Product: ABAQUS/Standard
The submodeling capability is applied to two-dimensional, three-dimensional and axisymmetric continuum elements with pore pressure. General steps invoking the soils consolidation procedure are used for both the global and submodel analyses.
All global models have dimensions 3.0 × 5.0 in the – or – plane. Each submodel has dimensions 2.05 × 3.45 in the – or – plane and occupies the lower right-hand corner of the corresponding global model. In all but the axisymmetric models, the out-of-plane dimension is 1.0. In axisymmetric models the structure analyzed is a hollow cylinder with outer radius 5.0.
Material:Loading:
In all models, a distributed flow of magnitude 0.002 is applied to the right face, where the sink pore pressure is 14.7.
Boundary and initial conditions:
In the global model, fixed boundary conditions = 0 and = 0 are prescribed on the left and bottom faces, respectively. In three-dimensional models the additional constraints = 0 are applied to the nodes on the front and back faces. The initial void ratio is unity everywhere and fixed pore pressure boundary conditions are applied on the left face. In the submodel, = 0 is prescribed everywhere on the bottom face, while degrees of freedom 1, 2 and 8 for the nodes on the top and left faces are being driven by the global solution.
In the global analyses, the pore pressure field predicted by ABAQUS varies linearly in the -direction in nonaxisymmetric models and logarithmically in the -direction in axisymmetric models. The predicted displacement field is nonuniform in all models. These results are depicted in the pore pressure and - or -displacement contour plots shown below. For comparison purposes, the pore pressure and displacement solutions predicted by the submodels are also presented in the same contour plots and excellent agreement between global and submodel results is obtained. Hence, 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.
Global and submodel analyses results for 8-node plane strain elements are shown in Figure 3.6.121 and Figure 3.6.122.
Global and submodel analyses results for 8-node axisymmetric elements are shown in Figure 3.6.123 and Figure 3.6.124.
Global and submodel analyses results for 20-node brick elements (front face) are shown in Figure 3.6.125 and Figure 3.6.126.
The following input files test the *SOILS, CONSOLIDATION procedure. Each test performs a single increment transient consolidation calculation for a time period of one.
C3D8PH elements; global analysis.
C3D8PH elements; submodel analysis.
C3D10MP elements; global analysis.
C3D10MP elements; submodel analysis.
C3D20P elements; global analysis.
C3D20P elements; submodel analysis.
C3D20RP elements; global analysis.
C3D20RP elements; submodel analysis.
CAX4RP elements; global analysis.
CAX4RP elements; submodel analysis.
CAX6MP elements; global analysis.
CAX6MP elements; submodel analysis.
CAX8P elements; global analysis.
CAX8P elements; submodel analysis.
CAX8RP elements; global analysis.
CAX8RP elements; submodel analysis.
CPE4P elements; global analysis.
CPE4P elements; submodel analysis.
CPE6MP elements; global analysis.
CPE6MP elements; submodel analysis.
CPE8P elements; global analysis.
CPE8P elements; submodel analysis.
CPE8RP elements; global analysis.
CPE8RP elements; submodel analysis.