Multipoint
Constraint Element: Point-in-plane Joint
The MPC184 point-in-plane joint element is a two-node element that has two relative displacement degrees of freedom. The relative rotational degrees of freedom are not considered and cannot be controlled.
Set KEYOPT(1) = 9 to define a two-node point-in-plane joint element.
Figure 184poin.1: MPC184 Point-in-plane Joint Geometry shows the geometry and node locations for this element. Two nodes (I and J) define the element.
A local Cartesian coordinate system must be specified at the first node, I, of the element. The second node, J, is constrained such that it remains on a plane defined by the local and axes. The normal distance from this plane containing node J to node I is held fixed. The local coordinate system specified at node I evolves with the rotations at node I. Use the SECJOINT command to specify the identifiers of the local coordinate systems.
The constraints imposed on a point-in-plane joint element are easily described by referring to Figure 184poin.1: MPC184 Point-in-plane Joint Geometry. At any given instant of time, the constraint imposed is as follows:
Where, xI and xJ are the positional vectors of nodes I and J in the current configuration, and XI and XJ are the position vectors of nodes I and J in the reference configuration. eI are in the current configuration, while EI are specified in the initial configuration.
The changes in the relative position of the nodes I and J are given by:
The constitutive calculations use the following definition of the joint displacement:
where:
= reference length specified on the SECDATA command |
= reference length specified on the SECDATA command |
If the reference lengths are not specified, the initial offsets are used.
Other input data that are common to all joint elements (material behavior, stops and limits, locks, etc.) are described in "Joint Input Data" in the MPC184 element description.
This input summary applies to the point-in-plane joint element option of MPC184: KEYOPT(1) = 9.
I, J
Note: For a grounded joint element, specify either node I or node J in the element definition and leave the other node (the grounded node) blank.
UX, UY, UZ, ROTX, ROTY, ROTZ
None
Use the JOIN label on the TB command to define stiffness and damping behavior. (See MPC184 Joint in the Material Reference for detailed information on defining joint materials.)
None
T(I), T(J)
None
Large deflection |
Linear perturbation |
Element behavior:
Point-in-plane joint element
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 184poin.1: MPC184 Point-in-plane Joint Element Output Definitions and Table 184poin.2: MPC184 Point-in-plane Joint Element - NMISC Output.
These tables use the following notation:
A colon (:) in the Name column indicates 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 number refers to a table footnote that describes when the item is conditionally available, and a - indicates that the item is not available.
Table 184poin.1: MPC184 Point-in-plane Joint Element Output Definitions
Name | Definition | O | R |
---|---|---|---|
EL | Element Number | - | Y |
NODES | Element node numbers (I, J) | - | Y |
FX | Constraint Force in X direction | - | Y |
CSTOP2 | Constraint force if stop is specified on DOF 2 | - | Y |
CSTOP3 | Constraint force if stop is specified on DOF 3 | - | Y |
CLOCK2 | Constraint force if lock is specified on DOF 2 | - | Y |
CLOCK3 | Constraint force if lock is specified on DOF 3 | - | Y |
CSST2 | Constraint stop status on DOF 2[1] | - | Y |
CLST2 | Constraint lock status on DOF 2[2] | - | Y |
CSST3 | Constraint stop status on DOF 3[1] | - | Y |
CLST3 | Constraint lock status on DOF 3[2] | - | Y |
JRP2 | Joint relative position of DOF2 | - | Y |
JRP3 | Joint relative position of DOF3 | - | Y |
JCD2 | Joint constitutive displacement on DOF2 | - | Y |
JCD3 | Joint constitutive displacement on DOF3 | - | Y |
JEF2 | Joint elastic force in direction -2 | - | Y |
JEF3 | Joint elastic force in direction -3 | - | Y |
JDF2 | Joint damping force in direction -2 | - | Y |
JDF3 | Joint damping force in direction -3 | - | Y |
JRU2 | Joint relative displacement in direction -2 | - | Y |
JRU3 | Joint relative displacement in direction -3 | - | Y |
JRV2 | Joint relative velocity in direction -2 | - | Y |
JRV3 | Joint relative velocity in direction -3 | - | Y |
JRA2 | Joint relative acceleration in direction -2 | - | Y |
JRA3 | Joint relative acceleration in direction -3 | - | Y |
JTEMP | Average temperature in the element[3] | - | Y |
0 = stop not active, or deactivated |
1 = stopped at minimum value |
2 = stopped at maximum value |
0 = lock not active |
1 = locked at minimum value |
2 = locked at maximum value |
Average temperature in the element when temperatures are applied on the nodes of the element using the BF command, or when temperature are applied on the element using the BFE command.
The following table shows additional non-summable miscellaneous (NMISC) output available for the point-in-plane joint element.
Note: This output is intended for use in the ANSYS Workbench program to track the evolution of local coordinate systems specified at the nodes of joint elements.
Table 184poin.2: MPC184 Point-in-plane Joint Element - NMISC Output
Name | Definition | O | R |
---|---|---|---|
E1X-I, E1Y-I, E1Z-I | X, Y, Z components of the evolved e1 axis at node I | - | Y |
E2X-I, E2Y-I, E2Z-I | X, Y, Z components of the evolved e2 axis at node I | - | Y |
E3X-I, E3Y-I, E3Z-I | X, Y, Z components of the evolved e3 axis at node I | - | Y |
E1X-J, E1Y-J, E1Z-J | X, Y, Z components of the evolved e1 axis at node J | - | Y |
E2X-J, E2Y-J, E2Z-J | X, Y, Z components of the evolved e2 axis at node J | - | Y |
E3X-J, E3Y-J, E3Z-J | X, Y, Z components of the evolved e3 axis at node J | - | Y |
JFX, JFY, JFZ | Constraint forces expressed in the evolved coordinate system specified at node I | - | Y |
JMX, JMY, JMZ | Constraint moments expressed in the evolved coordinate system specified at node I | - | Y |
Table 184poin.3: MPC184 Point-in-plane Joint Item and Sequence Numbers - SMISC Items and Table 184poin.4: MPC184 Point-in-plane Joint Item and Sequence Numbers - NMISC Items list output available via the ETABLE command using the Sequence Number method. See The General Postprocessor (POST1) in the Basic Analysis Guide and The Item and Sequence Number Table for further information. The table uses the following notation:
output quantity as defined in the Element Output Definitions table.
predetermined Item label for ETABLE command
sequence number for single-valued or constant element data
Table 184poin.3: MPC184 Point-in-plane Joint Item and Sequence Numbers - SMISC Items
Output Quantity Name | ETABLE and ESOL Command Input | |
---|---|---|
Item | E | |
FX | SMISC | 1 |
CSTOP2 | SMISC | 8 |
CSTOP3 | SMISC | 9 |
CLOCK2 | SMISC | 14 |
CLOCK3 | SMISC | 15 |
CSST2 | SMISC | 20 |
CLST2 | SMISC | 26 |
CSST3 | SMISC | 21 |
CLST3 | SMISC | 27 |
JRP2 | SMISC | 32 |
JRP3 | SMISC | 33 |
JCD2 | SMISC | 38 |
JCD3 | SMISC | 39 |
JEF2 | SMISC | 44 |
JEF3 | SMISC | 45 |
JDF2 | SMISC | 50 |
JDF3 | SMISC | 51 |
JRU2 | SMISC | 62 |
JRU3 | SMISC | 63 |
JRV2 | SMISC | 68 |
JRV3 | SMISC | 69 |
JRA2 | SMISC | 74 |
JRA3 | SMISC | 75 |
JTEMP | SMISC | 79 |
Table 184poin.4: MPC184 Point-in-plane Joint Item and Sequence Numbers - NMISC Items
Output Quantity Name | ETABLE and ESOL Command Input | |
---|---|---|
Item | E | |
E1X-I | NMISC | 1 |
E1Y-I | NMISC | 2 |
E1Z-I | NMISC | 3 |
E2X-I | NMISC | 4 |
E2Y-I | NMISC | 5 |
E2Z-I | NMISC | 6 |
E3X-I | NMISC | 7 |
E3Y-I | NMISC | 8 |
E3Z-I | NMISC | 9 |
E1X-J | NMISC | 10 |
E1Y-J | NMISC | 11 |
E1Z-J | NMISC | 12 |
E2X-J | NMISC | 13 |
E2Y-J | NMISC | 14 |
E2Z-J | NMISC | 15 |
E3X-J | NMISC | 16 |
E3Y-J | NMISC | 17 |
E3Z-J | NMISC | 18 |
JFX | NMISC | 19 |
JFY | NMISC | 20 |
JFZ | NMISC | 21 |
JMX | NMISC | 22 |
JMY | NMISC | 23 |
JMZ | NMISC | 24 |
Boundary conditions cannot be applied on the nodes forming the point-in-plane joint.
Rotational degrees of freedom are activated at the nodes forming the element. When these elements are used in conjunction with solid elements, the rotational degrees of freedom must be suitably constrained. Since boundary conditions cannot be applied to the nodes of the point-in-plane joint, a beam or shell element with very weak stiffness may be used with the underlying solid elements at the nodes forming the joint element to avoid any rigid body modes.
If both stops and locks are specified, then lock specification takes precedence. That is, if the degree of freedom is locked at a given value, then it will remain locked for the rest of the analysis.
In a nonlinear analysis, the components of relative motion are accumulated over all the substeps. It is essential that the substep size be restricted such that these rotations in a given substep are less than π for the values to be accumulated correctly.
The element currently does not support birth or death options.
The equation solver (EQSLV) must be the sparse solver or the PCG solver. The command PCGOPT,,,,,,,ON is also required in order to use the PCG solver.
The element coordinate system (/PSYMB,ESYS) is not relevant.