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Using joints: Material attributes

Using Joints: Mesh  |  Geometric attributes  |  Material attributes  |  Spring stiffnesses  |  Supports  |  Loadcase properties

The joint material attribute used in your model controls how the joint will behave when subjected to loading or displacements etc. There is a comprehensive selection of joint material available (listed below), appropriate for a wide range of common uses:

Linear Joint Models

  • Spring stiffness only corresponding to each local freedom. These local directions are defined for each joint element in the Element Reference Manual. 
  • General Properties advanced specification of joint properties of spring stiffness, mass, coefficient of linear expansion and damping factor. 

Nonlinear Joint Models

  • Elasto-Plastic (Tension and compression equal) with isotropic hardening and equal tension and compression yield conditions. 
  • Elasto-Plastic (Tension and compression unequal) with isotropic hardening and unequal tension and compression yield conditions. 
  • Smooth Contact with an initial gap. 
  • Frictional Contact with an initial gap. Friction contact joints can be specified to permit lift-off in a user-defined direction. 
  • Trilinear Earth Pressure creates a piecewise linear joint material whose properties vary with depth, such as those used to represent a layer or stratum in a soil-structure interaction or geotechnical analysis. 
  • Piecewise Linear, Elastic allows a single force/displacement (moment/rotation) curve to be defined for each freedom by defining a number of line (curve) segments. 
  • Piecewise Linear, Elastic (Axial Force Dependent) Allows any number of force/displacement (moment/rotation) curves representing the behaviour under different axial forces. 
  • Piecewise Linear, Hysteretic A range of inelastic hysteretic joint models for basic and complex hysteresis. 
  • Non-interacting Pushover Hinge material models the development of pushover hinges in members where failure is dominated by a single action; for example bracing members subject to axial forces, beam members in the floor of a building subject to seismic loading or shear in columns in which axial force can be ignored. 
  • Interacting Pushover Hinge (PMM) material models the development of pushover hinges considering the interaction of axial force and biaxial bending. 
  • Nonlinear user-defined A user-defined joint model. This allows user-supplied joint property subroutines to be used from within LUSAS. This facility provides controlled access to the pre- and post-solution constitutive processing and nonlinear state variable output via these user-supplied subroutines. 

Seismic Isolator Joint Models

  • Viscous dampers - Kelvin and Four Parameter Solid modules available. 
  • Lead Rubber Bearings with plastic yield and biaxial hysteric behaviour.
  • Friction Pendulum System with pressure and velocity dependent friction coefficient and biaxial hysteretic behaviour. 

Full information on all available joint materials is given in the help menu:

Help > Help Topics > Contents > Theory Manual Volume 1 > Chapter 4 Constitutive models > 4.12 Joint Models 

The orientation of your joint mesh elements, usually controlled using local coordinate attributes, is crucial.

 

Example Use: Lift Off or Tension-Only Joint Materials

Whilst lift-off/contact supports can be easily modelled in either a linear or nonlinear analysis, simply by choosing the "Lift-off" option for a particular freedom in a defined support attribute, and whilst for modelling tension-only cables there is a tension-only bar material for the purpose, there are cases where simple lift-off/contact between mesh is required or more control over the behaviour is desired/required and therefore a joint mesh may defined and used instead.  

There are generally three alternative material attributes applicable: "elasto-plastic", "frictional contact" or "smooth contact" for modelling contact and lift-off behaviour. The latter is recommended for simple contact problems where friction is not modelled because the input is straightforward and because it strains elastically and therefore allows the joint to go in and out of contact through different analysis stages recoverably, without accumulating and retaining any plastic strains.

Attributes > Material > Joint... > pick "Smooth contact"

For simple contact the "lift-off force" should be zero.  The "mass" would also be zero because in this case the joint represents merely the contact interface between other features. Where features are drawn and meshed to be initially in contact, the "Initial gap" would also be entered as zero.  With the other two input rows, the user then has control over the stiffness to be applied when there is contact (zero or negative force in the joint) and when there is lift-off (positive force in the joint) for each freedom.  Often, contact will be required in one direction only and so for the other freedoms the value entered for contact and lift-off stiffnesses will be equal - usually either both low/zero (free lift-off and sliding contact) or both high (fully guided contact and lift-off).  Note however, that if ill-conditioning warnings occur or convergence probelms are experienced, high extremes of stiffness used should be mitigated.

Similarly, the "Smooth contact" joint can be used to model the opposite behaviour, tension-only, whereby a high "lift-off stiffness" is entered for positive force in the joint (tension) and a low/zero stiffness is entered for the "Contact spring stiffness" for negative force in the joint (compression).

The stiffness values entered and the number of freedoms requiring input for this material will depend on the joint element type chosen and the features that the joint mesh and the associated material will be assigned to.  The different cases are descirbed for the more commonly used element types and example structural arrangments illustrated below. 

Between point features and at the ends of lines

The number of "Freedoms" specified in the material should match the DOF in joint mesh attribute selected.  

  • For a 2D beam model, JPH3, Freedom=3 should be used: the DOF are, in order, local x, y, THz.  
  • For a 3D thick beam model, JSH4, Freedom=6 should be used: the DOF are, in order, local x, y, z, THx, THy, THz.

A stiffness value for the DOF in compression (input row 1 "contact") and tension (input row 4, "lift-off stiffness") is required.  

Note that joints between points can often be required at the ends of lines, for example in a beam meshed model (see the images to the right).  In such cases, a joint can be quickly and easily added to the end of a beam meshed line, by choosing to include a joint via the "End Conditions" settings in a Line Mesh attributed.  The joint material in this case would be defined as if it is to be used for a joint between points, but assigned to a selected line, choosing the option to "Assign to line end(s)" when prompted.

Between line features

The number of "Freedoms" specified in the material should match the DOF in joint mesh attribute selected.  

  • For a 2D beam model, JPH3, Freedom=3 should be used: the DOF are, in order, local x, y, THz.  
  • For a 2D grillage/plate model, JF3, Freedom=3 should be used: the DOF are, in order, local z, THx, THy.  
  • For a 3D thick beam/thick shell model, For JSH4, Freedom=6 should be used: the DOF are, in order, local x, y, z, THx, THy, THz.
  • For a 3D thick beam/thick shell model, For JNT4, Freedom=3 can also be appropriate : the DOF are, in order, local x, y, z.  
  • For a 3D solid model, JNT4, Freedom=3 should be used: the DOF are, in order, local x, y, z.

A stiffness value per unit length for the DOF in compression (input row 1 "contact") and tension (input row 4, "lift-off stiffness") is required. 

 

Between surface feature faces

The number of "Freedoms" specified in the material should match the DOF in joint mesh attribute selected.  

  • For a 3D thick shell model, JSH4, Freedom=6 should be used: the DOF are, in order, local x, y, z, THx, THy, THz.
  • For a 3D solid model, JNT4, Freedom=3 should be used: the DOF are, in order, local x, y, z.  

A stiffness value per unit area for the 3 DOF in compression (input row 1 "contact") and tension (input row 4, "lift-off stiffness") is required. 


How do I choose suitable stiffnesses for joint materials?

How do I model lift off supports? (main page)

How do I model tension only members? (main page)

How do I model a hinged connection between shell meshed surfaces? (main page)

 


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