/H3D/SOLID

Engine Keyword Generate H3D contour output results for /BRICK, /BRIC20, /TETRA4, /TETRA10 solid elements and /BRICK, /PENTA6, /SHEL16 thick shells.

Format

/H3D/SOLID/Keyword3/Keyword4/Keyword5

#optional next line(s) that lists the parts to save results for.

part_ID₁... part_ID_N

Example

# Stress tensor results for one integration point

/H3D/SOLID/TENS/STRESS/IR=1/IS=2/IT=1

# All Stress tensor integration point results will be output

/H3D/SOLID/TENS/STRESS/IR=ALL/IS=ALL/IT=ALL

# Specific Energy output for only Parts 1, 55, and 75.

/H3D/SOLID/ENER 
1 55 75

Definitions

Data	Description	SI Unit Example
`Keyword3`	Output types. 3
`Keyword4`	Output types. 3
`Keyword5`	Output types. 3
`part_ID`_N	Optional list of part IDs for which results will be output.

Comments

The syntax /H3D/ELEM/Keyword3/Keyword4/Keyword5 is also valid.
When PART IDs are listed after the /H3D/SOLID line the specified results will only be output for those parts.

Output can be a Scalar or Tensor as defined in the following tables.

Table 1. Scalar Output
Keyword3	Keyword4	Description
`AMS`		Elements using `AMS` timestep due to /DT/CST_AMS.
`DAM1`, `DAM2`, `DAM3`		Principal damage values in local cracking skew direction 1, 2 or 3 for material LAW24 with /BRICK elements.
`DAMA`	`IR`= i or ALL `IS`= j or ALL `IT`= k or ALL	Maximum of damage over time of all /FAIL criteria acting on one material. Refer to the specific /FAIL law used for how damage is calculated.
`DENS`		Density
`DOMAIN`		SPMD domain number of an element.
`DT`		Element timestep
`ENER`		Specific energy density (internal energy divided by the element mass)
`EPSD`		Equivalent strain rate
`EPSP`		Plastic Strain
`FILL`		Filling percentage for /INIBRI/FILL
`FLAY`		Number of failed layers
`HOURGLASS`		Hourglass energy
`MASS`		Element mass
`OFF`		Element status. Where the result output is: = -1 Element is not active (it is defined in an activated rigid body). = 0 Deleted element. Between 0 and 1 Under failure process. = 1 Active element.
ORTHD	`LAYER`= i or ALL `IR`= i or ALL `IS`= j or ALL `IT`= k or ALL	Euler angles in degrees defining the rotation matrix to go from global reference system to orthotropic reference system. To request a specific angle use ORTHD/PSI, ORTHD/THETA, or ORTHD/PHI.
`P`		Pressure
`SIGEQ`		Equivalent stress based on a material’s yield criteria. Some examples of yield criteria are von Mises, Hill or Barlat.
`SIGX`, `SIGY`, `SIGZ`, `SIGXY`, `SIGYZ`, `SIGZX`		Mean element stress in specified direction.
`TDEL`		Time at which element is deleted due to failure defined using /FAIL criterion. Failure criteria built in materials is ignored.
`USER`	`UVAR`= i or ALL `IR`= i or ALL `IS`= j or ALL `IT`= k or ALL	User material (/MAT/USERij) law output for user defined variable `i`. Also, requests USR output for some Radioss material laws such as LAW59 or LAW70. `USR1` output is requested using `UVAR`=1. For integration point results, use `IR`, `IS` and `IT` options.
`VDAM1`	`IR`= i or ALL `IS`= j or ALL `IT`= k or ALL	Value of damage factor D, for /FAIL/SNCONNECT.
`VDAM2`	`IR`= i or ALL `IS`= j or ALL `IT`= k or ALL	Value of damage surface $σ_{y 0}$ for /FAIL/SNCONNECT.
`VDAM3`	`IR`= i or ALL `IS`= j or ALL `IT`= k or ALL	Value of rupture surface $σ_{y f}$ for /FAIL/SNCONNECT.
`VONM`		Mean element von Mises stress
`WPLA`		Plastic work for /MAT/LAW12 (3D_COMP) and /MAT/LAW25 (COMPSH)

Table 2. Scalar ALE and CFD Output
Keyword3	Keyword4	Description
`BFRAC`		Burn fraction (for JWL EOS: LAW5 and LAW51).
`BULK`		Artificial Viscosity.
`COLOR`		1vfrac1 + 2vfrac2 + .... + last*vfracN (LAW51 and LAW151 only).
`K`		Specific for turbulent energy in CFD.
`MACH`		Mach number (/MAT/LAW151 only)
`MOM`		Cell momentum Density (`MOM`) for FVM with Interface TYPE22 for all components and magnitude. To request each separately use, `MOMX`, `MOMY`, `MOMZ`, `MOMXY`, `MOMYZ`, `MOMXZ`, `\|MOM\|`.
`SCHLIEREN`		Schlieren image (optical method widely used in `CFD` field). ALE material laws.
`SSP`		Sound speed. Only available with ALE material laws.
`TDET`		Detonation time output.
`TVIS`		Specific for turbulent viscosity in CFD.
`VEL`		Cell velocity for FVM with Interface TYPE22 for all components and magnitude. To request each separately use, `VELX`, `VELY`, `VELZ`, `VELXY`, `VELYZ`, `VELXZ`, `\|VEL\|`.
`VFRAC1`,`VFRAC2`, `VFRAC3`,`VFRAC4`		Volumetric fractions (for ALE multi-material laws: LAW20, LAW37 and LAW51).
`VORT`, `VORTX`, `VORTY`, `VORTZ`		Vorticity for ALE material in resultant, X, Y, and Z components.
`VECT`	`VEL`	Velocity vectors at finite volume cell centroids.
`VECT`	`CONT`	Contact force vectors at finite volume cell centroids.

Table 3. Tensor Output
Keyword3	Keyword4	Keyword5	Description
`TENS`	`DAMA`		Cracks tensor at integration points for Material LAW24 only. If `Keyword5` is blank, the mean value in the element is output.
	`EPSP`	`IR`= i or ALL `IS`= j or ALL `IT`= k or ALL	Plastic strain tensor at integration points, only available for /MAT/LAW24 with `I`_cpre=2. If `Keyword5` is blank, the mean value element is output.
	`STRAIN`	`IR`= i or ALL `IS`= j or ALL `IT`= k or ALL	Strain tensor at integration points. If `Keyword5` is blank, the mean value in the element is output.
	`STRESS`	`IR`= i or ALL `IS`= j or ALL `IT`= k or ALL	Stress tensor at integration points. If `Keyword5` is blank, the mean value in the element is output.

To request integration point results, use /IR=i/IS=j/IT=k notation where the options can be entered in any order.