# RD-E: 2601 Failure Strain

Failure criteria defined in material LAW2 and LAW27.

In Radioss, one simple way to define material failure is by defining a failure strain in the material definition. In this example, a maximum plastic strain ${\epsilon}_{p}^{max}$ is defined in LAW2 and compared to LAW27 which uses a damage model based on strain. A model with one shell element is used to understand the failure definition. In a second model a metallic thick plate is perforated by a rigid sphere.

## Options and Keywords Used

- Imposed velocities (/IMPVEL)
- Max. plastic strain (/MAT/LAW2 (PLAS_JOHNS))
- Damage model input (/MAT/LAW27 (PLAS_BRIT))
- Rigid sphere (/RWALL)

## Input Files

Refer to Access the Model Files to download the required model file(s).

The model files used in this example are available in:

/radioss/example/26_Ruptured_plate

## Model Description

A one shell element is used to demonstrate the failure model.

The material undergoes an isotropic elasto-plastic behavior which can be reproduced by a Johnson-Cook model.

- Young's modulus
- 71000 $\left[\mathrm{MPa}\right]$
- Poisson's ratio
- 0.3
- Density
- 2.8 x 10
^{-3}g/mm^{3} - Yield stress
- 290 $\left[\mathrm{MPa}\right]$
- Hardening parameter
- 562.3 $\left[\mathrm{MPa}\right]$
- Hardening exponent
- 0.63
- Maximum stress
- 425

The maximum stress and the failure plastic strain are considered in the failure modeling section. The strain rate effect is not taken into account in this example. Although LAW2 and LAW27 both use a Johnson-Cook material model for elasto-plastic behavior, the failure definition included in the material law is different.

### LAW2: Use Plastic Strain for Failure

### LAW27: Use a Damage Model

LAW27 is used to simulate material damage using a Johnson-Cook plasticity law. A damage model is incorporated into the material law to take into account the damage evolution where stress decreases up to element rupture. When using the material failure included in LAW27, the failure and damage occur only in tension and not compression.

The damage parameters in the principal direction $i=1,2$ are ${\epsilon}_{ti},{\epsilon}_{fi},{\epsilon}_{mi}$.

${\epsilon}_{ti}=0.14$; ${\epsilon}_{mi}=0.15$; ${\epsilon}_{fi}=0.16$

In directions, $i=1,2$.

The stress is then reduced using the damage parameter, ${\sigma}_{i}^{reduced}={\sigma}_{i}\left(1-{d}_{i}\right)$.

## Results

### One Element Shell Model

- Test 1: Uniaxial testWith ${\epsilon}_{f1}\begin{array}{c}\end{array}in\begin{array}{c}\end{array}LAW27=({\epsilon}_{e}+{\epsilon}_{p}^{\mathrm{max}})\begin{array}{c}\end{array}in\begin{array}{c}\end{array}LAW2$
- In LAW27, ${\epsilon}_{ti},{\epsilon}_{mi},{\epsilon}_{fi}$ are total strain.
- In LAW2, ${\epsilon}_{p}^{max}$ is plastic strain.

In one shell element set:- In LAW27, ${\epsilon}_{f1}=0.16$
- In LAW2, ${\epsilon}_{p}^{\mathrm{max}}=0.1559$

So that element deleted at same strain.(3) ${\epsilon}_{total}={\epsilon}_{e}+{\epsilon}_{p}=\frac{{\sigma}_{y}}{E}+0.1559=\frac{290}{71000}+0.1559=0.16$ Although the element is deleted at same strain the internal energy at failure is different for LAW2 and LAW27, due to the difference the failure treatment. - Test 2: Equibiaxial testThe failure strain values from the uniaxial test are used in a equibiaxial test.
- In LAW27, ${\epsilon}_{f1}=0.16$
- In LAW2, ${\epsilon}_{p}^{\mathrm{max}}=0.1559$

In biaxial loading, the element deletion is different for LAW2 and LAW27, due to different failure treatment in LAW2 and LAW27. In LAW2, the element is deleted when ${\epsilon}_{p}^{max}$ is reached in the element. The change in plastic strain is:(4) ${\dot{\epsilon}}_{p}\cdot \text{\Delta}t=\frac{{\sigma}_{VM}-{\sigma}_{y}}{E}=\frac{\sqrt{\frac{1}{2}\left[{\left({\sigma}_{1}-{\sigma}_{2}\right)}^{2}+{\sigma}_{1}{}^{2}+{\sigma}_{2}{}^{2}\right]}}{E}-\frac{{\sigma}_{y}}{E}$ For

`I`_{plas}=2 radial return. For additional information, refer to Stress and Strain Calculation in the Theory Manual.

The second principal strain is calculated in a similar manner.

### Plate Impact Model

`I`

_{strain}=1 must be defined, so that the strains are calculated and output for post-processing. This can be defined for all shell elements using /DEF_SHELL.

- For LAW2, the message is:
`RUPTURE OF SHELL ELEMENT NUMBER #` - For LAW27, the message is:
`TOTAL ELEMENT TENSION FAILURE, ELEMENT #`

### Conclusion

Although LAW2 and LAW27 both use Johnson-Cook to describe elasto-plastic behavior, they use different failure treatment. LAW2 checks with plastic strain and LAW27 checks with principal strain. LAW27 uses damage parameter d to produce linear failure; which makes it difficult to get the same failure behavior between them.