/ANIM/NODA
Engine Keyword Generates animation files containing nodal scalar data.
Format
/ANIM/NODA/Restype
Definitions
Field  Content  SI Unit Example 

Restype  Nodal data type:

Comments

$\text{DMAS}=\frac{\text{DM}}{{\text{M}}_{0}}$
with
$DM=M{M}_{0}$
.Where,
 ${M}_{0}$
 Nodal mass at the beginning of the restart
 $M$
 Current mass

$DM$
is reset to 0 at the beginning of each restart
file.
(1) $$DINER=\left(\frac{Inertia\left(t\right){l}_{0}}{{l}_{0}}\right)$$Where, ${l}_{0}$
 Nodal inertia at the beginning of the current run
 $Inertia\left(t\right)$
 Current inertia
 In case
/DT/AMS is used, a nondiagonal mass matrix is used, which
allows to increase the time step on each line of the mass matrix, the lumped mass
M
${M}_{0}$
is increased with some value
$\text{\Delta}M$
which is compensated with nondiagonal terms, in
order for the total mass to remain constant. Then:
(2) $$NDMAS=\left(\frac{\text{\Delta}M}{{M}_{0}}\right)$$  DAMA2 damage percentages for /INTER/TYPE2 with rupture (Spot_{flag} = 20,
21, or 22):
(3) $$\mathrm{min}\left(100,100\cdot \frac{normal\text{\hspace{0.05em}}\text{\hspace{0.17em}}relative\text{\hspace{0.17em}}displacement}{\mathrm{max}normal\text{\hspace{0.17em}}relative\text{\hspace{0.17em}}displacement}\right)$$(4) $$\mathrm{min}\left(100,100\cdot \frac{\mathrm{tangent}\text{\hspace{0.05em}}\text{\hspace{0.17em}}relative\text{\hspace{0.17em}}displacement}{\mathrm{max}\text{\hspace{0.17em}}tangent\text{\hspace{0.17em}}relative\text{\hspace{0.17em}}displacement}\right)$$  /ANIM/NODA/TEMP is used generally to output nodal temperature for finite element formulation of thermal exchange.
 These options are also available for 3D ALE and FVM airbag problems. The material density, pressure, and temperature is extrapolated to the element nodes, in this case. For FVM airbags the values are extrapolated only to nodes of external and internal airbag surfaces.