# Materials

Different material tests could result in different material mechanic character.

- ${S}_{0}$
- Section area in the initial state
- ${l}_{0}$
- Initial length

- Yield point: where material begin to yield. Before yield you can assume
material is in elastic state (the Young's modulus
`E`could be measured) and after yield, material plastic strain which is non-reversible.- Some material in this test will first reach the upper yield point
(R
_{eH}) and then drop to the lower yield point (R_{eL}). In engineer stress-strain curve, lower yield stress (conservative value) could be taken. - Some material can not easily find yield point. Take the stress of 0.1 or 0.2% plastic strain as yield stress.

- Some material in this test will first reach the upper yield point
(R
- Necking point: where the material reaches the maximum stress in engineer stress-strain curve. After this point, the material begins to soften.
- Failure point: where material failed.

- R
_{m} - Maximum resistance
- F
_{max} - Maximum force
- R
_{eH} - Upper yield level
- R
_{eL} - Lower yield level
- A
_{g} - Uniform elongation
- A
_{gt} - Total uniform elongation
- A
_{t} - Total failure strain

True stress-strain curve which is requested in most materials in Radioss, except in LAW2, where both engineer stress-strain and true stress-strain are possible to input material data.

- Linear extrapolation: If stress-strain curve is as function input (LAW36), then stress-strain curve is linearly extrapolated with a slope defined by the last two points of the curve. It is recommended that the list of abscissa value be increased to a value greater than the previous abscissa value.
- Johnson-Cook: After necking point, Johnson-Cook hardening is one of the most
commonly used to extrapolate the true stress-strain curve.
(5) $${\sigma}_{y}=a+b{\epsilon}_{p}{}^{n}$$However, it may overestimate strain hardening for automotive steel, In this case, combination of swift-voce hardening is more accurate.

- Swift and Voce: After necking point, use one of the following equations to
extrapolate the true stress-strain curve.
- Swift model
- ${\sigma}_{y}=A{\left({\overline{\epsilon}}_{p}+{\epsilon}_{0}\right)}^{n}$
- Voce model
- ${\sigma}_{y}={k}_{0}+Q\left[1-\mathrm{exp}\left(-B{\overline{\epsilon}}_{p}\right)\right]$
- Combination of Swift and Voce model (LAW84 and LAW87)
- ${\sigma}_{y}=\alpha \underset{Swift\begin{array}{c}\end{array}hardening}{\underbrace{\left[A{\left({\overline{\epsilon}}_{p}+{\epsilon}_{0}\right)}^{n}\right]}}+(1-\alpha )\underset{Voce\begin{array}{c}\end{array}hardening}{\underbrace{\left\{{k}_{0}+Q\left[1-\mathrm{exp}\left(-B{\overline{\epsilon}}_{p}\right)\right]\right\}}}$