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/ANIM/Eltyp/Restype |
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/ANIM/Eltyp/Restype |
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/ANIM/Eltyp/Restype |
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/ANIM/Eltyp/Restype |
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/ANIM/Eltyp/Restype - Animation of Element Data for Specified Result
Generates animation files containing element data for the specified result.
/ANIM/Eltyp/Restype
Data |
Description |
|---|---|
Eltyp |
ELEM - The variable is saved for all types of elements; except where not applicable. |
BRICK - Brick elements |
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SHELL - Shell elements |
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BEAM - Beam elements |
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SPRING - Spring elements |
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TRUS - Truss elements |
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Restype |
DAM1, DAM2 or DAM3 - Damage in direction 1, 2 or 3 (see Element Compatibility: Comments 1 through 6). |
DENS - Density |
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ENER - Specific energy density (internal energy divided by the element mass) |
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EPSP - Plastic strain |
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EPSD - Equivalent strain rate in bricks and also in shells (only available in case of strain rate filtering) |
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FAIL - Number of failed layers for /PROP/TYPE10, /PROP/TYPE11, /PROP/TYPE17, /PROP/TYPE51, /PCOMPP, /MAT/LAW15 and /MAT/LAW25 For the other property sets and material laws the values are: = 0: if the element is not broken = 1: if the element is broken (only available in case shell element: /ANIM/SHELL/FAIL) |
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HOURG - Hourglass energy |
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K - Only used with Eltyp = ELEM, specific for turbulent energy in CFD |
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P - Pressure |
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SIGX - Stress XX |
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SIGY - Stress YY |
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SIGZ - Stress ZZ |
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SIGXY - Shear stress XY |
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SIGYZ - Shear stress YZ |
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SIGZX - Shear stress ZX |
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TEMP - Temperature |
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THIC - Thickness |
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TVIS - only used with Eltyp = ELEM, specific for turbulent viscosity in CFD |
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THIN - % thinning for shell. Only available with Eltyp = SHELL. |
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USRi - Variable of user law (i =1 to 18) |
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USRII/JJ - Variable of user law on each integration points (II =1 to 99 number of the variable, JJ =1 to 99 number of layer). (only available in case of shell element: /ANIM/SHELL/USRII/JJ) (Comment 7) |
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VONM - von Mises stress |
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SIGEQ – Equivalent stress, based on the yield criteria used for the corresponding material (Comment 17) |
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VORTX - Only used with Eltyp = ELEM, specific for vorticity in CFD |
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ERROR/THICK - Estimated error on shell thickness |
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FLAY - Number of failed layers for solids |
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PHI/N or PHI/ALL – Angle between element skew and direction 1 of orthotropy. It is only available with Eltyp = SHELL. PHI is only valid for /PROP/TYPE11 and /PROP/TYPE16. = N: Output angle in integration point N (through shell thickness). = ALL: Output angle in all integration points through shell thickness |
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VFRAC – Volumetric fractions (for ALE multi-material laws: LAW20, LAW37 and LAW51) BFRAC – burn fraction (for JWL EOS: LAW5 and LAW51) |
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ORTHDIR – Euler angles ( ORTHDIR/ALL – Euler angles ( Defining orthotropic reference system with global reference system - only for orthotropic solid properties. (Comment 15) |
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SSP - Sound speed. Only available with ALE material laws. |
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SCHLIEREN - Schlieren image (optical method widely used in CFD field). Only available with ALE material laws (Comment 15) |
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FILL - Filling percentage. This option is used only with Eltyp =BRICK for /INIBRI/FILL. |
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PLY - If the plyxfem option is activated, each layer is modeled as a shell element. |
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QVIS - Only used with Eltyp= ELEM, to display artificial viscous pressure. |
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VOLU - Volume of each phase (Only for LAW51 and Eltyp =BRICK) |
| 1. | Damage in springs is defined as the maximum value between time 0 and the current time of the displacement versus failure displacement ratio: |
| 2. | For TYPE13 (/PROP/SPR_BEAM) springs, damage direction 1 is traction/compression, 2 and 3 are shear y and z. |
| 3. | For TYPE8 (/PROP/SPR_GENE) springs, damage directions 1, 2 and 3 are, respectively x, y and z. |
| 4. | For quad or brick elements, /ANIM/ELEM/DAM1, DAM2, and DAM3, are available for Material LAW24. These values are the principal values of the damage (values in the local cracking skew). |
| 5. | For shell and 3-node shell elements, /ANIM/ELEM/DAM1, DAM2, and DAM3, are available for Material LAW15 and LAW25. These values are the principal values of the damage (values in the local orthotropic skew). |
| 6. | The "SPH outputs" are available with /ANIM/Eltyp = ELEM/Restype (all Restype values; except Restype = THIC or HOURG). The Restype values: DAM1, DAM2 or DAM3 are only available with Material LAW24. |
| 7. | User variables are only available for shell and brick elements. When an integration point is not explicitly described, returned integration point means the integration point is superior; computed as [(number of integration points in thickness + 1) / 2]. The result is then rounded up to the superior value. |
Example:
For two integration points in thickness, second integration point from bottom (top of thickness) is returned.
For three integration points in thickness, second integration point from bottom (middle one) is returned.
For four integration points in thickness, third integration point from bottom is returned.
| 8. | For brick elements, the stresses are output in the elemental (corotational) coordinate system for /PROP/SOLID elements, and in the orthotropic material coordinate system for /PROP/SOL_ORTH elements, when corotational formulation is used. For all other cases the stresses are output in the global coordinate system. |
| 9. | The option /ANIM/ELEM/SIGX is only applied for shell elements. For brick elements, /ANIM/BRICK/TENS must be used. |
| 10. | In /ANIM/ELEM/SIGX and /ANIM/ELEM/SIGY, shell stress is located on the center of the element. |
| 11. | The option /ANIM/SHELL/EPSP given for Material LAW25 the plastic work output. |
| 12. | THIN is only available with Eltyp = SHELL. |
| 13. | THIN is computed as: |
| 14. | With ERROR/THICK, an estimated error on shells and 3-node shells thickness is computed as follows: |
Nodal thickness is computed as:
where, A(Ek(n)), t(Ek(n)) are the area and thickness of element Ek(n) containing node n.
Then the thickness error is evaluated for each element E, using the formula
| 15. | Using /ANIM/BRICK/ORTHDIR with properties 6, 21, and 22 will output 3 real values of angle  in unit [deg]. Defining rotation matrix R, to go from global reference system to orthotropic reference system: |
Rotation matrices
A rotation of 
radians about the x-axis is defined as:
Similarly, a rotation of 
radians about the y-axis is defined as:
Finally, a rotation of 
radians about the z-axis is defined as:
The angles 
are the Euler angles:
| 16. | The Schlieren contour value is computed using  . RADIOSS outputs  using c - 1. The constant ‘c’ can be updated using HyperView by creating a Derived Result: |
| 17. | The option SIGEQ is available with Eltyp = SHELL or BRICK only. Each material law, in RADIOSS has its own yield criterion to calculate the equivalent stress. For some it is von Mises; for others, it is Hill or Barlat or something else. |
| 18. | The option PLY is only available for SHELL. In this case, composite shells using the plyxfem formulation or modeled with one shell/ply. Each created shell is offset from the original shell to its true position. |
| Note: | The size of the animation files may be highly increased. |
| 19. | For brick elements using LAW51, the following options are displayed per phase: |
/ANIM/ELEM/P
/ANIM/ELEM/DENS
/ANIM/ELEM/ENER
/ANIM/ELEM/SSP
/ANIM/ELEM/EPSP
/ANIM/ELEM/TEMP
/ANIM/ELEM/VOLU
/ANIM/MASS
) in unit 
) in all layers