/H3D/SOLID

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

Figure 1.

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

/H3D/SOLID/ENER 
1 55 75

Definitions

Comments

1. The syntax /H3D/ELEM/Keyword3/Keyword4/Keyword5 is also valid.
2. When PART IDs are listed after the /H3D/SOLID line the specified results will only be output for those parts.
3. 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. If Keyword4 is blank, the maximum integration point value in the element is output. 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
   FLDF	OUTER	FLD damage factor indicator. 6
   FLDZ	OUTER	FLD failure zone factor for the FLD failure model. = 1 Loose metal = 2 High wrinkle = 3 Compression = 4 Safe = 5 Marginal = 6 Failure 6
   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.
   TEMP		Temperature
   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 ${\sigma }_{y0}$ for /FAIL/SNCONNECT.
   VDAM3	IR= i or ALL IS= j or ALL IT= k or ALL	Value of rupture surface ${\sigma }_{yf}$ 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		1*vfrac1 + 2*vfrac2 + .... + 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.
   	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 Icpre=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.
   		OUTER	Membrane strain tensor on the outer surface of a solid or thick shell component. The membrane layer is automatically created, and the solid strain tensor is extrapolated to this surface.
   	STRAIN_ENG	--	Infinitesimal total strain. Only one tensor per element.
   	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.
   		OUTER	Membrane stress tensor on the outer surface of a solid or thick shell component. The membrane layer is automatically created, and the solid stress tensor is extrapolated to this surface.

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