REINF264


3D Discrete Reinforcing

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

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

 

Figure 264.1: REINF264 Coordinate System

REINF264 Coordinate System

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,VALUE1,VALUE2,VALUE3 ! Apply real part to element 2
BFE,2,FORC,4,VALUE1,VALUE2,VALUE3 ! Apply imaginary part to element 2

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,VALUE1,VALUE2 ! Member 1 of element 2
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,VALUE2 ! Member 4 of element 2
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:

A summary of the element input follows.

REINF264 Input Summary

Nodes

Structural

Same as those of the base element, as shown:

Base ElementREINF264 Nodes
3D 8-Node Solid or Solid ShellI,J,K,L,M,N,O,P
3D 20-Node SolidI,J,K,L,M,N,O,P,Q,R,S,T,U,V,W,X,Y,Z,A,B
3D 4-Node Tetrahedral SolidI,J,K,L
3D 10-Node Tetrahedral SolidI,J,K,L,M,N,O,P,Q,R
3D 4-Node ShellI,J,K,L
3D 8-Node ShellI,J,K,L,M,N,O,P
3D 2-Node BeamI,J,K (K is an optional orientation node)
3D 3-Node BeamI,J,K,L (L is an optional orientation node)
3D 2-Node SparI,J

Thermal

Base ElementREINF264 Nodes
3D 8-Node Thermal Solid SOLID278 (KEYOPT(3) = 0)I,J,K,L,M,N,O,P
3D 20-Node Thermal Solid SOLID279 (KEYOPT(3) = 0)I,J,K,L,M,N,O,P,Q,R,S,T,U,V,W,X,Y,Z,A,B
3D 10-Node Tetrahedral Thermal Solid SOLID291I, J, K, L, M, N, O, P, Q, R
Degrees of Freedom

Structural

Same as those of the base element, as shown:

Base ElementREINF264 DOFs
3D 8-Node Solid or Solid ShellUX, UY, UZ
3D 20-Node SolidUX, UY, UZ
3D 14-Node Tetrahedral SolidUX, UY, UZ
3D 10-Node Tetrahedral SolidUX, UY, UZ
3D 4-Node ShellUX, UY, UZ, ROTX, ROTY, ROTZ
3D 8-Node ShellUX, UY, UZ, ROTX, ROTY, ROTZ
3D 2-Node BeamUX, UY, UZ, ROTX, ROTY, ROTZ
3D 3-Node BeamUX, UY, UZ, ROTX, ROTY, ROTZ
3D 2-Node SparUX, UY, UZ

Thermal

Base ElementREINF264 Nodes
3D 8-Node Thermal Solid SOLID278 (KEYOPT(3) = 0)TEMP
3D 20-Node Thermal Solid SOLID279 (KEYOPT(3) = 0)TEMP
3D 10-Node Tetrahedral Thermal Solid SOLID291TEMP
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 –

Standard method – Specified via BFE
Mesh-independent method – Specified BFE or BF on MESH200 elements
Special Features
KEYOPTS

None

REINF264 Structural or Thermal Output Data

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

The axial stress component is illustrated in Figure 264.2: REINF264 Structural or Thermal Output.

Figure 264.2: REINF264 Structural or Thermal Output

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 (Main Menu> Preprocessor> Sections> Reinforcing> Display Options).

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

NameDefinitionOR
ELElement number and name-Y
NODESNodes (as shown in "REINF264 Input Summary")-Y
MATMaterial number-Y
AREAAveraged cross-section area of reinforcing fibers-Y
VOLU:Volume-Y
XC, YC, ZCCenter 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:xAxial stresses (uniaxial stiffness only)2Y
S:x, xy, xzElastic stresses (uniaxial, bending, and torsional stiffness)2Y
EPEL:xAxial elastic strains (uniaxial stiffness only)2Y
EPEL:x, xy, xzElastic strains (uniaxial, bending, and torsional stiffness)2Y
EPTH:xAxial thermal strains2Y
EPPL:xAxial plastic strains21
EPCR:xAxial creep strains21
EPTO:xTotal axial mechanical strains (EPEL + EPPL + EPCR)Y-
NL:EPEQAccumulated equivalent plastic strain-1
NL:CREQAccumulated equivalent creep strain-1
NL:SRATPlastic yielding (1 = actively yielding, 0 = not yielding)-1
NL:PLWKPlastic work/volume-1
N11Averaged axial force-Y
LOCI:X, Y, ZIntegration point locations-4

Table 264.3: REINF264 Element Output Definitions – Thermal Analysis

NameDefinitionOR
ELElement number and name2Y
NODESNodes (as shown in "REINF264 Input Summary")2Y
MATMaterial number2Y
AREAAveraged cross-section area of reinforcing fibers-Y
VOLU:Volume2Y
XC, YC, ZCCenter location-3
BFE TEMP

T1, T2 for reinforcing members [5]

-Y
TG:xTemperature gradient along the fiber for all reinforcing members [5]2Y
TF:xHeat flux along the fiber for all reinforcing members [5]2Y
LOCI:X, Y, ZIntegration point locations-4

  1. Nonlinear solution output if the element has a nonlinear material.

  2. 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.

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

  4. Available only if OUTRES,LOCI is used.

  5. A member is an individual reinforcing.

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

Table 264.4: REINF264 Item and Sequence Numbers

Output Quantity NameETABLE and ESOL Command Input
ItemE
N11SMISC(i - 1) * 4 + 1
AREASMISC(i - 1) * 4 + 2
HEATSMISC(i - 1) * 4 + 3
VOLUMESMISC(i - 1) * 4 + 4

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).

REINF264 Product Restrictions

There are no product-specific restrictions for this element.