PLANE82
2D 8-Node
Structural Solid
PLANE82 Element Description
Although this archived element is available for use in your analysis, Ansys, Inc. recommends using a current-technology element such as PLANE183. |
PLANE82 provides accurate results for mixed (quadrilateral-triangular) automatic meshes and can tolerate irregular shapes without as much loss of accuracy. The eight-node elements have compatible displacement shapes and are well suited to model curved boundaries.
The 8-node element is defined by eight nodes having two degrees of freedom at each node: translations in the nodal x and y directions. The element may be used as a plane element or as an axisymmetric element. The element has plasticity, creep, swelling, stress stiffening, large deflection, and large strain capabilities. Various printout options are also available. See SOLID273 for a description of an axisymmetric element which accepts nonaxisymmetric loading.
PLANE82 Input Data
The geometry, node locations, and the coordinate system for this element are shown in Figure 82.1: PLANE82 Geometry.
A triangular-shaped element may be formed by defining the same node number for nodes K, L and O. Besides the nodes, the element input data includes a thickness (TK) (for the plane stress option only) and the orthotropic material properties. Orthotropic material directions correspond to the element coordinate directions. The element coordinate system orientation is as described in Coordinate Systems.
Element loads are described in Element Loading. Pressures may be input as surface loads on the element faces as shown by the circled numbers on Figure 82.1: PLANE82 Geometry. Positive pressures act into the element. Temperatures and fluences 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). If all corner node temperatures are specified, each midside node temperature defaults to the average temperature of its adjacent corner nodes. For any other input temperature pattern, unspecified temperatures default to TUNIF. Similar defaults occurs for fluence except that zero is used instead of TUNIF.
The nodal forces, if any, should be input per unit of depth for a plane analysis (except for KEYOPT(3) = 3) and on a full 360° basis for an axisymmetric analysis. KEYOPT(5) and KEYOPT(6) parameters provide various element printout options (see Element Solution).
You cannot set initial state conditions (INISTATE) using this element. You can set initial state conditions using current-technology elements (such as LINK180,SHELL181). To continue using initial state conditions in future versions of Mechanical APDL, consider using a current element technology. For more information, see Legacy vs. Current Element Technologies in the Element Reference. For more information about setting initial state values, see INISTATE and Initial State Loading in the Basic Analysis Guide.
Pressure load stiffness effects are included in linear eigenvalue buckling automatically. If an unsymmetric matrix is needed for pressure load stiffness effects, use NROPT,UNSYM.
A summary of the element input is given in "PLANE82 Input Summary". A general description of element input is given in Element Input. For axisymmetric applications see Harmonic Axisymmetric Elements.
PLANE82 Input Summary
- Nodes
I, J, K, L, M, N, O, P
- Degrees of Freedom
UX, UY
- Real Constants
None, if KEYOPT (3) = 0, 1, or 2 THK - Thickness, if KEYOPT (3) = 3 - Material Properties
EX, EY, EZ, PRXY, PRYZ, PRXZ (or NUXY, NUYZ, NUXZ), ALPX, ALPY, ALPZ (or CTEX, CTEY, CTEZ or THSX, THSY, THSZ), DENS, GXY, BETD, ALPD, DMPR - Surface Loads
- Pressures --
face 1 (J-I), face 2 (K-J), face 3 (I-K), face 4 (I-L)
- Body Loads
- Temperatures --
T(I), T(J), T(K), T(L), T(M), T(N), T(O), T(P)
- Fluences --
FL(I), FL(J), FL(K), FL(L), FL(M), FL(N), FL(O), FL(P)
- Special Features
Plasticity (BISO, BKIN, DP, ANISO) Creep (CREEP, RATE) Swelling (SWELL) Elasticity (MELAS) Other material (USER) Stress stiffening Large deflection Large strain Birth and death Adaptive descent Items in parentheses refer to
Lab
data tables associated with the TB,Lab
command.- KEYOPT(3)
Element behavior:
- 0 --
Plane stress
- 1 --
Axisymmetric
- 2 --
Plane strain (Z strain = 0.0)
- 3 --
Plane stress with thickness (TK) real constant input
- KEYOPT(5)
Extra element output:
- 0 --
Basic element solution
- 1 --
Repeat basic solution for all integration points
- 2 --
Nodal Stress Solution
- KEYOPT(6)
Extra surface output:
- 0 --
Basic element solution
- 1 --
Surface solution for face I-J also
- 2 --
Surface solution for both faces I-J and K-L also (surface solution valid for linear materials only)
- 3 --
Nonlinear solution at each integration point also
- 4 --
Surface solution for faces with nonzero pressure
PLANE82 Output Data
The solution output associated with the element is in two forms:
Nodal displacements included in the overall nodal solution
Additional element output as shown in Table 82.1: PLANE82 Element Output Definitions
Several items are illustrated in Figure 82.2: PLANE82 Stress Output.
The element stress directions are parallel to the element coordinate system. Surface stresses are available on any face. Surface stresses on face IJ, for example, are defined parallel and perpendicular to the IJ line and along the Z axis for a plane analysis or in the hoop direction for an axisymmetric analysis. A general description of solution output is given in Solution Output. See the Basic Analysis Guide for ways to view results.
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 82.1: PLANE82 Element Output Definitions
Name | Definition | O | R |
---|---|---|---|
EL | Element Number | Y | Y |
NODES | Corner nodes - I, J, K, L | Y | Y |
MAT | Material number | Y | Y |
THICK | Average thickness | Y | Y |
VOLU: | Volume | Y | Y |
XC, YC | Location where results are reported | Y | 3 |
PRES | Pressures P1 at nodes J,I; P2 at K,J; P3 at L,K; P4 at I,L | Y | Y |
TEMP | Temperatures T(I), T(J), T(K), T(L), T(M), T(N), T(O), T(P) | Y | Y |
FLUEN | Fluences FL(I), FL(J), FL(K), FL(L), FL(M), FL(N), FL(O), FL(P) | Y | Y |
S:X, Y, Z, XY | Stresses (SZ = 0.0 for plane stress elements) | Y | Y |
S:1, 2, 3 | Principal stresses | Y | - |
S:INT | Stress intensity | Y | - |
S:EQV | Equivalent stress | Y | Y |
EPEL:X, Y, Z, XY | Elastic strains | Y | Y |
EPEL:1, 2, 3 | Principal elastic strains | Y | - |
EPEL:EQV | Equivalent elastic strain [4] | - | Y |
EPTH:X, Y, Z, XY | Average thermal strains | Y | Y |
EPTH:EQV | Equivalent thermal strain [4] | - | Y |
EPPL:X, Y, XY, Z | Average plastic strains | 2 | 2 |
EPPL:EQV | Equivalent plastic strain [4] | - | 2 |
EPCR:X, Y, XY, Z | Average creep strains | 2 | 2 |
EPCR:EQV | Equivalent creep strain [4] | - | 2 |
EPSW: | Swelling strain | 2 | 2 |
NL:EPEQ | Equivalent plastic strain | 2 | 2 |
NL:SRAT | Ratio of trial stress to stress on yield surface | 2 | 2 |
NL:SEPL | Equivalent stress on stress-strain curve | 2 | 2 |
NL:HPRES | Hydrostatic pressure | - | 2 |
FACE | Face label | 1 | 1 |
EPEL(PAR, PER, Z) | Surface elastic strains (parallel, perpendicular, Z or hoop) | 1 | 1 |
TEMP | Surface average temperature | 1 | 1 |
S(PAR, PER, Z) | Surface stresses (parallel, perpendicular, Z or hoop) | 1 | 1 |
SINT | Surface stress intensity | 1 | 1 |
SEQV | Surface equivalent stress | 1 | 1 |
LOCI:X, Y, Z | Integration point locations | - | Y |
Note: For axisymmetric solutions, the X, Y, XY, and Z stress and strain outputs correspond to the radial, axial, in-plane shear, and hoop stresses and strains.
Table 82.3: PLANE82 Item and Sequence Numbers lists output available through the ETABLE command using the Sequence Number method. See Creating an Element Table in the Basic Analysis Guide and The Item and Sequence Number Table in this manual for more information. The following notation is used in Table 82.3: PLANE82 Item and Sequence Numbers:
- Name
output quantity as defined in the Table 82.1: PLANE82 Element Output Definitions
- Item
predetermined Item label for ETABLE command
- E
sequence number for single-valued or constant element data
- I,J,...,P
sequence number for data at nodes I,J,...,P
See Surface Solution for the item and sequence numbers for surface output for the ETABLE command.
PLANE82 Assumptions and Restrictions
The area of the element must be positive.
The element must lie in a global X-Y plane as shown in Figure 82.1: PLANE82 Geometry and the Y-axis must be the axis of symmetry for axisymmetric analyses. An axisymmetric structure should be modeled in the +X quadrants.
A face with a removed midside node implies that the displacement varies linearly, rather than parabolically, along that face. See Quadratic Elements (Midside Nodes) in the Modeling and Meshing Guide for more information about the use of midside nodes.
PLANE82 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 Professional —
The ALPD and BETD material properties are not allowed.
Fluence body loads are not applicable.
The only special feature allowed is stress stiffening.
KEYOPT(6) = 3 is not applicable.