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PCNTX5

PCNTX5

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PCNTX5

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Bulk Data Entry

PCNTX5 – Extended CONTACT Property type 5 for Geometric Nonlinear Analysis

Description

Defines properties type 5 of a CONTACT interface for geometric nonlinear analysis.

Format

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PCNTX5

PID

 

 

 

 

IBAG

IDEL

 

 

 

STFAC

FRIC

GAP

TSTART

TEND

 

 

 

 

 

IBC

 

IRM

INACTI

 

 

 

 

 

 

IFRIC

IFILT

FFAC

 

 

 

 

 

 

 

FRICDAT

C1

C2

C3

C4

C5

C6

 

 

hmtoggle_plus1Example

(1)

(2)

(3)

(4)

(5)

(6)

(7)

(8)

(9)

(10)

PCONT

34

 

 

 

 

 

 

 

 

PCNTX5

34

 

 

 

 

 

 

 

 

Field

Contents

PID

Property identification number of the associated PCONT.

No default (Integer > 0)

IBAG

Airbag vent holes closure flag in case of contact.

Default = 0 (Integer)

0 - No closure

1 - Closure

IDEL

Flag for node and segment deletion.

Default as defined by CONTPRM (Integer = 0, 1, or 2)

0 - No deletion.

1 - When all the elements (shells and solids) associated to one segment are deleted, the segment is removed from the master side of the interface. Additionally, non-connected nodes are removed from the slave side of the interface. Has a CPU cost higher than IDEL = 2.

2 - When a shell or a solid element is deleted, the corresponding segment is removed from the master side of the interface. Additionally, non-connected nodes are removed from the slave side of the interface.

STFAC

Interface stiffness scale factor.

Default = 0.2 (Real > 0)

FRIC

Coulomb friction.

Default as defined by CONTPRM (Real > 0)

GAP

Gap for impact activation (See comment 4).

Default as defined by CONTPRM (Real > 0)

TSTART

Start time

Default = 0.0 (Real > 0)

TEND

Time for temporary deactivation.

Default = 1030 (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, XYZ)

IRM

Renumbering flag for segments of the master surface (Integer = 0, 1, or 2).

0 - If segment is connected to a solid element its normal is reversed if entering the solid element (the segment is renumbered).

1 - Normal is always reversed (segment 1234 is read 2143).

2 - Normal is never reversed (segment connected to a solid element are not renumbered).

INACTI

Handling of initial penetrations flag (See comment 5).

Default as defined by CONTPRM (Integer = 0, 3, or 4)

0 - No action.
3 - Change slave node coordinates to avoid small initial penetrations.
4 - Change master node coordinates to avoid small initial penetrations.
Invalid entries are ignored.

IFRIC

Friction formulation flag (See comment 6).

Default as defined by CONTPRM (Character = COUL, GEN, DARM, or REN)

COUL - Static Coulomb friction law.
GEN - Generalized viscous friction law.
DARM - Darmstad friction law.
REN - Renard friction law.

IFILT

Friction filtering flag (See comment 7).

Default as defined by CONTPRM (Character = NO, SIMP, PER, or CUTF)

NO - No filter is used.
SIMP - Simple numerical filter.
PER - Standard -3dB filter with filtering period.
CUTF - Standard -3dB filter with cutting frequency.

FFAC

Friction filtering factor.

Default as defined by CONTPRM (Real = 0.0 < FFAC < 1.0)

FRICDAT

Indicates that additional information for IFRIC will follow. Only available when IFRIC = GEN, DARM or REN.

C1, C2, C3, C4, C5, C6

Coefficients to define variable friction coefficient in IFRIC = GEN, DARM, or REN.

Default as defined by CONTPRM (Real > 0)

Comments

1.The property identification number must be that of an existing PCONT bulk data entry. Only one PCNTX5 property extension can be associated with a particular PCONT.
2.PCNTX5 is only applied in geometric nonlinear analysis subcases which are defined by ANALYSIS = NLGEOM or IMPDYN. It is ignored for all other subcases.
3.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.
4.In implicit analysis, different contact formulations are used for contact where slave and master set do not overlap and where they overlap (self-contact).

In the case of self-contact, the gap cannot be zero and a constant gap is used. For small initial gaps, the convergence will be more stable and faster, if GAP is larger than the initial gap.

In implicit analysis, sometimes a stiffness with scaling factor reduction (for example, STFAC = 0.01) or reduction in impacted thickness (if rigid one) might reduce unbalanced forces and improve convergence, particularly in shell structures under bending where the effective stiffness is much lower than membrane stiffness; but it should be noted that too low of a value could also lead to divergence.

5.INACTI = 3 or 4 are 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
6.IFRIC defines the friction model.

IFRIC = COUL – Coulomb friction with FT < FRIC * FN.

For IFRIC > 0 the friction coefficient is set by a function (µ = µ (p, V)), where p is the pressure of the normal force on the master segment and V is the tangential velocity of the slave node.

The following formulations are available:

IFRIC = 1 - Generalized viscous friction law

µ = FRIC + C1 * p + C2 * V + C3 * p * v + C4 * p2 + C5 * v2

IFRIC = 2 - Darmstad law

µ = C1 *  e(C2V)  *  p2 + C3 *  e(C4V) *  p + C5 *  e(C6V)

IFRIC = 3 - Renard law

renard1

0 < V < C5

renard2

C5 < V < C6

renard3

C6 < V

where:

renard4

The first critical velocity Vcr1 must not be 0 (C5 ≠ 0). It also must be lower than the second critical velocity Vcr2 (C5 < C6).
The static friction coefficient C1 and the dynamic friction coefficient C2, must be lower than the maximum friction C3 (C1 < C3 and C2 < C3).
The minimum friction coefficient C4, must be lower than the static friction coefficient C1 and the dynamic friction coefficient C2 (C4 < C1 and C4 < C2).
7.IFILT defines the method for computing the friction filtering coefficient. If IFILT NO, the tangential friction forces are smoothed using a filter:

FT = α * F'T + (1 - α) * F'T-1

where,

FT is the tangential force

F'T is the tangential force at time t

F'T-1 is the tangential force at time t-1

α is the filtering coefficient

IFILT = SIMP – α = FFAC

IFILT = PER – α = 2pidt/FFAC, where dt/T = FFAC, T is the filtering period

IFILT = CUTF – α = 2pi * FFAC * dt, where FFAC is the cutting frequency

8.This card is represented as an extension to a PCONT property in HyperMesh.

See Also:

Bulk Data Section

Guidelines for Bulk Data Entries

Bulk Data Entries by Function

The Input File