Accessing Material Point Data
You are provided with access to the values of the material point quantities through the utility
routine GETVRM described in Obtaining Material Point Information in an Abaqus/Standard Analysis. In a nonlinear analysis values returned will correspond to
the current solution iteration, representing a converged solution only at the final
iteration for each increment. In the static perturbation procedure, only those quantities
for which perturbation values are computed can be accessed. The values of the material point
data are recovered in the arrays ARRAY,
JARRAY, and FLGRAY for
floating point, integer, and character data, respectively. Floating point data are recovered
as double-precision data.
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.
Any number of user-defined output variables can be used.
Output Precision
The data are provided in double precision for output to the data (.dat) and
results (.fil) files and are written to the output database
(.odb) file in single precision. Because the user provides UVARM output variables in double
precision, numeric overflow errors related to output to the output database file might
occur in cases where the output results exceed the capacity for single-precision
representation even when no overflow errors occur in UVARM.
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
Variables 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.
- JMATYP
Variable that must be passed into the GETVRM utility routine to access an output variable.
- MATLAYO
Variable that must be passed into the GETVRM utility routine to access an output variable.
- LACCFLA
Variable that must be passed into the GETVRM
utility routine to access an output variable.
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
About metal plasticity models
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
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