ProductsAbaqus/StandardAbaqus/ExplicitAbaqus/CAE Specifying new data in an import analysisAdditional 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 definitionsNew 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 transformationNodal 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 analysisBy default, Abaqus/Standard uses a small-strain formulation (i.e., geometric nonlinearity is ignored) and Abaqus/Explicit uses a large-deformation formulation (i.e., 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 nodesInitial conditions (Initial conditions in Abaqus/Standard and Abaqus/Explicit) 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.
ProceduresResults 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/StandardWhen 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:
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 conditionsBoundary 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 in Abaqus/Standard and Abaqus/Explicit. LoadsLoads, including those applied for connector actuation, defined in the original analysis are not imported. Loads may, 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 fieldsThe field variables at nodes are not imported. If the elements being imported are coupled temperature-displacement elements, the temperature is imported if the associated material state is imported. The temperature is also imported for an adiabatic analysis if the associated material state is imported. For all other cases the temperatures at nodes are not imported. If the original analysis uses predefined temperature fields (Predefined temperature) to vary the temperatures at nodes, the import analysis will not be allowed to continue. If the original analysis uses predefined field variable definitions (Predefined field variables) to vary the field variables at nodes, the import analysis will be allowed to continue only if all the elements being imported are coupled temperature-displacement elements; however, the field variables are not imported. If the original analysis uses initial temperature (Defining initial temperatures) and field variable (Defining initial values of predefined field variables) conditions, the import analysis will be allowed to continue only if all the elements being imported are coupled temperature-displacement elements. In addition, specification of initial conditions for temperatures and field variables is not allowed in an import analysis, unless all the elements being imported are coupled temperature-displacement elements. In this case initial conditions for temperatures and field variables can be specified on the imported nodes if the reference configuration is updated and the material state is not imported. Initial temperatures can be specified in the import analysis if it is an adiabatic analysis. Material optionsAll 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 materialsWhen 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 elementsWhen 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 scalingIf 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 dampingThe material model must be redefined in the import analysis if changes to material damping are required. Changes to material definitionsWhen material definitions are changed, care must be taken to ensure that a consistent material state is maintained. It may 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. ElementsThe 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.
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:
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 and can contain at most three different element types.
Using section controls in an import analysisWhen 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 may 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: Element Controls: Membrane and shell element thickness computationThe computations for membrane and shell element thicknesses are described below. Shell elements defined using a general shell sectionFor 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 elementsFor 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 elementsThe contact angle, , 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. ConstraintsMost 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. InteractionsContact 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 may 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 may be different in Abaqus/Standard and Abaqus/Explicit. Examples of potential causes for differences include:
Thus, when the contact conditions are defined in the import analysis, the contact state that existed in the previous analysis may 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. OutputOutput 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 may 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. LimitationsThe import capability has the following known limitations. Where applicable, details are given in the relevant sections.
Input file templateTransferring 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 ** *** 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 ** *** 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 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 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 |