ansys.data1

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

  [KOP52] Centroidal solution + nodal stress solut
  ion (adds 9 more lines/element)
ST65d $$(Concrete Nonlinear Solution Listing Optio
  n)
  [KOP60] (Default) Listing of concrete nonlinear
   solution at centroid only
  [KOP63] Centroidal solution + solution at each i
  ntegration point (adds up to 29 more lines/eleme
  nt)
ST66 %(Material Options - Specify up to 5 constant
  s C0 C1 C2 C3 C4 (in order) to determine a tempe
  rature - dependent material property :   C0 + C1
  *T + C2*T**2 + C3*T**3 + C4*T**4.)
  [KXX] Thermal Conductivity
  [CH] Specific Heat
  [DENS] Density
  [MU] Coefficient of Friction
  [VISC] Viscosity
  [HF] Convection Film Coefficient
ST66.1 ansKXX
ST66.2 ansCH
ST66.3 ansDENS
ST66.4 ansMU
ST66.5 ansVISC
ST66.6 ansHF
ST66a $$(Film Coefficient Evaluation)
  [KOP20] (Default) Film coefficient evaluated at
   the average fluid temperature, (T(I)+T(J))/2
  [KOP21] Film coefficient evaluated at the avera
  ge wall temperature, (T(K)+T(L))/2
  [KOP22] Film coefficient evaluated at the avera
  ge film temperature, (T(I)+T(J)+T(K)+T(L))/4
  [KOP23] Film coefficient evaluated at the diffe
  rential temperature, |(T(I)+T(J)/2 - (T(K)+T(L)
  )/2|
ST66b $$(Specification of flow losses)
  [KOP60] (Default) Flow losses accounted for by
   specifying an additional length of the pipe (as
   geometric property LA)
  [KOP61] Flow losses accounted for by specifying
   a loss coefficient (as geometric property K)
ST69 %(Material Options - Specify up to 5 constant
  s C0 C1 C2 C3 C4 (in order) to determine a tempe
  rature - dependent material property :   C0 + C1
  *T + C2*T**2 + C3*T**3 + C4*T**4.)
  [KXX] Thermal Conductivity (x-direction)
  [KYY] Thermal Conductivity (y-direction)
  [KZZ] Thermal Conductivity (z-direction)
  [RSVX] Electrical Resistivity (x-direction)
  [RSVY] Electrical Resistivity (y-direction)
  [RSVZ] Electrical Resistivity (z-direction)
  [CH] Specific Heat
  [DENS] Density
ST69.1 ansKXX
ST69.2 ansKYY
ST69.3 ansKZZ
ST69.4 ansRSVX
ST69.5 ansRSVY
ST69.6 ansRSVZ
ST69.7 ansCH
ST69.8 ansDENS
ST69a $$(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|
ST70 %(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)
  [KZZ] Thermal Conductivity (z-direction)
  [DENS] Density
  [CH] Specific Heat
ST70.1 ansKXX
ST70.2 ansKYY
ST70.3 ansKZZ
ST70.4 ansDENS
ST70.5 ansCH
ST70a $$(Film coefficient evaluation)
  [KOP20] (Default) Film coefficient evaluated at
   the average of element surface temperature (TS)
   and bulk temperature, (TS+TB)/2
  [KOP21] Film coefficient evaluated at TS
  [KOP22] Film coefficient evaluated at TB
  [KOP23] Film coefficient evaluated at |TS-TB|
ST70b $$(Velocity Direction for Mass Transport)
  [KOP40] (Default) VX, VY and VZ are in global c
  oordinates
  [KOP42] VX, VY and VZ are in element coordinates
  . (VX parallel to I-J side of the element, VY in
   the IJK plane)
ST70c $$(Nonlinear Porous Flow Option)
  [KOP70] (Default) Standard heat transfer element
  [KOP71] Nonlinear steady-state fluid flow analog
  y
ST70c.2 ST70c2
ST70c2 %(Optional Material Options)
  [VISC] Viscosity
  [MU] Exponent on Velocity
ST70c2.1 ansVISC
ST70c2.2 ansMU
ST70d $$(Mass Transport Effects)
  [KOP80] (Default) No mass transport effects
  [KOP81] Mass transport effects included (by spec
  ifying the velocity component VX, VY and VZ as
   geometric properties)
ST80 %(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
  [ALPX] Coefficient of Thermal Expansion (x-direc
  tion)
  [DENS] Density
  [VISC] Viscosity
ST80.1 ansEX
ST80.2 ansALPX
ST80.3 ansDENS
ST80.4 ansVISC
ST80a $$(Controls Gravity Spring Locations)
  [KOP20] (Default) Gravity "springs" are assumed
   on all sides of the elements
  [KOP21] Gravity "springs" are asssumed only on e
  lement faces located on the Y=0.0 plane. (The el
  ements must not have positive Y coordinates)
ST85a $$(Listing of the Nonlinear Solution)
  [KOP40] (Default) Solution listing includes the
   nonlinear solution at the centroid
  [KOP41] Nonlinear solution at the centroid + non
  linear solution at each integration point (adds
   16 lines per element)
ST85b $$(Element Solution Listing Options)
  [KOP50] (Default) Basic element solution listing
  [KOP51] Basic solution + solution at each integr
  ation point (adds 24 lines per element)
  [KOP52] Basic solution + nodal stress solution (
  adds 9 lines per element)
ST85c $$(Coordinate system for Stress Output)
  [KOP60] (Default) Stress output is in the stress
   coordinate system
  [KOP61] Stress output is in the element coordina
  te system (automatically used if the element is
   defined by 8 unique nodes)
ST86 %(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
  [DENS] Density
ST86.1 ansEX
ST86.2 ansNUXY
ST86.3 ansDENS
ST86a $$(Strain Energy Function)
  [KOP20] (Default) Mooney-Rivlin nearly compressi
  ble material - use the ANSYNL command to define
   the constants
  [KOP21] Blatz-Ko compressible material
ST86b $$(Element Coordinate System Orientation)
  [KOP40] (Default) Element coordinate system is p
  arallel to the global Cartesian coordinate syste
  m
  [KOP41] Element coordinate system is based on th
  e undeformed element I-J side, i.e., X-axis para
  llel to I-J and Y-axis in the I-J-K plane
ST86c $$(Element Solution Listing Options)
  [KOP50] (Default) Basic element solution listing
  [KOP51] Basic solution + element strains (adds 1
   line per element)
  [KOP52] Basic solution + integration point stres
  ses (adds up to 27 lines/element)
  [KOP53] Basic solution + integration point strai
  ns (adds up to 18 lines/element)
  [KOP54] Basic solution + nodal stress solution (
  adds up to 8 lines/element)
  [KOP59] All of the above
ST86d $$(Integration of the Strain Energy Function
   - Available only for the Mooney-Rivlin material
  )
  [KOP60] (Default) Full integration of the strain
   energy function
  [KOP61] Full integration of the shear terms and
   reduced integration of the volumetric terms of
   the strain energy function
ST91a $$(Enter Number of Layers n < 16)
  [KOP3N] No choice is required for the default of
   1 layer
ST91a.1 ST91a1
ST91a1 #  n:|
ST91b $$(User Subroutine for Element Coordinate Sy
  stem)
  [KOP40] (Default) No user subroutines to define
   the element coordinate system
  [KOP44] Element X-axis is located by user subrou
  tine USERAN (see Appendix U of the ANSYS User's
   Man)
  [KOP45] Element X-axis is located by user subrou
  tine USERAN and the layer X-axis is located by u
  ser subroutine USANLY
ST91c $$(Layer Solution Listing Options)
  [KOP50] (Default) Listing of average results at
   the layer face farthest from the element center
  plane (one line per element)
  [KOP51] Listing of average results at the layer
   middle (one line per element)
  [KOP52] Listing of average results at layer top
   and bottom surfaces (2 lines per element)
  [KOP53] Listing of results at each of 4 integrat
  ion points for the top and bottom surfaces (10 l
  ines per element)
  [KOP54] Listing of results at each of 4 nodes fo
  r the top and bottom surfaces (10 lines per elem
  ent)
ST91d $$(Interlaminar Shear Stress Caculations)
  [KOP60] (Default) Interlaminar shear stresses no
  t calculated
  [KOP61] Interlaminar shear stresses calculated a
  nd included in the element solution listing
ST95d $$(Element Solution Listing Options)
  [KOP50] (Default) Basic element solution listing
  [KOP51] Basic solution + solution at each integr
  ation point (adds 24 more lines/element)
  [KOP52] Basic solution + nodal stress solution (
  adds 9 more lines/element)
ST95e $$(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
ansopt $(Choose from one of the listed analysis ty
  pes)
  [KAN] Structural
  [KAN 1] Buckling
  [KAN -1] Thermal
  [KAN] Fluid
  [KAN -1] Magnetic (3-D Static)
  [KAN] Coupled
ansopt.1 ansSTRUC
ansopt.3 ankt a-1KY3 a-1KY4 a0KY10
ansopt.4 ansFLUID
ansopt.5 ankt a-1KY3 a-1KY4 a0KY10
ansopt.6 ansCOUPL
ansSTRUC $[0] Static
  [2] Modal
  [ ] Transient
  [ ] Harmonic
ansSTRUC.1 a0KY3 a0KY6 a0KY8 a0KY9 a0KY10
ansSTRUC.2 a2KY1 a2KY2 a2KY3 a2KY7 a2KY8 a0KY10
ansSTRUC.3 ansTRANS
ansSTRUC.4 ansHARMO
ansTRANS $[5] Linear
  [4] Nonlinear
ansTRANS.1 a5KY1 a2KY8 a0KY10
ansTRANS.2 a0KY3 a4KY5 a0KY6 a0KY8 a4KY9 a0KY10
ansHARMO $[6] Reduced Harmonic Response Using Symm
  etric Matrices
  [3] Full Harmonic Response with Unsymmetric Matr
  ices
ansHARMO.1 a6KY3 a2KY8 a0KY10
ansHARMO.2 a3KY3 a0KY8 a0KY10
ansFLUID $[-1] Analysis of Heat and 1D Mass Transp
  ort Effects
  [ ] Analysis of a Non-Flowing Fluid
  [ ] Analysis of Fluid-Structure Interaction Effe
  cts (Acoustic)
ansFLUID.1 ankt a-1KY3 a-1KY4 a0KY10
ansFLUID.2 ansNONFL
ansFLUID.3 ansACOUS
ansNONFL $[0] Static Analysis
  [2] Modal Analysis
  [4] Nonlinear Transient Dynamic Analysis
  [5] Linear Transient Dynamic Analysis
ansNONFL.1 a0KY3 a0KY6 a0KY8 a0KY9 a0KY10
ansNONFL.2 a2KY1 a2KY2 a2KY3 a2KY7 a2KY8 a0KY10
ansNONFL.3 a0KY3 a4KY5 a0KY6 a0KY8 a4KY9 a0KY10
ansNONFL.4 a5KY1 a2KY8 a0KY10
ansCOUPL $[ ] 3-D Static
  [2] 3-D Modal
  [6] 3-D Harmonic
  [ ] 3-D Transient
ansCOUPL.1 ansINERT1
ansCOUPL.2 a2KY1 a2KY2 a2KY3 a2KY7 a2KY8 a0KY10
ansCOUPL.3 a6KY3 a2KY8 a0KY10
ansCOUPL.4 ansINERT4
ansINERT1 $[0] Inertial Effects are Required
  [-1] Internal Heat Generation is Required
ansINERT1.1 a0KY3 a0KY6 a0KY8 a0KY9 a0KY10
ansINERT1.2 ankt a-1KY3 a-1KY4 a0KY10
ansINERT4 $[4] Inertial Effects are Required
  [-1] Inertial Effects are Not Required
ansINERT4.1 a0KY3 a4KY5 a0KY6 a0KY8 a4KY9 a0KY10
ansINERT4.2 ankt a-1KY3 a-1KY4 a0KY10
ansACOUS $[3] Unsymmetric Harmonic Response Analy
  sis
  [4] Nonlinear Transient Dynamic Analysis
  [2] Nodal Analysis
  [0] Static Analysis
ansACOUS.1 a3KY3 a0KY8 a0KY10
ansACOUS.2 a0KY3 a4KY5 a0KY6 a0KY8 a4KY9 a0KY10
ansACOUS.3 a2KY1 a2KY2 a2KY3 a2KY7 a2KY8 a0KY10
ansACOUS.4 a0KY3 a0KY6 a0KY8 a0KY9 a0KY10
a0KY3 $$(Choose the Amount of Interpolation/Extrap
  olation to be applied to solution results for in
  put to the elements for the next solution result
  s.  Often used with next option to improve large
   deflection convergence)
  [KAY 3 0] No modification of solution (recommend
  ed)
  [KAY 3] Enter integer; e.g., 5 for 50% interpola
  tion (average of last two solutions), -5 for 50%
   extrapolation.
a0KY3.2 a0KY31
a0KY31 #  N:|
a0KY6 $$(Deflection Model)
  [KAY 6 0] Small deflection analysis
  [KAY 6 1] Large deflection analysis
a0KY8 $$(Include Stress Stiffening Effects)
  [KAY 8 0] No stress stiffening included in analy
  sis
  [KAY 8 1] Include stress stiffening in analysis
a0KY9 $$(Choose the Newton-Rhapson method)
  [KAY 9 0] Let the program choose the Newton-Rhap
  son method
  [KAY 9 1] Use full Newton-Rhapson (default if pl
  asticity or large deflections)
  [KAY 9 2] Use modified Newton_Rhapson
  [KAY 9 3] Use initial-stiffness Newton-Rhapson (
  default if only creep and/or nonlinear elements)
a0KY10 $$(Select a Virtual Equation Solver)
  [KAY 10 0] In-memory wavefront equation solution
  [KAY 10 1] Virtual wavefront equation solution
a2KY1 $$(Reduced/Full Mode Extraction)
  [KAY 1 0] Use reduced Householder or reduced sub
  space iteration
  [KAY 1 1] Use full subspace iteration
a2KY2 $$(Expand Modes of Load Steps)
  [KAY 2 0] Do not expand any modes in any load st
  ep
  [KAY 2] Expand first N modes of each load step (
  specify N)
  [KAY 2 -1] Expanded mode control is done at the
   load step level with the frequency range on the
   EXMODE command
a2KY2.2 a2KY22
a2KY22 #  Specify N:|
a2KY3 $$(Control Printout of Reduced Mode Shapes)
  [KAY 3 0] Do not print reduced mode shapes
  [KAY 3 1] Print all reduced mode shapes
  [KAY 3] Print only first N reduced mode shapes
a2KY3.3 a2KY33
a2KY33 #  Specify N:|
a2KY7 $$(Mode Extraction Technique)
  [KAY 7 0] Use reduced Householder procedure for
   mode extraction