beam_offset_coupling={OFF | ON}

beam_orientation_vector

If beam_orientation_vector=OFF, beam cross-section orientations are translated by creating new nodes at the tips of vectors defining the first principal direction of the cross-section and changing the beam connectivity to the new nodes.

If beam_orientation_vector=ON, beam cross-sections are translated by defining vectors on the *BEAM SECTION and *BEAM GENERAL SECTION options.

This option can be defined in the Abaqus environment file as follows:

fromnastran_beam_orientation_vector={OFF | ON}

cbar

This option is used to define the 2-node beam that is created from CBAR and CBEAM elements. The default is B31.

This option can be defined in the Abaqus environment file as follows:

fromnastran_cbar=2-node-beam-element

cquad4

This option is used to define the 4-node shell that is created from CQUAD4 elements. The default is S4R. If a reduced-integration element is chosen, the enhanced hourglass formulation is applied automatically.

This option can be defined in the Abaqus environment file as follows:

fromnastran_cquad4=4-node-shell-element

chexa

This option is used to define the 8-node brick that is created from CHEXA elements. The default is C3D8I. If a reduced-integration element is chosen, the enhanced hourglass formulation is applied automatically.

This option can be defined in the Abaqus environment file as follows:

fromnastran_chexa=8-node-brick-element

ctetra

This option is used to define the 10-node tetrahedron that is created from CTETRA elements. The default is C3D10.

This option can be defined in the Abaqus environment file as follows:

fromnastran_ctetra=10-node-tetrahedron-element

plotel

By default, PLOTEL elements are not translated. If plotel=ON, PLOTEL elements are translated to T3D2 truss elements in an element set named PLOTEL_TRUSSES. The cross-sectional area of the trusses is 1.0 × 10–20, and the material has a Young's modulus, E, equal to 1.0.

cdh_weld

By default, CHEXA elements with RBE3 elements at all eight corner nodes are translated to the type of 8-node element specified in the chexa parameter. If cdh_weld=RIGID, CHEXA elements with RBE3 elements at all eight corner nodes are translated to rigid fasteners in Abaqus. If cdh_weld=COMPLIANT, CHEXA elements with RBE3 elements at all eight corner nodes are translated to compliant fasteners in Abaqus.

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