Products: ABAQUS/Standard ABAQUS/Explicit
The submodeling capability is applied to the three-dimensional continuum stress/displacement elements and the continuum shell elements. In ABAQUS/Standard general static, dynamic, and linear perturbation procedures are used in various combinations for both the global and submodel analyses. In ABAQUS/Explicit both the global model and submodel are quasi-static analyses, except for the test that uses the GLOBAL ELSET parameter, which is a dynamic process. In the quasi-static tests each submodel can be driven from any of the global models.
The submodeling capability is also tested for a directly input matrix representing an element stiffness in static procedures (general and linear perturbation) in ABAQUS/Standard.
All global models have dimensions 8.0 × 1.5 × 1.0.
Material:Loading and boundary conditions:
All global models involving static procedures in ABAQUS/Standard and all the analyses in ABAQUS/Explicit are subject to the same loading and boundary conditions as depicted in Two-dimensional continuum stress/displacement submodeling, Section 3.6.2. The time history of the loading, the time at which the corresponding submodeled analysis is performed, and the requested file output from the global model are unique to each individual analysis. Smooth-step amplitudes are used to load the quasi-static models in ABAQUS/Explicit.
All global models involving dynamic procedures in ABAQUS/Standard are subject to the same loading and boundary conditions as depicted in Two-dimensional continuum stress/displacement submodeling, Section 3.6.2. For the transient simulations using the *DYNAMIC option, different excitation frequencies of the load can be tested by changing the parameters defined in the input files. As in the static analyses the time history of the loading, the time at which the corresponding submodeled analysis is performed, and the requested file output from the global model are unique to each individual analysis.
The amplitudes of all driven variables in the submodeled analysis are correctly identified in the global analysis file output and applied at the driven nodes in the submodel analysis.
The following input files test various combinations of static analyses using the *STATIC and *STATIC with *STEP, PERTURBATION procedures:
C3D4 elements; global analysis.
C3D4 elements; submodel analysis.
C3D6 elements; global analysis.
C3D6 elements; submodel analysis.
C3D8 elements; global analysis.
C3D8 elements; *MATRIX INPUT and *MATRIX ASSEMBLE; submodel analysis.
Matrix representing element stiffness for submodel analysis.
C3D8 elements; *SUBMODEL, GLOBAL ELSET; global analysis.
C3D8 elements; *SUBMODEL, GLOBAL ELSET; submodel analysis.
C3D8 elements; multiple *SUBMODEL options; global analysis.
C3D8 elements; multiple *SUBMODEL options; submodel analysis.
C3D10 elements; global analysis.
C3D10 elements; submodel analysis.
C3D10M elements; global analysis.
C3D10M elements; submodel analysis.
C3D20 elements; global analysis.
C3D20 elements; submodel analysis.
C3D27 elements; global analysis.
C3D27 elements; submodel analysis.
C3D27 elements; *SUBMODEL, GLOBAL ELSET; global analysis.
C3D27 elements; *SUBMODEL, GLOBAL ELSET; submodel analysis.
The following input files test the submodeling capability using the dynamic procedures:
C3D15 elements; global *MODAL DYNAMIC analysis.
C3D15 elements; submodel *MODAL DYNAMIC analysis.
C3D15 elements; global *DYNAMIC analysis.
C3D8 elements; submodel *DYNAMIC analysis.
C3D4 elements; global analysis.
C3D6 elements; global analysis.
C3D8R elements; global analysis.
C3D10M elements; global analysis.
C3D8R elements; submodel analysis.
C3D10M elements; submodel analysis.
SC6R elements; global analysis.
SC8R elements; global analysis.
SC8R elements; submodel analysis.
C3D8R elements; *SUBMODEL, GLOBAL ELSET; global analysis.
C3D8R elements; *SUBMODEL, GLOBAL ELSET; submodel analysis.
SC8R elements; *SUBMODEL, GLOBAL ELSET; global analysis.
SC8R elements; *SUBMODEL, GLOBAL ELSET; submodel analysis.