ansys.data1

Triangular mesh processing tool, currently very few people use this software, but it allows us to gr

ST42.5 ansALPY
ST42.6 ansALPZ
ST42.7 ansNUXY
ST42.8 ansNUYZ
ST42.9 ansNUXZ
ST42.10 ansGXY
ST42.11 ansDENS
ST42.12 ansCH
ST42.13 thk1
ST42a $$(Element Coordinate System)
  [KOP10] Element coordinate system is parallel to
   the global coordinate system
  [KOP11] Element coordinate system is based on th
  e element I-J side
ST42b $$(Modified Displacement Shapes)
  [KOP20] Include modified extra displacement sha
  pes
  [KOP21] Suppress extra displacement shapes
ST42c $$(Stress/Strain)
  [KOP30] Plane Stress
  [KOP31] Axisymmetric
  [KOP32] Plane Strain (Z Strain=0.0)
  [KOP33] Plane Stress with thickness input
ST42d $$(Element Printout I)
  [KOP50] Basic element prinout
  [KOP51] Repeat lines 2 and 3 of solution for all
   integration points
  [KOP52] Nodal stress printout
ST42e $$(Element Printout II)
  [KOP60] Basic element printout
  [KOP61] Surface printout for face 1 also
  [KOP62] Surface printout for both faces 1 and 3
   also
  [KOP63] Nonlinear printout at each integration p
  oint also.
  [KOP64] Surface printout for faces with nonzero
   pressure
ST43a $$(Element in-plane behaviour)
  [KOP30] (Default) In-plane modified extra displa
  cement shapes included in the element formulatio
  n
  [KOP31] No extra displacement shapes included
  [KOP32] Allman in-plane rotational stiffness inc
  luded.  Real constants ZSTIF1 and ZSTIF2 are use
  d with this option to prevent zero-enegery nodes
ST43b $$(User Subroutine for Element Coordinate Sy
  stem)
  [KOP40] (Default) No user subroutine to define t
  he element coordinate system
  [KOP41] Element X-axis is located by user subrou
  tine USERAN (see appendix U of ANSYS User's Man)
ST43c $$(Element Solution Listing Options)
  [KOP50] Basic element solution listing
  [KOP51] Basic solution + integration point solut
  ion at TOP, MID, and BOT surfaces (adds 135 more
   lines per element)
ST43d $$(More Element Solution Listing Options)
  [KOP60] (Default) Basic element solution listing
  [KOP61] Basic solution + nonlinear solution at e
  ach integration (adds 36 more lines per element)
ST43e $$(Interpretation of EP in the output)
  [KOP80] (Default) EP represents the elastric str
  ain
  [KOP81] EP represents the total strains, EP+EPPL
  +EPCR (sum of elastic, plastic, and creep strain
  s)
ST44 %(Material Options - Specify up to 5 constant
  s C0 C1 C2 C3 C4 (in order) to determine a tempe
  rature - dependent material property :   C0 + C1
  *T + C2*T**2 + C3*T**3 + C4*T**4.)
  [EX] Elastic Young's Modulus (x-direction)
  [NUXY] Poisson's Ratio (nuxy)
  [DENS] Density
  [ALPX] Coefficient of Thermal Expansion (x-direc
  tion)
ST44.1 ansEX
ST44.2 ansNUXY
ST44.3 ansDENS
ST44.4 ansALPX
ST44a $$(Type of Mass Matrix)
  [KOP20] (Default) Consistent mass matrix
  [KOP21] Reduced mass matrix
ST44b $$(To Release Rotational Stiffness at node I
  )
  [KOP30] (Default) No release of rotational stiff
  ness
  [KOP31] ROTX stiffness released
  [KOP32] ROTY stiffness released
  [KOP33] ROTZ stiffness released
  [KOP34] ROTX and ROTY stiffness released
  [KOP35] ROTY and ROTZ stiffness released
  [KOP36] ROTX and ROTZ stiffness released
  [KOP37] ROTX, ROTY, and ROTZ stiffness released
ST44c $$(To Release Rotational Stiffness at Node J
  )
  [KOP40] (Default) No release of rotational stiff
  ness
  [KOP41] ROTX stiffness released
  [KOP42] ROTY stiffness released
  [KOP43] ROTZ stiffness released
  [KOP44] ROTX and ROTY stiffness released
  [KOP45] ROTY and ROTZ stiffness released
  [KOP46] ROTX and ROTZ stiffness released
  [KOP47] ROTX, ROTY, and ROTZ stiffness released
ST44d $$(Element Output Options)
  [KOP50] (Default) Basic element output, based on
   24 geometric properties
  [KOP52] Output includes shear, bending, and tors
  ional stresses (30 properties)
  [KOP53] Output includes shear center offset and
   elastic foundation stiffness calculations, in a
  ddition to the above (36 properties)
  [KOP54] Output includes stresses at up to four a
  dditional points on the beam section at each end
  , in addition to the above (52 properties)
ST44e $$(Listing of Member Forces and Moments)
  [KOP60] (Default) Member forces and moments not
   included in the element solution listing
  [KOP61] Member forces and moments (in the elemen
  t coordinate system) included in the element sol
  ution listing
ST45a $$(Element Shape Functions)
  [KOP10] (Default) Modified extra displacement sh
  apes included in the element formulation
  [KOP11] No extra displacement shapes included
ST45b $$(General 3D Application or Plane Stress)
  [KOP30] (Default) General 3D application
  [KOP31] Generalized plane strain option
ST45c $$(Element Coordinate System Orientation)
  [KOP40] (Default) Element coordinate system in p
  arallel to the global Cartesian coordinate syste
  m
  [KOP41] Element coordinate system is based on th
  e element I-J side, i.e. X-axis along I-J, Y-axi
  s in the I-J-K plane, Z-axis normal
ST45d $$(Element Solution Listing Options)
  [KOP50] (Default) Basic element solution listing
  [KOP51] Basic solution + solution at each integr
  ation point (adds 24 more lines/element)
  [KOP52] Basic solution + nodal stress solution (
  adds 9 more lines/element)
ST45e $$(More Element Solution Listing Options)
  [KOP60] (Default) Basic element solution listing
  [KOP61] Basic solution + surface listing for fac
  e 2 (Surface listing is valid only for linear ma
  terials)
  [KOP62] Basic solution + surface listing for fac
  es 2 and 4
  [KOP63] Basic solution + nonlinear solution at e
  ach integration point (adds up to 29 more lines
   per element)
  [KOP64] Basic solution + surface listing for fac
  es with nonzero pressure
ST46a $$(Element Shape Functions)
  [KOP10] (Default) Modified extra displacement sh
  apes included in the element formulation
  [KOP11] No extra displacement shapes included
ST46b $$(Layer or Matrix Input)
  [KOP20] (Default) Element input data is in layer
   form.  Each layer has a uniform thickness.
  [KOP25] Same as above, but a listing of the mate
  rial property matrices integrated through the th
  ickness for the first element is also produced
  [KOP21] Element input data is in layer form.  Ea
  ch layer has a non-uniform thickness (tapered)
  [KOP26] Same as above, but a listing of the mate
  rial property matrices integrated through the th
  ickness for the first element is also produced
  [KOP23] Element input is in matrix form
  [KOP28] Same as above, but a listing of the mate
  rial property matrices integrated through the th
  ickness for the first element is also produced
ST46c $$(Element Solution Listing Options)
  [KOP30] Basic Element solution listing
  [KOP31] Basic solution + integration point strai
  ns at the bottom and top surfaces of the element
   (adds 10 lines of printout/element)
  [KOP32] Basic solution + nodal forces in the ele
  ment coordinate system (adds 5 lines/element)
  [KOP34] Basic solution + integration point strai
  ns at the bottom and top surfaces of the element
    + nodal forces in the element coordinate syste
  m (adds 15 lines of printout per element)
ST46d $$(User Subroutines for Element c.s.)
  [KOP40] (Default) No user-written subroutines to
  define the element coordinate system
  [KOP44] Element X-axis located by user subroutin
  e USERAN
  [KOP45] Element X-axis located by user subroutin
  e USERAN and layer X-axes located by user subrou
  tine USANLY
ST46e $$(Use of Strain or Stress Results)
  [KOP50] Strain results will be used for calculat
  ion of the failure criteria
  [KOP51] Stress results will be used for calculat
  ion of the failure criteria
  [KOP52] Both strain and stress results will be u
  sed for calculation of the failure criteria
ST46g $$(Stress/Strain Evaluation Options)
  [KOP90] Strains and Stresses are evaluated at th
  e top and bottom of each layer
  [KOP91] Strains and Stresses are evaluated at th
  e midthickness of each layer
ST52 %(Material Options - Specify up to 5 constant
  s C0 C1 C2 C3 C4 (in order) to determine a tempe
  rature - dependent material property :   C0 + C1
  *T + C2*T**2 + C3*T**3 + C4*T**4.)
  [MU] Coefficient of Friction
ST52.1 ansMU
ST52a $$(Sticking stiffness)
  [KOP10] (Default) Geometric property KS used for
   sticking stiffness
  [KOP11] Zero sticking stiffness (resisting force
   only)
ST52b $$(Coordinate Updating for Large Deflection)
  [KOP20] (Default) Updated coordinates used for l
  ocating the element during large deflection prob
  lems
  [KOP21] Original coordinates used for locating t
  he element during large deflection problems (no
   updating)
ST52c $$(Stiffness When Gap Opens)
  [KOP30] (Default) Zero stiffness when gap opens
  [KOP31] A small stiffness (= 1.0E-6*normal stiff
  ness assigned to separated interface for stabili
  ty)
ST52d $$(Value of Gap or Interface)
  [KOP40] (Default) Gap (or interface) based on ge
  ometric property GAP
  [KOP41] Gap (or interface) based on initial node
   locations (GAP ignored)
ST52e $$(Convergence criterion)
  [KOP60] (Default) Convergence based on changing
   element status within a 0.1% tolerance on slidi
  ng force
  [KOP61] Convergence based on changing element st
  atus within a 5% tolerance on sliding force
  [KOP62] Convergence based on changing element st
  atus within a 10% tolerance on sliding force
  [KOP63] Convergence based on unchanging element
   status
ST57 %(Material Options - Specify up to 5 constant
  s C0 C1 C2 C3 C4 (in order) to determine a tempe
  rature - dependent material property :   C0 + C1
  *T + C2*T**2 + C3*T**3 + C4*T**4.)
  [KXX] Thermal Conductivity (x-direction)
  [KYY] Thermal Conductivity (y-direction)
  [DENS] Density
  [CH] Specific Heat
ST57.1 ansKXX
ST57.2 ansKYY
ST57.3 ansDENS
ST57.4 ansCH
ST57a $$(Film Coefficient Evaluation)
  [KOP20] (Default) Film coefficient evaluated at
   the average of element surface temperature (TS)
   and bulk temperature, (TS+TB)/2
  [KOP21] Film coefficient evaluated at TS
  [KOP22] Film coefficient evaluated at TB
  [KOP23] Film coefficient evaluated at |TS-TB|
ST63 %(Material Options - Specify up to 5 constant
  s C0 C1 C2 C3 C4 (in order) to determine a tempe
  rature - dependent material property :   C0 + C1
  *T + C2*T**2 + C3*T**3 + C4*T**4.)
  [EX] Elastic Young's Modulus (x-direction)
  [EY] Elastic Young's Modulus (y-direction)
  [NUXY] Poisson's Ratio (nuxy)
  [GXY] Shear modulus (x-stress, y-strain)
  [ALPX] Coefficient of Thermal Expansion (x-direc
  tion)
  [ALPY] Coefficient of Thermal Expansion (y-direc
  tion)
  [DENS] Density
ST63.1 ansEX
ST63.2 ansEY
ST63.3 ansNUXY
ST63.4 ansGXY
ST63.5 ansALPX
ST63.6 ansALPY
ST63.7 ansDENS
ST63a $$(Bending and/or membrane stiffness)
  [KOP10] (Default) Both Bending and membrane stif
  fness used
  [KOP11] Membrane stiffness only
  [KOP12] Bending stiffness only
ST63b $$(Element Shape Functions)
  [KOP30] (Default) Modified extra displacement sh
  apes included in the element formulation
  [KOP31] No extra displacement shapes included
ST63c $$(Element Solution Listing Options)
  [KOP50] (Default) Basic element soltuion listing
  [KOP52] Basic solution + nodal stress solution (
  adds 15 more lines/element)
ST63d $$(Interpretation of Pressure Loading)
  [KOP60] (Default) Reduced pressure loading, i.e.
  , pressure is converted to equivalent nodal forc
  es.
  [KOP62] Consistent pressure loading, i.e., press
  ure is converted to equivalent nodal forces and
   moments
ST63e $$(Mass Matrix Formulation)
  [KOP70] (Default) Consistent Mass Matrix
  [KOP71] Lumped Mass Matrix
S63f $$(User Subroutine for Element Coordinate Sys
  tem)
  [KOP90] (Default) No user subroutine to define t
  he element coordinate system
  [KOP94] Element X-axis is located by user subrou
  tine USERAN (see Appendix U of the ANSYS User's
   Manual)
ST64a $$(Element Shape Functions)
  [KOP10] (Default) Modified extra displacement sh
  apes are included in the element formulation
  [KOP11] No extra displacement shapes are include
  d
ST64b $$(General 3D Application or Plane Strain)
  [KOP30] (Default) General 3-D application
  [KOP31] Generalized plane strain option
ST64c $$(Inverted or uninverted material matrix)
  [KOP40] (Default) The material matrix is input
   in its INVERTED form
  [KOP41] The material matrix is input in its UNI
  NVERTED form
ST64d $$(Element Solution Listing Options)
  [KOP50] (Default) Basic element solution listing
  [KOP51] Basic solution + solution at each integr
  ation point (adds up to 24 more lines/element)
  [KOP52] Basic solution + nodal stress solution (
  adds 9 more lines/element)
ST64e $$(Element Coordinate System Orientation)
  [KOP60] (Default) Element coordinate system is p
  arallel to the global Cartesian coordinate syste
  m
  [KOP61] Element coordinate system is parallel to
   the element, i.e., X-axis parallel to edge I-J,
   Y-axis in the I-J-K plane, Z-axis normal.
  [KOP64] Element X-axis is located by user-writte
  n subroutine, USERAN; see Appendix U of the User
  's Manual
ST65 %(Material Options - Specify up to 5 constant
  s C0 C1 C2 C3 C4 (in order) to determine a tempe
  rature - dependent material property :   C0 + C1
  *T + C2*T**2 + C3*T**3 + C4*T**4.)
  [EX] Elastic Young's Modulus
  [NUXY] Poisson's Ratio (nuxy) (concrete only)
  [ALPX] Coefficient of Thermal Expansion
  [DENS] Density
ST65.1 ansEX
ST65.2 ansNUXY
ST65.3 ansALPX
ST65.4 ansDENS
ST65a $$(Element Shape Functions)
  [KOP10] (Default) Modified extra displacement sh
  apes are included in the element formulation
  [KOP11] No extra displacement shapes are include
  d
ST65b $$(General 3D Application or Plane Stress)
  [KOP30] (Default) General 3-D Application
  [KOP31] Generalized plane strain option
ST65c $$(Concrete Linear Solution Listing Options)
  [KOP50] (Default) Listing of concrete linear sol
  ution at centroid only
  [KOP51] Centroidal solution + solution at each i
  ntegration point (adds up to 24 more lines/eleme
  nt)