Endochronic (internal time) model coupled with damage for elasto-plastic cyclic loading analysis in plane state at constant temperature.
This law is used for mechanical analysis of 2-D continuum element undergone large deformation by using endochronic (internal time) theory coupled with damage model for elasto-plastic cyclic loading.
Prepro: LENDC.F
Lagamine: ENDC2D.F
Plane stress state | NO |
Plane strain state | YES |
Axisymmetric state | YES |
3D state | NO |
Generalized plane state | NO |
Line 1 (2I5, 60A1) | |
---|---|
IL | Law number |
ITYPE | 85 |
COMMENT | Any comment (up to 60 characters) that will be reproduced on the output listing |
Line 1 (2I5) | |
---|---|
NINTV | Number of sub-steps used to integrate numerically the constitutive equation in a time step |
NPOINT | The function form |
= 1 : Linear expansion (for 2-terms kernal function) | |
= 2 : Saturated expansion (for 2-terms kernal function) | |
\[\rho(\zeta)=\rho_0+\rho_1(\zeta)\]\[\rho_1(\zeta)=\frac{E_1}{E}\;e^{-\alpha_1.\zeta}+\frac{E_2}{E}\] | |
= 3 : Linear expansion (for 3-terms kernal function) | |
= 4 : Saturated expansion (for 3-terms kernal function) | |
\[\rho(\zeta)=\rho_0+\rho_1(\zeta)\]\[\rho_1(\zeta)=\frac{E_1}{E}\;e^{-\alpha_1.\zeta}+\frac{E_2}{E}+\frac{E_3}{E}\;e^{-\alpha_3.\zeta}\] |
Line 1 (7G10.0) | |
---|---|
E | YOUNG's elastic modulus |
$\nu$ | POISSON's ratio |
$\sigma_o$ | Initial yield limit |
$\sigma_f$ | Yield limit at finite strain |
$E_{to}$ | Initial tangent modulus |
$E_{tf}$ | Tangent modulus at finite strain |
Thickness = 1.0 (by default) | |
$\varepsilon_f$ | Equivalent plastic strain at the unloading point |
Line 2 (7G10.0) | |
$2\sigma_y$ | Stress drop during the elastic unloading |
= 2$\sigma_0$ at initial yielding point | |
$A_o$ | Ratio of saturated and initial stress |
Only for the choice of saturated expansion form, meaning NPOINT = 2 or 4) | |
$\sigma_{po}$ | Yield limit for three-terms kernal function |
$E_{tpo}$ | Yield limit for three-terms kernal function |
Dam | Parameter of damage model |
Edam | Parameter of damage model |
Rdam | Parameter of damage model \[D(\zeta)=Dam\;e^{-Edam\;.\;\zeta\;.\;Rdam}\] |
4 for plane state
The stresses are the components of CAUCHY stress tensor in global (X,Y,Z) coordinates.
SIG(1) | $\sigma_{xx}$ |
SIG(2) | $\sigma_{yy}$ |
SIG(3) | $\sigma_{xy}$ |
SIG(4) | $\sigma_{zz}$ |
21
Q(1) | = 1 : Plane strain |
Circumferential strain rate ($\dot{\varepsilon}_{\theta}$) in axisymmetrical state | |
Q(2) | Current yield limit in tension |
Q(3) | = 0 : Current stress state is elastic |
= 1 : Current stress state is plastic | |
Q(4) | = 0 : Loading occurs |
= 1 : Neutral loading occurs | |
Q(5) | Equivalent plastic strain ($\bar{\varepsilon}^p$) |
Q(6) | Internal time $\zeta$ |
Q(7) | Current kernal function's value $f_n$ |
Q(8) | Current derived kernal function's value $df_n$ |
Q(9)$\rightarrow$Q(20) | Current back stresses |
Q(21) | Current damage coefficient |