PCNTX11
Bulk Data Entry Defines properties TYPE11 of a CONTACT interface for geometric nonlinear analysis.
Format
(1) | (2) | (3) | (4) | (5) | (6) | (7) | (8) | (9) | (10) |
---|---|---|---|---|---|---|---|---|---|
PCNTX11 | PID | ISTF | IGAP | IDEL | |||||
STMIN | STMAX | MESHSIZE | DTMIN | ||||||
STFAC | FRIC | GAP | TSTART | TEND | STF1 | ||||
IBC | INACTI | VISS | VISF | BMULT |
Example
(1) | (2) | (3) | (4) | (5) | (6) | (7) | (8) | (9) | (10) |
---|---|---|---|---|---|---|---|---|---|
PCONT | 34 | ||||||||
PCNTX11 | 34 |
Definitions
Field | Contents | SI Unit Example |
---|---|---|
PID | Property identification
number of the associated PCONT. No default (Integer > 0) |
|
ISTF | Stiffness definition flag.
5
Default as defined by CONTPRM (Integer = 0, ..., 5) |
|
IGAP | Gap definition flag.
Default as defined by CONTPRM (Character = CONST, VAR, or VAR3) |
|
IDEL | Flag for node and segment deletion.
Default as defined by CONTPRM (Integer) |
|
STMIN | Minimum stiffness (Only
with ISTF > 1). Default as defined by CONTPRM (Real ≥ 0) |
|
STMAX | Maximum stiffness (Only
with ISTF > 1). Default as defined by CONTPRM (Real ≥ 0) |
|
MESHSIZE | Percentage of mesh size
(Used only when IGAP = VAR3). Default = 0.4 (Real, 0.0 < MESHSIZE ≤ 1.0) |
|
DTMIN | Limiting nodal time step.
8 No default (Real ≥ 0) |
|
STFAC | Interface stiffness scale
factor (Only with ISTF ≠ 1). Default as defined by CONTPRM (Real ≥ 0) |
|
FRIC | Coulomb
friction. Default as defined by CONTPRM (Real ≥ 0) |
|
GAP | Gap for impact activation.
6
Default as defined by CONTPRM (Real ≥ 0) |
|
TSTART | Start time. Default = 0.0 (Real ≥ 0) |
|
TEND | Time for temporary
deactivation. Default = 1030 (Real ≥ 0) |
|
STIF1 | Interface stiffness (Only
with ISTF = 1). Default = 0.0 (Real ≥ 0) |
|
IBC | Flag for deactivation of
boundary conditions at impact applied to the slave grid
set. Default as defined by CONTPRM (Character = X, Y, Z, XY, XZ, YZ, or XYZ) |
|
INACTI | Handling of initial
penetrations flag. 7
Invalid entries are ignored. Default as defined by CONTPRM (Integer) |
|
VISS | Critical damping
coefficient on interface stiffness. Default as defined by CONTPRM (Real ≥ 0) |
|
VISF | Critical damping
coefficient on interface friction. Default as defined by CONTPRM (Real ≥ 0) |
|
BMULT | Sorting factor. Can be
used to speed up the sorting algorithm and is
machine-dependent. Default as defined by CONTPRM (Real ≥ 0) |
Comments
- The property identification number must be that of an existing PCONT Bulk Data Entry. Only one PCNTX11 property extension can be associated with a particular PCONT.
- PCNTX11 is only applied in geometric nonlinear analysis subcases which are defined by ANALYSIS = EXPDYN. It is ignored for all other subcases.
- If FRIC is not explicitly defined on the PCONTX/PCNTX# entries, the MU1 value on the CONTACT or PCONT entry is used for FRIC in the /INTER entries for Geometric Nonlinear Analysis. Otherwise, FRIC on PCONTX/PCNTX# overwrites the MU1 value on CONTACT/PCONT.
- PCNTX11 defines the
properties of contact interface type CONTX11, it describes the edge to edge or line to line interface. This interface
simulates impact between lines, a line can be a beam or truss element or a shell
edge or spring elements. The interface properties are:
- impacts occur between a master and a slave line
- a slave line can impact on one or more master lines
- a line can belong to the master and the slave side. This allows self impact.
- this interface can be used in addition to the interface TYPE7 PCNTX7 to solve the edge to edge limitation of interface TYPE7
- If ISTF ≠ 1, the interface stiffness K is computed from the master
segment stiffness Km and/or the slave segment stiffness Ks.
The master stiffness is computed from Km = STFAC * B * S * S/V for solids, Km = 0.5 * STFAC * E * t for shells.
The slave stiffness is an equivalent nodal stiffness computed as Ks = STFAC * B * V-3 for solids, Ks = 0.5 * STFAC * E * t for shells.
In these equations, B is the Bulk Modulus, S is the segment area, and V is the volume of a solid. There is no limitation to the value of stiffness factor (but a value larger than 1.0 can reduce the initial time step).
The interface stiffness is K = max (STMIN, min (STMAX, K1)) with:- ISTF = 0, K1 = Km
- ISTF = 2, K1 = 0.5 * (Km + Ks)
- ISTF = 3, K1 = max (Km, Ks)
- ISTF = 4, K1 = min (Km, Ks)
- ISTF = 5, K1 = Km * Ks / (Km + Ks)
- If IGAP = VAR, the variable gap is computed as: gm + gswith:
- gm - master element gap with
gm = t/2, t: thickness of the master element for shell elements.
gm = L/10, L - length of the smallest side of a solid element.
gm = 1/2√ for truss and beam elements, with S being the cross section of the element.
gm = 0 for spring elements.
- gs - slave element gap is computed as the same way.
If the slave node is connected to multiple shells and/or beams or trusses, the largest computed slave gap is used.
The variable gap is always at least equal to GAP.
- gm - master element gap with
- INACTI =
3, is only recommended for small initial penetrations and
should be used with caution because:
- the coordinate change is irreversible
- it may create other initial penetrations, if several surface layers are defined in the interfaces
- it may create initial energy, if the node belongs to a spring element
INACTI = 5 is recommended for airbag simulation deployment.
INACTI = 6 is recommended instead of INACTI = 5, in order to avoid high frequency effects into the interfaces. - Slave segment is deactivated from the contact when the segment kinematic time step calculated for this contact becomes smaller than DTMIN.