25.2.43 UVARM
User subroutine to generate element output.

Product: ABAQUS/Standard  

References

Overview

User subroutine UVARM:

  • will be called at all material calculation points of elements for which the material definition includes the specification of user-defined output variables;

  • allows you to define output quantities that are functions of any of the available integration point quantities listed in the Output Variable Identifiers table (ABAQUS/Standard output variable identifiers, Section 4.2.1);

  • allows you to define the material directions as output variables;

  • can be used for gasket elements;

  • can call utility routine GETVRM to access material point data; and

  • cannot be used with linear perturbation procedures.

Accessing material point data

You are provided with access to the values of the material point quantities at the end of the increment through the utility routine GETVRM described in Obtaining material point information, Section 26.2.5. The values of the material point data are recovered in the arrays ARRAY, JARRAY, and FLGRAY for floating point, integer, and character data, respectively.

Using user-defined output variables

The output identifier for the user-defined output quantities is UVARM. Individual components are accessed with UVARMn, where , NUVARM. You must specify the number of user-defined output variables, NUVARM, for a given material to allocate space at each material calculation point for each variable. The user-defined output variables are available for both printed and results file output and are written to the output database and restart files for contouring, printing, and X–Y plotting in ABAQUS/CAE. Any number of user-defined output variables can be used.

Input File Usage:           
*USER OUTPUT VARIABLES
NUVARM

User subroutine interface

      SUBROUTINE UVARM(UVAR,DIRECT,T,TIME,DTIME,CMNAME,ORNAME,
     1 NUVARM,NOEL,NPT,LAYER,KSPT,KSTEP,KINC,NDI,NSHR,COORD,
     2 JMAC,JMATYP,MATLAYO,LACCFLA)
      INCLUDE 'ABA_PARAM.INC'
C
      CHARACTER*80 CMNAME,ORNAME
      CHARACTER*3 FLGRAY(15)
      DIMENSION UVAR(NUVARM),DIRECT(3,3),T(3,3),TIME(2)
      DIMENSION ARRAY(15),JARRAY(15),JMAC(*),JMATYP(*),COORD(*)

C     The dimensions of the variables FLGRAY, ARRAY and JARRAY
C     must be set equal to or greater than 15.

      user coding to define UVAR

      RETURN
      END

Variable to be defined

UVAR(NUVARM)

An array containing the user-defined output variables. These are passed in as the values at the beginning of the increment and must be returned as the values at the end of the increment.

Variables passed in for information

DIRECT(3,3)

An array containing the direction cosines of the material directions in terms of the global basis directions. DIRECT(1,1), DIRECT(2,1), DIRECT(3,1) give the (1, 2, 3) components of the first material direction; DIRECT(1,2), DIRECT(2,2), DIRECT(3,2) give the second material direction, etc. For shell and membrane elements the first two directions are in the plane of the element and the third direction is the normal. This information is not available for beam and truss elements.

T(3,3)

An array containing the direction cosines of the material orientation components relative to the element basis directions. This is the orientation that defines the material directions (DIRECT) in terms of the element basis directions. For continuum elements T and DIRECT are identical. For shell and membrane elements T(1,1) , T(1,2) , T(2,1) , T(2,2) , T(3,3) , and all other components are zero, where is the counterclockwise rotation around the normal vector that defines the orientation. If no orientation is used, T is an identity matrix. Orientation is not available for beam and truss elements.

TIME(1)

Value of step time at the end of the current increment.

TIME(2)

Value of total time at the end of the current increment.

DTIME

Time increment.

CMNAME

User-specified material name, left justified.

ORNAME

User-specified local orientation name, left justified.

NUVARM

User-specified number of user-defined output variables.

NOEL

Element number.

NPT

Integration point number.

LAYER

Layer number (for composite shells and layered solids).

KSPT

Section point number within the current layer.

KSTEP

Step number.

KINC

Increment number.

NDI

Number of direct stress components at this point.

NSHR

Number of shear stress components at this point.

COORD

Coordinates at this material point.

JMAC

Variable that must be passed into the GETVRM utility routine to access an output variable using the utility routine.

JMATYP

Variable that must be passed into the GETVRM utility routine to access an output variable using the utility routine.

MATLAYO

Variable that must be passed into the GETVRM utility routine to access an output variable using the utility routine.

LACCFLA

Variable that must be passed into the GETVRM utility routine to access an output variable using the utility routine.

Example: Calculation of stress relative to shift tensor

Below is an example of user subroutine UVARM. The subroutine calculates the position of the current state of stress relative to the center of the yield surface for the kinematic hardening plasticity model by subtracting the kinematic shift tensor, , from the stress tensor, . See Metal plasticity models, Section 4.3.1 of the ABAQUS Theory Manual, for additional details.

      SUBROUTINE UVARM(UVAR,DIRECT,T,TIME,DTIME,CMNAME,ORNAME,
     1 NUVARM,NOEL,NPT,LAYER,KSPT,KSTEP,KINC,NDI,NSHR,COORD,
     2 JMAC,JMATYP,MATLAYO,LACCFLA) 
C
      INCLUDE 'ABA_PARAM.INC'
C
      CHARACTER*80 CMNAME,ORNAME
      CHARACTER*3 FLGRAY(15)
      DIMENSION UVAR(NUVARM),DIRECT(3,3),T(3,3),TIME(2)
      DIMENSION ARRAY(15),JARRAY(15),JMAC(*),JMATYP(*),COORD(*)
C
C Error counter:
      JERROR = 0
C Stress tensor:
      CALL GETVRM('S',ARRAY,JARRAY,FLGRAY,JRCD,JMAC,JMATYP,
     1 MATLAYO,LACCFLA)
      JERROR = JERROR + JRCD
      UVAR(1) = ARRAY(1)
      UVAR(2) = ARRAY(2)
      UVAR(3) = ARRAY(3)
      UVAR(4) = ARRAY(4)
      UVAR(5) = ARRAY(5)
      UVAR(6) = ARRAY(6)
C Kinematic shift tensor:
      CALL GETVRM('ALPHA',ARRAY,JARRAY,FLGRAY,JRCD,JMAC,JMATYP,
     1 MATLAYO,LACCFLA)
      JERROR = JERROR + JRCD
C Calculate the position relative to the center of the
C yield surface:
      UVAR(1) = UVAR(1) - ARRAY(1)
      UVAR(2) = UVAR(2) - ARRAY(2)
      UVAR(3) = UVAR(3) - ARRAY(3)
      UVAR(4) = UVAR(4) - ARRAY(4)
      UVAR(5) = UVAR(5) - ARRAY(5)
      UVAR(6) = UVAR(6) - ARRAY(6)
C If error, write comment to .DAT file:
      IF(JERROR.NE.0)THEN
        WRITE(6,*) 'REQUEST ERROR IN UVARM FOR ELEMENT NUMBER ',
     1      NOEL,'INTEGRATION POINT NUMBER ',NPT
      ENDIF
      RETURN
      END

Additional example