| Element Type | Supported Elements |
| Three-dimensional continuum | C3D4, C3D4H, C3D4T, C3D6, C3D6H, C3D6T, C3D8, C3D8H, C3D8HT, C3D8I, C3D8IH, C3D8R, C3D8RH, C3D8RHT, C3D8RT, C3D8S, C3D8HS, C3D8T, Q3D4, Q3D6, Q3D8, Q3D8H, Q3D8R, Q3D8RH |
| C3D10, C3D10H, C3D10HS, C3D10M, C3D10MH, C3D10MHT, C3D10MT, C3D15, C3D15H, C3D15V, C3D15VH, C3D20, C3D20H, C3D20HT, C3D20R, C3D20RHT, C3D20RT, C3D20T, C3D27, C3D27H, C3D27RH, Q3D10M, Q3D10MH, Q3D20, Q3D20H, Q3D20R, Q3D20RH |
| Axisymmetric continuum | CAX3, CAX3H, CAX3T, CAX4, CAX4H, CAX4HT, CAX4I, CAX4IH, CAX4R, CAX4RH, CAX4RHT, CAX4RT, CAX4T |
| CAX6, CAX6M, CAX6MH, CAX6MHT, CAX6MT, CAX8, CAX8H, CAX8HT, CAX8R, CAX8RH, CAX8RHT, CAX8RT, CAX8T |
| Membrane | M3D3, M3D4R |
| Two-dimensional rigid | R2D2 |
| Three-dimensional rigid | R3D3, R3D4 |
| Axisymmetric rigid | RAX2 |
| Three-dimensional shell | S4R, S3R, S4RT, S3RT, S4T, S3T |
| Axisymmetric shell | SAX1 |
| Continuum shell | SC6RT, SC8RT |
| Surface | SFM3D3, SFM3D4R |
| Two-dimensional truss | T2D2, T2D2T |
| Three-dimensional truss | T3D2, T3D2T |
| Cohesive | COH2D4, COHAX4, COH3D6, COH3D8 |
| Inertial | MASS, ROTARYI |
The following element types cannot be imported:
• Acoustic elements
• Axisymmetric-asymmetric continuum and shell elements
• Beam elements
• Connector elements
• Coupled thermal-electrical elements
• Diffusive heat transfer/mass diffusion elements and forced convection/diffusion elements
• Generalized plane strain elements
• Gasket elements
• Heat capacitance elements
• Infinite elements
• Piezoelectric elements
• Special-purpose elements
• Substructures
• User-defined elements
In addition, the following restrictions apply to the import capability:
• Rebars defined using rebar layers (“Defining reinforcement,” Section 2.2.3) are imported provided the underlying elements are also imported. Rebar reinforcements defined using the embedded element technique (“Embedded elements,” Section 35.4.1) are imported if the host and embedded elements used in this definition are also imported. Rebars defined as an element property (“Defining rebar as an element property,” Section 2.2.4) cannot be imported.
• A rigid body containing both deformable and rigid elements cannot be imported. A rigid body that includes rigid elements is imported when the element set used to define the rigid body is specified for import. A rigid body that includes deformable elements is imported when the element set used to define the rigid body is specified for import. The imported rigid body definition is overwritten if it is respecified using the same element set. When the model is defined in terms of an assembly of part instances, the reference node of an imported rigid body must belong to an imported instance.
• When a rigid body is imported, any associated data such as pin node sets and tie node sets are part of the imported definition. However, these sets as imported contain only those nodes that are connected to the imported elements.
# Constraints
Most types of kinematic constraints specified in the original analysis are not imported and must be defined again in the import analysis; however, surface-based tie constraints are imported by default. See “Kinematic constraints: overview,” Section 35.1.1, for a discussion of the various types of kinematic constraints.
# Interactions
The various aspects of most surface-based mechanical contact definitions (including the surface, contact pair, and contact property definitions) can be imported. Thermal interactions, electrical interactions, and pore fluid surface interactions cannot be imported. Certain types of mechanical contact aspects—pressure, penetration loads, and debonded surfaces—cannot be imported. The most commonly used mechanical contact aspects—pressure-overclosure behavior, frictional behavior, and damping—can be imported.
The ability to import element-based and node-based surfaces is determined by whether or not the underlying elements and nodes defining these surfaces are imported. If the underlying elements or nodes of a surface are not imported, that surface will not be imported. If only some of the underlying nodes or elements used in the original definition of the surface are imported, only that part of the surface corresponding to the imported elements will be imported. Rigid surface definitions are imported when the associated slave surface is also imported. Contact pair definitions are imported provided that all the slave and master surfaces used in the original definition of the contact pair are also imported.
Contact conditions modeled with contact elements will be ignored during the transfer process.
The contact state associated with a stress/displacement analysis is imported if the material state is imported. If the reference configuration is updated, the accumulated contact strains will be set to zero. The contact state associated with thermal, electrical, or pore fluid surface interactions is not imported. The contact state associated with a crack propagation analysis is not imported; initially bonded contact surface definitions are not transferred. If a contact pair was inactive in the step from which the import was done due to the use of contact pair removal (see “Removing and reactivating contact pairs” in “Defining contact pairs in Abaqus/Standard,” Section 36.3.1), it must be deactivated again in the first step of the import analysis.
Additional contact information can be defined in the import analysis by specifying new surfaces, contact pairs, and interactions. New contact pair definitions can use the imported surface interaction definitions.
For a detailed description of the contact capabilities in Abaqus/Standard, refer to “Contact interaction analysis: overview,” Section 36.1.1.
# Output
Output can be requested for an import analysis in the same way as for an analysis in which the results are not imported. Output requests in the original analysis are not transferred to the import analysis; output requests in the import analysis have to be respecified. The output variables available in Abaqus/Standard are listed in “Abaqus/Standard output variable identifiers,” Section 4.2.1.
The values of the following material point output variables will be continuous in an import analysis when the material state is imported: stress, equivalent plastic strain (PEEQ), and solution-dependent state variables (SDV) for UMAT.
If the reference configuration is not updated, the displacements, strains, whole element variables, section variables, and energy quantities will be reported relative to the original configuration.
If the reference configuration is updated, displacements, strains, whole element variables, section variables, and energy quantities will not be continuous in an import analysis and will be reported relative to the updated reference configuration.
Time and step number will not be continuous between the original and the import analyses if the reference configuration is updated. Time and step number will be continuous only if the reference configuration is not updated.
# Limitations
The import capability has the following known limitations. Where applicable, details are given in the relevant sections.
• The same release of Abaqus/Standard must be run on computers that are binary compatible.
• The capability is not available for fluid elements; infinite elements; and spring, dashpot, and connector elements. See the discussion on “Elements” earlier in this section for further details.
• Surfaces are not imported when the model is defined as an assembly of part instances.
• All elements and nodes must be included in at least one set in the original analysis when importing part instances.
• The contact state associated with thermal, electrical, and pore fluid surface interactions is not imported; the contact state associated with crack propagation is not imported.
• General contact definitions are not imported.
• If the material state is imported, only stresses will be imported for material models other than those defined by linear elasticity, hyperelasticity, hyperfoam, viscoelasticity, Mises plasticity, and damage for cohesive elements. See “Importing the material state” in “Transferring results between Abaqus analyses: overview,” Section 9.2.1, for details.
• Loads, boundary conditions, multi-point constraints, and equations are not imported.
• Kinematic and distributing coupling constraints are not imported. In addition, the reference node of a coupling constraint will not be imported unless the reference node is part of another element definition that is imported.
• When you import part instances individually from a previous analysis that was defined as an assembly of part instances, reference nodes associated with rigid body or coupling constraints defined on the imported instances will not be available in the import analysis for load or boundary condition application.
• Pre-tension section definitions are not imported; they have to be redefined in the import analysis.
• The capability is not available for elements with composite solid section definitions.
• If the elements that are removed in the original analysis (see “Element and contact pair removal and reactivation,” Section 11.2.1) are imported, they become active in the import analysis and should be removed in the first step of the import analysis.
• The symmetric model generation capability cannot be used in an import analysis in Abaqus/Standard.
• The results file, restart file, or output database file generated during the import analysis is not appended to the results file, restart file, or output database file of the original analysis.
• There may be a slight discontinuity during the transfer of state variables for analyses using fully integrated, first-order continuum elements if the elements are significantly deformed and the reference configuration is updated.
• Mesh-independent spot welds (see “Mesh-independent fasteners,” Section 35.3.4) are not imported. However, the spot weld reference nodes are imported and can be used to redefine spot welds in
the import analysis. The locations of the spot weld reference nodes and projection points are computed based upon the reference configuration of the import analysis. Therefore, if the deformed configuration of the imported model is significantly different from its reference configuration, it is recommended that the reference configuration be updated.
• If the value of the friction coefficient is changed from the value given in the model data of the original analysis, the changed value must be respecified in the first step of the import analysis (see “Changing friction properties during an Abaqus/Standard analysis” in “Frictional behavior,” Section 37.1.5).
• The capability is not available if adaptive meshing (see “ALE adaptive meshing and remapping in Abaqus/Standard,” Section 12.2.7) is used in the original analysis.
• Enriched features (see “Modeling discontinuities as an enriched feature using the extended finite element method,” Section 10.7.1) are not imported.
• Restart files from the original analysis are used in the analysis preprocessor and in the Abaqus/Standard execution in the import analysis. When the import job is run in parallel on computer clusters by using MPI-based parallelization, these restart files are copied to each host machine. The original job restart files are not decomposed to match the import analysis parallel domain and may be large relative to the local disk space available on the host machines. You can minimize this file size by requesting restart output only for the increment from which import will occur.
# Input file template
# Transferring results using models that are not defined as assemblies of part instances:
First Abaqus/Standard analysis:
```txt
*HEADING
...
*MATERIAL, NAME=mat1
*ELASTIC
Data lines to define linear elasticity
*PLASTIC
Data lines to define Mises plasticity
*DENSITY
Data line to define the density of the material
...
*BOUNDARY
Data lines to define boundary conditions
*STEP, NLGEOM=YES
*STATIC
...
*RESTART, WRITE
*END STEP
```
Abaqus/Standard import analysis:
```python
*HEADING
*IMPORT, STEP=step, INCREMENT=increment, STATE=YES, UPDATE=NO
Data lines to specify element sets to be imported
*IMPORT ELSET
Data lines to specify element set definitions to be imported
*IMPORT NSET
Data lines to specify node set definitions to be imported
**
*** Optionally define additional model information
**
*BOUNDARY
Data lines to redefine boundary conditions
*STEP, NLGEOM=YES
*STATIC
...
*END STEP
```
# Transferring results using models defined as assemblies of part instances:
First Abaqus/Standard analysis:
```txt
*HEADING
*PART, NAME=Part-1
Node, element, section, set, and surface definitions
*END PART
*ASSEMBLY, NAME=Assembly-1
*INSTANCE, NAME=i1, PART=Part-1