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Subsections


17.1.5 Rankine Principal Stress Model

The yield condition of Rankine is a maximum principal stress criterion and can be used to simulate cracking of brittle materials, such as concrete and rock. See also Feenstra [27]. The formulation of the Rankine yield condition reads

f1($\displaystyle \boldsymbol\sigma$,$\displaystyle \kappa_{{1}}^{}$) = $\displaystyle \sigma_{{1}}^{}$ - $\displaystyle \bar{{\sigma }}_{{1}}^{}$($\displaystyle \kappa_{{1}}^{}$) = $\displaystyle \sqrt{{ \tfrac{1}{2}{\boldsymbol{\sigma}}^{\mathrm{\scriptscriptstyle{T}}}\mathbf{P} \boldsymbol{\sigma}}}$ + $\displaystyle {\tfrac{{1}}{{2}}}$$\displaystyle \boldsymbol\pi$1T$\displaystyle \boldsymbol\sigma$ - $\displaystyle \bar{{\sigma }}_{{1}}^{}$($\displaystyle \kappa_{{1}}^{}$) (17.68)

with the projection matrix P given by

P = $\displaystyle \left[\vphantom{ \negthickspace \begin{array}{cccccc} \tfrac{1}{2...
...& 0 & 0 & 0 \\  [1ex] 0 & 0 & 0 & 0 & 0 & 0 \end{array} \negthickspace }\right.$ $\displaystyle \begin{array}{cccccc} \tfrac{1}{2}& -\tfrac{1}{2}& 0 & 0 & 0 & 0 ...
...& 0 \\  [1ex] 0 & 0 & 0 & 0 & 0 & 0 \\  [1ex] 0 & 0 & 0 & 0 & 0 & 0 \end{array}$ $\displaystyle \left.\vphantom{ \negthickspace \begin{array}{cccccc} \tfrac{1}{2...
...& 0 & 0 & 0 \\  [1ex] 0 & 0 & 0 & 0 & 0 & 0 \end{array} \negthickspace }\right]$ (17.69)

and the projection vector $ \boldsymbol\pi$1 is given by

$\displaystyle \boldsymbol\pi$1 = $\displaystyle \left\{\vphantom{ \negthickspace \begin{array}{c} 1 \\  1 \\  0 \\  0 \\  0 \\  0 \end{array} \negthickspace }\right.$ $\displaystyle \begin{array}{c} 1 \\  1 \\  0 \\  0 \\  0 \\  0 \end{array}$ $\displaystyle \left.\vphantom{ \negthickspace \begin{array}{c} 1 \\  1 \\  0 \\  0 \\  0 \\  0 \end{array} \negthickspace }\right\}$ (17.70)

The formulation shows the basic assumption that the yield condition is formulated for a plane stress situation only. For plane strain and axisymmetric stress situations, the Rankine yield condition is complemented with a tension cut-off criterion in the out-of-plane direction, which can be formulated as

f3($\displaystyle \boldsymbol\sigma$,$\displaystyle \kappa_{{3}}^{}$) = $\displaystyle \sigma_{{3}}^{}$ - $\displaystyle \bar{{\sigma }}_{{3}}^{}$($\displaystyle \kappa_{{3}}^{}$) = $\displaystyle \boldsymbol\pi$3T$\displaystyle \boldsymbol\sigma$ - $\displaystyle \bar{{\sigma }}_{{3}}^{}$($\displaystyle \kappa_{{3}}^{}$) (17.71)

with the projection vector $ \boldsymbol\pi$3 given by

$\displaystyle \boldsymbol\pi$3 = $\displaystyle \left\{\vphantom{ \negthickspace \begin{array}{c} 0 \\  0 \\  1 \\  0 \\  0 \\  0 \end{array} \negthickspace }\right.$ $\displaystyle \begin{array}{c} 0 \\  0 \\  1 \\  0 \\  0 \\  0 \end{array}$ $\displaystyle \left.\vphantom{ \negthickspace \begin{array}{c} 0 \\  0 \\  1 \\  0 \\  0 \\  0 \end{array} \negthickspace }\right\}$ (17.72)

The flow rule is in general given by the associated flow rule g1 $ \equiv$ f1 and g3 $ \equiv$ f3 . With the use of Koiter's rule [55], the plastic strain rate vector is determined by

$\displaystyle \dot{{\boldsymbol{\varepsilon}}}^{{\mathrm{p}}}_{}$ = $\displaystyle \dot{{\lambda}}_{{1}}^{}$$\displaystyle \left\{\vphantom{ \frac{ \mathbf{P} \boldsymbol{\sigma}}{ 2 \Psi } + \alpha_{1} \boldsymbol{\pi}_{1} }\right.$$\displaystyle {\frac{{ \mathbf{P} \boldsymbol{\sigma}}}{{ 2 \Psi }}}$ + $\displaystyle \alpha_{{1}}^{}$$\displaystyle \boldsymbol\pi$1$\displaystyle \left.\vphantom{ \frac{ \mathbf{P} \boldsymbol{\sigma}}{ 2 \Psi } + \alpha_{1} \boldsymbol{\pi}_{1} }\right\}$ + $\displaystyle \dot{{\lambda}}_{{3}}^{}$$\displaystyle \boldsymbol\pi$3 (17.73)

where the scalar $ \Psi$ is given by Equation (17.56).

17.1.5.1 Hardening

The relation between the internal state variables $ \kappa_{{1}}^{}$ and $ \kappa_{{3}}^{}$ , and the plastic process is given by the hardening hypothesis. For the Rankine yield condition we consider two different hypotheses: strain hardening and work hardening.

Strain hardening.

In the case of strain hardening the relation is given in the principal space by

\begin{displaymath}\begin{split}\dot{\kappa}_{1} &= \sqrt{ \dot{\varepsilon }_{1...
...^{\mathrm{p}} \dot{\varepsilon }_{3}^{\mathrm{p}} } \end{split}\end{displaymath} (17.74)

which can be elaborated to

\begin{displaymath}\begin{split}\dot{\kappa}_{1} &= \dot{\lambda}_{1} \\ [1ex] \dot{\kappa}_{3} &= \dot{\lambda}_{3} \end{split}\end{displaymath} (17.75)

Work hardening.

For work hardening the basic assumption is

\begin{displaymath}\begin{split}\dot{ W}_{1}^{\mathrm{p}} &= {\boldsymbol{\sigma...
...iv \bar{\sigma }_{3}( \kappa_{3} ) \dot{\kappa}_{3} \end{split}\end{displaymath} (17.76)

which can be elaborated to

\begin{displaymath}\begin{split}\dot{\kappa}_{1} &= \dot{\lambda}_{1} \\ [\smallskipamount] \dot{\kappa}_{3} &= \dot{\lambda}_{3} \end{split}\end{displaymath} (17.77)

Relation $ \bar{{\sigma }}$ -$ \kappa$ .

For the Rankine yield condition, the translation of uniaxial experimental data to the equivalent stress-internal state variable, the $ \bar{{\sigma }}$ -$ \kappa$ relation, does not depend of the hardening hypothesis as shown in the following example.
Figure 17.9: Derivation of hardening diagram for Rankine
\begin{figure}\begin{footnotesize}\setlength{\unitlength}{1cm}
\begin{picture...
...enterline{\raise 7.8cm\box\graph}
}
\end{picture}\end{footnotesize}
\end{figure}

Consider the uniaxial stress-strain diagram of Figure 17.9a. The plastic strain $ \varepsilon_{{1}}^{{\mathrm{p}}}$ is assumed to be given by $ \varepsilon_{{1}}^{}$ - $ \varepsilon_{{1}}^{{\mathrm{e}}}$ . Figure 17.9b shows the uniaxial stress-plastic strain diagram. The uniaxial plastic strain rate is given by

$\displaystyle \dot{{\varepsilon }}_{{1}}^{{\mathrm{p}}}$ = $\displaystyle \dot{{\lambda}}_{{1}}^{}$ (17.78)

The relation between the uniaxial stress and the equivalent stress is simply

$\displaystyle \bar{{\sigma }}_{{1}}^{}$ = $\displaystyle \sigma_{{1}}^{}$ (17.79)

so the following relation can be derived

$\displaystyle \dot{{\varepsilon }}_{{1}}^{{\mathrm{p}}}$ = $\displaystyle \dot{{\lambda}}_{{1}}^{}$ (17.80)

With this relation, we find for the relation between the uniaxial plastic strain and the internal state variable

$\displaystyle \dot{{\kappa}}_{{1}}^{}$ = $\displaystyle \dot{{\varepsilon }}_{{1}}^{{\mathrm{p}}}$ (17.81)

for both a strain hardening and a work hardening hypothesis. The same procedure holds for the derivation of the $ \bar{{\sigma }}_{{3}}^{}$ - $ \kappa_{{3}}^{}$ relation.


17.1.5.2 Tensile/Compression Combinations

The principal stress criterion of Rankine describes the tensile cracking of a material like concrete. However, the stress state in structures is often a biaxial stress state, i.e., a combination of tension and compression. These stress states can be modeled by a combination of the yield condition of Rankine to describe the tensile regime and another yield condition to describe the compressive regime. This combined yield condition is then treated as a multi-surface plasticity model which can be solved with stable algorithms. DIANA offers two such combinations: Rankine/Von Mises and Rankine/Drucker-Prager, described by Feenstra [27].


Rankine/Von Mises.

The biaxial stress state in a material can be modeled by a combination of the yield conditions of Rankine and Von Mises [§17.1.2]. The first to describe the tensile regime, the latter to describe the compressive regime. This combined yield surface is especially applicable in plane stress situations.

\begin{displaymath}\begin{split}f_{1} ( \boldsymbol{\sigma}, \kappa_{1} ) &= \sq...
...ldsymbol{\sigma} - \bar{\sigma }_{3} ( \kappa_{3} ) \end{split}\end{displaymath} (17.82)


Rankine/Drucker-Prager.

If the material properties depend on the pressure, the Rankine/Von Mises yield condition is not longer applicable. In these situations the yield condition of Rankine can be combined with the yield condition of Drucker-Prager [§17.1.4]. The combined yield condition is now given by

\begin{displaymath}\begin{split}f_{1} ( \boldsymbol{\sigma}, \kappa_{1} ) &= \sq...
...ldsymbol{\sigma} - \bar{\sigma }_{3} ( \kappa_{3} ) \end{split}\end{displaymath} (17.83)


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Next: 17.1.6 Egg Cam-clay Up: 17.1 Isotropic Plasticity Previous: 17.1.4 Drucker-Prager   Contents   Index
DIANA-9.3 User's Manual - Material Library
First ed.

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