Transferring Results between Abaqus/Explicit and Abaqus/Standard

Specifying New Data in an Import Analysis

Additional model definitions such as new elements, nodes, surfaces, etc. can be defined during the import analysis. Initial conditions can also be specified during the import analysis.

New Model Definitions

New nodes, elements, and material properties can be added to the model in an import analysis once import has been specified. Nodal coordinates must be defined in the updated configuration, regardless of whether or not the reference configuration is updated on import (see Updating the Reference Configuration). The usual Abaqus input can be used. Imported material definitions can be used with the new elements (which will need new section property definitions).

Nodal Transformation

Nodal transformations (Transformed Coordinate Systems) are not imported; transformations can be defined independently in the import analysis. Continuous displacements, velocities, etc. are obtained only if the nodal transformations in the import analysis are the same as those in the original analysis. Use of the same transformations is also recommended for nodes with boundary conditions or point loads defined in a local system.

Specifying Geometric Nonlinearity in an Import Analysis

By default, Abaqus/Standard uses a small-strain formulation (that is, geometric nonlinearity is ignored) and Abaqus/Explicit uses a large-deformation formulation (that is, geometric nonlinearity is included). For each step of an analysis, you can specify which formulation should be used; see Geometric Nonlinearity for details.

The default value for the formulation in an import analysis is the same as the value at the time of import. Once the large-displacement formulation is used during a given step in any analysis, it will remain active in all the subsequent steps, whether or not the analysis is imported.

If the small-displacement formulation is used at the time of import, the reference configuration cannot be updated.

Specifying Initial Conditions for Imported Elements and Nodes

Initial conditions (Initial Conditions) can be specified on the imported elements or nodes only under certain conditions. Table 1 lists the initial conditions that are allowed depending on whether or not the material state is imported (see Importing the Material State). The reference configuration can be updated or not, as desired.

Table 1. Valid initial conditions.
Initial condition	Material state imported?
Hardening	No
Relative density	No
Rotational velocity	Yes or No
Solution-dependent state variables	No
Stress	No
Velocity	Yes or No
Void ratio	No

Procedures

Results can be imported into Abaqus/Explicit only from a general analysis step involving static stress analysis, dynamic stress analysis, or steady-state transport analysis in Abaqus/Standard. Results transfer from linear perturbation procedures (General and Perturbation Procedures) is not allowed.

Abaqus/Standard offers several analysis procedures that can be used in an import analysis. These procedures can be used to perform an eigenvalue analysis, static or dynamic stress analysis, buckling analysis, etc. See Solving Analysis Problems for a discussion of the available procedures.

For springback analysis of a formed component the first step in the Abaqus/Standard analysis usually consists of a static analysis procedure so that the initial out-of-balance forces can be removed gradually from the system. The removal of these forces is performed automatically by Abaqus/Standard during the first static analysis step, as described below. If the first step in the Abaqus/Standard analysis is not a static step (such as a dynamic step), the analysis proceeds directly from the state imported from the Abaqus/Explicit analysis.

Achieving Static Equilibrium When Importing into Abaqus/Standard

When the current state of a deformed body in an explicit dynamic analysis is imported into a static analysis, the model will not initially be in static equilibrium. Initial out-of-balance forces must be applied to the deformed body in dynamic equilibrium to achieve static equilibrium. Both dynamic forces (inertia and damping) and boundary interaction forces contribute to the initial out-of-balance forces. The boundary forces are the result of interactions from fixed boundary and contact conditions. Any changes in the boundary and contact conditions from the Abaqus/Explicit analysis to the Abaqus/Standard analysis will contribute to the initial out-of-balance forces.

In general the instantaneous removal of the initial out-of-balance forces in a static analysis will lead to convergence problems. Hence, these forces need to be removed gradually until complete static equilibrium is achieved. During this process of removing the out-of-balance forces, the body will deform further and a redistribution of internal forces will occur, resulting in a new stress state. (This is essentially what occurs during “springback,” when a formed product is removed from the worktools.)

When the first step in the Abaqus/Standard import analysis is a static procedure, the following algorithm is used to remove the initial out-of-balance forces automatically:

The imported stresses are defined at the start of the analysis as the initial stresses in the material.
An additional set of artificial stresses is defined at each material point. These stresses are equal in magnitude to the imported stresses but are of opposite sign. The sum of the material point stresses and these artificial stresses, thus, creates zero internal forces at the beginning of the step.
The internal artificial stresses are ramped off linearly in time during the first step. Thus, at the end of the step the artificial stresses have been removed completely and the remaining stresses in the material will be the residual stress state associated with static equilibrium.

Once static equilibrium has been obtained, subsequent steps can be defined using any analysis procedure that would normally follow a static analysis in Abaqus.

When the first step is not a static analysis, no artificial stress state is applied and the imported stresses are used in the internal force computations for the element.

Boundary Conditions

Boundary conditions, including any connector motion, specified in the original analysis are not imported. They must be defined again in the import analysis. In some cases nonzero boundary conditions imposed in the original analysis need to be maintained at the same values in the import analysis when the imported configuration is not updated. In such cases you can prescribe a constant (step function) amplitude variation for the analysis step (see Prescribing Nondefault Amplitude Variations) so that the newly applied boundary conditions are applied instantaneously and held at that value for the duration of the step. Alternatively, you can refer to an amplitude curve in the boundary condition definition (see Amplitude Curves). If boundary conditions in the original analysis are applied in a transformed coordinate system (see Transformed Coordinate Systems), the same coordinate system should be defined and used in the import analysis.

For a discussion of applying boundary conditions, see Boundary Conditions.

Loads

Loads, including those applied for connector actuation, defined in the original analysis are not imported. Loads might, therefore, need to be redefined in the import analysis. There are no restrictions on the loads that can be applied when results are imported from one analysis to the other. In cases when the loads need to be maintained at the same values as in the original analysis, you can prescribe a constant (step function) amplitude variation for the analysis step (see Prescribing Nondefault Amplitude Variations) to apply the loads instantaneously at the start of the step and hold them for the duration of the step. Alternatively, you can refer to an amplitude curve in the load definition (see Amplitude Curves). If point loads in the original analysis are applied in a transformed coordinate system (see Transformed Coordinate Systems) and the loads must be maintained in the import analysis, the load application is simplified if the same coordinate system is defined and used in the import analysis.

See About Loads for an overview of the loading types available in Abaqus.

Predefined Fields

Temperatures, whether they are prescribed or are degrees of freedom (as in a coupled thermal-stress analysis), and field variables at nodes are imported if the material state is imported.

If the reference configuration is updated and the material state is imported, the initial conditions for temperatures and field variables at the imported nodes are reset to the imported values; for example, the thermal strains are measured relative to the imported temperatures. If the reference configuration is updated but the material state is not imported, the initial conditions are reset to zero. In this case you can respecify the initial conditions on the imported nodes.

If the temperature is a state variable (as in an adiabatic analysis where temperature is an integration point quantity), it is imported if the material state is imported.

Material Options

All material property definitions and the orientations associated with imported elements are imported by default. Material properties can be changed by respecifying the material property definitions with the same material name. All relevant material properties must be redefined since the old definitions that were imported by default will be overwritten. Material orientations associated with imported elements can be changed only if the reference configuration is updated and the material state is not imported; the material orientations associated with imported elements cannot be redefined for other combinations of the reference configuration and material state.

Hyperelastic Materials

When hyperelastic materials are imported, the state must be imported if the configuration is not updated; if the state is not imported, the configuration must be updated.

Connector Elements

When connector elements are imported, any associated connector behavior definitions are imported by default. The imported connector behavior definitions can be modified only if the state is not imported.

Mass Scaling

If mass scaling (Mass Scaling) is used in Abaqus/Explicit, the scaled masses will not be transferred to the subsequent import analysis in Abaqus/Standard. The mass of the model for the Abaqus/Standard analysis will be based on either the imported or the redefined density definitions.

Material Damping

The material model must be redefined in the import analysis if changes to material damping are required.

Changes to Material Definitions

When material definitions are changed, care must be taken to ensure that a consistent material state is maintained. It might sometimes be possible to simplify the material definition. For example, if a Mises plasticity model was used in the Abaqus/Explicit analysis and no further plastic yielding is expected in the Abaqus/Standard analysis (as is generally the case for springback simulations), a linear elastic material can be used for the Abaqus/Standard analysis. However, if further nonlinear material behavior is expected, no changes to the existing material definitions should be made. The history of the state variables will not be maintained if the material models are not the same in both the original analysis and the import analysis.

Elements

The import capability is available for first-order continuum, modified triangular and tetrahedral elements, conventional shell, continuum shell, membrane, beam (both linear and quadratic), pipe (linear), truss, connector, rigid, and surface elements that are common to both Abaqus/Explicit and Abaqus/Standard, as defined in Table 2.

Table 2. Common element types that can be transferred between Abaqus/Explicit and Abaqus/Standard.
Common element types
CPS3, CPS3T, CPS4R, CPS4RT, CPS6M, CPS6MT
CPE3, CPE3T, CPE4R, CPE4RT, CPE6M, CPE6MT
CAX3, CAX3T, CAX4R, CAX4RT, CAX6M, CAX6MT
C3D4, C3D4T, C3D6, C3D6T, C3D8, C3D8I, C3D8R, C3D8T, C3D8RT, C3D10,C3D10T, C3D10M, C3D10MT
M3D3, M3D4, M3D4R
R2D2
R3D3, R3D4
RAX2
S4, S4R, S3R, S4RT, S3RT
SC8R, SC8RT, SC6R, SC6RT
SAX1
SFM3D3, SFM3D4R
T2D2
T3D2
B21, B22, PIPE21
B31, B32, PIPE31
CONN2D2¹, CONN3D2¹
AC2D3, AC2D4R, AC2D4, ACIN2D2
AC3D4, AC3D6, AC3D8R, AC3D8, ACIN3D3, ACIN3D4
ACAX3, ACAX4R, ACAX4, ACINAX2
COH2D4, COHAX4, COH3D6, COH3D8
MASS, ROTARYI
¹Connector elements can be imported from Abaqus/Standard to Abaqus/Explicit; but not vice versa.

When S3R shell elements are imported from Abaqus/Explicit into Abaqus/Standard, they are converted into degenerated S4R elements automatically. However, when S3R shell elements are imported from Abaqus/Standard into Abaqus/Explicit, they remain S3R elements. When C3D6 and C3D6T solid elements are imported from Abaqus/Explicit into Abaqus/Standard, the results at the single point integration are applied to both integration points in Abaqus/Standard and the full integration is used automatically. However, when C3D6 and C3D6T solid elements are imported from Abaqus/Standard into Abaqus/Explicit, only the results at the first integration point are imported and are used in the reduced integration. When quadrilateral and hexahedral acoustic finite elements are imported between Abaqus/Explicit and Abaqus/Standard, they are converted to or from reduced-integration types, as required.

The following restrictions apply to the import capability:

Connector elements can be imported from Abaqus/Standard to Abaqus/Explicit but not vice versa. Further, if connector elements are imported, the configuration can be updated provided that the state is not imported and the state can be imported provided that the configuration is not updated.
Rebars defined using rebar layers (Defining Reinforcement) are imported provided the underlying elements are also imported. Rebar reinforcements defined using the embedded element technique (Embedded Elements) 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) cannot be imported.
Infinite elements and fluid elements cannot be imported.
Rigid elements for which the thickness is interpolated from the nodes in an Abaqus/Explicit analysis will not be imported into Abaqus/Standard.
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 all the elements used to define the rigid body are included in the element sets 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.
Failed elements in Abaqus/Explicit will not be imported into Abaqus/Standard.
Elements that are being removed or are inactive (see Element and Contact Pair Removal and Reactivation) in Abaqus/Standard will not be imported into Abaqus/Explicit.
Rigid surfaces will not be imported.

When importing results from an Abaqus/Standard analysis to an Abaqus/Explicit analysis, each element set specified can contain only compatible element types listed in Table 3. Element types from different cells are not compatible and cannot be combined in the same element set.

Table 3. Compatible element types.
ACINAX2, ACIN2D2, ACIN3D3, ACIN3D4
CPE4R, CPE3, AC2D3, AC2D4
CPS4R, CPS3
CAX4R, CAX3, ACAX3, ACAX4
AC3D4, AC3D6, AC3D8, C3D8, C3D8R, C3D4, C3D6
M3D4R, M3D3, M3D4
R3D3, R3D4
S4R, S3R, SC6R, SC8R, S4
SFM3D3, SFM3D4R
CAX6M, C3D10M
C3D8T, C3D4T, C3D6T
SC6RT, SC8RT, S4T, S4RT, S3T, S3RT
MASS, ROTARYI

Using Section Controls in an Import Analysis

When transferring results between Abaqus/Standard and Abaqus/Explicit, it is important that the hourglass forces are computed consistently. The enhanced hourglass control formulation (see Enhanced Hourglass Control Approach in Abaqus/Standard and Abaqus/Explicit) is recommended for computing hourglass forces in the original as well as all subsequent import analyses.

Once section controls have been defined in the original analysis, they cannot be modified in any subsequent Abaqus/Standard or Abaqus/Explicit analysis. Therefore, if section controls are to be used in any one analysis in a series of import analyses, they must be specified in the very first analysis. The section controls specified for an element set in the original analysis will be used for the elements belonging to that element set in all subsequent import analyses.

Section controls other than the hourglass control formulation have appropriate defaults depending on the type of analysis and, generally, do not need to be changed. Nondefault values can be chosen subject to certain restrictions.

In an Abaqus/Standard analysis only the average strain kinematic formulation and second-order accurate element formulation are available; other kinematic formulations, element formulations, or section controls that are relevant only in an Abaqus/Explicit analysis can be specified in the Abaqus/Standard analysis. Such controls will be ignored in the Abaqus/Standard analysis but retained for the subsequent Abaqus/Explicit import analysis.

If a kinematic formulation other than average strain is used for solid elements in the Abaqus/Explicit analysis, the differences in the kinematic formulations might lead to errors in Abaqus/Standard if the elements are distorted or undergo large rotations.

Using the first-order accurate element formulation (default) in Abaqus/Explicit and the second-order accurate element formulation (the only available formulation) in Abaqus/Standard is not expected to cause significant errors, since the time increment size in Abaqus/Explicit is inherently small. One exception to this is when the Abaqus/Explicit analysis involves components undergoing several revolutions, in which case it is recommended that the second-order accurate element formulation be used in Abaqus/Explicit.

Input File Usage

Use the following options in the original analysis:

MEMBRANE SECTION, CONTROLS=name1, ELSET=elset1
SHELL SECTION, CONTROLS=name2, ELSET=elset2
SHELL GENERAL SECTION, CONTROLS=name3, ELSET=elset3
SOLID SECTION, CONTROLS=name4, ELSET=elset4

Use options similar to the following one in the original analysis:

SECTION CONTROLS, NAME=name1

Abaqus/CAE Usage

Define section controls when you assign the element type in the original analysis:

Mesh module: MeshElement Type: Element Controls

Membrane and Shell Element Thickness Computation

The computations for membrane and shell element thicknesses are described below.

Shell Elements Defined Using a General Shell Section

For shells defined using a general shell section, the current thickness is computed based on the effective Poisson's ratio, which is 0.5 by default, in both Abaqus/Explicit and Abaqus/Standard.

Input File Usage

SHELL GENERAL SECTION, POISSON=

Abaqus/CAE Usage

Property module: homogeneous or composite shell section editor: Section integration: Before analysis: Advanced: Section Poisson's ratio

Shell Elements Defined Using Shell Sections Integrated during Analysis and Membrane Elements

For shells defined using shell sections integrated during analysis and for membranes in Abaqus/Standard, the current thickness is computed based on the effective Poisson's ratio, which is 0.5 by default. In Abaqus/Explicit, on the other hand, the computation of the thickness could be based either on the effective Poisson's ratio or the through-thickness strains, with the computation based on the through-thickness strains used by default.

If you do not specify a section Poisson's ratio for shell sections integrated during analysis or for membrane sections in an original Abaqus/Explicit or Abaqus/Standard analysis, the thickness computations in the original and all subsequent import analyses are carried out using the default methods. In other words, the thicknesses in all Abaqus/Standard analyses are computed using the default effective Poisson's ratio of 0.5, while the thicknesses in all Abaqus/Explicit analyses are computed using the through-thickness strains.

When the section Poisson's ratio is assigned a numerical value in an original Abaqus/Standard or Abaqus/Explicit analysis, the thickness computations in the original analysis and all subsequent import analyses are performed using the specified value for the effective Poisson's ratio.

Input File Usage

Use one of the following options:

SHELL SECTION, POISSON= 
SHELL SECTION, POISSON=MATERIAL
MEMBRANE SECTION, POISSON= 
MEMBRANE SECTION, POISSON=MATERIAL

Abaqus/CAE Usage

Property module: 
Homogeneous or composite shell section editor: Section integration: 
During analysis: Advanced: Section Poisson's ratio
Membrane section editor: Section Poisson's ratio

Contact Angle Computation in SLIPRING-Type Connector Elements

The contact angle, $α$ , made by the belt wrapping around node b (see Complex Connections) is computed automatically in Abaqus/Explicit, ignoring the value specified within the Abaqus/Standard analysis.

Constraints

Most types of kinematic constraints (including multi-point constraints and surface-based tie constraints) specified in the original analysis are not imported and must be defined again in the import analysis; however, embedded element constraints are imported by default. See About Kinematic Constraints for a discussion of the various types of kinematic constraints.

Similarly, surface-based kinematic and distributing coupling constraints specified in the original analysis are not imported and must be defined again in the import analysis. If transfer of material state is specified for import, the displacements and rotations of the coupling reference nodes are transferred in Abaqus/Standard to Abaqus/Explicit import analysis. This also applies to reference nodes that do not belong to any imported elements. By transferring nodal results, the constraint will be in initial equilibrium in the imported model. The transfer of nodal results is not supported in Abaqus/Explicit to Abaqus/Standard import analysis.

Interactions

Contact definitions specified in the original analysis and the contact state are not imported. Contact can be defined again in the import analysis by specifying the surfaces and contact pairs; however, you might not be able to use the exact contact definitions that were used in the original analysis because of differences in the contact capabilities between Abaqus/Standard and Abaqus/Explicit.

The contact constraint enforcement might be different in Abaqus/Standard and Abaqus/Explicit. Examples of potential causes for differences include:

Abaqus/Standard typically uses a “pure main-secondary” approach, whereas Abaqus/Explicit typically uses a “balanced main-secondary” approach.
Depending on the contact formulations used, Abaqus/Standard and Abaqus/Explicit sometimes treat shell thicknesses and midsurface offsets differently.

Thus, when the contact conditions are defined in the import analysis, the contact state that existed in the previous analysis might not be reproduced at the beginning of the import analysis. This could lead to a redistribution of stresses and an analysis that differs from what you desire. In some cases this problem can be mitigated by using nondefault options, such as ignoring shell thicknesses in the contact calculations, to match behaviors in Abaqus/Standard and Abaqus/Explicit.

For a detailed description of the contact capabilities in Abaqus and the differences in the contact capabilities between Abaqus/Standard and Abaqus/Explicit, see About Contact Interactions.

Output

Output can be requested for an import analysis in the same way as for an analysis in which the results are not imported. The output variables available in Abaqus/Standard are listed in Abaqus/Standard Output Variable Identifiers. The output variables available in Abaqus/Explicit are listed in Abaqus/Explicit Output Variable Identifiers.

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 and VUMAT. Similarly, for a connector behavior, the plastic relative displacement (CUP), kinematic hardening shift force (CALPHAF), overall damage (CDMG), damage initiation criteria (CDIF, CDIM, CDIP), friction accumulated slip (CASU), and connector status (CSLST, CFAILST) will be continuous.

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. Accelerations are recomputed at the start of an import analysis in Abaqus/Explicit and might be different from those obtained at the end of an Abaqus/Standard analysis. The differences in accelerations arise from the recalculation of the internal forces created by the imported stresses using the Abaqus/Explicit element formulation algorithms.

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/Explicit and Abaqus/Standard must be run on computers that are binary compatible.
The capability is not available for fluid elements, infinite elements, and spring and dashpot elements. Connector elements can be imported from Abaqus/Standard to Abaqus/Explicit but not vice versa. See the discussion on Elements earlier in this section for further details.
If connector elements are imported, the configuration can be updated provided that the state is not imported and the state can be imported provided that the configuration is not updated.
All elements and nodes must be included in at least one set in the original analysis when importing part instances.
Node sets that are generated from existing element sets (see Node Definition) must be defined in the original analysis.
Contact pair definitions and general contact definitions are not imported. Analytical rigid surfaces 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, Mullins effect, hyperfoam, viscoelasticity, Mises plasticity (including the kinematic hardening models), extended Drucker-Prager plasticity, crushable foam plasticity, Mohr-Coulomb plasticity, critical state (clay) plasticity, cast iron plasticity, concrete damaged plasticity, damage for cohesive elements, damage for ductile metals, or damage for fiber-reinforced composites. See Importing the Material State for details.
If the state is imported for connector elements with behavior defined, the plastic displacements, the frictional slip, and the damage state are imported and the connector forces are recomputed. Some of the connector output variables, such as CU, are also recomputed on import. The recomputed variables might differ slightly at the point of import due to precision and algorithmic differences between the two solvers across import. See Importing the Material State for details.
Temperatures and field variables at nodes are not imported. If the temperature is a state variable (as in an adiabatic analysis where temperature is an integration point quantity), it will be imported if the material state is imported. See the discussion on Predefined Fields 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 is not imported unless the reference node is part of another element definition that is imported.
Fluid cavity definitions are not imported. In addition, the reference node of a fluid cavity is not imported unless the reference node is part of another element definition that is imported.
Element and contact pair removal/reactivation (Element and Contact Pair Removal and Reactivation) cannot be used in the first step of an import analysis in Abaqus/Standard. It can be used in the subsequent steps.
For an Abaqus/Standard to Abaqus/Explicit import analysis in which elements in the Abaqus/Standard analysis were removed and reactivated in multiple steps (Element and Contact Pair Removal and Reactivation) and all elements are active for transfer at the import step, some of the element states, such as strains, might not be transferred correctly.
In a series of Abaqus/Standard and Abaqus/Explicit import analyses in the order Abaqus/Explicit(1) → Abaqus/Standard(1) → Abaqus/Explicit(2) →Abaqus/Standard(2), if elements in an element set are removed in the Abaqus/Standard(1) analysis, the subsequent Abaqus/Standard(2) import analysis does not recognize that this element set was removed in a previous analysis and fails with an error message stating that the element set is not found in the restart file. Such failures can be avoided by using flattened input files and requesting only the active element sets for import.
Section controls must be defined in the original analysis if any of a series of import analyses uses nondefault element formulations since section controls cannot be changed in an import analysis. See the discussion on Using Section Controls in an Import Analysis earlier in this section.
The symmetric model generation capability (Symmetric Model Generation) 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.
An Abaqus/Standard import analysis where the reference configuration is not updated is not allowed if the adaptive meshing capability (About ALE Adaptive Meshing) was used in the previous Abaqus/Explicit analysis.
Mesh-independent spot welds (see Mesh-Independent Fasteners) are not imported. These constraints can be redefined in the import analysis and are formed using the reference configuration of the import model. If the reference configuration is updated, the redefined constraints might not match the old constraints exactly due to the differences in geometry. If new constraints are defined and the reference configuration of the import model is not updated, they might not initially be in compliance if the nodes involved in the constraint have nonzero displacements. This might cause numerical difficulty and potential exit of the import analysis. In this case it is recommended that you update the reference configuration on import.
The first step after an import when the reference configuration is updated should not be used to generate a substructure.

For beam structures that have acute curvatures and undergo large permanent changes in curvatures, slightly different equilibrated configurations will be seen when using import depending on whether or not the reference configuration is to be updated to the imported configuration (see Updating the Reference Configuration). This configuration difference is due to beam element formulation differences between Abaqus/Standard and Abaqus/Explicit.

Input File Template

Transferring Results between Abaqus/Explicit and Abaqus/Standard Using Models That Are Not Defined as Assemblies of Part Instances:

Abaqus/Explicit analysis:

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
DYNAMIC, EXPLICIT
 …
RESTART, WRITE, NUMBER INTERVAL=n
END STEP

Abaqus/Standard analysis:

HEADING
IMPORT, STEP=step, INTERVAL=interval, 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
IMPORT SURFACE
Data lines to specify surface definitions to be imported
**
*** Optionally redefine the material block
**
MATERIAL, NAME=mat1
ELASTIC
Data lines to redefine linear elasticity
PLASTIC
Data lines to redefine Mises plasticity
 …
BOUNDARY
Data lines to redefine boundary conditions
STEP, NLGEOM=YES
STATIC
 …
END STEP

Transferring Results between Abaqus/Standard and Abaqus/Explicit Using Models That Are Not Defined as Assemblies of Part Instances:

Abaqus/Standard analysis:

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
STATIC
 …
RESTART, WRITE, FREQUENCY=n
END STEP

Abaqus/Explicit analysis:

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
IMPORT SURFACE
Data lines to specify surface definitions to be imported
**
*** Optionally redefine the material block
**
MATERIAL, NAME=mat1
ELASTIC
Data lines to redefine linear elasticity
PLASTIC
Data lines to redefine Mises plasticity
 …
BOUNDARY
Data lines to redefine boundary conditions
STEP
DYNAMIC, EXPLICIT
 …
END STEP

Transferring Results between Abaqus/Explicit and Abaqus/Standard Using Models Defined as Assemblies of Part Instances:

Abaqus/Explicit analysis:

HEADING
PART, NAME=Part-1
Node, element, section, set, and surface definitions
END PART
ASSEMBLY, NAME=Assembly-1
INSTANCE, NAME=i1, PART=Part-1
<positioning data>
Additional set and surface definitions (optional)
END INSTANCE
Assembly level set and surface definitions
 …
END ASSEMBLY
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
DYNAMIC, EXPLICIT
 …
RESTART, WRITE, NUMBER INTERVAL=n
END STEP

Abaqus/Standard analysis:

HEADING
Part definitions (optional)
ASSEMBLY, NAME=Assembly-1
INSTANCE, INSTANCE=i1, LIBRARY=oldjob-name
Additional set and surface definitions (optional)
IMPORT, STEP=step, INTERVAL=interval, STATE=YES, UPDATE=NO
IMPORT SURFACE
END INSTANCE
Additional part instance definitions (optional)
Assembly level set and surface definitions
 …
END ASSEMBLY
**
*** Optionally redefine the material block
**
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
 …
END STEP

Transferring Results between Abaqus/Standard and Abaqus/Explicit Using Models Defined as Assemblies of Part Instances:

Abaqus/Standard analysis:

HEADING
PART, NAME=Part-1
Node, element, section, set, and surface definitions
END PART
ASSEMBLY, NAME=Assembly-1
INSTANCE, NAME=i1, PART=Part-1
<positioning data>
Additional set and surface definitions (optional)
END INSTANCE
Assembly level set and surface definitions
 …
END ASSEMBLY
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
STATIC
 …
RESTART, WRITE, FREQUENCY=n
END STEP

Abaqus/Explicit analysis:

HEADING
Part definitions (optional)
ASSEMBLY, NAME=Assembly-1
INSTANCE, INSTANCE=i1, LIBRARY=oldjob-name
Additional set and surface definitions (optional)
IMPORT, STEP=step, INCREMENT=increment, STATE=YES, UPDATE=NO
IMPORT SURFACE
END INSTANCE
Additional part instance definitions (optional)
Assembly level set and surface definitions
END ASSEMBLY
**
*** Optionally redefine the material block
**
MATERIAL, NAME=mat1
ELASTIC
Data lines to redefine linear elasticity
PLASTIC
Data lines to redefine Mises plasticity
 …
BOUNDARY
Data lines to redefine boundary conditions
STEP
DYNAMIC, EXPLICIT
 …
END STEP