SOLID285


3D 4-Node Tetrahedral Structural Solid

Valid Products: Pro | Premium | Enterprise | PrepPost | Solver | AS add-on

SOLID285 Element Description

SOLID285 is a low-order 3D, 4-node element for solid structure analysis. The default element behavior has linear displacement with hydrostatic pressure, but also offers a pure linear displacement option. The element is suitable for modeling irregular meshes (such as those generated by various CAD/CAM systems).

With its hydrostatic pressure degree of freedom, the element is suitable for use with general materials (including incompressible materials). With its with displacement degree of freedom only, it is suitable only for linear elastic material and elastoplastic material with very small plastic deformations.

The element is defined by four nodes having either of the following configurations (depending on the formulation selected):

  • Four degrees of freedom at each node: three translations in the nodal x, y, and z directions, and one hydrostatic pressure (HDSP).

  • Three degrees of freedom at each node: three translations in the nodal x, y, and z directions.

HDSP is real hydrostatic pressure for all materials except nearly incompressible hyperelastic materials. For nearly incompressible materials, HDSP is the volume change rate at each node. In a nonlinear analysis, you can control the tolerance of HDSP separately (CNVTOL).

The element has plasticity, hyperelasticity, creep, stress stiffening, large deflection, and large strain capabilities. It is capable of simulating deformations of nearly incompressible elastoplastic materials, nearly incompressible hyperelastic materials, and fully incompressible hyperelastic materials.

For more details about this element, see SOLID285.

Figure 285.1: SOLID285 Geometry

SOLID285 Geometry

SOLID285 Input Data

The geometry, node locations, and the coordinate system for this element are shown in Figure 285.1: SOLID285 Geometry.

In addition to the nodes, the element input data includes the orthotropic or anisotropic material properties. Orthotropic and anisotropic material directions correspond to the element coordinate directions. The element coordinate system orientation is as described in the Material Reference.

Element loads are described in Element Loading. Pressure loads may be input as surface loads on the element faces as shown by the circled numbers on Figure 285.1: SOLID285 Geometry. Positive pressures act into the 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 temperature pattern, unspecified temperatures default to TUNIF.

As described in Coordinate Systems, you can use ESYS to orient the material properties and strain/stress output. Use RSYS to choose output that follows the material coordinate system or the global coordinate system.

KEYOPT(16) = 1 activates steady-state analysis (defined via SSTATE). For more information, see Steady-State Rolling in the Theory Reference. For a steady-state analysis, elements must be numbered as shown in Figure 285.1: SOLID285 Geometry.

You can apply an initial stress state to this element (INISTATE). For more information, see Initial State in the Advanced Analysis Guide.

The effects of pressure load stiffness are automatically included for this element. If an unsymmetric matrix is needed for pressure load stiffness effects, use NROPT,UNSYM.

The next table summarizes the element input. Element Input gives a general description of element input.

SOLID285 Input Summary

Nodes

I, J, K, L

Degrees of Freedom

UX, UY, UZ, HDSP (KEYOPT(1) = 0)

UX, UY, UZ (KEYOPT(1) = 1)

Real Constants

None

Material Properties
TB command: See Element Support for Material Models for this element.
MP command: EX, EY, EZ, ALPX, ALPY, ALPZ (or CTEX, CTEY, CTEZ or THSX, THSY, THSZ), PRXY, PRYZ, PRXZ (or NUXY, NUYZ, NUXZ), DENS, GXY, GYZ, GXZ, ALPD, BETD, DMPR, DMPS
Surface Loads
Pressures -- 

face 1 (J-I-K), face 2 (I-J-L), face 3 (J-K-L), face 4 (K-I-L)

To define general surface loads (or surface tractions) on the faces, issue SFCONTROL.

Body Loads
Temperatures -- 

T(I), T(J), T(K), T(L)

Body force densities -- 

The element values in the global X, Y, and Z directions. For analyses supporting complex loading, imaginary X, Y, and Z values are supported (see the BFE command for details).

Special Features
KEYOPT(1)

Element formulation:

0 -- 

Mixed u-P formulation with linear displacement and hydrostatic pressure at each node (default)

1 -- 

Pure displacement formulation with linear displacement in the element

KEYOPT(16)

Steady-state analysis flag:

0 -- 

Steady-state analysis disabled (default)

1 -- 

Enable steady-state analysis

Solid 285 Element Technology

This element has only a mixed u-P formulation with pressure stabilization. For more information, see Element Technologies.

SOLID285 Output Data

The solution output associated with the element is in two forms:

Several items are illustrated in Figure 285.2: SOLID285 Stress Output. The element stress directions are parallel to the element coordinate system. A general description of solution output is given in The Item and Sequence Number Table. See the Basic Analysis Guide for ways to view results.

Figure 285.2: SOLID285 Stress Output

SOLID285 Stress Output


The Element Output Definitions table uses the following notation:

A colon (:) in the Name column indicates that 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 letter or number refers to a table footnote that describes when the item is conditionally available, and “-” indicates that the item is not available.

Table 285.1: SOLID285 Element Output Definitions

NameDefinitionOR
ELElement Number-Y
NODESNodes - I, J, K, L-Y
MATMaterial number-Y
VOLU:Volume-Y
XC, YC, ZCLocation where results are reportedY3
PRESPressures P1 at nodes J, I, K; P2 at I, J, L; P3 at J, K, L; P4 at K, I, L-Y
TEMPTemperatures T(I), T(J), T(K), T(L)-Y
S:X, Y, Z, XY, YZ, XZStressesYY
S:1, 2, 3Principal stresses-Y
S:INTStress intensity-Y
S:EQVEquivalent stress-Y
EPEL:X, Y, Z, XY, YZ, XZElastic strainsYY
EPEL:EQVEquivalent elastic strains [6]-Y
EPTH:X, Y, Z, XY, YZ, XZThermal strains11
EPTH: EQVEquivalent thermal strains [6]11
EPPL:X, Y, Z, XY, YZ, XZPlastic strains [7]11
EPPL:EQVEquivalent plastic strains [6]11
EPCR:X, Y, Z, XY, YZ, XZCreep strains11
EPCR:EQVEquivalent creep strains [6]11
EPTO:X, Y, Z, XY, YZ, XZTotal mechanical strains (EPEL + EPPL + EPCR)Y-
EPTO:EQVTotal equivalent mechanical strains (EPEL + EPPL + EPCR)Y-
NL:EPEQAccumulated equivalent plastic strain11
NL:CREQAccumulated equivalent creep strain11
NL:SRATPlastic yielding (1 = actively yielding, 0 = not yielding)11
NL:HPRESHydrostatic pressure11
SEND:ELASTIC, PLASTIC, CREEP, ENTOStrain energy density-1
LOCI:X, Y, ZIntegration point locations-4
SVAR:1, 2, ... , NState variables-5

  1. Nonlinear solution, output only if the element has a nonlinear material, or if large-deflection effects are enabled (NLGEOM,ON) for SEND.

  2. Output only if element has a thermal load.

  3. Available only at centroid as a *GET item.

  4. Available only if OUTRES,LOCI is used.

  5. Available only if the UserMat subroutine and TB,STATE command are used.

  6. The equivalent strains use an effective Poisson's ratio: for elastic and thermal this value is set by the user (MP,PRXY); for plastic and creep this value is set at 0.5.

  7. For the shape memory alloy material model, transformation strains are reported as plasticity strain EPPL.

Table 285.2: SOLID285 Item and Sequence Numbers lists output available through ETABLE using the Sequence Number method. See The General Postprocessor (POST1) and The Item and Sequence Number Table in this document for more information. The following notation is used in Table 285.2: SOLID285 Item and Sequence Numbers:

Name

output quantity as defined in Table 285.1: SOLID285 Element Output Definitions

Item

predetermined Item label for ETABLE command

I,J,...,R

sequence number for data at nodes I, J, ..., R

Table 285.2: SOLID285 Item and Sequence Numbers

Output Quantity NameETABLE and ESOL Command Input
ItemIJKLM,...,R
P1SMISC213--
P2SMISC45-6-
P3SMISC-789-
P4SMISC11-1012-

SOLID285 Assumptions and Restrictions

  • The element must not have a zero volume.

  • Elements may be numbered either as shown in Figure 285.1: SOLID285 Geometry, or may have node L below the I, J, K plane (except when KEYOPT(16) = 1).

  • For a steady-state analysis (KEYOPT(16) = 1), elements must be numbered as shown in Figure 285.1: SOLID285 Geometry.

  • Only the sparse solver is valid when using this element with KEYOPT(1) = 0.

  • Pure displacement formulation should not be used for nearly incompressible and fully incompressible materials, such as hyperelastic materials, elastoplastic material when plastic deformation is significant and linear elastic materials when Poisson ratio is greater than 0.499.

  • The default formulation (KEYOPT(1) = 0) uses Lagrange multipliers and cannot be used in a substructure generation pass. (See Assumptions and Restrictions (Within Superelement) in the Theory Reference.)

  • Support is available for static and transient analyses.

  • The element may not offer sufficient accuracy for bending-dominant problems, especially if the mesh is not fine enough.

  • On the interfaces of different materials, the elements should not share nodes because the hydrostatic pressure value is not continuous at those nodes. This behavior can be overcome by either:

    • Coupling the displacements of the nodes on the interface but leaving HDSP unconstrained, or

    • Adding bonded contact elements on the interfaces.

  • Stress stiffening is always included in geometrically nonlinear analyses (NLGEOM,ON). Prestress effects can be activated by the PSTRES command.

SOLID285 Product Restrictions

When used in the product(s) listed below, the stated product-specific restrictions apply to this element in addition to the general assumptions and restrictions given in the previous section.

Ansys Mechanical Premium  —  

  • Fracture parameter calculation is not available.

  • Rezoning is not available.

  • Nonlinear adaptivity is not available.