marc.data1

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

156.12 321
156.13 321
156.14 321
156.15 321
156.16 321
156.17 321
156.18 320
157 %(Material Option ORTHO TEMP)
  [ve11]Slopes of E11 and Temperature
  [ve22]Slopes of E22 and Temperature
  [ve33]Slopes of E33 and Temperature
  [vv12]Slopes of V12 and Temperature
  [vv23]Slopes of V23 and Temperature
  [vv31]Slopes of V31 and Temperature
  [vg12]Slopes of G12 and Temperature
  [vg23]Slopes of G23 and Temperature
  [vg31]Slopes of G31 and Temperature
  [va11]Slopes of a11 and Temperature
  [va22]Slopes of a22 and Temperature
  [va33]Slopes of a33 and Temperature
  [vwhtemp]Slopes of Work Hardening and Temperature
  [vk11]Slopes of K11 and Temperature
  [vk22]Slopes of K22 and Temperature
  [vk33]Slopes of K33 and Temperature
  [vshtemp]Specific Heat and Temperature
  [lhtemp]Latent Heat, Solidus Temperature and
   Liquidus Temperature
157.1 322
157.2 322
157.3 322
157.4 322
157.5 322
157.6 322
157.7 322
157.8 322
157.9 322
157.10 322
157.11 322
157.12 322
157.13 322
157.14 322
157.15 322
157.16 322
157.17 322
157.18 320
158 $$(Material Option DAMAGE)
  [nonucle]No Nucleation
  [pscn]Plastic Strain Controlled Nucleation
  [scn]Stress Controlled Nucleation
  [uvoidn]User Subroutine UVOIDN
  [edm]Elastomeric Damage Model
  [ueldam]User Subroutine UELDAM
158.1 159 ;
158.2 160 ;
158.3 161 ;
158.5 162 ;
159 %(Material Option DAMAGE)
  [q1]First Yield Surface Multiplier
  [q2]Second Yield Surface Multiplier
  [ivf]Initial Volume Fraction
  [fc]Critical Void Volume Fraction
  [ff]Failure Void Volume Fraction
  [msn]Mean Strain for Nucleation
  [sdnr]Standard Deviation in Nucleation Relation
  [vfvnp]Volume Fraction of Void Nucleating
   Particles
159.1 314
159.2 314
159.3 313
159.4 313
159.5 313
159.6 318
159.7 318
159.8 313
160 %(Material Option DAMAGE)
  [q1]First Yield Surface Multiplier
  [q2]Second Yield Surface Multiplier
  [ivf]Initial Volume Fraction
  [fc]Critical Void Volume Fraction
  [ff]Failure Void Volume Fraction
  [msn]Mean Strain for Nucleation
  [sdnr]Standard Deviation in Nucleation Relation
  [vfvnp]Volume Fraction of Void Nucleating
   Particles
160.1 314
160.2 314
160.3 313
160.4 313
160.5 313
160.6 318
160.7 318
160.8 313
161 %(Material Option DAMAGE)
  [q1]First Yield Surface Multiplier
  [q2]Second Yield Surface Multiplier
  [ivf]Initial Volume Fraction
  [fc]Critical Void Volume Fraction
  [ff]Failure Void Volume Fraction
  [msn]Mean Stress for Nucleation
  [sdnr]Standard Deviation in Nucleation Relation
  [vfvnp]Volume Fraction of Void Nucleating
   Particles
161.1 314
161.2 314
161.3 313
161.4 313
161.5 313
161.6 318
161.7 318
161.8 313
162 %(Material Option DAMAGE)
  [ddr]Deviatoric Damage Rate
  [mddf]Maximum Deviatoric Damage Factor
  [vdr]Volumetric Damage Rate
  [mvdf]Maximum Volumetric Damage Factor
162.1 318
162.2 318
162.3 318
162.4 318
163 %(Material Option FAIL DATA)
  [pf]Progressive Failure
  [ffds]First Fail Data Set
  [sfds]Second Fail Data Set
  [tfds]Third Fail Data Set
163.2 164 ;
163.3 164 ;
163.4 164 ;
164 $$(Material Option FAIL DATA)
  [ufail]UFAIL
  [mxstress]MX STRESS
  [mxstrain]MX STRAIN
  [hoffmn]HOFFMAN
  [hill]HILL
  [tsaiwu]TSAI WU
164.2 166 ;
164.3 167 ;
164.4 168 ;
164.5 190 ;
164.6 169 ;
166 %(Material Option FAIL DATA MX STRESS)
  [x]Maximum Tensile Stress in x-dir
  [xc]Maximum Absolute Value of Compressive Stress
   in x-dir
  [y]Maximum Tensile Stress in y-dir
  [yc]Maximum Absolute Value of Compressive Stress
   in y-dir
  [z]Maximum Tensile Stress in z-dir
  [zc]Maximum Absolute Value of Compressive Stress
   in z-dir
  [sxy]Maximum Absolute Value of Shear Stress in xy
   plane
  [syz]Maximum Absolute Value of Shear Stress in yz
   plane
  [szx]Maximum Absolute Value of Shear Stress in zx
   plane
166.1 318
166.2 318
166.3 318
166.4 318
166.5 318
166.6 318
166.7 318
166.8 318
166.9 318
167 %(Material Option FAIL DATA MX STRAIN)
  [ex]Maximum Tensile strain in x-dir
  [exc]Maximum Absolute Value of Compressive
   strain in x-dir
  [ey]Maximum Tensile strain in y-dir
  [eyc]Maximum Absolute Value of Compressive
   strain in y-dir
  [ez]Maximum Tensile strain in z-dir
  [ezc]Maximum Absolute Value of Compressive
   strain in z-dir
  [gxy]Maximum Absolute Value of Shear strain in
   xy plane
  [gyz]Maximum Absolute Value of Shear strain in
   yz plane
  [gzx]Maximum Absolute Value of Shear strain in
   zx plane
167.1 318
167.2 318
167.3 318
167.4 318
167.5 318
167.6 318
167.7 318
167.8 318
167.9 318
168 %(Material Option FAIL DATA HOFFMAN)
  [x]Maximum Tensile Stress in x-dir
  [xc]Maximum Absolute Value of Compressive Stress
   in x-dir
  [y]Maximum Tensile Stress in y-dir
  [yc]Maximum Absolute Value of Compressive Stress
   in y-dir
  [z]Maximum Tensile Stress in z-dir
  [zc]Maximum Absolute Value of Compressive Stress
   in z-dir
  [sxy]Maximum Absolute Value of Shear Stress in
   xy plane
  [syz]Maximum Absolute Value of Shear Stress in
   yz plane
  [szx]Maximum Absolute Value of Shear Stress in
   zx plane
  [fi]Failure Index
168.1 318
168.2 318
168.3 318
168.4 318
168.5 318
168.6 318
168.7 318
168.8 318
168.9 318
168.10 318
169 %(Material Option TSAI WU)
  [x]Maximum Tensile Stress in x-dir
  [xc]Maximum Absolute Value of Compressive Stress
   in x-dir
  [y]Maximum Tensile Stress in y-dir
  [yc]Maximum Absolute Value of Compressive Stress
   in y-dir
  [z]Maximum Tensile Stress in z-dir
  [zc]Maximum Absolute Value of Compressive Stress
   in z-dir
  [sxy]Maximum Absolute Value of Shear Stress in
   xy plane
  [syz]Maximum Absolute Value of Shear Stress in
   yz plane
  [szx]Maximum Absolute Value of Shear Stress in
   zx plane
  [fi]Failure Index
  [fxy]Interactive Strength Tensor Constant for
  the xy-Plane
  [fyz]Interactive Strength Tensor Constant for
   the yz-Plane
  [fzx]Interactive Strength Tensor Constant for
   the zx-Plane
169.1 318
169.2 318
169.3 318
169.4 318
169.5 318
169.6 318
169.7 318
169.8 318
169.9 318
169.10 318
169.11 317
169.12 317
169.13 317
170 $(Material Option DAMPING)
  [ ]Modal Analysis
  [ ]Direct Integration
170.1 171 ;
170.2 172 ;
171 %(Material Option DAMPING MODAL)
  [modal]Fraction of Critical Damping for Modes
171.1 323
172 %(Material Option DAMPING DIRECT
   INTEGRATION)
  [alpha]Multiplier for Mass contribution to
   Damping Matrix
  [beta]Multiplier for Stiffness contribution to
   Damping Matrix
  [gama]Multiplier for Numerical Damping
172.1 314
172.2 314
172.3 314
173 $(Material Option ORIENTATION)
  [edge12]EDGE 1-2
  [edge23]EDGE 2-3
  [edge34]EDGE 3-4
  [edge31]EDGE 3-1
  [edge41]EDGE 4-1
  [xyplane]XY PLANE
  [yzplane]YZ PLANE
  [zxplane]ZX PLANE
  [xuplane]XU PLANE
  [yuplane]YU PLANE
  [zuplane]ZU PLANE
  [uuplane]UU PLANE
  [uorient]UORIENT
  [3daniso]3DANISO
173.1 174
173.2 174
173.3 174
173.4 174
173.5 174
173.6 174
173.7 174
173.8 174
173.9 174 175
173.10 174 175
173.11 174 175
173.12 174 175 176
173.13 174 175
173.14 174 175 176
174 $(Material Option ORIENTATION)
  [or]Orientation Angle
174.1 318
175 %(Material Option ORIENTATION)
  [uv1w]User vector 1 w
  [uv1r]User vector 1 r
  [uv1t]User vector 1 t
175.1 318
175.2 318
175.3 318
176 %(Material Option ORIENTATION)
  [uv2w]User vector 2 w
  [uv2r]User vector 2 r
  [uv2t]User vector 2 t
176.1 318
176.2 318
176.3 318
177 $(Material Option TEMPERATURE EFFECTS)
  [slopes]Slopes
  [values]Values
177.1 179
177.2 178
178 %(Material Option TEMPERATURE EFFECTS)
  [vcotemp]Conductivity and Temperature
  [vshtemp]Specific Heat and Temperature
  [vlhtemp]Latent Heat, Solidus Temperature and
   Liquidus Temperature
  [vretemp]Resistivity and Temperature
  [vetemp]Emissivity and Temperature
178.1 321
178.2 321
178.3 320
178.4 321
178.5 321
179 %(Material Option TEMPERATURE EFFECTS)
  [scotemp]Conductivity and Temperature
  [sshtemp]Specific Heat and Temperature
  [lhtemp]Latent Heat, Solidus Temperature and
   Liquidus Temperature
  [sretemp]Resistivity and Temperature
  [setemp]Emissivity and Temperature
179.1 322
179.2 322
179.3 320
179.4 322
179.5 322
180 $(Material Option ORTHO TEMP)
  [slopes]Slopes
  [values]Values
180.1 181
180.2 182
181 %(Material Option ORTHO TEMP)
  [vk11]Slope of K11 and Temperature
  [vk22]Slope of K22 and Temperature
  [vk33]Slope of K33 and Temperature
  [vshtemp]Slope of Specific Heat and Temperature
  [lhtemp]Latent Heat, Solidus Temperature and
   Liquidus Temperature
  [vr11]Slope of R11 and Temperature
  [vr22]Slope of R22 and Temperature
  [vr33]Slope of R33 and Temperature
181.1 322
181.2 322
181.3 322
181.4 322
181.5 320
181.6 322
181.7 322
181.8 322
182 %(Material Option ORTHO TEMP)
  [vk11]Value of K11 and Temperature
  [vk22]Value of K22 and Temperature
  [vk33]Value of K33 and Temperature
  [vshtemp]Specific Heat and Temperature
  [lhtemp]Latent Heat, Solidus Temperature and
   Liquidus Temperature
  [vr11]Value of R11 and Temperature
  [vr22]Value of R22 and Temperature
  [vr33]Value of R33 and Temperature
182.1 321
182.2 321
182.3 321
182.4 321
182.5 320
182.6 321
182.7 321
182.8 321
183 $(Material Option TEMPERATURE EFFECTS -
   BEARING)
  [slopes]Slopes
  [values]Values
183.1 185
183.2 184
184 %(Material Option TEMPERATURE EFFECTS -
   BEARING)
  [svitemp]Value of Viscosity and Temperature
184.1 321
185 %(Material Option TEMPERATURE EFFECTS -
   BEARING)
  [svitemp]Slope of Viscosity and Temperature
185.1 322
186 $(Material Option B-H RELATION)
  [iso]Isotropic
  [ortho]Orthotropic
186.1 187
186.2 188
187 %(Material Option B-H RELATION)
  [hb]H and B
187.1 319
188 %(Material Option B-H RELATION)
  [h1b1]H1 and B1
  [h2b2]H2 and B2
  [h3b3]H3 and B3
188.1 319
188.2 319
188.3 319
189 $(Stress-Strain Relationships)
  [strainrate]Strain Rate
  [workhard]Work Hard
189.1 136 ;
189.2 137 ;
190 %(Material Option FAIL DATA HILL)
  [x]Maximum Tensile Stress in x-dir
  [xc]Maximum Absolute Value of Compressive Stress
   in x-dir
  [y]Maximum Tensile Stress in y-dir
  [yc]Maximum Absolute Value of Compressive Stress
   in y-dir
  [z]Maximum Tensile Stress in z-dir
  [zc]Maximum Absolute Value of Compressive Stress
   in z-dir
  [sxy]Maximum Absolute Value of Shear Stress in
   xy plane
  [syz]Maximum Absolute Value of Shear Stress in
   yz plane
  [szx]Maximum Absolute Value of Shear Stress in
   zx plane
  [fi]Failure Index
190.1 318
190.2 318
190.3 318
190.4 318
190.5 318
190.6 318
190.7 318
190.8 318
190.9 318
190.10 318
301 # Modulus :|
302 # Ratio :|
303 # Density :|
304 # Coefficient :|
305 # Temperature :|
306 # Yield :|
307 # Conductivity :|
308 # Specific Heat :|
309 # Emissivity :|
310 # Resistivity :|
311 # Permitivity :|
312 # Permeability :|
313 # Fraction :|
314 # Multiplier :|
315 ## List of Viscoplastic Parameters >|
316 # Penalty :|
317 # Constant :|
318 # Value :|
319 ## List of Pairs of Values >|
320 ## List of Triplets of Values >|
321 ## List of Pairs of Function Values and
   Variable Values >|
322 ## List of Pairs of Function Slopes and
   Variable Values >|
323 ## List of Values >|
1350 %(MARC OPTIONS)[MAXALL] Size Of Work Space Ve
  ctor
  [CPU] Number Of CPUs
  [VLENGTH] Optimal Vector Length
  [BMPAR] Beta Matrices To Be Formed In Parallel
  [NOLIST] Suppress Printout Of Remainder Of Input
  [ELASTIC] Elastic Analysis With Multi-Loads
  [LINEAR] Matrices Saved For Linear Analysis
  [FOURIER] Arbitrary Loading Of Axisymmetric Stru
  ctures
  [NFEXP] Number Of Fourier Expansions
  [MXHARM] Maximum Number Of Harmonics
  [NLDFF] Number Of Load Degrees Of Freedom In Fou
  rier Expansion
  [FRSY] Expansion Symmetry Option
  [MXST] Maximum Number Of Fourier Expansion Stati
  ons Around Circumference
  [IMFSS] Initial Stress Stiffness Included In Mod
  al Fourier Expansion
  [DYOP] Dynamic Analysis
  [MXMO] Maximum Number Of Modes Used In The Modal
   Superposition
  [LANCZ] Lanczos Method
  [MSREC] Modal Stress Recovery Or Storing Eigenve
  ctors
  [HARM] Frequency Response Analysis
  [CXDP] Use Complex Damping Matrix
  [XCIT] Maximum Number Of Excitation Boundary Con
  ditions
  [XDLL] Maximum Number Of Excitation Distribution
   Load Lists
  [NELX] Maximum Number Of Elements In Any Excitat
  ion Distribution List
  [INRT] Include Inertia Effects In Calculation Of
   Harmonic Reaction Force
  [SPRA] Spectrum Response Analysis
  [SDPF] Number Of Data Points Used To Specify Spe
  ctral Density Function
  [RPFL] Rigid, Perfectly-Plastic Flow Flag
  [LDISP] Large Displacement Or Buckling Flag
  [UPLGR] Updated Lagrange Procedure
  [FSPL] Finite Strain Plasticity
  [FOLF] Follower Forces: Distributed Load Applica
  tion On Current Geometry
  [BUCK] Buckling Load Estimate Via Eigenvalue Ana
  lysis
  [CREEP] Creep Analysis
  [VISCO] Visco Elastic Analysis (Kelvin Model)
  [COUPLE] Coupled Thermal-Stress Analysis
  [PORE] Soil Analysis
1350.1 1351
1350.2 1352
1350.3 1353
1350.7 1354
1350.9 1355
1350.10 1356
1350.11 1357
1350.12 1358
1350.13 1359
1350.15 1360
1350.16 1361
1350.21 1362
1350.22 1363
1350.23 1364
1350.26 1365
1350.32 1366 1367
1350.33 1368 1369 1370
1350.36 1371 1372
1351 # number of words :|
1352 # number of CPUs :|
1353 # optimal vector length :|
1354 $[W] Save The BETA Matrix And The Stress-Stra
  in Law
  [WO] Save The BETA Matrix (Strain-Displacement)
1355 # number of Fourier expansions :|
1356 # maximum :|
1357 # number of degrees :|
1358 $[-2]only antisymmetric (sin) and skip increm
  ents 0, 1, and 2
  [-1]only symmetric (cos) and skip increments 0 a
  nd 1
  [0]full expansion
  [1]only symmetric (cos)
  [2]only antisymmetric (sin)
1359 # maximum number of stations :|
1360 $[MODAL] modal superposition dynamic response
  [NEWMARK] Newmark direct integration
  [HOUBOLT] Houbolt direct integration
  [CENTRAL] explicit direct time integration using
   central difference
1361 # maximum mode :|
1362 # maximum number of conditions :|
1363 # maximum number of load lists :|
1364 # maximum number of lists :|
1365 # number of points :|
1366 # maximum number of modes :|
  # number of buckling modes :|
1367 $[Y] Perform Modal Stress Recovery Or Store E
  igenvalues
  [N] Do Not Perform Modal Stress Recovery Or Stor
  e Eigenvalues
1368 $[0] normal creep
  [1] viscoplastic creep
  [2] viscoplastic creep with non-associative flow
   rule
1369 $[N] Do Not Use Kelvin Model
  [Y] Use Kelvin Model
1370 $[N] Do Not Use Maxwell Model
  [Y] Use Maxwell Model
1371 $[0] pore pressure data to be entered
  [1] perform steady state pore pressure calculati
  on
  [2] perform transient pore pressure calculation
1372 $[N] calculate only pore pressure
  [Y] perform stress analysis
END OF FILE