ZeroLengthImpact3D

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This command constructs a node-to-node zero-length contact element in 3D space to simulate the impact/pounding and friction phenomena.

element zeroLengthImpact3D $tag $slaveNode $masterNode $direction $initGap $frictionRatio $Kt $Kn $Kn2 $Delta_y $cohesion

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$tag	Unique element object tag
$slaveNode	Slave node tag
$masterNode	Master node tag
$direction	1 if out-normal vector of master plane points to +X direction 2 if out-normal vector of master plane points to +Y direction 3 if out-normal vector of master plane points to +Z direction
$initGap	Initial gap between master plane and slave plane
$frictionRatio	Friction ratio
$Kt	Penalty in two tangential directions (parallel to master and slave planes)
$Kn	Penalty in normal direction (normal to master and slave planes)
$Kn2	Penalty in normal direction after yielding based on Hertz impact model
$Delta_y	Yield deformation based on Hertz impact model
$cohesion	Cohesion, if no cohesion, it is zero

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NOTES:

1. This element has been developed on top of the “zeroLengthContact3D”. All the notes available in “zeroLengthContact3D” wiki page would apply to this element as well. It includes the definition of master and slave nodes, the number of degrees of freedom in the domain, etc.
2. It adds the capabilities of “ImpactMaterial” to “zeroLengthContact3D” .
3. For simulating a surface-to-surface contact, the element can be defined for connecting the nodes on slave surface to the nodes on master surface.
4. The element was found to be fast-converging and eliminating the need for extra elements and nodes in the modeling process.

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EXAMPLE: The following zip file contains an example script and the corresponding input cyclic displacement: File:ExampleScript1.zip

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REFERENCES: zeroLengthContact3D , ImpactMaterial

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Code Developed by: Dr. A.E. Zaghi, M. Cashany @ University of Connecticut (UConn)

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APPLICATION:

1. This element has been employed to simulate the bridge hinges including superstructure-abutment interaction at University of Connecticut (UConn) and University of Nevada, Reno (UNR).
2. It has been implemented in non-structural systems like suspended ceilings, simulating the impact/pounding and friction phenomena.