ansys.data1

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

  [KAY 7] Use subspace iteration procedure to ext
  ract first P modes
a2KY7.2 a2KY72
a2KY72 #  Specify P:|
a2KY8 $$(Include Stress Stiffening Effects)
  [KAY 8 0] No stress stiffening included in the a
  nalysis
  [KAY 8 1] Include stress stiffening in analysis
a3KY3 $$(Express Displacement Output in Terms of R
  eal and Imaginary Components)
  [KAY 3 0] Print complex displacements as real an
  d imaginary components
  [KAY 3 1] Print complex displacements as amplitu
  des and phase angles
a4KY5 $$(Define Initial Conditions at the Start of
   the Transient)
  [KAY 5 0] Initial velocity defined by first two
   iterations and initial acceleration defined to
   be 0
  [KAY 5 2] Initial velocity and acceleration defi
  ned to be 0
a4KY9 $$(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 and large deflections)
  [KAY 9 2] Use modified Newton-Rhapson (default o
  nly if plasticity or large deflections)
  [KAY 9 3] Use initial-stiffness Newton-Rhapson (
  default if only creep and/or nonlinear elements)
a5KY1 $$(Conveniently Ignore Damping)
  [KAY 1 0] Include damping, if any, in analysis
  [KAY 1 1] Ignore damping even though defined
a6KY3 $$(Express Displacement Output in Terms of R
  eal and Imaginary components or in Polar Form)
  [KAY 3 0] Print complex displacements as real an
  d imaginary components
  [KAY 3 1] Print complex displacements as amplitu
  des and phase angles
a-1KY3 $$(Choose the Amount of Steady-State
   interppolation/extrapolation to be applied to
   solution results for input to the elements for
   the next solution results)
  [KAY 3 0] No modification of solution (recommend
  ed by ANSYS)
  [KAY 3] Enter integer value; e.g., 5 for 50% int
  erpolation (average of last two solutions), -5 f
  or 50% extrapolation.
a-1KY3.2 a-1KY31
a-1KY31 #  N:|
a-1KY4 $$(Choose the Amount of Transient Extrapola
  tion/Interpolation to be applied to solution res
  ults for input to the elements for the next solu
  tion results)
  [KAY 4 0] 100% extrapolation (recommended with n
  onlinear properties)
  [KAY 4] Enter integer value; e.g., 5 for 50% ext
  rapolation, 10 for no modification
a-1KY4.2 a-1KY42
a-1KY42 #  N:|
ankt $(Choose One Of The Heat Generation Options)
  [KTEMP 0] All Nodal Heat Generations Rates 0
  [KTEMP -1] Use Nodal Heat Generation Rates (0 fo
  r undefined rates)
ansopts %[cgloc] Origin Of The Reference Coordina
  te System
  [domega] Base Angular Acceleration
  [omega] Base Angular Velocity
  [acel] Base Acceleration
ansopts.1 524 525 526
ansopts.2 acceleration
ansopts.3 velocity
ansopts.4 acceleration
ansnon #(Used to Specify Nonlinear Material Proper
  ties)
ansnon1 $(Select the Type of Nonlinear Specificati
  ion to be Set)
  [MP] Magnetic and/or Piezoelectric Properties
  [SRC] Current Sources
  [PLA] Plasticity
  [CRP] Creep
ansnon1.1 S50 S5f
ansnon1.2 S5a
ansnon1.3 S50 PLAa
ansnon1.4 S50 Ca Ch
S50 #(Specify the material number to which this no
  nlinear table is to be attached)  material_no:|
S5a %(Current Source Data)
  [NL55] Magnetic permeability of free space
  [NL56] Number of times to repeat element sources
   for circular symmetry
  [NL57] System of Units
  [NL58] Used to converge nonlinear magnetic probl
  ems.  Represents number of modified Newton-Rhaps
  on iterations to be used starting with the first
  [NL61] Current Sources
S5a.1 S5a1
S5a.2 S5a2
S5a.3 S5a3
S5a.4 S5a4
S5a.5 S5b S5c S5d
S5a1 #  mu:|
S5a2 #   N:|
S5a3 $[MKS] MKS units [CGS] CGS units
S5a4 #   N:|
S5b #(Source identifier between 1 and 26) id:|
S5c %(SOURCE CONSTANTS)
  [NL1] Specify Source Type
  [NL2] Total Current flowing through source
  [NL3] Characteristic length (mean radius or len
  gth, depending on type of source)
  [NL4] Cross-sectional dimensions
  [NL6] Coded number of integration points
  [NL7] Global Cartesian Source Coordinate System
  [NL13] Arc Angle (required only for arc source)
S5c.1 S5c1
S5c.2 S5c2
S5c.3 S5c3
S5c.4 S5c4
S5c.5 S5c5
S5c.6 S5c6
S5c.7 S5c7
S5c1 $[COIL] Coil[BAR] Bar[ARC] Arc Source
S5c2 #     current:|
S5c3 #      length:|
S5c4 #          dx:|#  dz (or dy):|
S5c5 #   no_of_pts:|
S5c6 #(Origin and Orientation Angles)    xc:|
  #    yc:|#    zc:|#  thxy:|#  thyz:|#  thxz:|
S5c7 #       angle:|
S5d $(You must choose one:)[;] Specify Another Cur
  rent Source[;] End Current Source List
S5d.1 S5e S5b S5c S5d
S5e #( )
S5f %[NL56] Enter a B-H Curve in one of three ways
  [NL97] Thermal conductivity in x-direction
  [NL151] Thermal conductivity in y-direction
  [NL205] Thermal conductivity in z-direction
  [NL103] Electrical conductivity in x-direction
  [NL157] Electrical conductivity in y-direction
  [NL211] Electrical conductivity in z-direction
  [NL262] Imaginary dielectric matrix diagonal ele
  ments
  [NL109] Magnetic coercive force in x-direction
  [NL163] Magnetic coercive force in y-direction
  [NL217] Magnetic coercive force in z-direction
  [NL115] Thermal gradient in x-direction
  [NL169] Thermal gradient in y-direction
  [NL223] Thermal gradient in z-direction
  [NL121] Electric gradient in x-direction
  [NL175] Electric gradient in y-direction
  [NL229] Electric gradient in z-direction
  [NL133] Piezoelectric matrix
  [NL259] Ratios of mu in global X,Y,Z directions
   (default to 1.0 each)
  [NL271] Elastic stiffness matrix constants
S5f.1 S5f1
S5f.2 S5f2
S5f.3 S5f3
S5f.4 S5f4
S5f.5 S5f5
S5f.6 S5f6
S5f.7 S5f7
S5f.8 S5f8
S5f.9 S5f9
S5f.10 S5f10
S5f.11 S5f11
S5f.12 S5f12
S5f.13 S5f13
S5f.14 S5f14
S5f.15 S5f15
S5f.16 S5f16
S5f.17 S5f17
S5f.18 S5f18
S5f.19 S5f19
S5f.20 S5f20
S5f1 $[6] Specify 6-point B-H curve at six tempera
  tures [21] Specify 21-point B-H curve at a singl
  e temperature [14] Specify 14-point B-H curve at
   two temperatures
S5f1.1 S5f1a
S5f1.2 S5f1b
S5f1.3 S5f1c
S5f1a #(Enter the values H of magnetic field inten
  sity, and then the values B of magnetic flux den
  sity at each of the 6 temperatures (the first va
  lues of B and H are assumed to be 0))
    H2:|  H3:|  H4:|  H5:|  H6:|
  #  B2:|  B3:|  B4:|  B5:|  B6:|
  #  B2:|  B3:|  B4:|  B5:|  B6:|
  #  B2:|  B3:|  B4:|  B5:|  B6:|
  #  B2:|  B3:|  B4:|  B5:|  B6:|
  #  B2:|  B3:|  B4:|  B5:|  B6:|
  #  B2:|  B3:|  B4:|  B5:|  B6:|
S5f1b #(Enter the values H of magnetic field inten
  sity, and then the values B of magnetic flux den
  sity (the first values of B and H are assumed to
   be 0))
    H2:|   H3:|   H4:|   H5:|   H6:|
  #  H7:|   H8:|   H9:|  H10:|  H11:|
  # H12:|  H13:|  H14:|  H15:|  H16:|
  # H17:|  H18:|  H19:|  H20:|  H21:|
  #  B2:|   B3:|   B4:|   B5:|   B6:|
  #  B7:|   B8:|   B9:|  B10:|  B11:|
  # B12:|  B13:|  B14:|  B15:|  B16:|
  # B17:|  B18:|  B19:|  B20:|  B21:|
S5f1c #(Enter the values H of magnetic field inten
  sity, and then the values B of magnetic flux den
  sity at each of the 6 temperatures (the first va
  lues of B and H are assumed to be 0))
    H2:|   H3:|   H4:|   H5:|   H6:|
  #  H7:|   H8:|   H9:|  H10:|  H11:|
  # H12:|  H13:|  H14:|
  #  B2:|   B3:|   B4:|   B5:|   B6:|
  #  B7:|   B8:|   B9:|  B10:|  B11:|
  # B12:|  B13:|  B14:|
  #  B2:|   B3:|   B4:|   B5:|   B6:|
  #  B7:|   B8:|   B9:|  B10:|  B11:|
  # B12:|  B13:|  B14:|
S5f2 #(Enter conductivities at all 6 temperatures)
   KXX1:|  KXX2:|  KXX3:|
  # KXX4:|  KXX5:|  KXX6:|
S5f3 #(Enter conductivities at all 6 temperatures)
   KYY1:|  KYY2:|  KYY3:|
  # KYY4:|  KYY5:|  KYY6:|
S5f4 #(Enter conductivities at all 6 temperatures)
   KZZ1:|  KZZ2:|  KZZ3:|
  # KZZ4:|  KZZ5:|  KZZ6:|
S5f5 #(Enter conductivities at all 6 temperatures)
   VXX1:|  VXX2:|  VXX3:|
  # VXX4:|  VXX5:|  VXX6:|
S5f6 #(Enter conductivities at all 6 temperatures)
   VYY1:|  VYY2:|  VYY3:|
  # VYY4:|  VYY5:|  VYY6:|
S5f7 #(Enter conductivities at all 6 temperatures)
   VZZ1:|  VZZ2:|  VZZ3:|
  # VZZ4:|  VZZ5:|  VZZ6:|
S5f8 #(Enter the 3 diagonal elements)  e11:|  e22:
  |  e33:|
S5f9 #(Enter coercive force at all 6 temperatures)
   MGXX1:|  MGXX2:|  MGXX3:|
  # MGXX4:|  MGXX5:|  MGXX6:|
S5f10 #(Enter coercive force at all 6 temperatures
  ) MGYY1:|  MGYY2:|  MGYY3:|
  # MGYY4:|  MGYY5:|  MGYY6:|
S5f11 #(Enter coercive force at all 6 temperatures
  ) MGZZ1:|  MGZZ2:|  MGZZ3:|
  # MGZZ4:|  MGZZ5:|  MGZZ6:|
S5f12 #(Enter thermal gradient at all 6 temperatur
  es) TGXX1:|  TGXX2:|  TGXX3:|
  # TGXX4:|  TGXX5:|  TGXX6:|
S5f13 #(Enter thermal gradient at all 6 temperatur
  es) TGYY1:|  TGYY2:|  TGYY3:|
  # TGYY4:|  TGYY5:|  TGYY6:|
S5f14 #(Enter thermal gradient at all 6 temperatur
  es) TGZZ1:|  TGZZ2:|  TGZZ3:|
  # TGZZ4:|  TGZZ5:|  TGZZ6:|
S5f15 #(Enter electric gradient at all 6 temperatu
  res) VGXX1:|  VGXX2:|  VGXX3:|
  # VGXX4:|  VGXX5:|  VGXX6:|
S5f16 #(Enter electric gradient at all 6 temperatu
  res) VGYY1:|  VGYY2:|  VGYY3:|
  # VGYY4:|  VGYY5:|  VGYY6:|
S5f17 #(Enter electric gradient at all 6 temperatu
  res) VGZZ1:|  VGZZ2:|  VGZZ3:|
  # VGZZ4:|  VGZZ5:|  VGZZ6:|
S5f18 #(Enter all 18 matrix elements)
    e11:|  e12:|  e13:|
  #  e21:|  e22:|  e23:|
  #  e31:|  e32:|  e33:|
  #  e41:|  e42:|  e43:|
  #  e51:|  e52:|  e53:|
  #  e61:|  e62:|  e63:|
S5f19 #(Enter the "mu" ratios) mu1:|  mu2:|  mu3:|
S5f20 #(Enter the upper part of the symmetric stif
  fness matrix)
   c11:|  c12:|  c13:|  c14:|  c15:|  c16:|
  #       c22:|  c23:|  c24:|  c25:|  c26:|
  #             c33:|  c34:|  c35:|  c36:|
  #                   c44:|  c45:|  c46:|
  #                         c55:|  c56:|
  #                               c66:|
PLAa $(Which Type of Plastic Model?)
  [BIKH] Classical bilinear kinematic hardening
  [ANIS] Anisotropic plasticity behaviour
  [DRPR] Drucker-Prager behaviour
  [MKHP] Multilinear kinematic hardening
  [MIHP] Multilinear isotropic hardening
  [NLEL] Nonlinear Elastic behaviour
PLAa.1 PLAa1a PLAa1b PLAa1c
PLAa.2 PLAa2a PLAa2b PLAa2c PLAa2d PLAa2e PLAa2f
PLAa.3 PLAa3a PLAa3b PLAa3c
PLAa.4 PLAa4a PLAa4b
PLAa.5 PLAa4a PLAa4b
PLAa.6 PLAa4a PLAa4b
PLAa1a ##(Specify up to 6 temperatures at which th
  e stress-strain curves are to be specified (must
   be in ascending order))  Values_of_T:|
PLAa1b ##(Specify the corresponding Yield Stresses
   at the above temperatures)  Yield_Stresses:|
PLAa1c ##(Specify second slopes corresponding to t
  he temperatures.  The second slope is given by t
  he tangent modulus)  Second_Slopes:|
PLAa2a #(Tensile yield stresses in the material x,
   y, and z directions)    Tx:|   Ty:|   Tz:|
PLAa2b #(Tangent moduli corresponding to the yield
   stresses)   TMx:|  TMy:|  TMz:|
PLAa2c #(Compressive yield stresses in the materia
  l x, y, and z directions)    Cx:|   Cy:|   Cz:|
PLAa2d #(Tangent moduli corresponding to the yield
   stresses)   TMx:|  TMy:|  TMz:|
PLAa2e #(Shear yield stresses in the material xy,
   yz, and xz directions)   Sxy:|  Syz:|  Sxz:|
PLAa2f #(Tangent moduli corresponding to the yield
   stresses)   TMx:|  TMy:|  TMz:|
PLAa3a #(Cohesion Value)    CV:|
PLAa3b #(Angle (degrees) of internal friction) the
  ta:|
PLAa3c #(Amount of dilatancy (the increase in mate
  rial volume due to yielding))    DL:|
PLAa4a ##(Specify up to 5 strains at which the str
  ess-strain curves are to be specified (the first
  one should not be 0)) S:|
PLAa4b %%(Choose the sets of temperature and stres
  ses at those temperatures that you wish to speci
  fy - temperatures must be in ascending order)
  [NL19] Set 1[NL25] Set 2[NL31] Set 3[NL37] Set 4
  [NL43] Set 5
PLAa4b.1 TSS1 TSS0
PLAa4b.2 TSS2 TSS0
PLAa4b.3 TSS3 TSS0
PLAa4b.4 TSS4 TSS0
PLAa4b.5 TSS5 TSS0
TSS1 #(Temperature for the first set of stresses)
   T:|
TSS2 #(Temperature for the second set of stresses)
   T:|
TSS3 #(Temperature for the third set of stresses)
   T:|
TSS4 #(Temperature for the fourth set of stresses)
   T:|
TSS5 #(Temperature for the fifth set of stresses)
   T:|
TSS0 ##(Specify the stresses at the given temperat
  ure (corresponding to the given strains)) S:|
Ca #(TYPES OF CREEP EQUATIONS)
  #( TYPE 1:)
  #(             C2   C3  -C4/T)
  #(d(ecr)=C1*sig  *es  *e     *d(t))
  #( )
  #( TYPE 2:)
  #(             C2  C3  -C4/T)
  #(d(ecr)=C1*sig  *t  *e     *d(t))
  #( )
  #( TYPE 3:)
  #(             C2    -rt)
  #(d(ecr)=C1*sig  *r*e   *d(t))
  #( )
  #(                C3  -C4/T)
  #(     r=C1*C5*sig  *e)
  #( )
  #( TYPE 4:)
  #(d(ecr)=C1*(d/dt ec)*d(t)