REINF264
3D Discrete Reinforcing
REINF264 Element Description
For a structural reinforcing analysis, use REINF264 with standard 3D link, beam, shell and solid elements (referred to here as the base elements) to provide extra reinforcing to those elements. For a thermal reinforcing analysis, the supported base elements are thermal solids SOLID278, SOLID279, and SOLID291.
The element is suitable for simulating reinforcing fibers with arbitrary orientations. Each fiber is modeled separately as a spar that has only uniaxial stiffness (default) or conductivity. When solid base elements are used, the element can also account for bending and torsional stiffness with either square (SECCONTROL,,,1) or circular (SECCONTROL,,,2) cross sections. You can specify multiple reinforcing fibers in one REINF264 element. The nodal locations, degrees of freedom, and connectivity of the REINF264 element are identical to those of the base element.
For smeared reinforcing modeling options, use the REINF263 and REINF265 elements.
REINF264 has plasticity, stress-stiffening, creep, large-deflection, and large-strain capabilities.
For more information, see Reinforcing and Direct Element Embedding in the Structural Analysis Guide.
Table 264.1: REINF264 Geometry
3D 8-Node Solid or Solid Shell | 3D 20-Node Solid |
3D 4-Node Tetrahedral Solid | 3D 10-Node Tetrahedral Solid |
3D 4-Node Shell | 3D 8-Node Shell |
3D 2-Node Beam | 3D 3-Node Beam |
3D 2-Node Spar |
REINF264 Input Data
The geometry and nodal locations for this element are shown in Table 264.1: REINF264 Geometry. The REINF264 element and its base element share the same nodes and element connectivity. Each reinforcing fiber is indicated by its intersection points (II, JJ for linear base elements, and II, JJ, KK for quadratic base elements) with the base elements.
You can easily create REINF264 elements from the selected base elements (EREINF). Section commands (SECTYPE and SECDATA) define the material ID, cross-section area, and location of reinforcing fibers. See Reinforcing and Direct Element Embedding in the Structural Analysis Guide for more information about creating REINF264 elements.
For structural analysis, REINF264 allows tension-only or compression-only reinforcing fibers. You can specify the desired fiber behavior (SECCONTROL).
The element can account for redundant base element material where the
reinforcing fibers are located
(SECCONTROL,,REMBASE
).
The coordinate system for one reinforcing fiber is shown in Figure 264.1: REINF264 Coordinate System. The coordinate system is solely determined by intersection points II, JJ, and KK; therefore, the element coordinate system (/PSYMB,ESYS) is not relevant for this element.
For a structural analysis, REINF264 allows body-force-density element loading (BFE), as shown in these examples:
BFE,2,FORC,1, |
BFE,2,FORC,4, |
If applying body-force density to REINF264 elements, the program applies a uniform load to all members in the element. You can apply non-uniform body-force density to individual members via the mesh-independent method by loading to MESH200 elements.
Apply other structural element loading only to the base element. The temperature of the REINF264 element is identical to the temperature of the base element in a structural analysis.
For thermal reinforcing analysis, REINF264 allows heat-generation (HGEN) element loading (BFE), as shown in these examples:
BFE,2,HGEN,1, |
BFE,2,HGEN,3,%tab1%,, ! Member 2 of element 2 |
BFE,2,HGEN,5,%tab2%,, ! Member 3 of element 2 |
BFE,2,HGEN,7, |
VALUE1 and VALUE2 are at the
corner points II JJ only. Midpoint values are not allowed. |
If using the mesh-independent method for defining reinforcing, apply the HGEN load to the MESH200 elements instead. |
You can apply an initial state to this element in either of the following ways:
By applying an initial state directly on each REINF264 element (INISTATE).
By using the mesh-independent method for defining reinforcing to apply an initial state to MESH200 elements, enabling Mechanical APDL to transfer the initial state to the resulting reinforcing elements automatically. For more information, see Applying an Initial State to Reinforcing Elements in the Structural Analysis Guide.
A summary of the element input follows.
REINF264 Input Summary
- Nodes
Structural
Same as those of the base element, as shown:
Base Element REINF264 Nodes 3D 8-Node Solid or Solid Shell I,J,K,L,M,N,O,P 3D 20-Node Solid I,J,K,L,M,N,O,P,Q,R,S,T,U,V,W,X,Y,Z,A,B 3D 4-Node Tetrahedral Solid I,J,K,L 3D 10-Node Tetrahedral Solid I,J,K,L,M,N,O,P,Q,R 3D 4-Node Shell I,J,K,L 3D 8-Node Shell I,J,K,L,M,N,O,P 3D 2-Node Beam I,J,K (K is an optional orientation node) 3D 3-Node Beam I,J,K,L (L is an optional orientation node) 3D 2-Node Spar I,J Thermal
- Degrees of Freedom
Structural
Same as those of the base element, as shown:
Base Element REINF264 DOFs 3D 8-Node Solid or Solid Shell UX, UY, UZ 3D 20-Node Solid UX, UY, UZ 3D 14-Node Tetrahedral Solid UX, UY, UZ 3D 10-Node Tetrahedral Solid UX, UY, UZ 3D 4-Node Shell UX, UY, UZ, ROTX, ROTY, ROTZ 3D 8-Node Shell UX, UY, UZ, ROTX, ROTY, ROTZ 3D 2-Node Beam UX, UY, UZ, ROTX, ROTY, ROTZ 3D 3-Node Beam UX, UY, UZ, ROTX, ROTY, ROTZ 3D 2-Node Spar UX, UY, UZ Thermal
- Real Constants
None - Material Properties
TB command: See Element Support for Material Models for this element. MP command: EX, (PRXY or NUXY), ALPX (or CTEX or THSX), DENS, GXY, ALPD, BETD, DMPR, DMPS, CP, KXX - Surface Loads
None - Body Loads
- Temperatures (Structural) --
Same as those of the base element
- Body-Force Density --
Standard method -- Specified via BFE
Mesh-independent method -- Specified via BFE on MESH200 elements
- Thermal --
HGEN –
- Special Features
- KEYOPTS
None
REINF264 Structural or Thermal 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 264.2: REINF264 Element Output Definitions – Structural Analysis.
The axial stress component is illustrated in Figure 264.2: REINF264 Structural or Thermal Output.
Unlike layered solid or shell elements (such as SHELL181), REINF264 always outputs the element solution for all reinforcing layers. You can select solution items for a specific reinforcing layer (LAYER) for listing and visualization by using full graphics (/GRAPHICS,FULL). Visualization via PowerGraphics (/GRAPHICS,POWER) is not affected by the LAYER command; all reinforcing layers are displayed simultaneously. See the Basic Analysis Guide for ways to review results.
REINF264 element solution is always output in the layer coordinate system and does not support transformation to a different coordinate system. RSYS has no effect on REINF264 element solution.
To inspect REINF264 element results, select only REINF264 element results or adjust the translucency level of the base elements before executing any plotting command. REINF264 display options are also available directly via the GUI ( ).
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 264.2: REINF264 Element Output Definitions – Structural Analysis
Name | Definition | O | R |
---|---|---|---|
EL | Element number and name | - | Y |
NODES | Nodes (as shown in "REINF264 Input Summary") | - | Y |
MAT | Material number | - | Y |
AREA | Averaged cross-section area of reinforcing fibers | - | Y |
VOLU: | Volume | - | Y |
XC, YC, ZC | Center location | - | 3 |
TEMP |
T1, T2 for reinforcing fiber 1; T3, T4 for reinforcing fiber 2; ending with temperatures for the last reinforcing fiber NL (2 * NL maximum) | - | Y |
S:x | Axial stresses (uniaxial stiffness only) | 2 | Y |
S:x, xy, xz | Elastic stresses (uniaxial, bending, and torsional stiffness) | 2 | Y |
EPEL:x | Axial elastic strains (uniaxial stiffness only) | 2 | Y |
EPEL:x, xy, xz | Elastic strains (uniaxial, bending, and torsional stiffness) | 2 | Y |
EPTH:x | Axial thermal strains | 2 | Y |
EPPL:x | Axial plastic strains | 2 | 1 |
EPCR:x | Axial creep strains | 2 | 1 |
EPTO:x | Total axial mechanical strains (EPEL + EPPL + EPCR) | Y | - |
NL:EPEQ | Accumulated equivalent plastic strain | - | 1 |
NL:CREQ | Accumulated equivalent creep strain | - | 1 |
NL:SRAT | Plastic yielding (1 = actively yielding, 0 = not yielding) | - | 1 |
NL:PLWK | Plastic work/volume | - | 1 |
N11 | Averaged axial force | - | Y |
LOCI:X, Y, Z | Integration point locations | - | 4 |
Table 264.3: REINF264 Element Output Definitions – Thermal Analysis
Name | Definition | O | R |
---|---|---|---|
EL | Element number and name | 2 | Y |
NODES | Nodes (as shown in "REINF264 Input Summary") | 2 | Y |
MAT | Material number | 2 | Y |
AREA | Averaged cross-section area of reinforcing fibers | - | Y |
VOLU: | Volume | 2 | Y |
XC, YC, ZC | Center location | - | 3 |
BFE TEMP |
T1, T2 for reinforcing members [5] | - | Y |
TG:x | Temperature gradient along the fiber for all reinforcing members [5] | 2 | Y |
TF:x | Heat flux along the fiber for all reinforcing members [5] | 2 | Y |
LOCI:X, Y, Z | Integration point locations | - | 4 |
Nonlinear solution output if the element has a nonlinear material.
For structural analysis, stresses, total strains, plastic strains, elastic strains, creep strains, and thermal strains in the element coordinate system are available for output. For thermal analysis, temperature gradients and heat flux in the element coordinate system are available for output. For stress and elastic strain output, by default (SECCONTROL,,,0), only axial components are available. With the axial, bending, and torsional stiffness option (SECCONTROL,,,1 or 1 or SECCONTROL,,,2), both axial and shear stress and elastic strain components are available.
Available only at centroid as a *GET item.
Available only if OUTRES,LOCI is used.
Table 264.4: REINF264 Item and Sequence Numbers lists output available via the ETABLE command using the Sequence Number method. See Creating an Element Table and The Item and Sequence Number Table in this document for more information. The following notation is used in Table 264.4: REINF264 Item and Sequence Numbers:
- Name
output quantity as defined in Table 264.2: REINF264 Element Output Definitions – Structural Analysis
- Item
predetermined Item label for ETABLE
- E
sequence number for single-valued or constant element data
The i
value (where i
= 1, 2, 3, ...,
NL
) represents the reinforcing member number of the element.
NL
is the maximum reinforcing member number (1
NL
250).
REINF264 Assumptions and Restrictions
Zero-volume elements are invalid.
This element can be used only with base element types:
A valid base element must be present for each REINF264 element.
The reinforcing element is firmly attached to its base element. No relative movement between the reinforcing element and the base is allowed. For a thermal analysis, the temperature field is continuous at the interface between the base element and the reinforcing.
Through-thickness reinforcing is not allowed in shells and layered solid elements.
Stress stiffening is always included in geometrically nonlinear analyses (NLGEOM,ON). You can activate prestress effects via the PSTRES command.
The warping degree of freedom in beam base elements are not accounted for.
REINF264 does not support BEAM188 with the quadratic or cubic interpolation option (KEYOPT(3)).
To simulate the tension-/compression-only reinforcing fibers, a nonlinear iterative solution approach is necessary.
Linear tetrahedral base elements (degenerated SOLID185 and SOLID285) have constant stress/strain in the element and are therefore not applicable to REINF264 bending and torsional stiffness (SECCONTROL,,,1).
By default, the program uses a zero effective Poisson’s ratio to calculate equivalent strain (PLNSOL, PLESOL, and PRESOL) for REINF264 elements with the axial, bending, and torsional stiffness option (SECCONTROL,,,1 or SECCONTROL,,,2). If necessary, you can define a non-zero effective Poisson’s ratio (AVPRIN).