box.data1

来自「Triangular mesh processing tool, current」· DATA1 代码 · 共 2,400 行 · 第 1/5 页

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734 $(THERE ARE 3 WAYS TO MOVE THE CURSOR)[KEY] B
  y certain keys[MOUSE] By mouse[OPTION] By selec
  ting certain options
734.1 735 744 745 746 747 736 748 738
734.2 737
734.3 739 740
735 #(INSERT mode is the default mode when the di
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744 #( )
745 #(STRIKEOVER mode is entered via the ESC key.
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746 #( )
747 #(The CTRL E key deletes the character at the
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748 #( )
736 #(A return moves the cursor to the next avail
  able spot, unless the input string has not been
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   string also does this if the code requires onl
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   purpose in the case of Fortran expressions.)
   Some of the following require lists, while oth
  ers require only single numbers.  See which are
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  ppens when a string is incorrectly ended, but t
  he user types 'RET') x1:| y1:| >|
738 ##  ??| ??|
737 ##(Placing the mouse on a character in an inp
  ut string places the cursor there.  However, be
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  e of a string, the syntax only up to the curren
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739 #(When an option requires numbers to be enter
  ed and all others were completed, the cursor au
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740 $[ ] Just to illustrate . . .
740.1 742
742 #(The cursor moves to here automatically)
     Here it is>|
743 #(TO RETURN TO THE MAIN MENU, deselect the cho
  sen entry (above and highlighted in yellow)
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600 $(NIKE3D Material Types)
  [1] Elastic
  [2] Orthotropic Elastic
  [3] Elastic-Plastic
  [4] Thermo-Elastic-Plastic
  [5] Soil And Crushable Foam
  [6] Viscoelastic
  [7] Thermo-Orthotropic Elastic
  [8] Thermo-Elastic-Creep
  [9] Power Law Plasticity
  [10] Power Law Thermo-Elastic Plastic
  [11] Transient Thermal Creep
  [12] Ramberg-Osgood Elastoplastic
  [13] General Anisotropic Thermo-Elastic
  [14] Oriented Brittle Damage
  [15] Mooney-Rivlin Rubber
  [16] Thermo-Plastic Melt
  [17] Foundation Boundary Spring
  [18] Transversely Isotropic Hyper-elasticity
  [19] Strain Rate Sensitive Power Law Plasticity
  [20] Rigid Body
  [23] Thermo-Orthotropic Elastic Laminate
  [35] Elastic-Plastic with Forming Limit Diagram
  [0] Experimental Material Model
600.1 1426 670 603
600.2 1426 1394 601 602
600.3 1426 670 621
600.4 1426 670 627
600.5 1426 1394 634
600.6 1426 1394 644
600.7 1426 1394 649 602
600.8 1426 1394 662
600.9 1426 1394 685
600.10 1426 1394 694
600.11 1426 1394 502
600.12 1426 1394 1389 1388
600.13 1426 1394 687 602
600.14 1426 1394 nk14
600.15 1426 1397 nk15
600.16 1426 1394 nk16
600.17 1426 1394 nk17
600.18 1426 1397 nk18
600.19 1426 1396 nk19
600.20 1426 670 nk20
600.21 1426 1396 1343 507 522
600.22 1426 1396 nk35
600.23 1426 1415 670 1414
nk14 %[e] Young's modulus
  [pr] Poisson's ratio
  [ft] Tensile strength
  [fs] Cracked shear strength
  [sigy] Compressive yield strength
  [gc] Fracture toughness
  [beta] Shear retention factor
  [eta] Viscosity
nk14.1 609
nk14.2 610
nk14.3 fT
nk14.4 fS
nk14.5 sigma-y
nk14.6 gc
nk14.7 beta
nk14.8 eta
fT #  fT:|
fS #  fS:|
sigma-y # sigma-y:|
gc #  gc:|
beta #  beta:|
eta #  eta:|
nk15 %[ai] Coefficient of first invariant term, A
  [bi] Coefficient of second invariant term, B
  [pr] Poisson's Ratio
  [aflg] Augmented Lagrangian flag
  [altol] Convergence tolerance for augmented Lagr
   angian method
nk15.1 ai
nk15.2 bi
nk15.3 610
nk15.4 aflg
nk15.5 tol
ai #  A:|
bi #  B:|
tol # tolerance:|
aflg $[0] Do not active augmented Lagrangian method
  [1] Activate augmented Lagrangian method
nk16 %[lcyt] Load curve for Young's modulus vs. T
  [lypt] Load curve for Poisson's ratio vs. T
  [lyet] Load curve for thermal expansion coeffici
  ent vs. T
  [fsm] Flow Strength Model
  [ffm] Fluid Flow Model
  [vgm] Void Growth Model
  [lsm] Liquid - Solid Transition Model
  [vardb] Variable Written to Plot Database
nk16.1 802
nk16.2 802
nk16.3 802
nk16.4 fsm
nk16.5 ffm
nk16.6 vgm
nk16.7 lsm
nk16.8 vardb
fsm $[0] elastic
  [1] rate independent elastic-plastic
  [2] rate dependent elastic-plastic
  [3] rate dependent elastic-plastic with recovery
fsm.2 fsm2
fsm.3 fsm3
fsm.4 fsm4
fsm2 %[bulk] Bulk modulus
  [lcyst] Load curve for Yield Stress vs. T
  [lcptt] Load curve for Plastic Tangent vs. T
fsm2.1 bulk
fsm2.2 802
fsm2.3 802
bulk #  k:|
fsm3 %[bulk] Bulk modulus
  [lcist] Load curve for Initial Strength,
   S0 vs. T
  [lcfst] Load curve for Flow Strength Coef.,
   A vs. T
  [lcsrt] Load curve for Strain Rate Sens.,
   m vs. T
  [lcscbt] Load curve for Strengthening Coef.,
   B vs. T
  [lcsent] Load curve for Strengthening Exp.,
   n vs. T
fsm3.1 bulk
fsm3.2 802
fsm3.3 802
fsm3.4 802
fsm3.5 802
fsm3.6 802
fsm4 %[bulk] Bulk modulus
  [lcist] Load curve for Initial Strength,
   S0 vs. T
  [lcfst] Load curve for Flow Strength Coef.,
   A vs. T
  [lcsrt] Load curve for Strain Rate Sens.,
   m vs. T
  [lcsck1t] Load curve for Strengthening Coef.,
   k1 vs. T
  [lcsen1t] Load curve for Strengthening Exp.,
   n1 vs. T
  [lcrck2t] Load curve for Recovery Coef.,
   k2 vs. T
  [lcfren2t] Load curve for First Recovery Coef.,
   n2 vs. T
  [lcsren3t] Load curve for Second Recovery Coef.,
   n3 vs. T
fsm4.1 bulk
fsm4.2 802
fsm4.3 802
fsm4.4 802
fsm4.5 802
fsm4.6 802
fsm4.7 802
fsm4.8 802
fsm4.9 802
ffm $[0] none
  [1] Newtonian
ffm.2 ffm2
ffm2 %[lcfvt] Load curve for Fluid Viscosity vs. T
ffm2.1 802
vgm $[0] none
  [1] pressure cut-off
  [2] Gurson-Tvergaard void growth
vgm.2 vgm2
vgm.3 vgm3
vgm2 %[ivs] Initial void strain
  [lctpt] Load curve for Tensile Pressure Cut-Off
   vs. T
  [lccpt] Load curve for Compress Pressure Cut-Off
   vs. T
  [cemf] Consistent elastic moduli flag
vgm2.1 strain
vgm2.2 802
vgm2.3 802
vgm2.4 offon
strain #  strain:|
offon $[0] off [1] on
vgm3 %[ivs] Initial void strain
  [g1] First Gurson parameter
  [g2] Second Gurson parameter
  [cemf] Consistent elastic moduli flag
vgm3.1 strain
vgm3.2 gurson1
vgm3.3 gurson2
vgm3.4 offon
gurson1 #  g1:|
gurson2 #  g2:|
lsm $[0] none [1] fraction solid interpolation
lsm.2 lsm2
lsm2 %[lcfsft] Load curve for Fraction Solid,
   f vs. T
lsm2.1 802
vardb $[0] effective plastic strain
  [1] void strain
  [2] flow strength
  [3] effective strain rate
nk17 %[matrix] Specify the stiffness matrix
nk17.1 nk171
nk171 #  K11:|  K12:|  K13:|  K14:|  K15:|  K16:|
  #        K22:|  K23:|  K24:|  K25:|  K26:|
  #              K33:|  K34:|  K35:|  K36:|
  #                    K44:|  K45:|  K46:|
  #                          K55:|  K56:|
  #                                K66:|
nk18 %[c1] Mooney-Rivlin Coefficient, C1
  [c2] Mooney-Rivlin Coefficient, C2
  [c3] Exponential Stress Coefficient, C3
  [c4] Fiber Uncrimping Coefficient, C4
  [c5] Modulus of Straightened Fibers, C5
  [k] Bulk Modulus
  [lambda] Fiber stretch for straightened fibers,
  [isf] Initial stretch flag
  [lcis] Load Curve for applying initial stretch
  [aflg] Augmented Lagrangian Flag
  [altol] Tolerance for augmented Lagrangian itera
  tions
  [aopt] Material axes option
nk18.1 c1
nk18.2 c2
nk18.3 c3
nk18.4 c4
nk18.5 c5
nk18.6 bulk
nk18.7 lambda
nk18.8 offon
nk18.9 802
nk18.10 aflg
nk18.11 tol
nk18.12 aopt
c1 #  c1:|
c2 #  c2:|
c3 #  c3:|
c4 #  c4:|
c5 #  c5:|
lambda #  lambda:|
aopt $(Material axes determined by)
  [0] Nodes of the element
  [1] A point and element integration points
  [2] Vectors c=axd, b=cxa
aopt.1 nodes
aopt.2 xpt
aopt.3 avec dvec
nodes %[nodes] Specify local element nodes
nodes.1 nodes1
nodes1 #  node1:|  node2:|  node3:|
xpt %[pt] Specify a fixed point
xpt.1 xpt1
xpt1 #  xp:|  yp:|  zp:|
avec %[avec] Specify the "A" vector
avec.1 avec1
avec1 #  ax:|  ay:|  az:|
dvec %[dvec] Specify the "D" vector
dvec.1 dvec1
dvec1 #  dx:|  dy:|  dz:|
nk19 %[e] Young's modulus
  [pr] Poisson's ratio
  [sck] Strength coefficient
  [hen] Hardening exponent
  [srsem] Strain rate sensitivity exponent
  [isr] Initial strain rate
nk19.1 609
nk19.2 610
nk19.3 nk193
nk19.4 nk194
nk19.5 nk195
nk19.6 nk196
nk193 #  k:|
nk194 #  n:|
nk195 #  m:|
nk196 #  rate:|
nk20 %[e] Young's modulus
  [pr] Poisson's ratio
  [xtrans] X-trans. boundary condition code
  [ytrans] Y-trans. boundary condition code
  [ztrans] Z-trans. boundary condition code
  [xrot] X-rot. boundary condition code
  [yrot] Y-rot. boundary condition code
  [zrot] Z-rot. boundary condition code
  [comflg] Center of mass input options
nk20.1 609
nk20.2 610
nk20.3 xxx
nk20.4 yyy
nk20.5 zzz
nk20.6 xxx
nk20.7 yyy
nk20.8 zzz
nk20.9 comflg
xxx #  x:|
yyy #  y:|
zzz #  z:|
comflg $[0] NIKE3D computes center of mass
  [1] Specify coordinates
comflg.2 comflg2
comflg2 %[xcom] X-coordinate of center of mass
  [ycom] Y-coordinate of center of mass
  [zcom] Z-coordinate of center of mass
comflg2.1 xxx
comflg2.2 yyy
comflg2.3 zzz
nk35 %[e] Young's modulus
  [pr] Poisson's ratio
  [sg0] Yield stress
  [lcxe] Tangent modulus or stress/strain load cur
  ve
  [lclh] Load curve for left side of diagram
  [lcrh] Load curve for right side of diagram
  [lcrx] Load curve giving pressure dependence
  [lcedf] Load curve giving rate dependence of FLD
  [lcedm] Load curve for rate dependent yield stre
  ss
  [eptr] Transient strain for constitutive effects
  [epf] Scalar effective strain to failure
  [scldev] Failure scale factor for deviatoric str
  ess
nk35.1 609
nk35.2 610
nk35.3 stress
nk35.4 802
nk35.5 802
nk35.6 802
nk35.7 802
nk35.8 802
nk35.9 802
nk35.10 strain
nk35.11 strain
nk35.12 2128
stress #  stress:|
601 %[ea] Constitutive Matrix Coefficient Ea[e
  b] Constitutive Matrix Coefficient Eb[ec] Const
  ituitive Matrix Coefficient Ec[prba] Constituti
  ve Matrix Coefficient vba[prca] Constitutive Ma
  trix Coefficient vca[prcb] Constitutive Matrix
   Coefficient vcb[gab] Constitutive Matrix Coeff
  icient Gab[gbc] Constitutive Matrix Coefficient
   Gbc[gca] Constitutive Matrix Coefficient Gca
601.1 611
601.2 612
601.3 613
601.4 614
601.5 615
601.6 616
601.7 617
601.8 618
601.9 619
602 $$(Material Axis Option)
  [aopt 0] By Nodes
  [aopt 1] By Point And Element Center
  [aopt 2] By Normal Vectors
602.2 604
602.3 605 620
603 %[e] Young's modulus[pr] Poisson's ratio
603.1 609
603.2 610
604 %(Coordinates of a Point In Space)
  [xp] x-coordinate of a point in space
  [yp] y-coordinate of a point in space
  [zp] z-coordinate of a point in space
604.1 606
604.2 607
604.3 608
605 %(First Vector)
  [a1] x-component of vector
  [a2] y-component of vector
  [a3] z-component of vector
605.1 637
605.2 638
605.3 639
606 # xp :|
607 # yp :|
608 # zp :|
609 # E :|
610 # v :|
611 # Ea :|
612 # Eb :|
613 # Ec :|
614 # vba :|
615 # vca :|
616 # vcb :|
617 # Gab :|
618 # Gbc :|
619 # Gca :|
620 %(Second Vector)
  [d1] x-component of vector
  [d2] y-component of vector
  [d3] z-component of vector
620.1 1391
620.2 1392
620.3 1393
621 %[e] Young's modulus
  [pr] Poisson's Ratio
  [sigy] Yield stress
  [etan] Hardening modulus
  [beta] Hardening parameter
  [eps] Effective plastic strain
  [es] Effective stress
621.1 609
621.2 610
621.3 622
621.4 623
621.5 624
621.6 625
621.7 626
622 # sigy :|
623 # etan :|
624 # beta :|
625 ##(Effective Plastic Strain Coordinates) >|
626 ##(Effective Plastic Stress Coordinates) >|
627 %[temp] Tempera
  ture[e] Young's Modulus[pr] Poisson's Ratio[alph
  a] Secant Coefficient Of Thermal Expansion[sigy]
   Yield Stress[etan] Plastic Hardening Modulus