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CHAB

Description

Chaboche elasto-visco-plastic constitutive model with thermal and cyclic effects for solid elements at constant or variable temperatures with damage computation.
The model is highly adjustable and can be used for very simple laws (elastic, bilinear plasticity) as well as for more complex behaviors (visco-plasticity, isotropic hardening, kinematic hardening, cyclic hardening, …)

Implemented by: Hélène Morch, 2016-2019

Files

Prepro: LCHAB.F
Lagamine: CHAB.F, CHABDAM.F

The model

The Chaboche model is a viscoplastic constitutive model that allows thermo-mechanical cyclic analysis of solids.

The viscosity function of the model is the Norton-Hoff equation: \[\dot{p}=\left<\frac{\sigma_v}{K}\right>^n \] Where:

  • $\dot{p}$ is the plastic strain rate norm
  • $\left<x\right>= \begin{cases} x & \text{if } x>0 \\ 0 & \text{if } x\leq 0 \end{cases}$
  • $\sigma_v=\Vert \underline{\sigma}-\underline{X} \Vert -R-\sigma_Y$

Parameter $K$ can be put to a value close to 0 to model elasto-plasticity (without viscous effects).
$R$ is the isotropic hardening variable, which evolves with the plastic strain rate: \[ \dot{R}=b(Q-R)\dot{p}\]

The back-stress $\underline{X}$ controls kinematic hardening. In the Chaboche model, the back-stress is determined through the summation of Armstrong-Fredericks equations: \[\underline{X}=\displaystyle\sum_{i=1}^{nAF} \underline{X}_i\] \[\underline{\dot{X}}_i=\frac{2}{3}C_i\underline{\dot{\varepsilon}}^p-\gamma_i(\underline{X}_i-\underline{Y}_i)\dot{p}-b_i\|\underline{X}_i\|^{r_i-1}\underline{X}_i+\frac{1}{C_i}\frac{dC_i}{dT}\dot{T}\underline{X}_i\]

The parameter $\gamma_i$ can be made to evolve in order to take into account cyclic hardening of the material: \[\dot{\gamma_i}=D_{\gamma_i}(\gamma_i^0-\gamma_i)\dot{p}\] \[\gamma_i^0=a_{\gamma_i}+b_{\gamma_i}\exp(-c_{\gamma_i}q)\]

Where $q$ is the radius of the plastic strain memory surface.

In the Armstrong-Fredericks equations, a modification tensor $\underline{Y}_i$ can be used to model mean stress evolution. This tensor evolves with respect to the norm of the back-stress: \[\dot{\underline{Y}}_i=-\alpha_{b,i}\left(\frac{3}{2}Y_{st,i}\frac{\underline{X}_i}{\|\underline{X}_i\|}+\underline{Y}_i\right)\|\underline{X}_i\|^{r_i}\]

Availability

Plane stress state NO
Plane strain state NO
Axisymmetric state NO
3D state YES
Generalized plane state NO

Input file

Parameters defining the type of constitutive law

(2I5, 60A1)
ILLaw number
ITYPE 271
COMMENT Any comment (up to 60 characters) that will be reproduced on the output listing

Integer parameters

(9I5)
NTEMP number of temperatures at which material data is given
IANISOTH = 1 if effect of maximum temperature in the loading history taken into account
= 0 else
MAXITER Maximum number of iterations for Newton-Raphson convergence (default = 25)
NAF Number of Armstrong-Fredericks equations used to define the back-stress X (minimum value=1)
NAFY Number of Armstrong-Fredericks equations taking into account evolution of the mean stress
NAFcyc Number of Armstrong-Fredericks equations taking into account cyclic hardening
NINTV number of time sub-steps in the material law
IDAM = 1 for isotropic uncoupled damage computation
= 2 for isotropic coupled damage computation
= 0 for no damage computation
IARRH = 1 expression of static recovery parameters using Arrhenius law
= 2 expression of all parameters as exponential function of temperature
= 0 parameters are interpolated linearly between to defined temperatures
ILCF = 1 computation of stress amplitude for cyclic loading (for Optim)

Real parameters

Parameters not depending on the temperature

Line 1 (4G10)
ETA strain memory rate
PRECNR precision for convergence of the Newton-Raphson algorithm (default=10-4)
PERIOD period of cyclic loading (only if ILCF=1)
tHHold time in the cyclic loading (only if ILCF=1)
If IANISOTH=1 - Line 2 (3G10)
BDGRate parameter controlling the evolution of Dγ
be Rate of evolution of the weighted average factor fe
fes Saturation value of the weighted average factor fe
If IDAM≠0 - Line 3 (2G10)
h micro-defects closure parameter (=0.2 in general for metals ; 1 if micro-defects closure not taken into account)
Dc Critical damage value (<1)
τ Specific time for the appearance of creep
If IARRH=1 - Line 3+i (i=1:nAF) (2G10)*i
Ai coefficient for expression of bi using Arrhenius equation
Bi coefficient for expression of bi using Arrhenius equation

Temperature-dependent parameters - Case where iarrh=0 or iarrh=1

2+IANISOTH+NAF+NAFcyc+NAFY lines repeated NTEMP times
:!: Parameters must be introduced by increasing temperature order

Line 1 (4G10)
TTemperature
E Young's modulus at temperature T
NU Poisson's ratio at temperature T
αThermal expansion coefficient at temperature T
NB: in the preprocessor, the thermal expansion coefficient is transformed in its enthalpic formulation
Line 2 (5G10)
σYYield stress at temperature T
b Rate of isotropic hardening
NB: to avoid convergence issues, b should be constant with temperature
Q Total isotropic saturation size of the yield surface
NB: to avoid convergence issues, Q should be constant with temperature
K Drag stress in Norton-Hoff law
n Viscosity exponent for Norton-Hoff law
Line 2+i (4G10) repeated NAF times (i=1:NAF)
CiPrager's linear coefficient in the ith A-F equation
γi Dynamic recovery parameter in the ith A-F equation
bi Static recovery parameter in the ith equation
ri Static recovery exponent in the ith equation
Line 2+NAF+i (4G10) repeated NAFcyc times (i=1:NAFcyc)
DγiParameter controlling the evolution of γi with increment of plastic strain norm
AγiParameter controlling the saturation value of γi
BγiParameter controlling the saturation value of γi
CγiParameter controlling the saturation value of γi
Line 2+NAF+NAFcyc+i (4G10) repeated NAFY times (i=1:NAFY)
αbi Rate of evolution of the mean stress tensor Yi
Yst,i Saturation value of the mean stress tensor Yi
If IDAM=1 - Line 2+NAF+NAFcyc+NAFY (8G10)
AParameter of correction in the energy stored by hardening
mExponent parameter of correction in the energy stored by hardening
wDStored energy threshold for damage initiation
SfFatigue damage parameter
expsfFatigue damage exponent parameter
ScCreep damage parameter
expscCreep damage exponent
kKachanov creep damage exponent

Temperature-dependent parameters - Case where iarrh=2

Parameters in this case follow an exponential law of the type: \[P(T)=A_P(1-B_P*\exp(\frac{T}{C_P}))\]

Line 1 (6G10)
AEYoung modulus parameter
BEYoung modulus parameter
CEYoung modulus parameter
AnuPoisson ratio parameter
BnuPoisson ratio parameter
CnuPoisson ratio parameter
Line 2 (6G10)
AαDilatation coefficient parameter
BαDilatation coefficient parameter
CαDilatation coefficient parameter
AσYYield stress parameter
BσYYield stress parameter
CσYYield stress parameter
Line 3 (6G10)
AKDrag stress parameter
BKDrag stress parameter
CKDrag stress parameter
AnNorton coefficient parameter
BnNorton coefficient parameter
CnNorton coefficient parameter
Line 4 (2G10)
b Rate of isotropic hardening
Q Total isotropic saturation size of the yield surface
Line 5 (6G10)
BCiParameter for Ci ∀i
CCiParameter for Ci ∀i
BγiParameter for γi ∀i
CγiParameter for γi ∀i
BbiParameter for bi ∀i
CbiParameter for bi ∀i
Line 5+i (4G10) repeated NAF times (i=1:NAF)
ACiPrager's linear coefficient in the ith A-F equation
Aγi Dynamic recovery parameter in the ith A-F equation
Abi Static recovery parameter in the ith equation
ri Static recovery exponent in the ith equation
laws/chab.1551707801.txt.gz · Last modified: 2020/08/25 15:34 (external edit)