LINK180


3D Spar (or Truss)

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

LINK180 Element Description

LINK180 is a 3D spar useful in a variety of engineering applications. The element can be used to model trusses, sagging cables, links, springs, and so on. The element is a uniaxial tension-compression element with three degrees of freedom at each node: translations in the nodal x, y, and z directions. Tension-only (cable) and compression-only (gap) options are supported. As in a pin-jointed structure, no bending of the element is considered. Plasticity, creep, rotation, large deflection, and large strain capabilities are included.

By default, LINK180 includes stress-stiffness terms in any analysis that includes large-deflection effects. Elasticity, isotropic hardening plasticity, kinematic hardening plasticity, Hill anisotropic plasticity, Chaboche nonlinear hardening plasticity, and creep are supported. To simulate the tension-/compression-only options, a nonlinear iterative solution approach is necessary. Added mass, hydrodynamic added mass and loading, and buoyant loading are available.

See LINK180 for more information about this element.

Figure 180.1: LINK180 Geometry

LINK180 Geometry

LINK180 Input Data

The geometry, node locations, and the coordinate system for this element are shown in Figure 180.1: LINK180 Geometry. The element is defined by two nodes, the cross-sectional area (A) input via the SECTYPE and SECDATA commands, added mass per unit length (ADDMAS) input via the SECCONTROL command, and the material properties.

The element x axis is oriented along the length of the element from node I toward node J. If ocean loading is present, the global origin is normally at the mean sea level, with the global Z axis pointing away from the center of the earth; however, the vertical location can be adjusted via Zmsl (Val6) on the OCDATA command (following the OCTYPE,BASIC command).

Element loads are described in Element Loading. Temperatures can be input as element body loads at the nodes. The node I temperature T(I) defaults to TUNIF. The node J temperature T(J) defaults to T(I).

By default, the element allows the cross-sectional area to change as a function of axial elongation; therefore, the volume of the element is preserved even after deformation. The default behavior is suitable for elastoplastic applications. (You can also maintain a constant or rigid cross-section via KEYOPT(2) = 1.)

LINK180 offers compression-and-tension, tension-only, and compression-only options (SECCONTROL).

Damping

The damping portion of the element contributes only damping coefficients to the structural damping matrix. The damping force is given by:

where is the damping coefficient given by , where is the velocity calculated in the previous substep.

The second damping coefficient is available to produce a nonlinear damping effect characteristic of some fluid environments. The damping coefficient units are Force * Time / Length.

Input damping coefficients via SECCONTROL,,,CV1,CV2.

Ocean Loading

For ocean loading, hydrodynamic added mass and loading, and buoyant loading, are available via the OCDATA and OCTABLE commands.

When ocean loading is applied, the loading is nonlinear (that is, based on the square of the relative velocity between the structure and the water). Accordingly, the full Newton-Raphson option (NROPT,FULL) may be necessary to achieve optimal results. (Full Newton-Raphson is applied automatically in an analysis involving large-deflection effects (NLGEOM,ON).)

Initial State

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

LINK180 Input Summary

For a general description of element input, see Element Input.

Nodes

I, J

Degrees of Freedom

UX, UY, UZ

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

Surface Loads

None

Body Loads
Temperatures -- 

T(I), T(J)

Special Features
KEYOPT(2)

Cross-section scaling (applies only when large-deflection effects (NLGEOM,ON) are specified):

0 -- 

Enforce incompressibility; cross section is scaled as a function of axial stretch (default).

1 -- 

Section is assumed to be rigid.

KEYOPT(12)

Hydrodynamic output (not available in harmonic analyses that include ocean wave effects (HROCEAN)):

0 -- 

None (default)

1 -- 

Additional hydrodynamic printout

LINK180 Output Data

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

Several items are illustrated in Figure 180.2: LINK180 Stress Output. A general description of solution output is given in Solution Output. Element results can be viewed in POST1 via PRESOL,ELEM.

Figure 180.2: LINK180 Stress Output

LINK180 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 180.1: LINK180 Element Output Definitions

Name Definition O R
ELElement numberYY
NODESNodes - I, JYY
MATMaterial numberYY
SECIDSection numberY-
XC, YC, ZCCenter locationY 1
TEMPTemperatures T(I), T(J)YY
AREACross-sectional areaYY
FORCEMember force in the element coordinate systemYY
SxxAxial stressYY
EPELxxAxial elastic strainYY
EPTOxxTotal strainYY
EPEQPlastic equivalent strain 2 2
Cur.Yld.FlagCurrent yield flag 2 2
PlwkPlastic strain energy density 2 2
PressureHydrostatic pressure 2 2
CreqCreep equivalent strain 2 2
Crwk_CreepCreep strain energy density 2 2
EPPLxxAxial plastic strain 2 2
EPCRxxAxial creep strain 2 2
EPTHxxAxial thermal strain 3 3
NL:SEPLPlastic yield stress-4
NL:SRATPlastic yielding (1 = actively yielding, 0 = not yeilding)-4
NL:HPRESHydrostatic pressure-4
NL:EPEQAccumulated equivalent plastic strain-4
NL:CREQAccumulated equivalent creep strain-4
NL:PLWKPlastic work/volume-4
EXT PRESSExternal pressure at integration point 5 5
EFFECTIVE TENSEffective tension on link 5 5
The following values apply to ocean loading only: [5]
GLOBAL COORDElement centroid location 6 Y
VR, VZRadial and vertical fluid particle velocities (VR is always > 0) 6 Y
AR, AZRadial and vertical fluid particle accelerations 6 Y
PHDYNDynamic fluid pressure head 6 Y
ETAWave amplitude over integration point 6 Y
TFLUIDFluid temperature (printed if VISC is nonzero) 6 Y
VISCViscosity (output if VISC is nonzero) 6 Y
REN, RETNormal and tangential Reynolds numbers (if VISC is nonzero) 6 Y
CTInput tangential drag coefficients evaluated at Reynolds numbers 6 Y
CDY, CDZInput normal drag coefficients evaluated at Reynolds numbers 6 Y
CMY, CMZInput inertia coefficients evaluated at Reynolds numbers 6 Y
URT, URNTangential (parallel to element axis) and normal relative velocities 6 Y
ABURNVector sum of normal (URN) velocities 6 Y
ANAccelerations normal to element 6 Y
FX, FY, FZHydrodynamic tangential and normal forces in element coordinates 6 Y
ARGUEffective position of wave (radians) 6 Y

  1. Available only at the centroid as a *GET item.

  2. Available only if the element has an appropriate nonlinear material.

  3. Available only if the element temperatures differ from the reference temperature.

  4. Available if the element has a nonlinear material.

  5. Values are given as the average of the hydrodynamic integration points, which are distributed along the wetted portion of the element.

  6. See KEYOPT(12) description.

The element printout also includes 'INT, SEC PTS' (which are always '1, Y Z' where Y and Z both have values of 0.0). These values are printed to maintain formatting consistency with the output printouts of the BEAM188, BEAM189, PIPE288, and PIPE289 elements.

Table 180.2: LINK180 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 reference for more information. The following notation is used in Table 180.2: LINK180 Item and Sequence Numbers:

Name

output quantity as defined in Table 180.1: LINK180 Element Output Definitions

Item

predetermined Item label for ETABLE and

ESOL

E

sequence number for single-valued or constant element data

I,J

sequence number for data at nodes I and J

Table 180.2: LINK180 Item and Sequence Numbers

Output Quantity Name ETABLE and ESOL Command Input
Item E I J
SxxLS-12
EPELxxLEPEL-12
EPTOxxLEPTO [1]-12
EPTHxxLEPTH-12
EPPLxxLEPPL-12
EPCRxxLEPCR-12
NL:SEPLNLIN1--
NL:SRATNLIN2--
NL:HPRESNLIN3--
NL:EPEQNLIN4--
NL:CREQNLIN5--
NL:PLWKNLIN6--
FORCESMISC1--
EXT PRESS [2]SMISC3--
EFFECTIVE TENS [2]SMISC4 --
TEMPLBFE-12
AREANMISC29--
The following output quantities are valid for ocean loading only and are averaged values for the element: [3]
GLOBAL COORDNMISC1, 2, 3-- --
VR, VZNMISC4, 5-- --
AR, AZNMISC6, 7 [4]-- --
PHDYNNMISC8 [4]-- --
ETANMISC9 [4]-- --
TFLUIDNMISC10-- --
VISCNMISC11-- --
REN, RETNMISC12, 13 [5]-- --
CTNMISC14-- --
CDY, CDZ NMISC15, 16-- --
CMY, CMZNMISC17, 18 [4]-- --
URT, URNNMISC19, 20, 21-- --
ABURNNMISC22 [4]-- --
ANNMISC23, 24 [4]-- --
FX, FY, FZNMISC25, 26, 27-- --
ARGUNMISC28 [4]-- --

  1. This item is not available via the ESOL command.

  2. External pressure (EXT PRESS) and effective tension (EFFECTIVE TENS) occur at mid-length.

  3. Values are given as the average of the hydrodynamic integration points, which are distributed along the wetted portion of the element.

  4. See KEYOPT(12) description.

  5. These quantities are output only if a Reynold's number dependency is used.

LINK180 Assumptions and Restrictions

  • The spar element assumes a straight bar, axially loaded at its ends, and of uniform properties from end to end.

  • The length of the spar must be greater than zero, so nodes I and J must not be coincident.

  • The cross-sectional area must be greater than zero.

  • The temperature is assumed to vary linearly along the length of the spar.

  • The displacement shape function implies a uniform stress in the spar.

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

  • To simulate the tension-/compression-only options, a nonlinear iterative solution approach is necessary.

  • When the link works as a rigid constraint, for example in the case of a free swinging pendulum, the rigid cross section option is recommended (KEYOPT(2) = 1).

  • When the element is used in an ocean environment:

LINK180 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 Pro  —  

  • Birth and death is not available.

  • Initial state is not available.

  • Ocean loading is not available.