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Item Comp Description
Valid Item Labels for Degree of Freedom Results
U X, Y, Z X, Y, or Z structural displacement.
ROT X, Y, Z X, Y, or Z structural rotation.
TEMP[1] Temperature.
PRES Pressure.
VOLT Electric potential.
MAG Magnetic scalar potential.
V X, Y, Z X, Y, or Z fluid velocity.
A X, Y, Z X, Y, or Z magnetic vector potential.
CURR Current.
EMF Electromotive force drop.
ENKE Turbulent kinetic energy.
ENDS Turbulent energy dissipation.
SP0n Mass fraction of species n, where n = 1 to 6. If a species is given a user-defined name [MSSPEC], use that name instead of SP0n.
Valid Item Labels for FLOTRAN Nodal Results
TTOT Total temperature.
HFLU Heat flux.
HFLM Heat transfer (film) coefficient.
COND Fluid laminar conductivity.
PCOE Pressure coefficient.
PTOT Total (stagnation) pressure.
MACH Mach number.
STRM Stream function. (2-D applications only.)
DENS Fluid density.
VISC Fluid laminar viscosity.
EVIS Fluid effective viscosity.
ECON Fluid effective conductivity.
YPLU Y+, a turbulent law of the wall parameter.
TAUW Shear stress at the wall.
LMDn Laminar mass diffusion coefficient for species n, where n = 1 to 6.
EMDn Effective mass diffusion coefficient for species n, where n = 1 to 6.
Valid Item and Component Labels for Element Results
S X, Y, Z, XY, YZ, XZ Component stress.
" 1, 2, 3 Principal stress.
" INT Stress intensity.
" EQV Equivalent stress.
EPEL X, Y, Z, XY, YZ, XZ Component elastic strain.
" 1, 2, 3 Principal elastic strain.
" INT Elastic strain intensity.
" EQV Elastic equivalent strain.
EPTH X, Y, Z, XY, YZ, XZ Component thermal strain.
" 1, 2, 3 Principal thermal strain.
" INT Thermal strain intensity.
" EQV Thermal equivalent strain.
EPPL X, Y, Z, XY, YZ, XZ Component plastic strain.
" 1, 2, 3 Principal plastic strain.
" INT Plastic strain intensity.
" EQV Plastic equivalent strain.
EPCR X, Y, Z, XY, YZ, XZ Component creep strain.
" 1, 2, 3 Principal creep strain.
" INT Creep strain intensity.
" EQV Creep equivalent strain.
EPSW Swelling strain.
EPTO X, Y, Z, XY, YZ, XZ Component total mechanical strain (excluding thermal) (EPEL + EPPL + EPCR).
" 1, 2, 3 Principal total mechanical strain.
" INT Total mechanical strain intensity.
" EQV Total equivalent mechanical strain.
EPTT X, Y, Z, XY, YZ, XZ Component total strain including thermal (EPEL + EPTH + EPPL + EPCR).
" 1, 2, 3 Principal total strain.
" INT Total strain intensity.
" EQV Total equivalent strain.
NL SEPL Equivalent stress (from stress-strain curve).
" SRAT Stress state ratio.
" HPRES Hydrostatic pressure.
" EPEQ Accumulated equivalent plastic strain.
" PSV Plastic state variable. VISCO106, VISCO107, and VISCO108 only.
" PLWK Plastic work/volume. VISCO106, VISCO107, and VISCO108 only.
SEND ELASTIC Elastic strain energy density.
" PLASTIC Plastic strain energy density.
" CREEP Creep strain energy density.
TG X, Y, Z, SUM Component thermal gradient or vector sum.
TF X, Y, Z, SUM Component thermal flux or vector sum.
PG X, Y, Z, SUM Component pressure gradient or vector sum.
EF X, Y, Z, SUM Component electric field or vector sum.
D X, Y, Z, SUM Component electric flux density or vector sum.
H X, Y, Z, SUM Component magnetic field intensity or vector sum.
B X, Y, Z, SUM Component magnetic flux density or vector sum.
FMAG X, Y, Z, SUM Component magnetic forces or vector sum.
SERR Structural error energy.
SDSG Absolute value of maximum variation of any nodal stress component.
TERR Thermal error energy.
TDSG Absolute value of the maximum variation of any nodal thermal gradient component.
F X, Y, Z Component structural force. Sum of element nodal values.
M X, Y, Z Component structural moment. Sum of element nodal values.
HEAT Heat flow. Sum of element nodal values.
FLOW Fluid flow. Sum of element nodal values.
AMPS Current flow. Sum of element nodal values.
FLUX Magnetic flux. Sum of element nodal values.
VF X, Y, Z Component fluid force.
CSG X, Y, Z Component magnetic current segment.
SENE "Stiffness" energy or thermal heat dissipation (applies to all elements where meaningful). Same as TENE.
AENE Artificial energy of the element. This includes the sum of hourglass control energy and energy generated by in-plane drilling stiffness from shell elements (applies to all elements where meaningful). The energy is used for comparisons to SENE energy to predict the solution error due to artificial stiffness. See the ANSYS, Inc. Theory Reference.
TENE Thermal heat dissipation or "stiffness" energy (applies to all elements where meaningful). Same as SENE.
KENE Kinetic energy (applies to all elements where meaningful).
JHEAT Element Joule heat generation (coupled-field calculation).
JS X, Y, Z, SUM Source current density (coupled-field calculation) and vector sum in the global Cartesian coordinate system. Valid only for current conduction and low-frequency electromagnetic analyses.
JT X, Y, Z, SUM Total current density and vector sum in the global Cartesian coordinate system. Valid only for low- frequency electromagnetic analyses.
JC X, Y, Z, SUM Conducting current density and vector sum in the global Cartesian coordinate system. Valid only for high-frequency electromagnetic analyses.
MRE Magnetics Reynolds number
VOLU Element volume. Based on unit thickness for 2-D plane elements (unless the thickness option is used) and on the full 360 degrees for 2-D axisymmetric elements.
CENT X, Y, Z Undeformed X, Y, or Z location (based on shape function) of the element centroid in the active coordinate system.
BFE TEMP Body temperatures (calculated from applied temperatures) as used in solution (area and volume elements only).
SMISC snum Element summable miscellaneous data value at sequence number snum (shown in the Output Data section of each applicable element description in the ANSYS Elements Reference).
NMISC snum Element non-summable miscellaneous data value at sequence number snum (shown in the Output Data section of each applicable element description found in the ANSYS Elements Reference).
SURF snum Element surface data value at sequence number snum (shown in Surface Solution of the ANSYS Elements Reference).
CONT[2] STAT Contact status. 3-closed and sticking, 2-closed and sliding, 1-open but near contact, 0-open and not near contact.
" PENE Contact penetration (zero or positive).
" PRES Contact pressure.
" SFRIC Contact friction stress.
" STOT Contact total stress (pressure plus friction).
" SLIDE Contact sliding distance.
" GAP Contact gap distance (0 or negative).
" FLUX Total heat flux at contact surface.
“ CNOS Total number of contact status changes during substep.
TOPO Densities used for topological optimization. This applies to the following types of elements: PLANE2, PLANE82, SOLID92, SHELL93, SOLID95.
For SHELL131 and SHELL132 elements with KEYOPT(3) = 0 or 1, use labels TBOT, TE2, TE3, . . ., TTOP instead of TEMP.
For the CONT items for elements CONTA171 through CONTA175, the reported data is averaged across the element.