This option is used to define properties of solid (continuum) elements, infinite elements, acoustic finite and infinite elements, particle elements, and truss elements.
Products: Abaqus/Standard Abaqus/Explicit Abaqus/CFD Abaqus/CAE
Type: Model data
Level: Part, Part instance
Abaqus/CAE: Property module
“Solid (continuum) elements,” Section 28.1.1 of the Abaqus Analysis User's Guide
“Infinite elements,” Section 28.3.1 of the Abaqus Analysis User's Guide
“Continuum particle elements,” Section 33.2.1 of the Abaqus Analysis User's Guide
“Truss elements,” Section 29.2.1 of the Abaqus Analysis User's Guide
This parameter applies only to Abaqus/Standard analyses.
This parameter can be used only with three-dimensional brick solid elements that have only displacement degrees of freedom. Include this parameter if the solid is made up of several layers of material.
The COMPOSITE and MATERIAL parameters are mutually exclusive.
Set this parameter equal to the name of the element set containing the elements for which the material behavior is being defined.
Set this parameter equal to the name of the material to be used with these elements.
The COMPOSITE and MATERIAL parameters are mutually exclusive.
This parameter is required only for generalized plane strain elements and acoustic infinite elements; it is ignored for all other element types.
Set this parameter equal to either the node number of the reference node or the name of a node set containing the reference node. If the name of a node set is chosen, the node set must contain exactly one node.
Set this parameter equal to the name of an orientation definition (“Orientations,” Section 2.2.5 of the Abaqus Analysis User's Guide) to be used to define a local coordinate system for material calculations in the elements in this set. This parameter is required when the material is anisotropic.
For a composite solid this orientation, together with the orientation angle specified on the layer data lines, can also be used to define the material orientations in the individual layers. Alternatively, a material orientation can be specified by referencing an orientation definition on each layer data line. In this case the reference given on the ORIENTATION parameter is ignored. Any layer definition line that does not have an orientation reference or an angle specified will use the section orientation defined on the keyword line.
In an Abaqus/Explicit analysis, set this parameter equal to the name of a section controls definition (see “Section controls,” Section 27.1.4 of the Abaqus Analysis User's Guide) to be used to specify a nondefault hourglass control formulation option or scale factor. The *SECTION CONTROLS option can be used to select the hourglass control and order of accuracy of the formulation for two- and three-dimensional solid elements and to select the kinematic formulation for 8-node brick elements.
In an Abaqus/Standard analysis, set this parameter equal to the name of a section controls definition (see “Section controls,” Section 27.1.4 of the Abaqus Analysis User's Guide) to be used to specify the enhanced hourglass control formulation or to be used in a subsequent Abaqus/Explicit import analysis.
This parameter is relevant only when the COMPOSITE parameter is used.
Set this parameter equal to the name of a composite layup (see Chapter 23, “Composite layups,” of the Abaqus/CAE User's Guide). Abaqus/CAE uses this name to identify the composite layup that contains the solid section.
This parameter can be used only with acoustic infinite elements in Abaqus/Explicit. It defines the number of ninth-order polynomials that will be used to resolve the variation of the acoustic field in the infinite direction. Set this parameter equal to N to indicate that the first N members of the set of ninth-order polynomials are to be used. The default is ORDER=10, which is the value always used in Abaqus/Standard.
This parameter applies only to Abaqus/Standard analyses.
This parameter can be used only with composite elements. It defines the stacking direction with respect to a pair of element faces. Set this parameter equal to 1, 2, or 3. The default is STACK DIRECTION=3.
This parameter is relevant only when the COMPOSITE parameter is used.
Include this parameter if the layers in the composite shell are symmetric about a central core. This parameter cannot be used if spatially varying orientation angles are defined on any composite layer using distributions (“Distribution definition,” Section 2.8.1 of the Abaqus Analysis User's Guide).
First (and only) line:
Enter any attribute values required. The default for the first attribute is 1.0. See the description in Part VI, “Elements,” of the Abaqus Analysis User's Guide of the element type being used for a definition of the data required.
First line:
Layer thickness. The layer thickness will be adjusted such that the sum of the layer thicknesses corresponds to the element length in the stack direction.
Number of integration points to be used through the layer. This number must be an odd number. The default is one integration point.
Name of the material forming this layer.
Name of the orientation to be used with this layer, an orientation angle, , or in Abaqus/Standard the name of a distribution (“Distribution definition,” Section 2.8.1 of the Abaqus Analysis User's Guide) that defines spatially varying orientation angles. If the name of an orientation is used, the orientation cannot be defined with distributions. Orientation angles (in degrees) are measured positive counterclockwise relative to the local direction, which must be defined on the *ORIENTATION definition. If the local directions for a composite solid section are defined with user subroutine ORIENT (see “ORIENT,” Section 1.1.15 of the Abaqus User Subroutines Reference Guide), orientation angles defined on the data lines of the section definition are ignored.
Name of the ply. Required only for composite layups defined in Abaqus/CAE.
Repeat this data line as often as necessary to define the properties for each layer of the composite solid. If the SYMMETRIC parameter is included, specify only half the layers, from the bottom layer to the midplane.