Products: ABAQUS/Standard ABAQUS/Explicit
The translator from NASTRAN to ABAQUS converts certain entities in a NASTRAN input file into their equivalent in ABAQUS.
The NASTRAN data must be in a file with the extension .bdf. 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 BULKFor normal termination, end the NASTRAN input data with the line
ENDDATANASTRAN solution sequences are translated to the ABAQUS procedures listed in Table 3.2.201. The translator attempts to create a history section based on the contents of the case control data in the NASTRAN file.
The INCLUDE command is not supported.
Table 3.2.201 Executive control data.
NASTRAN Statement | ABAQUS 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 3.2.202 Case control data.
NASTRAN Command | Comment |
---|---|
SPC | Selects SPC sets alone or in combinations |
LOAD | Selects individual loads and load combinations |
METHOD | Selects EIGRL, EIGR, or EIGB from bulk data for eigenfrequency extraction and eigenvalue buckling prediction procedures |
SUBCASE | Delimiter for steps or load cases; optional if there is only one step |
TITLE | Echoed as comment at top of input file and for each step |
SUBTITLE | Echoed as comment for the step to which it applies |
LABEL | Used as text following the *STEP option |
DLOAD | Selects dynamic loads from bulk data |
LOADSET | |
FREQUENCY | Selects forcing frequencies from bulk data |
MPC | Selects MPCADD and MPC from bulk data if referenced in the first SUBCASE |
SUPORT1 | Selects SUPORT1 from bulk data |
TSTEP | Selects TSTEP from bulk data |
K2GG | Selects DMIG from bulk data using the matrix name from the first SUBCASE |
K2PP | |
M2GG | |
M2PP | |
TEMPERATURE | Selects nodal temperatures from bulk data |
NASTRAN Data Entry | Comment |
---|---|
PARAM | Ignored 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 |
CDAMP1 | DASHPOT1/DASHPOT2 and *DASHPOT |
CDAMP2 | |
PDAMP | |
CELAS1 | SPRING1/SPRING2 and *SPRING |
CELAS2 | |
PELAS | |
CBUSH | CONN3D2 and *CONNECTOR SECTION |
PBUSH | |
PBUSHT | |
CONM1 | MASS and/or ROTARY INERTIA and/or UEL |
CONM2 | MASS and/or ROTARY INERTIA |
CHEXA | C3D8I/C3D20R/C3D6/C3D15/C3D4/C3D10 and *SOLID SECTION |
CPENTA | |
CTETRA | |
PSOLID | |
CQUAD4 | S4/S3R/S8R/STRI65, and *SHELL SECTION, *SHELL GENERAL SECTION, or *MEMBRANE SECTION. |
CTRIA3 | |
CQUAD8 | |
CTRIA6 | |
CQUADR | |
CTRIAR | |
PSHELL | |
PCOMP | |
PCOMPG | |
CSHEAR | M3D4 and *MEMBRANE SECTION; T3D2 and *SOLID SECTION |
PSHEAR | |
CBAR | B31 and *BEAM SECTION or *BEAM GENERAL SECTION |
CBEAM | |
PBAR | |
PBARL | |
PBEAM | |
PBEAML | |
CROD | T3D2 and *SOLID SECTION |
CONROD | |
PROD | |
CGAP | GAPUNI and *GAP |
PGAP | |
RBAR | *COUPLING or *MPC, TYPE=BEAM |
MAT1 | *ELASTIC, TYPE=ISO; *EXPANSION, TYPE=ISO; and *DENSITY (G is used only for *BEAM GENERAL SECTION) |
MAT2 | When 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; and *DENSITY |
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; and *EXPANSION, TYPE=ANISO or ORTHO. |
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 |
RBE3 | *COUPLING and *DISTRIBUTING; or DCOUP3D and *DISTRIBUTING COUPLING |
SPCADD | Used to combine SPC/SPC1/SPCD data into a new set |
SPC | *BOUNDARY |
SPC1 | |
SPCD | |
LOAD | Used to combine FORCE, MOMENT, etc. data into a new set |
FORCE | *CLOAD |
FORCE1 | |
FORCE2 | |
MOMENT | |
MOMENT1 | |
MOMENT2 | |
PLOAD | *DLOAD |
PLOAD1 | |
PLOAD2 | |
PLOAD4 | |
RFORCE | |
DLOAD | Dynamic 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 | |
TSTEP | Time step size for dynamic and modal dynamic procedures |
EIGB | *BUCKLE |
EIGR | *FREQUENCY |
EIGRL | |
EIGC | *COMPLEX FREQUENCY |
TABDMP1 | *MODAL DAMPING |
FREQ | Forcing frequencies for steady-state dynamic procedures |
FREQ1 | |
FREQ2 | |
MPCADD | *EQUATION |
MPC | |
SUPORT | *INERTIA RELIEF and *BOUNDARY |
SUPORT1 | |
DMIG | *MATRIX INPUT and *MATRIX ASSEMBLE |
GENEL | *USER ELEMENT, LINEAR and *MATRIX, TYPE=STIFFNESS |
abaqus fromnastran | job=job-name |
[input=input-file] [wtmass_fixup={OFF | ON}] [loadcases={OFF | ON}] [pbar_zero_reset=[small_real_number]] [distribution={OFF | ON}] [surface_based_coupling={OFF | ON}] [cbar=2_node_beam_element] [cquad4=4_node_shell_element] [chexa=8_node_brick_element] [ctetra=10_node_tetrahedron_element] |
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.
This option is used to specify the name of the file containing the NASTRAN data if it is different from job-name.
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}
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}
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 × 1020 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
NASTRAN shell elements may have their orientations and offsets defined on the element connectivity. By default, all elements that reference a single PSHELL translate to a single *SHELL SECTION or *SHELL GENERAL SECTION in ABAQUS and the variation in their properties will be defined using the *ELEMENT PROPERTIES and *DISTRIBUTION keywords. If distribution=OFF, a separate *SHELL SECTION or *SHELL GENERAL SECTION is created for each element set that has a unique combination of orientation, offset, and/or thickness.
This option can be defined in the ABAQUS environment file as follows:
fromnastran_distribution={OFF | ON}
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}
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
This option is used to define the 4-node shell that is created from CQUAD4 elements. The default is S4. 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
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
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