/H3D/QUAD
Engine Keyword Generate H3D contour output results for /QUAD quad elements.
Format
/H3D/QUAD/Keyword4/Keyword5
#optional next line(s) that lists the parts to save results for.
part_ID1... part_IDN
Example
/H3D/QUAD/VONM
/H3D/QUAD/ENER
1 55 75
/H3D/QUAD/USER/UVAR=12
/H3D/QUAD/LAW20/DENS1
Definitions
Comments
- The syntax /H3D/ELEM/Keyword3/Keyword4/Keyword5 is also valid.
- When PART IDs are listed after the /H3D/QUAD 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 BULK Artificial Viscosity DAM1, DAM2, DAM3 Principal damage values in local cracking skew direction 1, 2 or 3 for material LAW24 with /QUAD elements DENS Density DT Time Step ENER Specific energy density (internal energy divided by the element mass) HOURGLASS Hourglass energy 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.
FORC All forces and moments in local coordinate system. F1, F2, F3, M11, M21, M31, M12, M22, M32
P Pressure MASS Element Mass 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. VONM Mean element von Mises stress. USER - UVAR=
- i or ALL
User material (/MAT/USERij) law output for user defined variable i. Table 2. Scalar ALE and CFD Output Keyword3 Keyword4 Description BFRAC Burn fraction (for JWL EOS: LAW5 and LAW51) COLOR 1*vfrac1 + 2*vfrac2 + .... + last*vfracN (LAW51 and LAW151 only) K Specific for turbulent energy in CFD LAW20 DENS1 Density for first material DENS2 Density for second material ENER1 Specific Energy for first material ENER2 Specific Energy for second material EPSP1 Plastic Strain for first material P1 Pressure for first material P2 Pressure for second material QVIS1 Artificial Viscosity for first material QVIS2 Artificial Viscosity for second material SSP1 Sound speed for first material. Only available with ALE material laws. SSP2 Sound speed for second material. Only available with ALE material laws. TEMP1 Temperature for first material TEMP2 Temperature for second material VOLUM1 Volume for first material VOLUM2 Volume for second material MACH Mach number (/MAT/LAW151 only) 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 VFRAC1,VFRAC2, VFRAC3,VFRAC4 Volumetric fractions (for ALE multi-material laws: LAW20, LAW37 and LAW51) VORTX Vorticity for ALE material in X direction. Table 3. Tensor Output Keyword3 Keyword4 Keyword5 Description TENS DAMA Cracks tensor at integration points for /MAT/LAW24 only. If Keyword5 is blank, the mean value in the element is output.
EPSP - IR
- i or ALL
- IS
- j 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
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
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 notation where the options can be entered in any order.