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INTER203 is a 2-D 6-node quadratic interface element used for the 2-D modeling of structural assemblies. When used in conjunction with 2-D quadratic structural elements (PLANE82 and PLANE183), INTER203 simulates the interface surfaces and the subsequent delamination process, where the separation is represented by an increasing displacement between nodes, within the interface element itself, that are initially coincident. The element can be used either as a plane element (plane stress or plane strain) or as an axisymmetric element. It is defined by six nodes having two degrees of freedom at each node: translations in the nodal x and y directions.
See Cohesive Zone Material Model and INTER203 in the Theory Reference for ANSYS and ANSYS Workbench for more details about this element.
Also see Interface Delaminaton and Failure Simulation in the Structural Analysis Guide for more details on the interface failure/delamination capability in ANSYS.
The element geometry, node locations, connectivity, and the nodal coordinate system are shown in Figure 203.1: "INTER203 Geometry". The element geometry is defined by 6 nodes, which form bottom and top lines of the element. The bottom line is defined by nodes I, J, M; and the top line is defined by nodes K, L, O. This element has 2 integration points. Dropping mid side nodes M or O is not permitted.
INTER203 is used to simulate a separation along an interface defined by this element. At the outset of your simulation, nodes I,L, nodes M,O and nodes J,K are coincident, with each other, and with the corresponding nodes in the adjacent structural elements. The subsequent separation of the adjacent elements (usually defined contiguously as components) is represented by an increasing displacement between the initially coincident nodes within this element.
Temperatures may be input as element body loads at the nodes. The node I temperature T(I), defaults to TUNIF. If all other temperatures are unspecified, they default to T(I). For any other input pattern, unspecified temperatures default to TUNIF.
Input the nodal forces, if any, per unit of depth for a plane analysis (except for KEYOPT(3) = 3) and on a full 360° basis for an axisymmetric analysis.
The next table summarizes the element input. See Element Input in the Elements Reference for a general description of element input.
I, J, K, L, M, , O
UX, UY
| None, if KEYOPT(3) = 0, 1, or 2 |
| THK - Plane stress with thickness, if KEYOPT(3) = 3 |
T(I), T(J), T(K), T(L), T(M), T(O)
Temperature is used only to evaluate the material properties.
Interface material associated with TB,CZM.
See Cohesive Zone Material Model and INTER203 in the Theory Reference for ANSYS and ANSYS Workbench for details on the material model.
Element behavior:
Plane stress
Axisymmetric
Plane strain (Z strain = 0.0)
Plane stress with thickness (THK) real constant input
The solution output associated with the element is in two forms:
Nodal items such as nodal displacements are included in the overall nodal solution.
Element items such as tractions and separations are element outputs as shown in Table 203.1: "INTER203 Element Output Definitions".
The output directions for element items are parallel to the local element coordinate system based on the element midplane as illustrated in Figure 203.2: "INTER203 Stress Output". See Cohesive Zone Material Model and INTER203 in the Theory Reference for ANSYS and ANSYS Workbench for details.
A general description of solution output is given in Solution Output. See the Basic Analysis Guide for ways to review results.
The Element Output Definitions table uses the following notation:
A colon (:) in the Name column indicates the item can be accessed by the Component Name method [ETABLE, ESOL]. The O column indicates the availability of the items in the file Jobname.OUT. The R column indicates the availability of the items in the results file.
In either the O or R columns, Y indicates that the item is always available, a number refers to a table footnote that describes when the item is conditionally available, and a - indicates that the item is not available.
This element is not supported for initial stress.
Pressure as a type of surface load on element faces is not supported by this element.
This element is based on the local coordinate system. ESYS is not permitted.
This element is only available for static analyses.