The output variables listed below are available in
Abaqus/Explicit.
Tensors and Invariants
-
S
- Field: yes History: yes .fil: yes
All stress components.
-
MISESMAX
- Field: yes History: no .fil: no
Maximum Mises stress among all the section points. For a shell element, it represents
the maximum Mises value among all the section points in the layer, for a beam or pipe
element it is the maximum Mises stress among all the section points in the
cross-section, and for a solid element it represents the Mises stress at the
integration points.
-
Sij
- Field: no History: yes .fil: no
-component of stress (
).
-
SP
- Field: yes History: yes .fil: yes
All principal stress components.
-
SPn
- Field: no History: yes .fil: no
Minimum, intermediate, and maximum principal stress components (SP1
SP2
SP3).
-
E
- Field: yes History: yes .fil: yes
All infinitesimal strain components for geometrically linear analysis.
-
Eij
- Field: no History: yes .fil: no
-component of infinitesimal strain (
).
-
LE
- Field: yes History: yes .fil: yes
All logarithmic strain components.
-
LEij
- Field: no History: yes .fil: no
-component of logarithmic strain (
).
-
LEP
- Field: yes History: yes .fil: yes
All principal logarithmic strain components.
-
LEPn
- Field: no History: yes .fil: no
Minimum, intermediate, and maximum principal logarithmic strain components (LEP1
LEP2
LEP3).
-
THE
- Field: yes History: yes .fil: yes
All thermal strain components.
-
THEij
- Field: no History: yes .fil: no
-component of thermal strain (
).
-
THEP
- Field: yes History: yes .fil: yes
All principal thermal strains.
-
THEPn
- Field: no History: yes .fil: no
Minimum, intermediate, and maximum principal thermal strains (THEP1
THEP2
THEP3).
-
ER
- Field: yes History: yes .fil: yes
All logarithmic strain rate components.
-
ERij
- Field: no History: yes .fil: no
-component of logarithmic strain rate(
).
-
ERP
- Field: yes History: yes .fil: yes
All principal logarithmic strain rate components.
-
ERPn
- Field: no History: yes .fil: no
Minimum, intermediate, and maximum principal strain rate components (ERP1
ERP2
ERP3).
-
NE
- Field: yes History: yes .fil: yes
All nominal strain components.
-
NEij
- Field: no History: yes .fil: no
-component of nominal strain (
).
-
NEP
- Field: yes History: yes .fil: yes
All principal nominal strain components.
-
NEPn
- Field: no History: yes .fil: no
Minimum, intermediate, and maximum principal nominal strain components (NEP1
NEP2
NEP3).
-
PE
- Field: yes History: yes .fil: yes
All plastic strain components.
-
PEij
- Field: no History: yes .fil: no
-component of plastic strain (
).
-
PEP
- Field: yes History: yes .fil: no
All principal plastic strains.
-
PEPn
- Field: no History: yes .fil: no
Minimum, intermediate, and maximum principal plastic strains.
-
CE
- Field: yes History: yes .fil: no
All creep strain components.
-
CEij
- Field: no History: yes .fil: no
-component of creep strain (
).
-
ERV
- Field: yes History: yes .fil: yes
Volumetric strain rate.
-
MISES
- Field: yes History: yes .fil: yes
Mises equivalent stress, defined as
, where
is the deviatoric stress tensor, defined as
, where
is the stress and
is the equivalent pressure stress.
-
PRESS
- Field: yes History: yes .fil: yes
Equivalent pressure stress,
.
-
TRIAX
- Field: yes History: yes .fil: no
Stress triaxiality,
.
-
YIELDS
- Field: yes History: yes .fil: no
Yield stress,
, available for Mises, Tresca, Hosford, Johnson-Cook, Hill, Barlat,
and extended Drucker-Prager plasticity material models.
-
YIELDCRT
- Field: yes History: yes .fil: no
Yield criterion, available for extended Drucker-Prager plasticity material models.
-
YIELDPOT
- Field: yes History: yes .fil: no
Yield potential,
, available for Tresca, Hosford, Hill, and Barlat plasticity
material models.
-
MASSADJUST
- Field: yes History: no .fil: no
Adjusted or redistributed mass in each element that is included in the element sets
used with mass adjustment. This output is available only in the first output frame of
the first analysis step.
-
ALPHA
- Field: yes History: yes .fil: yes
All total kinematic hardening shift tensor components.
-
ALPHAij
- Field: no History: yes .fil: no
-component of the total shift tensor (
).
-
ALPHAP
- Field: yes History: yes .fil: yes
All principal values of the total shift tensor.
-
ALPHAPn
- Field: no History: yes .fil: no
Minimum, intermediate, and maximum principal values of the total shift tensor (ALPHAP1
ALPHAP2
ALPHAP3).
-
SNETk
- Field: yes History: yes .fil: no
All stress components in the
network (
). Available only for the parallel rheological framework.
-
SNETk_ij
- Field: no History: yes .fil: no
-component of stress in the
network (
and
). Available only for the parallel rheological framework.
-
PEEQ
- Field: yes History: yes .fil: yes
Equivalent plastic strain. For porous metal plasticity PEEQ is
the equivalent plastic strain in the matrix material defined as
. For cap plasticity PEEQ gives
(the cap position). For crushable foam plasticity with volumetric hardening
PEEQ gives the volumetric compacting
plastic strain defined as
. For crushable foam plasticity with isotropic hardening
PEEQ gives the equivalent plastic
strain defined as
, where
is the uniaxial compression yield stress.
-
PEEQT
- Field: yes History: yes .fil: no
Equivalent plastic strain in uniaxial tension for cast iron, Mohr-Coulomb tension
cutoff, and concrete damaged plasticity, which is defined as
.
-
PEEQR
- Field: yes History: yes .fil: no
Equivalent plastic strain rate. Available only for rate-dependent viscoplastic
models.
-
PEEQMAX
- Field: yes History: no .fil: no
Maximum equivalent plastic strain,
PEEQ, among all of the section
points. For a shell element it represents the maximum
PEEQ value among all the section
points in the layer, for a beam or a pipe element it is the maximum
PEEQ among all the section points in
the cross-section, and for a solid element it represents the
PEEQ at the integration points.
-
CEEQ
- Field: yes History: yes .fil: no
Equivalent creep strain.
-
DMICRTMAX
- Field: yes History: no .fil: no
Maximum damage initiation criteria value among all section points, all damage
initiation criteria, and all time increments up to the current time. This output variable generates three output quantities as follows: DMICRTMAXVAL outputs the maximum
damage initiation value. DMICRTPOS outputs the section point
in the layer in which the maximum damage initiation value occurred. For solid
elements, the output value is one. DMICRTTYPE outputs a value that
represents the damage initiation criteria type that reached the maximum value in the
element as follows: For elements that have failure with progressive damage:
1-DUCTCRT,
2-SHRCRT,
3-JCCRT,
4-FLDCRT,
5-MSFLDCRT,
6-FLSDCRT, and
7-MKCRT. For elements that have fiber-reinforced material damage:
11-HSNFTCRT,
12-HSNFCCRT,
13-HSNMTCRT, and
14-HSNMCCRT. For cohesive elements with traction-separation behavior:
21-MAXSCRT,
22-MAXECRT,
23-QUADSCRT, and
24-QUADECRT.
-
STATUSMP
- Field: yes History: no .fil: no
Status of each material point in the element (1.0 if the material point is active,
0.0 if it is not active).
-
LODE
- Field: yes History: yes .fil: no
Lode angle term,
, where
is the Lode angle.
-
ORITENS
- Field: yes History: no .fil: no
All orientation tensor components. Available only for elements with multiscale
material or linear orthotropic elastic material with fiber dispersion and only if the
orientation tensor is specified with a distribution (Distribution Definition).
Only written to the output database (.odb) file for the original
field output frame at zero time.
Geometric Quantities
- COORD
- Field: yes History: yes .fil: no
Coordinates of the integration point. These are the current coordinates if the large-displacement
formulation is being used.
- IVOL
- Field: yes History: yes .fil: no
Integration point volume. (Available only for continuum elements.)
- LOCALDIRn
- Field: automatic History: no .fil: no
Direction cosines of the local material directions for an anisotropic
hyperelastic material model, or yarn direction cosines for a fabric material
model. This variable is output automatically if any other element field output
is requested for anisotropic hyperelastic or fabric material (see
Output
and
Output).
Additional Element Stresses
- TSHR
- Field: yes History: yes .fil: yes
All transverse shear stress components for three-dimensional conventional
shell elements.
- TSHR13
- Field: no History: yes .fil: no
-component
of transverse shear stress.
- TSHR23
- Field: no History: yes .fil: no
-component
of transverse shear stress.
Energy Densities
- ENER
- Field: yes History: yes .fil: yes
All energy densities.
- SENER
- Field: yes History: yes .fil: no
Elastic strain energy density, per unit volume.
- PENER
- Field: yes History: yes .fil: no
Energy dissipated by rate-independent and rate-dependent plasticity, per unit volume. For
superelastic materials, this variable also includes recoverable phase-transformation
energy.
- CENER
- Field: yes History: yes .fil: no
Energy dissipated by viscoelasticity, per unit volume. (Not supported for
hyperelastic and hyperfoam material models with linear viscoelasticity.)
- VENER
- Field: yes History: yes .fil: no
Energy dissipated by viscous effects, per unit volume.
- DMENER
- Field: yes History: yes .fil: no
Energy dissipated by damage, per unit volume.
State and Field Variables
- SDV
- Field: yes History: yes .fil: yes
Solution-dependent state variables.
- SDVn
- Field: yes History: yes .fil: no
Solution-dependent state variable n.
- TEMP
- Field: yes History: yes .fil: yes
Temperature.
- DENSITY
- Field: yes History: yes .fil: no
Material density.
- FV
- Field: yes History: yes .fil: no
Field variables.
- FVn
- Field: no History: yes .fil: no
Field variable n.
Composite Failure Measures
- CFAILURE
- Field: yes History: no .fil: no
All failure measure components.
- MSTRS
- Field: no History: no .fil: no
Maximum stress theory failure measure.
- TSAIH
- Field: no History: no .fil: no
Tsai-Hill theory failure measure.
- TSAIW
- Field: no History: no .fil: no
Tsai-Wu theory failure measure.
- AZZIT
- Field: no History: no .fil: no
Azzi-Tsai-Hill theory failure measure.
- MSTRN
- Field: no History: no .fil: no
Maximum strain theory failure measure.
Additional Plasticity Quantities
- PEQC
- Field: yes History: yes .fil: yes
All equivalent plastic strains, when the model has more than one
yield/failure surface.
- PEQCn
- Field: no History: yes .fil: no
nth equivalent plastic strain
().
For cap plasticity: PEQC provides equivalent plastic strains for all three possible
yield/failure surfaces (Drucker-Prager failure surface - PEQC1, cap surface - PEQC2, and transition surface - PEQC3) and the total volumetric plastic strain (PEQC4). All identifiers also provide a yes/no flag (1/0 in the output
database), telling whether the yield surface is currently active or not
(AC YIELD: “actively yielding”).
When PEQC is requested as output to the output database, the active yield
flags for each component are named AC YIELD1,
AC YIELD2, etc.
-
RD
- Field: yes History: yes .fil: yes
Relative density (cap plasticity).
-
VVF
- Field: yes History: yes .fil: yes
Void volume fraction (cap plasticity).
Porous Metal Plasticity Quantities
-
RD
- Field: yes History: yes .fil: yes
Relative density (porous metal plasticity).
- VVF
- Field: yes History: yes .fil: yes
Void volume fraction (porous metal plasticity).
- VVFG
- Field: yes History: yes .fil: yes
Void volume fraction due to growth (porous metal plasticity).
- VVFN
- Field: yes History: yes .fil: yes
Void volume fraction due to nucleation (porous metal plasticity).
Concrete Damaged Plasticity
- DAMAGEC
- Field: yes History: yes .fil: no
Compressive damage variable, .
- DAMAGET
- Field: yes History: yes .fil: no
Tensile damage variable, .
- SDEG
- Field: yes History: yes .fil: no
Scalar stiffness degradation variable, d.
- PEEQ
- Field: yes History: yes .fil: no
Equivalent plastic strain in uniaxial compression, which is defined as
.
- PEEQR
- Field: yes History: yes .fil: no
Equivalent plastic strain rate.
Superelastic Material Quantities
- TE
- Field: yes History: yes .fil: no
Transformation strain tensor.
- TEij
- Field: no History: yes .fil: no
-component
of transformation strain ().
- TEEQ
- Field: yes History: yes .fil: no
Equivalent transformation strain.
- TEVOL
- Field: yes History: yes .fil: no
Volumetric transformation strain.
- MVF
- Field: yes History: yes .fil: no
Fraction of martensite.
- SEQUT
- Field: yes History: yes .fil: no
Equivalent uniaxial tensile stress.
- EEQUT
- Field: yes History: yes .fil: no
Equivalent uniaxial tensile total strain.
-
EE
- Field: yes History: yes .fil: no
Elastic strain tensor.
-
EEij
- Field: yes History: yes .fil: no
-component of elastic strain (
).
Cracking Model Quantities
- CKE
- Field: yes History: no .fil: yes
All cracking strain components.
- CKEij
- Field: no History: no .fil: no
-component
of cracking strain.
- CKLE
- Field: yes History: no .fil: yes
All cracking strain components in local crack axes.
- CKLEij
- Field: no History: no .fil: no
-component
of cracking strain in local crack axes.
- CKEMAG
- Field: yes History: no .fil: yes
Cracking strain magnitude, defined as .
- CKLS
- Field: yes History: no .fil: yes
All stress components in local crack axes.
- CKLSij
- Field: no History: no .fil: no
-component
of stress in local crack axes.
- CRACK
- Field: no History: no .fil: yes
Crack orientations.
- CKSTAT
- Field: yes History: no .fil: yes
Crack status of each crack. CKSTAT can have the following values for each crack: 0.0=uncracked,
1.0=closed crack, 2.0=actively cracking, 3.0=crack closing/reopening.
Failure with Progressive Damage
- DMICRT
- Field: yes History: yes .fil: no
All active components of the damage initiation criteria.
- DUCTCRT
- Field: no History: yes .fil: no
Ductile damage initiation criterion.
- JCCRT
- Field: no History: yes .fil: no
Johnson-Cook damage initiation criterion.
-
HCCRT
- Field: no History: yes .fil: no
Hosford-Coulomb damage initiation criterion.
- SHRCRT
- Field: no History: yes .fil: no
Shear damage initiation criterion.
- FLDCRT
- Field: no History: yes .fil: no
Forming limit diagram (FLD) damage
initiation criterion.
- FLSDCRT
- Field: no History: yes .fil: no
Forming limit stress diagram (FLSD) damage
initiation criterion.
- MSFLDCRT
- Field: no History: yes .fil: no
Müschenborn-Sonne forming limit stress diagram
(MSFLD) damage initiation criterion.
- MKCRT
- Field: no History: yes .fil: no
Marciniak-Kuczynski (M-K) damage initiation
criterion.
- SDEG
- Field: yes History: yes .fil: no
Overall scalar stiffness degradation.
- ERPRATIO
- Field: yes History: yes .fil: no
Ratio of principal strain rates, ,
used for the MSFLD damage initiation
criterion.
- SHRRATIO
- Field: yes History: yes .fil: no
Shear stress ratio, ,
used for the shear damage initiation criterion.
Fiber-Reinforced Materials Damage
-
DMICRT
- Field: yes History: yes .fil: no
All active components of the damage initiation criteria.
-
HSNFTCRT
- Field: no History: yes .fil: no
Hashin's fiber tensile damage initiation criterion.
-
HSNFCCRT
- Field: no History: yes .fil: no
Hashin's fiber compressive damage initiation criterion.
-
HSNMTCRT
- Field: no History: yes .fil: no
Hashin's matrix tensile damage initiation criterion.
-
HSNMCCRT
- Field: no History: yes .fil: no
Hashin's matrix compressive damage initiation criterion.
-
PLF1TCRT
- Field: no History: yes .fil: no
Fiber tensile damage initiation criterion in the local 1-direction for the ply fabric
model.
-
PLF1CCRT
- Field: no History: yes .fil: no
Fiber compressive damage initiation criterion in the local 1-direction for the ply
fabric model.
-
PLF2TCRT
- Field: no History: yes .fil: no
Fiber tensile damage initiation criterion in the local 2-direction for the ply fabric
model.
-
PLF2CCRT
- Field: no History: yes .fil: no
Fiber compressive damage initiation criterion in the local 2-direction for the ply
fabric model.
-
PLSHRCRT
- Field: no History: yes .fil: no
Matrix shear damage initiation criterion for the ply fabric model.
-
DAMAGEFT
- Field: yes History: yes .fil: no
Fiber tensile damage variable for the Hashin model.
-
DAMAGEFC
- Field: yes History: yes .fil: no
Fiber compressive damage variable for the Hashin model.
-
DAMAGEMT
- Field: yes History: yes .fil: no
Matrix tensile damage variable for the Hashin model.
-
DAMAGEMC
- Field: yes History: yes .fil: no
Matrix compressive damage variable for the Hashin model.
-
DAMAGESHR
- Field: yes History: yes .fil: no
Shear damage variable for the Hashin model and for the ply fabric model.
-
DAMAGEF1T
- Field: yes History: yes .fil: no
Fiber tensile damage variable in the local 1-direction for the ply fabric model.
-
DAMAGEF1C
- Field: yes History: yes .fil: no
Fiber compressive damage variable in the local 1-direction for the ply fabric model.
-
DAMAGEF2T
- Field: yes History: yes .fil: no
Fiber tensile damage variable in the local 2-direction for the ply fabric model.
-
DAMAGEF2C
- Field: yes History: yes .fil: no
Fiber compressive damage variable in the local 2-direction for the ply fabric
model.
Fabric Material
Output variable LOCALDIR (described above) is output automatically for fabric
materials. - SFABRIC
- Field: yes History: yes .fil: no
All fabric stress components.
- EFABRIC
- Field: yes History: yes .fil: no
All fabric strain components.
- SFABRICij
- Field: no History: yes .fil: no
-component
of fabric stress ().
- EFABRICij
- Field: no History: yes .fil: no
-component
of fabric strain ().
Equation of State
- BURNF
- Field: yes History: yes .fil: no
Burn fraction of the ignition and growth material.
- DBURNF
- Field: yes History: yes .fil: no
Reaction rate of the ignition and growth material.
- RHOE
- Field: yes History: yes .fil: no
Density of the unreacted explosive in the ignition and growth material.
- RHOP
- Field: yes History: yes .fil: no
Density of the reacted gas product in the ignition and growth material.
- PALPH
- Field: yes History: yes .fil: no
Distension, ,
of the
porous material.
- PALPHMIN
- Field: yes History: yes .fil: no
Minimum value, ,
of the distension attained during plastic compaction of the
porous material.
Rebar Quantities
- RBFOR
- Field: yes History: yes .fil: yes
Force in rebar.
- RBANG
- Field: yes History: yes .fil: yes
Angle, in degrees, between rebar and the user-specified isoparametric
direction. Available only for shell and membrane elements.
- RBROT
- Field: yes History: yes .fil: yes
Change in angle, in degrees, between rebar and the user-specified
isoparametric direction. Available only for shell and membrane elements.
Integration Point Coordinates
- COORD
- Field: yes History: yes .fil: no
Coordinates of element integration point.
Coupled Thermal-Stress Elements
- HFL
- Field: yes History: yes .fil: yes
Current magnitude and components of the heat flux per unit area vector.
- HFLM
- Field: no History: yes .fil: no
Current magnitude of the heat flux per unit area vector.
- HFLn
- Field: no History: yes .fil: no
Component n of the heat flux vector
().
Cohesive Elements
- NEEQ
- Field: yes History: yes .fil: no
Equivalent nominal strain.
- NEEQR
- Field: yes History: yes .fil: no
Equivalent nominal strain rate.
- MAXSCRT
- Field: no History: yes .fil: no
Maximum nominal stress damage initiation criterion.
- MAXECRT
- Field: no History: yes .fil: no
Maximum nominal strain damage initiation criterion.
- QUADSCRT
- Field: no History: yes .fil: no
Quadratic nominal stress damage initiation criterion.
- QUADECRT
- Field: no History: yes .fil: no
Quadratic nominal strain damage initiation criterion.
- DMICRT
- Field: yes History: yes .fil: no
All active components of the damage initiation criteria.
- SDEG
- Field: yes History: yes .fil: no
Overall scalar stiffness degradation.
- STATUS
- Field: yes History: yes .fil: no
Status of the element (the status of an element is 1.0 if the element is
active, 0.0 if the element is not).
The status output is added automatically by the analysis.
- MMIXDME
- Field: yes History: yes .fil: no
Mode mix ratio during damage evolution. It has a value of
before initiation of damage.
- MMIXDMI
- Field: yes History: yes .fil: no
Mode mix ratio at damage initiation. It has a value of
before initiation of damage.
Eulerian Elements
- EVF
- Field: yes History: yes .fil: no
Eulerian volume fraction. Output includes volume fraction data for each
material defined in the Eulerian section, plus the volume fraction of void.
- DENSITYVAVG
- Field: yes History: no .fil: no
Density, computed as a volume fraction weighted average of all materials in
the element.
- MISESVAVG
- Field: yes History: no .fil: no
Mises stress, computed as a volume fraction weighted average of all
materials in the element.
- PEVAVG
- Field: yes History: no .fil: no
Plastic strain components, computed as a volume fraction weighted average of
all materials in the element.
- PEEQVAVG
- Field: yes History: no .fil: no
Equivalent plastic strain, computed as a volume fraction weighted average of
all materials in the element.
- PRESSVAVG
- Field: yes History: no .fil: no
Equivalent pressure stress, computed as a volume fraction weighted average
of all materials in the element.
- SVAVG
- Field: yes History: no .fil: no
Stress components, computed as a volume fraction weighted average of all
materials in the element.
- TEMPMAVG
- Field: yes History: no .fil: no
Temperature, computed as a mass fraction weighted average of all materials
in the element.
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