Failure Models
The supported failure models in Radioss.
Failure Model Description
Failure Model Keyword | Type | Application | Description |
---|---|---|---|
/FAIL/ALTER | Stress-based for glass | Glass | Stress-based for glass |
/FAIL/BIQUAD | Strain failure model | Ductile metal | Direct input for effective plastic strain to failure |
/FAIL/CHANG | Chang-Chang model | Composite | Failure criteria for composites |
/FAIL/COCKCROFT | Ductile failure model | Ductile material | Cockcroft-Latham failure model |
/FAIL/CONNECT | Failure | Connection, spotweld | Normal and tangential failure model |
/FAIL/EMC | Extended Mohr Coulomb model | Metal | Failure dependent on effective plastic strain |
/FAIL/ENERGY | Energy isotrop | Metal, plastic | Energy density |
/FAIL/FABRIC | Traction | Fabric | Strain failure |
/FAIL/FLD | Forming limit diagram | Metal Forming | Fld |
/FAIL/GENE1 | Failure | Multiple failure model with multiple combinations | |
/FAIL/GURSON | Ductile failure model | Metal | Failure based on void nucleation and growth in metal plasticity |
/FAIL/HASHIN | Composite model | Composite | Hashin model |
/FAIL/HC_DSSE | Extended Mohr Coulomb failure model | Metal | Strain based Ductile Failure Model: Hosford-Coulomb with Domain of Shell-to-Solid Equivalence |
/FAIL/JOHNSON | Ductile failure model | Ductile metal | Johnson-Cook |
/FAIL/LAD_DAMA | Composite delamination | Composite | Ladeveze delamination model |
/FAIL/MULLINS_OR | Hyperelastic damage | Hyperelastic materials | Stress softening Mullins effect of hyperelastic materials |
/FAIL/NXT | NXT failure model | Metal forming | Similar to FLD, but based on stresses |
/FAIL/ORTHBIQUAD | Orthotropic strain failure model | Ductile metal | Direct input for orthotropic effective plastic strain to failure |
/FAIL/ORTHSTRAIN | Orthotropic strain failure | Composite | Orthotropic strain failure criteria with size effects and strain rate effects |
/FAIL/PUCK | Composite model | Composite | Puck model |
/FAIL/RTCL | Ductile failure model | Ductile metal | RTCL (Rice – Tracey – Cockroft – Latham) failure model |
/FAIL/SAHRAEI | Battery model | Battery cells | Orthotropic strain-based failure model to predict failure and shortcut in battery cells |
/FAIL/SNCONNECT | Failure | Connection, spot weld | Failure criteria for plastic strain |
/FAIL/SPALLING | Ductile + Spalling | Ductile metal | Spalling + Johnson-Cook |
/FAIL/TAB1 | Strain failure model | Ductile metal | Based on damage accumulation using user-defined functions |
/FAIL/TAB2 | Strain failure model | Ductile metal | Based on damage accumulation using user-defined functions |
/FAIL/TBUTCHER | Tuler-Butcher model | Ductile metal | Failure due to fatigue |
/FAIL/TENSSTRAIN | Traction | Metal, plastic | Strain failure |
USER1,USER2, USER3 | User failure model | ||
/FAIL/VISUAL | Visualization of max value | Visualization of the maximum value of every cycle in a simulation | |
/FAIL/WIERZBICKI | Ductile material | Ductile metal | Bao-Xue-Wierzbicki model |
/FAIL/WILKINS | Ductile failure model | Ductile metal | Wilkins model |
Element Compatibility - Part 1
Failure Model | 2D Quad | 8 node Brick | 20 node Brick | 4 node Tetra | 10 node Tetra | 8 node Thick Shell | 16 node Thick Shell |
---|---|---|---|---|---|---|---|
/FAIL/ALTER | |||||||
/FAIL/BIQUAD | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/CHANG | |||||||
/FAIL/COCKCROFT | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | |
/FAIL/CONNECT | ✓ | ||||||
/FAIL/EMC | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/ENERGY | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/FABRIC | |||||||
/FAIL/FLD | |||||||
/FAIL/GENE1 | |||||||
/FAIL/GURSON | ✓ | ✓ | ✓ | ||||
/FAIL/HASHIN | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/HC_DSSE | |||||||
/FAIL/JOHNSON | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/LAD_DAMA | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/MULLINS_OR | ✓ | ✓ | ✓ | ✓ | |||
/FAIL/NXT | |||||||
/FAIL/ORTHBIQUAD | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/ORTHSTRAIN | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/PUCK | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/RTCL | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/SAHRAEI | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/SNCONNECT | ✓ | ||||||
/FAIL/SPALLING | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/TAB1 | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/TAB2 | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/TBUTCHER | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/TENSSTRAIN | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/USERi | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/VISUAL | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/WIERZBICKI | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
/FAIL/WILKINS | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ | ✓ |
✓: yes
blank: no
Element Compatibility - Part 2
Failure Model | SHELL | TRUSS | BEAM |
---|---|---|---|
/FAIL/ALTER | ✓ | ||
/FAIL/BIQUAD | ✓ | ||
/FAIL/CHANG | ✓ | ||
/FAIL/COCKCROFT | ✓ | ||
/FAIL/CONNECT | |||
/FAIL/EMC | |||
/FAIL/ENERGY | ✓ | ||
/FAIL/FABRIC | ✓ | ||
/FAIL/FLD | ✓ | ||
/FAIL/GENE1 | |||
/FAIL/GURSON | |||
/FAIL/HASHIN | ✓ | ||
/FAIL/HC_DSSE | ✓ | ||
/FAIL/JOHNSON | ✓ | ||
/FAIL/LAD_DAMA | ✓ | ||
/FAIL/MULLINS_OR | |||
/FAIL/NXT | ✓ | ||
/FAIL/ORTHBIQUAD | ✓ | ||
/FAIL/ORTHSTRAIN | ✓ | ||
/FAIL/PUCK | ✓ | ||
/FAIL/RTCL | ✓ | ||
/FAIL/SAHRAEI | |||
/FAIL/SNCONNECT | |||
/FAIL/SPALLING | |||
/FAIL/TAB1 | ✓ | ||
/FAIL/TAB2 | ✓ | ||
/FAIL/TBUTCHER | ✓ | ||
/FAIL/TENSSTRAIN | ✓ | ||
/FAIL/USERi | ✓ | ||
/FAIL/VISUAL | ✓ | ||
/FAIL/WIERZBICKI | ✓ | ||
/FAIL/WILKINS | ✓ |
✓: yes
blank: no
Law Compatibility with (Metal) Failure Model
Law Compatibility for Composite and Other Failure Models
✓: yes
blank: no
* : for shells only
** : for solid only
***: LAW1 and /FAIL/LAD_DAMA could only together used as interply material by Plyxfem in /PROP/TYPE17
‡ : flag Istrain (defined in property card) must be activated
Comments
- Failure models are not available with global integration (N=0 in /PROP/SHELL) for shells.
- Keyword USER1, USER2 and USER3 refer to /FAIL/USERi for shell and brick elements.
- Up to 6 failure models can be applied to a single material, each failure model representing a failure mode.
- Failure models can be used for SPH simulation for all materials compatible with SPH formulation.
- Four failure models (FLD, JOHNSON, TAB1, and TBUTCHER) are compatible when X-FEM provided property TYPE1 (SHELL), TYPE11 (SH_SANDW), or TYPE51 is used.
- /FAIL/TAB1 and /PROP/TYPE51 cannot be used with XFEM yet.
- FAIL/ORTHSTRAIN is compatible with material or failure which could be used with orthotropic properties.