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NOARCLDA for no arc length damping
NREST for number of time steps between restart file generation
NSMD for nonlinear solution method which can be
BFGS for BFGS (default)
BROY for Broyden
DFP for Davidon-Fletcher-Powell
MDAV for modified Davidon
MNEWT for modified Newton
MARC for modified constant arc length
MCLS for modified constant arc length with line search
MABFGS for modified constant arc length with BFGS
MABROY for modified constant arc length with Broyden
MADFP for modified constant arc length with DFP
MAMBFGS for modified constant arc length with modified BFGS
MADAV for modified constant arc length with Davidon
NEWT for full Newton
NEWTLS for full Newton with line search
NSTEPS for number of time steps
NUNLOAD for number of unloading steps in modified arc length method
OPNIT for optimal number of iterations per step
PRLIS for linear iterative solver print-out flag with values
0 for no inner loop information
1 for time step convergence information
2 for iteration norm information
3 for residual input, solution output
4 for residual/solution each iteration
RETOL to set the convergence tolerance on residual norm
SEGS to set the shell element geometric stiffness flag
SFOR for shell element formulation which can be
HL for Hughes-Liu
YASE for YASE
BT for Belytschko-Tsay (DYNA3D-like)
SHIFT for frequency shift
SSDM for shell surface strain data dumps
STIFCORE for stiffness matrix storage option
SW3 for toggle the default sense switch number 3
SW6 for toggle the default sense switch number 6
SW7 for toggle the default sense switch number 7
TEO for thermal effects option
XVEL for load due to x-angular velocity
YVEL for load due to y-angular velocity
ZVEL for load due to z-angular velocity
LSNKOPTS: LSNIKE3D analysis options.
ANAL with the options
STAT for static
DYN for dynamic analysis
DYNS for dynamic analysis with stresses initialized statically
ARCL for desired arc length
ARCLCM for the arc length constraint method which can be
CRISFIELD
RAMM
ARCLDAMP for arc length damping
AUTO for automatic time step control invoked
BRSTIF for brick element geometric stiffness included
BWMO for bandwidth minimization on/off switch
DCTOL for displacement convergence tolerance
DELT for time step
DISPNODE for node number for displacement controlled arc length method
DISPDIR for direction of displacement at node for arc length control
1 is for the global x-direction
2 is for the global y-direction
3 is for the global z-direction
DSFCT for force vs. displacement table displacement scale factor
DTROC for type of force recovery resulting from enforced boundary conditions
ECTOL for energy convergence tolerance
FRQSHT for frequency shift, cycles per unit time
FSFCT for force vs. displacement table force scale factor
ICNT1 for initial stiffness matrix formulation frequency
ICNT2 for equilibrium iteration frequency
ICNVRG for displacement criteria to check convergence
IDYNRST for number of materials to initialize stresses in LSDYNA
IFB for output force balance table
IFDOF for degree-of-freedom for node in force vs. displacement table
IFFD for output force vs. displacement table
IFPRI for force dump print interval
INFNM1 for interface number to end first phase
INFNM2 for interface number to end second phase
INITSTR for read initial element stresses
IOBUF for buffer size (words) for element data I/O
IORO for Quasi-Newton update vectors storage
IPLT for TUARUS dump interval
IPRT for print dump interval
positive number causes printing each interval excluding step 0 0 causes
printing each step including step 0 negative number causes printing each
interval including step 0
ISLVDT for linear equation solver option
LAUTO for parameter to control of increase in the time step
LCLOD1 for load curve for first phase
LCLOD2 for load curve for second phase
LSTOL for line search convergence tolerance
MNSS for minimum allowable step size
MSRF for maximum number of reform/time steps
MUNLOAD for arc length unloading method which can be
BFGS for BFGS
BROY for Broyden
DFP for Davidon-Fletcher-Powell
DAV for Davidon
MNEWT for modified Newton
MEMSOL for percentage of memory for the solver
MXNRE for maximum number of retries allowable per step
MXSS for maximum allowable step size
NBEI for number of steps between equilibrium iterations
NBSR for number of steps between matrix reformations
NCYCSP for number of cycles for monotonic pressure after reversal
NDPT for node number for force vs. displacement table
NECHO for nodal input data echo flag
NEIG for number of eigenvectors
NGRAV grav_x load_curve grav_y load_curve grav_z load_curve
NIBSR for maximum number of equilibrium iter./matrix reform.
NIP1 for first Newmark integration parameter
NIP2 for second Newmark integration parameter
NPSD for discrete element input flag
NREST for number of time steps between restart file generation
NSMD for nonlinear solution method which can be
BFGS for BFGS (default)
BROY for Broyden
DFP for Davidon-Fletcher-Powell
MDAV for modified Davidon
MNEWT for modified Newton
MARC for modified constant arc length
MCLS for modified constant arc length with line search
MABFGS for modified constant arc length with BFGS
MABROY for modified constant arc length with Broyden
MADFP for modified constant arc length with DFP
MAMBFGS for modified constant arc length with modified BFGS
MADAV for modified constant arc length with Davidon
NEWT for full Newton
NEWTLS for full Newton with line search
NSTEPS for number of time steps
NUNLOAD for number of unloading steps in modified arc length method
NUSRLDP for number of user loading subroutine parameters
N1DECHO for beam element input data echo flag
N2DECHO for shell element input data echo flag
N3DECHO for solid element input data echo flag
OPNIT for optimal number of iterations per step
PENLDC for load curve defining multiple vs. time
PENSTAB for penalty stiffness multiplier for artificial stabilization
SCLMIN for minimum pressure load scale factor
SCLMAX for maximum pressure load scale factor
SPRCNT1 for percentage of nodes in contact to end first phase
SPRCNT2 for percentage of nodes in contact to end second phase
SSDM for shell surface strain data dumps
STIFCORE for stiffness matrix storage option
TARGET for target strain rate
TEO for thermal effects option
XVEL for load due to x-angular velocity
YVEL for load due to y-angular velocity
ZVEL for load due to z-angular velocity
TZ3DOPTS: TOPAZ3D analysis options. T
IUNIT for temperature units with the two exclusive options (enclosure
radiation data only)
Kelvin
Rankine
BWMO for bandwidth and profile minimization selection with
the three exclusive options
no minimization (default)
minimization
minimization, nodal destination vector is read from input file
PHASE to perform phase change calculations
SOLVER to select the analysis solver
FISSLE out of core profile solver
ACTCOL in core profile solver
DACTCOL nonsymmetric profile solver
DSCG diagonally scaled conjugate gradient
ICCG incomplete cholesky conjugate gradient
Nonsymmetric diagonally scaled conjugate gradient
Diagonally scaled bi-conjugate gradient
Incomplete LU bi-conjugate gradient
RADIATION to select the radiation calculation type
with the five exclusive options
VIEW for view factors
FBEXCHNG for familied binary exchange factors
FAEXCHNG for familied ascii exchange factors
BBEXCHNG for black body exchange factors
NFXCHNG for non-familied ascii exchange factors
select type of analysis from the two exclusive options
STEADY for steady state or
TRANSIENT with the options
FIXED for fixed time step with the options
TIMIN for the initial problem time
TIMEND for the final problem time
DELT for the time step size
VARIABLE for variable time step with the options
TIMIN for the initial problem time
TIMEND for the final problem time
DELT for the initial time step size
DTMIN for the minimum time step
DTMAX for the maximum time step
DCMX for the desired maximum temperature change in each time step
above which the time step will be decreased
MFTS for the modification factor for increasing/decreasing time step
IPRT for the number of time steps between printed data output
IPLT for the number of steps between plotted data output
SBRF for the number of time steps between dump file generation
TIPAR for the time integration parameter
select type of problem with the two exclusive options
LINEAR for a linear problem or
NONLINEAR for a nonlinear problem with the options
NBSR for the number of time steps between conductance matrix
reformations
NBEI for the number of time steps between equilibrium iterations
MSRF for the maximum number of conductance matrix reformations per time
step
NIBSR for the maximum number of equilibrium iterations permitted per
conductance matrix reformation
DCTOL for the convergence tolerance for equilibrium iterations
TZRELAX for the relaxation parameter
SBC for the Stefan-Boltzman constant
RCTOL for the radiosity convergence tolerance
MRDI for the maximum number of radiosity iterations
RBAND to specify a set of wavelength breakpoints
EMISSIVITY to specify multiple numbered 2D emissivity curves with the same
number of points as the number of wavelength breakpoints
ELEMENT commands:
BIND: Hughes-Liu beam user defined integration points.
BSD: global beam element cross section definition.
A cross section is referenced by every beam.
Each beam is defined by two end nodes and either a third node or
a coordinate triple to define the orientation of the cross-sectional
local coordinate system of the beam.
Throughout TG, the local coordinate system for the beam element
is referred to by x, y, and z.
They correspond to,respectively, the longitudinal axis
of the beam stretched between the first two nodes, the orthogonal
component from the first node to the third node/coordinate, and
the third direction orthogonal to the first two directions.
The thickness parameters STHI, STHI1, STHI2, TTHI, TTHI1, and TTHI2
are the distances from the center to the boundary of the element.
They are the half thicknesses used by DYNA3D and NIKE3D.
Other parameters are used to define specific dimensions for the
different types of cross sections.
When there is a possibility of specifying a quantity differently
at each end, there will be one option which assigns the same value
to both ends, and then two additional options, one for each end.
These two options are distinguished by the suffix of 1 and 2, respectively.
When multiple beams are generated from information at two ends, some
quantities such as thickness are linearly interpolated.
Other quantities, such as cross-sectional area and moments are not
interpolated.
In this latter case, the values found at the first cross section
are broadcast throughout the string of beams.
Some of the parameters in the cross section definition are also definable
within the definition of the individual beams.
The value of these parameters within the beam definition take
precedence over this beam cross section definition.
The parameters in this cross section definition are code dependent.
The parameters available for each code are listed.
The STHI, STHI1, STHI2, TTHI, TTHI1, TTHI2, AREA, SCAREA, IXX, IYY,
IZZ and LDP options can be
used any time.
ABAQUS: the *BEAM SECTION card is generated using CSTYPE with
7 which defines a Pipe cross section,
8 which defines a Box cross section,
9 which defines a Circle cross section,
10 which defines a I-Beam cross section,
11 which defines a Rectangle cross section,
12 which defines a Hexagon cross section,
13 which defines a Elbow cross section,
14 which defines a Trapezoid cross section,
15 which defines a L-Section cross section,
16 which defines a Arbitrary cross section.
ANSYS:
BAN4 defines the Elastic Beam element 4,
BAN8 defines the Spar element 8,
BAN10 defines the Tension/Compression Spar element 10,
BAN24 defines the Thin Walled Plastic element 24,
BAN33 defines the Thermal Bar element 33,
BAN44 defines the Tapered Unsymmetrical element 44.
DYNA3D: default cross section properties are defined within the
material definition. To override the default material definition
use STHI, STHI1, STHI2, TTHI, TTHI1, TTHI2, AREA, SCAREA, IXX,
IYY, IZZ;
LSDYNA: the following cross section options are available
for LSDYNA beam elements:
Thicknesses
Area and Inertia
Discrete Beams
W-section
C-section
angle section
T-section
rectangular tubing
Z-section
trapezoidal section
MARC: the following cross section options are available for MARC elements:
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